diff --git a/.DS_Store b/.DS_Store new file mode 100644 index 00000000..aae78760 Binary files /dev/null and b/.DS_Store differ diff --git a/_config.yml b/_config.yml index b40fbc65..fe441d96 100644 --- a/_config.yml +++ b/_config.yml @@ -4,7 +4,7 @@ email: suave-developers@lists.stanford.edu description: > # this means to ignore newlines until "baseurl:" A multi-fidelity conceptual design environment. Its purpose is to credibly produce conceptual-level design conclusions for future aircraft incorporating advanced technologies. baseurl: "" # the subpath of your site, e.g. /blog/ -url: "http://suavecode.github.io/" # the base hostname & protocol for your site +url: "https://suavecode.github.io/" # the base hostname & protocol for your site github_username: suavecode travis_username: suavecode permalink: /:title diff --git a/_includes/footer.html b/_includes/footer.html deleted file mode 100644 index 7145cff0..00000000 --- a/_includes/footer.html +++ /dev/null @@ -1,23 +0,0 @@ - - - diff --git a/_includes/head.html b/_includes/head.html deleted file mode 100644 index fe8e0638..00000000 --- a/_includes/head.html +++ /dev/null @@ -1,15 +0,0 @@ - - - - - - {% if page.title %}{{ page.title }} - {{ site.title }}{% else %}{{ site.title }}{% endif %} - - - - - - - - - diff --git a/_includes/header.html b/_includes/header.html deleted file mode 100644 index cfe381f7..00000000 --- a/_includes/header.html +++ /dev/null @@ -1,27 +0,0 @@ - diff --git a/_includes/left-nav.html b/_includes/left-nav.html deleted file mode 100644 index 658a0999..00000000 --- a/_includes/left-nav.html +++ /dev/null @@ -1,19 +0,0 @@ -   - - -
-

{{ site.greetings }}

- {{ site.description | markdownify }} -
- - diff --git a/_includes/main-content-footer.html b/_includes/main-content-footer.html deleted file mode 100644 index 15026897..00000000 --- a/_includes/main-content-footer.html +++ /dev/null @@ -1,34 +0,0 @@ - diff --git a/_layouts/awesome.html b/_layouts/awesome.html deleted file mode 100644 index f3f94efb..00000000 --- a/_layouts/awesome.html +++ /dev/null @@ -1,29 +0,0 @@ - - - {% include head.html %} - - - - -
-
- -
- {{ content }} - -
- -
-
- - - {% include footer.html %} - - - - diff --git a/_layouts/default.html b/_layouts/default.html deleted file mode 100644 index 158a7dab..00000000 --- a/_layouts/default.html +++ /dev/null @@ -1,20 +0,0 @@ - - - - {% include head.html %} - - - - -
-
- {{ content }} -
-
- - {% include footer.html %} - - - - - diff --git a/_layouts/page.html b/_layouts/page.html deleted file mode 100644 index c6801340..00000000 --- a/_layouts/page.html +++ /dev/null @@ -1,22 +0,0 @@ ---- -layout: awesome ---- -
- -
- -
-
-

{{ page.title }}

-

{{ page.subtitle }}

-
-
- -
- {{ content }} -
- - - - -
diff --git a/_layouts/post.html b/_layouts/post.html deleted file mode 100644 index e9c0b1da..00000000 --- a/_layouts/post.html +++ /dev/null @@ -1,35 +0,0 @@ ---- -layout: awesome ---- -
- -
- -
-
-

{{ page.title }}

-
-
- -
- {{ content }} -
- -
-
- - -
- -
diff --git a/_sass/_base.scss b/_sass/_base.scss deleted file mode 100644 index 7c3698ca..00000000 --- a/_sass/_base.scss +++ /dev/null @@ -1,332 +0,0 @@ -/** - * DEFAULTS - */ -$base-font-family: 'Open Sans', sans-serif; -$base-font-size: 16px; -$base-line-height: 1.5em; - -$content-width: 960px; -$spacing-unit: 0px; - -$nav-width: 320px; -$default-padding: 24px; -$default-margin-bottom: 44px; - -/* COLORS */ -$red: #8c1515; -$white: #ffffff; -$black: #000000; -$dark-grey: lighten($black, 10%); -$light-grey: lighten($black, 90%); -$burnt-red: #B3995D; - -/** - * Reset some basic elements - */ -body, h1, h2, h3, h4, h5, h6, -p, blockquote, pre, hr, -dl, dd, ol, ul, figure { - margin: 0; - padding: 0; -} - -hr { - margin-bottom: 24px; - border: 0; - height: 1px; - background-color: #000000; - opacity: 0.2; -} - - - -/** - * Basic styling - */ -body { - font-family: $base-font-family; - font-size: $base-font-size; - line-height: $base-line-height; - font-weight: 500; - color: $text-color; - background-color: $background-color; - @media screen and (min-width: 960px) { - background: url('/images/bg.jpg') top center repeat-y; - } - -webkit-text-size-adjust: 100%; -} - - - -/** - * Set `margin-bottom` to maintain vertical rhythm - */ -h1, h2, h3, h4, h5, h6, -p, blockquote, pre, -ul, ol, dl, figure, -%vertical-rhythm { - margin-bottom: 24px; -} - - - -/** - * Images - */ -img { - max-width: 100%; - vertical-align: middle; -} - - - -/** - * Figures - */ -figure > img { - display: block; -} - -figcaption { - font-size: $small-font-size; -} - - - -/** - * Lists - */ -ul, ol { - margin-left: 0px; - margin-right: 0px; -} - -li { - > ul, - > ol { - margin-bottom: 0; - } -} - - - -/** - * Headings - */ -h1, h2 { - font-weight: 700; -} - -h3, h4, h5, h6 { - font-weight: 700; -} - - - -/** - * Links - */ -a { - color: $burnt-red; - text-decoration: none; - //font-weight: bold; - -/* &:visited { - color: darken($burnt-red, 30%); - } -*/ - - &:hover { - color: $red; - text-decoration: underline; - } -} - -a.social-media-link{ - &:hover { - text-decoration: none; - } -} - - -/** - * Blockquotes - */ -blockquote { - border-left: 4px solid $grey-color-light; - padding: 6px 12px; - margin: 24px; - font-size: 14px; - font-weight: normal; - line-height: 21px; - opacity: 0.8; - - > :last-child { - margin-bottom: 0; - } -} - - -article { - margin-bottom: 120px; - - &.content { - ul, ol { - margin-left: 20px; - } - } - - a { - padding: 0px 0px; - } -} - - - -/** - * Code formatting - */ -pre, -code { - font-size: 15px; - font-weight: normal; - border: 1px solid $grey-color-light; - border-radius: 3px; - background-color: #eef; -} - -code { - padding: 1px 5px; -} - -pre { - padding: 8px 12px; - overflow-x: auto; - - > code { - border: 0; - padding-right: 0; - padding-left: 0; - } -} - - - -/** - * Wrapper - */ -.wrapper { - max-width: -webkit-calc(#{$content-width} - (#{$spacing-unit} * 2)); - max-width: calc(#{$content-width} - (#{$spacing-unit} * 2)); - margin-right: auto; - margin-left: auto; - padding-right: $spacing-unit; - padding-left: $spacing-unit; - @extend %clearfix; - - @include media-query($on-laptop) { - max-width: -webkit-calc(#{$content-width} - (#{$spacing-unit})); - max-width: calc(#{$content-width} - (#{$spacing-unit})); - padding-right: $spacing-unit / 2; - padding-left: $spacing-unit / 2; - } - - -} - -.border-box { - box-sizing: border-box; - -moz-box-sizing: border-box; - -webkit-box-sizing: border-box; -} - -@mixin round-corner($radius) { - -webkit-border-radius: $radius; - -moz-border-radius: $radius; - -ms-border-radius: $radius; - border-radius: $radius; -} - -.valign { - position: relative; - top: 50%; - - transform: translateY(-50%); - -webkit-transform: translateY(-50%); - -ms-transform: translateY(-50%); -} - -/** - * Clearfix - */ -%clearfix { - - &:after { - content: ""; - display: table; - clear: both; - } -} - -/** - * Icons - */ -.icon { - - > img { - display: inline-block; - width: 32px; - height: 32px; - vertical-align: middle; - } -} - -.btn { - color: $white !important; - display: inline-block; - padding: 6px 12px; - font-size: 14px; - text-decoration: none !important; - background-color: $red; - border: 2px solid $red; - @include round-corner(3px); - - &:hover { - background-color: lighten($red, 4%); - } - - &.active { - background-color: lighten($white, 17%); - color: $red !important; - } -} - - -::-webkit-scrollbar { - width: 8px; - height: 6px; -} - -::-webkit-scrollbar-button:start:decrement, -::-webkit-scrollbar-button:end:increment { - display: block; - height: 0px; -} - -::-webkit-scrollbar-button:vertical:increment -::-webkit-scrollbar-button:vertical:decrement { - background-color: #eee; -} - -::-webkit-scrollbar-track-piece { - background-color: #eee; - -webkit-border-radius: 0px; - border: 1px solid #ccc; -} - -::-webkit-scrollbar-thumb:vertical { - height: 50px; - background-color: #ccc; - -webkit-border-radius: 3px; -} - diff --git a/_sass/_layout.scss b/_sass/_layout.scss deleted file mode 100644 index e846d120..00000000 --- a/_sass/_layout.scss +++ /dev/null @@ -1,305 +0,0 @@ -/** - * Side Nav - */ -.left-nav { - position: fixed; - top: 0; - bottom: 0; - font-weight: 400; - color: $dark-grey; - width: $nav-width; - float: left; - padding: $default-padding; - text-align: center; - overflow: auto; - margin: 0px; - padding: 0px; - - @extend .border-box; - - .greetings { - font-size: 24px; - color: $red; - margin-bottom: $default-margin-bottom; - } - - .logo { - margin: auto auto; - width: 200px; - height: 222px; - display: block; - margin-bottom: $default-margin-bottom; - position: relative; - top: 30px; - - - img { - width: 100%; - height: 90%; - } - - span { - display: inline-block; - text-indent: -10000px; - } - } - - strong { - color: $red; - font-weight: bold; - padding: 2px 5px; - border-bottom: 1px solid lighten($red, 20%); - } - - section { - margin-bottom: $default-margin-bottom; - } - - ul { - list-style-type: none; - } - - .main-nav { - h5 { - color: lighten($red, 7%); - font-size: 12px; - margin-bottom: 24px; - } - - ul { - li { - margin-bottom: 10px; - - a { - width: 125px; - } - - @media screen and (max-width: 960px) { - display: inline; - margin-right: 12px; - } - - @media screen and (max-width: 580px) { - display: block; - width: 100%; - a { - width: 90%; - } - } - } - } - } - - - @media screen and (max-width: 960px) { - width: 100%; - float: none; - position: relative; - background-color: #F6F6F6; - border-bottom: 1px solid #CFCFCF; - } - - footer { - margin-top : 35px; - } - -} - - - -/** - * Main Content - */ -.main-content { - position: relative; - overflow: auto; - float: left; - width: 648px; - margin: 0px; - padding: 0px; - margin-left: $nav-width; - - @extend .border-box; - - @media screen and (max-width: 960px) { - width: 100%; - float: none !important; - margin-left: 0; - } - - footer { - width: 100%; - bottom: 24px; - font-weight: 400; - color: lighten($black, 60%); - text-align: center; - padding: 24px; - - margin-top: 88px; - @extend .border-box; - - hr { - background-color: lighten($black, 50%); - } - - ul { - margin-bottom: 24px; - li { - display: inline; - margin-right: 6px; - - a { - text-decoration: none !important; - } - a:hover { - opacity: 0.8; - } - } - } - - @media screen and (min-width: 960px) { - width: 264px; - position: fixed; - bottom: 0; - margin-top: 0px; - margin-left: -290px; - } - } - - -} - - - -/** - * hero - */ -.hero { - position: relative; - height: 160px; - text-align: center; - font-weight: bold; - - .title { - font-family: "Palatino Linotype", "Book Antiqua", Palatino, serif; - font-size: 48px; - margin-top: 0px; - margin-bottom: 4px; - line-height: 1.2em; - font-weight: normal; - - @media screen and (max-width: 600px) { - font-size: 38px; - } - } - - .subtitle { - color: $red; - font-size: 14px; - text-transform: uppercase; - } -} - -/** - * content - */ -.content { - padding: 24px; - - h1, h2 { - font-weight: normal; - } - h1 { - text-align: center; - font-size: 36px; - } - h2 { - font-size: 32px; - } - - p { - color: $dark-grey - //color: lighten($black, 40%) - } - -} - - -/** - * post - */ -.post { - list-style-type: none; - overflow: auto; - border-bottom: 1px solid $light-grey; - padding: 4px 0; - - &:last-child { - border-bottom: 0; - } - - > div { - float: left; - padding: 2px; - @extend .border-box; - - &.span-1 { - font-size: 11px; - width: 90px; - font-weight: bold; - text-transform: uppercase; - overflow: hidden; - &.comment-count { - width: 60px; - a, a:active, a:visited { - color: $red; - text-decoration: none !important; - } - } - - } - - &.span-10 { - width: 420px; - } - - @media screen and (max-width: 960px) { - &.span-10 { - float: none; - clear: both; - width: 100%; - } - } - } - - .post-date { - color: lighten($black, 60%); - } - - .post-link { - color: $black; - font-size: 18px; - font-weight: 700; - - &:hover { - color: $red; - } - } - -} - - -.disqus-comment-count { -} - -.comment-icon { - width: 16px; - height: 16px; - margin-left: 3px; -} - -em img { - float: left; - margin-right: 20px; - margin-bottom: 20px; -} diff --git a/_sass/_syntax-highlighting.scss b/_sass/_syntax-highlighting.scss deleted file mode 100644 index e36627da..00000000 --- a/_sass/_syntax-highlighting.scss +++ /dev/null @@ -1,67 +0,0 @@ -/** - * Syntax highlighting styles - */ -.highlight { - background: #fff; - @extend %vertical-rhythm; - - .c { color: #998; font-style: italic } // Comment - .err { color: #a61717; background-color: #e3d2d2 } // Error - .k { font-weight: bold } // Keyword - .o { font-weight: bold } // Operator - .cm { color: #998; font-style: italic } // Comment.Multiline - .cp { color: #999; font-weight: bold } // Comment.Preproc - .c1 { color: #998; font-style: italic } // Comment.Single - .cs { color: #999; font-weight: bold; font-style: italic } // Comment.Special - .gd { color: #000; background-color: #fdd } // Generic.Deleted - .gd .x { color: #000; background-color: #faa } // Generic.Deleted.Specific - .ge { font-style: italic } // Generic.Emph - .gr { color: #a00 } // Generic.Error - .gh { color: #999 } // Generic.Heading - .gi { color: #000; background-color: #dfd } // Generic.Inserted - .gi .x { color: #000; background-color: #afa } // Generic.Inserted.Specific - .go { color: #888 } // Generic.Output - .gp { color: #555 } // Generic.Prompt - .gs { font-weight: bold } // Generic.Strong - .gu { color: #aaa } // Generic.Subheading - .gt { color: #a00 } // Generic.Traceback - .kc { font-weight: bold } // Keyword.Constant - .kd { font-weight: bold } // Keyword.Declaration - .kp { font-weight: bold } // Keyword.Pseudo - .kr { font-weight: bold } // Keyword.Reserved - .kt { color: #458; font-weight: bold } // Keyword.Type - .m { color: #099 } // Literal.Number - .s { color: #d14 } // Literal.String - .na { color: #008080 } // Name.Attribute - .nb { color: #0086B3 } // Name.Builtin - .nc { color: #458; font-weight: bold } // Name.Class - .no { color: #008080 } // Name.Constant - .ni { color: #800080 } // Name.Entity - .ne { color: #900; font-weight: bold } // Name.Exception - .nf { color: #900; font-weight: bold } // Name.Function - .nn { color: #555 } // Name.Namespace - .nt { color: #000080 } // Name.Tag - .nv { color: #008080 } // Name.Variable - .ow { font-weight: bold } // Operator.Word - .w { color: #bbb } // Text.Whitespace - .mf { color: #099 } // Literal.Number.Float - .mh { color: #099 } // Literal.Number.Hex - .mi { color: #099 } // Literal.Number.Integer - .mo { color: #099 } // Literal.Number.Oct - .sb { color: #d14 } // Literal.String.Backtick - .sc { color: #d14 } // Literal.String.Char - .sd { color: #d14 } // Literal.String.Doc - .s2 { color: #d14 } // Literal.String.Double - .se { color: #d14 } // Literal.String.Escape - .sh { color: #d14 } // Literal.String.Heredoc - .si { color: #d14 } // Literal.String.Interpol - .sx { color: #d14 } // Literal.String.Other - .sr { color: #009926 } // Literal.String.Regex - .s1 { color: #d14 } // Literal.String.Single - .ss { color: #990073 } // Literal.String.Symbol - .bp { color: #999 } // Name.Builtin.Pseudo - .vc { color: #008080 } // Name.Variable.Class - .vg { color: #008080 } // Name.Variable.Global - .vi { color: #008080 } // Name.Variable.Instance - .il { color: #099 } // Literal.Number.Integer.Long -} diff --git a/_site/CNAME b/_site/CNAME deleted file mode 100644 index c952eece..00000000 --- a/_site/CNAME +++ /dev/null @@ -1 +0,0 @@ -suave.stanford.edu \ No newline at end of file diff --git a/_site/css/main.css b/_site/css/main.css deleted file mode 100644 index 0e80c559..00000000 --- a/_site/css/main.css +++ /dev/null @@ -1,591 +0,0 @@ -.verticalLineR { - border-right: 1px solid #CCCCCC; - height: 150%; } - -.verticalLineL { - border-left: 1px solid #CCCCCC; - height: 100%; } - -table { - border-collapse: collapse; - border-spacing: 0; - border: 1px solid #666666; - width: 70%; - margin-left: 15%; - margin-right: 15%; } - -th { - border: 1px solid #666666; - padding: 5px; } - -td { - border: 1px solid #666666; - padding: 5px; } - -/** - * DEFAULTS - */ -/* COLORS */ -/** - * Reset some basic elements - */ -body, h1, h2, h3, h4, h5, h6, -p, blockquote, pre, hr, -dl, dd, ol, ul, figure { - margin: 0; - padding: 0; } - -hr { - margin-bottom: 24px; - border: 0; - height: 1px; - background-color: #000000; - opacity: 0.2; } - -/** - * Basic styling - */ -body { - font-family: "Open Sans", sans-serif; - font-size: 16px; - line-height: 1.5em; - font-weight: 500; - color: #111; - background-color: #fdfdfd; - -webkit-text-size-adjust: 100%; } - @media screen and (min-width: 960px) { - body { - background: url("/images/bg.jpg") top center repeat-y; } } - -/** - * Set `margin-bottom` to maintain vertical rhythm - */ -h1, h2, h3, h4, h5, h6, -p, blockquote, pre, -ul, ol, dl, figure, -.highlight { - margin-bottom: 24px; } - -/** - * Images - */ -img { - max-width: 100%; - vertical-align: middle; } - -/** - * Figures - */ -figure > img { - display: block; } - -figcaption { - font-size: 14px; } - -/** - * Lists - */ -ul, ol { - margin-left: 0px; - margin-right: 0px; } - -li > ul, -li > ol { - margin-bottom: 0; } - -/** - * Headings - */ -h1, h2 { - font-weight: 700; } - -h3, h4, h5, h6 { - font-weight: 700; } - -/** - * Links - */ -a { - color: #B3995D; - text-decoration: none; - /* &:visited { - color: darken($burnt-red, 30%); - } - */ } - a:hover { - color: #8c1515; - text-decoration: underline; } - -a.social-media-link:hover { - text-decoration: none; } - -/** - * Blockquotes - */ -blockquote { - border-left: 4px solid #e8e8e8; - padding: 6px 12px; - margin: 24px; - font-size: 14px; - font-weight: normal; - line-height: 21px; - opacity: 0.8; } - blockquote > :last-child { - margin-bottom: 0; } - -article { - margin-bottom: 120px; } - article.content ul, article.content ol { - margin-left: 20px; } - article a { - padding: 0px 0px; } - -/** - * Code formatting - */ -pre, -code { - font-size: 15px; - font-weight: normal; - border: 1px solid #e8e8e8; - border-radius: 3px; - background-color: #eef; } - -code { - padding: 1px 5px; } - -pre { - padding: 8px 12px; - overflow-x: auto; } - pre > code { - border: 0; - padding-right: 0; - padding-left: 0; } - -/** - * Wrapper - */ -.wrapper { - max-width: -webkit-calc(960px - (0px * 2)); - max-width: calc(960px - (0px * 2)); - margin-right: auto; - margin-left: auto; - padding-right: 0px; - padding-left: 0px; } - @media screen and (max-width: 800px) { - .wrapper { - max-width: -webkit-calc(960px - (0px)); - max-width: calc(960px - (0px)); - padding-right: 0px; - padding-left: 0px; } } - -.border-box, .left-nav, .main-content, .main-content footer, .post > div { - box-sizing: border-box; - -moz-box-sizing: border-box; - -webkit-box-sizing: border-box; } - -.valign { - position: relative; - top: 50%; - transform: translateY(-50%); - -webkit-transform: translateY(-50%); - -ms-transform: translateY(-50%); } - -/** - * Clearfix - */ -.wrapper:after { - content: ""; - display: table; - clear: both; } - -/** - * Icons - */ -.icon > img { - display: inline-block; - width: 32px; - height: 32px; - vertical-align: middle; } - -.btn { - color: #ffffff !important; - display: inline-block; - padding: 6px 12px; - font-size: 14px; - text-decoration: none !important; - background-color: #8c1515; - border: 2px solid #8c1515; - -webkit-border-radius: 3px; - -moz-border-radius: 3px; - -ms-border-radius: 3px; - border-radius: 3px; } - .btn:hover { - background-color: #9e1818; } - .btn.active { - background-color: white; - color: #8c1515 !important; } - -::-webkit-scrollbar { - width: 8px; - height: 6px; } - -::-webkit-scrollbar-button:start:decrement, -::-webkit-scrollbar-button:end:increment { - display: block; - height: 0px; } - -::-webkit-scrollbar-button:vertical:increment -::-webkit-scrollbar-button:vertical:decrement { - background-color: #eee; } - -::-webkit-scrollbar-track-piece { - background-color: #eee; - -webkit-border-radius: 0px; - border: 1px solid #ccc; } - -::-webkit-scrollbar-thumb:vertical { - height: 50px; - background-color: #ccc; - -webkit-border-radius: 3px; } - -/** - * Side Nav - */ -.left-nav { - position: fixed; - top: 0; - bottom: 0; - font-weight: 400; - color: #1a1a1a; - width: 320px; - float: left; - padding: 24px; - text-align: center; - overflow: auto; - margin: 0px; - padding: 0px; } - .left-nav .greetings { - font-size: 24px; - color: #8c1515; - margin-bottom: 44px; } - .left-nav .logo { - margin: auto auto; - width: 200px; - height: 222px; - display: block; - margin-bottom: 44px; - position: relative; - top: 30px; } - .left-nav .logo img { - width: 100%; - height: 90%; } - .left-nav .logo span { - display: inline-block; - text-indent: -10000px; } - .left-nav strong { - color: #8c1515; - font-weight: bold; - padding: 2px 5px; - border-bottom: 1px solid #df2828; } - .left-nav section { - margin-bottom: 44px; } - .left-nav ul { - list-style-type: none; } - .left-nav .main-nav h5 { - color: #ab1a1a; - font-size: 12px; - margin-bottom: 24px; } - .left-nav .main-nav ul li { - margin-bottom: 10px; } - .left-nav .main-nav ul li a { - width: 125px; } - @media screen and (max-width: 960px) { - .left-nav .main-nav ul li { - display: inline; - margin-right: 12px; } } - @media screen and (max-width: 580px) { - .left-nav .main-nav ul li { - display: block; - width: 100%; } - .left-nav .main-nav ul li a { - width: 90%; } } - @media screen and (max-width: 960px) { - .left-nav { - width: 100%; - float: none; - position: relative; - background-color: #F6F6F6; - border-bottom: 1px solid #CFCFCF; } } - .left-nav footer { - margin-top: 35px; } - -/** - * Main Content - */ -.main-content { - position: relative; - overflow: auto; - float: left; - width: 648px; - margin: 0px; - padding: 0px; - margin-left: 320px; } - @media screen and (max-width: 960px) { - .main-content { - width: 100%; - float: none !important; - margin-left: 0; } } - .main-content footer { - width: 100%; - bottom: 24px; - font-weight: 400; 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Develop

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Make things more awesome

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If you want to make changes to SUAVE source, or contribute new functionalities back to the community, this is the page for you!

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Background

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SUAVE is developed via GitHub, and this page will describe how to get started. There is also a list of open topics available for contribution if you’re looking for ideas to get started.

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As a developer, you’ll want to fork SUAVE to your personal account. This creates a copy of the whole SUAVE repository, including all past versions, inside your GitHub account. Generally you’ll want to start from the develop branch, but you can check with the developers if you think it would be more appropriate to work on a feature branch.

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Development is done on separate branches. Our branching model is very similar to this one. Basically there are three types of branches.

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  • master – stable, latest release and fixes
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  • feature-* – feature specific branches, using names with underscores, check with the developer email list if you think this a better place to contribute
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SUAVE merges new code contributions through pull requests. As you make changes to your copy of SUAVE, you’ll upload them to your GitHub fork, and then when they’re ready for review you’ll submit them for merge via pull request.

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Style Guide

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SUAVE is built on a slightly modified PEP8 style guide, with changes made to implement a data-oriented view of the code. To help support discovering code, the SUAVE folder structure explicitly mirrors the package structure. Flexibility of the package structure is important, so in general all objects live in their own file, with the same file name as the object name. In order to maintain a separation between Analysis and Data structures, there are often parallel package trees inside the main branches of the package, like SUAVE.Methods.Aerodynamics and SUAVE.Analysis.Aerodynamics. Where possible the names of fields that live in the SUAVE package are written out verbosely, avoiding jargon built on mathematical variable names or acronyms.

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A full description of the style of SUAVE can be found on the Guides page.

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Templates for new methods and objects can be found in the SUAVE repo’s templates folder.

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Prerequisites

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In addition to the package dependencies listed on the download page, you will need to install git.

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Git-Client

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Git is an advanced distributed version control system. It is the core of the majority of current open source projects. Here are some instructions for installing git on your machine.
-linux , mac , windows , more info

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There are several GUI’s available to help manage the repository. On Windows TortoiseGit is a useful one.

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If you’re going to install TortoiseGit on windows, when installing the git client (MsysGit), uncheck “Windows Explorer Integration”. And when installing TortoiseGit, select “Checkout as-is, Unix-style line endings”

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Once you’ve installed git, there a few post-install commands to run, documented here.

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GitHub Account

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GitHub is a hosting service for git projects. SUAVE’s repository is located here.

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If you don’t have a github account already, go ahead and sign up!

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Then, go to the SUAVE github repo at github.com/suavecode/SUAVE and check out the code! If you wouldn’t mind, tick the “Watch” and “Star” buttons at the top-right of the page, if you think this is a useful repo.

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Developer Installation

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Time to pull code. If you had previously installed a release distribution according to the download page, you’ll want to uninstall the existing package first.

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  1. Go to the SUAVE github repo.
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  3. To get your own copy of the source, with links into real-time updates, you need to fork the repo. This button is on the top-right of the page too.
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  5. This will copy the repo and take you to your fork, notice that your web-browser’s URL has changed to include your username.
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  7. Now you can clone your fork to your computer. Find the clone url of your fork on the right hand side of the page and copy it. You can use the https url.
    clone
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  9. Open a command prompt, in a directory that you want to start the repository (for example in the SUAVE_Project folder), and run the git clone command
    git clone <git url>
    Now you should have the source code.
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  11. Change directory into the trunk folder and run a developer installation command.
    python setup.py develop
    Now you have a developer version of SUAVE installed! You can make changes to the source in this directory and the changes will appear the next time you run python, without having to rebuild or reinstall.
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  13. Test the installation by changing to any other directory, then start a python shell, and run the command
    >>> import SUAVE
    >>> print SUAVE.__file__
    This should print the file path to the SUAVE package init.py file in your trunk directory.
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Some Notes

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  • You may need to run a sudo (super user do) command to install SUAVE when working on linux or mac systems: sudo python setup.py develop
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Managing your repository

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As you make changes to your code, you’ll want to add and commit them to your clone, and push them to your fork. You’ll fetch changes from the upstream remote (the suavecode repository), and merge them into your clone. To send your changes back to the upstream repository, you can submit a pull-request.

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Setting the upstream

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Below is a summary of setting the upstream remote. There are a good references for this process here and here, and more via a google search for “git update fork”.

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  1. Inspect your current “remote”, this is the url of the repository to which your clone listens. -In the directory for the cloned repo, type
    git remote –v and it should show the “origin” directory for “fetch” and “push”. These are the remote urls for your own fork.
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  3. Add an upstream remote to the main suavecode/SUAVE repository using
    git remote add upstream https://github.com/suavecode/SUAVE.git
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  5. Run git remote -v again to see the new remotes.
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  7. Finally, download the code for the upstream remote with
    git fetch upstream.
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Changing branches

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You should work on the develop branch in general, it will have the most updated changes from the community.

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  1. Inspect your branches with git branch -a. You’ll see all the branches, for both upstream and origin. Generally you should only work off the origin branches
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  3. Start a new branch with git branch develop origin/develop. This comand aliases the branch “origin/develop” with the name “develop”.
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  5. Checkout the branch, git checkout develop.
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  7. You can see your current branch with, git branch, the one you have checked out will have a star next to it.
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  9. Commit all your changes to the current branch before checking out another branch, otherwise the changes will be lost.
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  11. To dump any changes that you don’t want, git stash, will be helpful.
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Store changes to your GitHub fork

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  1. Edit the code as you need on your machine
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  3. Inspect git’s view of the changes you’ve made with git status. This shows what files are new, changed and not yet part of the repo’s history.
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  5. Add the changed files to your commit with git add <path to file>, or to add all the changes with git add -a (be careful with this one). The add command does not make the changes part of your repo’s history! You can do multiple add commands for example.
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  7. Commit them to the history on your machine with
    git commit -m 'your message for the commit'
    Make sure to include a nice description. This command only affects your local repository! You can do multiple commits before sending them to the cloud.
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  9. Push the new commits to GitHub with git push origin. This will send all the commits to your fork on GitHub. This serves as a backup copy for you, and is needed to share the changes with the upstream suavecode repository via pull-requests.
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Get new changes from upstream

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In this example the upstream/develop branch is merged into the fork/develop branch.

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  1. Checkout your local develp branch with
    git checkout develop.
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  3. Fetch updates from the upstream repository with
    git fetch upstream.
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  5. Merge the changes from the upstream into your fork with
    git merge upstream/develop.
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  7. Push these changes to your fork on GitHub,
    git push origin master.
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Share your changes with upstream

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This creates a nice documentation of the changes that were made. More detail on pull requests can be found here.

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  1. Commit and push all your changes to your fork on GitHub.
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  3. Open a browser and navigate to your branch on the GitHub website.
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  5. Click the “Compare and Review” button.
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  7. Review the changes for any unexpected differences.
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  11. The devs will take a look and merge the request.
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Background on Git

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Git is an open source program for tracking changes in text files. It was written by the author of the Linux operating system, and is the core technology that GitHub, the social and user interface, is built on top of it.

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The term version control is used in Git and other such programs, and refers exactly to what it reads. It allows a group of software developers (the group may comprise one, many or “more than many”) to keep track of changes being made to the software’s code (i.e., versions of code) and have control on the changes (“versions”). This control helps the programmer(s) to decide

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  • Which versions can be put on the sidelines since they are a brainchild of a super whiz programmer who is simply playing with some cool ideas
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  • Which versions are now obsolete since there are alternate and better software/code available to do the same job (these versions are usually nixed!)
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  • Which versions are too new and require a lot of related work to be done before they can even be brought up for discussions at the weekly meetings
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  • And so on
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Bottom line is that the concept of version control is mainly to help software development by not losing one’s grip on reality and the primary objectives of the software being developed!

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For those interested in learning more about how version control systems (VCSs) such as Git work, refer to

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In addition to Git, there are other popular VCSs such as SVN (http://tortoisesvn.net/ and https://subversion.apache.org/), with their own sets of pros and cons. However, Git was chosen for SUAVE because SUAVE developers felt it can be easily implemented on Linux, Mac and Windows, and offers them a lot of flexibility and control in terms of developing and maintaining multiple parallel versions (“branches”) with each providing further parallelization (“forks”). For more information about the concepts of branching and forking, refer to http://nvie.com/posts/a-successful-git-branching-model/

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Areas of Development

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Short Term Feature Development

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These are the areas that are under development or suggested for development are available in our Github projects tab. There are two active projects that include feature development. One is the list of items we plan to accomplish for our next release. The other is a general feature development project, which contains features that we would like to have but are not currently priorities for the next release.

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Post to the forum if you’re intersted in working on any of these, or to suggest a new module!

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Long Term Development Goals

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Looking farther into the future, we have some key items envisioned for the next major release of SUAVE. So far these are:

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  • Upgrade to Python 3
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We’re always happy to hear feedback on what our users think is important in this kind of tool, so if you have another idea go ahead and ask about it on our forum.

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Back to Top!

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Documentation

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Everything you ever wanted to know to be SUAVE

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SUAVE is fully documented through doxygen. However, some starter high level documentation is available below.

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Download

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How to download and install this fantastic tool

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Jump in and design! Here are some helpful steps for downloading and installing the code. There are stable releases and beta releases. Also make sure to check out the license under which the code is available.

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Downloading

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SUAVE comes released as a set of project folders ready for learning and exploration.

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Please take a few seconds to register with us by filling out the form on the pages linked below. Upon registration, you’ll be redirected to the appropriate distribution of the software. The information we collect is used only for usage statistics by the development team. You’ll only be contacted for notification of critical bug fixes and major releases. To get more involved in growing the community, definitely check out the forum. Your support is greatly appreciated, it let’s us build a better tool for everyone!

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Stable Release

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Download the latest stable release of SUAVE:
-SUAVE Version 1.0.0

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License

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We want SUAVE to grow with the community, so it’s available under a
LGPL 2.1 License.

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Please if you are interested in re-publishing SUAVE source code as part of a commercial software.

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Tutorials

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We also update our tutorials repository with every release to show new users some of the capabilities and how to use the code. The tutorial files can be found here. If you would like to use these, you may either follow the Github download instructions on the develop page, but using https://github.com/suavecode/Tutorials.git, or you can download the files as a .zip using the “clone or download” button on the Tutorials Github page.

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Installation

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SUAVE is developed primarily on Python 2.7. It’s known to work on versions 2.4 through 2.7. Let us know if you find that it works on additonal versions.

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We strongly recommend using a scientific python distribution like Anaconda or Enthought-Canopy. All the package dependencies like scipy and numpy will come pre-packaged and stuff will just work.

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If you don’t have access to a scientific python distribution, you can install the dependent packages separately. Check out the specific dependencies for more information

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Simple Setup

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Once you’ve downloaded the code and prepared the software requrements, you’re ready to install it into python!

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  1. Download and extract the release archive
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  3. Open the directory SUAVE/trunk
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  5. Open a command prompt in that directory
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  7. Run this command: python setup.py install
    -If you are on a linux or mac, you may need to run
    sudo python setup.py install
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  9. Change to any other folder, open a python shell, and test the new module with the command import SUAVE
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If all goes well, you are now able to import SUAVE into your python projects. If you’ve downloaded the tutorials as well, check out the guides for examples on using thems!

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After trying out the guides you may find you want to make changes to the innards of the package to fit your problem, take a look at the develop notes for how to set this up.

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Have fun!

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If you had trouble installing or need to uninstall, there are some more tips ahead.

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Dependencies

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Below are the packages that SUAVE expects in order to run the tutorial cases. There are links to guides on using package managers for linux and mac, and python installers for windows. If these fail, check out the source forge links for additional installers or source code.

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packagelink
numpylinux, mac, windows, source
scipylinux, mac, windows, source
matplotliblinux, mac, windows, source
piplinux, mac, windows
scikit-learnlinux, mac, windows
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-Note: For the windows installers, you can pick the latest version, for “cp2.7” (C-Python 2.7), for your architecture (32 or 64bit), and for numpy pick the MKL version (it’s faster).
-Note: The pip installer above will also install setuptools, a sub-dependency.

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Dealing with Write Access

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You shouldn’t need this part of the guide, unless you are unable to write-access the python site-packages directory. In that case, you can try these approaches to install SUAVE.

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A. Install to local site-packages

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This involves the user install option
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B. Start a local site-packages folder

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This involves creating a local directory, and setting up your PYTHONPATH environment variable.

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  1. Create a local directory.
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    -~/python-site-packages or
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        - export PYTHONPATH = $PYTHONPATH:~/python-site-packages
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      • And source the bashrc file
        - $ source ~/.bashrc
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        - export PYTHONPATH = $PYTHONPATH:~/python-site-packages
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      • And source the bashrc file
        - $ source ~/.bash_profile
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      • Open the start menu and type “environ”, this opens the environment variable editor
      • -
      • Create or edit the PYTHONPATH “User” environment variable, appending the full path to your custom site-package directory, separating multiple paths with semicolons. For example:
        - %PYTHONPATH%;C:/Users/your-user-name/python-site-packages
      • -
      • After this you’ll need to open a new command line window
      • -
      -
    • -
    -
  4. -
  5. Now Install SUAVE
    -Using the example of the custom directoy ~/python-site-packages:
    -python setup.py install --prefix=~/python-site-packages
  6. -
- -

Additional Install Options

- -

Additional setup options, such as overriding the default install location, can be found with the following commands:
-python setup.py install --help
-python setup.py uninstall --help
-python setup.py develop --help
-python setup.py --help

- -


- -

Un-Installation

- -

SUAVE requires pip to uninstall. An alternate approach is provided further below if pip is not available.

- -

Un-Installation with pip:

- -
    -
  1. Navigate to the SUAVE/trunk directory by command line.
  2. -
  3. Run the uninstall command. (On unix platforms, these commands may require a sudo (‘super-user-do’) call.)
    -python setup.py uninstall
  4. -
- -

Alternate Approach:

-

Use this if you don’t have the pip package.

- -
    -
  1. -

    Find your site-packages folder. - Your site-packages folder is typically located in your python’s install directory, unless you manually created it. You can find it by using the following commands.
    - $ python
    - >>> import site
    - >>> site.getsitepackages()

    -
  2. -
  3. -

    Manually delete any file including the name “SUAVE”.
    -You may also check the file “easy_install.pth”, if it exists, for references to the SUAVE package, and delete them. Never said this would be pretty… However it is a typical uninstall process for python packages.

    -
  4. -
- - -
- - - - -
- - -
- -
-
- - - - - - - - - - diff --git a/_site/doxygen/annotated.html b/_site/doxygen/annotated.html deleted file mode 100644 index 74a63422..00000000 --- a/_site/doxygen/annotated.html +++ /dev/null @@ -1,688 +0,0 @@ - - - - - - - -SUAVE: Class List - - - - - - - - - - - - - - - -
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- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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- - - -
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- -
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- -
- -
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- - -
- -
- -
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Class List
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-
-
Here are the classes, structs, unions and interfaces with brief descriptions:
-
[detail level 12345678]
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
 NSUAVE
 NAnalyses
 NAerodynamics
 NAnalysis
 NAtmospheric
 NCosts
 NEnergy
 NGeometry
 NLoads
 NMission
 NNoise
 NPlanets
 NProcess
 NResults
 NSettings
 NSizing
 NStability
 NStructures
 NSurrogate
 NVehicle
 NWeights
 NAttributes
 NAirports
 NAtmospheres
 NConstants
 NGases
 NLiquids
 NPlanets
 NPropellants
 NComponents
 NComponent
 NConfigs
 NCosts
 NEnergy
 NEnvelope
 NFuselages
 NLanding_Gear
 NLofted_Body
 NMass_Properties
 NPayloads
 NPhysical_Component
 NPropulsors
 NSystems
 NWings
 NCore
 NContainer
 NContainerOrdered
 NData
 NDataOrdered
 NDiffed_Data
 Nredirect
 NInput_Output
 ND3JS
 NXML
 NMethods
 NAerodynamics
 NOptimization
 NNexus
 NPackage_Setups
 NSurrogate_Optimization
 NPlugins
 Npint
 NSizing
 NSizing_Loop
 NSurrogate
 NSurrogate_Problem
 NVehicle
 CCosts
 CVehicle
 CVehicle_Mass_Properties
-
-
-
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-
- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Aerodynamics.AERODAS.AERODAS Member List
-
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AERODAS_1_1AERODAS.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AERODAS_1_1AERODAS.html deleted file mode 100644 index 54099527..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AERODAS_1_1AERODAS.html +++ /dev/null @@ -1,246 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Aerodynamics.AERODAS.AERODAS Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Aerodynamics.AERODAS.AERODAS Class Reference
-
-
-
-Inheritance diagram for SUAVE.Analyses.Aerodynamics.AERODAS.AERODAS:
-
-
- - -SUAVE.Analyses.Aerodynamics.Markup.Markup -SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics -SUAVE.Analyses.Analysis.Analysis - -
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Aerodynamics.Markup.Markup
def __defaults__ (self)
 
def evaluate (self, state)
 
def initialize (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
def __defaults__ (self)
 
def evaluate (self, state)
 
def finalize (self)
 
def compute_forces (self, conditions)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

tag
 
- Public Attributes inherited from SUAVE.Analyses.Aerodynamics.Markup.Markup
tag
 
geometry
 
settings
 
process
 
- Public Attributes inherited from SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
tag
 
geometry
 
settings
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
This is an analysis based on the AERODAS models.
-
-Assumptions:
-None
-
-Source:
-NASA TR: "Models of Lift and Drag Coefficients of Stalled and Unstalled Airfoils in
-  Wind Turbines and Wind Tunnels" by D. A. Spera
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Aerodynamics.AERODAS.AERODAS.__defaults__ ( self)
-
-
This sets the default values and methods for the analysis.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Aerodynamics/AERODAS.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AERODAS_1_1AERODAS.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AERODAS_1_1AERODAS.js deleted file mode 100644 index a6f106a6..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AERODAS_1_1AERODAS.js +++ /dev/null @@ -1,5 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AERODAS_1_1AERODAS = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AERODAS_1_1AERODAS.html#a8e0794e9853d86883cbf0eb613584534", null ], - [ "tag", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AERODAS_1_1AERODAS.html#a1d53bc341fe8ba1800b7f06dd3ba311c", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AERODAS_1_1AERODAS.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AERODAS_1_1AERODAS.png deleted file mode 100644 index feb46d0b..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AERODAS_1_1AERODAS.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL_1_1AVL-members.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL_1_1AVL-members.html deleted file mode 100644 index 6f7edb03..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL_1_1AVL-members.html +++ /dev/null @@ -1,128 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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- -
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-
SUAVE.Analyses.Aerodynamics.AVL.AVL Member List
-
-
- -

This is the complete list of members for SUAVE.Analyses.Aerodynamics.AVL.AVL, including all inherited members.

- - - - - - - - - - - - - - - - - -
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Aerodynamics.AVL.AVL
compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
compute_forces(self, conditions)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
evaluate(self, state)SUAVE.Analyses.Aerodynamics.Markup.Markup
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize (defined in SUAVE.Analyses.Aerodynamics.AVL.AVL)SUAVE.Analyses.Aerodynamics.AVL.AVLstatic
SUAVE::Analyses::Aerodynamics::Markup::Markup.finalize(self)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
geometry (defined in SUAVE.Analyses.Aerodynamics.Markup.Markup)SUAVE.Analyses.Aerodynamics.Markup.Markup
initialize(self)SUAVE.Analyses.Aerodynamics.AVL.AVL
SUAVE::Analyses::Aerodynamics::Aerodynamics::Aerodynamics.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
process (defined in SUAVE.Analyses.Aerodynamics.Markup.Markup)SUAVE.Analyses.Aerodynamics.Markup.Markup
settings (defined in SUAVE.Analyses.Aerodynamics.Markup.Markup)SUAVE.Analyses.Aerodynamics.Markup.Markup
tag (defined in SUAVE.Analyses.Aerodynamics.AVL.AVL)SUAVE.Analyses.Aerodynamics.AVL.AVL
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL_1_1AVL.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL_1_1AVL.html deleted file mode 100644 index 8e14b04d..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL_1_1AVL.html +++ /dev/null @@ -1,288 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Aerodynamics.AVL.AVL Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Aerodynamics.AVL.AVL Class Reference
-
-
-
-Inheritance diagram for SUAVE.Analyses.Aerodynamics.AVL.AVL:
-
-
- - -SUAVE.Analyses.Aerodynamics.Markup.Markup -SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics -SUAVE.Analyses.Analysis.Analysis - -
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def initialize (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Aerodynamics.Markup.Markup
def __defaults__ (self)
 
def evaluate (self, state)
 
def initialize (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
def __defaults__ (self)
 
def evaluate (self, state)
 
def finalize (self)
 
def compute_forces (self, conditions)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

tag
 
- Public Attributes inherited from SUAVE.Analyses.Aerodynamics.Markup.Markup
tag
 
geometry
 
settings
 
process
 
- Public Attributes inherited from SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
tag
 
geometry
 
settings
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
- - - -

-Static Public Attributes

-def finalize = initialize
 
-

Detailed Description

-
This uses AVL to compute lift.
-
-Assumptions:
-None
-
-Source:
-None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Aerodynamics.AVL.AVL.__defaults__ ( self)
-
-
This sets the default values and methods for the analysis.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
-
- -

◆ initialize()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Aerodynamics.AVL.AVL.initialize ( self)
-
-
Initializes the surrogate needed for AVL.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-self.geometry
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Aerodynamics/AVL.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL_1_1AVL.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL_1_1AVL.js deleted file mode 100644 index 435c5626..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL_1_1AVL.js +++ /dev/null @@ -1,6 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL_1_1AVL = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL_1_1AVL.html#a03b5ac9f863b6d6afe9eeacaa287ec6a", null ], - [ "initialize", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL_1_1AVL.html#a831912f73bd7d76d2c627436b6e9149a", null ], - [ "tag", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL_1_1AVL.html#aea9470c5f9d1a9e6abf8eb6ae49c0497", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL_1_1AVL.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL_1_1AVL.png deleted file mode 100644 index 905d28d4..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL_1_1AVL.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL__Inviscid_1_1AVL__Inviscid-members.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL__Inviscid_1_1AVL__Inviscid-members.html deleted file mode 100644 index ee669cd2..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL__Inviscid_1_1AVL__Inviscid-members.html +++ /dev/null @@ -1,138 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid Member List
-
-
- -

This is the complete list of members for SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid, including all inherited members.

- - - - - - - - - - - - - - - - - - - - - - - - - - - -
__defaults__(self)SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid
aerodynamics (defined in SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics)SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics
build_surrogate(self)SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid
compile(self)SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
current_status (defined in SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid)SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid
energies (defined in SUAVE.Analyses.Mission.Segments.Conditions.Basic.Basic)SUAVE.Analyses.Mission.Segments.Conditions.Basic.Basic
evaluate(self, state, settings, geometry)SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid
evaluate_conditions(self, run_conditions)SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid
expand_rows(self, rows)SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
frames (defined in SUAVE.Analyses.Mission.Segments.Conditions.Basic.Basic)SUAVE.Analyses.Mission.Segments.Conditions.Basic.Basic
freestream (defined in SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics)SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics
geometry (defined in SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid)SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid
initialize(self)SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid
keep_files (defined in SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid)SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid
ones_row(self, cols)SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
ones_row_m1(self, cols)SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
ones_row_m2(self, cols)SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
propulsion (defined in SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics)SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics
sample_training(self)SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid
settings (defined in SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid)SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid
stability (defined in SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics)SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics
surrogates (defined in SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid)SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid
tag (defined in SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid)SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid
training (defined in SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid)SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid
training_file (defined in SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid)SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid
weights (defined in SUAVE.Analyses.Mission.Segments.Conditions.Basic.Basic)SUAVE.Analyses.Mission.Segments.Conditions.Basic.Basic
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL__Inviscid_1_1AVL__Inviscid.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL__Inviscid_1_1AVL__Inviscid.html deleted file mode 100644 index 284f480a..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL__Inviscid_1_1AVL__Inviscid.html +++ /dev/null @@ -1,488 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
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-
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SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid Class Reference
-
-
-
-Inheritance diagram for SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid:
-
-
- - -SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics -SUAVE.Analyses.Mission.Segments.Conditions.Basic.Basic -SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions - -
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def initialize (self)
 
def evaluate (self, state, settings, geometry)
 
def sample_training (self)
 
def build_surrogate (self)
 
def evaluate_conditions (self, run_conditions)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Conditions.Basic.Basic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
def ones_row (self, cols)
 
def ones_row_m1 (self, cols)
 
def ones_row_m2 (self, cols)
 
def expand_rows (self, rows)
 
def compile (self)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

tag
 
keep_files
 
settings
 
current_status
 
geometry
 
training
 
training_file
 
surrogates
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics
tag
 
freestream
 
aerodynamics
 
stability
 
propulsion
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Conditions.Basic.Basic
tag
 
frames
 
weights
 
energies
 
-

Detailed Description

-
This builds a surrogate and computes lift using AVL.
-
-Assumptions:
-None
-
-Source:
-None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid.__defaults__ ( self)
-
-
This sets the default values and methods for the analysis.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
-
- -

◆ build_surrogate()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid.build_surrogate ( self)
-
-
Builds a surrogate based on sample evalations using a Guassian process.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-self.training.
-  coefficients     [-] CL and CD
-  grid_points      [radians,-] angles of attack and mach numbers 
-
-Outputs:
-self.surrogates.
-  lift_coefficient <Guassian process surrogate>
-  drag_coefficient <Guassian process surrogate>
-
-Properties Used:
-No others
-
-
-
- -

◆ evaluate()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid.evaluate ( self,
 state,
 settings,
 geometry 
)
-
-
Evaluates lift and drag using available surrogates.
-
-Assumptions:
-Returned drag values are currently not meaningful.
-
-Source:
-N/A
-
-Inputs:
-state.conditions.
-  mach_number      [-]
-  angle_of_attack  [radians]
-
-Outputs:
-inviscid_lift      [-] CL
-inviscid_drag      [-] CD
-
-Properties Used:
-self.surrogates.
-  lift_coefficient [-] CL
-  drag_coefficient [-] CD
-
-
-
- -

◆ evaluate_conditions()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid.evaluate_conditions ( self,
 run_conditions 
)
-
-
Process vehicle to setup geometry, condititon, and configuration.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-run_conditions <SUAVE data type> aerodynamic conditions; until input
-method is finalized, will assume mass_properties are always as 
-defined in self.features
-
-Outputs:
-results        <SUAVE data type>
-
-Properties Used:
-self.settings.filenames.
-  run_folder
-  output_template
-  batch_template
-  deck_template
-self.current_status.
-  batch_index
-  batch_file
-  deck_file
-  cases
-
-
-
- -

◆ initialize()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid.initialize ( self)
-
-
Drives functions to get training samples and build a surrogate.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-self.tag = 'avl_analysis_of_{}'.format(geometry.tag)
-
-Properties Used:
-self.geometry.tag
-
-
-
- -

◆ sample_training()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid.sample_training ( self)
-
-
Call methods to run AVL for sample point evaluation.
-
-Assumptions:
-Returned drag values are not meaningful.
-
-Source:
-N/A
-
-Inputs:
-see properties used
-
-Outputs:
-self.training.
-  coefficients     [-] CL and CD
-  grid_points      [radians,-] angles of attack and mach numbers 
-
-Properties Used:
-self.geometry.tag  <string>
-self.training.     
-  angle_of_attack  [radians]
-  Mach             [-]
-self.training_file (optional - file containing previous AVL data)
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Aerodynamics/AVL_Inviscid.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL__Inviscid_1_1AVL__Inviscid.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL__Inviscid_1_1AVL__Inviscid.js deleted file mode 100644 index 5a768444..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL__Inviscid_1_1AVL__Inviscid.js +++ /dev/null @@ -1,17 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL__Inviscid_1_1AVL__Inviscid = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL__Inviscid_1_1AVL__Inviscid.html#a2674aeb739fbede3df8174cc5971117c", null ], - [ "build_surrogate", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL__Inviscid_1_1AVL__Inviscid.html#aa2a251b450d7a8bad81203841b9367e8", null ], - [ "evaluate", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL__Inviscid_1_1AVL__Inviscid.html#a5239bbcd5e0f5bcef56f07626ff903d5", null ], - [ "evaluate_conditions", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL__Inviscid_1_1AVL__Inviscid.html#a55e806c99124a4651a2bd74cd27b73a2", null ], - [ "initialize", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL__Inviscid_1_1AVL__Inviscid.html#a2c9bfba28deb4c834ead25ce3af9ba01", null ], - [ "sample_training", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL__Inviscid_1_1AVL__Inviscid.html#a8a56e051851235864dc8839d57ed9023", null ], - [ "current_status", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL__Inviscid_1_1AVL__Inviscid.html#ad8d7881165eb8c63bd430a38f1f38a21", null ], - [ "geometry", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL__Inviscid_1_1AVL__Inviscid.html#ab3413e0de53e813c992c5693fe668c9b", null ], - [ "keep_files", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL__Inviscid_1_1AVL__Inviscid.html#ac204dd9a499b67b481b39e4e8a5db082", null ], - [ "settings", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL__Inviscid_1_1AVL__Inviscid.html#a2bc68b59e7ead5a51ef3ab08c738b5fb", null ], - [ "surrogates", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL__Inviscid_1_1AVL__Inviscid.html#a8b545d9a8168b3ae0da29f0319dc3b44", null ], - [ "tag", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL__Inviscid_1_1AVL__Inviscid.html#a9bdf600c35e259c1a8b4a7f79628dcf0", null ], - [ "training", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL__Inviscid_1_1AVL__Inviscid.html#a9a05633a9487fa996e38577aec315090", null ], - [ "training_file", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL__Inviscid_1_1AVL__Inviscid.html#ad91470605d1cfcf0f0921bae27172015", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL__Inviscid_1_1AVL__Inviscid.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL__Inviscid_1_1AVL__Inviscid.png deleted file mode 100644 index 5182b9d1..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL__Inviscid_1_1AVL__Inviscid.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Aerodynamics_1_1Aerodynamics-members.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Aerodynamics_1_1Aerodynamics-members.html deleted file mode 100644 index 98f72bb0..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Aerodynamics_1_1Aerodynamics-members.html +++ /dev/null @@ -1,125 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
-
- - - -
-
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- - - - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Aerodynamics_1_1Aerodynamics.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Aerodynamics_1_1Aerodynamics.html deleted file mode 100644 index 1d1eb768..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Aerodynamics_1_1Aerodynamics.html +++ /dev/null @@ -1,356 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
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-
-
- - - -
-
- -
-
-
- -
- -
-
- - -
- -
- -
- -
-
SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics Class Reference
-
-
-
-Inheritance diagram for SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics:
-
-
- - -SUAVE.Analyses.Analysis.Analysis -SUAVE.Analyses.Aerodynamics.Markup.Markup -SUAVE.Analyses.Aerodynamics.SU2_inviscid.SU2_inviscid -SUAVE.Analyses.Aerodynamics.SU2_inviscid_Super.SU2_inviscid_Super -SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice -SUAVE.Analyses.Aerodynamics.AERODAS.AERODAS -SUAVE.Analyses.Aerodynamics.AVL.AVL -SUAVE.Analyses.Aerodynamics.Fidelity_Zero.Fidelity_Zero -SUAVE.Analyses.Aerodynamics.SU2_Euler.SU2_Euler -SUAVE.Analyses.Aerodynamics.SU2_Euler_Super.SU2_Euler_Super -SUAVE.Analyses.Aerodynamics.Supersonic_OpenVSP_Wave_Drag.Supersonic_OpenVSP_Wave_Drag -SUAVE.Analyses.Aerodynamics.Supersonic_Zero.Supersonic_Zero - -
- - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def evaluate (self, state)
 
def finalize (self)
 
def compute_forces (self, conditions)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - -

-Public Attributes

tag
 
geometry
 
settings
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
This is the base class for aerodynamics analyses. It contains functions
-that are built into the default class.
-
-Assumptions:
-None
-
-Source:
-N/A
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics.__defaults__ ( self)
-
-
This sets the default values and methods for the analysis.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
-
- -

◆ compute_forces()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics.compute_forces ( self,
 conditions 
)
-
-
The default function to compute forces.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-conditions.freestream.
-  dynamic_pressure       [Pa]
-conditions.aerodynamics.
-  lift_coefficient       [-]
-  drag_coefficient       [-]
-
-Outputs:
-results.
-  lift_force_vector      [N]
-  drag_force_vector      [N]
-
-Properties Used:
-self.geometry.reference_area [m^2]
-
-
-
- -

◆ evaluate()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics.evaluate ( self,
 state 
)
-
-
The default evaluate function.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-results   <Results class> (empty)
-
-Properties Used:
-N/A
-
-
-
- -

◆ finalize()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics.finalize ( self)
-
-
The default finalize function.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Aerodynamics/Aerodynamics.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Aerodynamics_1_1Aerodynamics.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Aerodynamics_1_1Aerodynamics.js deleted file mode 100644 index 02c203b0..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Aerodynamics_1_1Aerodynamics.js +++ /dev/null @@ -1,10 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Aerodynamics_1_1Aerodynamics = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Aerodynamics_1_1Aerodynamics.html#a102129619dc160ce8f979301029b3921", null ], - [ "compute_forces", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Aerodynamics_1_1Aerodynamics.html#a6702f0aabc084054884871464a89261b", null ], - [ "evaluate", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Aerodynamics_1_1Aerodynamics.html#a9684f9fe2c620a8715c73a4a43319fa1", null ], - [ "finalize", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Aerodynamics_1_1Aerodynamics.html#afc822038b10ccbcb3cefdb1a416d137f", null ], - [ "geometry", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Aerodynamics_1_1Aerodynamics.html#a1d2366be5c23f5d574e37280b708e67b", null ], - [ "settings", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Aerodynamics_1_1Aerodynamics.html#a2ed6a71bdd4404ee6792d807a381730a", null ], - [ "tag", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Aerodynamics_1_1Aerodynamics.html#a40b22553e887d6e65aea80b4f3f20581", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Aerodynamics_1_1Aerodynamics.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Aerodynamics_1_1Aerodynamics.png deleted file mode 100644 index 8e6b8be7..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Aerodynamics_1_1Aerodynamics.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Fidelity__Zero_1_1Fidelity__Zero-members.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Fidelity__Zero_1_1Fidelity__Zero-members.html deleted file mode 100644 index 94c2bc8b..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Fidelity__Zero_1_1Fidelity__Zero-members.html +++ /dev/null @@ -1,127 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
-
- - - -
-
- -
-
-
- -
- -
-
- - -
- -
- -
-
-
SUAVE.Analyses.Aerodynamics.Fidelity_Zero.Fidelity_Zero Member List
-
- -
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Fidelity__Zero_1_1Fidelity__Zero.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Fidelity__Zero_1_1Fidelity__Zero.html deleted file mode 100644 index 0cace917..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Fidelity__Zero_1_1Fidelity__Zero.html +++ /dev/null @@ -1,281 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Aerodynamics.Fidelity_Zero.Fidelity_Zero Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
-
- - - -
-
- -
-
-
- -
- -
-
- - -
- -
- -
- -
-
SUAVE.Analyses.Aerodynamics.Fidelity_Zero.Fidelity_Zero Class Reference
-
-
-
-Inheritance diagram for SUAVE.Analyses.Aerodynamics.Fidelity_Zero.Fidelity_Zero:
-
-
- - -SUAVE.Analyses.Aerodynamics.Markup.Markup -SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics -SUAVE.Analyses.Analysis.Analysis - -
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def initialize (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Aerodynamics.Markup.Markup
def __defaults__ (self)
 
def evaluate (self, state)
 
def initialize (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
def __defaults__ (self)
 
def evaluate (self, state)
 
def finalize (self)
 
def compute_forces (self, conditions)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

tag
 
- Public Attributes inherited from SUAVE.Analyses.Aerodynamics.Markup.Markup
tag
 
geometry
 
settings
 
process
 
- Public Attributes inherited from SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
tag
 
geometry
 
settings
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
This is an analysis based on low-fidelity models.
-
-Assumptions:
-Subsonic
-
-Source:
-Primarily based on adg.stanford.edu, see methods for details
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Aerodynamics.Fidelity_Zero.Fidelity_Zero.__defaults__ ( self)
-
-
This sets the default values and methods for the analysis.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
-
- -

◆ initialize()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Aerodynamics.Fidelity_Zero.Fidelity_Zero.initialize ( self)
-
-
Initializes the surrogate needed for lift calculation.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-self.geometry
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Aerodynamics/Fidelity_Zero.py
  • -
-
-
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Aerodynamics.Markup.Markup Class Reference
-
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-Inheritance diagram for SUAVE.Analyses.Aerodynamics.Markup.Markup:
-
-
- - -SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics -SUAVE.Analyses.Analysis.Analysis -SUAVE.Analyses.Aerodynamics.AERODAS.AERODAS -SUAVE.Analyses.Aerodynamics.AVL.AVL -SUAVE.Analyses.Aerodynamics.Fidelity_Zero.Fidelity_Zero -SUAVE.Analyses.Aerodynamics.SU2_Euler.SU2_Euler -SUAVE.Analyses.Aerodynamics.SU2_Euler_Super.SU2_Euler_Super -SUAVE.Analyses.Aerodynamics.Supersonic_OpenVSP_Wave_Drag.Supersonic_OpenVSP_Wave_Drag -SUAVE.Analyses.Aerodynamics.Supersonic_Zero.Supersonic_Zero - -
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def evaluate (self, state)
 
def initialize (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
def __defaults__ (self)
 
def evaluate (self, state)
 
def finalize (self)
 
def compute_forces (self, conditions)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

tag
 
geometry
 
settings
 
process
 
- Public Attributes inherited from SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
tag
 
geometry
 
settings
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
This is an intermediate class for aerodynamic analyses.
-
-Assumptions:
-None
-
-Source:
-N/A
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Aerodynamics.Markup.Markup.__defaults__ ( self)
-
-
This sets the default values and methods for the analysis.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
-
- -

◆ evaluate()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Analyses.Aerodynamics.Markup.Markup.evaluate ( self,
 state 
)
-
-
The default evaluate function.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-results   <SUAVE data class>
-
-Properties Used:
-self.settings
-self.geometry
-
-
-
- -

◆ initialize()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Aerodynamics.Markup.Markup.initialize ( self)
-
-
The default finalize function. Calls the initialize process.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Aerodynamics/Markup.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Markup_1_1Markup.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Markup_1_1Markup.js deleted file mode 100644 index d2773ef7..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Markup_1_1Markup.js +++ /dev/null @@ -1,10 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Markup_1_1Markup = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Markup_1_1Markup.html#a9df8aff26c0f7b9779522069069680d4", null ], - [ "evaluate", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Markup_1_1Markup.html#a2dcd4753410520a45e99e0bd3165ada9", null ], - [ "initialize", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Markup_1_1Markup.html#ae245433bcbe8036e917c4f0b4d21f7d2", null ], - [ "geometry", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Markup_1_1Markup.html#a665085a816238c4015570a5b7a960791", null ], - [ "process", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Markup_1_1Markup.html#ab4fdd63d93a0248bd487e6e9626bf3c3", null ], - [ "settings", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Markup_1_1Markup.html#a48fb50f5fb9852e928eb6e3161e03b97", null ], - [ "tag", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Markup_1_1Markup.html#a73c36817237275ada1b38de1b17f647b", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Markup_1_1Markup.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Markup_1_1Markup.png deleted file mode 100644 index d57f1d22..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Markup_1_1Markup.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Process__Geometry_1_1Process__Geometry-members.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Process__Geometry_1_1Process__Geometry-members.html deleted file mode 100644 index 4187389e..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Process__Geometry_1_1Process__Geometry-members.html +++ /dev/null @@ -1,118 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Aerodynamics.Process_Geometry.Process_Geometry Member List
-
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Process__Geometry_1_1Process__Geometry.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Process__Geometry_1_1Process__Geometry.html deleted file mode 100644 index 97a1622a..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Process__Geometry_1_1Process__Geometry.html +++ /dev/null @@ -1,261 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Aerodynamics.Process_Geometry.Process_Geometry Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Aerodynamics.Process_Geometry.Process_Geometry Class Reference
-
-
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-Inheritance diagram for SUAVE.Analyses.Aerodynamics.Process_Geometry.Process_Geometry:
-
-
- - -SUAVE.Analyses.Process.Process - -
- - - - - - - - - - - -

-Public Member Functions

def __init__ (self, geometry_key)
 
def evaluate (self, state, settings, geometry)
 
- Public Member Functions inherited from SUAVE.Analyses.Process.Process
def evaluate (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - -

-Static Public Attributes

geometry_key = None
 
- Static Public Attributes inherited from SUAVE.Analyses.Process.Process
-bool verbose = False
 
-

Detailed Description

-
A process for evaluate over a component group.
-
-Assumptions:
-None
-
-Source:
-N/A
-

Constructor & Destructor Documentation

- -

◆ __init__()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Analyses.Aerodynamics.Process_Geometry.Process_Geometry.__init__ ( self,
 geometry_key 
)
-
-
Sets the geometry key for this process.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-geometry_key      <string>
-
-Outputs:
-None
-
-Properties Used:
-self.geometry_key <string>
-
-
-
-

Member Function Documentation

- -

◆ evaluate()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Analyses.Aerodynamics.Process_Geometry.Process_Geometry.evaluate ( self,
 state,
 settings,
 geometry 
)
-
-
Evaluates preset processes for each component.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-state     (passed to an evaluation function)
-setting   (passed to an evaluation function)
-geometry  (used to get keys and passed to an evaluation function)
-
-Outputs:
-None
-
-Properties Used:
-self.geometry_key <string>
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Aerodynamics/Process_Geometry.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Process__Geometry_1_1Process__Geometry.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Process__Geometry_1_1Process__Geometry.js deleted file mode 100644 index 304f1c8a..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Process__Geometry_1_1Process__Geometry.js +++ /dev/null @@ -1,5 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Process__Geometry_1_1Process__Geometry = -[ - [ "__init__", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Process__Geometry_1_1Process__Geometry.html#aa49d1aa4ac6443b62296f0c02ae074be", null ], - [ "evaluate", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Process__Geometry_1_1Process__Geometry.html#a0247365f3e5fa2e49af9d0580f4a6233", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Process__Geometry_1_1Process__Geometry.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Process__Geometry_1_1Process__Geometry.png deleted file mode 100644 index e4f37b83..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Process__Geometry_1_1Process__Geometry.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Results_1_1Results-members.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Results_1_1Results-members.html deleted file mode 100644 index 4ef54a19..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Results_1_1Results-members.html +++ /dev/null @@ -1,117 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Aerodynamics.Results.Results Member List
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Aerodynamics.Results.Results Class Reference
-
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-Inheritance diagram for SUAVE.Analyses.Aerodynamics.Results.Results:
-
-
- - - -
- - - - -

-Public Member Functions

def __defaults__ (self)
 
- - - - - - - - - -

-Public Attributes

lift_coefficient
 
drag_coefficient
 
lift_force_vector
 
drag_force_vector
 
-

Detailed Description

-
A class for storing aerodynamic results.
-
-Assumptions:
-None
-
-Source:
-N/A
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Aerodynamics.Results.Results.__defaults__ ( self)
-
-
This sets the default values for the results.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Aerodynamics/Results.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Results_1_1Results.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Results_1_1Results.js deleted file mode 100644 index 9019bdc7..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Results_1_1Results.js +++ /dev/null @@ -1,8 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Results_1_1Results = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Results_1_1Results.html#a6551eed89371b92d55be76da3790a0ad", null ], - [ "drag_coefficient", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Results_1_1Results.html#a6365a549c4318ab31ee88413aee9db73", null ], - [ "drag_force_vector", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Results_1_1Results.html#aaeb551a3283ce47264ab96346139747f", null ], - [ "lift_coefficient", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Results_1_1Results.html#a3bb03ae797eb7dd2284c87bc3460a410", null ], - [ "lift_force_vector", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Results_1_1Results.html#a9c4f578990cf7afea65efed34822885e", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Results_1_1Results.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Results_1_1Results.png deleted file mode 100644 index c61d3940..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Results_1_1Results.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__Euler_1_1SU2__Euler-members.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__Euler_1_1SU2__Euler-members.html deleted file mode 100644 index e23d2e30..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__Euler_1_1SU2__Euler-members.html +++ /dev/null @@ -1,127 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Aerodynamics.SU2_Euler.SU2_Euler Member List
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__Euler_1_1SU2__Euler.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__Euler_1_1SU2__Euler.html deleted file mode 100644 index 9d8ad32d..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__Euler_1_1SU2__Euler.html +++ /dev/null @@ -1,287 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Aerodynamics.SU2_Euler.SU2_Euler Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Aerodynamics.SU2_Euler.SU2_Euler Class Reference
-
-
-
-Inheritance diagram for SUAVE.Analyses.Aerodynamics.SU2_Euler.SU2_Euler:
-
-
- - -SUAVE.Analyses.Aerodynamics.Markup.Markup -SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics -SUAVE.Analyses.Analysis.Analysis - -
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def initialize (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Aerodynamics.Markup.Markup
def __defaults__ (self)
 
def evaluate (self, state)
 
def initialize (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
def __defaults__ (self)
 
def evaluate (self, state)
 
def finalize (self)
 
def compute_forces (self, conditions)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

tag
 
- Public Attributes inherited from SUAVE.Analyses.Aerodynamics.Markup.Markup
tag
 
geometry
 
settings
 
process
 
- Public Attributes inherited from SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
tag
 
geometry
 
settings
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
This uses SU2 to compute lift.
-
-Assumptions:
-Subsonic
-
-Source:
-None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Aerodynamics.SU2_Euler.SU2_Euler.__defaults__ ( self)
-
-
This sets the default values and methods for the analysis.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
-
- -

◆ initialize()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Aerodynamics.SU2_Euler.SU2_Euler.initialize ( self)
-
-
Initializes the surrogate needed for SU2, including building the surface and volume meshes.
-
-Assumptions:
-Vehicle is available in OpenVSP
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-self.geometry.tag               <string> (geometry is also set as part of the lift process)
-self.process.compute.lift.
-  inviscid.training_file        (optional - determines if new SU2 runs are necessary)
-self.settings.
-  half_mesh_flag                <boolean> Determines if a symmetry plane is used
-  vsp_mesh_growth_ratio         [-] Determines how the mesh grows
-  vsp_mesh_growth_limiting_flag <boolean> Determines if 3D growth limiting is used
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Aerodynamics/SU2_Euler.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__Euler_1_1SU2__Euler.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__Euler_1_1SU2__Euler.js deleted file mode 100644 index 4fdd3375..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__Euler_1_1SU2__Euler.js +++ /dev/null @@ -1,6 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__Euler_1_1SU2__Euler = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__Euler_1_1SU2__Euler.html#a0437ac33b2fea2955ce838566cfd37a9", null ], - [ "initialize", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__Euler_1_1SU2__Euler.html#a80a236e6d10443f5757be5dce28d8ce4", null ], - [ "tag", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__Euler_1_1SU2__Euler.html#ab9cf92603db0380ed7d012d75e363535", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__Euler_1_1SU2__Euler.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__Euler_1_1SU2__Euler.png deleted file mode 100644 index a6a85ffe..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__Euler_1_1SU2__Euler.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__Euler__Super_1_1SU2__Euler__Super-members.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__Euler__Super_1_1SU2__Euler__Super-members.html deleted file mode 100644 index 0ada4a28..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__Euler__Super_1_1SU2__Euler__Super-members.html +++ /dev/null @@ -1,127 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
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-
- - - -
-
- -
-
-
- -
- -
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- - -
- -
- -
-
-
SUAVE.Analyses.Aerodynamics.SU2_Euler_Super.SU2_Euler_Super Member List
-
- -
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__Euler__Super_1_1SU2__Euler__Super.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__Euler__Super_1_1SU2__Euler__Super.html deleted file mode 100644 index cbb7f56c..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__Euler__Super_1_1SU2__Euler__Super.html +++ /dev/null @@ -1,287 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Aerodynamics.SU2_Euler_Super.SU2_Euler_Super Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
-
- - - -
-
- -
-
-
- -
- -
-
- - -
- -
- -
- -
-
SUAVE.Analyses.Aerodynamics.SU2_Euler_Super.SU2_Euler_Super Class Reference
-
-
-
-Inheritance diagram for SUAVE.Analyses.Aerodynamics.SU2_Euler_Super.SU2_Euler_Super:
-
-
- - -SUAVE.Analyses.Aerodynamics.Markup.Markup -SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics -SUAVE.Analyses.Analysis.Analysis - -
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def initialize (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Aerodynamics.Markup.Markup
def __defaults__ (self)
 
def evaluate (self, state)
 
def initialize (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
def __defaults__ (self)
 
def evaluate (self, state)
 
def finalize (self)
 
def compute_forces (self, conditions)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

tag
 
- Public Attributes inherited from SUAVE.Analyses.Aerodynamics.Markup.Markup
tag
 
geometry
 
settings
 
process
 
- Public Attributes inherited from SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
tag
 
geometry
 
settings
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
This uses SU2 to compute lift.
-
-Assumptions:
-Subsonic
-
-Source:
-None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Aerodynamics.SU2_Euler_Super.SU2_Euler_Super.__defaults__ ( self)
-
-
This sets the default values and methods for the analysis.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
-
- -

◆ initialize()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Aerodynamics.SU2_Euler_Super.SU2_Euler_Super.initialize ( self)
-
-
Initializes the surrogate needed for SU2, including building the surface and volume meshes.
-
-Assumptions:
-Vehicle is available in OpenVSP
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-self.geometry.tag               <string> (geometry is also set as part of the lift process)
-self.process.compute.lift.
-  inviscid.training_file        (optional - determines if new SU2 runs are necessary)
-self.settings.
-  half_mesh_flag                <boolean> Determines if a symmetry plane is used
-  vsp_mesh_growth_ratio         [-] Determines how the mesh grows
-  vsp_mesh_growth_limiting_flag <boolean> Determines if 3D growth limiting is used
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Aerodynamics/SU2_Euler_Super.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__Euler__Super_1_1SU2__Euler__Super.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__Euler__Super_1_1SU2__Euler__Super.js deleted file mode 100644 index 2b3d034f..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__Euler__Super_1_1SU2__Euler__Super.js +++ /dev/null @@ -1,6 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__Euler__Super_1_1SU2__Euler__Super = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__Euler__Super_1_1SU2__Euler__Super.html#a277c27498547785c51a5c188d13c8cfb", null ], - [ "initialize", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__Euler__Super_1_1SU2__Euler__Super.html#a60cc2d4e29fd4f68c5cf42861930d5e8", null ], - [ "tag", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__Euler__Super_1_1SU2__Euler__Super.html#af3a20ad5b6988eecddf2b0fd6db919cb", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__Euler__Super_1_1SU2__Euler__Super.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__Euler__Super_1_1SU2__Euler__Super.png deleted file mode 100644 index 178eb114..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__Euler__Super_1_1SU2__Euler__Super.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__inviscid_1_1SU2__inviscid-members.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__inviscid_1_1SU2__inviscid-members.html deleted file mode 100644 index 805bb2f1..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__inviscid_1_1SU2__inviscid-members.html +++ /dev/null @@ -1,132 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
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- -
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SUAVE.Analyses.Aerodynamics.SU2_inviscid.SU2_inviscid Member List
-
-
- -

This is the complete list of members for SUAVE.Analyses.Aerodynamics.SU2_inviscid.SU2_inviscid, including all inherited members.

- - - - - - - - - - - - - - - - - - - - - -
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Aerodynamics.SU2_inviscid.SU2_inviscid
build_surrogate(self)SUAVE.Analyses.Aerodynamics.SU2_inviscid.SU2_inviscid
compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
compute_forces(self, conditions)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
evaluate(self, state, settings, geometry)SUAVE.Analyses.Aerodynamics.SU2_inviscid.SU2_inviscid
SUAVE::Analyses::Aerodynamics::Aerodynamics::Aerodynamics.evaluate(self, state)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
geometry (defined in SUAVE.Analyses.Aerodynamics.SU2_inviscid.SU2_inviscid)SUAVE.Analyses.Aerodynamics.SU2_inviscid.SU2_inviscid
initialize(self)SUAVE.Analyses.Aerodynamics.SU2_inviscid.SU2_inviscid
SUAVE::Analyses::Aerodynamics::Aerodynamics::Aerodynamics.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
sample_training(self)SUAVE.Analyses.Aerodynamics.SU2_inviscid.SU2_inviscid
settings (defined in SUAVE.Analyses.Aerodynamics.SU2_inviscid.SU2_inviscid)SUAVE.Analyses.Aerodynamics.SU2_inviscid.SU2_inviscid
surrogates (defined in SUAVE.Analyses.Aerodynamics.SU2_inviscid.SU2_inviscid)SUAVE.Analyses.Aerodynamics.SU2_inviscid.SU2_inviscid
tag (defined in SUAVE.Analyses.Aerodynamics.SU2_inviscid.SU2_inviscid)SUAVE.Analyses.Aerodynamics.SU2_inviscid.SU2_inviscid
training (defined in SUAVE.Analyses.Aerodynamics.SU2_inviscid.SU2_inviscid)SUAVE.Analyses.Aerodynamics.SU2_inviscid.SU2_inviscid
training_file (defined in SUAVE.Analyses.Aerodynamics.SU2_inviscid.SU2_inviscid)SUAVE.Analyses.Aerodynamics.SU2_inviscid.SU2_inviscid
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__inviscid_1_1SU2__inviscid.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__inviscid_1_1SU2__inviscid.html deleted file mode 100644 index 06408ae4..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__inviscid_1_1SU2__inviscid.html +++ /dev/null @@ -1,420 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Aerodynamics.SU2_inviscid.SU2_inviscid Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
-
- - - -
-
- -
-
-
- -
- -
-
- - -
- -
- -
- -
-
SUAVE.Analyses.Aerodynamics.SU2_inviscid.SU2_inviscid Class Reference
-
-
-
-Inheritance diagram for SUAVE.Analyses.Aerodynamics.SU2_inviscid.SU2_inviscid:
-
-
- - -SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics -SUAVE.Analyses.Analysis.Analysis - -
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def initialize (self)
 
def evaluate (self, state, settings, geometry)
 
def sample_training (self)
 
def build_surrogate (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
def __defaults__ (self)
 
def evaluate (self, state)
 
def finalize (self)
 
def compute_forces (self, conditions)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

tag
 
geometry
 
settings
 
training
 
training_file
 
surrogates
 
- Public Attributes inherited from SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
tag
 
geometry
 
settings
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
This builds a surrogate and computes lift and drag using SU2
-
-Assumptions:
-Inviscid, subsonic
-
-Source:
-None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Aerodynamics.SU2_inviscid.SU2_inviscid.__defaults__ ( self)
-
-
This sets the default values and methods for the analysis.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
-
- -

◆ build_surrogate()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Aerodynamics.SU2_inviscid.SU2_inviscid.build_surrogate ( self)
-
-
Builds a surrogate based on sample evalations using a Guassian process.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-self.training.
-  coefficients     [-] CL and CD
-  grid_points      [radians,-] angles of attack and mach numbers 
-
-Outputs:
-self.surrogates.
-  lift_coefficient <Guassian process surrogate>
-  drag_coefficient <Guassian process surrogate>
-
-Properties Used:
-No others
-
-
-
- -

◆ evaluate()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Analyses.Aerodynamics.SU2_inviscid.SU2_inviscid.evaluate ( self,
 state,
 settings,
 geometry 
)
-
-
Evaluates lift and drag using available surrogates.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-state.conditions.
-  mach_number      [-]
-  angle_of_attack  [radians]
-
-Outputs:
-inviscid_lift      [-] CL
-inviscid_drag      [-] CD
-
-Properties Used:
-self.surrogates.
-  lift_coefficient [-] CL
-  drag_coefficient [-] CD
-
-
-
- -

◆ initialize()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Aerodynamics.SU2_inviscid.SU2_inviscid.initialize ( self)
-
-
Drives functions to get training samples and build a surrogate.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-None
-
-
-
- -

◆ sample_training()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Aerodynamics.SU2_inviscid.SU2_inviscid.sample_training ( self)
-
-
Call methods to run SU2 for sample point evaluation.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-see properties used
-
-Outputs:
-self.training.
-  coefficients     [-] CL and CD
-  grid_points      [radians,-] angles of attack and mach numbers 
-
-Properties Used:
-self.geometry.tag  <string>
-self.training.     
-  angle_of_attack  [radians]
-  Mach             [-]
-self.training_file (optional - file containing previous AVL data)
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Aerodynamics/SU2_inviscid.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__inviscid_1_1SU2__inviscid.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__inviscid_1_1SU2__inviscid.js deleted file mode 100644 index 903e3fa5..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__inviscid_1_1SU2__inviscid.js +++ /dev/null @@ -1,14 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__inviscid_1_1SU2__inviscid = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__inviscid_1_1SU2__inviscid.html#a9852a626d370716e36293f460e7b8b0a", null ], - [ "build_surrogate", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__inviscid_1_1SU2__inviscid.html#adbdafffbfe483edf5b6105aae783d95d", null ], - [ "evaluate", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__inviscid_1_1SU2__inviscid.html#a78660b0d690c291216c2c136bbabf143", null ], - [ "initialize", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__inviscid_1_1SU2__inviscid.html#a6907d31980e70c34b84cf4e09b3eb245", null ], - [ "sample_training", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__inviscid_1_1SU2__inviscid.html#a1c7429982b2f7e57130de7d810cb228b", null ], - [ "geometry", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__inviscid_1_1SU2__inviscid.html#adaf3c839f7bc62fd2fd854123207343f", null ], - [ "settings", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__inviscid_1_1SU2__inviscid.html#a3c0394a57e4d330471de232ecf4435de", null ], - [ "surrogates", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__inviscid_1_1SU2__inviscid.html#a1186090ab391eb9b3bb37503b036deda", null ], - [ "tag", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__inviscid_1_1SU2__inviscid.html#a3cd3f3384d899965d3702601c5eaa350", null ], - [ "training", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__inviscid_1_1SU2__inviscid.html#af4b2c64172dd61aa36bec4ec136776db", null ], - [ "training_file", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__inviscid_1_1SU2__inviscid.html#a82f498060da0e10675fe753f7a37ef02", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__inviscid_1_1SU2__inviscid.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__inviscid_1_1SU2__inviscid.png deleted file mode 100644 index cb180453..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__inviscid_1_1SU2__inviscid.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__inviscid__Super_1_1SU2__inviscid__Super-members.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__inviscid__Super_1_1SU2__inviscid__Super-members.html deleted file mode 100644 index 90e82abd..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__inviscid__Super_1_1SU2__inviscid__Super-members.html +++ /dev/null @@ -1,132 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
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- - - -
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SUAVE.Analyses.Aerodynamics.SU2_inviscid_Super.SU2_inviscid_Super Member List
-
-
- -

This is the complete list of members for SUAVE.Analyses.Aerodynamics.SU2_inviscid_Super.SU2_inviscid_Super, including all inherited members.

- - - - - - - - - - - - - - - - - - - - - -
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Aerodynamics.SU2_inviscid_Super.SU2_inviscid_Super
build_surrogate(self)SUAVE.Analyses.Aerodynamics.SU2_inviscid_Super.SU2_inviscid_Super
compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
compute_forces(self, conditions)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
evaluate(self, state, settings, geometry)SUAVE.Analyses.Aerodynamics.SU2_inviscid_Super.SU2_inviscid_Super
SUAVE::Analyses::Aerodynamics::Aerodynamics::Aerodynamics.evaluate(self, state)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
geometry (defined in SUAVE.Analyses.Aerodynamics.SU2_inviscid_Super.SU2_inviscid_Super)SUAVE.Analyses.Aerodynamics.SU2_inviscid_Super.SU2_inviscid_Super
initialize(self)SUAVE.Analyses.Aerodynamics.SU2_inviscid_Super.SU2_inviscid_Super
SUAVE::Analyses::Aerodynamics::Aerodynamics::Aerodynamics.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
sample_training(self)SUAVE.Analyses.Aerodynamics.SU2_inviscid_Super.SU2_inviscid_Super
settings (defined in SUAVE.Analyses.Aerodynamics.SU2_inviscid_Super.SU2_inviscid_Super)SUAVE.Analyses.Aerodynamics.SU2_inviscid_Super.SU2_inviscid_Super
surrogates (defined in SUAVE.Analyses.Aerodynamics.SU2_inviscid_Super.SU2_inviscid_Super)SUAVE.Analyses.Aerodynamics.SU2_inviscid_Super.SU2_inviscid_Super
tag (defined in SUAVE.Analyses.Aerodynamics.SU2_inviscid_Super.SU2_inviscid_Super)SUAVE.Analyses.Aerodynamics.SU2_inviscid_Super.SU2_inviscid_Super
training (defined in SUAVE.Analyses.Aerodynamics.SU2_inviscid_Super.SU2_inviscid_Super)SUAVE.Analyses.Aerodynamics.SU2_inviscid_Super.SU2_inviscid_Super
training_file (defined in SUAVE.Analyses.Aerodynamics.SU2_inviscid_Super.SU2_inviscid_Super)SUAVE.Analyses.Aerodynamics.SU2_inviscid_Super.SU2_inviscid_Super
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__inviscid__Super_1_1SU2__inviscid__Super.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__inviscid__Super_1_1SU2__inviscid__Super.html deleted file mode 100644 index a0246afd..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__inviscid__Super_1_1SU2__inviscid__Super.html +++ /dev/null @@ -1,420 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Aerodynamics.SU2_inviscid_Super.SU2_inviscid_Super Class Reference - - - - - - - - - - - - - - - -
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-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Aerodynamics.SU2_inviscid_Super.SU2_inviscid_Super Class Reference
-
-
-
-Inheritance diagram for SUAVE.Analyses.Aerodynamics.SU2_inviscid_Super.SU2_inviscid_Super:
-
-
- - -SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics -SUAVE.Analyses.Analysis.Analysis - -
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def initialize (self)
 
def evaluate (self, state, settings, geometry)
 
def sample_training (self)
 
def build_surrogate (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
def __defaults__ (self)
 
def evaluate (self, state)
 
def finalize (self)
 
def compute_forces (self, conditions)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

tag
 
geometry
 
settings
 
training
 
training_file
 
surrogates
 
- Public Attributes inherited from SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
tag
 
geometry
 
settings
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
This builds a surrogate and computes lift and drag using SU2
-
-Assumptions:
-Inviscid
-
-Source:
-None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Aerodynamics.SU2_inviscid_Super.SU2_inviscid_Super.__defaults__ ( self)
-
-
This sets the default values and methods for the analysis.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
-
- -

◆ build_surrogate()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Aerodynamics.SU2_inviscid_Super.SU2_inviscid_Super.build_surrogate ( self)
-
-
Builds a surrogate based on sample evalations using a Guassian process.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-self.training.
-  coefficients     [-] CL and CD
-  grid_points      [radians,-] angles of attack and mach numbers 
-
-Outputs:
-self.surrogates.
-  lift_coefficient <Guassian process surrogate>
-  drag_coefficient <Guassian process surrogate>
-
-Properties Used:
-No others
-
-
-
- -

◆ evaluate()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Analyses.Aerodynamics.SU2_inviscid_Super.SU2_inviscid_Super.evaluate ( self,
 state,
 settings,
 geometry 
)
-
-
Evaluates lift and drag using available surrogates.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-state.conditions.
-  mach_number      [-]
-  angle_of_attack  [radians]
-
-Outputs:
-inviscid_lift      [-] CL
-inviscid_drag      [-] CD
-
-Properties Used:
-self.surrogates.
-  lift_coefficient [-] CL
-  drag_coefficient [-] CD
-
-
-
- -

◆ initialize()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Aerodynamics.SU2_inviscid_Super.SU2_inviscid_Super.initialize ( self)
-
-
Drives functions to get training samples and build a surrogate.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-None
-
-
-
- -

◆ sample_training()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Aerodynamics.SU2_inviscid_Super.SU2_inviscid_Super.sample_training ( self)
-
-
Call methods to run SU2 for sample point evaluation.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-see properties used
-
-Outputs:
-self.training.
-  coefficients     [-] CL and CD
-  grid_points      [radians,-] angles of attack and mach numbers 
-
-Properties Used:
-self.geometry.tag  <string>
-self.training.     
-  angle_of_attack  [radians]
-  Mach             [-]
-self.training_file (optional - file containing previous AVL data)
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Aerodynamics/SU2_inviscid_Super.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__inviscid__Super_1_1SU2__inviscid__Super.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__inviscid__Super_1_1SU2__inviscid__Super.js deleted file mode 100644 index eb9539d1..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__inviscid__Super_1_1SU2__inviscid__Super.js +++ /dev/null @@ -1,14 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__inviscid__Super_1_1SU2__inviscid__Super = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__inviscid__Super_1_1SU2__inviscid__Super.html#aeca18d91241f94f80880085892266c81", null ], - [ "build_surrogate", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__inviscid__Super_1_1SU2__inviscid__Super.html#a2fc4b197ae0eef0024ecad9de8b36aeb", null ], - [ "evaluate", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__inviscid__Super_1_1SU2__inviscid__Super.html#a6d2dfe35a70e2ca116e2a97b042e3737", null ], - [ "initialize", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__inviscid__Super_1_1SU2__inviscid__Super.html#a96911fa57007a70334ad7387267edc8a", null ], - [ "sample_training", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__inviscid__Super_1_1SU2__inviscid__Super.html#a7487786ce46734be5e150af465813705", null ], - [ "geometry", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__inviscid__Super_1_1SU2__inviscid__Super.html#a4da114e35d54388b510826f075f4883d", null ], - [ "settings", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__inviscid__Super_1_1SU2__inviscid__Super.html#afe642fdcc299beefea8e9d68a13e1518", null ], - [ "surrogates", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__inviscid__Super_1_1SU2__inviscid__Super.html#a14b89a71364c858aa2ecad01719093d1", null ], - [ "tag", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__inviscid__Super_1_1SU2__inviscid__Super.html#a8bed23245c10960030ccedc37a04d9cd", null ], - [ "training", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__inviscid__Super_1_1SU2__inviscid__Super.html#a13df6ed45e2cd6a7af3434b15dfa0343", null ], - [ "training_file", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__inviscid__Super_1_1SU2__inviscid__Super.html#a1c778e2ea386d26c5ff4ac273f6d224d", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__inviscid__Super_1_1SU2__inviscid__Super.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__inviscid__Super_1_1SU2__inviscid__Super.png deleted file mode 100644 index 570054d8..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__inviscid__Super_1_1SU2__inviscid__Super.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Supersonic__OpenVSP__Wave__Drag_1_1Supersonic__OpenVSP__Wave__Drag-members.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Supersonic__OpenVSP__Wave__Drag_1_1Supersonic__OpenVSP__Wave__Drag-members.html deleted file mode 100644 index 2022c403..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Supersonic__OpenVSP__Wave__Drag_1_1Supersonic__OpenVSP__Wave__Drag-members.html +++ /dev/null @@ -1,127 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
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SUAVE.Analyses.Aerodynamics.Supersonic_OpenVSP_Wave_Drag.Supersonic_OpenVSP_Wave_Drag Member List
-
-
- -

This is the complete list of members for SUAVE.Analyses.Aerodynamics.Supersonic_OpenVSP_Wave_Drag.Supersonic_OpenVSP_Wave_Drag, including all inherited members.

- - - - - - - - - - - - - - - - -
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Aerodynamics.Supersonic_OpenVSP_Wave_Drag.Supersonic_OpenVSP_Wave_Drag
compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
compute_forces(self, conditions)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
evaluate(self, state)SUAVE.Analyses.Aerodynamics.Markup.Markup
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
geometry (defined in SUAVE.Analyses.Aerodynamics.Markup.Markup)SUAVE.Analyses.Aerodynamics.Markup.Markup
initialize(self)SUAVE.Analyses.Aerodynamics.Supersonic_OpenVSP_Wave_Drag.Supersonic_OpenVSP_Wave_Drag
SUAVE::Analyses::Aerodynamics::Aerodynamics::Aerodynamics.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
process (defined in SUAVE.Analyses.Aerodynamics.Markup.Markup)SUAVE.Analyses.Aerodynamics.Markup.Markup
settings (defined in SUAVE.Analyses.Aerodynamics.Markup.Markup)SUAVE.Analyses.Aerodynamics.Markup.Markup
tag (defined in SUAVE.Analyses.Aerodynamics.Supersonic_OpenVSP_Wave_Drag.Supersonic_OpenVSP_Wave_Drag)SUAVE.Analyses.Aerodynamics.Supersonic_OpenVSP_Wave_Drag.Supersonic_OpenVSP_Wave_Drag
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Supersonic__OpenVSP__Wave__Drag_1_1Supersonic__OpenVSP__Wave__Drag.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Supersonic__OpenVSP__Wave__Drag_1_1Supersonic__OpenVSP__Wave__Drag.html deleted file mode 100644 index b4056a28..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Supersonic__OpenVSP__Wave__Drag_1_1Supersonic__OpenVSP__Wave__Drag.html +++ /dev/null @@ -1,281 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Aerodynamics.Supersonic_OpenVSP_Wave_Drag.Supersonic_OpenVSP_Wave_Drag Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Aerodynamics.Supersonic_OpenVSP_Wave_Drag.Supersonic_OpenVSP_Wave_Drag Class Reference
-
-
-
-Inheritance diagram for SUAVE.Analyses.Aerodynamics.Supersonic_OpenVSP_Wave_Drag.Supersonic_OpenVSP_Wave_Drag:
-
-
- - -SUAVE.Analyses.Aerodynamics.Markup.Markup -SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics -SUAVE.Analyses.Analysis.Analysis - -
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def initialize (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Aerodynamics.Markup.Markup
def __defaults__ (self)
 
def evaluate (self, state)
 
def initialize (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
def __defaults__ (self)
 
def evaluate (self, state)
 
def finalize (self)
 
def compute_forces (self, conditions)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

tag
 
- Public Attributes inherited from SUAVE.Analyses.Aerodynamics.Markup.Markup
tag
 
geometry
 
settings
 
process
 
- Public Attributes inherited from SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
tag
 
geometry
 
settings
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
This is an analysis based on low-fidelity models.
-
-Assumptions:
-None
-
-Source:
-Many methods based on adg.stanford.edu, see methods for details
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Aerodynamics.Supersonic_OpenVSP_Wave_Drag.Supersonic_OpenVSP_Wave_Drag.__defaults__ ( self)
-
-
This sets the default values and methods for the analysis.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
-
- -

◆ initialize()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Aerodynamics.Supersonic_OpenVSP_Wave_Drag.Supersonic_OpenVSP_Wave_Drag.initialize ( self)
-
-
Initializes the surrogate needed for lift calculation and removes old volume drag data files.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-self.geometry.tag (geometry in full is also attached to a process)
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Aerodynamics/Supersonic_OpenVSP_Wave_Drag.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Supersonic__OpenVSP__Wave__Drag_1_1Supersonic__OpenVSP__Wave__Drag.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Supersonic__OpenVSP__Wave__Drag_1_1Supersonic__OpenVSP__Wave__Drag.js deleted file mode 100644 index 2fc4d51e..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Supersonic__OpenVSP__Wave__Drag_1_1Supersonic__OpenVSP__Wave__Drag.js +++ /dev/null @@ -1,6 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Supersonic__OpenVSP__Wave__Drag_1_1Supersonic__OpenVSP__Wave__Drag = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Supersonic__OpenVSP__Wave__Drag_1_1Supersonic__OpenVSP__Wave__Drag.html#a376803e85a4477fe063f3c90aa1a2aae", null ], - [ "initialize", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Supersonic__OpenVSP__Wave__Drag_1_1Supersonic__OpenVSP__Wave__Drag.html#a6138a9e05b97e44691424bb6f298a0ae", null ], - [ "tag", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Supersonic__OpenVSP__Wave__Drag_1_1Supersonic__OpenVSP__Wave__Drag.html#a1f4878fc56ead4f3e9c4eb5f150066c7", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Supersonic__OpenVSP__Wave__Drag_1_1Supersonic__OpenVSP__Wave__Drag.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Supersonic__OpenVSP__Wave__Drag_1_1Supersonic__OpenVSP__Wave__Drag.png deleted file mode 100644 index 19dc33c8..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Supersonic__OpenVSP__Wave__Drag_1_1Supersonic__OpenVSP__Wave__Drag.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Supersonic__Zero_1_1Supersonic__Zero-members.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Supersonic__Zero_1_1Supersonic__Zero-members.html deleted file mode 100644 index 81fadd39..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Supersonic__Zero_1_1Supersonic__Zero-members.html +++ /dev/null @@ -1,128 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
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-
-
- - - -
-
- -
-
-
- -
- -
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- - -
- -
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-
-
SUAVE.Analyses.Aerodynamics.Supersonic_Zero.Supersonic_Zero Member List
-
-
- -

This is the complete list of members for SUAVE.Analyses.Aerodynamics.Supersonic_Zero.Supersonic_Zero, including all inherited members.

- - - - - - - - - - - - - - - - - -
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Aerodynamics.Supersonic_Zero.Supersonic_Zero
compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
compute_forces(self, conditions)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
evaluate(self, state)SUAVE.Analyses.Aerodynamics.Markup.Markup
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize (defined in SUAVE.Analyses.Aerodynamics.Supersonic_Zero.Supersonic_Zero)SUAVE.Analyses.Aerodynamics.Supersonic_Zero.Supersonic_Zerostatic
SUAVE::Analyses::Aerodynamics::Markup::Markup.finalize(self)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
geometry (defined in SUAVE.Analyses.Aerodynamics.Markup.Markup)SUAVE.Analyses.Aerodynamics.Markup.Markup
initialize(self)SUAVE.Analyses.Aerodynamics.Supersonic_Zero.Supersonic_Zero
SUAVE::Analyses::Aerodynamics::Aerodynamics::Aerodynamics.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
process (defined in SUAVE.Analyses.Aerodynamics.Markup.Markup)SUAVE.Analyses.Aerodynamics.Markup.Markup
settings (defined in SUAVE.Analyses.Aerodynamics.Markup.Markup)SUAVE.Analyses.Aerodynamics.Markup.Markup
tag (defined in SUAVE.Analyses.Aerodynamics.Supersonic_Zero.Supersonic_Zero)SUAVE.Analyses.Aerodynamics.Supersonic_Zero.Supersonic_Zero
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Supersonic__Zero_1_1Supersonic__Zero.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Supersonic__Zero_1_1Supersonic__Zero.html deleted file mode 100644 index 702bba51..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Supersonic__Zero_1_1Supersonic__Zero.html +++ /dev/null @@ -1,288 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Aerodynamics.Supersonic_Zero.Supersonic_Zero Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Aerodynamics.Supersonic_Zero.Supersonic_Zero Class Reference
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-
-Inheritance diagram for SUAVE.Analyses.Aerodynamics.Supersonic_Zero.Supersonic_Zero:
-
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- - -SUAVE.Analyses.Aerodynamics.Markup.Markup -SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics -SUAVE.Analyses.Analysis.Analysis - -
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-Public Member Functions

def __defaults__ (self)
 
def initialize (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Aerodynamics.Markup.Markup
def __defaults__ (self)
 
def evaluate (self, state)
 
def initialize (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
def __defaults__ (self)
 
def evaluate (self, state)
 
def finalize (self)
 
def compute_forces (self, conditions)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

tag
 
- Public Attributes inherited from SUAVE.Analyses.Aerodynamics.Markup.Markup
tag
 
geometry
 
settings
 
process
 
- Public Attributes inherited from SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
tag
 
geometry
 
settings
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
- - - -

-Static Public Attributes

-def finalize = initialize
 
-

Detailed Description

-
This is an analysis based on low-fidelity models.
-
-Assumptions:
-None
-
-Source:
-Primarily based on adg.stanford.edu, see methods for details
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Aerodynamics.Supersonic_Zero.Supersonic_Zero.__defaults__ ( self)
-
-
This sets the default values and methods for the analysis.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
-
- -

◆ initialize()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Aerodynamics.Supersonic_Zero.Supersonic_Zero.initialize ( self)
-
-
Initializes the surrogate needed for lift calculation.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-self.geometry
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Aerodynamics/Supersonic_Zero.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Supersonic__Zero_1_1Supersonic__Zero.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Supersonic__Zero_1_1Supersonic__Zero.js deleted file mode 100644 index 9ef64fbc..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Supersonic__Zero_1_1Supersonic__Zero.js +++ /dev/null @@ -1,6 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Supersonic__Zero_1_1Supersonic__Zero = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Supersonic__Zero_1_1Supersonic__Zero.html#ac56c998c7dae9a493b94d491d715e74d", null ], - [ "initialize", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Supersonic__Zero_1_1Supersonic__Zero.html#afcc925b9d83b6024a4dcd21017403b6a", null ], - [ "tag", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Supersonic__Zero_1_1Supersonic__Zero.html#aeb7fdbef3bc198aae167cfd26645629a", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Supersonic__Zero_1_1Supersonic__Zero.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Supersonic__Zero_1_1Supersonic__Zero.png deleted file mode 100644 index f5a86091..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Supersonic__Zero_1_1Supersonic__Zero.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Vortex__Lattice_1_1Vortex__Lattice-members.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Vortex__Lattice_1_1Vortex__Lattice-members.html deleted file mode 100644 index df61ed77..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Vortex__Lattice_1_1Vortex__Lattice-members.html +++ /dev/null @@ -1,131 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
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- -
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SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice Member List
-
-
- -

This is the complete list of members for SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice, including all inherited members.

- - - - - - - - - - - - - - - - - - - - -
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice
build_surrogate(self)SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice
compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
compute_forces(self, conditions)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
evaluate(self, state, settings, geometry)SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice
SUAVE::Analyses::Aerodynamics::Aerodynamics::Aerodynamics.evaluate(self, state)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
geometry (defined in SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice)SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice
initialize(self)SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice
SUAVE::Analyses::Aerodynamics::Aerodynamics::Aerodynamics.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
sample_training(self)SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice
settings (defined in SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice)SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice
surrogates (defined in SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice)SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice
tag (defined in SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice)SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice
training (defined in SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice)SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Vortex__Lattice_1_1Vortex__Lattice.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Vortex__Lattice_1_1Vortex__Lattice.html deleted file mode 100644 index 292f0b0b..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Vortex__Lattice_1_1Vortex__Lattice.html +++ /dev/null @@ -1,421 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice Class Reference
-
-
-
-Inheritance diagram for SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice:
-
-
- - -SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics -SUAVE.Analyses.Analysis.Analysis - -
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def initialize (self)
 
def evaluate (self, state, settings, geometry)
 
def sample_training (self)
 
def build_surrogate (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
def __defaults__ (self)
 
def evaluate (self, state)
 
def finalize (self)
 
def compute_forces (self, conditions)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

tag
 
geometry
 
settings
 
training
 
surrogates
 
- Public Attributes inherited from SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
tag
 
geometry
 
settings
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
This builds a surrogate and computes lift using a basic vortex lattice.
-
-Assumptions:
-None
-
-Source:
-None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice.__defaults__ ( self)
-
-
This sets the default values and methods for the analysis.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
-
- -

◆ build_surrogate()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice.build_surrogate ( self)
-
-
Build a surrogate using sample evaluation results.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-see properties used
-
-Outputs:
-self.surrogates.
-  lift_coefficient       <np.poly1d>
-  wing_lift_coefficients <np.poly1d> (multiple surrogates)
-
-Properties Used:
-self.
-  training.
-    angle_of_attack        [radians]
-    lift_coefficient       [-]
-    wing_lift_coefficients [-] (wing specific)
-
-
-
- -

◆ evaluate()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice.evaluate ( self,
 state,
 settings,
 geometry 
)
-
-
Evaluates lift and drag using available surrogates.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-state.conditions.
-  freestream.dynamics_pressure       [-]
-  angle_of_attack                    [radians]
-
-Outputs:
-conditions.aerodynamics.lift_breakdown.
-  inviscid_wings_lift[wings.*.tag]   [-] CL (wing specific)
-  inviscid_wings_lift.total          [-] CL
-conditions.aerodynamics.
-  lift_coefficient_wing              [-] CL (wing specific)
-inviscid_wings_lift                  [-] CL
-
-Properties Used:
-self.surrogates.
-  lift_coefficient                   [-] CL
-  wing_lift_coefficient[wings.*.tag] [-] CL (wing specific)
-
-
-
- -

◆ initialize()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice.initialize ( self)
-
-
Drives functions to get training samples and build a surrogate.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-None
-
-
-
- -

◆ sample_training()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice.sample_training ( self)
-
-
Call methods to run vortex lattice for sample point evaluation.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-see properties used
-
-Outputs:
-self.training.
-  lift_coefficient            [-] 
-  wing_lift_coefficients      [-] (wing specific)
-
-Properties Used:
-self.geometry.wings.*.tag
-self.settings                 (passed to calculate vortex lattice)
-self.training.angle_of_attack [radians]
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Aerodynamics/Vortex_Lattice.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Vortex__Lattice_1_1Vortex__Lattice.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Vortex__Lattice_1_1Vortex__Lattice.js deleted file mode 100644 index d0e1fbc1..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Vortex__Lattice_1_1Vortex__Lattice.js +++ /dev/null @@ -1,13 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Vortex__Lattice_1_1Vortex__Lattice = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Vortex__Lattice_1_1Vortex__Lattice.html#a626460308767892310bb8ec904f3d3b9", null ], - [ "build_surrogate", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Vortex__Lattice_1_1Vortex__Lattice.html#a707b374ab283c62f6f1d4fe917854875", null ], - [ "evaluate", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Vortex__Lattice_1_1Vortex__Lattice.html#a655b0e93dd39403e711bc83c054cfef2", null ], - [ "initialize", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Vortex__Lattice_1_1Vortex__Lattice.html#ad5c19cbcf11eb96e5e5a5d3273784076", null ], - [ "sample_training", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Vortex__Lattice_1_1Vortex__Lattice.html#aa7a6045fc661f688b4aad3bf9e426950", null ], - [ "geometry", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Vortex__Lattice_1_1Vortex__Lattice.html#a070b444364458c846683fb0870d4fd40", null ], - [ "settings", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Vortex__Lattice_1_1Vortex__Lattice.html#a8bea7e1ceb61e329dadd4e96a2999d91", null ], - [ "surrogates", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Vortex__Lattice_1_1Vortex__Lattice.html#a2f3f00161e75df559ec9a6a1d8bdf4d4", null ], - [ "tag", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Vortex__Lattice_1_1Vortex__Lattice.html#adb9e4b35657faa29fb812ae901d4a937", null ], - [ "training", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Vortex__Lattice_1_1Vortex__Lattice.html#a4cf185a79623d40e09fe08f6a474aaaf", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Vortex__Lattice_1_1Vortex__Lattice.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Vortex__Lattice_1_1Vortex__Lattice.png deleted file mode 100644 index d7b5e779..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Vortex__Lattice_1_1Vortex__Lattice.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Analysis_1_1Analysis-members.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Analysis_1_1Analysis-members.html deleted file mode 100644 index f921fe62..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Analysis_1_1Analysis-members.html +++ /dev/null @@ -1,121 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Analysis.Analysis Member List
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Analysis_1_1Analysis.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Analysis_1_1Analysis.html deleted file mode 100644 index 81eb0a72..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Analysis_1_1Analysis.html +++ /dev/null @@ -1,457 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Analysis.Analysis Class Reference - - - - - - - - - - - - - - - -
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- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Analysis.Analysis Class Reference
-
-
-
-Inheritance diagram for SUAVE.Analyses.Analysis.Analysis:
-
-
- - -SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics -SUAVE.Analyses.Atmospheric.Atmospheric.Atmospheric -SUAVE.Analyses.Costs.Costs.Costs -SUAVE.Analyses.Energy.Energy.Energy -SUAVE.Analyses.Geometry.Geometry.Geometry -SUAVE.Analyses.Loads.Loads.Loads -SUAVE.Analyses.Mission.Segments.Segment.Segment -SUAVE.Analyses.Noise.Noise.Noise -SUAVE.Analyses.Planets.Planet.Planet -SUAVE.Analyses.Sizing.Sizing.Sizing -SUAVE.Analyses.Stability.Stability.Stability -SUAVE.Analyses.Structures.Structures.Structures -SUAVE.Analyses.Surrogate.Surrogate -SUAVE.Analyses.Weights.Weights.Weights - -
- - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - -

-Public Attributes

tag
 
features
 
settings
 
-

Detailed Description

-
SUAVE.Analyses.Analysis()
-
-    The Top Level Analysis Class
-    
-        Assumptions:
-        None
-        
-        Source:
-        N/A
-

Member Function Documentation

- -

◆ __call__()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Analyses.Analysis.Analysis.__call__ ( self,
 args,
 kwarg 
)
-
-
This is used to set the class' call behavior to the evaluate function.
-        
-Assumptions:
-None
-        
-Source:
-N/A
-        
-Inputs:
-None
-        
-Outputs:
-None
-        
-Properties Used:
-N/A
-
-
- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Analysis.Analysis.__defaults__ ( self)
-
-
This sets the default values and methods for the analysis.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
- -

◆ compile()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Analyses.Analysis.Analysis.compile ( self,
 args,
 kwarg 
)
-
-
This is used to compile the data, settings, etc. used in the
-   analysis' specific algorithms.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
- -

◆ evaluate()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Analyses.Analysis.Analysis.evaluate ( self,
 args,
 kwarg 
)
-
-
This is used to execute the analysis' specific algorithms.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
- -

◆ finalize()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Analyses.Analysis.Analysis.finalize ( self,
 args,
 kwarg 
)
-
-
This is used to finalize the analysis' specific algorithms.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
- -

◆ initialize()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Analyses.Analysis.Analysis.initialize ( self,
 args,
 kwarg 
)
-
-
This is used to initialize the analysis' specific algorithms.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Analysis.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Analysis_1_1Analysis.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Analysis_1_1Analysis.js deleted file mode 100644 index 792694b1..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Analysis_1_1Analysis.js +++ /dev/null @@ -1,12 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Analysis_1_1Analysis = -[ - [ "__call__", "classSUAVE_1_1Analyses_1_1Analysis_1_1Analysis.html#afeeaf88c2424003602f1a4c0503ed4fd", null ], - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Analysis_1_1Analysis.html#ab23ae346b8d6ad343384bc9b0f3bb712", null ], - [ "compile", "classSUAVE_1_1Analyses_1_1Analysis_1_1Analysis.html#ae1183f13918b2bdcb0bf6d0aa94ef4f8", null ], - [ "evaluate", "classSUAVE_1_1Analyses_1_1Analysis_1_1Analysis.html#a0c950af6a4ce899d2a29fccef38f47d7", null ], - [ "finalize", "classSUAVE_1_1Analyses_1_1Analysis_1_1Analysis.html#a070b60f6b134baf09c60583901c5176a", null ], - [ "initialize", "classSUAVE_1_1Analyses_1_1Analysis_1_1Analysis.html#a460a311d6ac29134ff52b7bec21b13f5", null ], - [ "features", "classSUAVE_1_1Analyses_1_1Analysis_1_1Analysis.html#ad4391599de0c0ccb845a5eb4c31a7247", null ], - [ "settings", "classSUAVE_1_1Analyses_1_1Analysis_1_1Analysis.html#aec47523bf171175d934cdbbb23e53327", null ], - [ "tag", "classSUAVE_1_1Analyses_1_1Analysis_1_1Analysis.html#ad2dbbc94e7f1e2518410e2f8a1ea5af3", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Analysis_1_1Analysis.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Analysis_1_1Analysis.png deleted file mode 100644 index 2d01b9f3..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Analysis_1_1Analysis.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Analysis_1_1Container-members.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Analysis_1_1Container-members.html deleted file mode 100644 index 0f2e7916..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Analysis_1_1Container-members.html +++ /dev/null @@ -1,117 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Analysis.Container Member List
-
-
- -

This is the complete list of members for SUAVE.Analyses.Analysis.Container, including all inherited members.

- - - - - - -
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Container
compile(self, args, kwarg)SUAVE.Analyses.Analysis.Container
evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Container
finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Container
initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Container
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Analysis_1_1Container.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Analysis_1_1Container.html deleted file mode 100644 index 8b5838bc..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Analysis_1_1Container.html +++ /dev/null @@ -1,399 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Analysis.Container Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
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- -
-
SUAVE.Analyses.Analysis.Container Class Reference
-
-
-
-Inheritance diagram for SUAVE.Analyses.Analysis.Container:
-
-
- - -SUAVE.Analyses.Vehicle.Vehicle - -
- - - - - - - - - - - - -

-Public Member Functions

def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
-

Detailed Description

-
SUAVE.Analyses.Analysis.Container()
-
-    The Analysis Container Class
-    
-        Assumptions:
-        None
-        
-        Source:
-        N/A
-

Member Function Documentation

- -

◆ __call__()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Analyses.Analysis.Container.__call__ ( self,
 args,
 kwarg 
)
-
-
This is used to set the class' call behavior to the evaluate functions.
-                                        
-Assumptions:
-None
-                                        
-Source:
-N/A
-                                        
-Inputs:
-None
-                                        
-Outputs:
-None
-                                        
-Properties Used:
-N/A
-
-
- -

◆ compile()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Analyses.Analysis.Container.compile ( self,
 args,
 kwarg 
)
-
-
This is used to execute the compile functions of the analyses
-   stored in the container.
-                
-Assumptions:
-None
-                
-Source:
-N/A
-                
-Inputs:
-None
-                
-Outputs:
-None
-                
-Properties Used:
-N/A
-
-
- -

◆ evaluate()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Analyses.Analysis.Container.evaluate ( self,
 args,
 kwarg 
)
-
-
This is used to execute the evaluate functions of the analyses
-    stored in the container.
-                                
-Assumptions:
-None
-                                
-Source:
-N/A
-                                
-Inputs:
-None
-                                
-Outputs:
-Results of the Evaluate Functions
-                                
-Properties Used:
-N/A
-
-
- -

◆ finalize()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Analyses.Analysis.Container.finalize ( self,
 args,
 kwarg 
)
-
-
This is used to execute the finalize functions of the analyses
-    stored in the container.
-                                
-Assumptions:
-None
-                                
-Source:
-N/A
-                                
-Inputs:
-None
-                                
-Outputs:
-None
-                                
-Properties Used:
-N/A
-
-
- -

◆ initialize()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Analyses.Analysis.Container.initialize ( self,
 args,
 kwarg 
)
-
-
This is used to execute the initialize functions of the analyses
-    stored in the container.
-                        
-Assumptions:
-None
-                        
-Source:
-N/A
-                        
-Inputs:
-None
-                        
-Outputs:
-None
-                        
-Properties Used:
-N/A
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Analysis.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Analysis_1_1Container.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Analysis_1_1Container.js deleted file mode 100644 index 6b66b67a..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Analysis_1_1Container.js +++ /dev/null @@ -1,8 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Analysis_1_1Container = -[ - [ "__call__", "classSUAVE_1_1Analyses_1_1Analysis_1_1Container.html#a7882a6fa0c914c5e89206af1c9a91052", null ], - [ "compile", "classSUAVE_1_1Analyses_1_1Analysis_1_1Container.html#a9f2fedb5cf37d61979893a6cde2f2642", null ], - [ "evaluate", "classSUAVE_1_1Analyses_1_1Analysis_1_1Container.html#ada471c993860c5f8301461e92a626dbd", null ], - [ "finalize", "classSUAVE_1_1Analyses_1_1Analysis_1_1Container.html#a83403e3f9b2b827c152ab0700f568405", null ], - [ "initialize", "classSUAVE_1_1Analyses_1_1Analysis_1_1Container.html#a775721af25dbdc38938223151f1370ad", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Analysis_1_1Container.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Analysis_1_1Container.png deleted file mode 100644 index cf42bb10..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Analysis_1_1Container.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Atmospheric_1_1Atmospheric_1_1Atmospheric-members.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Atmospheric_1_1Atmospheric_1_1Atmospheric-members.html deleted file mode 100644 index a66ac428..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Atmospheric_1_1Atmospheric_1_1Atmospheric-members.html +++ /dev/null @@ -1,122 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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- - - - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Atmospheric_1_1Atmospheric_1_1Atmospheric.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Atmospheric_1_1Atmospheric_1_1Atmospheric.html deleted file mode 100644 index 0a3a914c..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Atmospheric_1_1Atmospheric_1_1Atmospheric.html +++ /dev/null @@ -1,233 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Atmospheric.Atmospheric.Atmospheric Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Atmospheric.Atmospheric.Atmospheric Class Reference
-
-
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-Inheritance diagram for SUAVE.Analyses.Atmospheric.Atmospheric.Atmospheric:
-
-
- - -SUAVE.Analyses.Analysis.Analysis -SUAVE.Analyses.Atmospheric.Constant_Temperature.Constant_Temperature -SUAVE.Analyses.Atmospheric.US_Standard_1976.US_Standard_1976 - -
- - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def compute_values (self, altitude)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - -

-Additional Inherited Members

- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
This is the base class for atmospheric analyses. It contains functions
-that are built into the default class.
-
-Assumptions:
-None
-
-Source:
-N/A
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Atmospheric.Atmospheric.Atmospheric.__defaults__ ( self)
-
-
This sets the default values for the analysis to function.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
-
- -

◆ compute_values()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Analyses.Atmospheric.Atmospheric.Atmospheric.compute_values ( self,
 altitude 
)
-
-
This function is not implemented for the base class.
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Atmospheric/Atmospheric.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Atmospheric_1_1Atmospheric_1_1Atmospheric.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Atmospheric_1_1Atmospheric_1_1Atmospheric.js deleted file mode 100644 index 3439d803..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Atmospheric_1_1Atmospheric_1_1Atmospheric.js +++ /dev/null @@ -1,5 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Atmospheric_1_1Atmospheric_1_1Atmospheric = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Atmospheric_1_1Atmospheric_1_1Atmospheric.html#ad01a85ef670cb6e9b42085e4b6fe2f59", null ], - [ "compute_values", "classSUAVE_1_1Analyses_1_1Atmospheric_1_1Atmospheric_1_1Atmospheric.html#a91a4ddf63cf6d7d8d0680063932df489", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Atmospheric_1_1Atmospheric_1_1Atmospheric.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Atmospheric_1_1Atmospheric_1_1Atmospheric.png deleted file mode 100644 index 72bb9216..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Atmospheric_1_1Atmospheric_1_1Atmospheric.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Atmospheric_1_1Constant__Temperature_1_1Constant__Temperature-members.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Atmospheric_1_1Constant__Temperature_1_1Constant__Temperature-members.html deleted file mode 100644 index 8c44b0a0..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Atmospheric_1_1Constant__Temperature_1_1Constant__Temperature-members.html +++ /dev/null @@ -1,123 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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- - - - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Atmospheric_1_1Constant__Temperature_1_1Constant__Temperature.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Atmospheric_1_1Constant__Temperature_1_1Constant__Temperature.html deleted file mode 100644 index e9624a4f..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Atmospheric_1_1Constant__Temperature_1_1Constant__Temperature.html +++ /dev/null @@ -1,269 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Atmospheric.Constant_Temperature.Constant_Temperature Class Reference - - - - - - - - - - - - - - - -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Atmospheric.Constant_Temperature.Constant_Temperature Class Reference
-
-
-
-Inheritance diagram for SUAVE.Analyses.Atmospheric.Constant_Temperature.Constant_Temperature:
-
-
- - -SUAVE.Analyses.Atmospheric.Atmospheric.Atmospheric -SUAVE.Analyses.Analysis.Analysis - -
- - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def compute_values (self, altitude, temperature=288.15)
 
- Public Member Functions inherited from SUAVE.Analyses.Atmospheric.Atmospheric.Atmospheric
def __defaults__ (self)
 
def compute_values (self, altitude)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - -

-Additional Inherited Members

- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
Implements a constant temperature with U.S. Standard Atmosphere (1976 version) freestream pressure
-    
-Assumptions:
-None
-
-Source:
-U.S. Standard Atmosphere, 1976, U.S. Government Printing Office, Washington, D.C., 1976
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Atmospheric.Constant_Temperature.Constant_Temperature.__defaults__ ( self)
-
-
This sets the default values for the analysis to function.
-    
-Assumptions:
-None
-    
-Source:
-N/A
-    
-Inputs:
-None
-    
-Outputs:
-None
-    
-Properties Used:
-None
-
-
-
- -

◆ compute_values()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Analyses.Atmospheric.Constant_Temperature.Constant_Temperature.compute_values ( self,
 altitude,
 temperature = 288.15 
)
-
-
Computes atmospheric values.
-    
-Assumptions:
-Constant temperature atmosphere
-    
-Source:
-U.S. Standard Atmosphere, 1976, U.S. Government Printing Office, Washington, D.C., 1976
-    
-Inputs:
-altitude                                 [m]
-temperature                              [K]
-
-Outputs:
-atmo_data.
-  pressure                               [Pa]
-  temperature                            [K]
-  speed_of_sound                         [m/s]
-  dynamic_viscosity                      [kg/(m*s)]
-    
-Properties Used:
-self.
-  fluid_properties.gas_specific_constant [J/(kg*K)]
-  planet.sea_level_gravity               [m/s^2]
-  planet.mean_radius                     [m]
-  breaks.
-    altitude                             [m]
-    pressure                             [Pa]
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Atmospheric/Constant_Temperature.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Atmospheric_1_1Constant__Temperature_1_1Constant__Temperature.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Atmospheric_1_1Constant__Temperature_1_1Constant__Temperature.js deleted file mode 100644 index f4e4975a..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Atmospheric_1_1Constant__Temperature_1_1Constant__Temperature.js +++ /dev/null @@ -1,5 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Atmospheric_1_1Constant__Temperature_1_1Constant__Temperature = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Atmospheric_1_1Constant__Temperature_1_1Constant__Temperature.html#a003bc28ecb9085a464a80b33413f57bb", null ], - [ "compute_values", "classSUAVE_1_1Analyses_1_1Atmospheric_1_1Constant__Temperature_1_1Constant__Temperature.html#afb1d8419d7e0d5b406cb3c483d3323ea", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Atmospheric_1_1Constant__Temperature_1_1Constant__Temperature.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Atmospheric_1_1Constant__Temperature_1_1Constant__Temperature.png deleted file mode 100644 index 0dcff014..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Atmospheric_1_1Constant__Temperature_1_1Constant__Temperature.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Atmospheric_1_1US__Standard__1976_1_1US__Standard__1976-members.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Atmospheric_1_1US__Standard__1976_1_1US__Standard__1976-members.html deleted file mode 100644 index 6a343507..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Atmospheric_1_1US__Standard__1976_1_1US__Standard__1976-members.html +++ /dev/null @@ -1,123 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Atmospheric.US_Standard_1976.US_Standard_1976 Class Reference
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-Inheritance diagram for SUAVE.Analyses.Atmospheric.US_Standard_1976.US_Standard_1976:
-
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- - -SUAVE.Analyses.Atmospheric.Atmospheric.Atmospheric -SUAVE.Analyses.Analysis.Analysis - -
- - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def compute_values (self, altitude, temperature_deviation=0.0)
 
- Public Member Functions inherited from SUAVE.Analyses.Atmospheric.Atmospheric.Atmospheric
def __defaults__ (self)
 
def compute_values (self, altitude)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - -

-Additional Inherited Members

- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
Implements the U.S. Standard Atmosphere (1976 version)
-    
-Assumptions:
-None
-
-Source:
-U.S. Standard Atmosphere, 1976, U.S. Government Printing Office, Washington, D.C., 1976
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Atmospheric.US_Standard_1976.US_Standard_1976.__defaults__ ( self)
-
-
This sets the default values for the analysis to function.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Output:
-None
-
-Properties Used:
-None
-
-
-
- -

◆ compute_values()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Analyses.Atmospheric.US_Standard_1976.US_Standard_1976.compute_values ( self,
 altitude,
 temperature_deviation = 0.0 
)
-
-
Computes atmospheric values.
-
-Assumptions:
-US 1976 Standard Atmosphere
-
-Source:
-U.S. Standard Atmosphere, 1976, U.S. Government Printing Office, Washington, D.C., 1976
-
-Inputs:
-altitude                                 [m]
-temperature_deviation                    [K]
-
-Output:
-atmo_data.
-  pressure                               [Pa]
-  temperature                            [K]
-  speed_of_sound                         [m/s]
-  dynamic_viscosity                      [kg/(m*s)]
-
-Properties Used:
-self.
-  fluid_properties.gas_specific_constant [J/(kg*K)]
-  planet.sea_level_gravity               [m/s^2]
-  planet.mean_radius                     [m]
-  breaks.
-    altitude                             [m]
-    temperature                          [K]
-    pressure                             [Pa]
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Atmospheric/US_Standard_1976.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Atmospheric_1_1US__Standard__1976_1_1US__Standard__1976.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Atmospheric_1_1US__Standard__1976_1_1US__Standard__1976.js deleted file mode 100644 index ece755c2..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Atmospheric_1_1US__Standard__1976_1_1US__Standard__1976.js +++ /dev/null @@ -1,5 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Atmospheric_1_1US__Standard__1976_1_1US__Standard__1976 = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Atmospheric_1_1US__Standard__1976_1_1US__Standard__1976.html#a892125fc4febc126454d2f8fd2cd03f3", null ], - [ "compute_values", "classSUAVE_1_1Analyses_1_1Atmospheric_1_1US__Standard__1976_1_1US__Standard__1976.html#a201642664bd47167c2283e5fea997599", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Atmospheric_1_1US__Standard__1976_1_1US__Standard__1976.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Atmospheric_1_1US__Standard__1976_1_1US__Standard__1976.png deleted file mode 100644 index 6577cae3..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Atmospheric_1_1US__Standard__1976_1_1US__Standard__1976.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Costs_1_1Costs_1_1Costs-members.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Costs_1_1Costs_1_1Costs-members.html deleted file mode 100644 index 9139a83b..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Costs_1_1Costs_1_1Costs-members.html +++ /dev/null @@ -1,123 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
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- - - -
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- - - - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Costs_1_1Costs_1_1Costs.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Costs_1_1Costs_1_1Costs.html deleted file mode 100644 index ec7c8876..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Costs_1_1Costs_1_1Costs.html +++ /dev/null @@ -1,260 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Costs.Costs.Costs Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
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- -
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- -
- -
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- - -
- -
- -
- -
-
SUAVE.Analyses.Costs.Costs.Costs Class Reference
-
-
-
-Inheritance diagram for SUAVE.Analyses.Costs.Costs.Costs:
-
-
- - -SUAVE.Analyses.Analysis.Analysis - -
- - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def evaluate (self, conditions=None)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - -

-Public Attributes

tag
 
vehicle
 
settings
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
This is the base class for cost analyses. It contains functions
-that are built into the default class.
-
-Assumptions:
-None
-
-Source:
-N/A
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Costs.Costs.Costs.__defaults__ ( self)
-
-
This sets the default values for the analysis to function.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
-
- -

◆ evaluate()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Analyses.Costs.Costs.Costs.evaluate ( self,
 conditions = None 
)
-
-
This sets the default evaluation method for costs.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None used
-
-Outputs:
-None
-
-Properties Used:
-self.
-  vehicle                           SUAVE vehicle passed to the functions below
-  settings.industrial_costs_method  (function)
-  settings.operating_costs_method   (function)
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Costs/Costs.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Costs_1_1Costs_1_1Costs.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Costs_1_1Costs_1_1Costs.js deleted file mode 100644 index dbacec82..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Costs_1_1Costs_1_1Costs.js +++ /dev/null @@ -1,8 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Costs_1_1Costs_1_1Costs = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Costs_1_1Costs_1_1Costs.html#ad91474a13ce4efb179f56adc31c11f08", null ], - [ "evaluate", "classSUAVE_1_1Analyses_1_1Costs_1_1Costs_1_1Costs.html#a66ae6b57304d50de0c02a26a3972aa0a", null ], - [ "settings", "classSUAVE_1_1Analyses_1_1Costs_1_1Costs_1_1Costs.html#a302c338b92e815a2357ebed79234a5e5", null ], - [ "tag", "classSUAVE_1_1Analyses_1_1Costs_1_1Costs_1_1Costs.html#a20276a66368aa76ce9c8c16cf2fe1281", null ], - [ "vehicle", "classSUAVE_1_1Analyses_1_1Costs_1_1Costs_1_1Costs.html#aa62e994477273c9ab00c1d4c97916a98", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Costs_1_1Costs_1_1Costs.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Costs_1_1Costs_1_1Costs.png deleted file mode 100644 index 279e7ee0..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Costs_1_1Costs_1_1Costs.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Energy_1_1Energy_1_1Energy-members.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Energy_1_1Energy_1_1Energy-members.html deleted file mode 100644 index cdb57aa3..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Energy_1_1Energy_1_1Energy-members.html +++ /dev/null @@ -1,123 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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- - - - - - -
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- - - - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Energy_1_1Energy_1_1Energy.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Energy_1_1Energy_1_1Energy.html deleted file mode 100644 index a322c74e..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Energy_1_1Energy_1_1Energy.html +++ /dev/null @@ -1,246 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Energy.Energy.Energy Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
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SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
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-
-
- - - -
-
- -
-
-
- -
- -
-
- - -
- -
- -
- -
-
SUAVE.Analyses.Energy.Energy.Energy Class Reference
-
-
-
-Inheritance diagram for SUAVE.Analyses.Energy.Energy.Energy:
-
-
- - -SUAVE.Analyses.Analysis.Analysis - -
- - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def evaluate_thrust (self, state)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - -

-Public Attributes

tag
 
network
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
SUAVE.Analyses.Energy.Energy()
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Energy.Energy.Energy.__defaults__ ( self)
-
-
This sets the default values and methods for the analysis.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    N/A
-
-
-
- -

◆ evaluate_thrust()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Analyses.Energy.Energy.Energy.evaluate_thrust ( self,
 state 
)
-
-
Evaluate the thrust produced by the energy network.
-    
-Assumptions:
-Network has an "evaluate_thrust" method.
-    
-Source:
-N/A
-    
-Inputs:
-State data container
-    
-Outputs:
-Results of the thrust evaluation method.
-    
-Properties Used:
-N/A                
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Energy/Energy.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Energy_1_1Energy_1_1Energy.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Energy_1_1Energy_1_1Energy.js deleted file mode 100644 index 1264bc61..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Energy_1_1Energy_1_1Energy.js +++ /dev/null @@ -1,7 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Energy_1_1Energy_1_1Energy = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Energy_1_1Energy_1_1Energy.html#af38553b98394e44c50fbc5d718e324ac", null ], - [ "evaluate_thrust", "classSUAVE_1_1Analyses_1_1Energy_1_1Energy_1_1Energy.html#a3958ad6182afff9a0438a7976e13c3ed", null ], - [ "network", "classSUAVE_1_1Analyses_1_1Energy_1_1Energy_1_1Energy.html#abfba7d105cfe5daa8ef1fa18d0db348c", null ], - [ "tag", "classSUAVE_1_1Analyses_1_1Energy_1_1Energy_1_1Energy.html#a72fe01cf84cb1f29c4a0f6afe08aea95", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Energy_1_1Energy_1_1Energy.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Energy_1_1Energy_1_1Energy.png deleted file mode 100644 index aaadcf21..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Energy_1_1Energy_1_1Energy.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Geometry_1_1Geometry_1_1Geometry-members.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Geometry_1_1Geometry_1_1Geometry-members.html deleted file mode 100644 index 6999a80a..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Geometry_1_1Geometry_1_1Geometry-members.html +++ /dev/null @@ -1,122 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
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- - - -
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- - - - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Geometry_1_1Geometry_1_1Geometry.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Geometry_1_1Geometry_1_1Geometry.html deleted file mode 100644 index ca66868e..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Geometry_1_1Geometry_1_1Geometry.html +++ /dev/null @@ -1,263 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Geometry.Geometry.Geometry Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
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-
- -
- -
-
- - -
- -
- -
- -
-
SUAVE.Analyses.Geometry.Geometry.Geometry Class Reference
-
-
-
-Inheritance diagram for SUAVE.Analyses.Geometry.Geometry.Geometry:
-
-
- - -SUAVE.Analyses.Analysis.Analysis - -
- - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def evaluate (self, condtitions)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - -

-Public Attributes

tag
 
features
 
settings
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
This class defines the geometry data structure of an aircraft in SUAVE
-
-Assumptions:
-    None
-
-Source:
-    N/A
-
-Inputs:
-    None
-    
-Outputs:
-    None
-
-Properties Used:
-     N/A
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Geometry.Geometry.Geometry.__defaults__ ( self)
-
-
This sets the default values and methods for the analysis.
-    
-Assumptions:
-None
-    
-Source:
-N/A
-    
-Inputs:
-None
-    
-Outputs:
-None
-    
-Properties Used:
-N/A
-
-
- -

◆ evaluate()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Analyses.Geometry.Geometry.Geometry.evaluate ( self,
 condtitions 
)
-
-
Evaluate the Geometry analysis.
-    
-Assumptions:
-None
-    
-Source:
-N/A
-    
-Inputs:
-None
-    
-Outputs:
-Results of the Geometry Analysis
-    
-Properties Used:
-N/A                
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Geometry/Geometry.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Geometry_1_1Geometry_1_1Geometry.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Geometry_1_1Geometry_1_1Geometry.js deleted file mode 100644 index 19129616..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Geometry_1_1Geometry_1_1Geometry.js +++ /dev/null @@ -1,8 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Geometry_1_1Geometry_1_1Geometry = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Geometry_1_1Geometry_1_1Geometry.html#a1a40c89afab7d7ffe8d4285404f8abe1", null ], - [ "evaluate", "classSUAVE_1_1Analyses_1_1Geometry_1_1Geometry_1_1Geometry.html#a99ed99c2c0e6b8b2238cd146e757a901", null ], - [ "features", "classSUAVE_1_1Analyses_1_1Geometry_1_1Geometry_1_1Geometry.html#ae56f32a3e01434eb2015b785d05161f9", null ], - [ "settings", "classSUAVE_1_1Analyses_1_1Geometry_1_1Geometry_1_1Geometry.html#af0bdc7654e079d4a1cf5f999463c0dd9", null ], - [ "tag", "classSUAVE_1_1Analyses_1_1Geometry_1_1Geometry_1_1Geometry.html#af366e60e7e3c21cafbfd7121bc6d14a7", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Geometry_1_1Geometry_1_1Geometry.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Geometry_1_1Geometry_1_1Geometry.png deleted file mode 100644 index 1c2c2b6d..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Geometry_1_1Geometry_1_1Geometry.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Loads_1_1Loads_1_1Loads-members.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Loads_1_1Loads_1_1Loads-members.html deleted file mode 100644 index 08c56869..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Loads_1_1Loads_1_1Loads-members.html +++ /dev/null @@ -1,122 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
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-
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Loads.Loads.Loads Class Reference
-
-
-
-Inheritance diagram for SUAVE.Analyses.Loads.Loads.Loads:
-
-
- - -SUAVE.Analyses.Analysis.Analysis - -
- - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def evaluate (self, condtitions)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - -

-Public Attributes

tag
 
features
 
settings
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
SUAVE.Analyses.Loads.Loads()
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Loads.Loads.Loads.__defaults__ ( self)
-
-
This sets the default values and methods for the analysis.
-    
-Assumptions:
-None
-    
-Source:
-N/A
-    
-Inputs:
-None
-    
-Outputs:
-None
-    
-Properties Used:
-N/A
-
-
- -

◆ evaluate()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Analyses.Loads.Loads.Loads.evaluate ( self,
 condtitions 
)
-
-
Evaluate the Loads analysis.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-Results of the Loads Analysis
-
-Properties Used:
-N/A                
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Loads/Loads.py
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Loads_1_1Loads_1_1Loads.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Loads_1_1Loads_1_1Loads.js deleted file mode 100644 index 1ce9891a..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Loads_1_1Loads_1_1Loads.js +++ /dev/null @@ -1,8 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Loads_1_1Loads_1_1Loads = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Loads_1_1Loads_1_1Loads.html#af04f84783a1e7fcdbf586a62ba1594fa", null ], - [ "evaluate", "classSUAVE_1_1Analyses_1_1Loads_1_1Loads_1_1Loads.html#a53fd89d7710bec62997cddccadf4bc0d", null ], - [ "features", "classSUAVE_1_1Analyses_1_1Loads_1_1Loads_1_1Loads.html#a916c9fe322cb2fab9aa523f359b5d50f", null ], - [ "settings", "classSUAVE_1_1Analyses_1_1Loads_1_1Loads_1_1Loads.html#a62d27d9a4b737eb28fd3dea7daf0b031", null ], - [ "tag", "classSUAVE_1_1Analyses_1_1Loads_1_1Loads_1_1Loads.html#a3f369a27818738ee1f515f717ccc47e0", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Loads_1_1Loads_1_1Loads.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Loads_1_1Loads_1_1Loads.png deleted file mode 100644 index 10a4f9d1..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Loads_1_1Loads_1_1Loads.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1All__At__Once_1_1All__At__Once-members.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1All__At__Once_1_1All__At__Once-members.html deleted file mode 100644 index 8cffc7a2..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1All__At__Once_1_1All__At__Once-members.html +++ /dev/null @@ -1,133 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.All_At_Once.All_At_Once Member List
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This is the complete list of members for SUAVE.Analyses.Mission.All_At_Once.All_At_Once, including all inherited members.

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__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.All_At_Once.All_At_Once
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
append_segment(self, segment)SUAVE.Analyses.Mission.Segments.Segment.Container
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self)SUAVE.Analyses.Mission.All_At_Once.All_At_Once
SUAVE::Analyses::Mission::Segments::Simple::Container.finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
segments (defined in SUAVE.Analyses.Mission.Segments.Segment.Container)SUAVE.Analyses.Mission.Segments.Segment.Container
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Container)SUAVE.Analyses.Mission.Segments.Segment.Container
tag (defined in SUAVE.Analyses.Mission.All_At_Once.All_At_Once)SUAVE.Analyses.Mission.All_At_Once.All_At_Once
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1All__At__Once_1_1All__At__Once.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1All__At__Once_1_1All__At__Once.html deleted file mode 100644 index 88551e9d..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1All__At__Once_1_1All__At__Once.html +++ /dev/null @@ -1,295 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Mission.All_At_Once.All_At_Once Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.All_At_Once.All_At_Once Class Reference
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-Inheritance diagram for SUAVE.Analyses.Mission.All_At_Once.All_At_Once:
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-
- - -SUAVE.Analyses.Mission.Mission.Mission -SUAVE.Analyses.Mission.Segments.Simple.Container -SUAVE.Analyses.Mission.Segments.Segment.Container -SUAVE.Analyses.Mission.Segments.Segment.Segment -SUAVE.Analyses.Analysis.Analysis -SUAVE.Analyses.Mission.Vary_Cruise.Given_Weight.Given_Weight - -
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-Public Member Functions

def __defaults__ (self)
 
def finalize (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Mission.Mission
def __defaults__ (self)
 
def finalize (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Container
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Container
def __defaults__ (self)
 
def append_segment (self, segment)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def evaluate (self, state=None)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

tag
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Mission.Mission
tag
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Segment.Container
segments
 
state
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
settings
 
state
 
analyses
 
process
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
Solves all segments and sub segments at once
-
-    Assumptions:
-    None
-    
-    Source:
-    None
-

Member Function Documentation

- -

◆ __defaults__()

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def SUAVE.Analyses.Mission.All_At_Once.All_At_Once.__defaults__ ( self)
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This sets the default values.
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◆ finalize()

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def SUAVE.Analyses.Mission.All_At_Once.All_At_Once.finalize ( self)
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Stub
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-    Inputs:
-    None
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-    Outputs:
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-    Properties Used:
-    None
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The documentation for this class was generated from the following file:
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  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Mission/All_At_Once.py
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1All__At__Once_1_1All__At__Once.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1All__At__Once_1_1All__At__Once.js deleted file mode 100644 index 253702bc..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1All__At__Once_1_1All__At__Once.js +++ /dev/null @@ -1,6 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Mission_1_1All__At__Once_1_1All__At__Once = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1All__At__Once_1_1All__At__Once.html#a93f2d5ac782f2073421efc1ab79d886a", null ], - [ "finalize", "classSUAVE_1_1Analyses_1_1Mission_1_1All__At__Once_1_1All__At__Once.html#aacc29c766be36ede3de1730b10fdbf8d", null ], - [ "tag", "classSUAVE_1_1Analyses_1_1Mission_1_1All__At__Once_1_1All__At__Once.html#aa125e8bef1c0992dd904500fcd1b4551", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1All__At__Once_1_1All__At__Once.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1All__At__Once_1_1All__At__Once.png deleted file mode 100644 index 2670c439..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1All__At__Once_1_1All__At__Once.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Mission_1_1Container-members.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Mission_1_1Container-members.html deleted file mode 100644 index 670b3982..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Mission_1_1Container-members.html +++ /dev/null @@ -1,114 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Mission.Container Member List
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This is the complete list of members for SUAVE.Analyses.Mission.Mission.Container, including all inherited members.

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evaluate(self, state=None)SUAVE.Analyses.Mission.Mission.Container
finalize(self)SUAVE.Analyses.Mission.Mission.Container
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Mission_1_1Container.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Mission_1_1Container.html deleted file mode 100644 index 3fc51e2c..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Mission_1_1Container.html +++ /dev/null @@ -1,218 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Mission.Mission.Container Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Mission.Container Class Reference
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-Inheritance diagram for SUAVE.Analyses.Mission.Mission.Container:
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-Public Member Functions

def evaluate (self, state=None)
 
def finalize (self)
 
-

Detailed Description

-
Container for mission
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-    Assumptions:
-    None
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Member Function Documentation

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◆ evaluate()

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def SUAVE.Analyses.Mission.Mission.Container.evaluate ( self,
 state = None 
)
-
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Go through the missions, run through them, save the results
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-    None
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-    Source:
-    N/A
-    
-    Inputs:
-    state   [Data()]
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-    Outputs:
-    Results [Results()]
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-    Properties Used:
-    None
-
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◆ finalize()

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def SUAVE.Analyses.Mission.Mission.Container.finalize ( self)
-
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Stub
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-    None
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-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Mission/Mission.py
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Mission_1_1Container.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Mission_1_1Container.js deleted file mode 100644 index d19f7d1f..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Mission_1_1Container.js +++ /dev/null @@ -1,5 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Mission_1_1Mission_1_1Container = -[ - [ "evaluate", "classSUAVE_1_1Analyses_1_1Mission_1_1Mission_1_1Container.html#ad7a0b7f2da3de16902f06def24106774", null ], - [ "finalize", "classSUAVE_1_1Analyses_1_1Mission_1_1Mission_1_1Container.html#a945c792da49a6a8b918866230e5f03b8", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Mission_1_1Container.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Mission_1_1Container.png deleted file mode 100644 index 9e77f9af..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Mission_1_1Container.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Mission_1_1Mission-members.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Mission_1_1Mission-members.html deleted file mode 100644 index 8ba242ac..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Mission_1_1Mission-members.html +++ /dev/null @@ -1,133 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Mission.Mission Member List
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This is the complete list of members for SUAVE.Analyses.Mission.Mission.Mission, including all inherited members.

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__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Mission.Mission
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
append_segment(self, segment)SUAVE.Analyses.Mission.Segments.Segment.Container
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self)SUAVE.Analyses.Mission.Mission.Mission
SUAVE::Analyses::Mission::Segments::Simple::Container.finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
segments (defined in SUAVE.Analyses.Mission.Segments.Segment.Container)SUAVE.Analyses.Mission.Segments.Segment.Container
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Container)SUAVE.Analyses.Mission.Segments.Segment.Container
tag (defined in SUAVE.Analyses.Mission.Mission.Mission)SUAVE.Analyses.Mission.Mission.Mission
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Mission_1_1Mission.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Mission_1_1Mission.html deleted file mode 100644 index 241e10a4..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Mission_1_1Mission.html +++ /dev/null @@ -1,289 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Mission.Mission.Mission Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Mission.Mission Class Reference
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-Inheritance diagram for SUAVE.Analyses.Mission.Mission.Mission:
-
-
- - -SUAVE.Analyses.Mission.Segments.Simple.Container -SUAVE.Analyses.Mission.Segments.Segment.Container -SUAVE.Analyses.Mission.Segments.Segment.Segment -SUAVE.Analyses.Analysis.Analysis -SUAVE.Analyses.Mission.All_At_Once.All_At_Once -SUAVE.Analyses.Mission.Sequential_Segments.Sequential_Segments -SUAVE.Analyses.Mission.Vary_Cruise.Given_Weight.Given_Weight - -
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-Public Member Functions

def __defaults__ (self)
 
def finalize (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Container
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Container
def __defaults__ (self)
 
def append_segment (self, segment)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def evaluate (self, state=None)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

tag
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Segment.Container
segments
 
state
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
settings
 
state
 
analyses
 
process
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
Mission.py: Top-level mission class
-
-    Assumptions:
-    None
-    
-    Source:
-    None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Mission.Mission.Mission.__defaults__ ( self)
-
-
This sets the default values.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
- -

◆ finalize()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Mission.Mission.Mission.finalize ( self)
-
-
Stub
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Mission/Mission.py
  • -
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Mission_1_1Mission.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Mission_1_1Mission.js deleted file mode 100644 index 936d568b..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Mission_1_1Mission.js +++ /dev/null @@ -1,6 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Mission_1_1Mission_1_1Mission = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Mission_1_1Mission.html#ace30292b5f307fb6d73c2c10eef6490e", null ], - [ "finalize", "classSUAVE_1_1Analyses_1_1Mission_1_1Mission_1_1Mission.html#ace7d605af81ba3c12251eb210fcb98de", null ], - [ "tag", "classSUAVE_1_1Analyses_1_1Mission_1_1Mission_1_1Mission.html#a1e771c09e76fa15bff511ddfe3b02232", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Mission_1_1Mission.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Mission_1_1Mission.png deleted file mode 100644 index df5eced0..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Mission_1_1Mission.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Aerodynamic_1_1Aerodynamic-members.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Aerodynamic_1_1Aerodynamic-members.html deleted file mode 100644 index 36f5aed3..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Aerodynamic_1_1Aerodynamic-members.html +++ /dev/null @@ -1,131 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic Member List
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This is the complete list of members for SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic, including all inherited members.

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__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Aerodynamic_1_1Aerodynamic.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Aerodynamic_1_1Aerodynamic.html deleted file mode 100644 index 77943320..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Aerodynamic_1_1Aerodynamic.html +++ /dev/null @@ -1,251 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic Class Reference
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-
-
-Inheritance diagram for SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic:
-
-
- - -SUAVE.Analyses.Mission.Segments.Simple.Simple -SUAVE.Analyses.Mission.Segments.Segment.Segment -SUAVE.Analyses.Analysis.Analysis -SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Linear_Altitude.Constant_Speed_Linear_Altitude -SUAVE.Analyses.Mission.Segments.Climb.Constant_Throttle_Constant_Speed.Constant_Throttle_Constant_Speed -SUAVE.Analyses.Mission.Segments.Climb.Optimized.Optimized -SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle -SUAVE.Analyses.Mission.Segments.Cruise.Constant_Acceleration_Constant_Altitude.Constant_Acceleration_Constant_Altitude -SUAVE.Analyses.Mission.Segments.Cruise.Constant_Pitch_Rate_Constant_Altitude.Constant_Pitch_Rate_Constant_Altitude -SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude -SUAVE.Analyses.Mission.Segments.Cruise.Constant_Throttle_Constant_Altitude.Constant_Throttle_Constant_Altitude -SUAVE.Analyses.Mission.Segments.Descent.Unknown_Throttle.Unknown_Throttle -SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground -SUAVE.Analyses.Mission.Segments.Hover.Hover.Hover -SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude.Set_Speed_Set_Altitude -SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Throttle.Set_Speed_Set_Throttle - -
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def evaluate (self, state=None)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - - - - - - -

-Public Attributes

temperature_deviation
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
settings
 
state
 
analyses
 
process
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
Thethird basic piece of a mission which each segment will expand upon
-
-    Assumptions:
-    There's a detailed process flow outline in defaults. A mission must be solved in that order.
-    Assumes you're an atmospheric vehicle.
-    
-    Source:
-    None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic.__defaults__ ( self)
-
-
This sets the default values.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Mission/Segments/Aerodynamic.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Aerodynamic_1_1Aerodynamic.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Aerodynamic_1_1Aerodynamic.js deleted file mode 100644 index f116bf32..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Aerodynamic_1_1Aerodynamic.js +++ /dev/null @@ -1,5 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Aerodynamic_1_1Aerodynamic = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Aerodynamic_1_1Aerodynamic.html#aed8adfea20e60c1456b6d163e6ad9279", null ], - [ "temperature_deviation", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Aerodynamic_1_1Aerodynamic.html#ae878a8247dcffc628bdaccf944b08aaf", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Aerodynamic_1_1Aerodynamic.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Aerodynamic_1_1Aerodynamic.png deleted file mode 100644 index 74815566..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Aerodynamic_1_1Aerodynamic.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_0c868b4d8a039afb6f97eb86309f635e.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_0c868b4d8a039afb6f97eb86309f635e.html deleted file mode 100644 index ca113842..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_0c868b4d8a039afb6f97eb86309f635e.html +++ /dev/null @@ -1,135 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Rate.Constant_Dynamic_Pressure_Constant_Rate Member List
-
-
- -

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Rate.Constant_Dynamic_Pressure_Constant_Rate, including all inherited members.

- - - - - - - - - - - - - - - - - - - - - - - - -
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Rate.Constant_Dynamic_Pressure_Constant_Rate
altitude_end (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Rate.Constant_Dynamic_Pressure_Constant_Rate)SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Rate.Constant_Dynamic_Pressure_Constant_Rate
altitude_start (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Rate.Constant_Dynamic_Pressure_Constant_Rate)SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Rate.Constant_Dynamic_Pressure_Constant_Rate
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
climb_rate (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Rate.Constant_Dynamic_Pressure_Constant_Rate)SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Rate.Constant_Dynamic_Pressure_Constant_Rate
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
dynamic_pressure (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Rate.Constant_Dynamic_Pressure_Constant_Rate)SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Rate.Constant_Dynamic_Pressure_Constant_Rate
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_1a3019722a97e8cea99fa0e052a34a68.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_1a3019722a97e8cea99fa0e052a34a68.html deleted file mode 100644 index 5e039677..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_1a3019722a97e8cea99fa0e052a34a68.html +++ /dev/null @@ -1,265 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Rate.Constant_Dynamic_Pressure_Constant_Rate Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Rate.Constant_Dynamic_Pressure_Constant_Rate Class Reference
-
-
-
-Inheritance diagram for SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Rate.Constant_Dynamic_Pressure_Constant_Rate:
-
-
- - -SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle -SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic -SUAVE.Analyses.Mission.Segments.Simple.Simple -SUAVE.Analyses.Mission.Segments.Segment.Segment -SUAVE.Analyses.Analysis.Analysis - -
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def evaluate (self, state=None)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

altitude_start
 
altitude_end
 
climb_rate
 
dynamic_pressure
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle
altitude_start
 
altitude_end
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
temperature_deviation
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
settings
 
state
 
analyses
 
process
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
Climb at a constant dynamic pressure at a constant rate.
-
-    Assumptions:
-    None
-    
-    Source:
-    None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Rate.Constant_Dynamic_Pressure_Constant_Rate.__defaults__ ( self)
-
-
This sets the default solver flow. Anything in here can be modified after initializing a segment.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Mission/Segments/Climb/Constant_Dynamic_Pressure_Constant_Rate.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_1a3019722a97e8cea99fa0e052a34a68.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_1a3019722a97e8cea99fa0e052a34a68.js deleted file mode 100644 index 95a71d76..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_1a3019722a97e8cea99fa0e052a34a68.js +++ /dev/null @@ -1,8 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_1a3019722a97e8cea99fa0e052a34a68 = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_1a3019722a97e8cea99fa0e052a34a68.html#af40eb9718e86910d5da3ef7b8a6ff554", null ], - [ "altitude_end", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_1a3019722a97e8cea99fa0e052a34a68.html#abb17767b2b4bbe63066f3f992c3ff5ea", null ], - [ "altitude_start", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_1a3019722a97e8cea99fa0e052a34a68.html#a097ba6b578f8563acadd802d75edbb4f", null ], - [ "climb_rate", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_1a3019722a97e8cea99fa0e052a34a68.html#a441914c37efbf0b4ee7680408eb159db", null ], - [ "dynamic_pressure", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_1a3019722a97e8cea99fa0e052a34a68.html#ad3f9933f7b8cda2f2b962ef2da11f19d", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_1a3019722a97e8cea99fa0e052a34a68.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_1a3019722a97e8cea99fa0e052a34a68.png deleted file mode 100644 index 41808645..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_1a3019722a97e8cea99fa0e052a34a68.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_61b566f355ab199459fb54d7274e572f.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_61b566f355ab199459fb54d7274e572f.html deleted file mode 100644 index a3bd8b13..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_61b566f355ab199459fb54d7274e572f.html +++ /dev/null @@ -1,266 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Angle.Constant_Dynamic_Pressure_Constant_Angle Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Angle.Constant_Dynamic_Pressure_Constant_Angle Class Reference
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-Inheritance diagram for SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Angle.Constant_Dynamic_Pressure_Constant_Angle:
-
-
- - -SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle -SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic -SUAVE.Analyses.Mission.Segments.Simple.Simple -SUAVE.Analyses.Mission.Segments.Segment.Segment -SUAVE.Analyses.Analysis.Analysis - -
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def evaluate (self, state=None)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

altitude_start
 
altitude_end
 
climb_angle
 
dynamic_pressure
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle
altitude_start
 
altitude_end
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
temperature_deviation
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
settings
 
state
 
analyses
 
process
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
Climb at a constant dynamic pressure at a constant angle.
-    This segment takes longer to solve than most because it has extra unknowns and residuals
-
-    Assumptions:
-    None
-    
-    Source:
-    None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Angle.Constant_Dynamic_Pressure_Constant_Angle.__defaults__ ( self)
-
-
This sets the default solver flow. Anything in here can be modified after initializing a segment.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Mission/Segments/Climb/Constant_Dynamic_Pressure_Constant_Angle.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_61b566f355ab199459fb54d7274e572f.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_61b566f355ab199459fb54d7274e572f.js deleted file mode 100644 index e2730409..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_61b566f355ab199459fb54d7274e572f.js +++ /dev/null @@ -1,8 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_61b566f355ab199459fb54d7274e572f = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_61b566f355ab199459fb54d7274e572f.html#adc5246f0192b0ccfd3a019ec63035c83", null ], - [ "altitude_end", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_61b566f355ab199459fb54d7274e572f.html#acbde920a943796262c2a8a33d4c2ca7c", null ], - [ "altitude_start", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_61b566f355ab199459fb54d7274e572f.html#af9dae09118f0cb83578c8ea0628f4ac3", null ], - [ "climb_angle", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_61b566f355ab199459fb54d7274e572f.html#a850b859796a2e86d3b00db3fa0af7155", null ], - [ "dynamic_pressure", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_61b566f355ab199459fb54d7274e572f.html#ad57b2f5e25c189c0d5ef42c19bb55ede", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_61b566f355ab199459fb54d7274e572f.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_61b566f355ab199459fb54d7274e572f.png deleted file mode 100644 index b3941712..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_61b566f355ab199459fb54d7274e572f.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_d4885eddc1dc9286bf80c906e9327ed4.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_d4885eddc1dc9286bf80c906e9327ed4.html deleted file mode 100644 index c8abf4ef..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_d4885eddc1dc9286bf80c906e9327ed4.html +++ /dev/null @@ -1,135 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Angle.Constant_Dynamic_Pressure_Constant_Angle Member List
-
-
- -

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Angle.Constant_Dynamic_Pressure_Constant_Angle, including all inherited members.

- - - - - - - - - - - - - - - - - - - - - - - - -
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Angle.Constant_Dynamic_Pressure_Constant_Angle
altitude_end (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Angle.Constant_Dynamic_Pressure_Constant_Angle)SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Angle.Constant_Dynamic_Pressure_Constant_Angle
altitude_start (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Angle.Constant_Dynamic_Pressure_Constant_Angle)SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Angle.Constant_Dynamic_Pressure_Constant_Angle
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
climb_angle (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Angle.Constant_Dynamic_Pressure_Constant_Angle)SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Angle.Constant_Dynamic_Pressure_Constant_Angle
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
dynamic_pressure (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Angle.Constant_Dynamic_Pressure_Constant_Angle)SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Angle.Constant_Dynamic_Pressure_Constant_Angle
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__EAS__Constant__Rate_1_1Const472497e5093c13e072d3d7a0c8f99d2a.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__EAS__Constant__Rate_1_1Const472497e5093c13e072d3d7a0c8f99d2a.html deleted file mode 100644 index 6c0671ff..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__EAS__Constant__Rate_1_1Const472497e5093c13e072d3d7a0c8f99d2a.html +++ /dev/null @@ -1,135 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
-
- - - -
-
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- -
- -
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- -
- -
-
-
SUAVE.Analyses.Mission.Segments.Climb.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate Member List
-
-
- -

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Climb.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate, including all inherited members.

- - - - - - - - - - - - - - - - - - - - - - - - -
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Climb.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate
altitude_end (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate)SUAVE.Analyses.Mission.Segments.Climb.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate
altitude_start (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate)SUAVE.Analyses.Mission.Segments.Climb.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
climb_rate (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate)SUAVE.Analyses.Mission.Segments.Climb.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
equivalent_air_speed (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate)SUAVE.Analyses.Mission.Segments.Climb.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__EAS__Constant__Rate_1_1Constant__EAS__Constant__Rate.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__EAS__Constant__Rate_1_1Constant__EAS__Constant__Rate.html deleted file mode 100644 index 99d919fa..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__EAS__Constant__Rate_1_1Constant__EAS__Constant__Rate.html +++ /dev/null @@ -1,265 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Mission.Segments.Climb.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate Class Reference - - - - - - - - - - - - - - - -
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- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Climb.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate Class Reference
-
-
-
-Inheritance diagram for SUAVE.Analyses.Mission.Segments.Climb.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate:
-
-
- - -SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle -SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic -SUAVE.Analyses.Mission.Segments.Simple.Simple -SUAVE.Analyses.Mission.Segments.Segment.Segment -SUAVE.Analyses.Analysis.Analysis - -
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def evaluate (self, state=None)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

altitude_start
 
altitude_end
 
climb_rate
 
equivalent_air_speed
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle
altitude_start
 
altitude_end
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
temperature_deviation
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
settings
 
state
 
analyses
 
process
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
Climb at a constant Equivalent Airspeed (EAS) at a constant rate.
-
-    Assumptions:
-    None
-    
-    Source:
-    None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Mission.Segments.Climb.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate.__defaults__ ( self)
-
-
This sets the default solver flow. Anything in here can be modified after initializing a segment.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Mission/Segments/Climb/Constant_EAS_Constant_Rate.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__EAS__Constant__Rate_1_1Constant__EAS__Constant__Rate.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__EAS__Constant__Rate_1_1Constant__EAS__Constant__Rate.js deleted file mode 100644 index 21173593..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__EAS__Constant__Rate_1_1Constant__EAS__Constant__Rate.js +++ /dev/null @@ -1,8 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__EAS__Constant__Rate_1_1Constant__EAS__Constant__Rate = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__EAS__Constant__Rate_1_1Constant__EAS__Constant__Rate.html#a11e12db892cf993fce2531bbc69cf5c1", null ], - [ "altitude_end", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__EAS__Constant__Rate_1_1Constant__EAS__Constant__Rate.html#a1652a172541f5bba885b3abb05b40976", null ], - [ "altitude_start", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__EAS__Constant__Rate_1_1Constant__EAS__Constant__Rate.html#acc48821a55eb9c46ab29603feb7aa529", null ], - [ "climb_rate", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__EAS__Constant__Rate_1_1Constant__EAS__Constant__Rate.html#a71acc84d4b08d62fcb031e85c5d2b294", null ], - [ "equivalent_air_speed", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__EAS__Constant__Rate_1_1Constant__EAS__Constant__Rate.html#afc67dc595e4933d3bec86d31a221e47c", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__EAS__Constant__Rate_1_1Constant__EAS__Constant__Rate.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__EAS__Constant__Rate_1_1Constant__EAS__Constant__Rate.png deleted file mode 100644 index 8d71e86b..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__EAS__Constant__Rate_1_1Constant__EAS__Constant__Rate.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Angle_1_1Cond98340f1a23497f281dfc038523d4030.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Angle_1_1Cond98340f1a23497f281dfc038523d4030.html deleted file mode 100644 index 4804026e..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Angle_1_1Cond98340f1a23497f281dfc038523d4030.html +++ /dev/null @@ -1,135 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
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-
-
- - - -
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SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Angle.Constant_Mach_Constant_Angle Member List
-
-
- -

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Angle.Constant_Mach_Constant_Angle, including all inherited members.

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__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Angle.Constant_Mach_Constant_Angle
altitude_end (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Angle.Constant_Mach_Constant_Angle)SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Angle.Constant_Mach_Constant_Angle
altitude_start (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Angle.Constant_Mach_Constant_Angle)SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Angle.Constant_Mach_Constant_Angle
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
climb_angle (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Angle.Constant_Mach_Constant_Angle)SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Angle.Constant_Mach_Constant_Angle
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
mach (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Angle.Constant_Mach_Constant_Angle)SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Angle.Constant_Mach_Constant_Angle
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Angle_1_1Constant__Mach__Constant__Angle.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Angle_1_1Constant__Mach__Constant__Angle.html deleted file mode 100644 index 54d7bfd0..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Angle_1_1Constant__Mach__Constant__Angle.html +++ /dev/null @@ -1,266 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Angle.Constant_Mach_Constant_Angle Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Angle.Constant_Mach_Constant_Angle Class Reference
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-
-
-Inheritance diagram for SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Angle.Constant_Mach_Constant_Angle:
-
-
- - -SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle -SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic -SUAVE.Analyses.Mission.Segments.Simple.Simple -SUAVE.Analyses.Mission.Segments.Segment.Segment -SUAVE.Analyses.Analysis.Analysis - -
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def evaluate (self, state=None)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

altitude_start
 
altitude_end
 
climb_angle
 
mach
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle
altitude_start
 
altitude_end
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
temperature_deviation
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
settings
 
state
 
analyses
 
process
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
Climb at a constant mach number and at a constant angle.
-    This segment takes longer to solve than most because it has extra unknowns and residuals
-
-    Assumptions:
-    None
-    
-    Source:
-    None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Angle.Constant_Mach_Constant_Angle.__defaults__ ( self)
-
-
This sets the default solver flow. Anything in here can be modified after initializing a segment.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Mission/Segments/Climb/Constant_Mach_Constant_Angle.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Angle_1_1Constant__Mach__Constant__Angle.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Angle_1_1Constant__Mach__Constant__Angle.js deleted file mode 100644 index eebd2e2f..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Angle_1_1Constant__Mach__Constant__Angle.js +++ /dev/null @@ -1,8 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Angle_1_1Constant__Mach__Constant__Angle = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Angle_1_1Constant__Mach__Constant__Angle.html#a2dc96e7542db94c76affc894435641c7", null ], - [ "altitude_end", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Angle_1_1Constant__Mach__Constant__Angle.html#a2db347c82878d9ba79771ddd4643eb78", null ], - [ "altitude_start", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Angle_1_1Constant__Mach__Constant__Angle.html#a37f860123e25f89ff15c79df7eb58de9", null ], - [ "climb_angle", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Angle_1_1Constant__Mach__Constant__Angle.html#ade53ee4189ecd0ab2a8f77b974ec5f15", null ], - [ "mach", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Angle_1_1Constant__Mach__Constant__Angle.html#a6765373b2bf85eb7955b411ea5daf00c", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Angle_1_1Constant__Mach__Constant__Angle.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Angle_1_1Constant__Mach__Constant__Angle.png deleted file mode 100644 index 50ddfdf6..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Angle_1_1Constant__Mach__Constant__Angle.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Rate_1_1Conseeda9394fcf076a53ee13c4c243a002b.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Rate_1_1Conseeda9394fcf076a53ee13c4c243a002b.html deleted file mode 100644 index e1c1bb3f..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Rate_1_1Conseeda9394fcf076a53ee13c4c243a002b.html +++ /dev/null @@ -1,135 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Rate.Constant_Mach_Constant_Rate Member List
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- -

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Rate.Constant_Mach_Constant_Rate, including all inherited members.

- - - - - - - - - - - - - - - - - - - - - - - - -
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Rate.Constant_Mach_Constant_Rate
altitude_end (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Rate.Constant_Mach_Constant_Rate)SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Rate.Constant_Mach_Constant_Rate
altitude_start (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Rate.Constant_Mach_Constant_Rate)SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Rate.Constant_Mach_Constant_Rate
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
climb_rate (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Rate.Constant_Mach_Constant_Rate)SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Rate.Constant_Mach_Constant_Rate
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
mach_number (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Rate.Constant_Mach_Constant_Rate)SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Rate.Constant_Mach_Constant_Rate
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Rate_1_1Constant__Mach__Constant__Rate.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Rate_1_1Constant__Mach__Constant__Rate.html deleted file mode 100644 index 20ea7ae4..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Rate_1_1Constant__Mach__Constant__Rate.html +++ /dev/null @@ -1,265 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Rate.Constant_Mach_Constant_Rate Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Rate.Constant_Mach_Constant_Rate Class Reference
-
-
-
-Inheritance diagram for SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Rate.Constant_Mach_Constant_Rate:
-
-
- - -SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle -SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic -SUAVE.Analyses.Mission.Segments.Simple.Simple -SUAVE.Analyses.Mission.Segments.Segment.Segment -SUAVE.Analyses.Analysis.Analysis - -
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def evaluate (self, state=None)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

altitude_start
 
altitude_end
 
climb_rate
 
mach_number
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle
altitude_start
 
altitude_end
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
temperature_deviation
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
settings
 
state
 
analyses
 
process
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
Climb at a constant mach number and at a constant rate.
-
-    Assumptions:
-    None
-    
-    Source:
-    None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Rate.Constant_Mach_Constant_Rate.__defaults__ ( self)
-
-
This sets the default solver flow. Anything in here can be modified after initializing a segment.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Mission/Segments/Climb/Constant_Mach_Constant_Rate.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Rate_1_1Constant__Mach__Constant__Rate.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Rate_1_1Constant__Mach__Constant__Rate.js deleted file mode 100644 index b437dbc0..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Rate_1_1Constant__Mach__Constant__Rate.js +++ /dev/null @@ -1,8 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Rate_1_1Constant__Mach__Constant__Rate = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Rate_1_1Constant__Mach__Constant__Rate.html#acdb488e321ee4950f691fa5cd240e427", null ], - [ "altitude_end", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Rate_1_1Constant__Mach__Constant__Rate.html#a3236f8ba3d3fa8ce6fba1794f1a640c5", null ], - [ "altitude_start", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Rate_1_1Constant__Mach__Constant__Rate.html#ae0abdda540025af275b11c4642e61a26", null ], - [ "climb_rate", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Rate_1_1Constant__Mach__Constant__Rate.html#a919a255bb7c36308039fa83652ee4b52", null ], - [ "mach_number", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Rate_1_1Constant__Mach__Constant__Rate.html#a34c5ca143790bf7f3d2de5c64549fe13", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Rate_1_1Constant__Mach__Constant__Rate.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Rate_1_1Constant__Mach__Constant__Rate.png deleted file mode 100644 index b54056ff..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Rate_1_1Constant__Mach__Constant__Rate.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Linear__Altitude_1_1Co8c4ee3be4a98ae94054df578da4a2738.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Linear__Altitude_1_1Co8c4ee3be4a98ae94054df578da4a2738.html deleted file mode 100644 index a654b303..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Linear__Altitude_1_1Co8c4ee3be4a98ae94054df578da4a2738.html +++ /dev/null @@ -1,118 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Linear_Altitude.Constant_Mach_Linear_Altitude Member List
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Linear__Altitude_1_1Constant__Mach__Linear__Altitude.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Linear__Altitude_1_1Constant__Mach__Linear__Altitude.html deleted file mode 100644 index 7da82613..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Linear__Altitude_1_1Constant__Mach__Linear__Altitude.html +++ /dev/null @@ -1,192 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Linear_Altitude.Constant_Mach_Linear_Altitude Class Reference - - - - - - - - - - - - - - - -
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SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Linear_Altitude.Constant_Mach_Linear_Altitude Class Reference
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-Inheritance diagram for SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Linear_Altitude.Constant_Mach_Linear_Altitude:
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-Public Member Functions

def __defaults__ (self)
 
- - - - - - - - - - - -

-Public Attributes

altitude
 
mach
 
distance
 
altitude_start
 
altitude_end
 
-

Detailed Description

-
Climb at a constant mach number but linearly change altitudes over a distance.
-
-    Assumptions:
-    None
-    
-    Source:
-    None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Linear_Altitude.Constant_Mach_Linear_Altitude.__defaults__ ( self)
-
-
This sets the default solver flow. Anything in here can be modified after initializing a segment.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Mission/Segments/Climb/Constant_Mach_Linear_Altitude.py
  • -
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Linear__Altitude_1_1Constant__Mach__Linear__Altitude.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Linear__Altitude_1_1Constant__Mach__Linear__Altitude.js deleted file mode 100644 index 285a614d..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Linear__Altitude_1_1Constant__Mach__Linear__Altitude.js +++ /dev/null @@ -1,9 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Linear__Altitude_1_1Constant__Mach__Linear__Altitude = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Linear__Altitude_1_1Constant__Mach__Linear__Altitude.html#ac1fd9a08e71825dccdb21cb4e880f210", null ], - [ "altitude", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Linear__Altitude_1_1Constant__Mach__Linear__Altitude.html#a8d86b717a16fa1c8e9d8ab226204e859", null ], - [ "altitude_end", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Linear__Altitude_1_1Constant__Mach__Linear__Altitude.html#af4b0b41792a4349fe840f4d576afe7f1", null ], - [ "altitude_start", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Linear__Altitude_1_1Constant__Mach__Linear__Altitude.html#aed0f90918954a0e628428626496a00ee", null ], - [ "distance", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Linear__Altitude_1_1Constant__Mach__Linear__Altitude.html#a598c889032ae65c0ba75235d5267e3e4", null ], - [ "mach", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Linear__Altitude_1_1Constant__Mach__Linear__Altitude.html#aeb0f2f830a113f193a40fba4b6de704f", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Linear__Altitude_1_1Constant__Mach__Linear__Altitude.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Linear__Altitude_1_1Constant__Mach__Linear__Altitude.png deleted file mode 100644 index 3998e75e..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Linear__Altitude_1_1Constant__Mach__Linear__Altitude.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle_1_1Coe49fde66af63b5086460e1537e678aaa.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle_1_1Coe49fde66af63b5086460e1537e678aaa.html deleted file mode 100644 index 02e51358..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle_1_1Coe49fde66af63b5086460e1537e678aaa.html +++ /dev/null @@ -1,135 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle Member List
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-
- -

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle, including all inherited members.

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__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle
air_speed (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle)SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle
altitude_end (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle)SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle
altitude_start (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle)SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
climb_angle (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle)SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle_1_1Constant__Speed__Constant__Angle.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle_1_1Constant__Speed__Constant__Angle.html deleted file mode 100644 index 925280bb..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle_1_1Constant__Speed__Constant__Angle.html +++ /dev/null @@ -1,266 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle Class Reference
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-
-Inheritance diagram for SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle:
-
-
- - -SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle -SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic -SUAVE.Analyses.Mission.Segments.Simple.Simple -SUAVE.Analyses.Mission.Segments.Segment.Segment -SUAVE.Analyses.Analysis.Analysis - -
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def evaluate (self, state=None)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

altitude_start
 
altitude_end
 
climb_angle
 
air_speed
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle
altitude_start
 
altitude_end
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
temperature_deviation
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
settings
 
state
 
analyses
 
process
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
A basic constant true airspeed climb at a constant angle. Usually used for certification to ensure a vehicle
-    can clear and obstacle.
-
-    Assumptions:
-    None
-    
-    Source:
-    None
-

Member Function Documentation

- -

◆ __defaults__()

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def SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle.__defaults__ ( self)
-
-
This sets the default solver flow. Anything in here can be modified after initializing a segment.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Mission/Segments/Climb/Constant_Speed_Constant_Angle.py
  • -
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle_1_1Constant__Speed__Constant__Angle.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle_1_1Constant__Speed__Constant__Angle.js deleted file mode 100644 index cd11c1a4..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle_1_1Constant__Speed__Constant__Angle.js +++ /dev/null @@ -1,8 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle_1_1Constant__Speed__Constant__Angle = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle_1_1Constant__Speed__Constant__Angle.html#a22bde8f263ed34c28f30d66017f1c982", null ], - [ "air_speed", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle_1_1Constant__Speed__Constant__Angle.html#a074bc5776c3c78d43d5abb0a074a0156", null ], - [ "altitude_end", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle_1_1Constant__Speed__Constant__Angle.html#a5900968ee69b00b5f8e6b98f2da57e41", null ], - [ "altitude_start", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle_1_1Constant__Speed__Constant__Angle.html#acd39a3fecffc510bd6a15027cf48bedf", null ], - [ "climb_angle", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle_1_1Constant__Speed__Constant__Angle.html#a3562b40f80a73b2a9a99f92ccb1168b4", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle_1_1Constant__Speed__Constant__Angle.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle_1_1Constant__Speed__Constant__Angle.png deleted file mode 100644 index 4059e3a5..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle_1_1Constant__Speed__Constant__Angle.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle__Noisb1704f4c5e6114d87007dadfc99b2d01.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle__Noisb1704f4c5e6114d87007dadfc99b2d01.html deleted file mode 100644 index 62d6d2b1..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle__Noisb1704f4c5e6114d87007dadfc99b2d01.html +++ /dev/null @@ -1,135 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise Member List
-
-
- -

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise, including all inherited members.

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__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise
air_speed (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise)SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise
altitude_end (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise)SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise
altitude_start (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise)SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
climb_angle (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise)SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle__Noise1165f03ba148155cea33a06b04b964a.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle__Noise1165f03ba148155cea33a06b04b964a.html deleted file mode 100644 index 3905c738..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle__Noise1165f03ba148155cea33a06b04b964a.html +++ /dev/null @@ -1,268 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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- -
- -
-
SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise Class Reference
-
-
-
-Inheritance diagram for SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise:
-
-
- - -SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle -SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic -SUAVE.Analyses.Mission.Segments.Simple.Simple -SUAVE.Analyses.Mission.Segments.Segment.Segment -SUAVE.Analyses.Analysis.Analysis - -
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def evaluate (self, state=None)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

altitude_start
 
altitude_end
 
climb_angle
 
air_speed
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle
altitude_start
 
altitude_end
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
temperature_deviation
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
settings
 
state
 
analyses
 
process
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
Fixed at a true airspeed the vehicle will climb at a constant angle. This is a specific segment for Noise.
-    A vehicle performs a climb in accordance with a certification points for takeoff noise.
-    Don't use this segment unless you're planning on post process for noise. It is slower than the normal constant
-    speed constand angle segment.
-
-    Assumptions:
-    The points are linearly spaced rather than chebyshev spaced to give the proper "microphone" locations.
-    
-    Source:
-    None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise.__defaults__ ( self)
-
-
This sets the default solver flow. Anything in here can be modified after initializing a segment.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Mission/Segments/Climb/Constant_Speed_Constant_Angle_Noise.py
  • -
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle__Noise1165f03ba148155cea33a06b04b964a.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle__Noise1165f03ba148155cea33a06b04b964a.js deleted file mode 100644 index 12b655af..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle__Noise1165f03ba148155cea33a06b04b964a.js +++ /dev/null @@ -1,8 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle__Noise1165f03ba148155cea33a06b04b964a = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle__Noise1165f03ba148155cea33a06b04b964a.html#ae39906afac213a27963c0980a8cca90d", null ], - [ "air_speed", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle__Noise1165f03ba148155cea33a06b04b964a.html#a161831d0de82de6d65ec640cbd216709", null ], - [ "altitude_end", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle__Noise1165f03ba148155cea33a06b04b964a.html#ae5b755e424fa9fd62430622c061525f9", null ], - [ "altitude_start", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle__Noise1165f03ba148155cea33a06b04b964a.html#a0184a53853849f128c2c0da67d38a9b0", null ], - [ "climb_angle", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle__Noise1165f03ba148155cea33a06b04b964a.html#a115cf7a64f4135636271660181b097cf", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle__Noise1165f03ba148155cea33a06b04b964a.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle__Noise1165f03ba148155cea33a06b04b964a.png deleted file mode 100644 index 7c48a8dd..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle__Noise1165f03ba148155cea33a06b04b964a.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Rate_1_1Con98f50eb7047227d427afc04f6619e235.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Rate_1_1Con98f50eb7047227d427afc04f6619e235.html deleted file mode 100644 index 1735027d..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Rate_1_1Con98f50eb7047227d427afc04f6619e235.html +++ /dev/null @@ -1,135 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate Member List
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This is the complete list of members for SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate, including all inherited members.

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__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate
air_speed (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate)SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate
altitude_end (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate)SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate
altitude_start (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate)SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
climb_rate (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate)SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Rate_1_1Constant__Speed__Constant__Rate.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Rate_1_1Constant__Speed__Constant__Rate.html deleted file mode 100644 index 375f80ba..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Rate_1_1Constant__Speed__Constant__Rate.html +++ /dev/null @@ -1,265 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate Class Reference
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-Inheritance diagram for SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate:
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- - -SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle -SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic -SUAVE.Analyses.Mission.Segments.Simple.Simple -SUAVE.Analyses.Mission.Segments.Segment.Segment -SUAVE.Analyses.Analysis.Analysis - -
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-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def evaluate (self, state=None)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
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-Public Attributes

altitude_start
 
altitude_end
 
climb_rate
 
air_speed
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle
altitude_start
 
altitude_end
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
temperature_deviation
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
settings
 
state
 
analyses
 
process
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

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The most basic segment. Fly at a constant true airspeed at a fixed rate of climb between 2 altitudes.
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-    Assumptions:
-    None
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-    Source:
-    None
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Member Function Documentation

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◆ __defaults__()

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def SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate.__defaults__ ( self)
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This sets the default solver flow. Anything in here can be modified after initializing a segment.
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-    None
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-    Source:
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-    Inputs:
-    None
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-    Outputs:
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-    Properties Used:
-    None
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The documentation for this class was generated from the following file:
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Rate_1_1Constant__Speed__Constant__Rate.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Rate_1_1Constant__Speed__Constant__Rate.js deleted file mode 100644 index 82101723..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Rate_1_1Constant__Speed__Constant__Rate.js +++ /dev/null @@ -1,8 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Rate_1_1Constant__Speed__Constant__Rate = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Rate_1_1Constant__Speed__Constant__Rate.html#a9dd1fa4f184c74b7213c4d360920991f", null ], - [ "air_speed", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Rate_1_1Constant__Speed__Constant__Rate.html#a2218ec53554f8babfc14a0589d370408", null ], - [ "altitude_end", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Rate_1_1Constant__Speed__Constant__Rate.html#a97099b1d5412945f7ff501505ba97b12", null ], - [ "altitude_start", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Rate_1_1Constant__Speed__Constant__Rate.html#a814302292a45ce0a0473d8bfcd44b7cc", null ], - [ "climb_rate", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Rate_1_1Constant__Speed__Constant__Rate.html#a5e77679758ffc9ab01462176a1bce1b0", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Rate_1_1Constant__Speed__Constant__Rate.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Rate_1_1Constant__Speed__Constant__Rate.png deleted file mode 100644 index 11c07293..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Rate_1_1Constant__Speed__Constant__Rate.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Linear__Altitude_1_1Ca70c2a81d5de0f61273c53f05124d5dd.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Linear__Altitude_1_1Ca70c2a81d5de0f61273c53f05124d5dd.html deleted file mode 100644 index 385dbbfd..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Linear__Altitude_1_1Ca70c2a81d5de0f61273c53f05124d5dd.html +++ /dev/null @@ -1,136 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Linear_Altitude.Constant_Speed_Linear_Altitude Member List
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This is the complete list of members for SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Linear_Altitude.Constant_Speed_Linear_Altitude, including all inherited members.

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__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Linear_Altitude.Constant_Speed_Linear_Altitude
air_speed (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Linear_Altitude.Constant_Speed_Linear_Altitude)SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Linear_Altitude.Constant_Speed_Linear_Altitude
altitude (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Linear_Altitude.Constant_Speed_Linear_Altitude)SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Linear_Altitude.Constant_Speed_Linear_Altitude
altitude_end (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Linear_Altitude.Constant_Speed_Linear_Altitude)SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Linear_Altitude.Constant_Speed_Linear_Altitude
altitude_start (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Linear_Altitude.Constant_Speed_Linear_Altitude)SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Linear_Altitude.Constant_Speed_Linear_Altitude
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
distance (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Linear_Altitude.Constant_Speed_Linear_Altitude)SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Linear_Altitude.Constant_Speed_Linear_Altitude
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Linear__Altitude_1_1Cd58dc6a2d95bb161e2208f5800fce872.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Linear__Altitude_1_1Cd58dc6a2d95bb161e2208f5800fce872.html deleted file mode 100644 index 42cb93fa..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Linear__Altitude_1_1Cd58dc6a2d95bb161e2208f5800fce872.html +++ /dev/null @@ -1,257 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Linear_Altitude.Constant_Speed_Linear_Altitude Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Linear_Altitude.Constant_Speed_Linear_Altitude Class Reference
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-
-
-Inheritance diagram for SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Linear_Altitude.Constant_Speed_Linear_Altitude:
-
-
- - -SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic -SUAVE.Analyses.Mission.Segments.Simple.Simple -SUAVE.Analyses.Mission.Segments.Segment.Segment -SUAVE.Analyses.Analysis.Analysis - -
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def evaluate (self, state=None)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

altitude
 
air_speed
 
distance
 
altitude_start
 
altitude_end
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
temperature_deviation
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
settings
 
state
 
analyses
 
process
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
Climb at a constant true airspeed but linearly change altitudes over a distance.
-
-    Assumptions:
-    None
-    
-    Source:
-    None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Linear_Altitude.Constant_Speed_Linear_Altitude.__defaults__ ( self)
-
-
This sets the default solver flow. Anything in here can be modified after initializing a segment.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Mission/Segments/Climb/Constant_Speed_Linear_Altitude.py
  • -
-
-
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Climb.Constant_Throttle_Constant_Speed.Constant_Throttle_Constant_Speed Class Reference
-
-
-
-Inheritance diagram for SUAVE.Analyses.Mission.Segments.Climb.Constant_Throttle_Constant_Speed.Constant_Throttle_Constant_Speed:
-
-
- - -SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic -SUAVE.Analyses.Mission.Segments.Simple.Simple -SUAVE.Analyses.Mission.Segments.Segment.Segment -SUAVE.Analyses.Analysis.Analysis - -
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def evaluate (self, state=None)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

altitude_start
 
altitude_end
 
throttle
 
air_speed
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
temperature_deviation
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
settings
 
state
 
analyses
 
process
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
Climb at a constant throttle setting and true airspeed.
-    This segment may not always converge as the vehicle could be deficient in thrust.
-    Useful as a check to see the climb rate at the top of climb.
-
-    Assumptions:
-    You set a reasonable throttle setting that can provide enough thrust.
-    
-    Source:
-    None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Mission.Segments.Climb.Constant_Throttle_Constant_Speed.Constant_Throttle_Constant_Speed.__defaults__ ( self)
-
-
This sets the default solver flow. Anything in here can be modified after initializing a segment.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Mission/Segments/Climb/Constant_Throttle_Constant_Speed.py
  • -
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Throttle__Constant__Speed_1_02b90ea2f234e748373e0a5403527689.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Throttle__Constant__Speed_1_02b90ea2f234e748373e0a5403527689.js deleted file mode 100644 index 19854a95..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Throttle__Constant__Speed_1_02b90ea2f234e748373e0a5403527689.js +++ /dev/null @@ -1,8 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Throttle__Constant__Speed_1_02b90ea2f234e748373e0a5403527689 = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Throttle__Constant__Speed_1_02b90ea2f234e748373e0a5403527689.html#aab4fc2d66d7629f28d6ddc609304203b", null ], - [ "air_speed", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Throttle__Constant__Speed_1_02b90ea2f234e748373e0a5403527689.html#af44c9d2cbda7ae3ad64fb5ae259dbcbe", null ], - [ "altitude_end", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Throttle__Constant__Speed_1_02b90ea2f234e748373e0a5403527689.html#a0b0300d65d3255bb5b13b05b40054b07", null ], - [ "altitude_start", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Throttle__Constant__Speed_1_02b90ea2f234e748373e0a5403527689.html#aac4ecf672f3b9c52d65b994f5bd4884d", null ], - [ "throttle", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Throttle__Constant__Speed_1_02b90ea2f234e748373e0a5403527689.html#a73996582edfad573155a4c142bc2d53e", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Throttle__Constant__Speed_1_02b90ea2f234e748373e0a5403527689.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Throttle__Constant__Speed_1_02b90ea2f234e748373e0a5403527689.png deleted file mode 100644 index 0d1ed3f5..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Throttle__Constant__Speed_1_02b90ea2f234e748373e0a5403527689.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Throttle__Constant__Speed_1_5630685c5adb656512896887ec47e0bf.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Throttle__Constant__Speed_1_5630685c5adb656512896887ec47e0bf.html deleted file mode 100644 index 1746e2d1..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Throttle__Constant__Speed_1_5630685c5adb656512896887ec47e0bf.html +++ /dev/null @@ -1,135 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Climb.Constant_Throttle_Constant_Speed.Constant_Throttle_Constant_Speed Member List
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This is the complete list of members for SUAVE.Analyses.Mission.Segments.Climb.Constant_Throttle_Constant_Speed.Constant_Throttle_Constant_Speed, including all inherited members.

- - - - - - - - - - - - - - - - - - - - - - - - -
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Climb.Constant_Throttle_Constant_Speed.Constant_Throttle_Constant_Speed
air_speed (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Throttle_Constant_Speed.Constant_Throttle_Constant_Speed)SUAVE.Analyses.Mission.Segments.Climb.Constant_Throttle_Constant_Speed.Constant_Throttle_Constant_Speed
altitude_end (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Throttle_Constant_Speed.Constant_Throttle_Constant_Speed)SUAVE.Analyses.Mission.Segments.Climb.Constant_Throttle_Constant_Speed.Constant_Throttle_Constant_Speed
altitude_start (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Throttle_Constant_Speed.Constant_Throttle_Constant_Speed)SUAVE.Analyses.Mission.Segments.Climb.Constant_Throttle_Constant_Speed.Constant_Throttle_Constant_Speed
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
throttle (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Throttle_Constant_Speed.Constant_Throttle_Constant_Speed)SUAVE.Analyses.Mission.Segments.Climb.Constant_Throttle_Constant_Speed.Constant_Throttle_Constant_Speed
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Mach__Constant__Rate_1_1Linear__Mach__Constant__Rate-members.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Mach__Constant__Rate_1_1Linear__Mach__Constant__Rate-members.html deleted file mode 100644 index 1cb75aa6..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Mach__Constant__Rate_1_1Linear__Mach__Constant__Rate-members.html +++ /dev/null @@ -1,136 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Climb.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate Member List
-
-
- -

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Climb.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate, including all inherited members.

- - - - - - - - - - - - - - - - - - - - - - - - - -
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Climb.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate
altitude_end (defined in SUAVE.Analyses.Mission.Segments.Climb.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate)SUAVE.Analyses.Mission.Segments.Climb.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate
altitude_start (defined in SUAVE.Analyses.Mission.Segments.Climb.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate)SUAVE.Analyses.Mission.Segments.Climb.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
climb_rate (defined in SUAVE.Analyses.Mission.Segments.Climb.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate)SUAVE.Analyses.Mission.Segments.Climb.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
mach_end (defined in SUAVE.Analyses.Mission.Segments.Climb.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate)SUAVE.Analyses.Mission.Segments.Climb.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate
mach_start (defined in SUAVE.Analyses.Mission.Segments.Climb.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate)SUAVE.Analyses.Mission.Segments.Climb.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Mach__Constant__Rate_1_1Linear__Mach__Constant__Rate.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Mach__Constant__Rate_1_1Linear__Mach__Constant__Rate.html deleted file mode 100644 index 3d799168..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Mach__Constant__Rate_1_1Linear__Mach__Constant__Rate.html +++ /dev/null @@ -1,268 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Mission.Segments.Climb.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Climb.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate Class Reference
-
-
-
-Inheritance diagram for SUAVE.Analyses.Mission.Segments.Climb.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate:
-
-
- - -SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle -SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic -SUAVE.Analyses.Mission.Segments.Simple.Simple -SUAVE.Analyses.Mission.Segments.Segment.Segment -SUAVE.Analyses.Analysis.Analysis - -
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def evaluate (self, state=None)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

altitude_start
 
altitude_end
 
climb_rate
 
mach_end
 
mach_start
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle
altitude_start
 
altitude_end
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
temperature_deviation
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
settings
 
state
 
analyses
 
process
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
Linearly change mach number while climbing at a constant rate.
-
-    Assumptions:
-    None
-    
-    Source:
-    None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Mission.Segments.Climb.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate.__defaults__ ( self)
-
-
This sets the default solver flow. Anything in here can be modified after initializing a segment.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Mission/Segments/Climb/Linear_Mach_Constant_Rate.py
  • -
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Mach__Constant__Rate_1_1Linear__Mach__Constant__Rate.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Mach__Constant__Rate_1_1Linear__Mach__Constant__Rate.js deleted file mode 100644 index 0a2632a8..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Mach__Constant__Rate_1_1Linear__Mach__Constant__Rate.js +++ /dev/null @@ -1,9 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Mach__Constant__Rate_1_1Linear__Mach__Constant__Rate = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Mach__Constant__Rate_1_1Linear__Mach__Constant__Rate.html#a84db112844e99905a2e02b735f256353", null ], - [ "altitude_end", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Mach__Constant__Rate_1_1Linear__Mach__Constant__Rate.html#a7104ab23d04b5b54cc8c6c15f4e725eb", null ], - [ "altitude_start", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Mach__Constant__Rate_1_1Linear__Mach__Constant__Rate.html#a9a66ce5c5769a5a7b3a2d6f368b3e7b3", null ], - [ "climb_rate", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Mach__Constant__Rate_1_1Linear__Mach__Constant__Rate.html#a40a318890ae82ec9d0e010a1f6303723", null ], - [ "mach_end", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Mach__Constant__Rate_1_1Linear__Mach__Constant__Rate.html#a07701c31258186edd0c40d33d2a83d10", null ], - [ "mach_start", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Mach__Constant__Rate_1_1Linear__Mach__Constant__Rate.html#ae33f23541e9729e7bed9e0331b036be6", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Mach__Constant__Rate_1_1Linear__Mach__Constant__Rate.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Mach__Constant__Rate_1_1Linear__Mach__Constant__Rate.png deleted file mode 100644 index 74291f4e..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Mach__Constant__Rate_1_1Linear__Mach__Constant__Rate.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Speed__Constant__Rate_1_1Linea129dd2dcbc0fcf0bb1dbc899f23a2fdd.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Speed__Constant__Rate_1_1Linea129dd2dcbc0fcf0bb1dbc899f23a2fdd.html deleted file mode 100644 index 16903733..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Speed__Constant__Rate_1_1Linea129dd2dcbc0fcf0bb1dbc899f23a2fdd.html +++ /dev/null @@ -1,136 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Climb.Linear_Speed_Constant_Rate.Linear_Speed_Constant_Rate Member List
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This is the complete list of members for SUAVE.Analyses.Mission.Segments.Climb.Linear_Speed_Constant_Rate.Linear_Speed_Constant_Rate, including all inherited members.

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__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Climb.Linear_Speed_Constant_Rate.Linear_Speed_Constant_Rate
air_speed_end (defined in SUAVE.Analyses.Mission.Segments.Climb.Linear_Speed_Constant_Rate.Linear_Speed_Constant_Rate)SUAVE.Analyses.Mission.Segments.Climb.Linear_Speed_Constant_Rate.Linear_Speed_Constant_Rate
air_speed_start (defined in SUAVE.Analyses.Mission.Segments.Climb.Linear_Speed_Constant_Rate.Linear_Speed_Constant_Rate)SUAVE.Analyses.Mission.Segments.Climb.Linear_Speed_Constant_Rate.Linear_Speed_Constant_Rate
altitude_end (defined in SUAVE.Analyses.Mission.Segments.Climb.Linear_Speed_Constant_Rate.Linear_Speed_Constant_Rate)SUAVE.Analyses.Mission.Segments.Climb.Linear_Speed_Constant_Rate.Linear_Speed_Constant_Rate
altitude_start (defined in SUAVE.Analyses.Mission.Segments.Climb.Linear_Speed_Constant_Rate.Linear_Speed_Constant_Rate)SUAVE.Analyses.Mission.Segments.Climb.Linear_Speed_Constant_Rate.Linear_Speed_Constant_Rate
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
climb_rate (defined in SUAVE.Analyses.Mission.Segments.Climb.Linear_Speed_Constant_Rate.Linear_Speed_Constant_Rate)SUAVE.Analyses.Mission.Segments.Climb.Linear_Speed_Constant_Rate.Linear_Speed_Constant_Rate
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Speed__Constant__Rate_1_1Linear__Speed__Constant__Rate.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Speed__Constant__Rate_1_1Linear__Speed__Constant__Rate.html deleted file mode 100644 index a178a087..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Speed__Constant__Rate_1_1Linear__Speed__Constant__Rate.html +++ /dev/null @@ -1,268 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Mission.Segments.Climb.Linear_Speed_Constant_Rate.Linear_Speed_Constant_Rate Class Reference - - - - - - - - - - - - - - - -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Climb.Linear_Speed_Constant_Rate.Linear_Speed_Constant_Rate Class Reference
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-
-Inheritance diagram for SUAVE.Analyses.Mission.Segments.Climb.Linear_Speed_Constant_Rate.Linear_Speed_Constant_Rate:
-
-
- - -SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle -SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic -SUAVE.Analyses.Mission.Segments.Simple.Simple -SUAVE.Analyses.Mission.Segments.Segment.Segment -SUAVE.Analyses.Analysis.Analysis - -
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-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def evaluate (self, state=None)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

altitude_start
 
altitude_end
 
climb_rate
 
air_speed_start
 
air_speed_end
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle
altitude_start
 
altitude_end
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
temperature_deviation
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
settings
 
state
 
analyses
 
process
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
Linearly change true airspeed while climbing at a constant rate.
-
-    Assumptions:
-    None
-    
-    Source:
-    None
-

Member Function Documentation

- -

◆ __defaults__()

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def SUAVE.Analyses.Mission.Segments.Climb.Linear_Speed_Constant_Rate.Linear_Speed_Constant_Rate.__defaults__ ( self)
-
-
This sets the default solver flow. Anything in here can be modified after initializing a segment.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
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The documentation for this class was generated from the following file:
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  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Mission/Segments/Climb/Linear_Speed_Constant_Rate.py
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Speed__Constant__Rate_1_1Linear__Speed__Constant__Rate.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Speed__Constant__Rate_1_1Linear__Speed__Constant__Rate.js deleted file mode 100644 index 60760d11..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Speed__Constant__Rate_1_1Linear__Speed__Constant__Rate.js +++ /dev/null @@ -1,9 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Speed__Constant__Rate_1_1Linear__Speed__Constant__Rate = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Speed__Constant__Rate_1_1Linear__Speed__Constant__Rate.html#a5d41c0761bbf546d6c034baf639254d9", null ], - [ "air_speed_end", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Speed__Constant__Rate_1_1Linear__Speed__Constant__Rate.html#a2805e56aad8264b402e62dcaaa651814", null ], - [ "air_speed_start", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Speed__Constant__Rate_1_1Linear__Speed__Constant__Rate.html#ace9b207639faf169ec2b5d7232d2f851", null ], - [ "altitude_end", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Speed__Constant__Rate_1_1Linear__Speed__Constant__Rate.html#aa472350edc7ccf74fe26d9b6b282dfc0", null ], - [ "altitude_start", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Speed__Constant__Rate_1_1Linear__Speed__Constant__Rate.html#a18ed8f645570ccad3f87bf352ae76ad7", null ], - [ "climb_rate", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Speed__Constant__Rate_1_1Linear__Speed__Constant__Rate.html#a49fd27c4734fca69a5810b6406cb5b29", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Speed__Constant__Rate_1_1Linear__Speed__Constant__Rate.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Speed__Constant__Rate_1_1Linear__Speed__Constant__Rate.png deleted file mode 100644 index 2d0c24ab..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Speed__Constant__Rate_1_1Linear__Speed__Constant__Rate.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Optimized_1_1Optimized-members.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Optimized_1_1Optimized-members.html deleted file mode 100644 index cbe33cb1..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Optimized_1_1Optimized-members.html +++ /dev/null @@ -1,140 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Climb.Optimized.Optimized Member List
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This is the complete list of members for SUAVE.Analyses.Mission.Segments.Climb.Optimized.Optimized, including all inherited members.

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__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Climb.Optimized.Optimized
air_speed_end (defined in SUAVE.Analyses.Mission.Segments.Climb.Optimized.Optimized)SUAVE.Analyses.Mission.Segments.Climb.Optimized.Optimized
air_speed_start (defined in SUAVE.Analyses.Mission.Segments.Climb.Optimized.Optimized)SUAVE.Analyses.Mission.Segments.Climb.Optimized.Optimized
algorithm (defined in SUAVE.Analyses.Mission.Segments.Climb.Optimized.Optimized)SUAVE.Analyses.Mission.Segments.Climb.Optimized.Optimized
altitude_end (defined in SUAVE.Analyses.Mission.Segments.Climb.Optimized.Optimized)SUAVE.Analyses.Mission.Segments.Climb.Optimized.Optimized
altitude_start (defined in SUAVE.Analyses.Mission.Segments.Climb.Optimized.Optimized)SUAVE.Analyses.Mission.Segments.Climb.Optimized.Optimized
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
CL_limit (defined in SUAVE.Analyses.Mission.Segments.Climb.Optimized.Optimized)SUAVE.Analyses.Mission.Segments.Climb.Optimized.Optimized
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
minimize (defined in SUAVE.Analyses.Mission.Segments.Climb.Optimized.Optimized)SUAVE.Analyses.Mission.Segments.Climb.Optimized.Optimized
objective (defined in SUAVE.Analyses.Mission.Segments.Climb.Optimized.Optimized)SUAVE.Analyses.Mission.Segments.Climb.Optimized.Optimized
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
seed_climb_rate (defined in SUAVE.Analyses.Mission.Segments.Climb.Optimized.Optimized)SUAVE.Analyses.Mission.Segments.Climb.Optimized.Optimized
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Optimized_1_1Optimized.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Optimized_1_1Optimized.html deleted file mode 100644 index 060f237b..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Optimized_1_1Optimized.html +++ /dev/null @@ -1,278 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Mission.Segments.Climb.Optimized.Optimized Class Reference - - - - - - - - - - - - - - - -
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- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Climb.Optimized.Optimized Class Reference
-
-
-
-Inheritance diagram for SUAVE.Analyses.Mission.Segments.Climb.Optimized.Optimized:
-
-
- - -SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic -SUAVE.Analyses.Mission.Segments.Simple.Simple -SUAVE.Analyses.Mission.Segments.Segment.Segment -SUAVE.Analyses.Analysis.Analysis - -
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-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def evaluate (self, state=None)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

altitude_start
 
altitude_end
 
air_speed_start
 
air_speed_end
 
objective
 
minimize
 
CL_limit
 
seed_climb_rate
 
algorithm
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
temperature_deviation
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
settings
 
state
 
analyses
 
process
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
Optimize your climb segment. This is useful if you're not sure how your vehicle should climb.
-    You can set any conditions parameter as the objective, for example setting time to climb or vehicle mass:
-    segment.objective       = 'conditions.weights.total_mass[-1,0]'
-    
-    The ending airspeed is an optional parameter.
-    
-    This segment takes far longer to run than a normal segment. Wrapping this into a vehicle optimization
-    has not yet been tested for robustness.
-    
-
-    Assumptions:
-    Can use SNOPT if you have it installed through PyOpt. But defaults to SLSQP through 
-    Runs a linear true airspeed mission first to initialize conditions.
-    
-    Source:
-    None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Mission.Segments.Climb.Optimized.Optimized.__defaults__ ( self)
-
-
This sets the default solver flow. Anything in here can be modified after initializing a segment.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Mission/Segments/Climb/Optimized.py
  • -
-
-
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle Member List
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- -

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle, including all inherited members.

- - - - - - - - - - - - - - - - - - - - - - -
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle
altitude_end (defined in SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle)SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle
altitude_start (defined in SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle)SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Unknown__Throttle_1_1Unknown__Throttle.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Unknown__Throttle_1_1Unknown__Throttle.html deleted file mode 100644 index b502c727..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Unknown__Throttle_1_1Unknown__Throttle.html +++ /dev/null @@ -1,263 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle Class Reference
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-
-Inheritance diagram for SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle:
-
-
- - -SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic -SUAVE.Analyses.Mission.Segments.Simple.Simple -SUAVE.Analyses.Mission.Segments.Segment.Segment -SUAVE.Analyses.Analysis.Analysis -SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Angle.Constant_Dynamic_Pressure_Constant_Angle -SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Rate.Constant_Dynamic_Pressure_Constant_Rate -SUAVE.Analyses.Mission.Segments.Climb.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate -SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Angle.Constant_Mach_Constant_Angle -SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Rate.Constant_Mach_Constant_Rate -SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle -SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise -SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate -SUAVE.Analyses.Mission.Segments.Climb.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate -SUAVE.Analyses.Mission.Segments.Climb.Linear_Speed_Constant_Rate.Linear_Speed_Constant_Rate -SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle -SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise -SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate -SUAVE.Analyses.Mission.Segments.Descent.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate - -
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-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def evaluate (self, state=None)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

altitude_start
 
altitude_end
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
temperature_deviation
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
settings
 
state
 
analyses
 
process
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
This is a basic climb segment that is not callable by a user. All other variable throttle missions are based 
-    on this class as a building block.
-
-    Assumptions:
-    None
-    
-    Source:
-    None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle.__defaults__ ( self)
-
-
This sets the default solver flow. Anything in here can be modified after initializing a segment.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Mission/Segments/Climb/Unknown_Throttle.py
  • -
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-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Unknown__Throttle_1_1Unknown__Throttle.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Unknown__Throttle_1_1Unknown__Throttle.js deleted file mode 100644 index 89fb5b57..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Unknown__Throttle_1_1Unknown__Throttle.js +++ /dev/null @@ -1,6 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Unknown__Throttle_1_1Unknown__Throttle = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Unknown__Throttle_1_1Unknown__Throttle.html#a5541c59036630b00676c81954b6ac2b0", null ], - [ "altitude_end", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Unknown__Throttle_1_1Unknown__Throttle.html#a4163a7f22f1abbff8d4917ae5ef7c812", null ], - [ "altitude_start", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Unknown__Throttle_1_1Unknown__Throttle.html#a5d376c4c6c5076d614862ca1f78ebbae", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Unknown__Throttle_1_1Unknown__Throttle.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Unknown__Throttle_1_1Unknown__Throttle.png deleted file mode 100644 index 2b867b0b..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Unknown__Throttle_1_1Unknown__Throttle.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Aerodynamics_1_1Aerodynamics-members.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Aerodynamics_1_1Aerodynamics-members.html deleted file mode 100644 index cab499ee..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Aerodynamics_1_1Aerodynamics-members.html +++ /dev/null @@ -1,126 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics Member List
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This is the complete list of members for SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics, including all inherited members.

- - - - - - - - - - - - - - - -
__defaults__(self)SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics
aerodynamics (defined in SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics)SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics
compile(self)SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
energies (defined in SUAVE.Analyses.Mission.Segments.Conditions.Basic.Basic)SUAVE.Analyses.Mission.Segments.Conditions.Basic.Basic
expand_rows(self, rows)SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
frames (defined in SUAVE.Analyses.Mission.Segments.Conditions.Basic.Basic)SUAVE.Analyses.Mission.Segments.Conditions.Basic.Basic
freestream (defined in SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics)SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics
ones_row(self, cols)SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
ones_row_m1(self, cols)SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
ones_row_m2(self, cols)SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
propulsion (defined in SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics)SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics
stability (defined in SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics)SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics
tag (defined in SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics)SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics
weights (defined in SUAVE.Analyses.Mission.Segments.Conditions.Basic.Basic)SUAVE.Analyses.Mission.Segments.Conditions.Basic.Basic
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Aerodynamics_1_1Aerodynamics.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Aerodynamics_1_1Aerodynamics.html deleted file mode 100644 index 58e6d933..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Aerodynamics_1_1Aerodynamics.html +++ /dev/null @@ -1,222 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics Class Reference
-
-
-
-Inheritance diagram for SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics:
-
-
- - -SUAVE.Analyses.Mission.Segments.Conditions.Basic.Basic -SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions -SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid - -
- - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Conditions.Basic.Basic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
def ones_row (self, cols)
 
def ones_row_m1 (self, cols)
 
def ones_row_m2 (self, cols)
 
def expand_rows (self, rows)
 
def compile (self)
 
- - - - - - - - - - - - - - - - - - - - -

-Public Attributes

tag
 
freestream
 
aerodynamics
 
stability
 
propulsion
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Conditions.Basic.Basic
tag
 
frames
 
weights
 
energies
 
-

Detailed Description

-
This builds upon Basic, which itself builds on conditions, to add the data structure for aerodynamic mission analyses.
-
-    Assumptions:
-    None
-    
-    Source:
-    None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics.__defaults__ ( self)
-
-
This sets the default values.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Mission/Segments/Conditions/Aerodynamics.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Aerodynamics_1_1Aerodynamics.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Aerodynamics_1_1Aerodynamics.js deleted file mode 100644 index ad5df9b5..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Aerodynamics_1_1Aerodynamics.js +++ /dev/null @@ -1,9 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Aerodynamics_1_1Aerodynamics = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Aerodynamics_1_1Aerodynamics.html#a9ec64a71eda479dcc96205ddf7f5e5ab", null ], - [ "aerodynamics", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Aerodynamics_1_1Aerodynamics.html#a07fe15613d8fc3bc3db2c7374b0ea8c3", null ], - [ "freestream", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Aerodynamics_1_1Aerodynamics.html#a139f1fce458dda0ca1ce1fdf46ed1365", null ], - [ "propulsion", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Aerodynamics_1_1Aerodynamics.html#accc2c5673276771640f4386881624a8f", null ], - [ "stability", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Aerodynamics_1_1Aerodynamics.html#a1d1900314c6bf1ec5e76cb6bd1b9acbf", null ], - [ "tag", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Aerodynamics_1_1Aerodynamics.html#a13da6892fa732bdd73c6943955a0880f", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Aerodynamics_1_1Aerodynamics.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Aerodynamics_1_1Aerodynamics.png deleted file mode 100644 index 4148bfcb..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Aerodynamics_1_1Aerodynamics.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Basic_1_1Basic-members.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Basic_1_1Basic-members.html deleted file mode 100644 index 8f349afe..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Basic_1_1Basic-members.html +++ /dev/null @@ -1,122 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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- - - - - - - - -
-
SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Conditions.Basic.Basic Class Reference
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-
-
- - -SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions -SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics -SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid - -
- - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
def ones_row (self, cols)
 
def ones_row_m1 (self, cols)
 
def ones_row_m2 (self, cols)
 
def expand_rows (self, rows)
 
def compile (self)
 
- - - - - - - - - -

-Public Attributes

tag
 
frames
 
weights
 
energies
 
-

Detailed Description

-
Basic builds upon conditions to add the mission data structure. Here frames and weights are added.
-
-    Assumptions:
-    None
-    
-    Source:
-    None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Mission.Segments.Conditions.Basic.Basic.__defaults__ ( self)
-
-
This sets the default values.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Mission/Segments/Conditions/Basic.py
  • -
-
-
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions Class Reference
-
-
-
-Inheritance diagram for SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions:
-
-
- - -SUAVE.Analyses.Mission.Segments.Conditions.Basic.Basic -SUAVE.Analyses.Mission.Segments.Conditions.Numerics.Numerics -SUAVE.Analyses.Mission.Segments.Conditions.Residuals.Residuals -SUAVE.Analyses.Mission.Segments.Conditions.State.State -SUAVE.Analyses.Mission.Segments.Conditions.Unknowns.Unknowns -SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics -SUAVE.Analyses.Mission.Segments.Conditions.State.Container -SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid - -
- - - - - - - - - - - - -

-Public Member Functions

def ones_row (self, cols)
 
def ones_row_m1 (self, cols)
 
def ones_row_m2 (self, cols)
 
def expand_rows (self, rows)
 
def compile (self)
 
-

Detailed Description

-
Conditions are the magic Data that contains the information about the vehicle in flight.
-    At this point none of the information really exists. What is here are the methods that allow a mission
-    to collect the information.
-
-    Assumptions:
-    None
-    
-    Source:
-    None   
-

Member Function Documentation

- -

◆ compile()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions.compile ( self)
-
-
This is a call to expand_rows above...
-
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
- -

◆ expand_rows()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions.expand_rows ( self,
 rows 
)
-
-
Makes a 1-D array the right size. Often used after a mission is initialized to size out the vectors to the
-    right size.
-
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    rows   [int]
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
- -

◆ ones_row()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions.ones_row ( self,
 cols 
)
-
-
returns a row vector of ones with given number of columns 
-
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    cols   [in]
-    
-    Outputs:
-    Vector
-    
-    Properties Used:
-    None
-
-
-
- -

◆ ones_row_m1()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions.ones_row_m1 ( self,
 cols 
)
-
-
returns an N-1 row vector of ones with given number of columns
-
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    cols   [in]
-    
-    Outputs:
-    Vector
-    
-    Properties Used:
-    None
-
-
-
- -

◆ ones_row_m2()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions.ones_row_m2 ( self,
 cols 
)
-
-
returns an N-2 row vector of ones with given number of columns
-
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    cols   [int]
-    
-    Outputs:
-    Vector
-    
-    Properties Used:
-    None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Mission/Segments/Conditions/Conditions.py
  • -
-
-
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SUAVE.Analyses.Mission.Segments.Conditions.Numerics.Numerics Member List
-
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This is the complete list of members for SUAVE.Analyses.Mission.Segments.Conditions.Numerics.Numerics, including all inherited members.

- - - - - - - - - - - - - - - - -
__defaults__(self)SUAVE.Analyses.Mission.Segments.Conditions.Numerics.Numerics
compile(self)SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
converged (defined in SUAVE.Analyses.Mission.Segments.Conditions.Numerics.Numerics)SUAVE.Analyses.Mission.Segments.Conditions.Numerics.Numerics
dimensionless (defined in SUAVE.Analyses.Mission.Segments.Conditions.Numerics.Numerics)SUAVE.Analyses.Mission.Segments.Conditions.Numerics.Numerics
discretization_method (defined in SUAVE.Analyses.Mission.Segments.Conditions.Numerics.Numerics)SUAVE.Analyses.Mission.Segments.Conditions.Numerics.Numerics
expand_rows(self, rows)SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
number_control_points (defined in SUAVE.Analyses.Mission.Segments.Conditions.Numerics.Numerics)SUAVE.Analyses.Mission.Segments.Conditions.Numerics.Numerics
ones_row(self, cols)SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
ones_row_m1(self, cols)SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
ones_row_m2(self, cols)SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
solver_jacobian (defined in SUAVE.Analyses.Mission.Segments.Conditions.Numerics.Numerics)SUAVE.Analyses.Mission.Segments.Conditions.Numerics.Numerics
tag (defined in SUAVE.Analyses.Mission.Segments.Conditions.Numerics.Numerics)SUAVE.Analyses.Mission.Segments.Conditions.Numerics.Numerics
time (defined in SUAVE.Analyses.Mission.Segments.Conditions.Numerics.Numerics)SUAVE.Analyses.Mission.Segments.Conditions.Numerics.Numerics
tolerance_boundary_conditions (defined in SUAVE.Analyses.Mission.Segments.Conditions.Numerics.Numerics)SUAVE.Analyses.Mission.Segments.Conditions.Numerics.Numerics
tolerance_solution (defined in SUAVE.Analyses.Mission.Segments.Conditions.Numerics.Numerics)SUAVE.Analyses.Mission.Segments.Conditions.Numerics.Numerics
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Numerics_1_1Numerics.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Numerics_1_1Numerics.html deleted file mode 100644 index 0352ffd6..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Numerics_1_1Numerics.html +++ /dev/null @@ -1,216 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Mission.Segments.Conditions.Numerics.Numerics Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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-
SUAVE.Analyses.Mission.Segments.Conditions.Numerics.Numerics Class Reference
-
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-
-Inheritance diagram for SUAVE.Analyses.Mission.Segments.Conditions.Numerics.Numerics:
-
-
- - -SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions - -
- - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
def ones_row (self, cols)
 
def ones_row_m1 (self, cols)
 
def ones_row_m2 (self, cols)
 
def expand_rows (self, rows)
 
def compile (self)
 
- - - - - - - - - - - - - - - - - - - -

-Public Attributes

tag
 
number_control_points
 
discretization_method
 
solver_jacobian
 
tolerance_solution
 
tolerance_boundary_conditions
 
converged
 
dimensionless
 
time
 
-

Detailed Description

-
Creates the data structure for the numerical solving of a mission.
-
-    Assumptions:
-    None
-    
-    Source:
-    None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Mission.Segments.Conditions.Numerics.Numerics.__defaults__ ( self)
-
-
This sets the default values.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Mission/Segments/Conditions/Numerics.py
  • -
-
-
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Conditions.Residuals.Residuals Class Reference
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-Inheritance diagram for SUAVE.Analyses.Mission.Segments.Conditions.Residuals.Residuals:
-
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- - -SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions - -
- - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
def ones_row (self, cols)
 
def ones_row_m1 (self, cols)
 
def ones_row_m2 (self, cols)
 
def expand_rows (self, rows)
 
def compile (self)
 
- - - -

-Public Attributes

tag
 
-

Detailed Description

-
Creates the data structure for the residuals that solved in a mission
-
-    Assumptions:
-    None
-    
-    Source:
-    None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Mission.Segments.Conditions.Residuals.Residuals.__defaults__ ( self)
-
-
This sets the default values.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Mission/Segments/Conditions/Residuals.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Residuals_1_1Residuals.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Residuals_1_1Residuals.js deleted file mode 100644 index c9c4e144..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Residuals_1_1Residuals.js +++ /dev/null @@ -1,5 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Residuals_1_1Residuals = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Residuals_1_1Residuals.html#aceb2af45d389c182a0715dd04f1637d9", null ], - [ "tag", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Residuals_1_1Residuals.html#aea4a93810d30f3a64f04c88fb0201f56", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Residuals_1_1Residuals.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Residuals_1_1Residuals.png deleted file mode 100644 index 61d5ba70..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Residuals_1_1Residuals.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1State_1_1Container-members.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1State_1_1Container-members.html deleted file mode 100644 index 5581167f..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1State_1_1Container-members.html +++ /dev/null @@ -1,125 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Conditions.State.Container Member List
-
-
- -

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Conditions.State.Container, including all inherited members.

- - - - - - - - - - - - - - -
__defaults__(self)SUAVE.Analyses.Mission.Segments.Conditions.State.Container
compile(self)SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
conditions (defined in SUAVE.Analyses.Mission.Segments.Conditions.State.State)SUAVE.Analyses.Mission.Segments.Conditions.State.State
expand_rows(self, rows)SUAVE.Analyses.Mission.Segments.Conditions.State.State
initials (defined in SUAVE.Analyses.Mission.Segments.Conditions.State.State)SUAVE.Analyses.Mission.Segments.Conditions.State.State
merged(self)SUAVE.Analyses.Mission.Segments.Conditions.State.Container
numerics (defined in SUAVE.Analyses.Mission.Segments.Conditions.State.State)SUAVE.Analyses.Mission.Segments.Conditions.State.State
ones_row(self, cols)SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
ones_row_m1(self, cols)SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
ones_row_m2(self, cols)SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
residuals (defined in SUAVE.Analyses.Mission.Segments.Conditions.State.State)SUAVE.Analyses.Mission.Segments.Conditions.State.State
segments (defined in SUAVE.Analyses.Mission.Segments.Conditions.State.Container)SUAVE.Analyses.Mission.Segments.Conditions.State.Container
unknowns (defined in SUAVE.Analyses.Mission.Segments.Conditions.State.State)SUAVE.Analyses.Mission.Segments.Conditions.State.State
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1State_1_1Container.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1State_1_1Container.html deleted file mode 100644 index aa79f259..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1State_1_1Container.html +++ /dev/null @@ -1,242 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Mission.Segments.Conditions.State.Container Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Conditions.State.Container Class Reference
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-Inheritance diagram for SUAVE.Analyses.Mission.Segments.Conditions.State.Container:
-
-
- - -SUAVE.Analyses.Mission.Segments.Conditions.State.State -SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions - -
- - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def merged (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Conditions.State.State
def __defaults__ (self)
 
def expand_rows (self, rows)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
def ones_row (self, cols)
 
def ones_row_m1 (self, cols)
 
def ones_row_m2 (self, cols)
 
def expand_rows (self, rows)
 
def compile (self)
 
- - - - - - - - - - - - - - -

-Public Attributes

segments
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Conditions.State.State
unknowns
 
conditions
 
residuals
 
numerics
 
initials
 
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Mission.Segments.Conditions.State.Container.__defaults__ ( self)
-
-
This sets the default values.
-    
-    Assumptions:
-    Puts the segments in the right order
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
- -

◆ merged()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Mission.Segments.Conditions.State.Container.merged ( self)
-
-
Combines the states of multiple segments
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    state_out [State()]
-    
-    Properties Used:
-    None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Mission/Segments/Conditions/State.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1State_1_1Container.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1State_1_1Container.js deleted file mode 100644 index 40b1a102..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1State_1_1Container.js +++ /dev/null @@ -1,6 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1State_1_1Container = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1State_1_1Container.html#ad752d08d4eb6d2ba0ecd414a507d99ae", null ], - [ "merged", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1State_1_1Container.html#a8a8c886cda4892e24b661298f7941123", null ], - [ "segments", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1State_1_1Container.html#ac3933216404ed6c741d93d0f56a9a590", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1State_1_1Container.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1State_1_1Container.png deleted file mode 100644 index 13e5d60f..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1State_1_1Container.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1State_1_1State-members.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1State_1_1State-members.html deleted file mode 100644 index 7896ffc4..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1State_1_1State-members.html +++ /dev/null @@ -1,123 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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- - - - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1State_1_1State.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1State_1_1State.html deleted file mode 100644 index 784fb351..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1State_1_1State.html +++ /dev/null @@ -1,252 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Mission.Segments.Conditions.State.State Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Conditions.State.State Class Reference
-
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-Inheritance diagram for SUAVE.Analyses.Mission.Segments.Conditions.State.State:
-
-
- - -SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions -SUAVE.Analyses.Mission.Segments.Conditions.State.Container - -
- - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def expand_rows (self, rows)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
def ones_row (self, cols)
 
def ones_row_m1 (self, cols)
 
def ones_row_m2 (self, cols)
 
def expand_rows (self, rows)
 
def compile (self)
 
- - - - - - - - - - - -

-Public Attributes

unknowns
 
conditions
 
residuals
 
numerics
 
initials
 
-

Detailed Description

-
Creates the State data structure for storing daata that solved in a mission
-
-    Assumptions:
-    None
-    
-    Source:
-    None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Mission.Segments.Conditions.State.State.__defaults__ ( self)
-
-
This sets the default values.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
- -

◆ expand_rows()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Analyses.Mission.Segments.Conditions.State.State.expand_rows ( self,
 rows 
)
-
-
Makes a 1-D array the right size. Often used after a mission is initialized to size out the vectors to the
-    right size.
-
-    Assumptions:
-    Doesn't expand initials or numerics
-    
-    Source:
-    N/A
-    
-    Inputs:
-    rows   [int]
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Mission/Segments/Conditions/State.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1State_1_1State.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1State_1_1State.js deleted file mode 100644 index d7d1fb9b..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1State_1_1State.js +++ /dev/null @@ -1,10 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1State_1_1State = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1State_1_1State.html#a9d59416b9049579bf19c234c3ab863d2", null ], - [ "expand_rows", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1State_1_1State.html#af4ea11668dee52410256e88a59854557", null ], - [ "conditions", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1State_1_1State.html#a51990a4ffb54a995b7ea76c2a05637f7", null ], - [ "initials", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1State_1_1State.html#acb90768b54f38ef26e41276b3b12d420", null ], - [ "numerics", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1State_1_1State.html#a48045b581e869d5a67a53422d6843a77", null ], - [ "residuals", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1State_1_1State.html#ab2154a0f530fdbef75be6a5e6c983167", null ], - [ "unknowns", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1State_1_1State.html#a9bc1d1dddf44b75b0b1a41bc86b7c098", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1State_1_1State.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1State_1_1State.png deleted file mode 100644 index fcc52ddf..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1State_1_1State.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Unknowns_1_1Unknowns-members.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Unknowns_1_1Unknowns-members.html deleted file mode 100644 index d40e81e8..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Unknowns_1_1Unknowns-members.html +++ /dev/null @@ -1,119 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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- - - - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Unknowns_1_1Unknowns.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Unknowns_1_1Unknowns.html deleted file mode 100644 index 663e2653..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Unknowns_1_1Unknowns.html +++ /dev/null @@ -1,192 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Mission.Segments.Conditions.Unknowns.Unknowns Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Conditions.Unknowns.Unknowns Class Reference
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-Inheritance diagram for SUAVE.Analyses.Mission.Segments.Conditions.Unknowns.Unknowns:
-
-
- - -SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions - -
- - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
def ones_row (self, cols)
 
def ones_row_m1 (self, cols)
 
def ones_row_m2 (self, cols)
 
def expand_rows (self, rows)
 
def compile (self)
 
- - - -

-Public Attributes

tag
 
-

Detailed Description

-
Creates the data structure for the unknowns that solved in a mission
-
-    Assumptions:
-    None
-    
-    Source:
-    None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Mission.Segments.Conditions.Unknowns.Unknowns.__defaults__ ( self)
-
-
This sets the default values.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Mission/Segments/Conditions/Unknowns.py
  • -
-
-
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Cruise.Constant_Acceleration_Constant_Altitude.Constant_Acceleration_Constant_Altitude Class Reference
-
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-
-Inheritance diagram for SUAVE.Analyses.Mission.Segments.Cruise.Constant_Acceleration_Constant_Altitude.Constant_Acceleration_Constant_Altitude:
-
-
- - -SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic -SUAVE.Analyses.Mission.Segments.Simple.Simple -SUAVE.Analyses.Mission.Segments.Segment.Segment -SUAVE.Analyses.Analysis.Analysis - -
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def evaluate (self, state=None)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

altitude
 
acceleration
 
air_speed_start
 
air_speed_end
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
temperature_deviation
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
settings
 
state
 
analyses
 
process
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
Vehicle accelerates at a constant rate between two airspeeds.
-
-    Assumptions:
-    None
-    
-    Source:
-    None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Mission.Segments.Cruise.Constant_Acceleration_Constant_Altitude.Constant_Acceleration_Constant_Altitude.__defaults__ ( self)
-
-
This sets the default solver flow. Anything in here can be modified after initializing a segment.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
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The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Mission/Segments/Cruise/Constant_Acceleration_Constant_Altitude.py
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Acceleration__Constant__Alt225ba2acb5f380a25088694295eaa3d1.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Acceleration__Constant__Alt225ba2acb5f380a25088694295eaa3d1.js deleted file mode 100644 index bca8da1c..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Acceleration__Constant__Alt225ba2acb5f380a25088694295eaa3d1.js +++ /dev/null @@ -1,8 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Acceleration__Constant__Alt225ba2acb5f380a25088694295eaa3d1 = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Acceleration__Constant__Alt225ba2acb5f380a25088694295eaa3d1.html#aafe21f6215f0c838a53907a738a162b7", null ], - [ "acceleration", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Acceleration__Constant__Alt225ba2acb5f380a25088694295eaa3d1.html#a4dedcb5da3a186801fe8bed343c15064", null ], - [ "air_speed_end", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Acceleration__Constant__Alt225ba2acb5f380a25088694295eaa3d1.html#a181b8f25335143d630bdcde21aef34e1", null ], - [ "air_speed_start", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Acceleration__Constant__Alt225ba2acb5f380a25088694295eaa3d1.html#a69bd0b9baa712be94fa0042a4ea06358", null ], - [ "altitude", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Acceleration__Constant__Alt225ba2acb5f380a25088694295eaa3d1.html#a0ae8df4bb939228da3fb65bfc7966dca", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Acceleration__Constant__Alt225ba2acb5f380a25088694295eaa3d1.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Acceleration__Constant__Alt225ba2acb5f380a25088694295eaa3d1.png deleted file mode 100644 index 31e7b125..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Acceleration__Constant__Alt225ba2acb5f380a25088694295eaa3d1.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Acceleration__Constant__Altc5bd13c236150cb4a8fa295678e1052a.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Acceleration__Constant__Altc5bd13c236150cb4a8fa295678e1052a.html deleted file mode 100644 index df34a270..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Acceleration__Constant__Altc5bd13c236150cb4a8fa295678e1052a.html +++ /dev/null @@ -1,135 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Cruise.Constant_Acceleration_Constant_Altitude.Constant_Acceleration_Constant_Altitude Member List
-
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- -

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Cruise.Constant_Acceleration_Constant_Altitude.Constant_Acceleration_Constant_Altitude, including all inherited members.

- - - - - - - - - - - - - - - - - - - - - - - - -
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Acceleration_Constant_Altitude.Constant_Acceleration_Constant_Altitude
acceleration (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Acceleration_Constant_Altitude.Constant_Acceleration_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Acceleration_Constant_Altitude.Constant_Acceleration_Constant_Altitude
air_speed_end (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Acceleration_Constant_Altitude.Constant_Acceleration_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Acceleration_Constant_Altitude.Constant_Acceleration_Constant_Altitude
air_speed_start (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Acceleration_Constant_Altitude.Constant_Acceleration_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Acceleration_Constant_Altitude.Constant_Acceleration_Constant_Altitude
altitude (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Acceleration_Constant_Altitude.Constant_Acceleration_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Acceleration_Constant_Altitude.Constant_Acceleration_Constant_Altitude
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Dynamic__Pressure__Constant84b22d8b7fd8c219ab957928dcda16dd.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Dynamic__Pressure__Constant84b22d8b7fd8c219ab957928dcda16dd.html deleted file mode 100644 index 723b9f8f..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Dynamic__Pressure__Constant84b22d8b7fd8c219ab957928dcda16dd.html +++ /dev/null @@ -1,135 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude.Constant_Dynamic_Pressure_Constant_Altitude Member List
-
-
- -

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude.Constant_Dynamic_Pressure_Constant_Altitude, including all inherited members.

- - - - - - - - - - - - - - - - - - - - - - - - -
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude.Constant_Dynamic_Pressure_Constant_Altitude
air_speed (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude
altitude (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude.Constant_Dynamic_Pressure_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude.Constant_Dynamic_Pressure_Constant_Altitude
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
distance (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude.Constant_Dynamic_Pressure_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude.Constant_Dynamic_Pressure_Constant_Altitude
dynamic_pressure (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude.Constant_Dynamic_Pressure_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude.Constant_Dynamic_Pressure_Constant_Altitude
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Dynamic__Pressure__Constantd2bb54c5a6fd36eef28de53402e08b72.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Dynamic__Pressure__Constantd2bb54c5a6fd36eef28de53402e08b72.html deleted file mode 100644 index aad3fcb7..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Dynamic__Pressure__Constantd2bb54c5a6fd36eef28de53402e08b72.html +++ /dev/null @@ -1,266 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude_Loiter.Constant_Dynamic_Pressure_Constant_Altitude_Loiter Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude_Loiter.Constant_Dynamic_Pressure_Constant_Altitude_Loiter Class Reference
-
-
-
-Inheritance diagram for SUAVE.Analyses.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude_Loiter.Constant_Dynamic_Pressure_Constant_Altitude_Loiter:
-
-
- - -SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude -SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic -SUAVE.Analyses.Mission.Segments.Simple.Simple -SUAVE.Analyses.Mission.Segments.Segment.Segment -SUAVE.Analyses.Analysis.Analysis - -
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def evaluate (self, state=None)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

altitude
 
dynamic_pressure
 
time
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude
altitude
 
air_speed
 
distance
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
temperature_deviation
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
settings
 
state
 
analyses
 
process
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
Vehicle flies at a constant dynamic pressure at a set altitude for a fixed time.
-    This is useful for HALE UAVs like a solar UAV.
-
-    Assumptions:
-    Built off of a constant speed constant altitude segment
-    
-    Source:
-    None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude_Loiter.Constant_Dynamic_Pressure_Constant_Altitude_Loiter.__defaults__ ( self)
-
-
This sets the default solver flow. Anything in here can be modified after initializing a segment.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Mission/Segments/Cruise/Constant_Dynamic_Pressure_Constant_Altitude_Loiter.py
  • -
-
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude.Constant_Dynamic_Pressure_Constant_Altitude Class Reference
-
-
-
-Inheritance diagram for SUAVE.Analyses.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude.Constant_Dynamic_Pressure_Constant_Altitude:
-
-
- - -SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude -SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic -SUAVE.Analyses.Mission.Segments.Simple.Simple -SUAVE.Analyses.Mission.Segments.Segment.Segment -SUAVE.Analyses.Analysis.Analysis - -
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def evaluate (self, state=None)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
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-Public Attributes

altitude
 
dynamic_pressure
 
distance
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude
altitude
 
air_speed
 
distance
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
temperature_deviation
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
settings
 
state
 
analyses
 
process
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
Vehicle flies at a constant dynamic pressure at a set altitude for a fixed distance
-
-    Assumptions:
-    Built off of a constant speed constant altitude segment
-    
-    Source:
-    None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude.Constant_Dynamic_Pressure_Constant_Altitude.__defaults__ ( self)
-
-
This sets the default solver flow. Anything in here can be modified after initializing a segment.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Mission/Segments/Cruise/Constant_Dynamic_Pressure_Constant_Altitude.py
  • -
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Dynamic__Pressure__Constantd76ab8dcac489a382504762fcf2af994.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Dynamic__Pressure__Constantd76ab8dcac489a382504762fcf2af994.js deleted file mode 100644 index 934d2fa1..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Dynamic__Pressure__Constantd76ab8dcac489a382504762fcf2af994.js +++ /dev/null @@ -1,7 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Dynamic__Pressure__Constantd76ab8dcac489a382504762fcf2af994 = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Dynamic__Pressure__Constantd76ab8dcac489a382504762fcf2af994.html#ab1723f047fa6d695e59f2d664b433e4a", null ], - [ "altitude", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Dynamic__Pressure__Constantd76ab8dcac489a382504762fcf2af994.html#a2f69bc726928d18ce67c085726d0177b", null ], - [ "distance", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Dynamic__Pressure__Constantd76ab8dcac489a382504762fcf2af994.html#a9abea90b164a73098a749e1a11557e95", null ], - [ "dynamic_pressure", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Dynamic__Pressure__Constantd76ab8dcac489a382504762fcf2af994.html#a0eb01c172c4f38d2be4d6222d052a2ae", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Dynamic__Pressure__Constantd76ab8dcac489a382504762fcf2af994.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Dynamic__Pressure__Constantd76ab8dcac489a382504762fcf2af994.png deleted file mode 100644 index 88e9b303..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Dynamic__Pressure__Constantd76ab8dcac489a382504762fcf2af994.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Dynamic__Pressure__Constantf201c867d7444b46c0d67cf04180e6b4.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Dynamic__Pressure__Constantf201c867d7444b46c0d67cf04180e6b4.html deleted file mode 100644 index 1702de00..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Dynamic__Pressure__Constantf201c867d7444b46c0d67cf04180e6b4.html +++ /dev/null @@ -1,136 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude_Loiter.Constant_Dynamic_Pressure_Constant_Altitude_Loiter Member List
-
-
- -

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude_Loiter.Constant_Dynamic_Pressure_Constant_Altitude_Loiter, including all inherited members.

- - - - - - - - - - - - - - - - - - - - - - - - - -
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude_Loiter.Constant_Dynamic_Pressure_Constant_Altitude_Loiter
air_speed (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude
altitude (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude_Loiter.Constant_Dynamic_Pressure_Constant_Altitude_Loiter)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude_Loiter.Constant_Dynamic_Pressure_Constant_Altitude_Loiter
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
distance (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude
dynamic_pressure (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude_Loiter.Constant_Dynamic_Pressure_Constant_Altitude_Loiter)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude_Loiter.Constant_Dynamic_Pressure_Constant_Altitude_Loiter
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
time (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude_Loiter.Constant_Dynamic_Pressure_Constant_Altitude_Loiter)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude_Loiter.Constant_Dynamic_Pressure_Constant_Altitude_Loiter
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Mach__Constant__Altitude_1_5e827e2c08a67cbe4900629aad1dc2d8.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Mach__Constant__Altitude_1_5e827e2c08a67cbe4900629aad1dc2d8.html deleted file mode 100644 index 7453172c..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Mach__Constant__Altitude_1_5e827e2c08a67cbe4900629aad1dc2d8.html +++ /dev/null @@ -1,265 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude.Constant_Mach_Constant_Altitude Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude.Constant_Mach_Constant_Altitude Class Reference
-
-
-
-Inheritance diagram for SUAVE.Analyses.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude.Constant_Mach_Constant_Altitude:
-
-
- - -SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude -SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic -SUAVE.Analyses.Mission.Segments.Simple.Simple -SUAVE.Analyses.Mission.Segments.Segment.Segment -SUAVE.Analyses.Analysis.Analysis - -
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def evaluate (self, state=None)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

altitude
 
mach
 
distance
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude
altitude
 
air_speed
 
distance
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
temperature_deviation
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
settings
 
state
 
analyses
 
process
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
Vehicle flies at a constant Mach number at a set altitude for a fixed distance
-
-    Assumptions:
-    Built off of a constant speed constant altitude segment
-    
-    Source:
-    None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude.Constant_Mach_Constant_Altitude.__defaults__ ( self)
-
-
This sets the default solver flow. Anything in here can be modified after initializing a segment.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Mission/Segments/Cruise/Constant_Mach_Constant_Altitude.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Mach__Constant__Altitude_1_5e827e2c08a67cbe4900629aad1dc2d8.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Mach__Constant__Altitude_1_5e827e2c08a67cbe4900629aad1dc2d8.js deleted file mode 100644 index a9082707..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Mach__Constant__Altitude_1_5e827e2c08a67cbe4900629aad1dc2d8.js +++ /dev/null @@ -1,7 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Mach__Constant__Altitude_1_5e827e2c08a67cbe4900629aad1dc2d8 = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Mach__Constant__Altitude_1_5e827e2c08a67cbe4900629aad1dc2d8.html#a7d8b2b080993d6463d0fe6802cbb420d", null ], - [ "altitude", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Mach__Constant__Altitude_1_5e827e2c08a67cbe4900629aad1dc2d8.html#a19f94bf5f6fb32ca8d1620e31c50f16f", null ], - [ "distance", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Mach__Constant__Altitude_1_5e827e2c08a67cbe4900629aad1dc2d8.html#a9f5f25d0a706c222a47183d9453b0557", null ], - [ "mach", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Mach__Constant__Altitude_1_5e827e2c08a67cbe4900629aad1dc2d8.html#a2222cb39160b743fdeac2c9a606ee74b", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Mach__Constant__Altitude_1_5e827e2c08a67cbe4900629aad1dc2d8.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Mach__Constant__Altitude_1_5e827e2c08a67cbe4900629aad1dc2d8.png deleted file mode 100644 index 1cdfde03..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Mach__Constant__Altitude_1_5e827e2c08a67cbe4900629aad1dc2d8.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Mach__Constant__Altitude_1_b588333bf5d262abe2e6a6f7a38d9137.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Mach__Constant__Altitude_1_b588333bf5d262abe2e6a6f7a38d9137.html deleted file mode 100644 index 62808f99..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Mach__Constant__Altitude_1_b588333bf5d262abe2e6a6f7a38d9137.html +++ /dev/null @@ -1,135 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude.Constant_Mach_Constant_Altitude Member List
-
-
- -

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude.Constant_Mach_Constant_Altitude, including all inherited members.

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__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude.Constant_Mach_Constant_Altitude
air_speed (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude
altitude (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude.Constant_Mach_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude.Constant_Mach_Constant_Altitude
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
distance (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude.Constant_Mach_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude.Constant_Mach_Constant_Altitude
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
mach (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude.Constant_Mach_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude.Constant_Mach_Constant_Altitude
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Mach__Constant__Altitude__L04d64fe23756079239c105324cc22cfa.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Mach__Constant__Altitude__L04d64fe23756079239c105324cc22cfa.html deleted file mode 100644 index d2ff8d40..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Mach__Constant__Altitude__L04d64fe23756079239c105324cc22cfa.html +++ /dev/null @@ -1,136 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude_Loiter.Constant_Mach_Constant_Altitude_Loiter Member List
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-
- -

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude_Loiter.Constant_Mach_Constant_Altitude_Loiter, including all inherited members.

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__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude_Loiter.Constant_Mach_Constant_Altitude_Loiter
air_speed (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude
altitude (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude_Loiter.Constant_Mach_Constant_Altitude_Loiter)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude_Loiter.Constant_Mach_Constant_Altitude_Loiter
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
distance (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
mach (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude_Loiter.Constant_Mach_Constant_Altitude_Loiter)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude_Loiter.Constant_Mach_Constant_Altitude_Loiter
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
time (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude_Loiter.Constant_Mach_Constant_Altitude_Loiter)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude_Loiter.Constant_Mach_Constant_Altitude_Loiter
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Mach__Constant__Altitude__Le692539278d1a1cd0f056698409097dd.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Mach__Constant__Altitude__Le692539278d1a1cd0f056698409097dd.html deleted file mode 100644 index 346d8eac..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Mach__Constant__Altitude__Le692539278d1a1cd0f056698409097dd.html +++ /dev/null @@ -1,266 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude_Loiter.Constant_Mach_Constant_Altitude_Loiter Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude_Loiter.Constant_Mach_Constant_Altitude_Loiter Class Reference
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-
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-Inheritance diagram for SUAVE.Analyses.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude_Loiter.Constant_Mach_Constant_Altitude_Loiter:
-
-
- - -SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude -SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic -SUAVE.Analyses.Mission.Segments.Simple.Simple -SUAVE.Analyses.Mission.Segments.Segment.Segment -SUAVE.Analyses.Analysis.Analysis - -
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-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def evaluate (self, state=None)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
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-Public Attributes

altitude
 
mach
 
time
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude
altitude
 
air_speed
 
distance
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
temperature_deviation
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
settings
 
state
 
analyses
 
process
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
Vehicle flies at a constant Mach number at a set altitude for a fixed time.
-    This is useful aircraft who need to station keep.
-
-    Assumptions:
-    Built off of a constant speed constant altitude segment
-    
-    Source:
-    None
-

Member Function Documentation

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◆ __defaults__()

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def SUAVE.Analyses.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude_Loiter.Constant_Mach_Constant_Altitude_Loiter.__defaults__ ( self)
-
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This sets the default solver flow. Anything in here can be modified after initializing a segment.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Mission/Segments/Cruise/Constant_Mach_Constant_Altitude_Loiter.py
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-
- - - - - - - - -
-
SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Cruise.Constant_Pitch_Rate_Constant_Altitude.Constant_Pitch_Rate_Constant_Altitude Member List
-
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- -

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Cruise.Constant_Pitch_Rate_Constant_Altitude.Constant_Pitch_Rate_Constant_Altitude, including all inherited members.

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__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Pitch_Rate_Constant_Altitude.Constant_Pitch_Rate_Constant_Altitude
altitude (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Pitch_Rate_Constant_Altitude.Constant_Pitch_Rate_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Pitch_Rate_Constant_Altitude.Constant_Pitch_Rate_Constant_Altitude
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
pitch_final (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Pitch_Rate_Constant_Altitude.Constant_Pitch_Rate_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Pitch_Rate_Constant_Altitude.Constant_Pitch_Rate_Constant_Altitude
pitch_initial (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Pitch_Rate_Constant_Altitude.Constant_Pitch_Rate_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Pitch_Rate_Constant_Altitude.Constant_Pitch_Rate_Constant_Altitude
pitch_rate (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Pitch_Rate_Constant_Altitude.Constant_Pitch_Rate_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Pitch_Rate_Constant_Altitude.Constant_Pitch_Rate_Constant_Altitude
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Pitch__Rate__Constant__Altid7ab7e269824a308d0bb2c170f87d30a.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Pitch__Rate__Constant__Altid7ab7e269824a308d0bb2c170f87d30a.html deleted file mode 100644 index d2a1d735..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Pitch__Rate__Constant__Altid7ab7e269824a308d0bb2c170f87d30a.html +++ /dev/null @@ -1,255 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Mission.Segments.Cruise.Constant_Pitch_Rate_Constant_Altitude.Constant_Pitch_Rate_Constant_Altitude Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Cruise.Constant_Pitch_Rate_Constant_Altitude.Constant_Pitch_Rate_Constant_Altitude Class Reference
-
-
-
-Inheritance diagram for SUAVE.Analyses.Mission.Segments.Cruise.Constant_Pitch_Rate_Constant_Altitude.Constant_Pitch_Rate_Constant_Altitude:
-
-
- - -SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic -SUAVE.Analyses.Mission.Segments.Simple.Simple -SUAVE.Analyses.Mission.Segments.Segment.Segment -SUAVE.Analyses.Analysis.Analysis - -
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def evaluate (self, state=None)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

altitude
 
pitch_rate
 
pitch_initial
 
pitch_final
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
temperature_deviation
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
settings
 
state
 
analyses
 
process
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
Vehicle flies at a constant pitch rate at a set altitude. This is maneuvering flight.
-    This is used in VTOL aircraft which need to transition from one pitch attitude to another.
-
-    Assumptions:
-    None
-    
-    Source:
-    None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Mission.Segments.Cruise.Constant_Pitch_Rate_Constant_Altitude.Constant_Pitch_Rate_Constant_Altitude.__defaults__ ( self)
-
-
This sets the default solver flow. Anything in here can be modified after initializing a segment.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Mission/Segments/Cruise/Constant_Pitch_Rate_Constant_Altitude.py
  • -
-
-
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude Member List
-
-
- -

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude, including all inherited members.

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__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude
air_speed (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude
altitude (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
distance (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Speed__Constant__Altitude_1f9238ad770ff99e466228b3c4a43d18b.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Speed__Constant__Altitude_1f9238ad770ff99e466228b3c4a43d18b.html deleted file mode 100644 index cf97f540..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Speed__Constant__Altitude_1f9238ad770ff99e466228b3c4a43d18b.html +++ /dev/null @@ -1,257 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude Class Reference - - - - - - - - - - - - - - - -
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- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude Class Reference
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-
-Inheritance diagram for SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude:
-
-
- - -SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic -SUAVE.Analyses.Mission.Segments.Simple.Simple -SUAVE.Analyses.Mission.Segments.Segment.Segment -SUAVE.Analyses.Analysis.Analysis -SUAVE.Analyses.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude.Constant_Dynamic_Pressure_Constant_Altitude -SUAVE.Analyses.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude_Loiter.Constant_Dynamic_Pressure_Constant_Altitude_Loiter -SUAVE.Analyses.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude.Constant_Mach_Constant_Altitude -SUAVE.Analyses.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude_Loiter.Constant_Mach_Constant_Altitude_Loiter -SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude_Loiter.Constant_Speed_Constant_Altitude_Loiter - -
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def evaluate (self, state=None)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

altitude
 
air_speed
 
distance
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
temperature_deviation
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
settings
 
state
 
analyses
 
process
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
The CLASSIC! Fixed true airspeed and altitude and a set distance.
-    Most other cruise segments are built off this segment. The most simple segment you can fly.
-
-    Assumptions:
-    None
-    
-    Source:
-    None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude.__defaults__ ( self)
-
-
This sets the default solver flow. Anything in here can be modified after initializing a segment.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Mission/Segments/Cruise/Constant_Speed_Constant_Altitude.py
  • -
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Speed__Constant__Altitude_1f9238ad770ff99e466228b3c4a43d18b.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Speed__Constant__Altitude_1f9238ad770ff99e466228b3c4a43d18b.js deleted file mode 100644 index b2a41361..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Speed__Constant__Altitude_1f9238ad770ff99e466228b3c4a43d18b.js +++ /dev/null @@ -1,7 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Speed__Constant__Altitude_1f9238ad770ff99e466228b3c4a43d18b = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Speed__Constant__Altitude_1f9238ad770ff99e466228b3c4a43d18b.html#ac08d33a39d5aac732a1834dc4c34a033", null ], - [ "air_speed", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Speed__Constant__Altitude_1f9238ad770ff99e466228b3c4a43d18b.html#a894853f8ec11e54beaf3ce8c69424441", null ], - [ "altitude", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Speed__Constant__Altitude_1f9238ad770ff99e466228b3c4a43d18b.html#a3fef73e1e7145c5524bb8c149f92a216", null ], - [ "distance", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Speed__Constant__Altitude_1f9238ad770ff99e466228b3c4a43d18b.html#a19e019305903b3b2c83f96894694912a", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Speed__Constant__Altitude_1f9238ad770ff99e466228b3c4a43d18b.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Speed__Constant__Altitude_1f9238ad770ff99e466228b3c4a43d18b.png deleted file mode 100644 index ab95ed28..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Speed__Constant__Altitude_1f9238ad770ff99e466228b3c4a43d18b.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Speed__Constant__Altitude__467b5797fe6882a2f528d361be26a113.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Speed__Constant__Altitude__467b5797fe6882a2f528d361be26a113.html deleted file mode 100644 index 9ed3bce5..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Speed__Constant__Altitude__467b5797fe6882a2f528d361be26a113.html +++ /dev/null @@ -1,135 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude_Loiter.Constant_Speed_Constant_Altitude_Loiter Member List
-
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- -

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude_Loiter.Constant_Speed_Constant_Altitude_Loiter, including all inherited members.

- - - - - - - - - - - - - - - - - - - - - - - - -
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude_Loiter.Constant_Speed_Constant_Altitude_Loiter
air_speed (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude_Loiter.Constant_Speed_Constant_Altitude_Loiter)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude_Loiter.Constant_Speed_Constant_Altitude_Loiter
altitude (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude_Loiter.Constant_Speed_Constant_Altitude_Loiter)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude_Loiter.Constant_Speed_Constant_Altitude_Loiter
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
distance (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
time (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude_Loiter.Constant_Speed_Constant_Altitude_Loiter)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude_Loiter.Constant_Speed_Constant_Altitude_Loiter
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Speed__Constant__Altitude__fa03d2425e79228138954539409d2195.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Speed__Constant__Altitude__fa03d2425e79228138954539409d2195.html deleted file mode 100644 index 83519ba1..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Speed__Constant__Altitude__fa03d2425e79228138954539409d2195.html +++ /dev/null @@ -1,266 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude_Loiter.Constant_Speed_Constant_Altitude_Loiter Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude_Loiter.Constant_Speed_Constant_Altitude_Loiter Class Reference
-
-
-
-Inheritance diagram for SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude_Loiter.Constant_Speed_Constant_Altitude_Loiter:
-
-
- - -SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude -SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic -SUAVE.Analyses.Mission.Segments.Simple.Simple -SUAVE.Analyses.Mission.Segments.Segment.Segment -SUAVE.Analyses.Analysis.Analysis - -
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-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def evaluate (self, state=None)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

altitude
 
air_speed
 
time
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude
altitude
 
air_speed
 
distance
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
temperature_deviation
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
settings
 
state
 
analyses
 
process
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
Fixed true airspeed and altitude for a fixed time.
-    This is useful aircraft who need to station keep.
-
-    Assumptions:
-    Built off of a constant speed constant altitude segment
-    
-    Source:
-    None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude_Loiter.Constant_Speed_Constant_Altitude_Loiter.__defaults__ ( self)
-
-
This sets the default solver flow. Anything in here can be modified after initializing a segment.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Mission/Segments/Cruise/Constant_Speed_Constant_Altitude_Loiter.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Speed__Constant__Altitude__fa03d2425e79228138954539409d2195.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Speed__Constant__Altitude__fa03d2425e79228138954539409d2195.js deleted file mode 100644 index b31afef8..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Speed__Constant__Altitude__fa03d2425e79228138954539409d2195.js +++ /dev/null @@ -1,7 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Speed__Constant__Altitude__fa03d2425e79228138954539409d2195 = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Speed__Constant__Altitude__fa03d2425e79228138954539409d2195.html#a4958b4d5ef63b8904d06aa5aac837509", null ], - [ "air_speed", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Speed__Constant__Altitude__fa03d2425e79228138954539409d2195.html#a73c7b378aa0b5718c378b6b5c761e8df", null ], - [ "altitude", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Speed__Constant__Altitude__fa03d2425e79228138954539409d2195.html#ac661b21ede548701bac1dd471d52c5e9", null ], - [ "time", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Speed__Constant__Altitude__fa03d2425e79228138954539409d2195.html#a01ff1a698df40df8ab82a6bd94676a36", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Speed__Constant__Altitude__fa03d2425e79228138954539409d2195.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Speed__Constant__Altitude__fa03d2425e79228138954539409d2195.png deleted file mode 100644 index e8fd4dd8..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Speed__Constant__Altitude__fa03d2425e79228138954539409d2195.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Throttle__Constant__Altitud087b9361606d9421bb3adf969d22c3d7.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Throttle__Constant__Altitud087b9361606d9421bb3adf969d22c3d7.html deleted file mode 100644 index 09190b08..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Throttle__Constant__Altitud087b9361606d9421bb3adf969d22c3d7.html +++ /dev/null @@ -1,254 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Mission.Segments.Cruise.Constant_Throttle_Constant_Altitude.Constant_Throttle_Constant_Altitude Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Cruise.Constant_Throttle_Constant_Altitude.Constant_Throttle_Constant_Altitude Class Reference
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-
-
-Inheritance diagram for SUAVE.Analyses.Mission.Segments.Cruise.Constant_Throttle_Constant_Altitude.Constant_Throttle_Constant_Altitude:
-
-
- - -SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic -SUAVE.Analyses.Mission.Segments.Simple.Simple -SUAVE.Analyses.Mission.Segments.Segment.Segment -SUAVE.Analyses.Analysis.Analysis - -
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def evaluate (self, state=None)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
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-Public Attributes

throttle
 
altitude
 
air_speed_start
 
air_speed_end
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
temperature_deviation
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
settings
 
state
 
analyses
 
process
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
Vehicle flies at a set throttle setting. Allows a vehicle to do a level acceleration.
-
-    Assumptions:
-    None
-    
-    Source:
-    None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Mission.Segments.Cruise.Constant_Throttle_Constant_Altitude.Constant_Throttle_Constant_Altitude.__defaults__ ( self)
-
-
This sets the default solver flow. Anything in here can be modified after initializing a segment.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
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-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Mission/Segments/Cruise/Constant_Throttle_Constant_Altitude.py
  • -
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Throttle__Constant__Altitud087b9361606d9421bb3adf969d22c3d7.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Throttle__Constant__Altitud087b9361606d9421bb3adf969d22c3d7.js deleted file mode 100644 index ec6baa02..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Throttle__Constant__Altitud087b9361606d9421bb3adf969d22c3d7.js +++ /dev/null @@ -1,8 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Throttle__Constant__Altitud087b9361606d9421bb3adf969d22c3d7 = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Throttle__Constant__Altitud087b9361606d9421bb3adf969d22c3d7.html#a00abe2b17d918ec7e9444a4e17dd5075", null ], - [ "air_speed_end", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Throttle__Constant__Altitud087b9361606d9421bb3adf969d22c3d7.html#a8ac186fce3147771184f518da49309e9", null ], - [ "air_speed_start", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Throttle__Constant__Altitud087b9361606d9421bb3adf969d22c3d7.html#a211059093e2b63971f53b3b29cbe2cc1", null ], - [ "altitude", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Throttle__Constant__Altitud087b9361606d9421bb3adf969d22c3d7.html#a0acce9610081c654dc2d9eefb0033e79", null ], - [ "throttle", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Throttle__Constant__Altitud087b9361606d9421bb3adf969d22c3d7.html#a9c3834d7b80dbf89ee79ef10d8909c8f", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Throttle__Constant__Altitud087b9361606d9421bb3adf969d22c3d7.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Throttle__Constant__Altitud087b9361606d9421bb3adf969d22c3d7.png deleted file mode 100644 index 5126319b..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Throttle__Constant__Altitud087b9361606d9421bb3adf969d22c3d7.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Throttle__Constant__Altitudce228370873e346df4c962017addcbe3.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Throttle__Constant__Altitudce228370873e346df4c962017addcbe3.html deleted file mode 100644 index 4778e9b6..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Throttle__Constant__Altitudce228370873e346df4c962017addcbe3.html +++ /dev/null @@ -1,135 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Cruise.Constant_Throttle_Constant_Altitude.Constant_Throttle_Constant_Altitude Member List
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This is the complete list of members for SUAVE.Analyses.Mission.Segments.Cruise.Constant_Throttle_Constant_Altitude.Constant_Throttle_Constant_Altitude, including all inherited members.

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__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Throttle_Constant_Altitude.Constant_Throttle_Constant_Altitude
air_speed_end (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Throttle_Constant_Altitude.Constant_Throttle_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Throttle_Constant_Altitude.Constant_Throttle_Constant_Altitude
air_speed_start (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Throttle_Constant_Altitude.Constant_Throttle_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Throttle_Constant_Altitude.Constant_Throttle_Constant_Altitude
altitude (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Throttle_Constant_Altitude.Constant_Throttle_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Throttle_Constant_Altitude.Constant_Throttle_Constant_Altitude
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
throttle (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Throttle_Constant_Altitude.Constant_Throttle_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Throttle_Constant_Altitude.Constant_Throttle_Constant_Altitude
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__EAS__Constant__Rate_1_1Con60fcaf9d1adb0d2602b65938abb41d71.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__EAS__Constant__Rate_1_1Con60fcaf9d1adb0d2602b65938abb41d71.html deleted file mode 100644 index 2e153702..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__EAS__Constant__Rate_1_1Con60fcaf9d1adb0d2602b65938abb41d71.html +++ /dev/null @@ -1,135 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Descent.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate Member List
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-
- -

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Descent.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate, including all inherited members.

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__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Descent.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate
altitude_end (defined in SUAVE.Analyses.Mission.Segments.Descent.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate)SUAVE.Analyses.Mission.Segments.Descent.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate
altitude_start (defined in SUAVE.Analyses.Mission.Segments.Descent.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate)SUAVE.Analyses.Mission.Segments.Descent.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
descent_rate (defined in SUAVE.Analyses.Mission.Segments.Descent.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate)SUAVE.Analyses.Mission.Segments.Descent.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate
equivalent_air_speed (defined in SUAVE.Analyses.Mission.Segments.Descent.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate)SUAVE.Analyses.Mission.Segments.Descent.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__EAS__Constant__Rate_1_1Constant__EAS__Constant__Rate.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__EAS__Constant__Rate_1_1Constant__EAS__Constant__Rate.html deleted file mode 100644 index 377354e4..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__EAS__Constant__Rate_1_1Constant__EAS__Constant__Rate.html +++ /dev/null @@ -1,265 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Mission.Segments.Descent.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Descent.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate Class Reference
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-Inheritance diagram for SUAVE.Analyses.Mission.Segments.Descent.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate:
-
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- - -SUAVE.Analyses.Mission.Segments.Descent.Unknown_Throttle.Unknown_Throttle -SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic -SUAVE.Analyses.Mission.Segments.Simple.Simple -SUAVE.Analyses.Mission.Segments.Segment.Segment -SUAVE.Analyses.Analysis.Analysis - -
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-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Descent.Unknown_Throttle.Unknown_Throttle
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def evaluate (self, state=None)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

altitude_start
 
altitude_end
 
descent_rate
 
equivalent_air_speed
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Descent.Unknown_Throttle.Unknown_Throttle
altitude_start
 
altitude_end
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
temperature_deviation
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
settings
 
state
 
analyses
 
process
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
Fixed at an Equivalent Airspeed (EAS) the vehicle will descent at a constant rate.
-
-    Assumptions:
-    None
-    
-    Source:
-    None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Mission.Segments.Descent.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate.__defaults__ ( self)
-
-
This sets the default solver flow. Anything in here can be modified after initializing a segment.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Mission/Segments/Descent/Constant_EAS_Constant_Rate.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__EAS__Constant__Rate_1_1Constant__EAS__Constant__Rate.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__EAS__Constant__Rate_1_1Constant__EAS__Constant__Rate.js deleted file mode 100644 index d53a26c1..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__EAS__Constant__Rate_1_1Constant__EAS__Constant__Rate.js +++ /dev/null @@ -1,8 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__EAS__Constant__Rate_1_1Constant__EAS__Constant__Rate = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__EAS__Constant__Rate_1_1Constant__EAS__Constant__Rate.html#a7615c15af3da139e2fb65d2cc68837b7", null ], - [ "altitude_end", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__EAS__Constant__Rate_1_1Constant__EAS__Constant__Rate.html#ae75a8b7764cc805f814f91291bac2e3f", null ], - [ "altitude_start", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__EAS__Constant__Rate_1_1Constant__EAS__Constant__Rate.html#a939e431f3199b662d851509bb58ae2e4", null ], - [ "descent_rate", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__EAS__Constant__Rate_1_1Constant__EAS__Constant__Rate.html#aaa9430333d797a3a4e139072db72a148", null ], - [ "equivalent_air_speed", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__EAS__Constant__Rate_1_1Constant__EAS__Constant__Rate.html#a13dc0023d967eaa2c500d9d541b29cb5", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__EAS__Constant__Rate_1_1Constant__EAS__Constant__Rate.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__EAS__Constant__Rate_1_1Constant__EAS__Constant__Rate.png deleted file mode 100644 index 27061858..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__EAS__Constant__Rate_1_1Constant__EAS__Constant__Rate.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Angle_1_113016f07454f53dbac238312756446d6.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Angle_1_113016f07454f53dbac238312756446d6.html deleted file mode 100644 index 350007d9..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Angle_1_113016f07454f53dbac238312756446d6.html +++ /dev/null @@ -1,265 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle Class Reference
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-
-
-Inheritance diagram for SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle:
-
-
- - -SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle -SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic -SUAVE.Analyses.Mission.Segments.Simple.Simple -SUAVE.Analyses.Mission.Segments.Segment.Segment -SUAVE.Analyses.Analysis.Analysis - -
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def evaluate (self, state=None)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

altitude_start
 
altitude_end
 
descent_angle
 
air_speed
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle
altitude_start
 
altitude_end
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
temperature_deviation
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
settings
 
state
 
analyses
 
process
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
Fixed at a true airspeed the vehicle will descend at a constant angle.
-
-    Assumptions:
-    None
-    
-    Source:
-    None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle.__defaults__ ( self)
-
-
This sets the default solver flow. Anything in here can be modified after initializing a segment.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Mission/Segments/Descent/Constant_Speed_Constant_Angle.py
  • -
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Angle_1_113016f07454f53dbac238312756446d6.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Angle_1_113016f07454f53dbac238312756446d6.js deleted file mode 100644 index 04eb783b..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Angle_1_113016f07454f53dbac238312756446d6.js +++ /dev/null @@ -1,8 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Angle_1_113016f07454f53dbac238312756446d6 = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Angle_1_113016f07454f53dbac238312756446d6.html#a196ee3d4d062a6d50c967e67106b6114", null ], - [ "air_speed", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Angle_1_113016f07454f53dbac238312756446d6.html#ab65eb0ec80ac2813a4680da642ae6fa7", null ], - [ "altitude_end", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Angle_1_113016f07454f53dbac238312756446d6.html#a3f3a26a19a34597691602e182e61ab00", null ], - [ "altitude_start", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Angle_1_113016f07454f53dbac238312756446d6.html#afb7d66ea4d3e838ee14b6a6305249dcf", null ], - [ "descent_angle", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Angle_1_113016f07454f53dbac238312756446d6.html#a5e3e5ccf847de44bad50edc23fba581c", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Angle_1_113016f07454f53dbac238312756446d6.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Angle_1_113016f07454f53dbac238312756446d6.png deleted file mode 100644 index 74d1dccf..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Angle_1_113016f07454f53dbac238312756446d6.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Angle_1_13c1191d3d0ed5ed2722fffd200c9b64b.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Angle_1_13c1191d3d0ed5ed2722fffd200c9b64b.html deleted file mode 100644 index ad2125b3..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Angle_1_13c1191d3d0ed5ed2722fffd200c9b64b.html +++ /dev/null @@ -1,135 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle Member List
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This is the complete list of members for SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle, including all inherited members.

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__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle
air_speed (defined in SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle)SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle
altitude_end (defined in SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle)SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle
altitude_start (defined in SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle)SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
descent_angle (defined in SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle)SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Angle__No6c766c7d7f943d7125da304d9336dbfa.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Angle__No6c766c7d7f943d7125da304d9336dbfa.html deleted file mode 100644 index 813b698d..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Angle__No6c766c7d7f943d7125da304d9336dbfa.html +++ /dev/null @@ -1,135 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise Member List
-
-
- -

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise, including all inherited members.

- - - - - - - - - - - - - - - - - - - - - - - - -
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise
air_speed (defined in SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise)SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise
altitude_end (defined in SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise)SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise
altitude_start (defined in SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise)SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
descent_angle (defined in SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise)SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Angle__Noa39040ebc44f8c6e229921b8045d6b6f.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Angle__Noa39040ebc44f8c6e229921b8045d6b6f.html deleted file mode 100644 index 4d9cfffa..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Angle__Noa39040ebc44f8c6e229921b8045d6b6f.html +++ /dev/null @@ -1,268 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise Class Reference
-
-
-
-Inheritance diagram for SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise:
-
-
- - -SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle -SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic -SUAVE.Analyses.Mission.Segments.Simple.Simple -SUAVE.Analyses.Mission.Segments.Segment.Segment -SUAVE.Analyses.Analysis.Analysis - -
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def evaluate (self, state=None)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

altitude_start
 
altitude_end
 
descent_angle
 
air_speed
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle
altitude_start
 
altitude_end
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
temperature_deviation
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
settings
 
state
 
analyses
 
process
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
Fixed at a true airspeed the vehicle will descend at a constant angle. This is a specific segment for Noise.
-    A vehicle performs a descent to landing in accordance with a certification points for landing noise.
-    Don't use this segment unless you're planning on post process for noise. It is slower than the normal constant
-    speed constand angle segment.
-
-    Assumptions:
-    The points are linearly spaced rather than chebyshev spaced to give the proper "microphone" locations.
-    
-    Source:
-    None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise.__defaults__ ( self)
-
-
This sets the default solver flow. Anything in here can be modified after initializing a segment.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Mission/Segments/Descent/Constant_Speed_Constant_Angle_Noise.py
  • -
-
-
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SUAVE -  1.0.0 -
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SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate Member List
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- -

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate, including all inherited members.

- - - - - - - - - - - - - - - - - - - - - - - - -
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate
air_speed (defined in SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate)SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate
altitude_end (defined in SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate)SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate
altitude_start (defined in SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate)SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
descent_rate (defined in SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate)SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Rate_1_1Constant__Speed__Constant__Rate.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Rate_1_1Constant__Speed__Constant__Rate.html deleted file mode 100644 index 2c9bde0b..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Rate_1_1Constant__Speed__Constant__Rate.html +++ /dev/null @@ -1,257 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate Class Reference
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-
-Inheritance diagram for SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate:
-
-
- - -SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle -SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic -SUAVE.Analyses.Mission.Segments.Simple.Simple -SUAVE.Analyses.Mission.Segments.Segment.Segment -SUAVE.Analyses.Analysis.Analysis - -
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def evaluate (self, state=None)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

altitude_start
 
altitude_end
 
descent_rate
 
air_speed
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle
altitude_start
 
altitude_end
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
temperature_deviation
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
settings
 
state
 
analyses
 
process
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Member Function Documentation

- -

◆ __defaults__()

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def SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate.__defaults__ ( self)
-
-
This sets the default solver flow. Anything in here can be modified after initializing a segment.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
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-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Mission/Segments/Descent/Constant_Speed_Constant_Rate.py
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Rate_1_1Constant__Speed__Constant__Rate.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Rate_1_1Constant__Speed__Constant__Rate.js deleted file mode 100644 index d8880637..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Rate_1_1Constant__Speed__Constant__Rate.js +++ /dev/null @@ -1,8 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Rate_1_1Constant__Speed__Constant__Rate = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Rate_1_1Constant__Speed__Constant__Rate.html#a23552ef382453348ce05aa599e9bd788", null ], - [ "air_speed", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Rate_1_1Constant__Speed__Constant__Rate.html#a343792d9b4f79b994002a2c30833b5c0", null ], - [ "altitude_end", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Rate_1_1Constant__Speed__Constant__Rate.html#a1f6f7fd6634fc2c64a6fe418fdaa75d1", null ], - [ "altitude_start", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Rate_1_1Constant__Speed__Constant__Rate.html#ae8d2f863a4a89e7a80bbfcdce7120813", null ], - [ "descent_rate", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Rate_1_1Constant__Speed__Constant__Rate.html#a17b5479e0213916e6bab9828d1f15c3a", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Rate_1_1Constant__Speed__Constant__Rate.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Rate_1_1Constant__Speed__Constant__Rate.png deleted file mode 100644 index 1b1e0346..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Rate_1_1Constant__Speed__Constant__Rate.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Linear__Mach__Constant__Rate_1_1Linear__Mach__Constant__Rate.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Linear__Mach__Constant__Rate_1_1Linear__Mach__Constant__Rate.html deleted file mode 100644 index bd887fe5..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Linear__Mach__Constant__Rate_1_1Linear__Mach__Constant__Rate.html +++ /dev/null @@ -1,269 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Mission.Segments.Descent.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Descent.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate Class Reference
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-
-Inheritance diagram for SUAVE.Analyses.Mission.Segments.Descent.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate:
-
-
- - -SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle -SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic -SUAVE.Analyses.Mission.Segments.Simple.Simple -SUAVE.Analyses.Mission.Segments.Segment.Segment -SUAVE.Analyses.Analysis.Analysis - -
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-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def evaluate (self, state=None)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

altitude_start
 
altitude_end
 
climb_rate
 
mach_end
 
mach_start
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle
altitude_start
 
altitude_end
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
temperature_deviation
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
settings
 
state
 
analyses
 
process
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
Change Mach numbers during a descent while descending at a constant rate. The Mach number changes linearly
-    throughout the descent.
-
-    Assumptions:
-    None
-    
-    Source:
-    None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Mission.Segments.Descent.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate.__defaults__ ( self)
-
-
This sets the default solver flow. Anything in here can be modified after initializing a segment.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Mission/Segments/Descent/Linear_Mach_Constant_Rate.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Linear__Mach__Constant__Rate_1_1Linear__Mach__Constant__Rate.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Linear__Mach__Constant__Rate_1_1Linear__Mach__Constant__Rate.js deleted file mode 100644 index 3258b84e..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Linear__Mach__Constant__Rate_1_1Linear__Mach__Constant__Rate.js +++ /dev/null @@ -1,9 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Linear__Mach__Constant__Rate_1_1Linear__Mach__Constant__Rate = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Linear__Mach__Constant__Rate_1_1Linear__Mach__Constant__Rate.html#aabd70bf6c064eba2425ab03d501bc362", null ], - [ "altitude_end", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Linear__Mach__Constant__Rate_1_1Linear__Mach__Constant__Rate.html#a532a94b40f26577b5292c260538f661c", null ], - [ "altitude_start", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Linear__Mach__Constant__Rate_1_1Linear__Mach__Constant__Rate.html#a55f9dbc099bdc473c3ad9a9fd42d053d", null ], - [ "climb_rate", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Linear__Mach__Constant__Rate_1_1Linear__Mach__Constant__Rate.html#a833105ed7f276464e01d8c53f20537cd", null ], - [ "mach_end", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Linear__Mach__Constant__Rate_1_1Linear__Mach__Constant__Rate.html#aafbc811cbfe78bcd603a7f6cc2af6e48", null ], - [ "mach_start", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Linear__Mach__Constant__Rate_1_1Linear__Mach__Constant__Rate.html#aa056e902972480320d0ced21d1789840", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Linear__Mach__Constant__Rate_1_1Linear__Mach__Constant__Rate.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Linear__Mach__Constant__Rate_1_1Linear__Mach__Constant__Rate.png deleted file mode 100644 index 556d8f81..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Linear__Mach__Constant__Rate_1_1Linear__Mach__Constant__Rate.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Linear__Mach__Constant__Rate_1_1Linec3b1df3c7852606c53bfd248df7e005e.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Linear__Mach__Constant__Rate_1_1Linec3b1df3c7852606c53bfd248df7e005e.html deleted file mode 100644 index 9e03a55f..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Linear__Mach__Constant__Rate_1_1Linec3b1df3c7852606c53bfd248df7e005e.html +++ /dev/null @@ -1,136 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
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SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Descent.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate Member List
-
-
- -

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Descent.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate, including all inherited members.

- - - - - - - - - - - - - - - - - - - - - - - - - -
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Descent.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate
altitude_end (defined in SUAVE.Analyses.Mission.Segments.Descent.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate)SUAVE.Analyses.Mission.Segments.Descent.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate
altitude_start (defined in SUAVE.Analyses.Mission.Segments.Descent.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate)SUAVE.Analyses.Mission.Segments.Descent.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
climb_rate (defined in SUAVE.Analyses.Mission.Segments.Descent.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate)SUAVE.Analyses.Mission.Segments.Descent.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
mach_end (defined in SUAVE.Analyses.Mission.Segments.Descent.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate)SUAVE.Analyses.Mission.Segments.Descent.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate
mach_start (defined in SUAVE.Analyses.Mission.Segments.Descent.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate)SUAVE.Analyses.Mission.Segments.Descent.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Unknown__Throttle_1_1Unknown__Throttle-members.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Unknown__Throttle_1_1Unknown__Throttle-members.html deleted file mode 100644 index 0bf0990b..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Unknown__Throttle_1_1Unknown__Throttle-members.html +++ /dev/null @@ -1,133 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Descent.Unknown_Throttle.Unknown_Throttle Member List
-
-
- -

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Descent.Unknown_Throttle.Unknown_Throttle, including all inherited members.

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__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Descent.Unknown_Throttle.Unknown_Throttle
altitude_end (defined in SUAVE.Analyses.Mission.Segments.Descent.Unknown_Throttle.Unknown_Throttle)SUAVE.Analyses.Mission.Segments.Descent.Unknown_Throttle.Unknown_Throttle
altitude_start (defined in SUAVE.Analyses.Mission.Segments.Descent.Unknown_Throttle.Unknown_Throttle)SUAVE.Analyses.Mission.Segments.Descent.Unknown_Throttle.Unknown_Throttle
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Unknown__Throttle_1_1Unknown__Throttle.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Unknown__Throttle_1_1Unknown__Throttle.html deleted file mode 100644 index 1820e732..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Unknown__Throttle_1_1Unknown__Throttle.html +++ /dev/null @@ -1,250 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Mission.Segments.Descent.Unknown_Throttle.Unknown_Throttle Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Descent.Unknown_Throttle.Unknown_Throttle Class Reference
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-
-
-Inheritance diagram for SUAVE.Analyses.Mission.Segments.Descent.Unknown_Throttle.Unknown_Throttle:
-
-
- - -SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic -SUAVE.Analyses.Mission.Segments.Simple.Simple -SUAVE.Analyses.Mission.Segments.Segment.Segment -SUAVE.Analyses.Analysis.Analysis -SUAVE.Analyses.Mission.Segments.Descent.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate - -
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def evaluate (self, state=None)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

altitude_start
 
altitude_end
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
temperature_deviation
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
settings
 
state
 
analyses
 
process
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
This is not a usable segment for missions. Rather other descent segments that require throttle determination
-    are based off this segment type.
-
-    Assumptions:
-    None
-    
-    Source:
-    None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Mission.Segments.Descent.Unknown_Throttle.Unknown_Throttle.__defaults__ ( self)
-
-
This sets the default solver flow. Anything in here can be modified after initializing a segment.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Mission/Segments/Descent/Unknown_Throttle.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Unknown__Throttle_1_1Unknown__Throttle.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Unknown__Throttle_1_1Unknown__Throttle.js deleted file mode 100644 index 93209e5b..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Unknown__Throttle_1_1Unknown__Throttle.js +++ /dev/null @@ -1,6 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Unknown__Throttle_1_1Unknown__Throttle = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Unknown__Throttle_1_1Unknown__Throttle.html#ad3184a3e2dd7b80e19e34e9977878749", null ], - [ "altitude_end", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Unknown__Throttle_1_1Unknown__Throttle.html#a4fd0667c8d4690b702cf8936c158208d", null ], - [ "altitude_start", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Unknown__Throttle_1_1Unknown__Throttle.html#af2248d48041ebf36c2c16beacdf215a4", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Unknown__Throttle_1_1Unknown__Throttle.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Unknown__Throttle_1_1Unknown__Throttle.png deleted file mode 100644 index 50a6ab93..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Unknown__Throttle_1_1Unknown__Throttle.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Ground_1_1Ground-members.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Ground_1_1Ground-members.html deleted file mode 100644 index c575a8e2..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Ground_1_1Ground-members.html +++ /dev/null @@ -1,136 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground Member List
-
-
- -

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground, including all inherited members.

- - - - - - - - - - - - - - - - - - - - - - - - - -
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
friction_coefficient (defined in SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground)SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground
ground_incline (defined in SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground)SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
throttle (defined in SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground)SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground
velocity_end (defined in SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground)SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground
velocity_start (defined in SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground)SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Ground_1_1Ground.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Ground_1_1Ground.html deleted file mode 100644 index e78b8b46..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Ground_1_1Ground.html +++ /dev/null @@ -1,268 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground Class Reference
-
-
-
-Inheritance diagram for SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground:
-
-
- - -SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic -SUAVE.Analyses.Mission.Segments.Simple.Simple -SUAVE.Analyses.Mission.Segments.Segment.Segment -SUAVE.Analyses.Analysis.Analysis -SUAVE.Analyses.Mission.Segments.Ground.Landing.Landing -SUAVE.Analyses.Mission.Segments.Ground.Takeoff.Takeoff - -
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def evaluate (self, state=None)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

ground_incline
 
friction_coefficient
 
throttle
 
velocity_start
 
velocity_end
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
temperature_deviation
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
settings
 
state
 
analyses
 
process
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
Base segment for takeoff and landing segments. Integrates equations of motion
-    including rolling friction.
-    
-    Assumptions:
-    Notes Regarding Friction Coefficients
-    Dry asphalt or concrete: .04 brakes off, .4 brakes on
-    Wet asphalt or concrete: .05 brakes off, .225 brakes on
-    Icy asphalt or concrete: .02 brakes off, .08 brakes on
-    Hard turf:               .05 brakes off, .4 brakes on
-    Firm dirt:               .04 brakes off, .3 brakes on
-    Soft turf:               .07 brakes off, .2 brakes on
-    Wet grass:               .08 brakes off, .2 brakes on
-    
-    Source: General Aviation Aircraft Design: Applied Methods and Procedures,
-    by Snorri Gudmundsson, copyright 2014, published by Elsevier, Waltham,
-    MA, USA [p.938]
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground.__defaults__ ( self)
-
-
This sets the default solver flow. Anything in here can be modified after initializing a segment.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Mission/Segments/Ground/Ground.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Ground_1_1Ground.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Ground_1_1Ground.js deleted file mode 100644 index f51a2481..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Ground_1_1Ground.js +++ /dev/null @@ -1,9 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Ground_1_1Ground = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Ground_1_1Ground.html#a6f38f44f721bb677895014bf41e7f943", null ], - [ "friction_coefficient", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Ground_1_1Ground.html#ab464f078ee2c739e3752a9f8eb2d0138", null ], - [ "ground_incline", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Ground_1_1Ground.html#a6c8d24e8dff25fd1e76317107c787261", null ], - [ "throttle", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Ground_1_1Ground.html#ad700f1e66d0496426a5cf6a9f08fdfe8", null ], - [ "velocity_end", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Ground_1_1Ground.html#a0cdc0346e4d35f90948231559f21304a", null ], - [ "velocity_start", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Ground_1_1Ground.html#af92084c59eb4341c8aef909f32b33aa8", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Ground_1_1Ground.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Ground_1_1Ground.png deleted file mode 100644 index 7faec0ef..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Ground_1_1Ground.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Landing_1_1Landing-members.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Landing_1_1Landing-members.html deleted file mode 100644 index 5523160a..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Landing_1_1Landing-members.html +++ /dev/null @@ -1,136 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Ground.Landing.Landing Member List
-
-
- -

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Ground.Landing.Landing, including all inherited members.

- - - - - - - - - - - - - - - - - - - - - - - - - -
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Ground.Landing.Landing
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
friction_coefficient (defined in SUAVE.Analyses.Mission.Segments.Ground.Landing.Landing)SUAVE.Analyses.Mission.Segments.Ground.Landing.Landing
ground_incline (defined in SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground)SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
throttle (defined in SUAVE.Analyses.Mission.Segments.Ground.Landing.Landing)SUAVE.Analyses.Mission.Segments.Ground.Landing.Landing
velocity_end (defined in SUAVE.Analyses.Mission.Segments.Ground.Landing.Landing)SUAVE.Analyses.Mission.Segments.Ground.Landing.Landing
velocity_start (defined in SUAVE.Analyses.Mission.Segments.Ground.Landing.Landing)SUAVE.Analyses.Mission.Segments.Ground.Landing.Landing
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Landing_1_1Landing.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Landing_1_1Landing.html deleted file mode 100644 index 36ab4d3f..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Landing_1_1Landing.html +++ /dev/null @@ -1,283 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Mission.Segments.Ground.Landing.Landing Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Ground.Landing.Landing Class Reference
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-
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-Inheritance diagram for SUAVE.Analyses.Mission.Segments.Ground.Landing.Landing:
-
-
- - -SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground -SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic -SUAVE.Analyses.Mission.Segments.Simple.Simple -SUAVE.Analyses.Mission.Segments.Segment.Segment -SUAVE.Analyses.Analysis.Analysis - -
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def evaluate (self, state=None)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
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-Public Attributes

velocity_start
 
velocity_end
 
friction_coefficient
 
throttle
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground
ground_incline
 
friction_coefficient
 
throttle
 
velocity_start
 
velocity_end
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
temperature_deviation
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
settings
 
state
 
analyses
 
process
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
Segment for landing. Integrates equations of motion
-    including rolling friction.
-    
-    Assumptions:
-    Notes Regarding Friction Coefficients
-    Dry asphalt or concrete: .04 brakes off, .4 brakes on
-    Wet asphalt or concrete: .05 brakes off, .225 brakes on
-    Icy asphalt or concrete: .02 brakes off, .08 brakes on
-    Hard turf:               .05 brakes off, .4 brakes on
-    Firm dirt:               .04 brakes off, .3 brakes on
-    Soft turf:               .07 brakes off, .2 brakes on
-    Wet grass:               .08 brakes off, .2 brakes on
-    
-    Source: General Aviation Aircraft Design: Applied Methods and Procedures,
-    by Snorri Gudmundsson, copyright 2014, published by Elsevier, Waltham,
-    MA, USA [p.938]
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Mission.Segments.Ground.Landing.Landing.__defaults__ ( self)
-
-
This sets the default solver flow. Anything in here can be modified after initializing a segment.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Mission/Segments/Ground/Landing.py
  • -
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Landing_1_1Landing.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Landing_1_1Landing.js deleted file mode 100644 index aa294e63..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Landing_1_1Landing.js +++ /dev/null @@ -1,8 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Landing_1_1Landing = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Landing_1_1Landing.html#a72dcf1c5eb695dfb5496ab15b1fadf89", null ], - [ "friction_coefficient", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Landing_1_1Landing.html#aeb35b4252ace3965b9cf636f4dde25b1", null ], - [ "throttle", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Landing_1_1Landing.html#a588dfb3c26a66472501cabd36a8aaaec", null ], - [ "velocity_end", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Landing_1_1Landing.html#a7ffa35d28ce048a76380dfb48a9fb3b5", null ], - [ "velocity_start", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Landing_1_1Landing.html#a31af2911950e8226415dcfd098cc9649", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Landing_1_1Landing.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Landing_1_1Landing.png deleted file mode 100644 index 05197bd9..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Landing_1_1Landing.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Takeoff_1_1Takeoff-members.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Takeoff_1_1Takeoff-members.html deleted file mode 100644 index 76c41cdf..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Takeoff_1_1Takeoff-members.html +++ /dev/null @@ -1,136 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Ground.Takeoff.Takeoff Member List
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This is the complete list of members for SUAVE.Analyses.Mission.Segments.Ground.Takeoff.Takeoff, including all inherited members.

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__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Ground.Takeoff.Takeoff
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
friction_coefficient (defined in SUAVE.Analyses.Mission.Segments.Ground.Takeoff.Takeoff)SUAVE.Analyses.Mission.Segments.Ground.Takeoff.Takeoff
ground_incline (defined in SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground)SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
throttle (defined in SUAVE.Analyses.Mission.Segments.Ground.Takeoff.Takeoff)SUAVE.Analyses.Mission.Segments.Ground.Takeoff.Takeoff
velocity_end (defined in SUAVE.Analyses.Mission.Segments.Ground.Takeoff.Takeoff)SUAVE.Analyses.Mission.Segments.Ground.Takeoff.Takeoff
velocity_start (defined in SUAVE.Analyses.Mission.Segments.Ground.Takeoff.Takeoff)SUAVE.Analyses.Mission.Segments.Ground.Takeoff.Takeoff
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Takeoff_1_1Takeoff.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Takeoff_1_1Takeoff.html deleted file mode 100644 index c839436e..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Takeoff_1_1Takeoff.html +++ /dev/null @@ -1,283 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Mission.Segments.Ground.Takeoff.Takeoff Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Ground.Takeoff.Takeoff Class Reference
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-
-Inheritance diagram for SUAVE.Analyses.Mission.Segments.Ground.Takeoff.Takeoff:
-
-
- - -SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground -SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic -SUAVE.Analyses.Mission.Segments.Simple.Simple -SUAVE.Analyses.Mission.Segments.Segment.Segment -SUAVE.Analyses.Analysis.Analysis - -
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def evaluate (self, state=None)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

velocity_start
 
velocity_end
 
friction_coefficient
 
throttle
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground
ground_incline
 
friction_coefficient
 
throttle
 
velocity_start
 
velocity_end
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
temperature_deviation
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
settings
 
state
 
analyses
 
process
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
Segment for takeoff. Integrates equations of motion
-    including rolling friction.
-    
-    Assumptions:
-    Notes Regarding Friction Coefficients
-    Dry asphalt or concrete: .04 brakes off, .4 brakes on
-    Wet asphalt or concrete: .05 brakes off, .225 brakes on
-    Icy asphalt or concrete: .02 brakes off, .08 brakes on
-    Hard turf:               .05 brakes off, .4 brakes on
-    Firm dirt:               .04 brakes off, .3 brakes on
-    Soft turf:               .07 brakes off, .2 brakes on
-    Wet grass:               .08 brakes off, .2 brakes on
-    
-    Source: General Aviation Aircraft Design: Applied Methods and Procedures,
-    by Snorri Gudmundsson, copyright 2014, published by Elsevier, Waltham,
-    MA, USA [p.938]
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Mission.Segments.Ground.Takeoff.Takeoff.__defaults__ ( self)
-
-
This sets the default solver flow. Anything in here can be modified after initializing a segment.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Mission/Segments/Ground/Takeoff.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Takeoff_1_1Takeoff.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Takeoff_1_1Takeoff.js deleted file mode 100644 index e5f8cb00..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Takeoff_1_1Takeoff.js +++ /dev/null @@ -1,8 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Takeoff_1_1Takeoff = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Takeoff_1_1Takeoff.html#ae81502ad7f17cf737e304adbd9195140", null ], - [ "friction_coefficient", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Takeoff_1_1Takeoff.html#a9b960ebffa99dc7aa77c0a4e3cde453c", null ], - [ "throttle", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Takeoff_1_1Takeoff.html#a9c715fcf97335e66e47382d416f2cab0", null ], - [ "velocity_end", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Takeoff_1_1Takeoff.html#abb5a7876221072baa4f2ed7bcbdeaa69", null ], - [ "velocity_start", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Takeoff_1_1Takeoff.html#abe0789c18abb310302ff523386487cc5", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Takeoff_1_1Takeoff.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Takeoff_1_1Takeoff.png deleted file mode 100644 index 88101459..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Takeoff_1_1Takeoff.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Climb_1_1Climb-members.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Climb_1_1Climb-members.html deleted file mode 100644 index 9ca27f18..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Climb_1_1Climb-members.html +++ /dev/null @@ -1,136 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Hover.Climb.Climb Member List
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This is the complete list of members for SUAVE.Analyses.Mission.Segments.Hover.Climb.Climb, including all inherited members.

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__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Hover.Climb.Climb
altitude (defined in SUAVE.Analyses.Mission.Segments.Hover.Hover.Hover)SUAVE.Analyses.Mission.Segments.Hover.Hover.Hover
altitude_end (defined in SUAVE.Analyses.Mission.Segments.Hover.Climb.Climb)SUAVE.Analyses.Mission.Segments.Hover.Climb.Climb
altitude_start (defined in SUAVE.Analyses.Mission.Segments.Hover.Climb.Climb)SUAVE.Analyses.Mission.Segments.Hover.Climb.Climb
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
climb_rate (defined in SUAVE.Analyses.Mission.Segments.Hover.Climb.Climb)SUAVE.Analyses.Mission.Segments.Hover.Climb.Climb
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
time (defined in SUAVE.Analyses.Mission.Segments.Hover.Hover.Hover)SUAVE.Analyses.Mission.Segments.Hover.Hover.Hover
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Climb_1_1Climb.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Climb_1_1Climb.html deleted file mode 100644 index 4dbad855..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Climb_1_1Climb.html +++ /dev/null @@ -1,262 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Mission.Segments.Hover.Climb.Climb Class Reference - - - - - - - - - - - - - - - -
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- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Hover.Climb.Climb Class Reference
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-
-
-Inheritance diagram for SUAVE.Analyses.Mission.Segments.Hover.Climb.Climb:
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-
- - -SUAVE.Analyses.Mission.Segments.Hover.Hover.Hover -SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic -SUAVE.Analyses.Mission.Segments.Simple.Simple -SUAVE.Analyses.Mission.Segments.Segment.Segment -SUAVE.Analyses.Analysis.Analysis - -
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Hover.Hover.Hover
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def evaluate (self, state=None)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

altitude_start
 
altitude_end
 
climb_rate
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Hover.Hover.Hover
altitude
 
time
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
temperature_deviation
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
settings
 
state
 
analyses
 
process
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
A vertically climbing hover for VTOL aircraft. Although the vehicle moves, no aerodynamic drag and lift are used.
-
-    Assumptions:
-    Your vehicle creates a negligible drag and lift force during a vertical climb.
-    
-    Source:
-    None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Mission.Segments.Hover.Climb.Climb.__defaults__ ( self)
-
-
This sets the default solver flow. Anything in here can be modified after initializing a segment.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Mission/Segments/Hover/Climb.py
  • -
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Climb_1_1Climb.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Climb_1_1Climb.js deleted file mode 100644 index 0f896950..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Climb_1_1Climb.js +++ /dev/null @@ -1,7 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Climb_1_1Climb = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Climb_1_1Climb.html#a233064e0afad5ed01ac48ae3b48bbadd", null ], - [ "altitude_end", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Climb_1_1Climb.html#a955d04a352b94d270e55212d079de955", null ], - [ "altitude_start", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Climb_1_1Climb.html#a927c7c629a6350300bd748d1f5715a63", null ], - [ "climb_rate", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Climb_1_1Climb.html#a6153d33484e9e525785f64cab8bfaece", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Climb_1_1Climb.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Climb_1_1Climb.png deleted file mode 100644 index 8c46445c..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Climb_1_1Climb.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Descent_1_1Descent-members.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Descent_1_1Descent-members.html deleted file mode 100644 index f76ec7c7..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Descent_1_1Descent-members.html +++ /dev/null @@ -1,136 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Hover.Descent.Descent Member List
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This is the complete list of members for SUAVE.Analyses.Mission.Segments.Hover.Descent.Descent, including all inherited members.

- - - - - - - - - - - - - - - - - - - - - - - - - -
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Hover.Descent.Descent
altitude (defined in SUAVE.Analyses.Mission.Segments.Hover.Hover.Hover)SUAVE.Analyses.Mission.Segments.Hover.Hover.Hover
altitude_end (defined in SUAVE.Analyses.Mission.Segments.Hover.Descent.Descent)SUAVE.Analyses.Mission.Segments.Hover.Descent.Descent
altitude_start (defined in SUAVE.Analyses.Mission.Segments.Hover.Descent.Descent)SUAVE.Analyses.Mission.Segments.Hover.Descent.Descent
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
descent_rate (defined in SUAVE.Analyses.Mission.Segments.Hover.Descent.Descent)SUAVE.Analyses.Mission.Segments.Hover.Descent.Descent
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
time (defined in SUAVE.Analyses.Mission.Segments.Hover.Hover.Hover)SUAVE.Analyses.Mission.Segments.Hover.Hover.Hover
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Descent_1_1Descent.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Descent_1_1Descent.html deleted file mode 100644 index e19aab79..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Descent_1_1Descent.html +++ /dev/null @@ -1,262 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Mission.Segments.Hover.Descent.Descent Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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- -
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- -
- -
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-
SUAVE.Analyses.Mission.Segments.Hover.Descent.Descent Class Reference
-
-
-
-Inheritance diagram for SUAVE.Analyses.Mission.Segments.Hover.Descent.Descent:
-
-
- - -SUAVE.Analyses.Mission.Segments.Hover.Hover.Hover -SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic -SUAVE.Analyses.Mission.Segments.Simple.Simple -SUAVE.Analyses.Mission.Segments.Segment.Segment -SUAVE.Analyses.Analysis.Analysis - -
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-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Hover.Hover.Hover
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def evaluate (self, state=None)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

altitude_start
 
altitude_end
 
descent_rate
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Hover.Hover.Hover
altitude
 
time
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
temperature_deviation
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
settings
 
state
 
analyses
 
process
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
A vertically descending hover for VTOL aircraft. Although the vehicle moves, no aerodynamic drag and lift are used.
-
-    Assumptions:
-    Your vehicle creates a negligible drag and lift force during a vertical descent.
-    
-    Source:
-    None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Mission.Segments.Hover.Descent.Descent.__defaults__ ( self)
-
-
This sets the default solver flow. Anything in here can be modified after initializing a segment.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Mission/Segments/Hover/Descent.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Descent_1_1Descent.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Descent_1_1Descent.js deleted file mode 100644 index e5c18e65..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Descent_1_1Descent.js +++ /dev/null @@ -1,7 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Descent_1_1Descent = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Descent_1_1Descent.html#aa0c504cca16b88e4441f11853b8d9a26", null ], - [ "altitude_end", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Descent_1_1Descent.html#a1ff421c11066e8f449d486678644b34d", null ], - [ "altitude_start", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Descent_1_1Descent.html#a182d95a39be2ec5e4079cfeb99d3804e", null ], - [ "descent_rate", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Descent_1_1Descent.html#a891ceac6c0178b9090ea3ef750af9a98", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Descent_1_1Descent.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Descent_1_1Descent.png deleted file mode 100644 index 9245b668..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Descent_1_1Descent.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Hover_1_1Hover-members.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Hover_1_1Hover-members.html deleted file mode 100644 index d9be2b40..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Hover_1_1Hover-members.html +++ /dev/null @@ -1,133 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Hover.Hover.Hover Member List
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-
- -

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Hover.Hover.Hover, including all inherited members.

- - - - - - - - - - - - - - - - - - - - - - -
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Hover.Hover.Hover
altitude (defined in SUAVE.Analyses.Mission.Segments.Hover.Hover.Hover)SUAVE.Analyses.Mission.Segments.Hover.Hover.Hover
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
time (defined in SUAVE.Analyses.Mission.Segments.Hover.Hover.Hover)SUAVE.Analyses.Mission.Segments.Hover.Hover.Hover
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Hover_1_1Hover.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Hover_1_1Hover.html deleted file mode 100644 index 56af1854..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Hover_1_1Hover.html +++ /dev/null @@ -1,250 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Mission.Segments.Hover.Hover.Hover Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Hover.Hover.Hover Class Reference
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-
-
-Inheritance diagram for SUAVE.Analyses.Mission.Segments.Hover.Hover.Hover:
-
-
- - -SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic -SUAVE.Analyses.Mission.Segments.Simple.Simple -SUAVE.Analyses.Mission.Segments.Segment.Segment -SUAVE.Analyses.Analysis.Analysis -SUAVE.Analyses.Mission.Segments.Hover.Climb.Climb -SUAVE.Analyses.Mission.Segments.Hover.Descent.Descent - -
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def evaluate (self, state=None)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

altitude
 
time
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
temperature_deviation
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
settings
 
state
 
analyses
 
process
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
A stationary hover for VTOL aircraft. No aerodynamic drag and lift are used, since there is no velocity.
-
-    Assumptions:
-    None
-    
-    Source:
-    None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Mission.Segments.Hover.Hover.Hover.__defaults__ ( self)
-
-
This sets the default solver flow. Anything in here can be modified after initializing a segment.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Mission/Segments/Hover/Hover.py
  • -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Segment.Container Member List
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This is the complete list of members for SUAVE.Analyses.Mission.Segments.Segment.Container, including all inherited members.

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__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Segment.Container
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
append_segment(self, segment)SUAVE.Analyses.Mission.Segments.Segment.Container
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
segments (defined in SUAVE.Analyses.Mission.Segments.Segment.Container)SUAVE.Analyses.Mission.Segments.Segment.Container
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Container)SUAVE.Analyses.Mission.Segments.Segment.Container
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Container.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Container.html deleted file mode 100644 index 2e310233..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Container.html +++ /dev/null @@ -1,287 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Mission.Segments.Segment.Container Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Segment.Container Class Reference
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-Inheritance diagram for SUAVE.Analyses.Mission.Segments.Segment.Container:
-
-
- - -SUAVE.Analyses.Mission.Segments.Segment.Segment -SUAVE.Analyses.Analysis.Analysis -SUAVE.Analyses.Mission.Segments.Simple.Container -SUAVE.Analyses.Mission.Mission.Mission -SUAVE.Analyses.Mission.All_At_Once.All_At_Once -SUAVE.Analyses.Mission.Sequential_Segments.Sequential_Segments -SUAVE.Analyses.Mission.Vary_Cruise.Given_Weight.Given_Weight - -
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-Public Member Functions

def __defaults__ (self)
 
def append_segment (self, segment)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def evaluate (self, state=None)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

segments
 
state
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
settings
 
state
 
analyses
 
process
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
A container for the segment
-
-    Assumptions:
-    None
-    
-    Source:
-    None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Mission.Segments.Segment.Container.__defaults__ ( self)
-
-
This sets the default values.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
- -

◆ append_segment()

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-
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def SUAVE.Analyses.Mission.Segments.Segment.Container.append_segment ( self,
 segment 
)
-
-
Add a SubSegment
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    segment  [Segment()]
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Mission/Segments/Segment.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Container.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Container.js deleted file mode 100644 index e1f4dcc7..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Container.js +++ /dev/null @@ -1,7 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Container = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Container.html#a8873a89d3547fadf4abff2af3203a11b", null ], - [ "append_segment", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Container.html#a6005045d015d9fb626ad31f43dd008d8", null ], - [ "segments", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Container.html#a8358c522f4af250442bd1a0310821c8d", null ], - [ "state", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Container.html#ad5a498c3112171b69f5eecdaa59af854", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Container.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Container.png deleted file mode 100644 index ea7d6cdb..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Container.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Segment-members.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Segment-members.html deleted file mode 100644 index b757e94d..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Segment-members.html +++ /dev/null @@ -1,130 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Segment.Segment Member List
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This is the complete list of members for SUAVE.Analyses.Mission.Segments.Segment.Segment, including all inherited members.

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__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Segment.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Segment.html deleted file mode 100644 index e5ca0a54..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Segment.html +++ /dev/null @@ -1,497 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Mission.Segments.Segment.Segment Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Segment.Segment Class Reference
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-Inheritance diagram for SUAVE.Analyses.Mission.Segments.Segment.Segment:
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- - -SUAVE.Analyses.Analysis.Analysis -SUAVE.Analyses.Mission.Segments.Segment.Container -SUAVE.Analyses.Mission.Segments.Simple.Simple -SUAVE.Analyses.Mission.Segments.Simple.Container -SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic -SUAVE.Analyses.Mission.Mission.Mission -SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Linear_Altitude.Constant_Speed_Linear_Altitude -SUAVE.Analyses.Mission.Segments.Climb.Constant_Throttle_Constant_Speed.Constant_Throttle_Constant_Speed -SUAVE.Analyses.Mission.Segments.Climb.Optimized.Optimized -SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle -SUAVE.Analyses.Mission.Segments.Cruise.Constant_Acceleration_Constant_Altitude.Constant_Acceleration_Constant_Altitude -SUAVE.Analyses.Mission.Segments.Cruise.Constant_Pitch_Rate_Constant_Altitude.Constant_Pitch_Rate_Constant_Altitude -SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude -SUAVE.Analyses.Mission.Segments.Cruise.Constant_Throttle_Constant_Altitude.Constant_Throttle_Constant_Altitude -SUAVE.Analyses.Mission.Segments.Descent.Unknown_Throttle.Unknown_Throttle -SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground -SUAVE.Analyses.Mission.Segments.Hover.Hover.Hover -SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude.Set_Speed_Set_Altitude -SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Throttle.Set_Speed_Set_Throttle - -
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-Public Member Functions

def __defaults__ (self)
 
def initialize (self, state)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def evaluate (self, state=None)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - - - -

-Public Attributes

settings
 
state
 
analyses
 
process
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
The first basic piece of a mission which each segment will expand upon
-
-    Assumptions:
-    There's a detailed process flow outline in defaults. A mission must be solved in that order.
-    
-    Source:
-    None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Mission.Segments.Segment.Segment.__defaults__ ( self)
-
-
This sets the default values.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
- -

◆ compile()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Mission.Segments.Segment.Segment.compile ( self)
-
-
This does nothing
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    State  [Data()]
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
- -

◆ converge()

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-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Analyses.Mission.Segments.Segment.Segment.converge ( self,
 state 
)
-
-
This executes the converge process
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    State  [Data()]
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
- -

◆ evaluate()

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-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Analyses.Mission.Segments.Segment.Segment.evaluate ( self,
 state = None 
)
-
-
This executes the entire process
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    State  [Data()]
-    
-    Outputs:
-    State  [Data()]
-    
-    Properties Used:
-    None
-
-
-
- -

◆ finalize()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Analyses.Mission.Segments.Segment.Segment.finalize ( self,
 state 
)
-
-
This executes the finalize process
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    State  [Data()]
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
- -

◆ initialize()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Analyses.Mission.Segments.Segment.Segment.initialize ( self,
 state 
)
-
-
This executes the initialize process
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    State  [Data()]
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
- -

◆ iterate()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Analyses.Mission.Segments.Segment.Segment.iterate ( self,
 state 
)
-
-
This executes the iterate process
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    State  [Data()]
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Mission/Segments/Segment.py
  • -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Simple.Container Member List
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This is the complete list of members for SUAVE.Analyses.Mission.Segments.Simple.Container, including all inherited members.

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__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Simple.Container
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
append_segment(self, segment)SUAVE.Analyses.Mission.Segments.Segment.Container
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
segments (defined in SUAVE.Analyses.Mission.Segments.Segment.Container)SUAVE.Analyses.Mission.Segments.Segment.Container
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Container)SUAVE.Analyses.Mission.Segments.Segment.Container
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Simple_1_1Container.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Simple_1_1Container.html deleted file mode 100644 index 0f2716d0..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Simple_1_1Container.html +++ /dev/null @@ -1,246 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Mission.Segments.Simple.Container Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Simple.Container Class Reference
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-Inheritance diagram for SUAVE.Analyses.Mission.Segments.Simple.Container:
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- - -SUAVE.Analyses.Mission.Segments.Segment.Container -SUAVE.Analyses.Mission.Segments.Segment.Segment -SUAVE.Analyses.Analysis.Analysis -SUAVE.Analyses.Mission.Mission.Mission -SUAVE.Analyses.Mission.All_At_Once.All_At_Once -SUAVE.Analyses.Mission.Sequential_Segments.Sequential_Segments -SUAVE.Analyses.Mission.Vary_Cruise.Given_Weight.Given_Weight - -
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-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Container
def __defaults__ (self)
 
def append_segment (self, segment)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def evaluate (self, state=None)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - - - - - - - - - -

-Additional Inherited Members

- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Segment.Container
segments
 
state
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
settings
 
state
 
analyses
 
process
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
A container for the segment
-
-    Assumptions:
-    None
-    
-    Source:
-    None
-

Member Function Documentation

- -

◆ __defaults__()

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def SUAVE.Analyses.Mission.Segments.Simple.Container.__defaults__ ( self)
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This sets the default values.
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-    Assumptions:
-    None
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-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
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-
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The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Mission/Segments/Simple.py
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Simple_1_1Container.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Simple_1_1Container.js deleted file mode 100644 index f14bae85..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Simple_1_1Container.js +++ /dev/null @@ -1,4 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Simple_1_1Container = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Simple_1_1Container.html#a2df84b54616783b4e06053ca36038620", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Simple_1_1Container.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Simple_1_1Container.png deleted file mode 100644 index 2a540e6d..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Simple_1_1Container.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Simple_1_1Simple-members.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Simple_1_1Simple-members.html deleted file mode 100644 index 07ef0e53..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Simple_1_1Simple-members.html +++ /dev/null @@ -1,130 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Simple.Simple Member List
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This is the complete list of members for SUAVE.Analyses.Mission.Segments.Simple.Simple, including all inherited members.

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__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Simple.Simple
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Simple_1_1Simple.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Simple_1_1Simple.html deleted file mode 100644 index 44fba75d..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Simple_1_1Simple.html +++ /dev/null @@ -1,243 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Mission.Segments.Simple.Simple Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Simple.Simple Class Reference
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-Inheritance diagram for SUAVE.Analyses.Mission.Segments.Simple.Simple:
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- - -SUAVE.Analyses.Mission.Segments.Segment.Segment -SUAVE.Analyses.Analysis.Analysis -SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic -SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Linear_Altitude.Constant_Speed_Linear_Altitude -SUAVE.Analyses.Mission.Segments.Climb.Constant_Throttle_Constant_Speed.Constant_Throttle_Constant_Speed -SUAVE.Analyses.Mission.Segments.Climb.Optimized.Optimized -SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle -SUAVE.Analyses.Mission.Segments.Cruise.Constant_Acceleration_Constant_Altitude.Constant_Acceleration_Constant_Altitude -SUAVE.Analyses.Mission.Segments.Cruise.Constant_Pitch_Rate_Constant_Altitude.Constant_Pitch_Rate_Constant_Altitude -SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude -SUAVE.Analyses.Mission.Segments.Cruise.Constant_Throttle_Constant_Altitude.Constant_Throttle_Constant_Altitude -SUAVE.Analyses.Mission.Segments.Descent.Unknown_Throttle.Unknown_Throttle -SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground -SUAVE.Analyses.Mission.Segments.Hover.Hover.Hover -SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude.Set_Speed_Set_Altitude -SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Throttle.Set_Speed_Set_Throttle - -
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-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def evaluate (self, state=None)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - - - - -

-Additional Inherited Members

- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
settings
 
state
 
analyses
 
process
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
The Second basic piece of a mission which each segment will expand upon
-
-    Assumptions:
-    There's a detailed process flow outline in defaults. A mission must be solved in that order.
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-    Source:
-    None
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Member Function Documentation

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◆ __defaults__()

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- - - - - - - - -
def SUAVE.Analyses.Mission.Segments.Simple.Simple.__defaults__ ( self)
-
-
This sets the default values.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Mission/Segments/Simple.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Simple_1_1Simple.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Simple_1_1Simple.js deleted file mode 100644 index 642c2912..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Simple_1_1Simple.js +++ /dev/null @@ -1,4 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Simple_1_1Simple = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Simple_1_1Simple.html#a80e4962f423662c0f31df02278deab7e", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Simple_1_1Simple.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Simple_1_1Simple.png deleted file mode 100644 index 9eec3c93..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Simple_1_1Simple.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Altitude_1_1Seae0052171c39704a97e8acae6ffdafb.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Altitude_1_1Seae0052171c39704a97e8acae6ffdafb.html deleted file mode 100644 index a5c50535..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Altitude_1_1Seae0052171c39704a97e8acae6ffdafb.html +++ /dev/null @@ -1,136 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude.Set_Speed_Set_Altitude Member List
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This is the complete list of members for SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude.Set_Speed_Set_Altitude, including all inherited members.

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__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude.Set_Speed_Set_Altitude
air_speed (defined in SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude.Set_Speed_Set_Altitude)SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude.Set_Speed_Set_Altitude
altitude (defined in SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude.Set_Speed_Set_Altitude)SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude.Set_Speed_Set_Altitude
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
distance (defined in SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude.Set_Speed_Set_Altitude)SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude.Set_Speed_Set_Altitude
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
x_accel (defined in SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude.Set_Speed_Set_Altitude)SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude.Set_Speed_Set_Altitude
z_accel (defined in SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude.Set_Speed_Set_Altitude)SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude.Set_Speed_Set_Altitude
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Altitude_1_1Set__Speed__Set__Altitude.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Altitude_1_1Set__Speed__Set__Altitude.html deleted file mode 100644 index a39681d7..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Altitude_1_1Set__Speed__Set__Altitude.html +++ /dev/null @@ -1,258 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude.Set_Speed_Set_Altitude Class Reference - - - - - - - - - - - - - - - -
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SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude.Set_Speed_Set_Altitude Class Reference
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-
-
-Inheritance diagram for SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude.Set_Speed_Set_Altitude:
-
-
- - -SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic -SUAVE.Analyses.Mission.Segments.Simple.Simple -SUAVE.Analyses.Mission.Segments.Segment.Segment -SUAVE.Analyses.Analysis.Analysis - -
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def evaluate (self, state=None)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

altitude
 
air_speed
 
distance
 
x_accel
 
z_accel
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
temperature_deviation
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
settings
 
state
 
analyses
 
process
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
This is a segment that is solved using a single point. A snapshot in time.
-    We fix the speed and altitude. Throttle is solved from those.
-
-    Assumptions:
-    None
-    
-    Source:
-    None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude.Set_Speed_Set_Altitude.__defaults__ ( self)
-
-
This sets the default solver flow. Anything in here can be modified after initializing a segment.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Mission/Segments/Single_Point/Set_Speed_Set_Altitude.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Altitude_1_1Set__Speed__Set__Altitude.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Altitude_1_1Set__Speed__Set__Altitude.js deleted file mode 100644 index cff49993..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Altitude_1_1Set__Speed__Set__Altitude.js +++ /dev/null @@ -1,9 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Altitude_1_1Set__Speed__Set__Altitude = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Altitude_1_1Set__Speed__Set__Altitude.html#ab30e5a1bd6bb2fab6bf0506e344c8b07", null ], - [ "air_speed", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Altitude_1_1Set__Speed__Set__Altitude.html#a1bb43df9ce81ed7841ec792b7e900053", null ], - [ "altitude", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Altitude_1_1Set__Speed__Set__Altitude.html#ad51ead850dada3514c0c7c82dc95e00f", null ], - [ "distance", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Altitude_1_1Set__Speed__Set__Altitude.html#a1b477ee88203e74ab8399196ba3e4758", null ], - [ "x_accel", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Altitude_1_1Set__Speed__Set__Altitude.html#a56b1e1aff3d78e49f323c92bdc11b1d0", null ], - [ "z_accel", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Altitude_1_1Set__Speed__Set__Altitude.html#a2739c0df766a5d1fbf576ab1484ca9e8", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Altitude_1_1Set__Speed__Set__Altitude.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Altitude_1_1Set__Speed__Set__Altitude.png deleted file mode 100644 index 6723a222..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Altitude_1_1Set__Speed__Set__Altitude.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Throttle_1_1S9161113e971a925856bf4082306f653a.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Throttle_1_1S9161113e971a925856bf4082306f653a.html deleted file mode 100644 index e2108190..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Throttle_1_1S9161113e971a925856bf4082306f653a.html +++ /dev/null @@ -1,135 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Throttle.Set_Speed_Set_Throttle Member List
-
-
- -

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Throttle.Set_Speed_Set_Throttle, including all inherited members.

- - - - - - - - - - - - - - - - - - - - - - - - -
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Throttle.Set_Speed_Set_Throttle
air_speed (defined in SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Throttle.Set_Speed_Set_Throttle)SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Throttle.Set_Speed_Set_Throttle
altitude (defined in SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Throttle.Set_Speed_Set_Throttle)SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Throttle.Set_Speed_Set_Throttle
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
throttle (defined in SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Throttle.Set_Speed_Set_Throttle)SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Throttle.Set_Speed_Set_Throttle
z_accel (defined in SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Throttle.Set_Speed_Set_Throttle)SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Throttle.Set_Speed_Set_Throttle
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Throttle_1_1Set__Speed__Set__Throttle.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Throttle_1_1Set__Speed__Set__Throttle.html deleted file mode 100644 index 8f89194e..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Throttle_1_1Set__Speed__Set__Throttle.html +++ /dev/null @@ -1,255 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Throttle.Set_Speed_Set_Throttle Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Throttle.Set_Speed_Set_Throttle Class Reference
-
-
-
-Inheritance diagram for SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Throttle.Set_Speed_Set_Throttle:
-
-
- - -SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic -SUAVE.Analyses.Mission.Segments.Simple.Simple -SUAVE.Analyses.Mission.Segments.Segment.Segment -SUAVE.Analyses.Analysis.Analysis - -
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def evaluate (self, state=None)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

altitude
 
air_speed
 
throttle
 
z_accel
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
temperature_deviation
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
settings
 
state
 
analyses
 
process
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
This is a segment that is solved using a single point. A snapshot in time.
-    We fix the speed and throttle. Acceleration is solved from those.
-
-    Assumptions:
-    None
-    
-    Source:
-    None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Throttle.Set_Speed_Set_Throttle.__defaults__ ( self)
-
-
This sets the default solver flow. Anything in here can be modified after initializing a segment.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Mission/Segments/Single_Point/Set_Speed_Set_Throttle.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Throttle_1_1Set__Speed__Set__Throttle.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Throttle_1_1Set__Speed__Set__Throttle.js deleted file mode 100644 index 4af95317..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Throttle_1_1Set__Speed__Set__Throttle.js +++ /dev/null @@ -1,8 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Throttle_1_1Set__Speed__Set__Throttle = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Throttle_1_1Set__Speed__Set__Throttle.html#a1d031a6b1908cc3dda51144295d6e419", null ], - [ "air_speed", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Throttle_1_1Set__Speed__Set__Throttle.html#abb7625cbc9cc662f2c76868f26cb0690", null ], - [ "altitude", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Throttle_1_1Set__Speed__Set__Throttle.html#ab749fb4dab5849cfe9a0846888dbc67d", null ], - [ "throttle", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Throttle_1_1Set__Speed__Set__Throttle.html#a42901c599bdb4ae4161766298e847034", null ], - [ "z_accel", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Throttle_1_1Set__Speed__Set__Throttle.html#ab65bcf48c8e0056d4a91b62f3e77bc29", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Throttle_1_1Set__Speed__Set__Throttle.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Throttle_1_1Set__Speed__Set__Throttle.png deleted file mode 100644 index bca2b872..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Throttle_1_1Set__Speed__Set__Throttle.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Sequential__Segments_1_1Container-members.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Sequential__Segments_1_1Container-members.html deleted file mode 100644 index d96a1e77..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Sequential__Segments_1_1Container-members.html +++ /dev/null @@ -1,114 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Sequential_Segments.Container Member List
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Sequential__Segments_1_1Container.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Sequential__Segments_1_1Container.html deleted file mode 100644 index b5e294ba..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Sequential__Segments_1_1Container.html +++ /dev/null @@ -1,218 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Mission.Sequential_Segments.Container Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Sequential_Segments.Container Class Reference
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-Inheritance diagram for SUAVE.Analyses.Mission.Sequential_Segments.Container:
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-Public Member Functions

def evaluate (self, state=None)
 
def finalize (self)
 
-

Detailed Description

-
Container for mission
-
-    Assumptions:
-    None
-    
-    Source:
-    None
-

Member Function Documentation

- -

◆ evaluate()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Analyses.Mission.Sequential_Segments.Container.evaluate ( self,
 state = None 
)
-
-
Go through the missions, run through them, save the results
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    state   [Data()]
-    
-    Outputs:
-    Results [Results()]
-    
-    Properties Used:
-    None
-
-
-
- -

◆ finalize()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Mission.Sequential_Segments.Container.finalize ( self)
-
-
Stub
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Mission/Sequential_Segments.py
  • -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Sequential_Segments.Sequential_Segments Member List
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This is the complete list of members for SUAVE.Analyses.Mission.Sequential_Segments.Sequential_Segments, including all inherited members.

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__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Sequential_Segments.Sequential_Segments
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
append_segment(self, segment)SUAVE.Analyses.Mission.Segments.Segment.Container
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self)SUAVE.Analyses.Mission.Sequential_Segments.Sequential_Segments
SUAVE::Analyses::Mission::Segments::Simple::Container.finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
segments (defined in SUAVE.Analyses.Mission.Segments.Segment.Container)SUAVE.Analyses.Mission.Segments.Segment.Container
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Container)SUAVE.Analyses.Mission.Segments.Segment.Container
tag (defined in SUAVE.Analyses.Mission.Sequential_Segments.Sequential_Segments)SUAVE.Analyses.Mission.Sequential_Segments.Sequential_Segments
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Sequential__Segments_1_1Sequential__Segments.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Sequential__Segments_1_1Sequential__Segments.html deleted file mode 100644 index b01999c5..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Sequential__Segments_1_1Sequential__Segments.html +++ /dev/null @@ -1,296 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Mission.Sequential_Segments.Sequential_Segments Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Sequential_Segments.Sequential_Segments Class Reference
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-Inheritance diagram for SUAVE.Analyses.Mission.Sequential_Segments.Sequential_Segments:
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- - -SUAVE.Analyses.Mission.Mission.Mission -SUAVE.Analyses.Mission.Segments.Simple.Container -SUAVE.Analyses.Mission.Segments.Segment.Container -SUAVE.Analyses.Mission.Segments.Segment.Segment -SUAVE.Analyses.Analysis.Analysis - -
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-Public Member Functions

def __defaults__ (self)
 
def finalize (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Mission.Mission
def __defaults__ (self)
 
def finalize (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Container
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Container
def __defaults__ (self)
 
def append_segment (self, segment)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def evaluate (self, state=None)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

tag
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Mission.Mission
tag
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Segment.Container
segments
 
state
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
settings
 
state
 
analyses
 
process
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
Solves each segment one at time
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-    Assumptions:
-    None
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-    Source:
-    None
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Member Function Documentation

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◆ __defaults__()

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def SUAVE.Analyses.Mission.Sequential_Segments.Sequential_Segments.__defaults__ ( self)
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This sets the default values.
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◆ finalize()

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def SUAVE.Analyses.Mission.Sequential_Segments.Sequential_Segments.finalize ( self)
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Stub
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-    Properties Used:
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The documentation for this class was generated from the following file:
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  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Mission/Sequential_Segments.py
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Vary_Cruise.Given_Weight.Given_Weight Member List
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This is the complete list of members for SUAVE.Analyses.Mission.Vary_Cruise.Given_Weight.Given_Weight, including all inherited members.

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__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Vary_Cruise.Given_Weight.Given_Weight
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
append_segment(self, segment)SUAVE.Analyses.Mission.Segments.Segment.Container
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
cruise_tag (defined in SUAVE.Analyses.Mission.Vary_Cruise.Given_Weight.Given_Weight)SUAVE.Analyses.Mission.Vary_Cruise.Given_Weight.Given_Weight
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self)SUAVE.Analyses.Mission.All_At_Once.All_At_Once
SUAVE::Analyses::Mission::Segments::Simple::Container.finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
segments (defined in SUAVE.Analyses.Mission.Segments.Segment.Container)SUAVE.Analyses.Mission.Segments.Segment.Container
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Container)SUAVE.Analyses.Mission.Segments.Segment.Container
tag (defined in SUAVE.Analyses.Mission.Vary_Cruise.Given_Weight.Given_Weight)SUAVE.Analyses.Mission.Vary_Cruise.Given_Weight.Given_Weight
target_landing_weight (defined in SUAVE.Analyses.Mission.Vary_Cruise.Given_Weight.Given_Weight)SUAVE.Analyses.Mission.Vary_Cruise.Given_Weight.Given_Weight
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Mission.Vary_Cruise.Given_Weight.Given_Weight Class Reference
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-Inheritance diagram for SUAVE.Analyses.Mission.Vary_Cruise.Given_Weight.Given_Weight:
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-
- - -SUAVE.Analyses.Mission.All_At_Once.All_At_Once -SUAVE.Analyses.Mission.Mission.Mission -SUAVE.Analyses.Mission.Segments.Simple.Container -SUAVE.Analyses.Mission.Segments.Segment.Container -SUAVE.Analyses.Mission.Segments.Segment.Segment -SUAVE.Analyses.Analysis.Analysis - -
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-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.All_At_Once.All_At_Once
def __defaults__ (self)
 
def finalize (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Mission.Mission
def __defaults__ (self)
 
def finalize (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Container
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Container
def __defaults__ (self)
 
def append_segment (self, segment)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def evaluate (self, state=None)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

tag
 
cruise_tag
 
target_landing_weight
 
- Public Attributes inherited from SUAVE.Analyses.Mission.All_At_Once.All_At_Once
tag
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Mission.Mission
tag
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Segment.Container
segments
 
state
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
settings
 
state
 
analyses
 
process
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
Given a target landing weight, select the cruise distance by adding a residual to the mission
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-    Assumptions:
-    None
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-    Source:
-    None
-

Member Function Documentation

- -

◆ __defaults__()

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def SUAVE.Analyses.Mission.Vary_Cruise.Given_Weight.Given_Weight.__defaults__ ( self)
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This sets the default flow of methods for the mission.
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-    Assumptions:
-    None
-    
-    Source:
-    N/A
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-    Inputs:
-    None
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-    Outputs:
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-    Properties Used:
-    None
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The documentation for this class was generated from the following file:
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  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Mission/Vary_Cruise/Given_Weight.py
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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- - - - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Noise_1_1Fidelity__One_1_1Fidelity__One.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Noise_1_1Fidelity__One_1_1Fidelity__One.html deleted file mode 100644 index 46dd55ce..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Noise_1_1Fidelity__One_1_1Fidelity__One.html +++ /dev/null @@ -1,224 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Noise.Fidelity_One.Fidelity_One Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Noise.Fidelity_One.Fidelity_One Class Reference
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-Inheritance diagram for SUAVE.Analyses.Noise.Fidelity_One.Fidelity_One:
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-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Noise.Noise.Noise
def __defaults__ (self)
 
def evaluate (self, state)
 
def finalize (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
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-Public Attributes

tag
 
- Public Attributes inherited from SUAVE.Analyses.Noise.Noise.Noise
tag
 
geometry
 
settings
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
SUAVE.Analyses.Noise.Fidelity_One()
-
-    The Fidelity One Noise Analysis Class
-    
-        Assumptions:
-        None
-        
-        Source:
-        N/A
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Member Function Documentation

- -

◆ __defaults__()

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def SUAVE.Analyses.Noise.Fidelity_One.Fidelity_One.__defaults__ ( self)
-
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This sets the default values for the analysis.
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-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Output:
-None
-
-Properties Used:
-N/A
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Noise/Fidelity_One.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Noise_1_1Fidelity__One_1_1Fidelity__One.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Noise_1_1Fidelity__One_1_1Fidelity__One.js deleted file mode 100644 index e8c69fad..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Noise_1_1Fidelity__One_1_1Fidelity__One.js +++ /dev/null @@ -1,5 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Noise_1_1Fidelity__One_1_1Fidelity__One = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Noise_1_1Fidelity__One_1_1Fidelity__One.html#a60572d766f474ddcd227997f1ebb450d", null ], - [ "tag", "classSUAVE_1_1Analyses_1_1Noise_1_1Fidelity__One_1_1Fidelity__One.html#a67874a2ed5da3cb341240e47337a65e3", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Noise_1_1Fidelity__One_1_1Fidelity__One.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Noise_1_1Fidelity__One_1_1Fidelity__One.png deleted file mode 100644 index 074e36cf..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Noise_1_1Fidelity__One_1_1Fidelity__One.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Noise_1_1Noise_1_1Noise-members.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Noise_1_1Noise_1_1Noise-members.html deleted file mode 100644 index e89d04a8..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Noise_1_1Noise_1_1Noise-members.html +++ /dev/null @@ -1,124 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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- - - - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Noise_1_1Noise_1_1Noise.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Noise_1_1Noise_1_1Noise.html deleted file mode 100644 index d1d2f443..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Noise_1_1Noise_1_1Noise.html +++ /dev/null @@ -1,294 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Noise.Noise.Noise Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Noise.Noise.Noise Class Reference
-
-
-
-Inheritance diagram for SUAVE.Analyses.Noise.Noise.Noise:
-
-
- - -SUAVE.Analyses.Analysis.Analysis -SUAVE.Analyses.Noise.Fidelity_One.Fidelity_One - -
- - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def evaluate (self, state)
 
def finalize (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - -

-Public Attributes

tag
 
geometry
 
settings
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
SUAVE.Analyses.Noise.Noise()
-
-    The Top Level Noise Analysis Class
-    
-        Assumptions:
-        None
-        
-        Source:
-        N/A
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Noise.Noise.Noise.__defaults__ ( self)
-
-
This sets the default values and methods for the analysis.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    N/A
-
-
- -

◆ evaluate()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Analyses.Noise.Noise.Noise.evaluate ( self,
 state 
)
-
-
The default evaluate function.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-results   <Results class> (empty)
-
-Properties Used:
-N/A
-
-
-
- -

◆ finalize()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Noise.Noise.Noise.finalize ( self)
-
-
The default finalize function.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Noise/Noise.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Noise_1_1Noise_1_1Noise.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Noise_1_1Noise_1_1Noise.js deleted file mode 100644 index a43ff1b0..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Noise_1_1Noise_1_1Noise.js +++ /dev/null @@ -1,9 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Noise_1_1Noise_1_1Noise = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Noise_1_1Noise_1_1Noise.html#a2342b71d85757a91c54c62e06cac186c", null ], - [ "evaluate", "classSUAVE_1_1Analyses_1_1Noise_1_1Noise_1_1Noise.html#a1fe410522336b9578209ab9a245d6f23", null ], - [ "finalize", "classSUAVE_1_1Analyses_1_1Noise_1_1Noise_1_1Noise.html#adecd3b40e0449ce10c16a09720f38519", null ], - [ "geometry", "classSUAVE_1_1Analyses_1_1Noise_1_1Noise_1_1Noise.html#ac87f12023c475fd6c7ab439b6d0a36ec", null ], - [ "settings", "classSUAVE_1_1Analyses_1_1Noise_1_1Noise_1_1Noise.html#a4ace4776e761a67659693b7d0b65fe82", null ], - [ "tag", "classSUAVE_1_1Analyses_1_1Noise_1_1Noise_1_1Noise.html#a975777b61111316f783b4c995ceff381", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Noise_1_1Noise_1_1Noise.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Noise_1_1Noise_1_1Noise.png deleted file mode 100644 index 8a514c38..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Noise_1_1Noise_1_1Noise.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Planets_1_1Planet_1_1Planet-members.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Planets_1_1Planet_1_1Planet-members.html deleted file mode 100644 index b576f388..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Planets_1_1Planet_1_1Planet-members.html +++ /dev/null @@ -1,121 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Planets.Planet.Planet Member List
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SUAVE.Analyses.Planets.Planet.Planet Class Reference
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-Inheritance diagram for SUAVE.Analyses.Planets.Planet.Planet:
-
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- - -SUAVE.Analyses.Analysis.Analysis - -
- - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - -

-Public Attributes

tag
 
features
 
settings
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
SUAVE.Analyses.Planet()
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Planets.Planet.Planet.__defaults__ ( self)
-
-
This sets the default values and methods for the analysis.
-    
-    Assumptions:
-    Planet is Earth.
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    N/A
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Planets/Planet.py
  • -
-
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Planets_1_1Planet_1_1Planet.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Planets_1_1Planet_1_1Planet.js deleted file mode 100644 index 22ed10e8..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Planets_1_1Planet_1_1Planet.js +++ /dev/null @@ -1,7 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Planets_1_1Planet_1_1Planet = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Planets_1_1Planet_1_1Planet.html#a4375e1c51c7e4a17fc7990b173f47f2e", null ], - [ "features", "classSUAVE_1_1Analyses_1_1Planets_1_1Planet_1_1Planet.html#a733c4d16e42d6d08c854e741116685dc", null ], - [ "settings", "classSUAVE_1_1Analyses_1_1Planets_1_1Planet_1_1Planet.html#a069e019c0f3d32f8eac1a3d14c62816a", null ], - [ "tag", "classSUAVE_1_1Analyses_1_1Planets_1_1Planet_1_1Planet.html#a24e4ba909bfc859d37b1e192caee9844", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Planets_1_1Planet_1_1Planet.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Planets_1_1Planet_1_1Planet.png deleted file mode 100644 index 099a0fdd..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Planets_1_1Planet_1_1Planet.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Process_1_1Process-members.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Process_1_1Process-members.html deleted file mode 100644 index 00c24d78..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Process_1_1Process-members.html +++ /dev/null @@ -1,115 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Process.Process Member List
-
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- -

This is the complete list of members for SUAVE.Analyses.Process.Process, including all inherited members.

- - - - -
__call__(self, args, kwarg)SUAVE.Analyses.Process.Process
evaluate(self, args, kwarg)SUAVE.Analyses.Process.Process
verbose (defined in SUAVE.Analyses.Process.Process)SUAVE.Analyses.Process.Processstatic
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Process_1_1Process.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Process_1_1Process.html deleted file mode 100644 index d0d470dc..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Process_1_1Process.html +++ /dev/null @@ -1,250 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Process.Process Class Reference - - - - - - - - - - - - - - - -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Process.Process Class Reference
-
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-Inheritance diagram for SUAVE.Analyses.Process.Process:
-
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- - -SUAVE.Analyses.Aerodynamics.Process_Geometry.Process_Geometry - -
- - - - - - -

-Public Member Functions

def evaluate (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - -

-Static Public Attributes

-bool verbose = False
 
-

Detailed Description

-
SUAVE.Analyses.Process()
-
-    The Top Level Process Container Class
-    
-        Assumptions:
-        None
-        
-        Source:
-        N/A
-

Member Function Documentation

- -

◆ __call__()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Analyses.Process.Process.__call__ ( self,
 args,
 kwarg 
)
-
-
This is used to set the class' call behavior to the evaluate functions.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
- -

◆ evaluate()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Analyses.Process.Process.evaluate ( self,
 args,
 kwarg 
)
-
-
This is used to execute the evaluate functions of the analyses
-    stored in the container.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-Results of the Evaluate Functions
-
-Properties Used:
-N/A
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Process.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Process_1_1Process.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Process_1_1Process.js deleted file mode 100644 index e4c124f7..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Process_1_1Process.js +++ /dev/null @@ -1,5 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Process_1_1Process = -[ - [ "__call__", "classSUAVE_1_1Analyses_1_1Process_1_1Process.html#af4161c87be7d7b6c2ace43ca2ecad54e", null ], - [ "evaluate", "classSUAVE_1_1Analyses_1_1Process_1_1Process.html#a85d9cc1c2a36047100d9ce8abee28bda", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Process_1_1Process.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Process_1_1Process.png deleted file mode 100644 index dcfe0664..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Process_1_1Process.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Results_1_1Results.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Results_1_1Results.html deleted file mode 100644 index 13a0409a..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Results_1_1Results.html +++ /dev/null @@ -1,121 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Results.Results Class Reference - - - - - - - - - - - - - - - -
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SUAVE.Analyses.Results.Results Class Reference
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-Inheritance diagram for SUAVE.Analyses.Results.Results:
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The documentation for this class was generated from the following file:
    -
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SUAVE.Analyses.Settings.Container Member List
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Container (defined in SUAVE.Analyses.Settings.Container)SUAVE.Analyses.Settings.Containerstatic
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Settings_1_1Container.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Settings_1_1Container.html deleted file mode 100644 index 89394a1c..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Settings_1_1Container.html +++ /dev/null @@ -1,141 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Settings.Container Class Reference - - - - - - - - - - - - - - - -
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SUAVE.Analyses.Settings.Container Class Reference
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-Static Public Attributes

Container
 
-

Detailed Description

-
SUAVE.Analyses.Settings.Container()
-
-    The Top Level Settings Container Class
-    
-        Assumptions:
-        None
-        
-        Source:
-        N/A
-

The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Settings.py
  • -
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SUAVE.Analyses.Settings.Settings Member List
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This is the complete list of members for SUAVE.Analyses.Settings.Settings, including all inherited members.

- - - - -
__defaults__(self)SUAVE.Analyses.Settings.Settings
tag (defined in SUAVE.Analyses.Settings.Settings)SUAVE.Analyses.Settings.Settings
verbose_process (defined in SUAVE.Analyses.Settings.Settings)SUAVE.Analyses.Settings.Settings
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Settings_1_1Settings.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Settings_1_1Settings.html deleted file mode 100644 index 9e8b8e09..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Settings_1_1Settings.html +++ /dev/null @@ -1,184 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Settings.Settings Class Reference - - - - - - - - - - - - - - - -
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SUAVE.Analyses.Settings.Settings Class Reference
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-Public Member Functions

def __defaults__ (self)
 
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-Public Attributes

tag
 
verbose_process
 
-

Detailed Description

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SUAVE.Analyses.Settings()
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-    The Top Level Settings Class
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-        Assumptions:
-        None
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-        Source:
-        N/A
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Member Function Documentation

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◆ __defaults__()

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def SUAVE.Analyses.Settings.Settings.__defaults__ ( self)
-
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This sets the default values and methods for the settings.
-
-Assumptions:
-None
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-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
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The documentation for this class was generated from the following file:
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  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Settings.py
  • -
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Settings_1_1Settings.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Settings_1_1Settings.js deleted file mode 100644 index 89fd9fc2..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Settings_1_1Settings.js +++ /dev/null @@ -1,6 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Settings_1_1Settings = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Settings_1_1Settings.html#aa2d3d070627f1559b8929bc2ed280a0b", null ], - [ "tag", "classSUAVE_1_1Analyses_1_1Settings_1_1Settings.html#a8a826847043dbb77d04ceceef7302c5d", null ], - [ "verbose_process", "classSUAVE_1_1Analyses_1_1Settings_1_1Settings.html#a5b24b1eb97fd67544c9fe3b5b7d8c551", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Settings_1_1Settings.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Settings_1_1Settings.png deleted file mode 100644 index 348cc90a..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Settings_1_1Settings.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Sizing_1_1Sizing_1_1Sizing-members.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Sizing_1_1Sizing_1_1Sizing-members.html deleted file mode 100644 index d8a165eb..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Sizing_1_1Sizing_1_1Sizing-members.html +++ /dev/null @@ -1,122 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Sizing.Sizing.Sizing Class Reference
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-
-
-Inheritance diagram for SUAVE.Analyses.Sizing.Sizing.Sizing:
-
-
- - -SUAVE.Analyses.Analysis.Analysis - -
- - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def evaluate (self, conditions)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - -

-Public Attributes

tag
 
features
 
settings
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
SUAVE.Analyses.Sizing.Sizing()
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Sizing.Sizing.Sizing.__defaults__ ( self)
-
-
This sets the default values and methods for the analysis.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    N/A
-
-
-
- -

◆ evaluate()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Analyses.Sizing.Sizing.Sizing.evaluate ( self,
 conditions 
)
-
-
Evaluate the sizing analysis.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    Results of the Sizing Analysis
-    
-    Properties Used:
-    N/A                
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Sizing/Sizing.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Sizing_1_1Sizing_1_1Sizing.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Sizing_1_1Sizing_1_1Sizing.js deleted file mode 100644 index 4ce9ad1f..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Sizing_1_1Sizing_1_1Sizing.js +++ /dev/null @@ -1,8 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Sizing_1_1Sizing_1_1Sizing = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Sizing_1_1Sizing_1_1Sizing.html#ad8e65d15082bd0687cedbc5aa0d24452", null ], - [ "evaluate", "classSUAVE_1_1Analyses_1_1Sizing_1_1Sizing_1_1Sizing.html#a04d64dca02f05c95c937883ec87a3700", null ], - [ "features", "classSUAVE_1_1Analyses_1_1Sizing_1_1Sizing_1_1Sizing.html#a4ad59dbf0d8003e457c7ff74dbd61135", null ], - [ "settings", "classSUAVE_1_1Analyses_1_1Sizing_1_1Sizing_1_1Sizing.html#adf0c42754a8d0827f9195cfa3345a65c", null ], - [ "tag", "classSUAVE_1_1Analyses_1_1Sizing_1_1Sizing_1_1Sizing.html#a5e3dc9182bfe9c1b8990ddcbd99e2759", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Sizing_1_1Sizing_1_1Sizing.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Sizing_1_1Sizing_1_1Sizing.png deleted file mode 100644 index 65e00b01..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Sizing_1_1Sizing_1_1Sizing.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1AVL2_1_1AVL2-members.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1AVL2_1_1AVL2-members.html deleted file mode 100644 index 3e0d3341..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1AVL2_1_1AVL2-members.html +++ /dev/null @@ -1,204 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Stability.AVL2.AVL2 Member List
-
-
- -

This is the complete list of members for SUAVE.Analyses.Stability.AVL2.AVL2, including all inherited members.

- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
__call__(self, conditions) (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2
SUAVE::Analyses::Stability::Stability::Stability.__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self) (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2
angle_of_attack (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
AoA (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
AoA_data (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
AoA_mesh (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
AoA_points (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
batch_file (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
batch_index (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
build_surrogate(self) (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2
cases (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
CD (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
CD_data (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
CD_sur (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
cd_surrogate (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
CL (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
CL_data (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
CL_sur (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
cl_surrogate (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
CM (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
CM_data (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
CM_sur (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
cm_surrogate (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
coefficients (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
configuration (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
count (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
current_status (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
damping_ratio (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
data_array (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
data_len (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
deck_file (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
density (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
drag_coefficient (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
dutch_roll (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
dynamic (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
dynamic_stability (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
err_filename (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
evaluate(self, conditions)SUAVE.Analyses.Stability.Stability.Stability
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self) (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
fmt (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
fuel (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
geometry (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
gravity (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
grid_points (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
header (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
keep_files (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
lift_coefficient (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
log_filename (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
mac (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
mach (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
Mach (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
mach_data (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
mach_mesh (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
mach_number (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
mach_points (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
mass (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
moment_coefficient (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
moment_model (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
natural_frequency (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
phugoid (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
q (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
regr_cd (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
regr_cl (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
regr_cm (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
results (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
roll_tau (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
run_conditions (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
sample_training(self) (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2
settings (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
short_period (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
Span (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
spiral_tau (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
Sref (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
stability_model (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
static (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
static_stability (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
surrogates (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
table_size (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
tag (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
time0 (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
time1 (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
total_mass (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
training (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
training_file (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
velocity (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
xy (defined in SUAVE.Analyses.Stability.AVL2.AVL2)SUAVE.Analyses.Stability.AVL2.AVL2static
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Stability.AVL2.AVL2 Class Reference
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- -


-

Class

- - More...

-
-Inheritance diagram for SUAVE.Analyses.Stability.AVL2.AVL2:
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-Public Member Functions

-def __defaults__ (self)
 
-def finalize (self)
 
-def sample_training (self)
 
-def build_surrogate (self)
 
-def __call__ (self, conditions)
 
- Public Member Functions inherited from SUAVE.Analyses.Stability.Stability.Stability
def __defaults__ (self)
 
def evaluate (self, conditions)
 
def finalize (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Static Public Attributes

tag
 
keep_files
 
settings
 
current_status
 
batch_index
 
batch_file
 
deck_file
 
cases
 
log_filename
 
err_filename
 
training = self.training
 
angle_of_attack
 
Mach
 
lift_coefficient
 
drag_coefficient
 
training_file
 
surrogates = self.surrogates
 
moment_coefficient
 
configuration = self.configuration
 
geometry = self.geometry
 
stability_model = self.stability_model
 
short_period
 
natural_frequency
 
damping_ratio
 
phugoid
 
roll_tau
 
spiral_tau
 
dutch_roll
 
fuel = SUAVE.Components.Physical_Component()
 
mass
 
AoA = training.angle_of_attack
 
mach = training.Mach
 
CL = np.zeros([len(AoA)*len(mach),1])
 
CD = np.zeros([len(AoA)*len(mach),1])
 
CM = np.zeros([len(AoA)*len(mach),1])
 
table_size = len(AoA)*len(mach)
 
xy = np.zeros([table_size,2])
 
-int count = 0
 
time0 = time.time()
 
run_conditions = Aerodynamics()
 
total_mass
 
density = conditions.freestream.density
 
gravity
 
mach_number
 
velocity = conditions.freestream.velocity
 
results = self.evaluate_conditions(run_conditions)
 
time1 = time.time()
 
data_array = np.loadtxt(self.training_file)
 
fmt
 
header
 
coefficients
 
grid_points
 
AoA_data = training.angle_of_attack
 
mach_data = training.Mach
 
CL_data = training.coefficients[:,0]
 
CD_data = training.coefficients[:,1]
 
CM_data = training.coefficients[:,2]
 
regr_cm = gaussian_process.GaussianProcess()
 
regr_cl = gaussian_process.GaussianProcess()
 
regr_cd = gaussian_process.GaussianProcess()
 
cl_surrogate = regr_cl.fit(xy, CL_data)
 
cd_surrogate = regr_cd.fit(xy, CD_data)
 
cm_surrogate = regr_cm.fit(xy, CM_data)
 
AoA_points = np.linspace(-1.,7.,100)*Units.deg
 
mach_points = np.linspace(.25,.9,100)
 
AoA_mesh
 
mach_mesh
 
CL_sur = np.zeros(np.shape(AoA_mesh))
 
CD_sur = np.zeros(np.shape(AoA_mesh))
 
CM_sur = np.zeros(np.shape(AoA_mesh))
 
q = conditions.freestream.dynamic_pressure
 
Sref = geometry.reference_area
 
Span = geometry.wings['main_wing'].spans.projected
 
mac = geometry.wings['main_wing'].chords.mean_aerodynamic
 
moment_model = surrogates.moment_coefficient
 
static_stability = Data()
 
dynamic_stability = Data()
 
data_len = len(AoA)
 
static
 
dynamic
 
- - - - - - - - - - - - - - - -

-Additional Inherited Members

- Public Attributes inherited from SUAVE.Analyses.Stability.Stability.Stability
tag
 
geometry
 
settings
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-

-

Class

-
SUAVE.Analyses.Aerodynamics.AVL
-    aerodynamic model that performs a vortex lattice analysis using AVL
-    (Athena Vortex Lattice, by Mark Drela of MIT).
-
-    this class is callable, see self.__call__

The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Stability/AVL2.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1AVL2_1_1AVL2.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1AVL2_1_1AVL2.js deleted file mode 100644 index 20a96c2e..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1AVL2_1_1AVL2.js +++ /dev/null @@ -1,8 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Stability_1_1AVL2_1_1AVL2 = -[ - [ "__call__", "classSUAVE_1_1Analyses_1_1Stability_1_1AVL2_1_1AVL2.html#a8c2e1b483d8195ed4ad0a354bc22691f", null ], - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Stability_1_1AVL2_1_1AVL2.html#aba82fb46dedb531b5840b9007cf51e6f", null ], - [ "build_surrogate", "classSUAVE_1_1Analyses_1_1Stability_1_1AVL2_1_1AVL2.html#ad9da24f313e3882ff98cb70fa3987a32", null ], - [ "finalize", "classSUAVE_1_1Analyses_1_1Stability_1_1AVL2_1_1AVL2.html#a7914c48f7c40a53dbd08febfd6a69470", null ], - [ "sample_training", "classSUAVE_1_1Analyses_1_1Stability_1_1AVL2_1_1AVL2.html#a5a5c0123157c3fb961e5afc004b791c8", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1AVL2_1_1AVL2.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1AVL2_1_1AVL2.png deleted file mode 100644 index 4479d3d3..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1AVL2_1_1AVL2.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1AVL_1_1AVL-members.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1AVL_1_1AVL-members.html deleted file mode 100644 index 2a0bfbb4..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1AVL_1_1AVL-members.html +++ /dev/null @@ -1,135 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
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SUAVE.Analyses.Stability.AVL.AVL Member List
-
-
- -

This is the complete list of members for SUAVE.Analyses.Stability.AVL.AVL, including all inherited members.

- - - - - - - - - - - - - - - - - - - - - - - - -
__call__(self, conditions)SUAVE.Analyses.Stability.AVL.AVL
SUAVE::Analyses::Stability::Stability::Stability.__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Stability.AVL.AVL
build_surrogate(self)SUAVE.Analyses.Stability.AVL.AVL
compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
configuration (defined in SUAVE.Analyses.Stability.AVL.AVL)SUAVE.Analyses.Stability.AVL.AVL
current_status (defined in SUAVE.Analyses.Stability.AVL.AVL)SUAVE.Analyses.Stability.AVL.AVL
evaluate(self, conditions)SUAVE.Analyses.Stability.Stability.Stability
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
evaluate_conditions(self, run_conditions)SUAVE.Analyses.Stability.AVL.AVL
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self)SUAVE.Analyses.Stability.AVL.AVL
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
geometry (defined in SUAVE.Analyses.Stability.AVL.AVL)SUAVE.Analyses.Stability.AVL.AVL
initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
keep_files (defined in SUAVE.Analyses.Stability.AVL.AVL)SUAVE.Analyses.Stability.AVL.AVL
sample_training(self)SUAVE.Analyses.Stability.AVL.AVL
settings (defined in SUAVE.Analyses.Stability.AVL.AVL)SUAVE.Analyses.Stability.AVL.AVL
stability_model (defined in SUAVE.Analyses.Stability.AVL.AVL)SUAVE.Analyses.Stability.AVL.AVL
surrogates (defined in SUAVE.Analyses.Stability.AVL.AVL)SUAVE.Analyses.Stability.AVL.AVL
tag (defined in SUAVE.Analyses.Stability.AVL.AVL)SUAVE.Analyses.Stability.AVL.AVL
training (defined in SUAVE.Analyses.Stability.AVL.AVL)SUAVE.Analyses.Stability.AVL.AVL
training_file (defined in SUAVE.Analyses.Stability.AVL.AVL)SUAVE.Analyses.Stability.AVL.AVL
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1AVL_1_1AVL.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1AVL_1_1AVL.html deleted file mode 100644 index 8b6bfa0f..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1AVL_1_1AVL.html +++ /dev/null @@ -1,482 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Stability.AVL.AVL Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
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- -
- -
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- - -
- -
- -
- -
-
SUAVE.Analyses.Stability.AVL.AVL Class Reference
-
-
-
-Inheritance diagram for SUAVE.Analyses.Stability.AVL.AVL:
-
-
- - -SUAVE.Analyses.Stability.Stability.Stability -SUAVE.Analyses.Analysis.Analysis - -
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def finalize (self)
 
def __call__ (self, conditions)
 
def sample_training (self)
 
def build_surrogate (self)
 
def evaluate_conditions (self, run_conditions)
 
- Public Member Functions inherited from SUAVE.Analyses.Stability.Stability.Stability
def __defaults__ (self)
 
def evaluate (self, conditions)
 
def finalize (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

tag
 
keep_files
 
settings
 
current_status
 
training
 
training_file
 
surrogates
 
configuration
 
geometry
 
stability_model
 
- Public Attributes inherited from SUAVE.Analyses.Stability.Stability.Stability
tag
 
geometry
 
settings
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
This builds a surrogate and computes moment using AVL.
-
-Assumptions:
-None
-
-Source:
-None
-

Member Function Documentation

- -

◆ __call__()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Analyses.Stability.AVL.AVL.__call__ ( self,
 conditions 
)
-
-
Evaluates moment coefficient, stability deriviatives and neutral point using available surrogates.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-state.conditions.
-  mach_number      [-]
-  angle_of_attack  [radians]
-
-Outputs:
-results
-    results.static_stability
-    results.dynamic_stability
-
-
-Properties Used:
-self.surrogates.
-   pitch_moment_coefficient [-] CM
-   cm_alpha                 [-] Cm_alpha
-   cn_beta                  [-] Cn_beta
-   neutral_point            [-] NP
-
-
- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Stability.AVL.AVL.__defaults__ ( self)
-
-
This sets the default values and methods for the analysis.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
-
- -

◆ build_surrogate()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Stability.AVL.AVL.build_surrogate ( self)
-
-
Builds a surrogate based on sample evalations using a Guassian process.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-self.training.
-  coefficients     [-] CM, Cm_alpha, Cn_beta
-  neutral point    [meters] NP
-  grid_points      [radians,-] angles of attack and mach numbers 
-
-Outputs:
-self.surrogates.
-  moment_coefficient             <Guassian process surrogate>
-  Cm_alpha_moment_coefficient    <Guassian process surrogate>
-  Cn_beta_moment_coefficient     <Guassian process surrogate>
-  neutral_point                  <Guassian process surrogate>       
-
-Properties Used:
-No others
-
-
-
- -

◆ evaluate_conditions()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Analyses.Stability.AVL.AVL.evaluate_conditions ( self,
 run_conditions 
)
-
-
Process vehicle to setup geometry, condititon, and configuration.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-run_conditions <SUAVE data type> aerodynamic conditions; until input
-method is finalized, will assume mass_properties are always as 
-defined in self.features
-
-Outputs:
-results        <SUAVE data type>
-
-Properties Used:
-self.settings.filenames.
-  run_folder
-  output_template
-  batch_template
-  deck_template
-self.current_status.
-  batch_index
-  batch_file
-  deck_file
-  cases
-
-
-
- -

◆ finalize()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Stability.AVL.AVL.finalize ( self)
-
-
Drives functions to get training samples and build a surrogate.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-self.tag = 'avl_analysis_of_{}'.format(geometry.tag)
-
-Properties Used:
-self.geometry.tag
-
-
-
- -

◆ sample_training()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Stability.AVL.AVL.sample_training ( self)
-
-
Call methods to run AVL for sample point evaluation.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-see properties used
-
-Outputs:
-self.training.
-  coefficients     [-] CM, Cm_alpha, Cn_beta CD
-  neutral point    [-] NP
-  grid_points      [radians,-] angles of attack and mach numbers 
-
-Properties Used:
-self.geometry.tag  <string>
-self.training.     
-  angle_of_attack  [radians]
-  Mach             [-]
-self.training_file (optional - file containing previous AVL data)
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Stability/AVL.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1AVL_1_1AVL.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1AVL_1_1AVL.js deleted file mode 100644 index 109ef67b..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1AVL_1_1AVL.js +++ /dev/null @@ -1,19 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Stability_1_1AVL_1_1AVL = -[ - [ "__call__", "classSUAVE_1_1Analyses_1_1Stability_1_1AVL_1_1AVL.html#ae7f5a136d4f914773b415c5c017b176d", null ], - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Stability_1_1AVL_1_1AVL.html#a9f37075e2a9c2fbc72f7cd566644e76f", null ], - [ "build_surrogate", "classSUAVE_1_1Analyses_1_1Stability_1_1AVL_1_1AVL.html#a5347926425ec1203182205229dc97d64", null ], - [ "evaluate_conditions", "classSUAVE_1_1Analyses_1_1Stability_1_1AVL_1_1AVL.html#a657bb443e967af278f6c71dd9984e51f", null ], - [ "finalize", "classSUAVE_1_1Analyses_1_1Stability_1_1AVL_1_1AVL.html#af45ebff1bbb70f893a8acf375a3bf22b", null ], - [ "sample_training", "classSUAVE_1_1Analyses_1_1Stability_1_1AVL_1_1AVL.html#a562e6b7c59034a322413caecdaf20a0b", null ], - [ "configuration", "classSUAVE_1_1Analyses_1_1Stability_1_1AVL_1_1AVL.html#a8eea7bc16140884d265413b200d0b8d4", null ], - [ "current_status", "classSUAVE_1_1Analyses_1_1Stability_1_1AVL_1_1AVL.html#a5e02a873dd1c9343fd8aad6958cc6745", null ], - [ "geometry", "classSUAVE_1_1Analyses_1_1Stability_1_1AVL_1_1AVL.html#a986baf42d99f5aceecd129b0e96dfeef", null ], - [ "keep_files", "classSUAVE_1_1Analyses_1_1Stability_1_1AVL_1_1AVL.html#afa2cccd337ca32296250e3a064452d2e", null ], - [ "settings", "classSUAVE_1_1Analyses_1_1Stability_1_1AVL_1_1AVL.html#a7166eeacc3407b0cf419bd38540d2bce", null ], - [ "stability_model", "classSUAVE_1_1Analyses_1_1Stability_1_1AVL_1_1AVL.html#a5df82e27a841c273c87e0ad921e694e0", null ], - [ "surrogates", "classSUAVE_1_1Analyses_1_1Stability_1_1AVL_1_1AVL.html#a0531b41b4becb72563a55c5a1a512064", null ], - [ "tag", "classSUAVE_1_1Analyses_1_1Stability_1_1AVL_1_1AVL.html#acb0b333f0664e897af228b7636682b7b", null ], - [ "training", "classSUAVE_1_1Analyses_1_1Stability_1_1AVL_1_1AVL.html#a93ec6a80598d06260202387cdc472a85", null ], - [ "training_file", "classSUAVE_1_1Analyses_1_1Stability_1_1AVL_1_1AVL.html#a659419bbaa3a1c31714b103baaaa237f", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1AVL_1_1AVL.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1AVL_1_1AVL.png deleted file mode 100644 index 3cfcde73..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1AVL_1_1AVL.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1Fidelity__Zero_1_1Fidelity__Zero-members.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1Fidelity__Zero_1_1Fidelity__Zero-members.html deleted file mode 100644 index 9fbf71e9..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1Fidelity__Zero_1_1Fidelity__Zero-members.html +++ /dev/null @@ -1,164 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
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-
- -
-
-
- -
- -
-
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SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero Member List
-
-
- -

This is the complete list of members for SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero, including all inherited members.

- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
__call__(self, conditions)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero
SUAVE::Analyses::Stability::Stability::Stability.__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self) (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero
cDw (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
cl_beta (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
cl_p (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
cl_psi (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
cl_r (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
cL_u (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
cm_alpha_dot (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
cm_q (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
cn_beta (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
cn_r (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
configurationSUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
cx_alpha (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
cx_u (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
cy_beta (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
cy_phi (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
cz_alpha (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
cz_alpha_dot (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
cz_q (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
cz_u (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
damping_ratio (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
dutch_roll (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
dynamic (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
evaluate(self, conditions)SUAVE.Analyses.Stability.Stability.Stability
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self) (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
fuel (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
geometrySUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
l_t (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
l_v (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
lateral_directional (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
longitudinal (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
mass (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
mass_properties (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
natural_frequency (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
phugoid (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
results (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
roll_tau (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
settings (defined in SUAVE.Analyses.Stability.Stability.Stability)SUAVE.Analyses.Stability.Stability.Stability
short_period (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
spiral_tau (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
stability_model (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
static (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
static_margin (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
tag (defined in SUAVE.Analyses.Stability.Stability.Stability)SUAVE.Analyses.Stability.Stability.Stability
theta (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1Fidelity__Zero_1_1Fidelity__Zero.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1Fidelity__Zero_1_1Fidelity__Zero.html deleted file mode 100644 index 1a5a4b1c..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1Fidelity__Zero_1_1Fidelity__Zero.html +++ /dev/null @@ -1,433 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
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- - - -
-
- -
-
-
- -
- -
-
- - -
- -
- -
- -
-
SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero Class Reference
-
-
-
-Inheritance diagram for SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero:
-
-
- - -SUAVE.Analyses.Stability.Stability.Stability -SUAVE.Analyses.Analysis.Analysis - -
- - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

-def __defaults__ (self)
 
-def finalize (self)
 
def __call__ (self, conditions)
 
- Public Member Functions inherited from SUAVE.Analyses.Stability.Stability.Stability
def __defaults__ (self)
 
def evaluate (self, conditions)
 
def finalize (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Static Public Attributes

 configuration = self.configuration
 
 geometry = self.geometry
 
stability_model = self.stability_model
 
short_period
 
natural_frequency
 
damping_ratio
 
phugoid
 
roll_tau
 
spiral_tau
 
dutch_roll
 
mass_properties
 
fuel = SUAVE.Components.Physical_Component()
 
mass
 
cn_beta
 
static_margin
 
cDw = aero.drag_breakdown.parasite['main_wing'].parasite_drag_coefficient
 
l_v = geometry.wings['vertical_stabilizer'].origin[0] + geometry.wings['vertical_stabilizer'].aerodynamic_center[0] - geometry.wings['main_wing'].origin[0] - geometry.wings['main_wing'].aerodynamic_center[0]
 
cn_r
 
cl_p
 
cl_beta
 
cy_beta
 
l_t = geometry.wings['horizontal_stabilizer'].origin[0] + geometry.wings['horizontal_stabilizer'].aerodynamic_center[0] - geometry.wings['main_wing'].origin[0] - geometry.wings['main_wing'].aerodynamic_center[0]
 
cm_q
 
cm_alpha_dot
 
cz_alpha
 
cy_phi
 
cl_r
 
theta = conditions.frames.wind.body_rotations[:,1]
 
cl_psi
 
cL_u
 
cz_u
 
cz_alpha_dot
 
cz_q
 
cx_u
 
cx_alpha
 
lateral_directional = Full_Linearized_Equations.lateral_directional(velocity, static_stability.cn_beta , Sref, density, Span, configuration.mass_properties.moments_of_inertia.tensor[2][2], dynamic_stability.cn_r, configuration.mass_properties.moments_of_inertia.tensor[0][0], dynamic_stability.cl_p, configuration.mass_properties.moments_of_inertia.tensor[0][2], dynamic_stability.cl_r, dynamic_stability.cl_beta, dynamic_stability.cn_p, dynamic_stability.cy_phi, dynamic_stability.cy_psi, dynamic_stability.cy_beta, conditions.weights.total_mass)
 
longitudinal = Full_Linearized_Equations.longitudinal(velocity, density, Sref, mac, dynamic_stability.cm_q, dynamic_stability.cz_alpha, conditions.weights.total_mass, static_stability.cm_alpha, configuration.mass_properties.moments_of_inertia.tensor[1][1], dynamic_stability.cm_alpha_dot, dynamic_stability.cz_u, dynamic_stability.cz_alpha_dot, dynamic_stability.cz_q, -aero.lift_coefficient, theta, dynamic_stability.cx_u, dynamic_stability.cx_alpha)
 
results = Data()
 
static
 
dynamic
 
- - - - - - - - - - - - - - - -

-Additional Inherited Members

- Public Attributes inherited from SUAVE.Analyses.Stability.Stability.Stability
tag
 
geometry
 
settings
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
This is an analysis based on low-fidelity models.
-
-Assumptions:
-Subsonic
-
-Source:
-Primarily based on adg.stanford.edu, see methods for details
-

Member Function Documentation

- -

◆ __call__()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero.__call__ ( self,
 conditions 
)
-
-
Process vehicle to setup geometry, condititon and configuration
-    
-Assumptions:
-None
-       
-Source:
-    N/A
-
-    Inputs:
-conditions - DataDict() of aerodynamic conditions
-results    - DataDict() of moment coeffients and stability derivatives
-
-    Outputs:
-    None
- 
-    Properties Used:
-    self.geometry
-
-
-

Member Data Documentation

- -

◆ configuration

- -
-
- - - - - -
- - - - -
SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero.configuration = self.configuration
-
-static
-
-
This sets the default values and methods for the analysis.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
-
- -

◆ geometry

- -
-
- - - - - -
- - - - -
SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero.geometry = self.geometry
-
-static
-
-
Finalizes the surrogate needed for lift calculation.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-self.geometry
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Stability/Fidelity_Zero.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1Fidelity__Zero_1_1Fidelity__Zero.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1Fidelity__Zero_1_1Fidelity__Zero.js deleted file mode 100644 index b3f89a9e..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1Fidelity__Zero_1_1Fidelity__Zero.js +++ /dev/null @@ -1,6 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Stability_1_1Fidelity__Zero_1_1Fidelity__Zero = -[ - [ "__call__", "classSUAVE_1_1Analyses_1_1Stability_1_1Fidelity__Zero_1_1Fidelity__Zero.html#acbce9b7e47bacb187aa72ba799652b5a", null ], - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Stability_1_1Fidelity__Zero_1_1Fidelity__Zero.html#abf23a7cc154b9b9cf5f7a54b2e7d746d", null ], - [ "finalize", "classSUAVE_1_1Analyses_1_1Stability_1_1Fidelity__Zero_1_1Fidelity__Zero.html#a8aca95c7e34ed2d1edffd84bd1c666e0", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1Fidelity__Zero_1_1Fidelity__Zero.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1Fidelity__Zero_1_1Fidelity__Zero.png deleted file mode 100644 index 3712580d..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1Fidelity__Zero_1_1Fidelity__Zero.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1Stability_1_1Stability-members.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1Stability_1_1Stability-members.html deleted file mode 100644 index 54c650d5..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1Stability_1_1Stability-members.html +++ /dev/null @@ -1,124 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
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- - - -
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- - - - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1Stability_1_1Stability.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1Stability_1_1Stability.html deleted file mode 100644 index d959dcb4..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1Stability_1_1Stability.html +++ /dev/null @@ -1,289 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Stability.Stability.Stability Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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- -
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SUAVE.Analyses.Stability.Stability.Stability Class Reference
-
-
-
-Inheritance diagram for SUAVE.Analyses.Stability.Stability.Stability:
-
-
- - -SUAVE.Analyses.Analysis.Analysis -SUAVE.Analyses.Stability.AVL2.AVL2 -SUAVE.Analyses.Stability.AVL.AVL -SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero - -
- - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def evaluate (self, conditions)
 
def finalize (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - -

-Public Attributes

tag
 
geometry
 
settings
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
SUAVE.Analyses.Stability.Stability()
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Stability.Stability.Stability.__defaults__ ( self)
-
-
This sets the default values and methods for the analysis.
-    
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
-
- -

◆ evaluate()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Analyses.Stability.Stability.Stability.evaluate ( self,
 conditions 
)
-
-
Evaluate the stability analysis.
-    
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-results
-
-Properties Used:
-N/A
-
-
-
- -

◆ finalize()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Stability.Stability.Stability.finalize ( self)
-
-
Finalize the stability analysis.
-    
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Stability/Stability.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1Stability_1_1Stability.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1Stability_1_1Stability.js deleted file mode 100644 index 6095cf7b..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1Stability_1_1Stability.js +++ /dev/null @@ -1,9 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Stability_1_1Stability_1_1Stability = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Stability_1_1Stability_1_1Stability.html#ad9415b49f7e7abbf438c580408d04fd6", null ], - [ "evaluate", "classSUAVE_1_1Analyses_1_1Stability_1_1Stability_1_1Stability.html#a5d0b08724b00a16cf37e4847a1097911", null ], - [ "finalize", "classSUAVE_1_1Analyses_1_1Stability_1_1Stability_1_1Stability.html#a0f6a8084c69a5ffac117a936abff057a", null ], - [ "geometry", "classSUAVE_1_1Analyses_1_1Stability_1_1Stability_1_1Stability.html#ae61490a43e7f58d68dc00a466c815b95", null ], - [ "settings", "classSUAVE_1_1Analyses_1_1Stability_1_1Stability_1_1Stability.html#a36c6d2d49b3f67fb0a7f596d984702da", null ], - [ "tag", "classSUAVE_1_1Analyses_1_1Stability_1_1Stability_1_1Stability.html#a372454e530a7219aa07a7dda0fab4da5", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1Stability_1_1Stability.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1Stability_1_1Stability.png deleted file mode 100644 index 3ded378a..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1Stability_1_1Stability.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Structures_1_1Structures_1_1Structures-members.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Structures_1_1Structures_1_1Structures-members.html deleted file mode 100644 index 14ed4d49..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Structures_1_1Structures_1_1Structures-members.html +++ /dev/null @@ -1,122 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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- -
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SUAVE.Analyses.Structures.Structures.Structures Class Reference
-
-
-
-Inheritance diagram for SUAVE.Analyses.Structures.Structures.Structures:
-
-
- - -SUAVE.Analyses.Analysis.Analysis - -
- - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def evaluate (self, conditions)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - -

-Public Attributes

tag
 
features
 
settings
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
SUAVE.Analyses.Structures.Structures()
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Structures.Structures.Structures.__defaults__ ( self)
-
-
This sets the default values and methods for the analysis.
-    
-Assumptions:
-None
-    
-Source:
-N/A
-    
-Inputs:
-None
-    
-Outputs:
-None
-    
-Properties Used:
-N/A
-
-
- -

◆ evaluate()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Analyses.Structures.Structures.Structures.evaluate ( self,
 conditions 
)
-
-
Evaluate the Structures analysis.
-    
-Assumptions:
-None
-    
-Source:
-N/A
-    
-Inputs:
-None
-    
-Outputs:
-Results of the Structures Analysis
-    
-Properties Used:
-N/A                
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Structures/Structures.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Structures_1_1Structures_1_1Structures.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Structures_1_1Structures_1_1Structures.js deleted file mode 100644 index bd3dc201..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Structures_1_1Structures_1_1Structures.js +++ /dev/null @@ -1,8 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Structures_1_1Structures_1_1Structures = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Structures_1_1Structures_1_1Structures.html#af4900ed36ae06effa0ecb10080e0a667", null ], - [ "evaluate", "classSUAVE_1_1Analyses_1_1Structures_1_1Structures_1_1Structures.html#ab08fe047a6db230f0029c0d99f8d44f7", null ], - [ "features", "classSUAVE_1_1Analyses_1_1Structures_1_1Structures_1_1Structures.html#a4de2b7356404f1e4d38b3509bf8dc9ad", null ], - [ "settings", "classSUAVE_1_1Analyses_1_1Structures_1_1Structures_1_1Structures.html#a7010fe6e6c8eee4c11c401441855d3ae", null ], - [ "tag", "classSUAVE_1_1Analyses_1_1Structures_1_1Structures_1_1Structures.html#a8a7a57d3440fa99c345d107250296f5e", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Structures_1_1Structures_1_1Structures.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Structures_1_1Structures_1_1Structures.png deleted file mode 100644 index 9c85adf2..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Structures_1_1Structures_1_1Structures.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Surrogate_1_1Surrogate-members.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Surrogate_1_1Surrogate-members.html deleted file mode 100644 index 7c766fed..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Surrogate_1_1Surrogate-members.html +++ /dev/null @@ -1,127 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Surrogate.Surrogate Class Reference
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-Public Member Functions

def __defaults__ (self)
 
def finalize (self)
 
def sample_training (self)
 
def build_surrogate (self)
 
def evaluate (self, state)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - -

-Public Attributes

training
 
surrogates
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
SUAVE.Analyses.Surrogate()
-
-    The Top Level Surrogate Class
-    
-        Assumptions:
-        None
-        
-        Source:
-        N/A
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Surrogate.Surrogate.__defaults__ ( self)
-
-
This sets the default values for the surrogate.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
- -

◆ build_surrogate()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Surrogate.Surrogate.build_surrogate ( self)
-
-
This is used to build the surrogate based on previous training.
-       
-Assumptions:
-None
-       
-Source:
-N/A
-       
-Inputs:
-None
-       
-Outputs:
-None
-       
-Properties Used:
-N/A
-
-
- -

◆ evaluate()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Analyses.Surrogate.Surrogate.evaluate ( self,
 state 
)
-
-
This is used to evaluate the surrogate.
-               
-Assumptions:
-None
-               
-Source:
-N/A
-               
-Inputs:
-None
-               
-Outputs:
-Results of the surrogate model
-               
-Properties Used:
-N/A
-
-
- -

◆ finalize()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Surrogate.Surrogate.finalize ( self)
-
-
This is used to finalize the surrogate's training and build
-   the final surrogate.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
- -

◆ sample_training()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Surrogate.Surrogate.sample_training ( self)
-
-
This is used to train the surrogate on the sampled data
-   according the optimization plan.
-       
-Assumptions:
-None
-       
-Source:
-N/A
-       
-Inputs:
-None
-       
-Outputs:
-None
-       
-Properties Used:
-N/A
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Surrogate.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Surrogate_1_1Surrogate.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Surrogate_1_1Surrogate.js deleted file mode 100644 index f5f31e04..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Surrogate_1_1Surrogate.js +++ /dev/null @@ -1,10 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Surrogate_1_1Surrogate = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Surrogate_1_1Surrogate.html#a63d74ea95e3ee3d75b421763b1b7eab0", null ], - [ "build_surrogate", "classSUAVE_1_1Analyses_1_1Surrogate_1_1Surrogate.html#ae64ef8c0d281e8bf19f00ffaa42e1ad6", null ], - [ "evaluate", "classSUAVE_1_1Analyses_1_1Surrogate_1_1Surrogate.html#abbabba1804ca34f98a001e05a97e9438", null ], - [ "finalize", "classSUAVE_1_1Analyses_1_1Surrogate_1_1Surrogate.html#ab1a1e389cc333127b68d622554f188c0", null ], - [ "sample_training", "classSUAVE_1_1Analyses_1_1Surrogate_1_1Surrogate.html#a7fd280baca4ac2ad8a73e4858b2c3906", null ], - [ "surrogates", "classSUAVE_1_1Analyses_1_1Surrogate_1_1Surrogate.html#a1728feddc45a65ba7a71ee8ba510fb70", null ], - [ "training", "classSUAVE_1_1Analyses_1_1Surrogate_1_1Surrogate.html#a24906c9735ddd0f6775997b00bcab98e", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Surrogate_1_1Surrogate.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Surrogate_1_1Surrogate.png deleted file mode 100644 index f60487b9..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Surrogate_1_1Surrogate.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Vehicle_1_1Vehicle-members.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Vehicle_1_1Vehicle-members.html deleted file mode 100644 index aae2de29..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Vehicle_1_1Vehicle-members.html +++ /dev/null @@ -1,130 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
-
- - - -
-
- -
-
-
- - - - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Vehicle_1_1Vehicle.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Vehicle_1_1Vehicle.html deleted file mode 100644 index d867c371..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Vehicle_1_1Vehicle.html +++ /dev/null @@ -1,364 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Vehicle.Vehicle Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
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-
- - - -
-
- -
-
-
- -
- -
-
- - -
- -
- -
- -
-
SUAVE.Analyses.Vehicle.Vehicle Class Reference
-
-
-
-Inheritance diagram for SUAVE.Analyses.Vehicle.Vehicle:
-
-
- - -SUAVE.Analyses.Analysis.Container - -
- - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def append (self, analysis)
 
def __init__ (self, args, kwarg)
 
def get_root (self, analysis)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Container
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - - - - - - -

-Public Attributes

sizing
 
weights
 
aerodynamics
 
stability
 
energy
 
atmosphere
 
planet
 
noise
 
costs
 
-

Detailed Description

-
SUAVE.Analyses.Vehicle()
-
-    The Vehicle Analyses Container Class
-    
-        Assumptions:
-        None
-        
-        Source:
-        N/A
-

Constructor & Destructor Documentation

- -

◆ __init__()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Analyses.Vehicle.Vehicle.__init__ ( self,
 args,
 kwarg 
)
-
-
This sets the initialization behavior of the vehicle analysis
-   container. Maps analysis paths to string keys.
-   
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
-
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Vehicle.Vehicle.__defaults__ ( self)
-
-
This sets the default analyses to be applied to the vehicle.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
-
- -

◆ append()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Analyses.Vehicle.Vehicle.append ( self,
 analysis 
)
-
-
This is used to add new analyses to the container.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-Analysis to be added
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
-
- -

◆ get_root()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Analyses.Vehicle.Vehicle.get_root ( self,
 analysis 
)
-
-
This is used to determine the root of the analysis path associated
-    with a particular analysis key by the analysis map.
-    
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-Analysis key to be checked
-
-Outputs:
-Path root of analysis
-
-Properties Used:
-N/A
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Vehicle.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Vehicle_1_1Vehicle.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Vehicle_1_1Vehicle.js deleted file mode 100644 index 5ba9c378..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Vehicle_1_1Vehicle.js +++ /dev/null @@ -1,16 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Vehicle_1_1Vehicle = -[ - [ "__init__", "classSUAVE_1_1Analyses_1_1Vehicle_1_1Vehicle.html#aac80b206b29af7818940de54f437ebec", null ], - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Vehicle_1_1Vehicle.html#a6fbadfc951c25c01c181e75c8b07db75", null ], - [ "append", "classSUAVE_1_1Analyses_1_1Vehicle_1_1Vehicle.html#a47da109afe71d431d2c6e31b12ce51e9", null ], - [ "get_root", "classSUAVE_1_1Analyses_1_1Vehicle_1_1Vehicle.html#a7432f659914e8bc502addeb53b571bc8", null ], - [ "aerodynamics", "classSUAVE_1_1Analyses_1_1Vehicle_1_1Vehicle.html#a9f63f0a638abd847efb142870d99d6da", null ], - [ "atmosphere", "classSUAVE_1_1Analyses_1_1Vehicle_1_1Vehicle.html#abfbfa7b9d3e6f832de7eae358052643d", null ], - [ "costs", "classSUAVE_1_1Analyses_1_1Vehicle_1_1Vehicle.html#a936c3a05e3b0d18b61e115661d07f993", null ], - [ "energy", "classSUAVE_1_1Analyses_1_1Vehicle_1_1Vehicle.html#a7977b26001a2c93886019c354934af77", null ], - [ "noise", "classSUAVE_1_1Analyses_1_1Vehicle_1_1Vehicle.html#aa75d0cc7054bd5c97f19274aefb2de86", null ], - [ "planet", "classSUAVE_1_1Analyses_1_1Vehicle_1_1Vehicle.html#a3b8f4e4495e3b397038fca89ee6adcf9", null ], - [ "sizing", "classSUAVE_1_1Analyses_1_1Vehicle_1_1Vehicle.html#a5b283acbd14d520e53fa261eac9f6408", null ], - [ "stability", "classSUAVE_1_1Analyses_1_1Vehicle_1_1Vehicle.html#a465d497f092020fea50d48d859932e69", null ], - [ "weights", "classSUAVE_1_1Analyses_1_1Vehicle_1_1Vehicle.html#a76913f0ea1d78e7e6c5effbf2e9f5f58", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Vehicle_1_1Vehicle.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Vehicle_1_1Vehicle.png deleted file mode 100644 index eac82867..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Vehicle_1_1Vehicle.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights_1_1Weights-members.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights_1_1Weights-members.html deleted file mode 100644 index 5bb5c1f6..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights_1_1Weights-members.html +++ /dev/null @@ -1,124 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
-
- - - -
-
- -
-
-
- - - - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights_1_1Weights.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights_1_1Weights.html deleted file mode 100644 index 661b3ae1..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights_1_1Weights.html +++ /dev/null @@ -1,295 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Weights.Weights.Weights Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
-
- - - -
-
- -
-
-
- -
- -
-
- - -
- -
- -
- -
-
SUAVE.Analyses.Weights.Weights.Weights Class Reference
-
-
-
-Inheritance diagram for SUAVE.Analyses.Weights.Weights.Weights:
-
-
- - -SUAVE.Analyses.Analysis.Analysis -SUAVE.Analyses.Weights.Weights_BWB.Weights_BWB -SUAVE.Analyses.Weights.Weights_Tube_Wing.Weights_Tube_Wing -SUAVE.Analyses.Weights.Weights_UAV.Weights_UAV - -
- - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def evaluate (self)
 
def finalize (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - -

-Public Attributes

tag
 
vehicle
 
settings
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
This is a class that call the functions that computes the weight of 
-an aircraft depending on its configration
-
-Assumptions:
-    None
-
-Source:
-    N/A
-
-Inputs:
-    None
-    
-Outputs:
-    None
-
-Properties Used:
-     N/A
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Weights.Weights.Weights.__defaults__ ( self)
-
-
This sets the default values and methods for the weights analysis.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
-
- -

◆ evaluate()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Weights.Weights.Weights.evaluate ( self)
-
-
Evaluate the weight analysis.
-    
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
-
- -

◆ finalize()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Weights.Weights.Weights.finalize ( self)
-
-
Finalize the weight analysis.
-    
-Assumptions:
-None
-    
-Source:
-N/A
-    
-Inputs:
-None
-    
-Outputs:
-None
-    
-Properties Used:
-N/A
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Weights/Weights.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights_1_1Weights.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights_1_1Weights.js deleted file mode 100644 index f92bb97e..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights_1_1Weights.js +++ /dev/null @@ -1,9 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Weights_1_1Weights_1_1Weights = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights_1_1Weights.html#a86cc65bf0c5930a39233813eff22a7d6", null ], - [ "evaluate", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights_1_1Weights.html#ac9645a2ebbd1e56c398e1f4c140aa92b", null ], - [ "finalize", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights_1_1Weights.html#a7baa0de30c63153a9d786f962678efc0", null ], - [ "settings", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights_1_1Weights.html#a99617252b6aabe071d5d227009e46faf", null ], - [ "tag", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights_1_1Weights.html#a50368d1720b2d063aa80c22144adb0e6", null ], - [ "vehicle", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights_1_1Weights.html#aa9247e038c8fffe1d74089cbf3204751", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights_1_1Weights.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights_1_1Weights.png deleted file mode 100644 index 0f76726e..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights_1_1Weights.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__BWB_1_1Weights__BWB-members.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__BWB_1_1Weights__BWB-members.html deleted file mode 100644 index 4a6416fa..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__BWB_1_1Weights__BWB-members.html +++ /dev/null @@ -1,126 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
-
- - - -
-
- -
-
-
- - - - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__BWB_1_1Weights__BWB.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__BWB_1_1Weights__BWB.html deleted file mode 100644 index b97ec31d..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__BWB_1_1Weights__BWB.html +++ /dev/null @@ -1,321 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Weights.Weights_BWB.Weights_BWB Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
-
- - - -
-
- -
-
-
- -
- -
-
- - -
- -
- -
- -
-
SUAVE.Analyses.Weights.Weights_BWB.Weights_BWB Class Reference
-
-
-
-Inheritance diagram for SUAVE.Analyses.Weights.Weights_BWB.Weights_BWB:
-
-
- - -SUAVE.Analyses.Weights.Weights.Weights -SUAVE.Analyses.Analysis.Analysis - -
- - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def evaluate (self, conditions=None)
 
def finalize (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Weights.Weights.Weights
def __defaults__ (self)
 
def evaluate (self)
 
def finalize (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

tag
 
vehicle
 
settings
 
mass_properties
 
- Public Attributes inherited from SUAVE.Analyses.Weights.Weights.Weights
tag
 
vehicle
 
settings
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
This is class that evaluates the weight of a BWB aircraft
-
-Assumptions:
-    None
-
-Source:
-    N/A
-
-Inputs:
-    None
-  
-Outputs:
-    None
-
-Properties Used:
-     N/A
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Weights.Weights_BWB.Weights_BWB.__defaults__ ( self)
-
-
This sets the default values and methods for the BWB weight analysis.
-    
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
-
- -

◆ evaluate()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Analyses.Weights.Weights_BWB.Weights_BWB.evaluate ( self,
 conditions = None 
)
-
-
Evaluate the weight analysis.
-    
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-results
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-Properties Used:
-N/A
-
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-
- -

◆ finalize()

- -
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def SUAVE.Analyses.Weights.Weights_BWB.Weights_BWB.finalize ( self)
-
-
Finalize the weight analysis.
-    
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Weights/Weights_BWB.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__BWB_1_1Weights__BWB.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__BWB_1_1Weights__BWB.js deleted file mode 100644 index 21a411ed..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__BWB_1_1Weights__BWB.js +++ /dev/null @@ -1,10 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Weights_1_1Weights__BWB_1_1Weights__BWB = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights__BWB_1_1Weights__BWB.html#a9b49241023c3d24a518d49adeed118b1", null ], - [ "evaluate", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights__BWB_1_1Weights__BWB.html#a430f1609a90328f8e742f6549f71b26d", null ], - [ "finalize", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights__BWB_1_1Weights__BWB.html#a6045a46a2240c16d562c6206f6f61778", null ], - [ "mass_properties", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights__BWB_1_1Weights__BWB.html#a83f284897ffee3e8ec2fc6e229eac08f", null ], - [ "settings", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights__BWB_1_1Weights__BWB.html#a26bc811bcc5941a70f37a53381c66787", null ], - [ "tag", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights__BWB_1_1Weights__BWB.html#a63b040cecfd2d1adcad13a91cad5f4b5", null ], - [ "vehicle", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights__BWB_1_1Weights__BWB.html#a9a5d8ea00331456f8a423aa1d2562c34", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__BWB_1_1Weights__BWB.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__BWB_1_1Weights__BWB.png deleted file mode 100644 index 20609af3..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__BWB_1_1Weights__BWB.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__Tube__Wing_1_1Weights__Tube__Wing-members.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__Tube__Wing_1_1Weights__Tube__Wing-members.html deleted file mode 100644 index a5da1139..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__Tube__Wing_1_1Weights__Tube__Wing-members.html +++ /dev/null @@ -1,126 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Weights.Weights_Tube_Wing.Weights_Tube_Wing Member List
-
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- -

This is the complete list of members for SUAVE.Analyses.Weights.Weights_Tube_Wing.Weights_Tube_Wing, including all inherited members.

- - - - - - - - - - - - - - - -
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Weights.Weights_Tube_Wing.Weights_Tube_Wing
compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
evaluate(self, conditions=None)SUAVE.Analyses.Weights.Weights_Tube_Wing.Weights_Tube_Wing
SUAVE::Analyses::Weights::Weights::Weights.evaluate(self)SUAVE.Analyses.Weights.Weights.Weights
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self)SUAVE.Analyses.Weights.Weights_Tube_Wing.Weights_Tube_Wing
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
mass_properties (defined in SUAVE.Analyses.Weights.Weights_Tube_Wing.Weights_Tube_Wing)SUAVE.Analyses.Weights.Weights_Tube_Wing.Weights_Tube_Wing
settings (defined in SUAVE.Analyses.Weights.Weights_Tube_Wing.Weights_Tube_Wing)SUAVE.Analyses.Weights.Weights_Tube_Wing.Weights_Tube_Wing
tag (defined in SUAVE.Analyses.Weights.Weights_Tube_Wing.Weights_Tube_Wing)SUAVE.Analyses.Weights.Weights_Tube_Wing.Weights_Tube_Wing
vehicle (defined in SUAVE.Analyses.Weights.Weights_Tube_Wing.Weights_Tube_Wing)SUAVE.Analyses.Weights.Weights_Tube_Wing.Weights_Tube_Wing
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__Tube__Wing_1_1Weights__Tube__Wing.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__Tube__Wing_1_1Weights__Tube__Wing.html deleted file mode 100644 index 163469d4..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__Tube__Wing_1_1Weights__Tube__Wing.html +++ /dev/null @@ -1,323 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Weights.Weights_Tube_Wing.Weights_Tube_Wing Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Weights.Weights_Tube_Wing.Weights_Tube_Wing Class Reference
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-
-
-Inheritance diagram for SUAVE.Analyses.Weights.Weights_Tube_Wing.Weights_Tube_Wing:
-
-
- - -SUAVE.Analyses.Weights.Weights.Weights -SUAVE.Analyses.Analysis.Analysis - -
- - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def evaluate (self, conditions=None)
 
def finalize (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Weights.Weights.Weights
def __defaults__ (self)
 
def evaluate (self)
 
def finalize (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

tag
 
vehicle
 
settings
 
mass_properties
 
- Public Attributes inherited from SUAVE.Analyses.Weights.Weights.Weights
tag
 
vehicle
 
settings
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
This is class that evaluates the weight of Tube and Wing aircraft
-
-Assumptions:
-    None
-
-Source:
-    N/A
-
-Inputs:
-    None
-  
-Outputs:
-    None
-    
-Properties Used:
-     N/A
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Weights.Weights_Tube_Wing.Weights_Tube_Wing.__defaults__ ( self)
-
-
This sets the default values and methods for the tube and wing 
-aircraft weight analysis.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
-
- -

◆ evaluate()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Analyses.Weights.Weights_Tube_Wing.Weights_Tube_Wing.evaluate ( self,
 conditions = None 
)
-
-
Evaluate the weight analysis.
-    
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-results
-
-Properties Used:
-N/A
-
-
-
- -

◆ finalize()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Weights.Weights_Tube_Wing.Weights_Tube_Wing.finalize ( self)
-
-
Finalize the weight analysis.
-    
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Weights/Weights_Tube_Wing.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__Tube__Wing_1_1Weights__Tube__Wing.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__Tube__Wing_1_1Weights__Tube__Wing.js deleted file mode 100644 index c676a04d..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__Tube__Wing_1_1Weights__Tube__Wing.js +++ /dev/null @@ -1,10 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Weights_1_1Weights__Tube__Wing_1_1Weights__Tube__Wing = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights__Tube__Wing_1_1Weights__Tube__Wing.html#a0ac33c072e13422a12ecdbb92c7852d9", null ], - [ "evaluate", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights__Tube__Wing_1_1Weights__Tube__Wing.html#ad35348c45018dccd149502cb3fc6f651", null ], - [ "finalize", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights__Tube__Wing_1_1Weights__Tube__Wing.html#a63e58bfa4de1fba841192378ad8ddf66", null ], - [ "mass_properties", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights__Tube__Wing_1_1Weights__Tube__Wing.html#a759f242a10f3e0a4290a8dbc55321508", null ], - [ "settings", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights__Tube__Wing_1_1Weights__Tube__Wing.html#aabb5d1da81c78511840076358db78a6f", null ], - [ "tag", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights__Tube__Wing_1_1Weights__Tube__Wing.html#a51e51ed65132fc1b36d5c05b184d18e6", null ], - [ "vehicle", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights__Tube__Wing_1_1Weights__Tube__Wing.html#af64e9c01c287f9ede9b477893a0f0cd8", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__Tube__Wing_1_1Weights__Tube__Wing.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__Tube__Wing_1_1Weights__Tube__Wing.png deleted file mode 100644 index 6ac4fb5e..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__Tube__Wing_1_1Weights__Tube__Wing.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__UAV_1_1Weights__UAV-members.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__UAV_1_1Weights__UAV-members.html deleted file mode 100644 index a7ee0388..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__UAV_1_1Weights__UAV-members.html +++ /dev/null @@ -1,126 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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- - - - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__UAV_1_1Weights__UAV.html b/_site/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__UAV_1_1Weights__UAV.html deleted file mode 100644 index d10c8283..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__UAV_1_1Weights__UAV.html +++ /dev/null @@ -1,322 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Weights.Weights_UAV.Weights_UAV Class Reference - - - - - - - - - - - - - - - -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Analyses.Weights.Weights_UAV.Weights_UAV Class Reference
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-Inheritance diagram for SUAVE.Analyses.Weights.Weights_UAV.Weights_UAV:
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- - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def evaluate (self, conditions=None)
 
def finalize (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Weights.Weights.Weights
def __defaults__ (self)
 
def evaluate (self)
 
def finalize (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

tag
 
vehicle
 
settings
 
mass_properties
 
- Public Attributes inherited from SUAVE.Analyses.Weights.Weights.Weights
tag
 
vehicle
 
settings
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
This is class that evaluates the weight of a UAV
-
-Assumptions:
-    None
-
-Source:
-    N/A
-
-Inputs:
-    None
-  
-Outputs:
-    None
-
-Properties Used:
-    N/A
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Weights.Weights_UAV.Weights_UAV.__defaults__ ( self)
-
-
This sets the default values and methods for the UAV weight analysis.
-    
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
-
- -

◆ evaluate()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Analyses.Weights.Weights_UAV.Weights_UAV.evaluate ( self,
 conditions = None 
)
-
-
Evaluate the weight analysis.
-    
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-results
-
-Properties Used:
-N/A
-
-
-
- -

◆ finalize()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Weights.Weights_UAV.Weights_UAV.finalize ( self)
-
-
Finalize the weight analysis.
-    
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Analyses/Weights/Weights_UAV.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__UAV_1_1Weights__UAV.js b/_site/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__UAV_1_1Weights__UAV.js deleted file mode 100644 index 59cb0230..00000000 --- a/_site/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__UAV_1_1Weights__UAV.js +++ /dev/null @@ -1,10 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Weights_1_1Weights__UAV_1_1Weights__UAV = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights__UAV_1_1Weights__UAV.html#aab27bc0adcb4cef4b858359180f446fb", null ], - [ "evaluate", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights__UAV_1_1Weights__UAV.html#a024fb6f0e56a5f8ed417c66dc8f03da1", null ], - [ "finalize", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights__UAV_1_1Weights__UAV.html#a9b0a34e0576380cea29e321b7457633b", null ], - [ "mass_properties", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights__UAV_1_1Weights__UAV.html#a9d1b4383e0cc6e638356850d2d7c6c8b", null ], - [ "settings", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights__UAV_1_1Weights__UAV.html#a0fdd37d1c7f22da4f19c1e74d2cfe928", null ], - [ "tag", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights__UAV_1_1Weights__UAV.html#ad48a29ba78115b5a6f32b759ce5ddd39", null ], - [ "vehicle", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights__UAV_1_1Weights__UAV.html#ac1e4b37a1a54b147233300cdba8b07f3", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__UAV_1_1Weights__UAV.png b/_site/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__UAV_1_1Weights__UAV.png deleted file mode 100644 index 0f671fb2..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__UAV_1_1Weights__UAV.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Airports_1_1Airport_1_1Airport-members.html b/_site/doxygen/classSUAVE_1_1Attributes_1_1Airports_1_1Airport_1_1Airport-members.html deleted file mode 100644 index 2e85dc1f..00000000 --- a/_site/doxygen/classSUAVE_1_1Attributes_1_1Airports_1_1Airport_1_1Airport-members.html +++ /dev/null @@ -1,117 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Attributes.Airports.Airport.Airport Class Reference
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-Public Member Functions

def __defaults__ (self)
 
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-Public Attributes

tag
 
altitude
 
atmosphere
 
delta_isa
 
-

Detailed Description

-
A basic airport.
-
-Assumptions:
-None
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-Source:
-None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Attributes.Airports.Airport.Airport.__defaults__ ( self)
-
-
This sets the default values.
-    
-Assumptions:
-None
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-Source:
-N/A
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-Inputs:
-None
-
-Outputs:
-None
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-Properties Used:
-None
-
-
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The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Attributes/Airports/Airport.py
  • -
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Airports_1_1Airport_1_1Airport.js b/_site/doxygen/classSUAVE_1_1Attributes_1_1Airports_1_1Airport_1_1Airport.js deleted file mode 100644 index 202b2d90..00000000 --- a/_site/doxygen/classSUAVE_1_1Attributes_1_1Airports_1_1Airport_1_1Airport.js +++ /dev/null @@ -1,8 +0,0 @@ -var classSUAVE_1_1Attributes_1_1Airports_1_1Airport_1_1Airport = -[ - [ "__defaults__", "classSUAVE_1_1Attributes_1_1Airports_1_1Airport_1_1Airport.html#a87751519698b56e2366bf388d21052d1", null ], - [ "altitude", "classSUAVE_1_1Attributes_1_1Airports_1_1Airport_1_1Airport.html#afeb3e603029ff1b68262205550dfd4aa", null ], - [ "atmosphere", "classSUAVE_1_1Attributes_1_1Airports_1_1Airport_1_1Airport.html#a67a9bede56cdd73aa673e5a1b36f7790", null ], - [ "delta_isa", "classSUAVE_1_1Attributes_1_1Airports_1_1Airport_1_1Airport.html#a62abe14755e7944ad08f587861c17452", null ], - [ "tag", "classSUAVE_1_1Attributes_1_1Airports_1_1Airport_1_1Airport.html#a1cf3dc8bf593783283bf1a807385fb31", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Airports_1_1Airport_1_1Airport.png b/_site/doxygen/classSUAVE_1_1Attributes_1_1Airports_1_1Airport_1_1Airport.png deleted file mode 100644 index 9a565781..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Attributes_1_1Airports_1_1Airport_1_1Airport.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Airports_1_1Runway_1_1Runway-members.html b/_site/doxygen/classSUAVE_1_1Attributes_1_1Airports_1_1Runway_1_1Runway-members.html deleted file mode 100644 index 1c2b5cbf..00000000 --- a/_site/doxygen/classSUAVE_1_1Attributes_1_1Airports_1_1Runway_1_1Runway-members.html +++ /dev/null @@ -1,114 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Attributes.Airports.Runway.Runway Member List
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SUAVE.Attributes.Airports.Runway.Runway Class Reference
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-Public Member Functions

def __defaults__ (self)
 
- - - -

-Public Attributes

tag
 
-

Detailed Description

-
A basic runway.
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-Assumptions:
-None
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-None
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Member Function Documentation

- -

◆ __defaults__()

- -
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def SUAVE.Attributes.Airports.Runway.Runway.__defaults__ ( self)
-
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This sets the default values.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Attributes/Airports/Runway.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Airports_1_1Runway_1_1Runway.js b/_site/doxygen/classSUAVE_1_1Attributes_1_1Airports_1_1Runway_1_1Runway.js deleted file mode 100644 index 510affb2..00000000 --- a/_site/doxygen/classSUAVE_1_1Attributes_1_1Airports_1_1Runway_1_1Runway.js +++ /dev/null @@ -1,5 +0,0 @@ -var classSUAVE_1_1Attributes_1_1Airports_1_1Runway_1_1Runway = -[ - [ "__defaults__", "classSUAVE_1_1Attributes_1_1Airports_1_1Runway_1_1Runway.html#a952b090516a9563fc9f040c891493737", null ], - [ "tag", "classSUAVE_1_1Attributes_1_1Airports_1_1Runway_1_1Runway.html#a90f4ba576b4d5091fb0ce8caf86bf9e3", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Airports_1_1Runway_1_1Runway.png b/_site/doxygen/classSUAVE_1_1Attributes_1_1Airports_1_1Runway_1_1Runway.png deleted file mode 100644 index b6a7bc2d..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Attributes_1_1Airports_1_1Runway_1_1Runway.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Atmospheres_1_1Atmosphere_1_1Atmosphere-members.html b/_site/doxygen/classSUAVE_1_1Attributes_1_1Atmospheres_1_1Atmosphere_1_1Atmosphere-members.html deleted file mode 100644 index 3ac25d98..00000000 --- a/_site/doxygen/classSUAVE_1_1Attributes_1_1Atmospheres_1_1Atmosphere_1_1Atmosphere-members.html +++ /dev/null @@ -1,115 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Attributes.Atmospheres.Atmosphere.Atmosphere Member List
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Attributes.Atmospheres.Atmosphere.Atmosphere Class Reference
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-Inheritance diagram for SUAVE.Attributes.Atmospheres.Atmosphere.Atmosphere:
-
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- - -SUAVE.Attributes.Atmospheres.Earth.Constant_Temperature.Constant_Temperature -SUAVE.Attributes.Atmospheres.Earth.US_Standard_1976.US_Standard_1976 - -
- - - - -

-Public Member Functions

def __defaults__ (self)
 
- - - - - -

-Public Attributes

tag
 
composition
 
-

Detailed Description

-
The base atmosphere class.
-
-Assumptions:
-None
-
-Source:
-None
-

Member Function Documentation

- -

◆ __defaults__()

- -
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def SUAVE.Attributes.Atmospheres.Atmosphere.Atmosphere.__defaults__ ( self)
-
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This sets the default values.
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-Assumptions:
-None
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-Source:
-N/A
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-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-None
-
-
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The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Attributes/Atmospheres/Atmosphere.py
  • -
-
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Atmospheres_1_1Atmosphere_1_1Atmosphere.js b/_site/doxygen/classSUAVE_1_1Attributes_1_1Atmospheres_1_1Atmosphere_1_1Atmosphere.js deleted file mode 100644 index 5ee57275..00000000 --- a/_site/doxygen/classSUAVE_1_1Attributes_1_1Atmospheres_1_1Atmosphere_1_1Atmosphere.js +++ /dev/null @@ -1,6 +0,0 @@ -var classSUAVE_1_1Attributes_1_1Atmospheres_1_1Atmosphere_1_1Atmosphere = -[ - [ "__defaults__", "classSUAVE_1_1Attributes_1_1Atmospheres_1_1Atmosphere_1_1Atmosphere.html#a9d8a5f30feab5db53614da2d28119934", null ], - [ "composition", "classSUAVE_1_1Attributes_1_1Atmospheres_1_1Atmosphere_1_1Atmosphere.html#a8171df94869d5bcfe0fe1dca1b8ea45a", null ], - [ "tag", "classSUAVE_1_1Attributes_1_1Atmospheres_1_1Atmosphere_1_1Atmosphere.html#a290b17de8364ac83049dc3a96235a6a7", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Atmospheres_1_1Atmosphere_1_1Atmosphere.png b/_site/doxygen/classSUAVE_1_1Attributes_1_1Atmospheres_1_1Atmosphere_1_1Atmosphere.png deleted file mode 100644 index 53aa924f..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Attributes_1_1Atmospheres_1_1Atmosphere_1_1Atmosphere.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Atmospheres_1_1Earth_1_1Constant__Temperature_1_1Constant__Temperature-members.html b/_site/doxygen/classSUAVE_1_1Attributes_1_1Atmospheres_1_1Earth_1_1Constant__Temperature_1_1Constant__Temperature-members.html deleted file mode 100644 index 5559a4bf..00000000 --- a/_site/doxygen/classSUAVE_1_1Attributes_1_1Atmospheres_1_1Earth_1_1Constant__Temperature_1_1Constant__Temperature-members.html +++ /dev/null @@ -1,118 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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- - - - - - diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Atmospheres_1_1Earth_1_1Constant__Temperature_1_1Constant__Temperature.html b/_site/doxygen/classSUAVE_1_1Attributes_1_1Atmospheres_1_1Earth_1_1Constant__Temperature_1_1Constant__Temperature.html deleted file mode 100644 index 53d4aa36..00000000 --- a/_site/doxygen/classSUAVE_1_1Attributes_1_1Atmospheres_1_1Earth_1_1Constant__Temperature_1_1Constant__Temperature.html +++ /dev/null @@ -1,197 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Attributes.Atmospheres.Earth.Constant_Temperature.Constant_Temperature Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Attributes.Atmospheres.Earth.Constant_Temperature.Constant_Temperature Class Reference
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-Inheritance diagram for SUAVE.Attributes.Atmospheres.Earth.Constant_Temperature.Constant_Temperature:
-
-
- - -SUAVE.Attributes.Atmospheres.Atmosphere.Atmosphere - -
- - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Attributes.Atmospheres.Atmosphere.Atmosphere
def __defaults__ (self)
 
- - - - - - - - - - - - -

-Public Attributes

fluid_properties
 
planet
 
breaks
 
- Public Attributes inherited from SUAVE.Attributes.Atmospheres.Atmosphere.Atmosphere
tag
 
composition
 
-

Detailed Description

-
Contains US Standard 1976 values with temperature modified to be constant.
-
-Assumptions:
-Constant temperature
-
-Source:
-U.S. Standard Atmosphere (1976 version)
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Attributes.Atmospheres.Earth.Constant_Temperature.Constant_Temperature.__defaults__ ( self)
-
-
This sets the default values at breaks in the atmosphere.
-
-Assumptions:
-Constant temperature
-
-Source:
-U.S. Standard Atmosphere (1976 version)
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Attributes/Atmospheres/Earth/Constant_Temperature.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Atmospheres_1_1Earth_1_1Constant__Temperature_1_1Constant__Temperature.js b/_site/doxygen/classSUAVE_1_1Attributes_1_1Atmospheres_1_1Earth_1_1Constant__Temperature_1_1Constant__Temperature.js deleted file mode 100644 index f96d2399..00000000 --- a/_site/doxygen/classSUAVE_1_1Attributes_1_1Atmospheres_1_1Earth_1_1Constant__Temperature_1_1Constant__Temperature.js +++ /dev/null @@ -1,7 +0,0 @@ -var classSUAVE_1_1Attributes_1_1Atmospheres_1_1Earth_1_1Constant__Temperature_1_1Constant__Temperature = -[ - [ "__defaults__", "classSUAVE_1_1Attributes_1_1Atmospheres_1_1Earth_1_1Constant__Temperature_1_1Constant__Temperature.html#a92622bef320a1c81d3af37c7596f6c1d", null ], - [ "breaks", "classSUAVE_1_1Attributes_1_1Atmospheres_1_1Earth_1_1Constant__Temperature_1_1Constant__Temperature.html#a38e7bf852e905f3fb8fe792a17fb214a", null ], - [ "fluid_properties", "classSUAVE_1_1Attributes_1_1Atmospheres_1_1Earth_1_1Constant__Temperature_1_1Constant__Temperature.html#ae1c49eaf59f3dab65e6765b11db601b2", null ], - [ "planet", "classSUAVE_1_1Attributes_1_1Atmospheres_1_1Earth_1_1Constant__Temperature_1_1Constant__Temperature.html#affc343bce9f9d20caed0a663c773eb36", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Atmospheres_1_1Earth_1_1Constant__Temperature_1_1Constant__Temperature.png b/_site/doxygen/classSUAVE_1_1Attributes_1_1Atmospheres_1_1Earth_1_1Constant__Temperature_1_1Constant__Temperature.png deleted file mode 100644 index 7bcc76a3..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Attributes_1_1Atmospheres_1_1Earth_1_1Constant__Temperature_1_1Constant__Temperature.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Atmospheres_1_1Earth_1_1US__Standard__1976_1_1US__Standard__1976-members.html b/_site/doxygen/classSUAVE_1_1Attributes_1_1Atmospheres_1_1Earth_1_1US__Standard__1976_1_1US__Standard__1976-members.html deleted file mode 100644 index 9d6fceb2..00000000 --- a/_site/doxygen/classSUAVE_1_1Attributes_1_1Atmospheres_1_1Earth_1_1US__Standard__1976_1_1US__Standard__1976-members.html +++ /dev/null @@ -1,118 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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- - - - - - diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Atmospheres_1_1Earth_1_1US__Standard__1976_1_1US__Standard__1976.html b/_site/doxygen/classSUAVE_1_1Attributes_1_1Atmospheres_1_1Earth_1_1US__Standard__1976_1_1US__Standard__1976.html deleted file mode 100644 index 57682987..00000000 --- a/_site/doxygen/classSUAVE_1_1Attributes_1_1Atmospheres_1_1Earth_1_1US__Standard__1976_1_1US__Standard__1976.html +++ /dev/null @@ -1,200 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Attributes.Atmospheres.Earth.US_Standard_1976.US_Standard_1976 Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Attributes.Atmospheres.Earth.US_Standard_1976.US_Standard_1976 Class Reference
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-Inheritance diagram for SUAVE.Attributes.Atmospheres.Earth.US_Standard_1976.US_Standard_1976:
-
-
- - -SUAVE.Attributes.Atmospheres.Atmosphere.Atmosphere - -
- - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Attributes.Atmospheres.Atmosphere.Atmosphere
def __defaults__ (self)
 
- - - - - - - - - - - - - - -

-Public Attributes

tag
 
fluid_properties
 
planet
 
breaks
 
- Public Attributes inherited from SUAVE.Attributes.Atmospheres.Atmosphere.Atmosphere
tag
 
composition
 
-

Detailed Description

-
Contains US Standard 1976 values.
-
-Assumptions:
-None
-
-Source:
-U.S. Standard Atmosphere (1976 version)
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Attributes.Atmospheres.Earth.US_Standard_1976.US_Standard_1976.__defaults__ ( self)
-
-
This sets the default values at breaks in the atmosphere.
-
-Assumptions:
-None
-
-Source:
-U.S. Standard Atmosphere (1976 version)
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Attributes/Atmospheres/Earth/US_Standard_1976.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Atmospheres_1_1Earth_1_1US__Standard__1976_1_1US__Standard__1976.js b/_site/doxygen/classSUAVE_1_1Attributes_1_1Atmospheres_1_1Earth_1_1US__Standard__1976_1_1US__Standard__1976.js deleted file mode 100644 index d5c50b1e..00000000 --- a/_site/doxygen/classSUAVE_1_1Attributes_1_1Atmospheres_1_1Earth_1_1US__Standard__1976_1_1US__Standard__1976.js +++ /dev/null @@ -1,8 +0,0 @@ -var classSUAVE_1_1Attributes_1_1Atmospheres_1_1Earth_1_1US__Standard__1976_1_1US__Standard__1976 = -[ - [ "__defaults__", "classSUAVE_1_1Attributes_1_1Atmospheres_1_1Earth_1_1US__Standard__1976_1_1US__Standard__1976.html#ac126d272ade6b9e6cdf4676fa1a74481", null ], - [ "breaks", "classSUAVE_1_1Attributes_1_1Atmospheres_1_1Earth_1_1US__Standard__1976_1_1US__Standard__1976.html#a1f5d0138162f34940d6c70708f60ec3d", null ], - [ "fluid_properties", "classSUAVE_1_1Attributes_1_1Atmospheres_1_1Earth_1_1US__Standard__1976_1_1US__Standard__1976.html#aafe591a742dabc7c30eb0102e36e0e6f", null ], - [ "planet", "classSUAVE_1_1Attributes_1_1Atmospheres_1_1Earth_1_1US__Standard__1976_1_1US__Standard__1976.html#a1d06e1096c3fd570851ab5d70c85842a", null ], - [ "tag", "classSUAVE_1_1Attributes_1_1Atmospheres_1_1Earth_1_1US__Standard__1976_1_1US__Standard__1976.html#a282283c9824da8bfaabc7fb112ef47a5", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Atmospheres_1_1Earth_1_1US__Standard__1976_1_1US__Standard__1976.png b/_site/doxygen/classSUAVE_1_1Attributes_1_1Atmospheres_1_1Earth_1_1US__Standard__1976_1_1US__Standard__1976.png deleted file mode 100644 index 1154bfd3..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Attributes_1_1Atmospheres_1_1Earth_1_1US__Standard__1976_1_1US__Standard__1976.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Constants_1_1Composition_1_1Composition-members.html b/_site/doxygen/classSUAVE_1_1Attributes_1_1Constants_1_1Composition_1_1Composition-members.html deleted file mode 100644 index 281cc390..00000000 --- a/_site/doxygen/classSUAVE_1_1Attributes_1_1Constants_1_1Composition_1_1Composition-members.html +++ /dev/null @@ -1,115 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Attributes.Constants.Composition.Composition Member List
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Attributes.Constants.Composition.Composition Class Reference
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-Inheritance diagram for SUAVE.Attributes.Constants.Composition.Composition:
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-Public Member Functions

def __defaults__ (self)
 
def __check__ (self)
 
- Public Member Functions inherited from SUAVE.Attributes.Constants.Constant.Constant
def __defaults__ (self)
 
- - - -

-Public Attributes

Other
 
-

Detailed Description

-
A container to store chemical compositions.
-
-Assumptions:
-None
-
-Source:
-None
-

Member Function Documentation

- -

◆ __check__()

- -
-
- - - - - - - - -
def SUAVE.Attributes.Constants.Composition.Composition.__check__ ( self)
-
-
Checks that the composition values sum to 1.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-self.values       [-]
-self.Other        [-] (optional)
-
-
-
- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Attributes.Constants.Composition.Composition.__defaults__ ( self)
-
-
This sets the default values (just a pass here).
-    
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Attributes/Constants/Composition.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Constants_1_1Composition_1_1Composition.js b/_site/doxygen/classSUAVE_1_1Attributes_1_1Constants_1_1Composition_1_1Composition.js deleted file mode 100644 index bf19ae53..00000000 --- a/_site/doxygen/classSUAVE_1_1Attributes_1_1Constants_1_1Composition_1_1Composition.js +++ /dev/null @@ -1,6 +0,0 @@ -var classSUAVE_1_1Attributes_1_1Constants_1_1Composition_1_1Composition = -[ - [ "__check__", "classSUAVE_1_1Attributes_1_1Constants_1_1Composition_1_1Composition.html#a0e2d715388e03fa0fbf6d040f94cc539", null ], - [ "__defaults__", "classSUAVE_1_1Attributes_1_1Constants_1_1Composition_1_1Composition.html#ac911ebb7c1f208a92274a87a8f4216f0", null ], - [ "Other", "classSUAVE_1_1Attributes_1_1Constants_1_1Composition_1_1Composition.html#a27849489fdfdc856ccd68b242b071315", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Constants_1_1Composition_1_1Composition.png b/_site/doxygen/classSUAVE_1_1Attributes_1_1Constants_1_1Composition_1_1Composition.png deleted file mode 100644 index 041c92d8..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Attributes_1_1Constants_1_1Composition_1_1Composition.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Constants_1_1Constant_1_1Constant-members.html b/_site/doxygen/classSUAVE_1_1Attributes_1_1Constants_1_1Constant_1_1Constant-members.html deleted file mode 100644 index 9016246e..00000000 --- a/_site/doxygen/classSUAVE_1_1Attributes_1_1Constants_1_1Constant_1_1Constant-members.html +++ /dev/null @@ -1,113 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Attributes.Constants.Constant.Constant Member List
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__defaults__(self)SUAVE.Attributes.Constants.Constant.Constant
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Constants_1_1Constant_1_1Constant.html b/_site/doxygen/classSUAVE_1_1Attributes_1_1Constants_1_1Constant_1_1Constant.html deleted file mode 100644 index 844f2ac4..00000000 --- a/_site/doxygen/classSUAVE_1_1Attributes_1_1Constants_1_1Constant_1_1Constant.html +++ /dev/null @@ -1,177 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Attributes.Constants.Constant.Constant Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Attributes.Constants.Constant.Constant Class Reference
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-Inheritance diagram for SUAVE.Attributes.Constants.Constant.Constant:
-
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- - -SUAVE.Attributes.Constants.Composition.Composition -SUAVE.Attributes.Planets.Planet.Planet -SUAVE.Attributes.Planets.Earth.Earth -SUAVE.Attributes.Planets.Mars.Mars - -
- - - - -

-Public Member Functions

def __defaults__ (self)
 
-

Detailed Description

-
A container for constant values.
-
-Assumptions:
-None
-
-Source:
-None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Attributes.Constants.Constant.Constant.__defaults__ ( self)
-
-
This sets the default values (just a pass here).
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
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-Outputs:
-None
-
-Properties Used:
-None
-
-
-
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The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Attributes/Constants/Constant.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Constants_1_1Constant_1_1Constant.js b/_site/doxygen/classSUAVE_1_1Attributes_1_1Constants_1_1Constant_1_1Constant.js deleted file mode 100644 index 7583d284..00000000 --- a/_site/doxygen/classSUAVE_1_1Attributes_1_1Constants_1_1Constant_1_1Constant.js +++ /dev/null @@ -1,4 +0,0 @@ -var classSUAVE_1_1Attributes_1_1Constants_1_1Constant_1_1Constant = -[ - [ "__defaults__", "classSUAVE_1_1Attributes_1_1Constants_1_1Constant_1_1Constant.html#a33bb2df4428cdbd5d9ceda90b30055fb", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Constants_1_1Constant_1_1Constant.png b/_site/doxygen/classSUAVE_1_1Attributes_1_1Constants_1_1Constant_1_1Constant.png deleted file mode 100644 index f4fef294..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Attributes_1_1Constants_1_1Constant_1_1Constant.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Constants_1_1Constant_1_1Container-members.html b/_site/doxygen/classSUAVE_1_1Attributes_1_1Constants_1_1Constant_1_1Container-members.html deleted file mode 100644 index 60da855c..00000000 --- a/_site/doxygen/classSUAVE_1_1Attributes_1_1Constants_1_1Constant_1_1Container-members.html +++ /dev/null @@ -1,113 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Attributes.Constants.Constant.Container Member List
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This is the complete list of members for SUAVE.Attributes.Constants.Constant.Container, including all inherited members.

- - -
Container (defined in SUAVE.Attributes.Constants.Constant.Container)SUAVE.Attributes.Constants.Constant.Containerstatic
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Constants_1_1Constant_1_1Container.html b/_site/doxygen/classSUAVE_1_1Attributes_1_1Constants_1_1Constant_1_1Container.html deleted file mode 100644 index 57ceb886..00000000 --- a/_site/doxygen/classSUAVE_1_1Attributes_1_1Constants_1_1Constant_1_1Container.html +++ /dev/null @@ -1,139 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Attributes.Constants.Constant.Container Class Reference - - - - - - - - - - - - - - - -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Attributes.Constants.Constant.Container Class Reference
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-
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- - - - -

-Static Public Attributes

Container
 
-

Detailed Description

-
A subcontainer for constant values.
-
-Assumptions:
-None
-
-Source:
-None
-

The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Attributes/Constants/Constant.py
  • -
-
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Constants_1_1Constant_1_1Container.png b/_site/doxygen/classSUAVE_1_1Attributes_1_1Constants_1_1Constant_1_1Container.png deleted file mode 100644 index 5e7c3d56..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Attributes_1_1Constants_1_1Constant_1_1Container.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1Air_1_1Air-members.html b/_site/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1Air_1_1Air-members.html deleted file mode 100644 index c21c7bad..00000000 --- a/_site/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1Air_1_1Air-members.html +++ /dev/null @@ -1,122 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Attributes.Gases.Air.Air Member List
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This is the complete list of members for SUAVE.Attributes.Gases.Air.Air, including all inherited members.

- - - - - - - - - - - -
__defaults__(self)SUAVE.Attributes.Gases.Air.Air
composition (defined in SUAVE.Attributes.Gases.Gas.Gas)SUAVE.Attributes.Gases.Gas.Gas
compute_absolute_viscosity(self, T=300., p=101325.)SUAVE.Attributes.Gases.Air.Air
compute_cp(self, T=300., p=101325.)SUAVE.Attributes.Gases.Air.Air
compute_cv(self, T=300., p=101325.)SUAVE.Attributes.Gases.Air.Air
compute_density(self, T=300., p=101325.)SUAVE.Attributes.Gases.Air.Air
compute_gamma(self, T=300., p=101325.)SUAVE.Attributes.Gases.Air.Air
compute_speed_of_sound(self, T=300., p=101325., variable_gamma=False)SUAVE.Attributes.Gases.Air.Air
gas_specific_constant (defined in SUAVE.Attributes.Gases.Air.Air)SUAVE.Attributes.Gases.Air.Air
molecular_mass (defined in SUAVE.Attributes.Gases.Air.Air)SUAVE.Attributes.Gases.Air.Air
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1Air_1_1Air.html b/_site/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1Air_1_1Air.html deleted file mode 100644 index 66cf2b50..00000000 --- a/_site/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1Air_1_1Air.html +++ /dev/null @@ -1,521 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Attributes.Gases.Air.Air Class Reference - - - - - - - - - - - - - - - -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Attributes.Gases.Air.Air Class Reference
-
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-Inheritance diagram for SUAVE.Attributes.Gases.Air.Air:
-
-
- - -SUAVE.Attributes.Gases.Gas.Gas - -
- - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def compute_density (self, T=300., p=101325.)
 
def compute_speed_of_sound (self, T=300., p=101325., variable_gamma=False)
 
def compute_cv (self, T=300., p=101325.)
 
def compute_cp (self, T=300., p=101325.)
 
def compute_gamma (self, T=300., p=101325.)
 
def compute_absolute_viscosity (self, T=300., p=101325.)
 
- Public Member Functions inherited from SUAVE.Attributes.Gases.Gas.Gas
def __defaults__ (self)
 
- - - - - - - - - - - - -

-Public Attributes

molecular_mass
 
gas_specific_constant
 
- Public Attributes inherited from SUAVE.Attributes.Gases.Gas.Gas
molecular_mass
 
gas_specific_constant
 
composition
 
-

Detailed Description

-
Holds constants and functions that compute gas properties for air.
-
-Assumptions:
-None
-
-Source:
-None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Attributes.Gases.Air.Air.__defaults__ ( self)
-
-
This sets the default values.
-
-Assumptions:
-None
-
-Source:
-Values commonly available
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-None
-
-
-
- -

◆ compute_absolute_viscosity()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Attributes.Gases.Air.Air.compute_absolute_viscosity ( self,
 T = 300.,
 p = 101325. 
)
-
-
Compute the absolute (dynamic) viscosity
-    
-Assumptions:
-Ideal gas
-
-Source:
-https://www.cfd-online.com/Wiki/Sutherland's_law
-
-Inputs:
-T                  [K]       - Temperature
-
-Outputs:
-absolute viscosity [kg/(m-s)]
-
-Properties Used:
-None
-
-
-
- -

◆ compute_cp()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Attributes.Gases.Air.Air.compute_cp ( self,
 T = 300.,
 p = 101325. 
)
-
-
Computes Cp by 3rd-order polynomial data fit:
-cp(T) = c1*T^3 + c2*T^2 + c3*T + c4
-
-Coefficients (with 95% confidence bounds):
-c1 = -7.357e-007  (-9.947e-007, -4.766e-007)
-c2 =    0.001307  (0.0009967, 0.001617)
-c3 =     -0.5558  (-0.6688, -0.4429)
-c4 =        1074  (1061, 1086) 
-    
-Assumptions:
-123 K < T < 673 K 
-
-Source:
-Unknown, possibly Combustion Technologies for a Clean Environment 
-(Energy, Combustion and the Environment), Jun 15, 1995, Carvalhoc
-
-Inputs:
-T              [K]       - Temperature
-p              [Pa]      - Pressure
-
-Outputs:
-cp             [J/kg-K]
-
-Properties Used:
-None
-
-
-
- -

◆ compute_cv()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Attributes.Gases.Air.Air.compute_cv ( self,
 T = 300.,
 p = 101325. 
)
-
-
Stub for computing Cv - not functional
-
-
-
- -

◆ compute_density()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Attributes.Gases.Air.Air.compute_density ( self,
 T = 300.,
 p = 101325. 
)
-
-
Computes air density given temperature and pressure
-
-Assumptions:
-Ideal gas
-
-Source:
-Common equation
-
-Inputs:
-T         [K]  - Temperature
-p         [Pa] - Pressure
-
-Outputs:
-density   [kg/m^3]
-
-Properties Used:
-self.gas_specific_constant
-
-
-
- -

◆ compute_gamma()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Attributes.Gases.Air.Air.compute_gamma ( self,
 T = 300.,
 p = 101325. 
)
-
-
Computes Cp by 3rd-order polynomial data fit:
-gamma(T) = c1*T^3 + c2*T^2 + c3*T + c4
-
-Coefficients (with 95% confidence bounds):
-c1 =  1.629e-010  (1.486e-010, 1.773e-010)
-c2 = -3.588e-007  (-3.901e-007, -3.274e-007)
-c3 =   0.0001418  (0.0001221, 0.0001614)
-c4 =       1.386  (1.382, 1.389)
-    
-Assumptions:
-233 K < T < 1273 K 
-
-Source:
-Unknown
-
-Inputs:
-T              [K]       - Temperature
-p              [Pa]      - Pressure
-
-Outputs:
-g              [-]
-
-Properties Used:
-None
-
-
-
- -

◆ compute_speed_of_sound()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Attributes.Gases.Air.Air.compute_speed_of_sound ( self,
 T = 300.,
 p = 101325.,
 variable_gamma = False 
)
-
-
Computes speed of sound given temperature and pressure
-
-Assumptions:
-Ideal gas with gamma = 1.4 if variable gamma is False
-
-Source:
-Common equation
-
-Inputs:
-T              [K]       - Temperature
-p              [Pa]      - Pressure
-variable_gamma <boolean> - Determines if gamma is computed
-
-Outputs:
-speed of sound [m/s]
-
-Properties Used:
-self.compute_gamma() (if variable gamma is True)
-self.gas_specific_constant
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Attributes/Gases/Air.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1Air_1_1Air.js b/_site/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1Air_1_1Air.js deleted file mode 100644 index fafe9b98..00000000 --- a/_site/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1Air_1_1Air.js +++ /dev/null @@ -1,12 +0,0 @@ -var classSUAVE_1_1Attributes_1_1Gases_1_1Air_1_1Air = -[ - [ "__defaults__", "classSUAVE_1_1Attributes_1_1Gases_1_1Air_1_1Air.html#a68ef4a3c510f1d378e614fe517044451", null ], - [ "compute_absolute_viscosity", "classSUAVE_1_1Attributes_1_1Gases_1_1Air_1_1Air.html#a01a524cdc8c8032501ff41f2a2679407", null ], - [ "compute_cp", "classSUAVE_1_1Attributes_1_1Gases_1_1Air_1_1Air.html#af2049f5193f71254180aa25263b253a9", null ], - [ "compute_cv", "classSUAVE_1_1Attributes_1_1Gases_1_1Air_1_1Air.html#a41d259545d5fbdaae61ab22b2afbde71", null ], - [ "compute_density", "classSUAVE_1_1Attributes_1_1Gases_1_1Air_1_1Air.html#a7e7724b5a0f3b55f1d22207de5eb95c3", null ], - [ "compute_gamma", "classSUAVE_1_1Attributes_1_1Gases_1_1Air_1_1Air.html#a30b8f6bcf3ad36115e67d482ec406602", null ], - [ "compute_speed_of_sound", "classSUAVE_1_1Attributes_1_1Gases_1_1Air_1_1Air.html#a86d93dc502a49cdf39a1d8f063021776", null ], - [ "gas_specific_constant", "classSUAVE_1_1Attributes_1_1Gases_1_1Air_1_1Air.html#a971ac13cf64d6a8c4e5e184e3cee8666", null ], - [ "molecular_mass", "classSUAVE_1_1Attributes_1_1Gases_1_1Air_1_1Air.html#afb2bd7b10f13b0aa8d9a1fd2b78d9309", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1Air_1_1Air.png b/_site/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1Air_1_1Air.png deleted file mode 100644 index 24f66e3d..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1Air_1_1Air.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1CO2_1_1CO2-members.html b/_site/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1CO2_1_1CO2-members.html deleted file mode 100644 index 5a5bb344..00000000 --- a/_site/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1CO2_1_1CO2-members.html +++ /dev/null @@ -1,116 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Attributes.Gases.CO2.CO2 Member List
-
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- -

This is the complete list of members for SUAVE.Attributes.Gases.CO2.CO2, including all inherited members.

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__defaults__(self)SUAVE.Attributes.Gases.CO2.CO2
composition (defined in SUAVE.Attributes.Gases.Gas.Gas)SUAVE.Attributes.Gases.Gas.Gas
gas_specific_constant (defined in SUAVE.Attributes.Gases.CO2.CO2)SUAVE.Attributes.Gases.CO2.CO2
molecular_mass (defined in SUAVE.Attributes.Gases.CO2.CO2)SUAVE.Attributes.Gases.CO2.CO2
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1CO2_1_1CO2.html b/_site/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1CO2_1_1CO2.html deleted file mode 100644 index 4ca8472f..00000000 --- a/_site/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1CO2_1_1CO2.html +++ /dev/null @@ -1,197 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Attributes.Gases.CO2.CO2 Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Attributes.Gases.CO2.CO2 Class Reference
-
-
-
-Inheritance diagram for SUAVE.Attributes.Gases.CO2.CO2:
-
-
- - -SUAVE.Attributes.Gases.Gas.Gas - -
- - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Attributes.Gases.Gas.Gas
def __defaults__ (self)
 
- - - - - - - - - - - - -

-Public Attributes

molecular_mass
 
gas_specific_constant
 
- Public Attributes inherited from SUAVE.Attributes.Gases.Gas.Gas
molecular_mass
 
gas_specific_constant
 
composition
 
-

Detailed Description

-
Holds constants for CO2.
- 
-Assumptions:
-None
- 
-Source:
-None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Attributes.Gases.CO2.CO2.__defaults__ ( self)
-
-
This sets the default values.
-
-Assumptions:
-None
-
-Source:
-Values commonly available
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Attributes/Gases/CO2.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1CO2_1_1CO2.js b/_site/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1CO2_1_1CO2.js deleted file mode 100644 index 4f69edc3..00000000 --- a/_site/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1CO2_1_1CO2.js +++ /dev/null @@ -1,6 +0,0 @@ -var classSUAVE_1_1Attributes_1_1Gases_1_1CO2_1_1CO2 = -[ - [ "__defaults__", "classSUAVE_1_1Attributes_1_1Gases_1_1CO2_1_1CO2.html#af5f8d34d26d75384069a564e850c26cf", null ], - [ "gas_specific_constant", "classSUAVE_1_1Attributes_1_1Gases_1_1CO2_1_1CO2.html#a2f45f35a4c6870cef5748765f10b6a95", null ], - [ "molecular_mass", "classSUAVE_1_1Attributes_1_1Gases_1_1CO2_1_1CO2.html#ac6f75e5944b60254978d9815a738d333", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1CO2_1_1CO2.png b/_site/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1CO2_1_1CO2.png deleted file mode 100644 index 19c25b54..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1CO2_1_1CO2.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1Gas_1_1Gas-members.html b/_site/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1Gas_1_1Gas-members.html deleted file mode 100644 index 85f62986..00000000 --- a/_site/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1Gas_1_1Gas-members.html +++ /dev/null @@ -1,116 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Attributes.Gases.Gas.Gas Member List
-
-
- -

This is the complete list of members for SUAVE.Attributes.Gases.Gas.Gas, including all inherited members.

- - - - - -
__defaults__(self)SUAVE.Attributes.Gases.Gas.Gas
composition (defined in SUAVE.Attributes.Gases.Gas.Gas)SUAVE.Attributes.Gases.Gas.Gas
gas_specific_constant (defined in SUAVE.Attributes.Gases.Gas.Gas)SUAVE.Attributes.Gases.Gas.Gas
molecular_mass (defined in SUAVE.Attributes.Gases.Gas.Gas)SUAVE.Attributes.Gases.Gas.Gas
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1Gas_1_1Gas.html b/_site/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1Gas_1_1Gas.html deleted file mode 100644 index 16be41c0..00000000 --- a/_site/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1Gas_1_1Gas.html +++ /dev/null @@ -1,189 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Attributes.Gases.Gas.Gas Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
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SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
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- -
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- -
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SUAVE.Attributes.Gases.Gas.Gas Class Reference
-
-
-
-Inheritance diagram for SUAVE.Attributes.Gases.Gas.Gas:
-
-
- - -SUAVE.Attributes.Gases.Air.Air -SUAVE.Attributes.Gases.CO2.CO2 -SUAVE.Attributes.Gases.Steam.Steam - -
- - - - -

-Public Member Functions

def __defaults__ (self)
 
- - - - - - - -

-Public Attributes

molecular_mass
 
gas_specific_constant
 
composition
 
-

Detailed Description

-
Base class for gases
-
-Assumptions:
-None
-
-Source:
-None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Attributes.Gases.Gas.Gas.__defaults__ ( self)
-
-
This sets the default values.
-    
-Assumptions:
-None
-    
-Source:
-N/A
-    
-Inputs:
-None
-    
-Outputs:
-None
-    
-Properties Used:
-None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Attributes/Gases/Gas.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1Gas_1_1Gas.js b/_site/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1Gas_1_1Gas.js deleted file mode 100644 index 43f40b8d..00000000 --- a/_site/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1Gas_1_1Gas.js +++ /dev/null @@ -1,7 +0,0 @@ -var classSUAVE_1_1Attributes_1_1Gases_1_1Gas_1_1Gas = -[ - [ "__defaults__", "classSUAVE_1_1Attributes_1_1Gases_1_1Gas_1_1Gas.html#a57159410d8c1a8e43da05f8faa255288", null ], - [ "composition", "classSUAVE_1_1Attributes_1_1Gases_1_1Gas_1_1Gas.html#a890da3c2d8264228bcb0ac9936d16e35", null ], - [ "gas_specific_constant", "classSUAVE_1_1Attributes_1_1Gases_1_1Gas_1_1Gas.html#a9472faacd37b54512bd462b4ec467f70", null ], - [ "molecular_mass", "classSUAVE_1_1Attributes_1_1Gases_1_1Gas_1_1Gas.html#af1a58498a684124a1bddd171eed7a8af", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1Gas_1_1Gas.png b/_site/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1Gas_1_1Gas.png deleted file mode 100644 index 66a5ac6c..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1Gas_1_1Gas.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1Steam_1_1Steam-members.html b/_site/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1Steam_1_1Steam-members.html deleted file mode 100644 index 72c09575..00000000 --- a/_site/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1Steam_1_1Steam-members.html +++ /dev/null @@ -1,122 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Attributes.Gases.Steam.Steam Member List
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Attributes.Gases.Steam.Steam Class Reference
-
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-
-Inheritance diagram for SUAVE.Attributes.Gases.Steam.Steam:
-
-
- - -SUAVE.Attributes.Gases.Gas.Gas - -
- - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def compute_density (self, T=300, p=101325)
 
def compute_speed_of_sound (self, T=300, p=101325, variable_gamma=False)
 
def compute_cv (self, T=300, p=101325)
 
def compute_cp (self, T=300, p=101325)
 
def compute_gamma (self, T=300, p=101325)
 
def compute_absolute_viscosity (self, T=300, p=101325)
 
- Public Member Functions inherited from SUAVE.Attributes.Gases.Gas.Gas
def __defaults__ (self)
 
- - - - - - - - - - - - -

-Public Attributes

molecular_mass
 
gas_specific_constant
 
- Public Attributes inherited from SUAVE.Attributes.Gases.Gas.Gas
molecular_mass
 
gas_specific_constant
 
composition
 
-

Detailed Description

-
Holds constants and functions that compute gas properties for steam.
-
-Assumptions:
-None
-
-Source:
-None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Attributes.Gases.Steam.Steam.__defaults__ ( self)
-
-
This sets the default values.
-
-Assumptions:
-None
-
-Source:
-Values commonly available
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-None
-
-
-
- -

◆ compute_absolute_viscosity()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Attributes.Gases.Steam.Steam.compute_absolute_viscosity ( self,
 T = 300,
 p = 101325 
)
-
-
Gives constant absolute viscosity of 1e-6
-WARNING: this value appears to be incorrect
-    
-Assumptions:
-Constant value
-
-Source:
-Common value
-
-Inputs:
-None
-
-Outputs:
-mu0        [kg/(m-s)]
-
-Properties Used:
-None
-
-
-
- -

◆ compute_cp()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Attributes.Gases.Steam.Steam.compute_cp ( self,
 T = 300,
 p = 101325 
)
-
-
Computes Cp by 3rd-order polynomial data fit:
-cp(T) = c1*T^3 + c2*T^2 + c3*T + c4
-    
-Assumptions:
-300 K < T < 1500 K
-
-Source:
-Unknown, possibly Combustion Technologies for a Clean Environment 
-(Energy, Combustion and the Environment), Jun 15, 1995, Carvalhoc
-
-Inputs:
-T              [K]       - Temperature
-p              [Pa]      - Pressure
-
-Outputs:
-cp             [J/kg-K]
-
-Properties Used:
-None
-
-
-
- -

◆ compute_cv()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Attributes.Gases.Steam.Steam.compute_cv ( self,
 T = 300,
 p = 101325 
)
-
-
Stub for computing Cv - not functional
-
-
-
- -

◆ compute_density()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Attributes.Gases.Steam.Steam.compute_density ( self,
 T = 300,
 p = 101325 
)
-
-
Computes air density given temperature and pressure
-
-Assumptions:
-Ideal gas
-
-Source:
-Common equation
-
-Inputs:
-T         [K]  - Temperature
-p         [Pa] - Pressure
-
-Outputs:
-density   [kg/m^3]
-
-Properties Used:
-self.gas_specific_constant
-
-
-
- -

◆ compute_gamma()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Attributes.Gases.Steam.Steam.compute_gamma ( self,
 T = 300,
 p = 101325 
)
-
-
Gives constant gamma of 1.33
-    
-Assumptions:
-233 K < T < 1273 K 
-
-Source:
-Common value
-
-Inputs:
-None
-
-Outputs:
-g              [-]
-
-Properties Used:
-None
-
-
-
- -

◆ compute_speed_of_sound()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Attributes.Gases.Steam.Steam.compute_speed_of_sound ( self,
 T = 300,
 p = 101325,
 variable_gamma = False 
)
-
-
Computes speed of sound given temperature and pressure
-
-Assumptions:
-Ideal gas with gamma = 1.33 if variable gamma is False
-
-Source:
-Common equation
-
-Inputs:
-T              [K]       - Temperature
-p              [Pa]      - Pressure
-variable_gamma <boolean> - Determines if gamma is computed
-
-Outputs:
-speed of sound [m/s]
-
-Properties Used:
-self.compute_gamma() (if variable gamma is True)
-self.gas_specific_constant
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Attributes/Gases/Steam.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1Steam_1_1Steam.js b/_site/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1Steam_1_1Steam.js deleted file mode 100644 index 309fcbac..00000000 --- a/_site/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1Steam_1_1Steam.js +++ /dev/null @@ -1,12 +0,0 @@ -var classSUAVE_1_1Attributes_1_1Gases_1_1Steam_1_1Steam = -[ - [ "__defaults__", "classSUAVE_1_1Attributes_1_1Gases_1_1Steam_1_1Steam.html#a7175c34a32620fd4799bee6c0a318c64", null ], - [ "compute_absolute_viscosity", "classSUAVE_1_1Attributes_1_1Gases_1_1Steam_1_1Steam.html#a617bf03d6569307125d9188411ff961c", null ], - [ "compute_cp", "classSUAVE_1_1Attributes_1_1Gases_1_1Steam_1_1Steam.html#a6d54b52a4fef07da7ad816a87220f6ec", null ], - [ "compute_cv", "classSUAVE_1_1Attributes_1_1Gases_1_1Steam_1_1Steam.html#ab8cf99ffa6a286f6004342fe26f2c930", null ], - [ "compute_density", "classSUAVE_1_1Attributes_1_1Gases_1_1Steam_1_1Steam.html#acc6343cdaff57cd4beb66d049443772f", null ], - [ "compute_gamma", "classSUAVE_1_1Attributes_1_1Gases_1_1Steam_1_1Steam.html#a66d54aac1e188e801ca276ca2d48fdd8", null ], - [ "compute_speed_of_sound", "classSUAVE_1_1Attributes_1_1Gases_1_1Steam_1_1Steam.html#a86ba9c1313cae71b544a4be1edf05bad", null ], - [ "gas_specific_constant", "classSUAVE_1_1Attributes_1_1Gases_1_1Steam_1_1Steam.html#ab45dc8c7c1186e41c21deb0a2ff1d82e", null ], - [ "molecular_mass", "classSUAVE_1_1Attributes_1_1Gases_1_1Steam_1_1Steam.html#a54398bd1c5ff2db7e010ce52851621b0", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1Steam_1_1Steam.png b/_site/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1Steam_1_1Steam.png deleted file mode 100644 index aa643857..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1Steam_1_1Steam.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Liquids_1_1Liquid_1_1Liquid-members.html b/_site/doxygen/classSUAVE_1_1Attributes_1_1Liquids_1_1Liquid_1_1Liquid-members.html deleted file mode 100644 index 69ee7956..00000000 --- a/_site/doxygen/classSUAVE_1_1Attributes_1_1Liquids_1_1Liquid_1_1Liquid-members.html +++ /dev/null @@ -1,118 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Attributes.Liquids.Liquid.Liquid Member List
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Attributes.Liquids.Liquid.Liquid Class Reference
-
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-Inheritance diagram for SUAVE.Attributes.Liquids.Liquid.Liquid:
-
-
- - -SUAVE.Attributes.Liquids.Water.Water - -
- - - - -

-Public Member Functions

def __defaults__ (self)
 
- - - - - - - - - - - -

-Public Attributes

molecular_mass
 
composition
 
heat_of_vaporization
 
density
 
boiling_point
 
-

Detailed Description

-
Base class for liquids
-
-Assumptions:
-None
-
-Source:
-None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Attributes.Liquids.Liquid.Liquid.__defaults__ ( self)
-
-
This sets the default values.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Attributes/Liquids/Liquid.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Liquids_1_1Liquid_1_1Liquid.js b/_site/doxygen/classSUAVE_1_1Attributes_1_1Liquids_1_1Liquid_1_1Liquid.js deleted file mode 100644 index a4c906e4..00000000 --- a/_site/doxygen/classSUAVE_1_1Attributes_1_1Liquids_1_1Liquid_1_1Liquid.js +++ /dev/null @@ -1,9 +0,0 @@ -var classSUAVE_1_1Attributes_1_1Liquids_1_1Liquid_1_1Liquid = -[ - [ "__defaults__", "classSUAVE_1_1Attributes_1_1Liquids_1_1Liquid_1_1Liquid.html#a7a914b29e3f95b7e3077924fdab26b75", null ], - [ "boiling_point", "classSUAVE_1_1Attributes_1_1Liquids_1_1Liquid_1_1Liquid.html#a12a13ffeb5bb6578b37361055d5338c2", null ], - [ "composition", "classSUAVE_1_1Attributes_1_1Liquids_1_1Liquid_1_1Liquid.html#a31ff0cf7acd5fda18cb2b60d83af9621", null ], - [ "density", "classSUAVE_1_1Attributes_1_1Liquids_1_1Liquid_1_1Liquid.html#a2d467e83e2ffebbb799f88c27acf279e", null ], - [ "heat_of_vaporization", "classSUAVE_1_1Attributes_1_1Liquids_1_1Liquid_1_1Liquid.html#a85f870a09a056ef2b1eedd43899c9a2c", null ], - [ "molecular_mass", "classSUAVE_1_1Attributes_1_1Liquids_1_1Liquid_1_1Liquid.html#a08a7c2c7a09bfda8f90e5e5a7185df2f", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Liquids_1_1Liquid_1_1Liquid.png b/_site/doxygen/classSUAVE_1_1Attributes_1_1Liquids_1_1Liquid_1_1Liquid.png deleted file mode 100644 index 50ce6562..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Attributes_1_1Liquids_1_1Liquid_1_1Liquid.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Liquids_1_1Water_1_1Water-members.html b/_site/doxygen/classSUAVE_1_1Attributes_1_1Liquids_1_1Water_1_1Water-members.html deleted file mode 100644 index 2769a25c..00000000 --- a/_site/doxygen/classSUAVE_1_1Attributes_1_1Liquids_1_1Water_1_1Water-members.html +++ /dev/null @@ -1,120 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Attributes.Liquids.Water.Water Member List
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Attributes.Liquids.Water.Water Class Reference
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-Inheritance diagram for SUAVE.Attributes.Liquids.Water.Water:
-
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- - -SUAVE.Attributes.Liquids.Liquid.Liquid - -
- - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def compute_cp (self, temperature=300, pressure=101325)
 
def compute_absolute_viscosity (self, temperature=300, pressure=101325)
 
- Public Member Functions inherited from SUAVE.Attributes.Liquids.Liquid.Liquid
def __defaults__ (self)
 
- - - - - - - - - - - - - - - - - - - - -

-Public Attributes

molecular_mass
 
heat_of_vaporization
 
density
 
boiling_point
 
- Public Attributes inherited from SUAVE.Attributes.Liquids.Liquid.Liquid
molecular_mass
 
composition
 
heat_of_vaporization
 
density
 
boiling_point
 
-

Detailed Description

-
Holds constants and functions that compute properties for water.
-
-Assumptions:
-None
-
-Source:
-None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Attributes.Liquids.Water.Water.__defaults__ ( self)
-
-
This sets the default values.
-
-Assumptions:
-None
-
-Source:
-Values commonly available
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-None
-
-
-
- -

◆ compute_absolute_viscosity()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Attributes.Liquids.Water.Water.compute_absolute_viscosity ( self,
 temperature = 300,
 pressure = 101325 
)
-
-
Compute the absolute (dynamic) viscosity. Model accurate to within 
-2.5% between 0 C and 370C
-    
-Assumptions:
-None
-
-Source:
-Engineering Fluid Mechanics, Al-Shemmeri, pg. 18
-
-Inputs:
-temperature  [K]
-
-Outputs:
-mu           [kg/(m-s)]
-
-Properties Used:
-None
-
-
-
- -

◆ compute_cp()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Attributes.Liquids.Water.Water.compute_cp ( self,
 temperature = 300,
 pressure = 101325 
)
-
-
Computes Cp by 4th-order polynomial data fit:
-cp(T) = c1*T^4 + c2*T^3 + c3*T^2 + c4*T+c
-    
-Assumptions:
-278 K < T < 373.15 K
-
-Source:
-Unknown
-
-Inputs:
-temperature    [K]
-
-Outputs:
-cp             [J/kg-K]
-
-Properties Used:
-None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Attributes/Liquids/Water.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Liquids_1_1Water_1_1Water.js b/_site/doxygen/classSUAVE_1_1Attributes_1_1Liquids_1_1Water_1_1Water.js deleted file mode 100644 index ee54d6e5..00000000 --- a/_site/doxygen/classSUAVE_1_1Attributes_1_1Liquids_1_1Water_1_1Water.js +++ /dev/null @@ -1,10 +0,0 @@ -var classSUAVE_1_1Attributes_1_1Liquids_1_1Water_1_1Water = -[ - [ "__defaults__", "classSUAVE_1_1Attributes_1_1Liquids_1_1Water_1_1Water.html#a26e34166234e5e4e859b1518457236f6", null ], - [ "compute_absolute_viscosity", "classSUAVE_1_1Attributes_1_1Liquids_1_1Water_1_1Water.html#afed25d8331b81ad9da36630f1c9ce0d8", null ], - [ "compute_cp", "classSUAVE_1_1Attributes_1_1Liquids_1_1Water_1_1Water.html#a2f39eb3e6e84ed4134aa572bccb21261", null ], - [ "boiling_point", "classSUAVE_1_1Attributes_1_1Liquids_1_1Water_1_1Water.html#a448bd07a86d29731585666cc182ec2eb", null ], - [ "density", "classSUAVE_1_1Attributes_1_1Liquids_1_1Water_1_1Water.html#ac5f6687060722912a9faa90a640913eb", null ], - [ "heat_of_vaporization", "classSUAVE_1_1Attributes_1_1Liquids_1_1Water_1_1Water.html#ae5986eb8fb5b5bef379c1ae53ac9c65b", null ], - [ "molecular_mass", "classSUAVE_1_1Attributes_1_1Liquids_1_1Water_1_1Water.html#a4121d521d9f3a398495d406c42c67348", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Liquids_1_1Water_1_1Water.png b/_site/doxygen/classSUAVE_1_1Attributes_1_1Liquids_1_1Water_1_1Water.png deleted file mode 100644 index a0501367..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Attributes_1_1Liquids_1_1Water_1_1Water.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Planets_1_1Earth_1_1Earth-members.html b/_site/doxygen/classSUAVE_1_1Attributes_1_1Planets_1_1Earth_1_1Earth-members.html deleted file mode 100644 index 5e19b8cf..00000000 --- a/_site/doxygen/classSUAVE_1_1Attributes_1_1Planets_1_1Earth_1_1Earth-members.html +++ /dev/null @@ -1,118 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
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SUAVE -  1.0.0 -
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SUAVE.Attributes.Planets.Earth.Earth Member List
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Planets_1_1Earth_1_1Earth.html b/_site/doxygen/classSUAVE_1_1Attributes_1_1Planets_1_1Earth_1_1Earth.html deleted file mode 100644 index a0305207..00000000 --- a/_site/doxygen/classSUAVE_1_1Attributes_1_1Planets_1_1Earth_1_1Earth.html +++ /dev/null @@ -1,210 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Attributes.Planets.Earth.Earth Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Attributes.Planets.Earth.Earth Class Reference
-
-
-
-Inheritance diagram for SUAVE.Attributes.Planets.Earth.Earth:
-
-
- - -SUAVE.Attributes.Planets.Planet.Planet -SUAVE.Attributes.Constants.Constant.Constant - -
- - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Attributes.Planets.Planet.Planet
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Attributes.Constants.Constant.Constant
def __defaults__ (self)
 
- - - - - - - - - - - - - - - - - - -

-Public Attributes

tag
 
mass
 
mean_radius
 
sea_level_gravity
 
HitchHikersGuide
 
- Public Attributes inherited from SUAVE.Attributes.Planets.Planet.Planet
mass
 
mean_radius
 
sea_level_gravity
 
-

Detailed Description

-
Holds constants for Earth
-
-Assumptions:
-None
-
-Source:
-None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Attributes.Planets.Earth.Earth.__defaults__ ( self)
-
-
This sets the default values.
-
-Assumptions:
-None
-
-Source:
-Values commonly available
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Attributes/Planets/Earth.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Planets_1_1Earth_1_1Earth.js b/_site/doxygen/classSUAVE_1_1Attributes_1_1Planets_1_1Earth_1_1Earth.js deleted file mode 100644 index bc1b22cd..00000000 --- a/_site/doxygen/classSUAVE_1_1Attributes_1_1Planets_1_1Earth_1_1Earth.js +++ /dev/null @@ -1,9 +0,0 @@ -var classSUAVE_1_1Attributes_1_1Planets_1_1Earth_1_1Earth = -[ - [ "__defaults__", "classSUAVE_1_1Attributes_1_1Planets_1_1Earth_1_1Earth.html#af9d701e61dcaa8db64215d233dbab41e", null ], - [ "HitchHikersGuide", "classSUAVE_1_1Attributes_1_1Planets_1_1Earth_1_1Earth.html#ab7c1fd327fdcc282f3c074679ac7b4f5", null ], - [ "mass", "classSUAVE_1_1Attributes_1_1Planets_1_1Earth_1_1Earth.html#ab153ac9436b492099517ed685efcddbf", null ], - [ "mean_radius", "classSUAVE_1_1Attributes_1_1Planets_1_1Earth_1_1Earth.html#a6f45b05a9497a24d54cf3f11c1d0aeba", null ], - [ "sea_level_gravity", "classSUAVE_1_1Attributes_1_1Planets_1_1Earth_1_1Earth.html#a7d7d8928e3a052946e0c48bb90ca8e4d", null ], - [ "tag", "classSUAVE_1_1Attributes_1_1Planets_1_1Earth_1_1Earth.html#a421ca1bfa3d0594813b3160438caac98", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Planets_1_1Earth_1_1Earth.png b/_site/doxygen/classSUAVE_1_1Attributes_1_1Planets_1_1Earth_1_1Earth.png deleted file mode 100644 index dbf3afaa..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Attributes_1_1Planets_1_1Earth_1_1Earth.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Planets_1_1Mars_1_1Mars-members.html b/_site/doxygen/classSUAVE_1_1Attributes_1_1Planets_1_1Mars_1_1Mars-members.html deleted file mode 100644 index 027feff3..00000000 --- a/_site/doxygen/classSUAVE_1_1Attributes_1_1Planets_1_1Mars_1_1Mars-members.html +++ /dev/null @@ -1,116 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE.Attributes.Planets.Mars.Mars Member List
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SUAVE.Attributes.Planets.Mars.Mars Class Reference
-
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-Inheritance diagram for SUAVE.Attributes.Planets.Mars.Mars:
-
-
- - -SUAVE.Attributes.Planets.Planet.Planet -SUAVE.Attributes.Constants.Constant.Constant - -
- - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Attributes.Planets.Planet.Planet
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Attributes.Constants.Constant.Constant
def __defaults__ (self)
 
- - - - - - - - - - - - - - -

-Public Attributes

mass
 
mean_radius
 
sea_level_gravity
 
- Public Attributes inherited from SUAVE.Attributes.Planets.Planet.Planet
mass
 
mean_radius
 
sea_level_gravity
 
-

Detailed Description

-
Holds constants for Earth
-
-Assumptions:
-None
-
-Source:
-None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Attributes.Planets.Mars.Mars.__defaults__ ( self)
-
-
This sets the default values.
-
-Assumptions:
-None
-
-Source:
-Values commonly available
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Attributes/Planets/Mars.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Planets_1_1Mars_1_1Mars.js b/_site/doxygen/classSUAVE_1_1Attributes_1_1Planets_1_1Mars_1_1Mars.js deleted file mode 100644 index c1341386..00000000 --- a/_site/doxygen/classSUAVE_1_1Attributes_1_1Planets_1_1Mars_1_1Mars.js +++ /dev/null @@ -1,7 +0,0 @@ -var classSUAVE_1_1Attributes_1_1Planets_1_1Mars_1_1Mars = -[ - [ "__defaults__", "classSUAVE_1_1Attributes_1_1Planets_1_1Mars_1_1Mars.html#a6a69df61b3f4613a5bb317eafe141525", null ], - [ "mass", "classSUAVE_1_1Attributes_1_1Planets_1_1Mars_1_1Mars.html#a86e73c31eea6ce54a0ac517234181eff", null ], - [ "mean_radius", "classSUAVE_1_1Attributes_1_1Planets_1_1Mars_1_1Mars.html#a843cbafebe8b18e69b4cc8d8590bd69b", null ], - [ "sea_level_gravity", "classSUAVE_1_1Attributes_1_1Planets_1_1Mars_1_1Mars.html#aa4c5f4ccd0aa0f3e036b016dcb48917a", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Planets_1_1Mars_1_1Mars.png b/_site/doxygen/classSUAVE_1_1Attributes_1_1Planets_1_1Mars_1_1Mars.png deleted file mode 100644 index 02d77db5..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Attributes_1_1Planets_1_1Mars_1_1Mars.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Planets_1_1Planet_1_1Planet-members.html b/_site/doxygen/classSUAVE_1_1Attributes_1_1Planets_1_1Planet_1_1Planet-members.html deleted file mode 100644 index 0c1beb73..00000000 --- a/_site/doxygen/classSUAVE_1_1Attributes_1_1Planets_1_1Planet_1_1Planet-members.html +++ /dev/null @@ -1,116 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE.Attributes.Planets.Planet.Planet Member List
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Attributes.Planets.Planet.Planet Class Reference
-
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-Inheritance diagram for SUAVE.Attributes.Planets.Planet.Planet:
-
-
- - -SUAVE.Attributes.Constants.Constant.Constant -SUAVE.Attributes.Planets.Earth.Earth -SUAVE.Attributes.Planets.Mars.Mars - -
- - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Attributes.Constants.Constant.Constant
def __defaults__ (self)
 
- - - - - - - -

-Public Attributes

mass
 
mean_radius
 
sea_level_gravity
 
-

Detailed Description

-
Holds constants for a planet
-
-Assumptions:
-None
-
-Source:
-None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Attributes.Planets.Planet.Planet.__defaults__ ( self)
-
-
This sets the default values.
-
-Assumptions:
-None
-
-Source:
-None
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Attributes/Planets/Planet.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Planets_1_1Planet_1_1Planet.js b/_site/doxygen/classSUAVE_1_1Attributes_1_1Planets_1_1Planet_1_1Planet.js deleted file mode 100644 index cb3e1d22..00000000 --- a/_site/doxygen/classSUAVE_1_1Attributes_1_1Planets_1_1Planet_1_1Planet.js +++ /dev/null @@ -1,7 +0,0 @@ -var classSUAVE_1_1Attributes_1_1Planets_1_1Planet_1_1Planet = -[ - [ "__defaults__", "classSUAVE_1_1Attributes_1_1Planets_1_1Planet_1_1Planet.html#ad2e5a754d11025380430fc1077b33fbf", null ], - [ "mass", "classSUAVE_1_1Attributes_1_1Planets_1_1Planet_1_1Planet.html#ac5c620d87e383037b8d2573eeb9516b4", null ], - [ "mean_radius", "classSUAVE_1_1Attributes_1_1Planets_1_1Planet_1_1Planet.html#ac4ae9a26ea590e1502485b45fb23c617", null ], - [ "sea_level_gravity", "classSUAVE_1_1Attributes_1_1Planets_1_1Planet_1_1Planet.html#adf5a1d15b4d592b8eae648e055c51f8c", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Planets_1_1Planet_1_1Planet.png b/_site/doxygen/classSUAVE_1_1Attributes_1_1Planets_1_1Planet_1_1Planet.png deleted file mode 100644 index 759855b7..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Attributes_1_1Planets_1_1Planet_1_1Planet.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Aviation__Gasoline_1_1Aviation__Gasoline-members.html b/_site/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Aviation__Gasoline_1_1Aviation__Gasoline-members.html deleted file mode 100644 index 37164583..00000000 --- a/_site/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Aviation__Gasoline_1_1Aviation__Gasoline-members.html +++ /dev/null @@ -1,120 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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- - - - - - diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Aviation__Gasoline_1_1Aviation__Gasoline.html b/_site/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Aviation__Gasoline_1_1Aviation__Gasoline.html deleted file mode 100644 index feea7ebf..00000000 --- a/_site/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Aviation__Gasoline_1_1Aviation__Gasoline.html +++ /dev/null @@ -1,212 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Attributes.Propellants.Aviation_Gasoline.Aviation_Gasoline Class Reference - - - - - - - - - - - - - - - -
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SUAVE.Attributes.Propellants.Aviation_Gasoline.Aviation_Gasoline Class Reference
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-Inheritance diagram for SUAVE.Attributes.Propellants.Aviation_Gasoline.Aviation_Gasoline:
-
-
- - -SUAVE.Attributes.Propellants.Propellant.Propellant - -
- - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Attributes.Propellants.Propellant.Propellant
def __defaults__ (self)
 
- - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

tag
 
density
 
specific_energy
 
- Public Attributes inherited from SUAVE.Attributes.Propellants.Propellant.Propellant
tag
 
reactant
 
density
 
specific_energy
 
energy_density
 
max_mass_fraction
 
temperatures
 
-

Detailed Description

-
Holds values for this propellant
-
-Assumptions:
-None
-
-Source:
-None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Attributes.Propellants.Aviation_Gasoline.Aviation_Gasoline.__defaults__ ( self)
-
-
This sets the default values.
-
-Assumptions:
-None
-
-Source:
-Values commonly available
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Attributes/Propellants/Aviation_Gasoline.py
  • -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Attributes.Propellants.Gaseous_H2.Gaseous_H2 Member List
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This is the complete list of members for SUAVE.Attributes.Propellants.Gaseous_H2.Gaseous_H2, including all inherited members.

- - - - - - - - - - - - - - - -
__defaults__(self)SUAVE.Attributes.Propellants.Gaseous_H2.Gaseous_H2
composition (defined in SUAVE.Attributes.Propellants.Gaseous_H2.Gaseous_H2)SUAVE.Attributes.Propellants.Gaseous_H2.Gaseous_H2
compressibility_factor (defined in SUAVE.Attributes.Propellants.Gaseous_H2.Gaseous_H2)SUAVE.Attributes.Propellants.Gaseous_H2.Gaseous_H2
density (defined in SUAVE.Attributes.Propellants.Gaseous_H2.Gaseous_H2)SUAVE.Attributes.Propellants.Gaseous_H2.Gaseous_H2
energy_density (defined in SUAVE.Attributes.Propellants.Gaseous_H2.Gaseous_H2)SUAVE.Attributes.Propellants.Gaseous_H2.Gaseous_H2
gas_constant (defined in SUAVE.Attributes.Propellants.Gaseous_H2.Gaseous_H2)SUAVE.Attributes.Propellants.Gaseous_H2.Gaseous_H2
max_mass_fraction (defined in SUAVE.Attributes.Propellants.Gaseous_H2.Gaseous_H2)SUAVE.Attributes.Propellants.Gaseous_H2.Gaseous_H2
molecular_mass (defined in SUAVE.Attributes.Propellants.Gaseous_H2.Gaseous_H2)SUAVE.Attributes.Propellants.Gaseous_H2.Gaseous_H2
pressure (defined in SUAVE.Attributes.Propellants.Gaseous_H2.Gaseous_H2)SUAVE.Attributes.Propellants.Gaseous_H2.Gaseous_H2
reactant (defined in SUAVE.Attributes.Propellants.Gaseous_H2.Gaseous_H2)SUAVE.Attributes.Propellants.Gaseous_H2.Gaseous_H2
specific_energy (defined in SUAVE.Attributes.Propellants.Gaseous_H2.Gaseous_H2)SUAVE.Attributes.Propellants.Gaseous_H2.Gaseous_H2
tag (defined in SUAVE.Attributes.Propellants.Gaseous_H2.Gaseous_H2)SUAVE.Attributes.Propellants.Gaseous_H2.Gaseous_H2
temperature (defined in SUAVE.Attributes.Propellants.Gaseous_H2.Gaseous_H2)SUAVE.Attributes.Propellants.Gaseous_H2.Gaseous_H2
temperatures (defined in SUAVE.Attributes.Propellants.Propellant.Propellant)SUAVE.Attributes.Propellants.Propellant.Propellant
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Gaseous__H2_1_1Gaseous__H2.html b/_site/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Gaseous__H2_1_1Gaseous__H2.html deleted file mode 100644 index 0d307eec..00000000 --- a/_site/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Gaseous__H2_1_1Gaseous__H2.html +++ /dev/null @@ -1,239 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Attributes.Propellants.Gaseous_H2.Gaseous_H2 Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Attributes.Propellants.Gaseous_H2.Gaseous_H2 Class Reference
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-Inheritance diagram for SUAVE.Attributes.Propellants.Gaseous_H2.Gaseous_H2:
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- - -SUAVE.Attributes.Propellants.Propellant.Propellant - -
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-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Attributes.Propellants.Propellant.Propellant
def __defaults__ (self)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

tag
 
reactant
 
specific_energy
 
energy_density
 
max_mass_fraction
 
composition
 
molecular_mass
 
gas_constant
 
pressure
 
temperature
 
compressibility_factor
 
density
 
- Public Attributes inherited from SUAVE.Attributes.Propellants.Propellant.Propellant
tag
 
reactant
 
density
 
specific_energy
 
energy_density
 
max_mass_fraction
 
temperatures
 
-

Detailed Description

-
Holds values for this propellant
-
-Assumptions:
-None
-
-Source:
-None
-

Member Function Documentation

- -

◆ __defaults__()

- -
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def SUAVE.Attributes.Propellants.Gaseous_H2.Gaseous_H2.__defaults__ ( self)
-
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This sets the default values.
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-Assumptions:
-None
-
-Source:
-Values commonly available
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-None
-
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The documentation for this class was generated from the following file:
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  • /home/tim/Documents/SUAVE/trunk/SUAVE/Attributes/Propellants/Gaseous_H2.py
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Gaseous__H2_1_1Gaseous__H2.js b/_site/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Gaseous__H2_1_1Gaseous__H2.js deleted file mode 100644 index dd85b164..00000000 --- a/_site/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Gaseous__H2_1_1Gaseous__H2.js +++ /dev/null @@ -1,16 +0,0 @@ -var classSUAVE_1_1Attributes_1_1Propellants_1_1Gaseous__H2_1_1Gaseous__H2 = -[ - [ "__defaults__", "classSUAVE_1_1Attributes_1_1Propellants_1_1Gaseous__H2_1_1Gaseous__H2.html#aa88c1ff8872aa28be87ccca3f0f8eb5e", null ], - [ "composition", "classSUAVE_1_1Attributes_1_1Propellants_1_1Gaseous__H2_1_1Gaseous__H2.html#a2f2c2715fa5127e9666792ecf2e85fb2", null ], - [ "compressibility_factor", "classSUAVE_1_1Attributes_1_1Propellants_1_1Gaseous__H2_1_1Gaseous__H2.html#a0a2106a04150933e1f1b20174e01ebdf", null ], - [ "density", "classSUAVE_1_1Attributes_1_1Propellants_1_1Gaseous__H2_1_1Gaseous__H2.html#adb599acfb2b1226cfa491a4112f1eed6", null ], - [ "energy_density", "classSUAVE_1_1Attributes_1_1Propellants_1_1Gaseous__H2_1_1Gaseous__H2.html#a3cec539e1ff8053d533bf8ed8d613e3c", null ], - [ "gas_constant", "classSUAVE_1_1Attributes_1_1Propellants_1_1Gaseous__H2_1_1Gaseous__H2.html#a04ff680cdc7a21f308607abe5c156aea", null ], - [ "max_mass_fraction", "classSUAVE_1_1Attributes_1_1Propellants_1_1Gaseous__H2_1_1Gaseous__H2.html#a748c32df31b6edd84a565e9b9df5f2a2", null ], - [ "molecular_mass", "classSUAVE_1_1Attributes_1_1Propellants_1_1Gaseous__H2_1_1Gaseous__H2.html#ac183ee3bc943ba02359d09c650fad706", null ], - [ "pressure", "classSUAVE_1_1Attributes_1_1Propellants_1_1Gaseous__H2_1_1Gaseous__H2.html#a6962120963298e12eb7b007ce452935f", null ], - [ "reactant", "classSUAVE_1_1Attributes_1_1Propellants_1_1Gaseous__H2_1_1Gaseous__H2.html#a236430b5e78b1ac04e4e2a01de829ac7", null ], - [ "specific_energy", "classSUAVE_1_1Attributes_1_1Propellants_1_1Gaseous__H2_1_1Gaseous__H2.html#a1e97deb59291ece5d898782dda45a0af", null ], - [ "tag", "classSUAVE_1_1Attributes_1_1Propellants_1_1Gaseous__H2_1_1Gaseous__H2.html#ae5d302678be1fa936ec37aa25621bf0e", null ], - [ "temperature", "classSUAVE_1_1Attributes_1_1Propellants_1_1Gaseous__H2_1_1Gaseous__H2.html#a76085e68dd9bab2e66d6129045e7f017", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Gaseous__H2_1_1Gaseous__H2.png b/_site/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Gaseous__H2_1_1Gaseous__H2.png deleted file mode 100644 index 067fa20a..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Gaseous__H2_1_1Gaseous__H2.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Jet__A1_1_1Jet__A1-members.html b/_site/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Jet__A1_1_1Jet__A1-members.html deleted file mode 100644 index 3d5979ee..00000000 --- a/_site/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Jet__A1_1_1Jet__A1-members.html +++ /dev/null @@ -1,120 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Attributes.Propellants.Jet_A1.Jet_A1 Class Reference
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-Inheritance diagram for SUAVE.Attributes.Propellants.Jet_A1.Jet_A1:
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- - -SUAVE.Attributes.Propellants.Propellant.Propellant - -
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-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Attributes.Propellants.Propellant.Propellant
def __defaults__ (self)
 
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-Public Attributes

tag
 
reactant
 
density
 
specific_energy
 
energy_density
 
max_mass_fraction
 
- Public Attributes inherited from SUAVE.Attributes.Propellants.Propellant.Propellant
tag
 
reactant
 
density
 
specific_energy
 
energy_density
 
max_mass_fraction
 
temperatures
 
-

Detailed Description

-
Holds values for this propellant
-
-Assumptions:
-None
-
-Source:
-None
-

Member Function Documentation

- -

◆ __defaults__()

- -
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def SUAVE.Attributes.Propellants.Jet_A1.Jet_A1.__defaults__ ( self)
-
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This sets the default values.
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-Assumptions:
-None
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-Source:
-Values commonly available
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-None
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The documentation for this class was generated from the following file:
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  • /home/tim/Documents/SUAVE/trunk/SUAVE/Attributes/Propellants/Jet_A1.py
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Attributes.Propellants.Jet_A.Jet_A Class Reference
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-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Attributes.Propellants.Propellant.Propellant
def __defaults__ (self)
 
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-Public Attributes

tag
 
reactant
 
density
 
specific_energy
 
energy_density
 
max_mass_fraction
 
- Public Attributes inherited from SUAVE.Attributes.Propellants.Propellant.Propellant
tag
 
reactant
 
density
 
specific_energy
 
energy_density
 
max_mass_fraction
 
temperatures
 
-

Detailed Description

-
Holds values for this propellant
-
-Assumptions:
-None
-
-Source:
-None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Attributes.Propellants.Jet_A.Jet_A.__defaults__ ( self)
-
-
This sets the default values.
-
-Assumptions:
-None
-
-Source:
-Values commonly available
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Attributes/Propellants/Jet_A.py
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Jet__A_1_1Jet__A.js b/_site/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Jet__A_1_1Jet__A.js deleted file mode 100644 index c03301b9..00000000 --- a/_site/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Jet__A_1_1Jet__A.js +++ /dev/null @@ -1,10 +0,0 @@ -var classSUAVE_1_1Attributes_1_1Propellants_1_1Jet__A_1_1Jet__A = -[ - [ "__defaults__", "classSUAVE_1_1Attributes_1_1Propellants_1_1Jet__A_1_1Jet__A.html#a1f9a117c0360a3d758b5295ffbd14558", null ], - [ "density", "classSUAVE_1_1Attributes_1_1Propellants_1_1Jet__A_1_1Jet__A.html#aecce9f170a3bd8df5944a826d34961fe", null ], - [ "energy_density", "classSUAVE_1_1Attributes_1_1Propellants_1_1Jet__A_1_1Jet__A.html#ab1fc99e27bb7be1faebea3914fb560f6", null ], - [ "max_mass_fraction", "classSUAVE_1_1Attributes_1_1Propellants_1_1Jet__A_1_1Jet__A.html#a48826b852cf37bfd7f81df2580bcbd2d", null ], - [ "reactant", "classSUAVE_1_1Attributes_1_1Propellants_1_1Jet__A_1_1Jet__A.html#a9780fca9f6edf371c244f89c11f1032f", null ], - [ "specific_energy", "classSUAVE_1_1Attributes_1_1Propellants_1_1Jet__A_1_1Jet__A.html#aa4c720d94f651037b80de3a5a54a0f77", null ], - [ "tag", "classSUAVE_1_1Attributes_1_1Propellants_1_1Jet__A_1_1Jet__A.html#ae6a3929d8876f7f4844ff4cd3fb728f9", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Jet__A_1_1Jet__A.png b/_site/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Jet__A_1_1Jet__A.png deleted file mode 100644 index eefd49df..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Jet__A_1_1Jet__A.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Liquid__Natural__Gas_1_1Liquid__Natural__Gas-members.html b/_site/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Liquid__Natural__Gas_1_1Liquid__Natural__Gas-members.html deleted file mode 100644 index 34498d6c..00000000 --- a/_site/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Liquid__Natural__Gas_1_1Liquid__Natural__Gas-members.html +++ /dev/null @@ -1,120 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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-Inheritance diagram for SUAVE.Attributes.Propellants.Liquid_Natural_Gas.Liquid_Natural_Gas:
-
-
- - -SUAVE.Attributes.Propellants.Propellant.Propellant - -
- - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Attributes.Propellants.Propellant.Propellant
def __defaults__ (self)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

tag
 
reactant
 
density
 
specific_energy
 
energy_density
 
- Public Attributes inherited from SUAVE.Attributes.Propellants.Propellant.Propellant
tag
 
reactant
 
density
 
specific_energy
 
energy_density
 
max_mass_fraction
 
temperatures
 
-

Detailed Description

-
Holds values for this propellant
-
-Assumptions:
-None
-
-Source:
-None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Attributes.Propellants.Liquid_Natural_Gas.Liquid_Natural_Gas.__defaults__ ( self)
-
-
This sets the default values.
-
-Assumptions:
-None
-
-Source:
-Values commonly available
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Attributes/Propellants/Liquid_Natural_Gas.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Liquid__Natural__Gas_1_1Liquid__Natural__Gas.js b/_site/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Liquid__Natural__Gas_1_1Liquid__Natural__Gas.js deleted file mode 100644 index 37a51094..00000000 --- a/_site/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Liquid__Natural__Gas_1_1Liquid__Natural__Gas.js +++ /dev/null @@ -1,9 +0,0 @@ -var classSUAVE_1_1Attributes_1_1Propellants_1_1Liquid__Natural__Gas_1_1Liquid__Natural__Gas = -[ - [ "__defaults__", "classSUAVE_1_1Attributes_1_1Propellants_1_1Liquid__Natural__Gas_1_1Liquid__Natural__Gas.html#af68453a6c62a42495fd182677f31e63a", null ], - [ "density", "classSUAVE_1_1Attributes_1_1Propellants_1_1Liquid__Natural__Gas_1_1Liquid__Natural__Gas.html#aba3b4bfc3847a541fcfc252493dc5b6f", null ], - [ "energy_density", "classSUAVE_1_1Attributes_1_1Propellants_1_1Liquid__Natural__Gas_1_1Liquid__Natural__Gas.html#ad0217de71ac131307ecd727974a757ce", null ], - [ "reactant", "classSUAVE_1_1Attributes_1_1Propellants_1_1Liquid__Natural__Gas_1_1Liquid__Natural__Gas.html#a307bfab2ec215fa47aeadd5dcd57695f", null ], - [ "specific_energy", "classSUAVE_1_1Attributes_1_1Propellants_1_1Liquid__Natural__Gas_1_1Liquid__Natural__Gas.html#a75b2c1f0705ba55652f7cc31fe66fb21", null ], - [ "tag", "classSUAVE_1_1Attributes_1_1Propellants_1_1Liquid__Natural__Gas_1_1Liquid__Natural__Gas.html#a9ad68be52549385d8e4b691686fc4730", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Liquid__Natural__Gas_1_1Liquid__Natural__Gas.png b/_site/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Liquid__Natural__Gas_1_1Liquid__Natural__Gas.png deleted file mode 100644 index 53e14690..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Liquid__Natural__Gas_1_1Liquid__Natural__Gas.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Propellant_1_1Propellant-members.html b/_site/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Propellant_1_1Propellant-members.html deleted file mode 100644 index 79522561..00000000 --- a/_site/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Propellant_1_1Propellant-members.html +++ /dev/null @@ -1,120 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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- - - - - - diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Propellant_1_1Propellant.html b/_site/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Propellant_1_1Propellant.html deleted file mode 100644 index f1a7c8e6..00000000 --- a/_site/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Propellant_1_1Propellant.html +++ /dev/null @@ -1,204 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Attributes.Propellants.Propellant.Propellant Class Reference - - - - - - - - - - - - - - - -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Attributes.Propellants.Propellant.Propellant Class Reference
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-Inheritance diagram for SUAVE.Attributes.Propellants.Propellant.Propellant:
-
-
- - -SUAVE.Attributes.Propellants.Aviation_Gasoline.Aviation_Gasoline -SUAVE.Attributes.Propellants.Gaseous_H2.Gaseous_H2 -SUAVE.Attributes.Propellants.Jet_A1.Jet_A1 -SUAVE.Attributes.Propellants.Jet_A.Jet_A -SUAVE.Attributes.Propellants.Liquid_H2.Liquid_H2 -SUAVE.Attributes.Propellants.Liquid_Natural_Gas.Liquid_Natural_Gas - -
- - - - -

-Public Member Functions

def __defaults__ (self)
 
- - - - - - - - - - - - - - - -

-Public Attributes

tag
 
reactant
 
density
 
specific_energy
 
energy_density
 
max_mass_fraction
 
temperatures
 
-

Detailed Description

-
Holds values for a propellant
-
-Assumptions:
-None
-
-Source:
-None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Attributes.Propellants.Propellant.Propellant.__defaults__ ( self)
-
-
This sets the default values.
-
-Assumptions:
-None
-
-Source:
-Values commonly available
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Attributes/Propellants/Propellant.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Propellant_1_1Propellant.js b/_site/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Propellant_1_1Propellant.js deleted file mode 100644 index a1906ea2..00000000 --- a/_site/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Propellant_1_1Propellant.js +++ /dev/null @@ -1,11 +0,0 @@ -var classSUAVE_1_1Attributes_1_1Propellants_1_1Propellant_1_1Propellant = -[ - [ "__defaults__", "classSUAVE_1_1Attributes_1_1Propellants_1_1Propellant_1_1Propellant.html#a613e61ecbcf6282645170663ea33f60c", null ], - [ "density", "classSUAVE_1_1Attributes_1_1Propellants_1_1Propellant_1_1Propellant.html#a9657ba38159e9030e85e07c902b075e8", null ], - [ "energy_density", "classSUAVE_1_1Attributes_1_1Propellants_1_1Propellant_1_1Propellant.html#a9ae53320c505320b4da1666a4e1e0a4f", null ], - [ "max_mass_fraction", "classSUAVE_1_1Attributes_1_1Propellants_1_1Propellant_1_1Propellant.html#a8127519358259b594d8a9e89ba1264fa", null ], - [ "reactant", "classSUAVE_1_1Attributes_1_1Propellants_1_1Propellant_1_1Propellant.html#a1edb5b2eb8f1309d8c89d270a4855c1f", null ], - [ "specific_energy", "classSUAVE_1_1Attributes_1_1Propellants_1_1Propellant_1_1Propellant.html#ae192ea1029775e334d9ef0773fa357c0", null ], - [ "tag", "classSUAVE_1_1Attributes_1_1Propellants_1_1Propellant_1_1Propellant.html#ab05a5bb0c5c7c5a3e7a4d5a0f7985161", null ], - [ "temperatures", "classSUAVE_1_1Attributes_1_1Propellants_1_1Propellant_1_1Propellant.html#afdad4dd8353e1bd9bfa7aa93ba7635e4", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Propellant_1_1Propellant.png b/_site/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Propellant_1_1Propellant.png deleted file mode 100644 index 1954d90e..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Propellant_1_1Propellant.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Component_1_1Component-members.html b/_site/doxygen/classSUAVE_1_1Components_1_1Component_1_1Component-members.html deleted file mode 100644 index 972679a4..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Component_1_1Component-members.html +++ /dev/null @@ -1,115 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE.Components.Component.Component Member List
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Component.Component Class Reference
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-Inheritance diagram for SUAVE.Components.Component.Component:
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- - -SUAVE.Components.Envelope.Envelope -SUAVE.Components.Lofted_Body.Curve -SUAVE.Components.Lofted_Body.Section -SUAVE.Components.Lofted_Body.Segment -SUAVE.Components.Physical_Component.Physical_Component -SUAVE.Components.Systems.System.System -SUAVE.Components.Wings.Airfoils.Airfoil.Airfoil -SUAVE.Components.Wings.Control_Surface.Control_Surface_Section -SUAVE.Components.Wings.Segment.Segment -SUAVE.Components.Energy.Energy.Component -SUAVE.Components.Energy.Energy.Energy -SUAVE.Components.Energy.Energy_Component.Energy_Component -SUAVE.Components.Landing_Gear.Landing_Gear.Landing_Gear -SUAVE.Components.Lofted_Body.Lofted_Body -SUAVE.Components.Payloads.Payload.Payload -SUAVE.Components.Propulsors.Propulsor.Propulsor - -
- - - - -

-Public Member Functions

def __defaults__ (self)
 
- - - - - -

-Public Attributes

tag
 
origin
 
-

Detailed Description

-
the base component class
-    Assumptions:
-    None
-    
-    Source:
-    None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Components.Component.Component.__defaults__ ( self)
-
-
This sets the default values.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Component.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Component_1_1Component.js b/_site/doxygen/classSUAVE_1_1Components_1_1Component_1_1Component.js deleted file mode 100644 index 9e83bea7..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Component_1_1Component.js +++ /dev/null @@ -1,6 +0,0 @@ -var classSUAVE_1_1Components_1_1Component_1_1Component = -[ - [ "__defaults__", "classSUAVE_1_1Components_1_1Component_1_1Component.html#a2d9252624c70b5d919bc9ec4809aaeff", null ], - [ "origin", "classSUAVE_1_1Components_1_1Component_1_1Component.html#a73f01c28d509653b176d616ddf5774d6", null ], - [ "tag", "classSUAVE_1_1Components_1_1Component_1_1Component.html#a03eb542a5d248132cad459e2b1da0712", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Component_1_1Component.png b/_site/doxygen/classSUAVE_1_1Components_1_1Component_1_1Component.png deleted file mode 100644 index 89bb7035..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Component_1_1Component.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Component_1_1Container-members.html b/_site/doxygen/classSUAVE_1_1Components_1_1Component_1_1Container-members.html deleted file mode 100644 index a05e82dd..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Component_1_1Container-members.html +++ /dev/null @@ -1,113 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Component.Container Member List
-
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- -

This is the complete list of members for SUAVE.Components.Component.Container, including all inherited members.

- - -
Container (defined in SUAVE.Components.Component.Container)SUAVE.Components.Component.Containerstatic
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Component_1_1Container.html b/_site/doxygen/classSUAVE_1_1Components_1_1Component_1_1Container.html deleted file mode 100644 index 460c30b2..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Component_1_1Container.html +++ /dev/null @@ -1,148 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Components.Component.Container Class Reference - - - - - - - - - - - - - - - -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Component.Container Class Reference
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-Inheritance diagram for SUAVE.Components.Component.Container:
-
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- - -SUAVE.Components.Lofted_Body.CurveContainer -SUAVE.Components.Lofted_Body.SectionContainer -SUAVE.Components.Physical_Component.Container -SUAVE.Components.Systems.System.Container -SUAVE.Components.Wings.Wing.Container -SUAVE.Components.Energy.Energy.ComponentContainer -SUAVE.Components.Fuselages.Fuselage.Container -SUAVE.Components.Payloads.Payload.Container -SUAVE.Components.Propulsors.Propulsor.Container - -
- - - - -

-Static Public Attributes

Container
 
-

Detailed Description

-
the base component container class
-
-    Assumptions:
-    None
-    
-    Source:
-    None
-

The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Component.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Component_1_1Container.png b/_site/doxygen/classSUAVE_1_1Components_1_1Component_1_1Container.png deleted file mode 100644 index a93a56d0..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Component_1_1Container.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Configs_1_1Config_1_1Config-members.html b/_site/doxygen/classSUAVE_1_1Components_1_1Configs_1_1Config_1_1Config-members.html deleted file mode 100644 index 4240f114..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Configs_1_1Config_1_1Config-members.html +++ /dev/null @@ -1,114 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Configs.Config.Config Member List
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This is the complete list of members for SUAVE.Components.Configs.Config.Config, including all inherited members.

- - - -
__defaults__(self)SUAVE.Components.Configs.Config.Config
tag (defined in SUAVE.Components.Configs.Config.Config)SUAVE.Components.Configs.Config.Config
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Configs_1_1Config_1_1Config.html b/_site/doxygen/classSUAVE_1_1Components_1_1Configs_1_1Config_1_1Config.html deleted file mode 100644 index a5f12831..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Configs_1_1Config_1_1Config.html +++ /dev/null @@ -1,182 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Components.Configs.Config.Config Class Reference - - - - - - - - - - - - - - - -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Configs.Config.Config Class Reference
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-Inheritance diagram for SUAVE.Components.Configs.Config.Config:
-
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- - - - -

-Public Member Functions

def __defaults__ (self)
 
- - - -

-Public Attributes

tag
 
-

Detailed Description

-
SUAVE.Components.Config()
-
-    The Top Level Configuration Class
-    
-        Assumptions:
-        None
-        
-        Source:
-        N/A
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Components.Configs.Config.Config.__defaults__ ( self)
-
-
This sets the default values for the configuration.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Configs/Config.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Configs_1_1Config_1_1Config.js b/_site/doxygen/classSUAVE_1_1Components_1_1Configs_1_1Config_1_1Config.js deleted file mode 100644 index eced8df4..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Configs_1_1Config_1_1Config.js +++ /dev/null @@ -1,5 +0,0 @@ -var classSUAVE_1_1Components_1_1Configs_1_1Config_1_1Config = -[ - [ "__defaults__", "classSUAVE_1_1Components_1_1Configs_1_1Config_1_1Config.html#aca0bf9b86b4f0f0dc6052ae69f2252c5", null ], - [ "tag", "classSUAVE_1_1Components_1_1Configs_1_1Config_1_1Config.html#a80e05cad540c898def5efdab8d23dfc2", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Configs_1_1Config_1_1Config.png b/_site/doxygen/classSUAVE_1_1Components_1_1Configs_1_1Config_1_1Config.png deleted file mode 100644 index 7887e3d1..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Configs_1_1Config_1_1Config.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Configs_1_1Config_1_1Container-members.html b/_site/doxygen/classSUAVE_1_1Components_1_1Configs_1_1Config_1_1Container-members.html deleted file mode 100644 index 9e201f3b..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Configs_1_1Config_1_1Container-members.html +++ /dev/null @@ -1,113 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Configs.Config.Container Member List
-
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This is the complete list of members for SUAVE.Components.Configs.Config.Container, including all inherited members.

- - -
Container (defined in SUAVE.Components.Configs.Config.Container)SUAVE.Components.Configs.Config.Containerstatic
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Configs_1_1Config_1_1Container.html b/_site/doxygen/classSUAVE_1_1Components_1_1Configs_1_1Config_1_1Container.html deleted file mode 100644 index 8c63d878..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Configs_1_1Config_1_1Container.html +++ /dev/null @@ -1,141 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Components.Configs.Config.Container Class Reference - - - - - - - - - - - - - - - -
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SUAVE.Components.Configs.Config.Container Class Reference
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-Inheritance diagram for SUAVE.Components.Configs.Config.Container:
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-Static Public Attributes

Container
 
-

Detailed Description

-
SUAVE.Components.Config.Container()
-
-    The top level configuration container class
-    
-        Assumptions:
-        None:
-        
-        Source:
-        N/A
-

The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Configs/Config.py
  • -
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SUAVE.Components.Costs.Costs.Industrial_Costs Member List
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This is the complete list of members for SUAVE.Components.Costs.Costs.Industrial_Costs, including all inherited members.

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__defaults__(self)SUAVE.Components.Costs.Costs.Industrial_Costs
aircraft_type (defined in SUAVE.Components.Costs.Costs.Industrial_Costs)SUAVE.Components.Costs.Costs.Industrial_Costs
avionics_cost (defined in SUAVE.Components.Costs.Costs.Industrial_Costs)SUAVE.Components.Costs.Costs.Industrial_Costs
cad_factor (defined in SUAVE.Components.Costs.Costs.Industrial_Costs)SUAVE.Components.Costs.Costs.Industrial_Costs
development_total_years (defined in SUAVE.Components.Costs.Costs.Industrial_Costs)SUAVE.Components.Costs.Costs.Industrial_Costs
difficulty_factor (defined in SUAVE.Components.Costs.Costs.Industrial_Costs)SUAVE.Components.Costs.Costs.Industrial_Costs
escalation_factor (defined in SUAVE.Components.Costs.Costs.Industrial_Costs)SUAVE.Components.Costs.Costs.Industrial_Costs
hourly_rates (defined in SUAVE.Components.Costs.Costs.Industrial_Costs)SUAVE.Components.Costs.Costs.Industrial_Costs
manufacturing_facilities_cost (defined in SUAVE.Components.Costs.Costs.Industrial_Costs)SUAVE.Components.Costs.Costs.Industrial_Costs
material_factor (defined in SUAVE.Components.Costs.Costs.Industrial_Costs)SUAVE.Components.Costs.Costs.Industrial_Costs
production_total_units (defined in SUAVE.Components.Costs.Costs.Industrial_Costs)SUAVE.Components.Costs.Costs.Industrial_Costs
prototypes_units (defined in SUAVE.Components.Costs.Costs.Industrial_Costs)SUAVE.Components.Costs.Costs.Industrial_Costs
reference_year (defined in SUAVE.Components.Costs.Costs.Industrial_Costs)SUAVE.Components.Costs.Costs.Industrial_Costs
stealth (defined in SUAVE.Components.Costs.Costs.Industrial_Costs)SUAVE.Components.Costs.Costs.Industrial_Costs
tag (defined in SUAVE.Components.Costs.Costs.Industrial_Costs)SUAVE.Components.Costs.Costs.Industrial_Costs
test_facilities_cost (defined in SUAVE.Components.Costs.Costs.Industrial_Costs)SUAVE.Components.Costs.Costs.Industrial_Costs
units_to_amortize (defined in SUAVE.Components.Costs.Costs.Industrial_Costs)SUAVE.Components.Costs.Costs.Industrial_Costs
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Costs.Costs.Industrial_Costs Class Reference
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-Inheritance diagram for SUAVE.Components.Costs.Costs.Industrial_Costs:
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-Public Member Functions

def __defaults__ (self)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

tag
 
reference_year
 
production_total_units
 
units_to_amortize
 
prototypes_units
 
avionics_cost
 
test_facilities_cost
 
manufacturing_facilities_cost
 
escalation_factor
 
development_total_years
 
aircraft_type
 
difficulty_factor
 
cad_factor
 
stealth
 
material_factor
 
hourly_rates
 
-

Detailed Description

-
A class containing industrial cost variables.
-
-Assumptions:
-None
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-Source:
-N/A
-

Member Function Documentation

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◆ __defaults__()

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def SUAVE.Components.Costs.Costs.Industrial_Costs.__defaults__ ( self)
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This sets the default values used in the industrial cost methods.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
-
-
The documentation for this class was generated from the following file:
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  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Costs/Costs.py
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Costs_1_1Costs_1_1Industrial__Costs.js b/_site/doxygen/classSUAVE_1_1Components_1_1Costs_1_1Costs_1_1Industrial__Costs.js deleted file mode 100644 index 4f187cb3..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Costs_1_1Costs_1_1Industrial__Costs.js +++ /dev/null @@ -1,20 +0,0 @@ -var classSUAVE_1_1Components_1_1Costs_1_1Costs_1_1Industrial__Costs = -[ - [ "__defaults__", "classSUAVE_1_1Components_1_1Costs_1_1Costs_1_1Industrial__Costs.html#a2656af946c2bf8fb3eb9e0645ef687f6", null ], - [ "aircraft_type", "classSUAVE_1_1Components_1_1Costs_1_1Costs_1_1Industrial__Costs.html#aa18aed9f47b76f2c5e9e8e48f3258b50", null ], - [ "avionics_cost", "classSUAVE_1_1Components_1_1Costs_1_1Costs_1_1Industrial__Costs.html#a3b93301fe80b9b12bff9ff799eb7388e", null ], - [ "cad_factor", "classSUAVE_1_1Components_1_1Costs_1_1Costs_1_1Industrial__Costs.html#a7e396a8e2a3044f02cc54c2bc7ebd4f9", null ], - [ "development_total_years", "classSUAVE_1_1Components_1_1Costs_1_1Costs_1_1Industrial__Costs.html#a58752daa2f13ca5b5d838849668f2dc8", null ], - [ "difficulty_factor", "classSUAVE_1_1Components_1_1Costs_1_1Costs_1_1Industrial__Costs.html#a0647a246b7400a16d5a0a7ede00032f8", null ], - [ "escalation_factor", "classSUAVE_1_1Components_1_1Costs_1_1Costs_1_1Industrial__Costs.html#a268a2638768b54b78202c762b0c88ac4", null ], - [ "hourly_rates", "classSUAVE_1_1Components_1_1Costs_1_1Costs_1_1Industrial__Costs.html#af009e84b27b37c549b71b7a20019b07c", null ], - [ "manufacturing_facilities_cost", "classSUAVE_1_1Components_1_1Costs_1_1Costs_1_1Industrial__Costs.html#add68606611ccf20fe327c6a2ac88f3bb", null ], - [ "material_factor", "classSUAVE_1_1Components_1_1Costs_1_1Costs_1_1Industrial__Costs.html#aeb5c4475deb1b7269967ee083b6c8b64", null ], - [ "production_total_units", "classSUAVE_1_1Components_1_1Costs_1_1Costs_1_1Industrial__Costs.html#a491c866149cd932b4c2da6fe34f1e1e2", null ], - [ "prototypes_units", "classSUAVE_1_1Components_1_1Costs_1_1Costs_1_1Industrial__Costs.html#a4c6b835e96521c7d3b6c512abc03a4c6", null ], - [ "reference_year", "classSUAVE_1_1Components_1_1Costs_1_1Costs_1_1Industrial__Costs.html#acc51176d5290166ca5c9c4df82670eef", null ], - [ "stealth", "classSUAVE_1_1Components_1_1Costs_1_1Costs_1_1Industrial__Costs.html#a0e69af3787f91f7a2c8368f1549caf85", null ], - [ "tag", "classSUAVE_1_1Components_1_1Costs_1_1Costs_1_1Industrial__Costs.html#acc0eae6377af4e4bb22c07d85a27ffdb", null ], - [ "test_facilities_cost", "classSUAVE_1_1Components_1_1Costs_1_1Costs_1_1Industrial__Costs.html#a9f6ac4de1804ad1da7106b8bee423137", null ], - [ "units_to_amortize", "classSUAVE_1_1Components_1_1Costs_1_1Costs_1_1Industrial__Costs.html#af2ff6f4f5c3da9fb940f8099b36d75ea", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Costs_1_1Costs_1_1Industrial__Costs.png b/_site/doxygen/classSUAVE_1_1Components_1_1Costs_1_1Costs_1_1Industrial__Costs.png deleted file mode 100644 index 72f99afa..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Costs_1_1Costs_1_1Industrial__Costs.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Costs_1_1Costs_1_1Operating__Costs-members.html b/_site/doxygen/classSUAVE_1_1Components_1_1Costs_1_1Costs_1_1Operating__Costs-members.html deleted file mode 100644 index 8172ba64..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Costs_1_1Costs_1_1Operating__Costs-members.html +++ /dev/null @@ -1,123 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE.Components.Costs.Costs.Operating_Costs Class Reference
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-Public Member Functions

def __defaults__ (self)
 
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-Public Attributes

tag
 
depreciate_years
 
fuel_price
 
oil_price
 
insure_rate
 
maintenance_rate
 
pilot_rate
 
crew_rate
 
inflator
 
reference_dollars
 
-

Detailed Description

-
A class containing operating cost variables.
-
-Assumptions:
-None
-
-Source:
-N/A
-

Member Function Documentation

- -

◆ __defaults__()

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def SUAVE.Components.Costs.Costs.Operating_Costs.__defaults__ ( self)
-
-
This sets the default values used in the operating cost methods.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Costs/Costs.py
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Energy.Converters.Combustor.Combustor Member List
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This is the complete list of members for SUAVE.Components.Energy.Converters.Combustor.Combustor, including all inherited members.

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__defaults__(self)SUAVE.Components.Energy.Converters.Combustor.Combustor
alphac (defined in SUAVE.Components.Energy.Converters.Combustor.Combustor)SUAVE.Components.Energy.Converters.Combustor.Combustor
compute(self, conditions)SUAVE.Components.Energy.Converters.Combustor.Combustor
fuel_data (defined in SUAVE.Components.Energy.Converters.Combustor.Combustor)SUAVE.Components.Energy.Converters.Combustor.Combustor
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Energy.Converters.Combustor.Combustor)SUAVE.Components.Energy.Converters.Combustor.Combustor
turbine_inlet_temperature (defined in SUAVE.Components.Energy.Converters.Combustor.Combustor)SUAVE.Components.Energy.Converters.Combustor.Combustor
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Combustor_1_1Combustor.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Combustor_1_1Combustor.html deleted file mode 100644 index a994ded4..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Combustor_1_1Combustor.html +++ /dev/null @@ -1,290 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Components.Energy.Converters.Combustor.Combustor Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Energy.Converters.Combustor.Combustor Class Reference
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-Inheritance diagram for SUAVE.Components.Energy.Converters.Combustor.Combustor:
-
-
- - -SUAVE.Components.Energy.Energy_Component.Energy_Component -SUAVE.Components.Physical_Component.Physical_Component -SUAVE.Components.Component.Component - -
- - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def compute (self, conditions)
 
- Public Member Functions inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

tag
 
fuel_data
 
alphac
 
turbine_inlet_temperature
 
- Public Attributes inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
inputs
 
outputs
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
-

Detailed Description

-
This is provides output values for a combustor
-Calling this class calls the compute function.
-
-Assumptions:
-None
-
-Source:
-https://web.stanford.edu/~cantwell/AA283_Course_Material/AA283_Course_Notes/
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Components.Energy.Converters.Combustor.Combustor.__defaults__ ( self)
-
-
This sets the default values for the component to function.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-None
-
-
-
- -

◆ compute()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Components.Energy.Converters.Combustor.Combustor.compute ( self,
 conditions 
)
-
-
This computes the output values from the input values according to
-equations from the source.
-
-Assumptions:
-Constant efficiency and pressure ratio
-
-Source:
-https://web.stanford.edu/~cantwell/AA283_Course_Material/AA283_Course_Notes/
-
-Inputs:
-conditions.freestream.
-  isentropic_expansion_factor         [-]
-  specific_heat_at_constant_pressure  [J/(kg K)]
-  temperature                         [K]
-  stagnation_temperature              [K]
-self.inputs.
-  stagnation_temperature              [K]
-  stagnation_pressure                 [Pa]
-
-Outputs:
-self.outputs.
-  stagnation_temperature              [K]  
-  stagnation_pressure                 [Pa]
-  stagnation_enthalpy                 [J/kg]
-  fuel_to_air_ratio                   [-]
-
-Properties Used:
-self.
-  turbine_inlet_temperature           [K]
-  pressure_ratio                      [-]
-  efficiency                          [-]
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Energy/Converters/Combustor.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Combustor_1_1Combustor.js b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Combustor_1_1Combustor.js deleted file mode 100644 index 3731eba6..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Combustor_1_1Combustor.js +++ /dev/null @@ -1,9 +0,0 @@ -var classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Combustor_1_1Combustor = -[ - [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Combustor_1_1Combustor.html#a2a0f7c8f68137486dd2fec4e90f64ad2", null ], - [ "compute", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Combustor_1_1Combustor.html#ab7ff2679c7aa46e60388a448b7d44120", null ], - [ "alphac", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Combustor_1_1Combustor.html#abad75b1005d3585a7a56d4848997b5f9", null ], - [ "fuel_data", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Combustor_1_1Combustor.html#a167de0d8770cf94173f256e36921e3ed", null ], - [ "tag", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Combustor_1_1Combustor.html#ab3a4977f8218e87a868b4693c7d06873", null ], - [ "turbine_inlet_temperature", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Combustor_1_1Combustor.html#a42bc5e129081949bec715e938e3a7536", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Combustor_1_1Combustor.png b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Combustor_1_1Combustor.png deleted file mode 100644 index e5fd2ea2..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Combustor_1_1Combustor.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Compression__Nozzle_1_1Compression__Nozzle-members.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Compression__Nozzle_1_1Compression__Nozzle-members.html deleted file mode 100644 index 05d65296..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Compression__Nozzle_1_1Compression__Nozzle-members.html +++ /dev/null @@ -1,122 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
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SUAVE.Components.Energy.Converters.Compression_Nozzle.Compression_Nozzle Member List
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-
- -

This is the complete list of members for SUAVE.Components.Energy.Converters.Compression_Nozzle.Compression_Nozzle, including all inherited members.

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__defaults__(self)SUAVE.Components.Energy.Converters.Compression_Nozzle.Compression_Nozzle
compute(self, conditions)SUAVE.Components.Energy.Converters.Compression_Nozzle.Compression_Nozzle
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
polytropic_efficiency (defined in SUAVE.Components.Energy.Converters.Compression_Nozzle.Compression_Nozzle)SUAVE.Components.Energy.Converters.Compression_Nozzle.Compression_Nozzle
pressure_ratio (defined in SUAVE.Components.Energy.Converters.Compression_Nozzle.Compression_Nozzle)SUAVE.Components.Energy.Converters.Compression_Nozzle.Compression_Nozzle
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Energy.Converters.Compression_Nozzle.Compression_Nozzle)SUAVE.Components.Energy.Converters.Compression_Nozzle.Compression_Nozzle
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Compression__Nozzle_1_1Compression__Nozzle.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Compression__Nozzle_1_1Compression__Nozzle.html deleted file mode 100644 index 571ae254..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Compression__Nozzle_1_1Compression__Nozzle.html +++ /dev/null @@ -1,290 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Components.Energy.Converters.Compression_Nozzle.Compression_Nozzle Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Energy.Converters.Compression_Nozzle.Compression_Nozzle Class Reference
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-Inheritance diagram for SUAVE.Components.Energy.Converters.Compression_Nozzle.Compression_Nozzle:
-
-
- - -SUAVE.Components.Energy.Energy_Component.Energy_Component -SUAVE.Components.Physical_Component.Physical_Component -SUAVE.Components.Component.Component - -
- - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def compute (self, conditions)
 
- Public Member Functions inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

tag
 
polytropic_efficiency
 
pressure_ratio
 
- Public Attributes inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
inputs
 
outputs
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
-

Detailed Description

-
This is a nozzle component intended for use in compression.
-Calling this class calls the compute function.
-
-Assumptions:
-Pressure ratio and efficiency do not change with varying conditions.
-Subsonic or choked output.
-
-Source:
-https://web.stanford.edu/~cantwell/AA283_Course_Material/AA283_Course_Notes/
-

Member Function Documentation

- -

◆ __defaults__()

- -
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- - - - - - - - -
def SUAVE.Components.Energy.Converters.Compression_Nozzle.Compression_Nozzle.__defaults__ ( self)
-
-
This sets the default values for the component to function.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-None
-
-
-
- -

◆ compute()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Components.Energy.Converters.Compression_Nozzle.Compression_Nozzle.compute ( self,
 conditions 
)
-
-
This computes the output values from the input values according to
-equations from the source.
-
-Assumptions:
-Constant polytropic efficiency and pressure ratio
-
-Source:
-https://web.stanford.edu/~cantwell/AA283_Course_Material/AA283_Course_Notes/
-
-Inputs:
-conditions.freestream.
-  isentropic_expansion_factor         [-]
-  specific_heat_at_constant_pressure  [J/(kg K)]
-  pressure                            [Pa]
-  universal_gas_constant              [J/(kg K)] (this is misnamed - actually refers to the gas specific constant)
-self.inputs.
-  stagnation_temperature              [K]
-  stagnation_pressure                 [Pa]
-
-Outputs:
-self.outputs.
-  stagnation_temperature              [K]  
-  stagnation_pressure                 [Pa]
-  stagnation_enthalpy                 [J/kg]
-  mach_number                         [-]
-  static_temperature                  [K]
-  static_enthalpy                     [J/kg]
-  velocity                            [m/s]
-
-Properties Used:
-self.
-  pressure_ratio                      [-]
-  polytropic_efficiency               [-]
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Energy/Converters/Compression_Nozzle.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Compression__Nozzle_1_1Compression__Nozzle.js b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Compression__Nozzle_1_1Compression__Nozzle.js deleted file mode 100644 index 6503b2ec..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Compression__Nozzle_1_1Compression__Nozzle.js +++ /dev/null @@ -1,8 +0,0 @@ -var classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Compression__Nozzle_1_1Compression__Nozzle = -[ - [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Compression__Nozzle_1_1Compression__Nozzle.html#aac9c90445bd9c7d1bdfd4fad2f668b1e", null ], - [ "compute", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Compression__Nozzle_1_1Compression__Nozzle.html#acdaf2c6eec5fbe7f8f56b2254b6461a0", null ], - [ "polytropic_efficiency", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Compression__Nozzle_1_1Compression__Nozzle.html#a189581236c66eaa42b59787a0a21fab6", null ], - [ "pressure_ratio", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Compression__Nozzle_1_1Compression__Nozzle.html#a001dd3301c2cefa6421b41c417338534", null ], - [ "tag", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Compression__Nozzle_1_1Compression__Nozzle.html#adc44bf1576cef3fbefa090fd7468bbe5", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Compression__Nozzle_1_1Compression__Nozzle.png b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Compression__Nozzle_1_1Compression__Nozzle.png deleted file mode 100644 index 9a31b6b5..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Compression__Nozzle_1_1Compression__Nozzle.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Compressor_1_1Compressor-members.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Compressor_1_1Compressor-members.html deleted file mode 100644 index c35ba43a..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Compressor_1_1Compressor-members.html +++ /dev/null @@ -1,122 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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- - - - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Compressor_1_1Compressor.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Compressor_1_1Compressor.html deleted file mode 100644 index dd4dd396..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Compressor_1_1Compressor.html +++ /dev/null @@ -1,284 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Components.Energy.Converters.Compressor.Compressor Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Energy.Converters.Compressor.Compressor Class Reference
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-Inheritance diagram for SUAVE.Components.Energy.Converters.Compressor.Compressor:
-
-
- - -SUAVE.Components.Energy.Energy_Component.Energy_Component -SUAVE.Components.Physical_Component.Physical_Component -SUAVE.Components.Component.Component - -
- - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def compute (self, conditions)
 
- Public Member Functions inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
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-Public Attributes

tag
 
polytropic_efficiency
 
pressure_ratio
 
- Public Attributes inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
inputs
 
outputs
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
-

Detailed Description

-
This is a compressor component typically used in a turbofan.
-Calling this class calls the compute function.
-
-Assumptions:
-Pressure ratio and efficiency do not change with varying conditions.
-
-Source:
-https://web.stanford.edu/~cantwell/AA283_Course_Material/AA283_Course_Notes/
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Components.Energy.Converters.Compressor.Compressor.__defaults__ ( self)
-
-
This sets the default values for the component to function.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-None
-
-
-
- -

◆ compute()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Components.Energy.Converters.Compressor.Compressor.compute ( self,
 conditions 
)
-
-
This computes the output values from the input values according to
-equations from the source.
-
-Assumptions:
-Constant polytropic efficiency and pressure ratio
-
-Source:
-https://web.stanford.edu/~cantwell/AA283_Course_Material/AA283_Course_Notes/
-
-Inputs:
-conditions.freestream.
-  isentropic_expansion_factor         [-]
-  specific_heat_at_constant_pressure  [J/(kg K)]
-self.inputs.
-  stagnation_temperature              [K]
-  stagnation_pressure                 [Pa]
-
-Outputs:
-self.outputs.
-  stagnation_temperature              [K]  
-  stagnation_pressure                 [Pa]
-  stagnation_enthalpy                 [J/kg]
-  work_done                           [J/kg]
-
-Properties Used:
-self.
-  pressure_ratio                      [-]
-  polytropic_efficiency               [-]
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Energy/Converters/Compressor.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Compressor_1_1Compressor.js b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Compressor_1_1Compressor.js deleted file mode 100644 index c0c26f18..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Compressor_1_1Compressor.js +++ /dev/null @@ -1,8 +0,0 @@ -var classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Compressor_1_1Compressor = -[ - [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Compressor_1_1Compressor.html#a68973a5592953a2711b2c8c75ef97871", null ], - [ "compute", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Compressor_1_1Compressor.html#a51bce028331205d4849f7ba23e2acdec", null ], - [ "polytropic_efficiency", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Compressor_1_1Compressor.html#a7f68c1dd56b54d796afa9c4df66f638f", null ], - [ "pressure_ratio", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Compressor_1_1Compressor.html#ab63d7199865eca42415ef1d5259151c2", null ], - [ "tag", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Compressor_1_1Compressor.html#ad00758ae48d6abff33f9d3258b4793d0", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Compressor_1_1Compressor.png b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Compressor_1_1Compressor.png deleted file mode 100644 index 74b3994d..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Compressor_1_1Compressor.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Expansion__Nozzle_1_1Expansion__Nozzle-members.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Expansion__Nozzle_1_1Expansion__Nozzle-members.html deleted file mode 100644 index 429739bf..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Expansion__Nozzle_1_1Expansion__Nozzle-members.html +++ /dev/null @@ -1,155 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle Member List
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-
- -

This is the complete list of members for SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle, including all inherited members.

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__defaults__(self)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle
area_ratio (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic
area_ratio (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic
compute(self, conditions)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle
Cp (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic
density (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic
etapold (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic
gamma (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic
h_out (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic
ht_out (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic
i_high (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic
i_low (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
Mach (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic
mach_number (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
Mo (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
P_out (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic
pid (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic
Po (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic
polytropic_efficiency (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle
pressure_ratio (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle
Pt_in (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic
Pt_out (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic
Pto (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic
R (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic
rho_out (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic
stagnation_enthalpy (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic
stagnation_pressure (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic
stagnation_temperature (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic
static_enthalpy (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic
static_pressure (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic
static_temperature (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
T_out (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic
tag (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle
Tt_in (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic
Tt_out (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic
Tto (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic
u_out (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic
velocity (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Expansion__Nozzle_1_1Expansion__Nozzle.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Expansion__Nozzle_1_1Expansion__Nozzle.html deleted file mode 100644 index d775539f..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Expansion__Nozzle_1_1Expansion__Nozzle.html +++ /dev/null @@ -1,399 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle Class Reference - - - - - - - - - - - - - - - -
-
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle Class Reference
-
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-
-Inheritance diagram for SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle:
-
-
- - -SUAVE.Components.Energy.Energy_Component.Energy_Component -SUAVE.Components.Physical_Component.Physical_Component -SUAVE.Components.Component.Component - -
- - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def compute (self, conditions)
 
- Public Member Functions inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

tag
 
polytropic_efficiency
 
pressure_ratio
 
- Public Attributes inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
inputs
 
outputs
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Static Public Attributes

gamma = conditions.freestream.isentropic_expansion_factor
 
Cp = conditions.freestream.specific_heat_at_constant_pressure
 
Po = conditions.freestream.pressure
 
Pto = conditions.freestream.stagnation_pressure
 
Tto = conditions.freestream.stagnation_temperature
 
R = conditions.freestream.universal_gas_constant
 
Mo = conditions.freestream.mach_number
 
Tt_in = self.inputs.stagnation_temperature
 
Pt_in = self.inputs.stagnation_pressure
 
pid = self.pressure_ratio
 
etapold = self.polytropic_efficiency
 
Pt_out = Pt_in*pid
 
Tt_out = Tt_in*pid**((gamma-1)/(gamma)*etapold)
 
ht_out = Cp*Tt_out
 
Mach = np.sqrt((((Pt_out/Po)**((gamma-1)/gamma))-1)*2/(gamma-1))
 
-float i_low = Mach < 1.0
 
-float i_high = 1.0
 
-float P_out = 1.0 *Mach/Mach
 
T_out = Tt_out/(1+(gamma-1)/2*Mach*Mach)
 
h_out = Cp*T_out
 
u_out = np.sqrt(2*(ht_out-h_out))
 
-float rho_out = P_out/(R*T_out)
 
-tuple area_ratio = (fm_id(Mo)/fm_id(Mach)*(1/(Pt_out/Pto))*(np.sqrt(Tt_out/Tto)))
 
stagnation_temperature
 
stagnation_pressure
 
stagnation_enthalpy
 
mach_number
 
static_temperature
 
density
 
static_enthalpy
 
velocity
 
static_pressure
 
area_ratio
 
-

Detailed Description

-
This is a nozzle component intended for use in expansion.
-Calling this class calls the compute function.
-
-Assumptions:
-Pressure ratio and efficiency do not change with varying conditions.
-Subsonic or choked output.
-
-Source:
-https://web.stanford.edu/~cantwell/AA283_Course_Material/AA283_Course_Notes/
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle.__defaults__ ( self)
-
-
This sets the default values for the component to function.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-None
-
-
-
- -

◆ compute()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle.compute ( self,
 conditions 
)
-
-
This computes the output values from the input values according to
-equations from the source.
-
-Assumptions:
-Constant polytropic efficiency and pressure ratio
-
-Source:
-https://web.stanford.edu/~cantwell/AA283_Course_Material/AA283_Course_Notes/
-
-Inputs:
-conditions.freestream.
-  isentropic_expansion_factor         [-]
-  specific_heat_at_constant_pressure  [J/(kg K)]
-  pressure                            [Pa]
-  stagnation_pressure                 [Pa]
-  stagnation_temperature              [K]
-  universal_gas_constant              [J/(kg K)] (this is misnamed - actually refers to the gas specific constant)
-  mach_number                         [-]
-self.inputs.
-  stagnation_temperature              [K]
-  stagnation_pressure                 [Pa]
-
-Outputs:
-self.outputs.
-  stagnation_temperature              [K]  
-  stagnation_pressure                 [Pa]
-  stagnation_enthalpy                 [J/kg]
-  mach_number                         [-]
-  static_temperature                  [K]
-  static_enthalpy                     [J/kg]
-  velocity                            [m/s]
-  static_pressure                     [Pa]
-  area_ratio                          [-]
-  denisty                             [kg/m^3]
-
-Properties Used:
-self.
-  pressure_ratio                      [-]
-  polytropic_efficiency               [-]
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Energy/Converters/Expansion_Nozzle.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Expansion__Nozzle_1_1Expansion__Nozzle.js b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Expansion__Nozzle_1_1Expansion__Nozzle.js deleted file mode 100644 index d6923b1c..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Expansion__Nozzle_1_1Expansion__Nozzle.js +++ /dev/null @@ -1,8 +0,0 @@ -var classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Expansion__Nozzle_1_1Expansion__Nozzle = -[ - [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Expansion__Nozzle_1_1Expansion__Nozzle.html#aa2283a618471995ca158dc2df95a37dd", null ], - [ "compute", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Expansion__Nozzle_1_1Expansion__Nozzle.html#ac772d7eab1ab6775201959a298ceed80", null ], - [ "polytropic_efficiency", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Expansion__Nozzle_1_1Expansion__Nozzle.html#a00eeecbb4a61e72b2314d29e91bf639c", null ], - [ "pressure_ratio", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Expansion__Nozzle_1_1Expansion__Nozzle.html#add093947d1e4ced493e187e9466501b9", null ], - [ "tag", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Expansion__Nozzle_1_1Expansion__Nozzle.html#a83cec72ca64b4a51431d663051bd4a60", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Expansion__Nozzle_1_1Expansion__Nozzle.png b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Expansion__Nozzle_1_1Expansion__Nozzle.png deleted file mode 100644 index dfbd3cff..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Expansion__Nozzle_1_1Expansion__Nozzle.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Fan_1_1Fan-members.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Fan_1_1Fan-members.html deleted file mode 100644 index c3166470..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Fan_1_1Fan-members.html +++ /dev/null @@ -1,122 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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- - - - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Fan_1_1Fan.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Fan_1_1Fan.html deleted file mode 100644 index 145ff555..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Fan_1_1Fan.html +++ /dev/null @@ -1,284 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Components.Energy.Converters.Fan.Fan Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Energy.Converters.Fan.Fan Class Reference
-
-
-
-Inheritance diagram for SUAVE.Components.Energy.Converters.Fan.Fan:
-
-
- - -SUAVE.Components.Energy.Energy_Component.Energy_Component -SUAVE.Components.Physical_Component.Physical_Component -SUAVE.Components.Component.Component - -
- - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def compute (self, conditions)
 
- Public Member Functions inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

tag
 
polytropic_efficiency
 
pressure_ratio
 
- Public Attributes inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
inputs
 
outputs
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
-

Detailed Description

-
This is a fan component typically used in a turbofan.
-Calling this class calls the compute function.
-
-Assumptions:
-Pressure ratio and efficiency do not change with varying conditions.
-
-Source:
-https://web.stanford.edu/~cantwell/AA283_Course_Material/AA283_Course_Notes/
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Components.Energy.Converters.Fan.Fan.__defaults__ ( self)
-
-
This sets the default values for the component to function.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-None
-
-
-
- -

◆ compute()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Components.Energy.Converters.Fan.Fan.compute ( self,
 conditions 
)
-
-
This computes the output values from the input values according to
-equations from the source.
-
-Assumptions:
-Constant polytropic efficiency and pressure ratio
-
-Source:
-https://web.stanford.edu/~cantwell/AA283_Course_Material/AA283_Course_Notes/
-
-Inputs:
-conditions.freestream.
-  isentropic_expansion_factor         [-]
-  specific_heat_at_constant_pressure  [J/(kg K)]
-self.inputs.
-  stagnation_temperature              [K]
-  stagnation_pressure                 [Pa]
-
-Outputs:
-self.outputs.
-  stagnation_temperature              [K]  
-  stagnation_pressure                 [Pa]
-  stagnation_enthalpy                 [J/kg]
-  work_done                           [J/kg]
-
-Properties Used:
-self.
-  pressure_ratio                      [-]
-  polytropic_efficiency               [-]
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Energy/Converters/Fan.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Fan_1_1Fan.js b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Fan_1_1Fan.js deleted file mode 100644 index ed5a9440..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Fan_1_1Fan.js +++ /dev/null @@ -1,8 +0,0 @@ -var classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Fan_1_1Fan = -[ - [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Fan_1_1Fan.html#a0f79ff253e2c6f491817eb914ffd6c10", null ], - [ "compute", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Fan_1_1Fan.html#aec19dd67bde884b36912bfd8546f4c12", null ], - [ "polytropic_efficiency", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Fan_1_1Fan.html#a6cb8c9f1b278edadbf7f6622d148b12a", null ], - [ "pressure_ratio", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Fan_1_1Fan.html#a3d502283c993d3fd15074d281542e927", null ], - [ "tag", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Fan_1_1Fan.html#af99c54e607ce05b33355d2b16a9e1ccc", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Fan_1_1Fan.png b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Fan_1_1Fan.png deleted file mode 100644 index 8b9573b4..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Fan_1_1Fan.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Fuel__Cell_1_1Fuel__Cell-members.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Fuel__Cell_1_1Fuel__Cell-members.html deleted file mode 100644 index ff60a98d..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Fuel__Cell_1_1Fuel__Cell-members.html +++ /dev/null @@ -1,128 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Energy.Converters.Fuel_Cell.Fuel_Cell Member List
-
-
- -

This is the complete list of members for SUAVE.Components.Energy.Converters.Fuel_Cell.Fuel_Cell, including all inherited members.

- - - - - - - - - - - - - - - - - -
__defaults__(self)SUAVE.Components.Energy.Converters.Fuel_Cell.Fuel_Cell
discharge_model (defined in SUAVE.Components.Energy.Converters.Fuel_Cell.Fuel_Cell)SUAVE.Components.Energy.Converters.Fuel_Cell.Fuel_Cell
efficiency (defined in SUAVE.Components.Energy.Converters.Fuel_Cell.Fuel_Cell)SUAVE.Components.Energy.Converters.Fuel_Cell.Fuel_Cell
energy_calc(self, conditions, numerics)SUAVE.Components.Energy.Converters.Fuel_Cell.Fuel_Cell
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
mass_density (defined in SUAVE.Components.Energy.Converters.Fuel_Cell.Fuel_Cell)SUAVE.Components.Energy.Converters.Fuel_Cell.Fuel_Cell
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
max_power (defined in SUAVE.Components.Energy.Converters.Fuel_Cell.Fuel_Cell)SUAVE.Components.Energy.Converters.Fuel_Cell.Fuel_Cell
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
oxidizer (defined in SUAVE.Components.Energy.Converters.Fuel_Cell.Fuel_Cell)SUAVE.Components.Energy.Converters.Fuel_Cell.Fuel_Cell
propellant (defined in SUAVE.Components.Energy.Converters.Fuel_Cell.Fuel_Cell)SUAVE.Components.Energy.Converters.Fuel_Cell.Fuel_Cell
specific_power (defined in SUAVE.Components.Energy.Converters.Fuel_Cell.Fuel_Cell)SUAVE.Components.Energy.Converters.Fuel_Cell.Fuel_Cell
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
volume (defined in SUAVE.Components.Energy.Converters.Fuel_Cell.Fuel_Cell)SUAVE.Components.Energy.Converters.Fuel_Cell.Fuel_Cell
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Fuel__Cell_1_1Fuel__Cell.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Fuel__Cell_1_1Fuel__Cell.html deleted file mode 100644 index 4fb15241..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Fuel__Cell_1_1Fuel__Cell.html +++ /dev/null @@ -1,292 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Components.Energy.Converters.Fuel_Cell.Fuel_Cell Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
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- - - -
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- -
-
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- -
- -
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- - -
- -
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SUAVE.Components.Energy.Converters.Fuel_Cell.Fuel_Cell Class Reference
-
-
-
-Inheritance diagram for SUAVE.Components.Energy.Converters.Fuel_Cell.Fuel_Cell:
-
-
- - -SUAVE.Components.Energy.Energy_Component.Energy_Component -SUAVE.Components.Physical_Component.Physical_Component -SUAVE.Components.Component.Component - -
- - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def energy_calc (self, conditions, numerics)
 
- Public Member Functions inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

propellant
 
oxidizer
 
efficiency
 
specific_power
 
mass_density
 
volume
 
max_power
 
discharge_model
 
- Public Attributes inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
inputs
 
outputs
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
-

Detailed Description

-
This is a fuel cell component.
-
-Assumptions:
-None
-
-Source:
-None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Components.Energy.Converters.Fuel_Cell.Fuel_Cell.__defaults__ ( self)
-
-
This sets the default values for the component to function.
-
-Assumptions:
-None
-
-Source:
-Some default values come from a Nissan 2011 fuel cell
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-None
-
-
-
- -

◆ energy_calc()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Components.Energy.Converters.Fuel_Cell.Fuel_Cell.energy_calc ( self,
 conditions,
 numerics 
)
-
-
This call the assigned discharge method.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-see properties used
-
-Outputs:
-mdot     [kg/s] (units may change depending on selected model)
-
-Properties Used:
-self.discharge_model(self, conditions, numerics)
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Energy/Converters/Fuel_Cell.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Fuel__Cell_1_1Fuel__Cell.js b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Fuel__Cell_1_1Fuel__Cell.js deleted file mode 100644 index 4d31efb8..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Fuel__Cell_1_1Fuel__Cell.js +++ /dev/null @@ -1,13 +0,0 @@ -var classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Fuel__Cell_1_1Fuel__Cell = -[ - [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Fuel__Cell_1_1Fuel__Cell.html#abe578d251543e912d141bcab686b70dc", null ], - [ "energy_calc", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Fuel__Cell_1_1Fuel__Cell.html#aa55b712f2848b45a7dc585b3748a1e38", null ], - [ "discharge_model", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Fuel__Cell_1_1Fuel__Cell.html#a1c6c0c67bed289fb5492baa5c118d515", null ], - [ "efficiency", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Fuel__Cell_1_1Fuel__Cell.html#a10ae10b99028997d6748c923cf607d32", null ], - [ "mass_density", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Fuel__Cell_1_1Fuel__Cell.html#abbffffb8d21af81cccf8eb2810a8ab71", null ], - [ "max_power", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Fuel__Cell_1_1Fuel__Cell.html#ab05024911c72966fdb06831dba3f4ac9", null ], - [ "oxidizer", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Fuel__Cell_1_1Fuel__Cell.html#a94e61e1b970a8055d7633ff1f8905fb1", null ], - [ "propellant", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Fuel__Cell_1_1Fuel__Cell.html#ac3e739f257c3474b95aa329fabef2742", null ], - [ "specific_power", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Fuel__Cell_1_1Fuel__Cell.html#ac8f0dbdd5b2effcb502df4f49d3d331b", null ], - [ "volume", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Fuel__Cell_1_1Fuel__Cell.html#ace7f30d49433a748d4de4899f2e506e9", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Fuel__Cell_1_1Fuel__Cell.png b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Fuel__Cell_1_1Fuel__Cell.png deleted file mode 100644 index c7086ba5..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Fuel__Cell_1_1Fuel__Cell.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Gearbox_1_1Gearbox-members.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Gearbox_1_1Gearbox-members.html deleted file mode 100644 index 626da8df..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Gearbox_1_1Gearbox-members.html +++ /dev/null @@ -1,128 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Energy.Converters.Gearbox.Gearbox Member List
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This is the complete list of members for SUAVE.Components.Energy.Converters.Gearbox.Gearbox, including all inherited members.

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__defaults__(self)SUAVE.Components.Energy.Converters.Gearbox.Gearbox
compute(self)SUAVE.Components.Energy.Converters.Gearbox.Gearbox
efficiency (defined in SUAVE.Components.Energy.Converters.Gearbox.Gearbox)SUAVE.Components.Energy.Converters.Gearbox.Gearbox
gearwhell_radius1 (defined in SUAVE.Components.Energy.Converters.Gearbox.Gearbox)SUAVE.Components.Energy.Converters.Gearbox.Gearbox
gearwhell_radius2 (defined in SUAVE.Components.Energy.Converters.Gearbox.Gearbox)SUAVE.Components.Energy.Converters.Gearbox.Gearbox
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
mass_weight (defined in SUAVE.Components.Energy.Converters.Gearbox.Gearbox)SUAVE.Components.Energy.Converters.Gearbox.Gearbox
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
speed_1 (defined in SUAVE.Components.Energy.Converters.Gearbox.Gearbox)SUAVE.Components.Energy.Converters.Gearbox.Gearbox
speed_2 (defined in SUAVE.Components.Energy.Converters.Gearbox.Gearbox)SUAVE.Components.Energy.Converters.Gearbox.Gearbox
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Energy.Converters.Gearbox.Gearbox)SUAVE.Components.Energy.Converters.Gearbox.Gearbox
torque_1 (defined in SUAVE.Components.Energy.Converters.Gearbox.Gearbox)SUAVE.Components.Energy.Converters.Gearbox.Gearbox
torque_2 (defined in SUAVE.Components.Energy.Converters.Gearbox.Gearbox)SUAVE.Components.Energy.Converters.Gearbox.Gearbox
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Gearbox_1_1Gearbox.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Gearbox_1_1Gearbox.html deleted file mode 100644 index 801b9ee5..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Gearbox_1_1Gearbox.html +++ /dev/null @@ -1,287 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Components.Energy.Converters.Gearbox.Gearbox Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Energy.Converters.Gearbox.Gearbox Class Reference
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-Inheritance diagram for SUAVE.Components.Energy.Converters.Gearbox.Gearbox:
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-
- - -SUAVE.Components.Energy.Energy_Component.Energy_Component -SUAVE.Components.Physical_Component.Physical_Component -SUAVE.Components.Component.Component - -
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-Public Member Functions

def __defaults__ (self)
 
def compute (self)
 
- Public Member Functions inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
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-Public Attributes

tag
 
gearwhell_radius1
 
gearwhell_radius2
 
torque_1
 
torque_2
 
speed_1
 
speed_2
 
efficiency
 
mass_weight
 
- Public Attributes inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
inputs
 
outputs
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
-

Detailed Description

-
This is a gear box component.
-
-Assumptions:
-None
-
-Source:
-None
-

Member Function Documentation

- -

◆ __defaults__()

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def SUAVE.Components.Energy.Converters.Gearbox.Gearbox.__defaults__ ( self)
-
-
This sets the default values for the component to function.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
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-Outputs:
-None
-
-Properties Used:
-None
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- -

◆ compute()

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def SUAVE.Components.Energy.Converters.Gearbox.Gearbox.compute ( self)
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Computes gearbox values.
-
-Assumptions:
-None
-
-Source:
-None
-
-Inputs:
-see properties used
-
-Outputs:
-self.outputs.
-  rotation_speed    [radian/s]
-  torque            [Nm]
-  power             [W]
-
-Properties Used:
-self.
-  gearwhell_radius1 [m]
-  gearwhell_radius2 [m]
-  torque1           [Nm]
-  speed_1           [radian/s]
-  efficiency        [-]
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The documentation for this class was generated from the following file:
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  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Energy/Converters/Gearbox.py
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Gearbox_1_1Gearbox.js b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Gearbox_1_1Gearbox.js deleted file mode 100644 index 5aa34890..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Gearbox_1_1Gearbox.js +++ /dev/null @@ -1,14 +0,0 @@ -var classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Gearbox_1_1Gearbox = -[ - [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Gearbox_1_1Gearbox.html#aae942d6c125bcaf5be47aaf69f290fce", null ], - [ "compute", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Gearbox_1_1Gearbox.html#aad8e3af09759982461dd014ce41b6dea", null ], - [ "efficiency", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Gearbox_1_1Gearbox.html#a67d43cd1ee31af6aed137acaf266a400", null ], - [ "gearwhell_radius1", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Gearbox_1_1Gearbox.html#a07f3413bb27609d129bb15f0c7e029a2", null ], - [ "gearwhell_radius2", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Gearbox_1_1Gearbox.html#ab206d384c80a8004e3811a7ba7c74759", null ], - [ "mass_weight", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Gearbox_1_1Gearbox.html#a96816790fe81237581ef24cea5734aec", null ], - [ "speed_1", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Gearbox_1_1Gearbox.html#a25846e8c0f2b69438d3d0666177c6b57", null ], - [ "speed_2", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Gearbox_1_1Gearbox.html#ae4f4e5cbade217b0d81fd2f509095e13", null ], - [ "tag", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Gearbox_1_1Gearbox.html#ab95ab2b40d1e96c58aaab46ee1e532a1", null ], - [ "torque_1", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Gearbox_1_1Gearbox.html#ad3011a75aa077e352379d8d45bf2e5b2", null ], - [ "torque_2", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Gearbox_1_1Gearbox.html#a9e46ec723c2948f8514290edd4294d03", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Gearbox_1_1Gearbox.png b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Gearbox_1_1Gearbox.png deleted file mode 100644 index 33ede8f7..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Gearbox_1_1Gearbox.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor_1_1Motor-members.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor_1_1Motor-members.html deleted file mode 100644 index 70ffde86..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor_1_1Motor-members.html +++ /dev/null @@ -1,129 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Energy.Converters.Motor.Motor Member List
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This is the complete list of members for SUAVE.Components.Energy.Converters.Motor.Motor, including all inherited members.

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__defaults__(self)SUAVE.Components.Energy.Converters.Motor.Motor
current(self, conditions)SUAVE.Components.Energy.Converters.Motor.Motor
expected_current (defined in SUAVE.Components.Energy.Converters.Motor.Motor)SUAVE.Components.Energy.Converters.Motor.Motor
gear_ratio (defined in SUAVE.Components.Energy.Converters.Motor.Motor)SUAVE.Components.Energy.Converters.Motor.Motor
gearbox_efficiency (defined in SUAVE.Components.Energy.Converters.Motor.Motor)SUAVE.Components.Energy.Converters.Motor.Motor
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
no_load_current (defined in SUAVE.Components.Energy.Converters.Motor.Motor)SUAVE.Components.Energy.Converters.Motor.Motor
omega(self, conditions)SUAVE.Components.Energy.Converters.Motor.Motor
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
propeller_Cp (defined in SUAVE.Components.Energy.Converters.Motor.Motor)SUAVE.Components.Energy.Converters.Motor.Motor
propeller_radius (defined in SUAVE.Components.Energy.Converters.Motor.Motor)SUAVE.Components.Energy.Converters.Motor.Motor
resistance (defined in SUAVE.Components.Energy.Converters.Motor.Motor)SUAVE.Components.Energy.Converters.Motor.Motor
speed_constant (defined in SUAVE.Components.Energy.Converters.Motor.Motor)SUAVE.Components.Energy.Converters.Motor.Motor
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor_1_1Motor.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor_1_1Motor.html deleted file mode 100644 index a70b07da..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor_1_1Motor.html +++ /dev/null @@ -1,355 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Components.Energy.Converters.Motor.Motor Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Energy.Converters.Motor.Motor Class Reference
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-Inheritance diagram for SUAVE.Components.Energy.Converters.Motor.Motor:
-
-
- - -SUAVE.Components.Energy.Energy_Component.Energy_Component -SUAVE.Components.Physical_Component.Physical_Component -SUAVE.Components.Component.Component - -
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-Public Member Functions

def __defaults__ (self)
 
def omega (self, conditions)
 
def current (self, conditions)
 
- Public Member Functions inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
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-Public Attributes

resistance
 
no_load_current
 
speed_constant
 
propeller_radius
 
propeller_Cp
 
gear_ratio
 
gearbox_efficiency
 
expected_current
 
- Public Attributes inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
inputs
 
outputs
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
-

Detailed Description

-
This is a motor component.
-
-Assumptions:
-None
-
-Source:
-None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Components.Energy.Converters.Motor.Motor.__defaults__ ( self)
-
-
This sets the default values for the component to function.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-None
-
-
-
- -

◆ current()

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-
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def SUAVE.Components.Energy.Converters.Motor.Motor.current ( self,
 conditions 
)
-
-
Calculates the motor's current
-
-Assumptions:
-Cp (power coefficient) is constant
-
-Source:
-N/A
-
-Inputs:
-self.inputs.voltage    [V]
-
-Outputs:
-self.outputs.current   [A]
-conditions.
-  propulsion.etam      [-]
-i                      [A]
-
-Properties Used:
-self.
-  gear_ratio           [-]
-  speed_constant       [radian/s/V]
-  resistance           [ohm]
-  outputs.omega        [radian/s]
-  gearbox_efficiency   [-]
-  expected_current     [A]
-  no_load_current      [A]
-
-
-
- -

◆ omega()

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def SUAVE.Components.Energy.Converters.Motor.Motor.omega ( self,
 conditions 
)
-
-
Calculates the motor's rotation rate
-
-Assumptions:
-Cp (power coefficient) is constant
-
-Source:
-N/A
-
-Inputs:
-conditions.
-  freestream.velocity                    [m/s]
-  freestream.density                     [kg/m^3]
-  propulsion.propeller_power_coefficient [-]
-self.inputs.voltage                      [V]
-
-Outputs:
-self.outputs.
-  torque                                 [Nm]
-  omega                                  [radian/s]
-
-Properties Used:
-self.
-  resistance                             [ohms]
-  gearbox_efficiency                     [-]
-  expected_current                       [A]
-  no_load_current                        [A]
-  gear_ratio                             [-]
-  speed_constant                         [radian/s/V]
-  propeller_radius                       [m]
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Energy/Converters/Motor.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor_1_1Motor.js b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor_1_1Motor.js deleted file mode 100644 index c1dc914e..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor_1_1Motor.js +++ /dev/null @@ -1,14 +0,0 @@ -var classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor_1_1Motor = -[ - [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor_1_1Motor.html#af941ec8976ff2b39156a3e3ceb25f1fc", null ], - [ "current", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor_1_1Motor.html#a4f50c2270b78bede450b3e9db6c195f3", null ], - [ "omega", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor_1_1Motor.html#ad9ab86d7bab611ffdc596a6c65dc86c2", null ], - [ "expected_current", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor_1_1Motor.html#a4f7b6aa5b6e6bb31cfec03cbcf5aad35", null ], - [ "gear_ratio", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor_1_1Motor.html#a79e6c4ee71fb685fbd9bba825ec65b0d", null ], - [ "gearbox_efficiency", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor_1_1Motor.html#a3dcd5ec5090f588d31f63965299cd825", null ], - [ "no_load_current", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor_1_1Motor.html#a1f0b94313d59a16a6eea49a3d4e1311e", null ], - [ "propeller_Cp", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor_1_1Motor.html#a16cb7590afcba652e316f45f8a761a31", null ], - [ "propeller_radius", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor_1_1Motor.html#a683409fa2bccf383f2f54484848021d2", null ], - [ "resistance", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor_1_1Motor.html#a13e5285d973e90a3b4caea45ed2d9d55", null ], - [ "speed_constant", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor_1_1Motor.html#adea69680702442a7a3d8489722c208d6", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor_1_1Motor.png b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor_1_1Motor.png deleted file mode 100644 index 6eb44489..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor_1_1Motor.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__Lo__Fid_1_1Motor__Lo__Fid-members.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__Lo__Fid_1_1Motor__Lo__Fid-members.html deleted file mode 100644 index 8f1c3e5c..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__Lo__Fid_1_1Motor__Lo__Fid-members.html +++ /dev/null @@ -1,128 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Energy.Converters.Motor_Lo_Fid.Motor_Lo_Fid Member List
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-
- -

This is the complete list of members for SUAVE.Components.Energy.Converters.Motor_Lo_Fid.Motor_Lo_Fid, including all inherited members.

- - - - - - - - - - - - - - - - - -
__defaults__(self)SUAVE.Components.Energy.Converters.Motor_Lo_Fid.Motor_Lo_Fid
current(self, conditions)SUAVE.Components.Energy.Converters.Motor_Lo_Fid.Motor_Lo_Fid
expected_current (defined in SUAVE.Components.Energy.Converters.Motor_Lo_Fid.Motor_Lo_Fid)SUAVE.Components.Energy.Converters.Motor_Lo_Fid.Motor_Lo_Fid
gear_ratio (defined in SUAVE.Components.Energy.Converters.Motor_Lo_Fid.Motor_Lo_Fid)SUAVE.Components.Energy.Converters.Motor_Lo_Fid.Motor_Lo_Fid
gearbox_efficiency (defined in SUAVE.Components.Energy.Converters.Motor_Lo_Fid.Motor_Lo_Fid)SUAVE.Components.Energy.Converters.Motor_Lo_Fid.Motor_Lo_Fid
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
motor_efficiency (defined in SUAVE.Components.Energy.Converters.Motor_Lo_Fid.Motor_Lo_Fid)SUAVE.Components.Energy.Converters.Motor_Lo_Fid.Motor_Lo_Fid
no_load_current (defined in SUAVE.Components.Energy.Converters.Motor_Lo_Fid.Motor_Lo_Fid)SUAVE.Components.Energy.Converters.Motor_Lo_Fid.Motor_Lo_Fid
omega(self, conditions)SUAVE.Components.Energy.Converters.Motor_Lo_Fid.Motor_Lo_Fid
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
resistance (defined in SUAVE.Components.Energy.Converters.Motor_Lo_Fid.Motor_Lo_Fid)SUAVE.Components.Energy.Converters.Motor_Lo_Fid.Motor_Lo_Fid
speed_constant (defined in SUAVE.Components.Energy.Converters.Motor_Lo_Fid.Motor_Lo_Fid)SUAVE.Components.Energy.Converters.Motor_Lo_Fid.Motor_Lo_Fid
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__Lo__Fid_1_1Motor__Lo__Fid.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__Lo__Fid_1_1Motor__Lo__Fid.html deleted file mode 100644 index 82129564..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__Lo__Fid_1_1Motor__Lo__Fid.html +++ /dev/null @@ -1,350 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Components.Energy.Converters.Motor_Lo_Fid.Motor_Lo_Fid Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Energy.Converters.Motor_Lo_Fid.Motor_Lo_Fid Class Reference
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-
-Inheritance diagram for SUAVE.Components.Energy.Converters.Motor_Lo_Fid.Motor_Lo_Fid:
-
-
- - -SUAVE.Components.Energy.Energy_Component.Energy_Component -SUAVE.Components.Physical_Component.Physical_Component -SUAVE.Components.Component.Component - -
- - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def omega (self, conditions)
 
def current (self, conditions)
 
- Public Member Functions inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

resistance
 
no_load_current
 
speed_constant
 
gear_ratio
 
gearbox_efficiency
 
expected_current
 
motor_efficiency
 
- Public Attributes inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
inputs
 
outputs
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
-

Detailed Description

-
This is a low-fidelity motor component.
-
-Assumptions:
-None
-
-Source:
-None
-

Member Function Documentation

- -

◆ __defaults__()

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-
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def SUAVE.Components.Energy.Converters.Motor_Lo_Fid.Motor_Lo_Fid.__defaults__ ( self)
-
-
This sets the default values for the component to function.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-None
-
-
-
- -

◆ current()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Components.Energy.Converters.Motor_Lo_Fid.Motor_Lo_Fid.current ( self,
 conditions 
)
-
-
Calculates the motor's rotation rate
-    
-Assumptions:
-Cp (power coefficient) is constant
-    
-Source:
-N/A
-    
-Inputs:
-self.inputs.voltage    [V]
-    
-Outputs:
-self.outputs.current   [A]
-conditions.
-  propulsion.etam      [-]
-i                      [A]
-    
-Properties Used:
-self.
-  gear_ratio           [-]
-  speed_constant       [radian/s/V]
-  resistance           [ohm]
-  omega(conditions)    [radian/s] (calls the function)
-  gearbox_efficiency   [-]
-  expected_current     [A]
-  no_load_current      [A]
-
-
-
- -

◆ omega()

- -
-
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def SUAVE.Components.Energy.Converters.Motor_Lo_Fid.Motor_Lo_Fid.omega ( self,
 conditions 
)
-
-
Calculates the motor's rotation rate
-    
-Assumptions:
-Cp (power coefficient) is constant
-    
-Source:
-N/A
-    
-Inputs:
-conditions.
-  freestream.velocity                    [m/s]
-  freestream.density                     [kg/m^3]
-self.inputs.voltage                      [V]
-    
-Outputs:
-self.outputs.
-  torque                                 [Nm]
-  omega                                  [radian/s]
-    
-Properties Used:
-self.
-  resistance                             [ohms]
-  gearbox_efficiency                     [-]
-  expected_current                       [A]
-  no_load_current                        [A]
-  gear_ratio                             [-]
-  speed_constant                         [radian/s/V]
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Energy/Converters/Motor_Lo_Fid.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__Lo__Fid_1_1Motor__Lo__Fid.js b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__Lo__Fid_1_1Motor__Lo__Fid.js deleted file mode 100644 index a8da841a..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__Lo__Fid_1_1Motor__Lo__Fid.js +++ /dev/null @@ -1,13 +0,0 @@ -var classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__Lo__Fid_1_1Motor__Lo__Fid = -[ - [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__Lo__Fid_1_1Motor__Lo__Fid.html#a1b9bb23be0478adab9351cf9c715f123", null ], - [ "current", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__Lo__Fid_1_1Motor__Lo__Fid.html#a55ff976700d1e5f089b06bb788c7cbd1", null ], - [ "omega", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__Lo__Fid_1_1Motor__Lo__Fid.html#a0e3d5a3b41ca71612ed130bfc64fc132", null ], - [ "expected_current", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__Lo__Fid_1_1Motor__Lo__Fid.html#a8ee1e69ab8ae5631b88055efc3929f03", null ], - [ "gear_ratio", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__Lo__Fid_1_1Motor__Lo__Fid.html#a1a51a431aa3c7a764c4425df5ed6b2e8", null ], - [ "gearbox_efficiency", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__Lo__Fid_1_1Motor__Lo__Fid.html#a7cc17da0e703afd6ee2014f56b8852bd", null ], - [ "motor_efficiency", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__Lo__Fid_1_1Motor__Lo__Fid.html#aa153f6a56e0ac6c9fad72d00cb29e479", null ], - [ "no_load_current", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__Lo__Fid_1_1Motor__Lo__Fid.html#abc0ef203bdc48a1df5a063a2fdef0ba8", null ], - [ "resistance", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__Lo__Fid_1_1Motor__Lo__Fid.html#aafd9b227ddd7d6da1e0e6ee2edeea5db", null ], - [ "speed_constant", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__Lo__Fid_1_1Motor__Lo__Fid.html#a67aeabb364e970ae2009652abd33738d", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__Lo__Fid_1_1Motor__Lo__Fid.png b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__Lo__Fid_1_1Motor__Lo__Fid.png deleted file mode 100644 index 4ef12ae6..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__Lo__Fid_1_1Motor__Lo__Fid.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Propeller_1_1Propeller-members.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Propeller_1_1Propeller-members.html deleted file mode 100644 index 5afd2b48..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Propeller_1_1Propeller-members.html +++ /dev/null @@ -1,122 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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- - - - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Propeller_1_1Propeller.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Propeller_1_1Propeller.html deleted file mode 100644 index 9d78fc81..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Propeller_1_1Propeller.html +++ /dev/null @@ -1,302 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Components.Energy.Converters.Propeller.Propeller Class Reference - - - - - - - - - - - - - - - -
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SUAVE.Components.Energy.Converters.Propeller.Propeller Class Reference
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-Inheritance diagram for SUAVE.Components.Energy.Converters.Propeller.Propeller:
-
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- - -SUAVE.Components.Energy.Energy_Component.Energy_Component -SUAVE.Components.Physical_Component.Physical_Component -SUAVE.Components.Component.Component - -
- - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def spin (self, conditions)
 
- Public Member Functions inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
- - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

prop_attributes
 
thrust_angle
 
- Public Attributes inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
inputs
 
outputs
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
-

Detailed Description

-
This is a propeller component.
-
-Assumptions:
-None
-
-Source:
-None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Components.Energy.Converters.Propeller.Propeller.__defaults__ ( self)
-
-
This sets the default values for the component to function.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-None
-
-
-
- -

◆ spin()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Components.Energy.Converters.Propeller.Propeller.spin ( self,
 conditions 
)
-
-
Analyzes a propeller given geometry and operating conditions.
-
-Assumptions:
-per source
-
-Source:
-Qprop theory document
-
-Inputs:
-self.inputs.omega            [radian/s]
-conditions.freestream.
-  density                    [kg/m^3]
-  dynamic_viscosity          [kg/(m-s)]
-  speed_of_sound             [m/s]
-  temperature                [K]
-conditions.frames.
-  body.transform_to_inertial (rotation matrix)
-  inertial.velocity_vector   [m/s]
-conditions.propulsion.
-  throttle                   [-]
-
-Outputs:
-conditions.propulsion.acoustic_outputs.
-  number_sections            [-]
-  r0                         [m]
-  airfoil_chord              [m]
-  blades_number              [-]
-  propeller_diameter         [m]
-  drag_coefficient           [-]
-  lift_coefficient           [-]
-  omega                      [radian/s]
-  velocity                   [m/s]
-  thrust                     [N]
-  power                      [W]
-  mid_chord_aligment         [m] (distance from the mid chord to the line axis out of the center of the blade)
-conditions.propulsion.etap   [-]
-thrust                       [N]
-torque                       [Nm]
-power                        [W]
-Cp                           [-] (coefficient of power)
-
-Properties Used:
-self.prop_attributes.
-  number_blades              [-]
-  tip_radius                 [m]
-  hub_radius                 [m]
-  twist_distribution         [radians]
-  chord_distribution         [m]
-  mid_chord_aligment         [m] (distance from the mid chord to the line axis out of the center of the blade)
-self.thrust_angle            [radians]
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Energy/Converters/Propeller.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Propeller_1_1Propeller.js b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Propeller_1_1Propeller.js deleted file mode 100644 index c69a1727..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Propeller_1_1Propeller.js +++ /dev/null @@ -1,7 +0,0 @@ -var classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Propeller_1_1Propeller = -[ - [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Propeller_1_1Propeller.html#aad1f23ecbcb98693cc81e258edd4a783", null ], - [ "spin", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Propeller_1_1Propeller.html#a7a6c4f4d97b3c18c3f7ef5878803aa4e", null ], - [ "prop_attributes", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Propeller_1_1Propeller.html#a5b098880963977153526442dc3f3ebe1", null ], - [ "thrust_angle", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Propeller_1_1Propeller.html#acd508103c9560b9c36a71f9c99028827", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Propeller_1_1Propeller.png b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Propeller_1_1Propeller.png deleted file mode 100644 index 9272932f..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Propeller_1_1Propeller.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Propeller__Lo__Fid_1_1Propeller__Lo__Fid-members.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Propeller__Lo__Fid_1_1Propeller__Lo__Fid-members.html deleted file mode 100644 index 79fe4910..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Propeller__Lo__Fid_1_1Propeller__Lo__Fid-members.html +++ /dev/null @@ -1,122 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
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SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Energy.Converters.Propeller_Lo_Fid.Propeller_Lo_Fid Member List
-
- -
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Propeller__Lo__Fid_1_1Propeller__Lo__Fid.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Propeller__Lo__Fid_1_1Propeller__Lo__Fid.html deleted file mode 100644 index 5ceabd2b..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Propeller__Lo__Fid_1_1Propeller__Lo__Fid.html +++ /dev/null @@ -1,280 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Components.Energy.Converters.Propeller_Lo_Fid.Propeller_Lo_Fid Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
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- -
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SUAVE.Components.Energy.Converters.Propeller_Lo_Fid.Propeller_Lo_Fid Class Reference
-
-
-
-Inheritance diagram for SUAVE.Components.Energy.Converters.Propeller_Lo_Fid.Propeller_Lo_Fid:
-
-
- - -SUAVE.Components.Energy.Energy_Component.Energy_Component -SUAVE.Components.Physical_Component.Physical_Component -SUAVE.Components.Component.Component - -
- - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def spin (self, conditions)
 
- Public Member Functions inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
- - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

tip_radius
 
propulsive_efficiency
 
- Public Attributes inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
inputs
 
outputs
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
-

Detailed Description

-
This is a low-fidelity propeller component.
-
-Assumptions:
-None
-
-Source:
-None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Components.Energy.Converters.Propeller_Lo_Fid.Propeller_Lo_Fid.__defaults__ ( self)
-
-
This sets the default values for the component to function.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-None
-
-
-
- -

◆ spin()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Components.Energy.Converters.Propeller_Lo_Fid.Propeller_Lo_Fid.spin ( self,
 conditions 
)
-
-
Analyzes a propeller given geometry and operating conditions.
-
-Assumptions:
-per source
-
-Source:
-Qprop theory document
-
-Inputs:
-self.inputs.omega            [radian/s]
-self.inputs.torque           [Nm]
-conditions.freestream.
-  density                    [kg/m^3]
-  dynamic_viscosity          [kg/(m-s)]
-  velocity                   [m/s]
-  speed_of_sound             [m/s]
-  temperature                [K]
-
-Outputs:
-conditions.propulsion.etap   [-]  (propulsive efficiency)
-thrust                       [N]
-Qm                           [Nm] (torque)
-power                        [W]
-Cp                           [-]  (coefficient of power)
-
-Properties Used:
-self.tip_radius              [m]
-self.propulsive_efficiency   [-]
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Energy/Converters/Propeller_Lo_Fid.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Propeller__Lo__Fid_1_1Propeller__Lo__Fid.js b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Propeller__Lo__Fid_1_1Propeller__Lo__Fid.js deleted file mode 100644 index 618982d8..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Propeller__Lo__Fid_1_1Propeller__Lo__Fid.js +++ /dev/null @@ -1,7 +0,0 @@ -var classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Propeller__Lo__Fid_1_1Propeller__Lo__Fid = -[ - [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Propeller__Lo__Fid_1_1Propeller__Lo__Fid.html#a94edbec39894815f56920b17b59d480d", null ], - [ "spin", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Propeller__Lo__Fid_1_1Propeller__Lo__Fid.html#a02f4c09ac47354fdd7662ae01e7deede", null ], - [ "propulsive_efficiency", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Propeller__Lo__Fid_1_1Propeller__Lo__Fid.html#ab832b1290a84db4fe9afacf106b2ab37", null ], - [ "tip_radius", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Propeller__Lo__Fid_1_1Propeller__Lo__Fid.html#aae1acf19e4556d7ab0a0026fddcf97d9", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Propeller__Lo__Fid_1_1Propeller__Lo__Fid.png b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Propeller__Lo__Fid_1_1Propeller__Lo__Fid.png deleted file mode 100644 index b6151364..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Propeller__Lo__Fid_1_1Propeller__Lo__Fid.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Ram_1_1Ram-members.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Ram_1_1Ram-members.html deleted file mode 100644 index 9d1cde17..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Ram_1_1Ram-members.html +++ /dev/null @@ -1,120 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
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- - - - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Ram_1_1Ram.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Ram_1_1Ram.html deleted file mode 100644 index e4f948b2..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Ram_1_1Ram.html +++ /dev/null @@ -1,283 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Components.Energy.Converters.Ram.Ram Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Energy.Converters.Ram.Ram Class Reference
-
-
-
-Inheritance diagram for SUAVE.Components.Energy.Converters.Ram.Ram:
-
-
- - -SUAVE.Components.Energy.Energy_Component.Energy_Component -SUAVE.Components.Physical_Component.Physical_Component -SUAVE.Components.Component.Component - -
- - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def compute (self, conditions)
 
- Public Member Functions inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
- - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

tag
 
- Public Attributes inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
inputs
 
outputs
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
-

Detailed Description

-
This represent the compression of incoming air flow.
-Calling this class calls the compute function.
-
-Assumptions:
-None
-
-Source:
-https://web.stanford.edu/~cantwell/AA283_Course_Material/AA283_Course_Notes/
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Components.Energy.Converters.Ram.Ram.__defaults__ ( self)
-
-
This sets the default values for the component to function.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-None
-
-
-
- -

◆ compute()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Components.Energy.Converters.Ram.Ram.compute ( self,
 conditions 
)
-
-
This computes the output values from the input values according to
-equations from the source.
-
-Assumptions:
-None
-
-Source:
-https://web.stanford.edu/~cantwell/AA283_Course_Material/AA283_Course_Notes/
-
-Inputs:
-conditions.freestream.
-  pressure
-  temperature
-  mach_number
-self.inputs.working_fluid
-
-Outputs:
-self.outputs.
-  stagnation_temperature              [K]  
-  stagnation_pressure                 [Pa]
-  isentropic_expansion_factor         [-]
-  specific_heat_at_constant_pressure  [J/(kg K)]
-  universal_gas_constant              [J/(kg K)]
-conditions.freestream.
-  stagnation_temperature              [K]
-  stagnation_pressure                 [Pa]
-  isentropic_expansion_factor         [-]
-  specific_heat_at_constant_pressure  [J/(kg K)]
-  universal_gas_constant              [J/(kg K)]
-  speed_of_sound                      [m/s]
-
-Properties Used:
-None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Energy/Converters/Ram.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Ram_1_1Ram.js b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Ram_1_1Ram.js deleted file mode 100644 index 27dd59da..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Ram_1_1Ram.js +++ /dev/null @@ -1,6 +0,0 @@ -var classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Ram_1_1Ram = -[ - [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Ram_1_1Ram.html#a85e86fecc0f9cf2aac3ebbcfef7caf04", null ], - [ "compute", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Ram_1_1Ram.html#a2a68e39407e5fcf664264ff0faaf071b", null ], - [ "tag", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Ram_1_1Ram.html#aef27226649962c1bf79c9281ee407803", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Ram_1_1Ram.png b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Ram_1_1Ram.png deleted file mode 100644 index f76e4f8a..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Ram_1_1Ram.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Shaft__Power__Off__Take_1_1Shaft__Power__Off__Take-members.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Shaft__Power__Off__Take_1_1Shaft__Power__Off__Take-members.html deleted file mode 100644 index 7985b133..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Shaft__Power__Off__Take_1_1Shaft__Power__Off__Take-members.html +++ /dev/null @@ -1,123 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Energy.Converters.Shaft_Power_Off_Take.Shaft_Power_Off_Take Member List
-
-
- -

This is the complete list of members for SUAVE.Components.Energy.Converters.Shaft_Power_Off_Take.Shaft_Power_Off_Take, including all inherited members.

- - - - - - - - - - - - -
__defaults__(self)SUAVE.Components.Energy.Converters.Shaft_Power_Off_Take.Shaft_Power_Off_Take
compute(self, state)SUAVE.Components.Energy.Converters.Shaft_Power_Off_Take.Shaft_Power_Off_Take
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
power_draw (defined in SUAVE.Components.Energy.Converters.Shaft_Power_Off_Take.Shaft_Power_Off_Take)SUAVE.Components.Energy.Converters.Shaft_Power_Off_Take.Shaft_Power_Off_Take
reference_pressure (defined in SUAVE.Components.Energy.Converters.Shaft_Power_Off_Take.Shaft_Power_Off_Take)SUAVE.Components.Energy.Converters.Shaft_Power_Off_Take.Shaft_Power_Off_Take
reference_temperature (defined in SUAVE.Components.Energy.Converters.Shaft_Power_Off_Take.Shaft_Power_Off_Take)SUAVE.Components.Energy.Converters.Shaft_Power_Off_Take.Shaft_Power_Off_Take
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Shaft__Power__Off__Take_1_1Shaft__Power__Off__Take.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Shaft__Power__Off__Take_1_1Shaft__Power__Off__Take.html deleted file mode 100644 index 4c0b224f..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Shaft__Power__Off__Take_1_1Shaft__Power__Off__Take.html +++ /dev/null @@ -1,276 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Components.Energy.Converters.Shaft_Power_Off_Take.Shaft_Power_Off_Take Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
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- - - - - - -
-
-
- - - -
-
- -
-
-
- -
- -
-
- - -
- -
- -
- -
-
SUAVE.Components.Energy.Converters.Shaft_Power_Off_Take.Shaft_Power_Off_Take Class Reference
-
-
-
-Inheritance diagram for SUAVE.Components.Energy.Converters.Shaft_Power_Off_Take.Shaft_Power_Off_Take:
-
-
- - -SUAVE.Components.Energy.Energy_Component.Energy_Component -SUAVE.Components.Physical_Component.Physical_Component -SUAVE.Components.Component.Component - -
- - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def compute (self, state)
 
- Public Member Functions inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

power_draw
 
reference_temperature
 
reference_pressure
 
- Public Attributes inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
inputs
 
outputs
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
-

Detailed Description

-
This is a component representing the power draw from the shaft.
-
-Assumptions:
-None
-
-Source:
-None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Components.Energy.Converters.Shaft_Power_Off_Take.Shaft_Power_Off_Take.__defaults__ ( self)
-
-
This sets the default values for the component to function.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-None
-
-
-
- -

◆ compute()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Components.Energy.Converters.Shaft_Power_Off_Take.Shaft_Power_Off_Take.compute ( self,
 state 
)
-
-
This computes the work done from the power draw.
-
-Assumptions:
-None
-
-Source:
-https://web.stanford.edu/~cantwell/AA283_Course_Material/AA283_Course_Notes/
-
-Inputs:
-self.inputs.
-  mdhc                  [-] Compressor nondimensional mass flow
-  reference_temperature [K]
-  reference_pressure    [Pa]
-
-Outputs:
-self.outputs.
-  power                 [W]
-  work_done             [J/kg] (if power draw is not zero)
-
-Properties Used:
-self.power_draw         [W]
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Energy/Converters/Shaft_Power_Off_Take.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Shaft__Power__Off__Take_1_1Shaft__Power__Off__Take.js b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Shaft__Power__Off__Take_1_1Shaft__Power__Off__Take.js deleted file mode 100644 index 1e13dd8a..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Shaft__Power__Off__Take_1_1Shaft__Power__Off__Take.js +++ /dev/null @@ -1,8 +0,0 @@ -var classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Shaft__Power__Off__Take_1_1Shaft__Power__Off__Take = -[ - [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Shaft__Power__Off__Take_1_1Shaft__Power__Off__Take.html#a8c2af7487923df0d19f2f30c048f9297", null ], - [ "compute", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Shaft__Power__Off__Take_1_1Shaft__Power__Off__Take.html#ac70d45b4f2ef3f91ac3fe418a1740c0c", null ], - [ "power_draw", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Shaft__Power__Off__Take_1_1Shaft__Power__Off__Take.html#af621d82d7fb79c2af8513b699c79db24", null ], - [ "reference_pressure", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Shaft__Power__Off__Take_1_1Shaft__Power__Off__Take.html#a25f149218b754c708af1a0b5c0b5ccd9", null ], - [ "reference_temperature", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Shaft__Power__Off__Take_1_1Shaft__Power__Off__Take.html#a9848ee4c441bda08ec5aa6d38ea67290", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Shaft__Power__Off__Take_1_1Shaft__Power__Off__Take.png b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Shaft__Power__Off__Take_1_1Shaft__Power__Off__Take.png deleted file mode 100644 index 5abd6068..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Shaft__Power__Off__Take_1_1Shaft__Power__Off__Take.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Solar__Panel_1_1Solar__Panel-members.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Solar__Panel_1_1Solar__Panel-members.html deleted file mode 100644 index fa294e5d..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Solar__Panel_1_1Solar__Panel-members.html +++ /dev/null @@ -1,122 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
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- - - - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Solar__Panel_1_1Solar__Panel.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Solar__Panel_1_1Solar__Panel.html deleted file mode 100644 index 4bb8f8d4..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Solar__Panel_1_1Solar__Panel.html +++ /dev/null @@ -1,267 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Components.Energy.Converters.Solar_Panel.Solar_Panel Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Energy.Converters.Solar_Panel.Solar_Panel Class Reference
-
-
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-

Solar_Panel Class

- - More...

-
-Inheritance diagram for SUAVE.Components.Energy.Converters.Solar_Panel.Solar_Panel:
-
-
- - -SUAVE.Components.Energy.Energy_Component.Energy_Component -SUAVE.Components.Physical_Component.Physical_Component -SUAVE.Components.Component.Component - -
- - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def power (self)
 
- Public Member Functions inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
- - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

area
 
efficiency
 
- Public Attributes inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
inputs
 
outputs
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
-

Detailed Description

-

-

Solar_Panel Class

-
This is a solar cell component.
-
-Assumptions:
-None
-
-Source:
-None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Components.Energy.Converters.Solar_Panel.Solar_Panel.__defaults__ ( self)
-
-
This sets the default values for the component to function.
-
-Assumptions:
-None
-
-Source:
-None
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-None
-
-
-
- -

◆ power()

- -
-
- - - - - - - - -
def SUAVE.Components.Energy.Converters.Solar_Panel.Solar_Panel.power ( self)
-
-
This determines the power output of the solar cell.
-
-Assumptions:
-None
-
-Source:
-None
-
-Inputs:
-self.inputs.flux   [W/m^2]
-
-Outputs:
-self.outputs.power [W]
-power              [W]
-
-Properties Used:
-self.efficiency    [-]
-self.area          [m^2]
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Energy/Converters/Solar_Panel.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Solar__Panel_1_1Solar__Panel.js b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Solar__Panel_1_1Solar__Panel.js deleted file mode 100644 index 59b93d52..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Solar__Panel_1_1Solar__Panel.js +++ /dev/null @@ -1,7 +0,0 @@ -var classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Solar__Panel_1_1Solar__Panel = -[ - [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Solar__Panel_1_1Solar__Panel.html#a8a1a7584c2190bfa6a71b6fb5473f09a", null ], - [ "power", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Solar__Panel_1_1Solar__Panel.html#a879b1ad3e7da54e24d69cdc1cfdb9574", null ], - [ "area", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Solar__Panel_1_1Solar__Panel.html#af986c69828364cb9c66556c69f31f807", null ], - [ "efficiency", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Solar__Panel_1_1Solar__Panel.html#a9db5c21e0456ce47a64cfdcb35bf060e", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Solar__Panel_1_1Solar__Panel.png b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Solar__Panel_1_1Solar__Panel.png deleted file mode 100644 index 9cb17490..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Solar__Panel_1_1Solar__Panel.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Supersonic__Nozzle_1_1Supersonic__Nozzle-members.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Supersonic__Nozzle_1_1Supersonic__Nozzle-members.html deleted file mode 100644 index d917a183..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Supersonic__Nozzle_1_1Supersonic__Nozzle-members.html +++ /dev/null @@ -1,122 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
-
- - - -
-
- -
-
-
- -
- -
-
- - -
- -
- -
-
-
SUAVE.Components.Energy.Converters.Supersonic_Nozzle.Supersonic_Nozzle Member List
-
-
- -

This is the complete list of members for SUAVE.Components.Energy.Converters.Supersonic_Nozzle.Supersonic_Nozzle, including all inherited members.

- - - - - - - - - - - -
__defaults__(self)SUAVE.Components.Energy.Converters.Supersonic_Nozzle.Supersonic_Nozzle
compute(self, conditions)SUAVE.Components.Energy.Converters.Supersonic_Nozzle.Supersonic_Nozzle
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
polytropic_efficiency (defined in SUAVE.Components.Energy.Converters.Supersonic_Nozzle.Supersonic_Nozzle)SUAVE.Components.Energy.Converters.Supersonic_Nozzle.Supersonic_Nozzle
pressure_ratio (defined in SUAVE.Components.Energy.Converters.Supersonic_Nozzle.Supersonic_Nozzle)SUAVE.Components.Energy.Converters.Supersonic_Nozzle.Supersonic_Nozzle
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Energy.Converters.Supersonic_Nozzle.Supersonic_Nozzle)SUAVE.Components.Energy.Converters.Supersonic_Nozzle.Supersonic_Nozzle
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Supersonic__Nozzle_1_1Supersonic__Nozzle.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Supersonic__Nozzle_1_1Supersonic__Nozzle.html deleted file mode 100644 index 6b21b1fb..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Supersonic__Nozzle_1_1Supersonic__Nozzle.html +++ /dev/null @@ -1,294 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Components.Energy.Converters.Supersonic_Nozzle.Supersonic_Nozzle Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
-
- - - -
-
- -
-
-
- -
- -
-
- - -
- -
- -
- -
-
SUAVE.Components.Energy.Converters.Supersonic_Nozzle.Supersonic_Nozzle Class Reference
-
-
-
-Inheritance diagram for SUAVE.Components.Energy.Converters.Supersonic_Nozzle.Supersonic_Nozzle:
-
-
- - -SUAVE.Components.Energy.Energy_Component.Energy_Component -SUAVE.Components.Physical_Component.Physical_Component -SUAVE.Components.Component.Component - -
- - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def compute (self, conditions)
 
- Public Member Functions inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

tag
 
polytropic_efficiency
 
pressure_ratio
 
- Public Attributes inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
inputs
 
outputs
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
-

Detailed Description

-
This is a nozzle component that allows for supersonic outflow.
-Calling this class calls the compute function.
-
-Assumptions:
-Pressure ratio and efficiency do not change with varying conditions.
-
-Source:
-https://web.stanford.edu/~cantwell/AA283_Course_Material/AA283_Course_Notes/
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Components.Energy.Converters.Supersonic_Nozzle.Supersonic_Nozzle.__defaults__ ( self)
-
-
This sets the default values for the component to function.
-
-Assumptions:
-None
-    
-Source:
-N/A
-    
-Inputs:
-None
-    
-Outputs:
-None
-    
-Properties Used:
-None
-
-
-
- -

◆ compute()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Components.Energy.Converters.Supersonic_Nozzle.Supersonic_Nozzle.compute ( self,
 conditions 
)
-
-
This computes the output values from the input values according to
-equations from the source.
-
-Assumptions:
-Constant polytropic efficiency and pressure ratio
-
-Source:
-https://web.stanford.edu/~cantwell/AA283_Course_Material/AA283_Course_Notes/
-
-Inputs:
-conditions.freestream.
-  isentropic_expansion_factor         [-]
-  specific_heat_at_constant_pressure  [J/(kg K)]
-  pressure                            [Pa]
-  stagnation_pressure                 [Pa]
-  stagnation_temperature              [K]
-  universal_gas_constant              [J/(kg K)] (this is misnamed - actually refers to the gas specific constant)
-  mach_number                         [-]
-self.inputs.
-  stagnation_temperature              [K]
-  stagnation_pressure                 [Pa]
-   
-Outputs:
-self.outputs.
-  stagnation_temperature              [K]  
-  stagnation_pressure                 [Pa]
-  stagnation_enthalpy                 [J/kg]
-  mach_number                         [-]
-  static_temperature                  [K]
-  static_enthalpy                     [J/kg]
-  velocity                            [m/s]
-  static_pressure                     [Pa]
-  area_ratio                          [-]
-
-Properties Used:
-self.
-  pressure_ratio                      [-]
-  polytropic_efficiency               [-]
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Energy/Converters/Supersonic_Nozzle.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Supersonic__Nozzle_1_1Supersonic__Nozzle.js b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Supersonic__Nozzle_1_1Supersonic__Nozzle.js deleted file mode 100644 index 5e9b48e1..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Supersonic__Nozzle_1_1Supersonic__Nozzle.js +++ /dev/null @@ -1,8 +0,0 @@ -var classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Supersonic__Nozzle_1_1Supersonic__Nozzle = -[ - [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Supersonic__Nozzle_1_1Supersonic__Nozzle.html#a861ed50883715716b13cf3d2e21e8ede", null ], - [ "compute", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Supersonic__Nozzle_1_1Supersonic__Nozzle.html#a2356fafa6315dd101857f0d18b95098e", null ], - [ "polytropic_efficiency", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Supersonic__Nozzle_1_1Supersonic__Nozzle.html#af9f1fbb06060df1c3b0af8f339c2ab9f", null ], - [ "pressure_ratio", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Supersonic__Nozzle_1_1Supersonic__Nozzle.html#a781262fe820e701c453715717494bbb9", null ], - [ "tag", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Supersonic__Nozzle_1_1Supersonic__Nozzle.html#a7bf619594c30ca8ea126f5e0b5177d0a", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Supersonic__Nozzle_1_1Supersonic__Nozzle.png b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Supersonic__Nozzle_1_1Supersonic__Nozzle.png deleted file mode 100644 index 1a535920..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Supersonic__Nozzle_1_1Supersonic__Nozzle.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Turbine_1_1Turbine-members.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Turbine_1_1Turbine-members.html deleted file mode 100644 index fcc2e655..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Turbine_1_1Turbine-members.html +++ /dev/null @@ -1,122 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
-
- - - -
-
- -
-
-
- - - - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Turbine_1_1Turbine.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Turbine_1_1Turbine.html deleted file mode 100644 index cac7ac51..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Turbine_1_1Turbine.html +++ /dev/null @@ -1,288 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Components.Energy.Converters.Turbine.Turbine Class Reference - - - - - - - - - - - - - - - -
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- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Energy.Converters.Turbine.Turbine Class Reference
-
-
-
-Inheritance diagram for SUAVE.Components.Energy.Converters.Turbine.Turbine:
-
-
- - -SUAVE.Components.Energy.Energy_Component.Energy_Component -SUAVE.Components.Physical_Component.Physical_Component -SUAVE.Components.Component.Component - -
- - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def compute (self, conditions)
 
- Public Member Functions inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

tag
 
mechanical_efficiency
 
polytropic_efficiency
 
- Public Attributes inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
inputs
 
outputs
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
-

Detailed Description

-
This is a turbine component typically used in a turbofan.
-Calling this class calls the compute function.
-
-Assumptions:
-Efficiencies do not change with varying conditions.
-
-Source:
-https://web.stanford.edu/~cantwell/AA283_Course_Material/AA283_Course_Notes/
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Components.Energy.Converters.Turbine.Turbine.__defaults__ ( self)
-
-
This sets the default values for the component to function.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-None
-
-
-
- -

◆ compute()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Components.Energy.Converters.Turbine.Turbine.compute ( self,
 conditions 
)
-
-
This computes the output values from the input values according to
-equations from the source.
-
-Assumptions:
-Constant polytropic efficiency and pressure ratio
-
-Source:
-https://web.stanford.edu/~cantwell/AA283_Course_Material/AA283_Course_Notes/
-
-Inputs:
-conditions.freestream.
-  isentropic_expansion_factor         [-]
-  specific_heat_at_constant_pressure  [J/(kg K)]
-self.inputs.
-  stagnation_temperature              [K]
-  stagnation_pressure                 [Pa]
-  bypass_ratio                        [-]
-  fuel_to_air_ratio                   [-]
-  compressor.work_done                [J/kg]
-  fan.work_done                       [J/kg]
-  shaft_power_off_take.work_done      [J/kg]
-
-Outputs:
-self.outputs.
-  stagnation_temperature              [K]  
-  stagnation_pressure                 [Pa]
-  stagnation_enthalpy                 [J/kg]
-
-Properties Used:
-self.
-  mechanical_efficiency               [-]
-  polytropic_efficiency               [-]
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Energy/Converters/Turbine.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Turbine_1_1Turbine.js b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Turbine_1_1Turbine.js deleted file mode 100644 index 292d4947..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Turbine_1_1Turbine.js +++ /dev/null @@ -1,8 +0,0 @@ -var classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Turbine_1_1Turbine = -[ - [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Turbine_1_1Turbine.html#a81e69a599da16a271a72471d4147335a", null ], - [ "compute", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Turbine_1_1Turbine.html#a74c47863b401000230e9de230cadb38f", null ], - [ "mechanical_efficiency", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Turbine_1_1Turbine.html#a90ad790cc69e261b61cbcb157bd49e97", null ], - [ "polytropic_efficiency", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Turbine_1_1Turbine.html#a53934300dc270755531c70dd55414f25", null ], - [ "tag", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Turbine_1_1Turbine.html#ae88373b058988671c08ab795093a403b", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Turbine_1_1Turbine.png b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Turbine_1_1Turbine.png deleted file mode 100644 index 11915a0d..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Turbine_1_1Turbine.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Electronic__Speed__Controller_1_1Electronic__Speed__Controller-members.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Electronic__Speed__Controller_1_1Electronic__Speed__Controller-members.html deleted file mode 100644 index 911d2229..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Electronic__Speed__Controller_1_1Electronic__Speed__Controller-members.html +++ /dev/null @@ -1,122 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
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SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Energy.Distributors.Electronic_Speed_Controller.Electronic_Speed_Controller Member List
-
-
- -

This is the complete list of members for SUAVE.Components.Energy.Distributors.Electronic_Speed_Controller.Electronic_Speed_Controller, including all inherited members.

- - - - - - - - - - - -
__defaults__(self)SUAVE.Components.Energy.Distributors.Electronic_Speed_Controller.Electronic_Speed_Controller
currentin(self)SUAVE.Components.Energy.Distributors.Electronic_Speed_Controller.Electronic_Speed_Controller
efficiency (defined in SUAVE.Components.Energy.Distributors.Electronic_Speed_Controller.Electronic_Speed_Controller)SUAVE.Components.Energy.Distributors.Electronic_Speed_Controller.Electronic_Speed_Controller
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
voltageout(self, conditions)SUAVE.Components.Energy.Distributors.Electronic_Speed_Controller.Electronic_Speed_Controller
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Electronic__Speed__Controller_1_1Electronic__Speed__Controller.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Electronic__Speed__Controller_1_1Electronic__Speed__Controller.html deleted file mode 100644 index 47b4ef20..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Electronic__Speed__Controller_1_1Electronic__Speed__Controller.html +++ /dev/null @@ -1,289 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Components.Energy.Distributors.Electronic_Speed_Controller.Electronic_Speed_Controller Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
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-
- - - -
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-
- - -
- -
- -
- -
-
SUAVE.Components.Energy.Distributors.Electronic_Speed_Controller.Electronic_Speed_Controller Class Reference
-
-
-
-Inheritance diagram for SUAVE.Components.Energy.Distributors.Electronic_Speed_Controller.Electronic_Speed_Controller:
-
-
- - -SUAVE.Components.Energy.Energy_Component.Energy_Component -SUAVE.Components.Physical_Component.Physical_Component -SUAVE.Components.Component.Component - -
- - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def voltageout (self, conditions)
 
def currentin (self)
 
- Public Member Functions inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
- - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

efficiency
 
- Public Attributes inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
inputs
 
outputs
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Components.Energy.Distributors.Electronic_Speed_Controller.Electronic_Speed_Controller.__defaults__ ( self)
-
-
This sets the default values.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
- -

◆ currentin()

- -
-
- - - - - - - - -
def SUAVE.Components.Energy.Distributors.Electronic_Speed_Controller.Electronic_Speed_Controller.currentin ( self)
-
-
The current going into the speed controller
-
-    Assumptions:
-The ESC draws current.
-    
-    Inputs:
-self.inputs.currentout [amps]
-       
-    Outputs:
-outputs.currentin      [amps]
-    
-    Properties Used:
-self.efficiency - [0-1] efficiency of the ESC
-
-
- -

◆ voltageout()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Components.Energy.Distributors.Electronic_Speed_Controller.Electronic_Speed_Controller.voltageout ( self,
 conditions 
)
-
-
The voltage out of the electronic speed controller
-
-    Assumptions:
-    The ESC's output voltage is linearly related to throttle setting
-    
-    Source:
-    N/A
-    
-    Inputs:
-    conditions.propulsion.throttle [0-1] 
-    self.inputs.voltage            [volts]
-    
-    Outputs:
-    voltsout                       [volts]
-    self.outputs.voltageout        [volts]
-    
-    Properties Used:
-    None
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Energy/Distributors/Electronic_Speed_Controller.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Electronic__Speed__Controller_1_1Electronic__Speed__Controller.js b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Electronic__Speed__Controller_1_1Electronic__Speed__Controller.js deleted file mode 100644 index 0528f68e..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Electronic__Speed__Controller_1_1Electronic__Speed__Controller.js +++ /dev/null @@ -1,7 +0,0 @@ -var classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Electronic__Speed__Controller_1_1Electronic__Speed__Controller = -[ - [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Electronic__Speed__Controller_1_1Electronic__Speed__Controller.html#ade7b4c9066bfdee04532a683a20849b7", null ], - [ "currentin", "classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Electronic__Speed__Controller_1_1Electronic__Speed__Controller.html#ad8605cbf070de0139fee6ece5116580f", null ], - [ "voltageout", "classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Electronic__Speed__Controller_1_1Electronic__Speed__Controller.html#a59e19c06939c4420d52a3f645e9b0c20", null ], - [ "efficiency", "classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Electronic__Speed__Controller_1_1Electronic__Speed__Controller.html#af2049585ddd8e6ba97dc13591526b273", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Electronic__Speed__Controller_1_1Electronic__Speed__Controller.png b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Electronic__Speed__Controller_1_1Electronic__Speed__Controller.png deleted file mode 100644 index eef1d90f..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Electronic__Speed__Controller_1_1Electronic__Speed__Controller.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Solar__Logic_1_1Solar__Logic-members.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Solar__Logic_1_1Solar__Logic-members.html deleted file mode 100644 index 02fff4fd..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Solar__Logic_1_1Solar__Logic-members.html +++ /dev/null @@ -1,123 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
-
- - - -
-
- -
-
-
- -
- -
-
- - -
- -
- -
-
-
SUAVE.Components.Energy.Distributors.Solar_Logic.Solar_Logic Member List
-
- -
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Solar__Logic_1_1Solar__Logic.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Solar__Logic_1_1Solar__Logic.html deleted file mode 100644 index 0b339b20..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Solar__Logic_1_1Solar__Logic.html +++ /dev/null @@ -1,321 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Components.Energy.Distributors.Solar_Logic.Solar_Logic Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
-
- - - -
-
- -
-
-
- -
- -
-
- - -
- -
- -
- -
-
SUAVE.Components.Energy.Distributors.Solar_Logic.Solar_Logic Class Reference
-
-
-
-Inheritance diagram for SUAVE.Components.Energy.Distributors.Solar_Logic.Solar_Logic:
-
-
- - -SUAVE.Components.Energy.Energy_Component.Energy_Component -SUAVE.Components.Physical_Component.Physical_Component -SUAVE.Components.Component.Component - -
- - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def voltage (self)
 
def logic (self, conditions, numerics)
 
- Public Member Functions inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
- - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

MPPT_efficiency
 
system_voltage
 
- Public Attributes inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
inputs
 
outputs
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
-

Detailed Description

-
The distributor is a component unique to a solar aircraft. This controls the flow of energy in to and from the battery.
-    This includes the basic logic of the maximum power point tracker that modifies the voltage of the panels to
-    extract maximum power.
-
-    Assumptions:
-    None
-    
-    Source:
-    None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Components.Energy.Distributors.Solar_Logic.Solar_Logic.__defaults__ ( self)
-
-
This sets the default values.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
- -

◆ logic()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Components.Energy.Distributors.Solar_Logic.Solar_Logic.logic ( self,
 conditions,
 numerics 
)
-
-
The power being sent to the battery
-
-    Assumptions:
-the system voltage is constant
-the maximum power point is at a constant voltage
-
-    Source:
-    N/A
-    
-    Inputs:
-self.inputs:
-    powerin
-    pavionics
-    ppayload
-    volts_motor
-    currentesc
-numerics.time.integrate
-
-    Outputs:
-self.outputs:
-    current
-    power_in
-    energy_transfer
-    
-    Properties Used:
-self.MPPT_efficiency
-
-
- -

◆ voltage()

- -
-
- - - - - - - - -
def SUAVE.Components.Energy.Distributors.Solar_Logic.Solar_Logic.voltage ( self)
-
-
The system voltage
-
-    Assumptions:
-this function practically does nothing
-    
-    Source:
-    N/A
-    
-    Inputs:
-self.system_voltage         [volts]
-       
-    Outputs:
-self.outputs.system_voltage [volts]
-
-    Properties Used:
-    None               
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Energy/Distributors/Solar_Logic.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Solar__Logic_1_1Solar__Logic.js b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Solar__Logic_1_1Solar__Logic.js deleted file mode 100644 index 3bbd2f5a..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Solar__Logic_1_1Solar__Logic.js +++ /dev/null @@ -1,8 +0,0 @@ -var classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Solar__Logic_1_1Solar__Logic = -[ - [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Solar__Logic_1_1Solar__Logic.html#ad90736f1fa00d5a922b73a84529d4606", null ], - [ "logic", "classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Solar__Logic_1_1Solar__Logic.html#a82fe732f5efcb0427a6ac822b676aecb", null ], - [ "voltage", "classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Solar__Logic_1_1Solar__Logic.html#ab9170ae4fd2da9b58a8dabbffd81044a", null ], - [ "MPPT_efficiency", "classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Solar__Logic_1_1Solar__Logic.html#add5f689ed37fa7df476dfc95e9a24b05", null ], - [ "system_voltage", "classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Solar__Logic_1_1Solar__Logic.html#a3fdffe4991de8f9335f9af4672553fd2", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Solar__Logic_1_1Solar__Logic.png b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Solar__Logic_1_1Solar__Logic.png deleted file mode 100644 index 79f2dd80..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Solar__Logic_1_1Solar__Logic.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Energy_1_1Component-members.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Energy_1_1Component-members.html deleted file mode 100644 index 2c208792..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Energy_1_1Component-members.html +++ /dev/null @@ -1,118 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
-
- - - -
-
- -
-
-
- - - - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Energy_1_1Component.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Energy_1_1Component.html deleted file mode 100644 index 4d820561..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Energy_1_1Component.html +++ /dev/null @@ -1,243 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Components.Energy.Energy.Component Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
-
- - - -
-
- -
-
-
- -
- -
-
- - -
- -
- -
- -
-
SUAVE.Components.Energy.Energy.Component Class Reference
-
-
-
-Inheritance diagram for SUAVE.Components.Energy.Energy.Component:
-
-
- - -SUAVE.Components.Physical_Component.Physical_Component -SUAVE.Components.Component.Component - -
- - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def provide_power ()
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
- - - - - - - - - - - - - - - - - -

-Public Attributes

tag
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
-

Detailed Description

-
A class representing an generic energy component.
-
-Assumptions:
-None
-
-Source:
-N/A
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Components.Energy.Energy.Component.__defaults__ ( self)
-
-
This sets the default tag for a component.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
-
- -

◆ provide_power()

- -
-
- - - - - - - -
def SUAVE.Components.Energy.Energy.Component.provide_power ()
-
-
A stub for providing power.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Energy/Energy.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Energy_1_1Component.js b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Energy_1_1Component.js deleted file mode 100644 index 007f652b..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Energy_1_1Component.js +++ /dev/null @@ -1,6 +0,0 @@ -var classSUAVE_1_1Components_1_1Energy_1_1Energy_1_1Component = -[ - [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Energy_1_1Component.html#a5c071d20776a4a810ff0c1d93f77aacf", null ], - [ "provide_power", "classSUAVE_1_1Components_1_1Energy_1_1Energy_1_1Component.html#a05eb658c37fc02dc277b7c2e92a07477", null ], - [ "tag", "classSUAVE_1_1Components_1_1Energy_1_1Energy_1_1Component.html#ac2570133e1c3a8c729ff21866f88ebcb", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Energy_1_1Component.png b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Energy_1_1Component.png deleted file mode 100644 index 869dc4a5..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Energy_1_1Component.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Energy_1_1ComponentContainer-members.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Energy_1_1ComponentContainer-members.html deleted file mode 100644 index 56d7871f..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Energy_1_1ComponentContainer-members.html +++ /dev/null @@ -1,115 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
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- - - -
-
- -
-
-
- -
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- -
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SUAVE.Components.Energy.Energy.ComponentContainer Member List
-
- -
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Energy_1_1ComponentContainer.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Energy_1_1ComponentContainer.html deleted file mode 100644 index fca1d014..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Energy_1_1ComponentContainer.html +++ /dev/null @@ -1,154 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Components.Energy.Energy.ComponentContainer Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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- - -
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- -
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SUAVE.Components.Energy.Energy.ComponentContainer Class Reference
-
-
-
-Inheritance diagram for SUAVE.Components.Energy.Energy.ComponentContainer:
-
-
- - -SUAVE.Components.Physical_Component.Container -SUAVE.Components.Component.Container - -
- - - - - - - - - -

-Static Public Attributes

Component
 
Container
 
- Static Public Attributes inherited from SUAVE.Components.Component.Container
Container
 
- - - - -

-Additional Inherited Members

- Public Member Functions inherited from SUAVE.Components.Physical_Component.Container
def sum_mass (self)
 
-

Detailed Description

-
A container for an energy component.
-
-Assumptions:
-None
-
-Source:
-N/A
-

The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Energy/Energy.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Energy_1_1ComponentContainer.png b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Energy_1_1ComponentContainer.png deleted file mode 100644 index 5872f8ac..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Energy_1_1ComponentContainer.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Energy_1_1Energy-members.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Energy_1_1Energy-members.html deleted file mode 100644 index e0829d41..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Energy_1_1Energy-members.html +++ /dev/null @@ -1,117 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
-
- - - -
-
- -
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- - - - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Energy_1_1Energy.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Energy_1_1Energy.html deleted file mode 100644 index cfdc36b3..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Energy_1_1Energy.html +++ /dev/null @@ -1,204 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Components.Energy.Energy.Energy Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
-
- - - -
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- -
-
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- -
- -
-
- - -
- -
- -
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-
SUAVE.Components.Energy.Energy.Energy Class Reference
-
-
-
-Inheritance diagram for SUAVE.Components.Energy.Energy.Energy:
-
-
- - -SUAVE.Components.Physical_Component.Physical_Component -SUAVE.Components.Component.Component - -
- - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
- - - - - - - - - - - - - - - -

-Additional Inherited Members

- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
-

Detailed Description

-
A class representing an energy component.
-
-Assumptions:
-None
-
-Source:
-N/A
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Components.Energy.Energy.Energy.__defaults__ ( self)
-
-
This sets the defaults. (Currently empty)
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Energy/Energy.py
  • -
-
-
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Energy.Energy_Component.Energy_Component Class Reference
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-Inheritance diagram for SUAVE.Components.Energy.Energy_Component.Energy_Component:
-
-
- - -SUAVE.Components.Physical_Component.Physical_Component -SUAVE.Components.Component.Component -SUAVE.Components.Energy.Converters.Combustor.Combustor -SUAVE.Components.Energy.Converters.Compression_Nozzle.Compression_Nozzle -SUAVE.Components.Energy.Converters.Compressor.Compressor -SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle -SUAVE.Components.Energy.Converters.Fan.Fan -SUAVE.Components.Energy.Converters.Fuel_Cell.Fuel_Cell -SUAVE.Components.Energy.Converters.Gearbox.Gearbox -SUAVE.Components.Energy.Converters.Motor.Motor -SUAVE.Components.Energy.Converters.Motor_Lo_Fid.Motor_Lo_Fid -SUAVE.Components.Energy.Converters.Propeller.Propeller -SUAVE.Components.Energy.Converters.Propeller_Lo_Fid.Propeller_Lo_Fid -SUAVE.Components.Energy.Converters.Ram.Ram -SUAVE.Components.Energy.Converters.Shaft_Power_Off_Take.Shaft_Power_Off_Take -SUAVE.Components.Energy.Converters.Solar_Panel.Solar_Panel -SUAVE.Components.Energy.Converters.Supersonic_Nozzle.Supersonic_Nozzle -SUAVE.Components.Energy.Converters.Turbine.Turbine -SUAVE.Components.Energy.Distributors.Electronic_Speed_Controller.Electronic_Speed_Controller -SUAVE.Components.Energy.Distributors.Solar_Logic.Solar_Logic -SUAVE.Components.Energy.Peripherals.Avionics.Avionics -SUAVE.Components.Energy.Peripherals.Payload.Payload -SUAVE.Components.Energy.Processes.Solar_Radiation.Solar_Radiation -SUAVE.Components.Energy.Processes.Thrust.Thrust -SUAVE.Components.Energy.Storages.Batteries.Battery.Battery - -
- - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
- - - - - - - - - - - - - - - - - - - -

-Public Attributes

inputs
 
outputs
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
-

Detailed Description

-
A class representing an energy component.
-
-Assumptions:
-None
-
-Source:
-N/A
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Components.Energy.Energy_Component.Energy_Component.__defaults__ ( self)
-
-
This sets the default inputs and outputs data structure.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Energy/Energy_Component.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Energy__Component_1_1Energy__Component.js b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Energy__Component_1_1Energy__Component.js deleted file mode 100644 index 38c886af..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Energy__Component_1_1Energy__Component.js +++ /dev/null @@ -1,6 +0,0 @@ -var classSUAVE_1_1Components_1_1Energy_1_1Energy__Component_1_1Energy__Component = -[ - [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Energy__Component_1_1Energy__Component.html#aa84b64cd5f7e49a35c3b64474559b1cc", null ], - [ "inputs", "classSUAVE_1_1Components_1_1Energy_1_1Energy__Component_1_1Energy__Component.html#acfd2e28f6bda810670943a55b453aa25", null ], - [ "outputs", "classSUAVE_1_1Components_1_1Energy_1_1Energy__Component_1_1Energy__Component.html#a1e67e94f3a6bd97b6dc7bd79ede0f54d", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Energy__Component_1_1Energy__Component.png b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Energy__Component_1_1Energy__Component.png deleted file mode 100644 index 28b35d32..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Energy__Component_1_1Energy__Component.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Ducted__Fan_1_1Battery__Ducted__Fan-members.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Ducted__Fan_1_1Battery__Ducted__Fan-members.html deleted file mode 100644 index 1dd9086c..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Ducted__Fan_1_1Battery__Ducted__Fan-members.html +++ /dev/null @@ -1,121 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Energy.Networks.Battery_Ducted_Fan.Battery_Ducted_Fan Member List
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Ducted__Fan_1_1Battery__Ducted__Fan.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Ducted__Fan_1_1Battery__Ducted__Fan.html deleted file mode 100644 index 3d148c4c..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Ducted__Fan_1_1Battery__Ducted__Fan.html +++ /dev/null @@ -1,273 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Components.Energy.Networks.Battery_Ducted_Fan.Battery_Ducted_Fan Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
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SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Energy.Networks.Battery_Ducted_Fan.Battery_Ducted_Fan Class Reference
-
-
-
-Inheritance diagram for SUAVE.Components.Energy.Networks.Battery_Ducted_Fan.Battery_Ducted_Fan:
-
-
- - -SUAVE.Components.Propulsors.Propulsor.Propulsor -SUAVE.Components.Physical_Component.Physical_Component -SUAVE.Components.Component.Component - -
- - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def evaluate_thrust (self, state)
 
- Public Member Functions inherited from SUAVE.Components.Propulsors.Propulsor.Propulsor
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

propulsor
 
battery
 
motor_efficiency
 
tag
 
- Public Attributes inherited from SUAVE.Components.Propulsors.Propulsor.Propulsor
tag
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
-

Detailed Description

-
Simply connects a battery to a ducted fan, with an assumed motor efficiency
-
-    Assumptions:
-    None
-    
-    Source:
-    None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Components.Energy.Networks.Battery_Ducted_Fan.Battery_Ducted_Fan.__defaults__ ( self)
-
-
This sets the default values for the network to function.
-    This network operates slightly different than most as it attaches a propulsor to the net.
-    
-    Assumptions:
-    Your system always uses 90 amps...?
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    N/A
-
-
-
- -

◆ evaluate_thrust()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Components.Energy.Networks.Battery_Ducted_Fan.Battery_Ducted_Fan.evaluate_thrust ( self,
 state 
)
-
-
Calculate thrust given the current state of the vehicle
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    state [state()]
-    
-    Outputs:
-    results.thrust_force_vector [newtons]
-    results.vehicle_mass_rate   [kg/s]
-    
-    Properties Used:
-    Defaulted values
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Energy/Networks/Battery_Ducted_Fan.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Ducted__Fan_1_1Battery__Ducted__Fan.js b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Ducted__Fan_1_1Battery__Ducted__Fan.js deleted file mode 100644 index bdd45ca3..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Ducted__Fan_1_1Battery__Ducted__Fan.js +++ /dev/null @@ -1,9 +0,0 @@ -var classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Ducted__Fan_1_1Battery__Ducted__Fan = -[ - [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Ducted__Fan_1_1Battery__Ducted__Fan.html#a25ca87a711e6e06670a7d5c5a24aefd3", null ], - [ "evaluate_thrust", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Ducted__Fan_1_1Battery__Ducted__Fan.html#a3c59ba5cb308705cc000fd5e28f60037", null ], - [ "battery", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Ducted__Fan_1_1Battery__Ducted__Fan.html#aa221541e0cf9cdeb125438cb052a0814", null ], - [ "motor_efficiency", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Ducted__Fan_1_1Battery__Ducted__Fan.html#a66b405209d8c43afa01255f145b427df", null ], - [ "propulsor", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Ducted__Fan_1_1Battery__Ducted__Fan.html#a122cf7faaa300ac90724b4bad1be7c98", null ], - [ "tag", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Ducted__Fan_1_1Battery__Ducted__Fan.html#ac60dafe42beba94bd1f313c2a329ad3d", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Ducted__Fan_1_1Battery__Ducted__Fan.png b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Ducted__Fan_1_1Battery__Ducted__Fan.png deleted file mode 100644 index b5ad1180..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Ducted__Fan_1_1Battery__Ducted__Fan.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Ducted__Fan__Parallel__Hybrid_1_1Batt8b72d6d15ac8ee5e3d4b10da1f3a8c15.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Ducted__Fan__Parallel__Hybrid_1_1Batt8b72d6d15ac8ee5e3d4b10da1f3a8c15.html deleted file mode 100644 index 5ec5c205..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Ducted__Fan__Parallel__Hybrid_1_1Batt8b72d6d15ac8ee5e3d4b10da1f3a8c15.html +++ /dev/null @@ -1,122 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Energy.Networks.Battery_Ducted_Fan_Parallel_Hybrid.Battery_Ducted_Fan_Parallel_Hybrid Member List
-
-
- -

This is the complete list of members for SUAVE.Components.Energy.Networks.Battery_Ducted_Fan_Parallel_Hybrid.Battery_Ducted_Fan_Parallel_Hybrid, including all inherited members.

- - - - - - - - - - - -
__defaults__(self)SUAVE.Components.Energy.Networks.Battery_Ducted_Fan_Parallel_Hybrid.Battery_Ducted_Fan_Parallel_Hybrid
auxiliary_battery (defined in SUAVE.Components.Energy.Networks.Battery_Ducted_Fan_Parallel_Hybrid.Battery_Ducted_Fan_Parallel_Hybrid)SUAVE.Components.Energy.Networks.Battery_Ducted_Fan_Parallel_Hybrid.Battery_Ducted_Fan_Parallel_Hybrid
evaluate_thrust(self, state)SUAVE.Components.Energy.Networks.Battery_Ducted_Fan_Parallel_Hybrid.Battery_Ducted_Fan_Parallel_Hybrid
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
motor_efficiency (defined in SUAVE.Components.Energy.Networks.Battery_Ducted_Fan_Parallel_Hybrid.Battery_Ducted_Fan_Parallel_Hybrid)SUAVE.Components.Energy.Networks.Battery_Ducted_Fan_Parallel_Hybrid.Battery_Ducted_Fan_Parallel_Hybrid
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
primary_battery (defined in SUAVE.Components.Energy.Networks.Battery_Ducted_Fan_Parallel_Hybrid.Battery_Ducted_Fan_Parallel_Hybrid)SUAVE.Components.Energy.Networks.Battery_Ducted_Fan_Parallel_Hybrid.Battery_Ducted_Fan_Parallel_Hybrid
propulsor (defined in SUAVE.Components.Energy.Networks.Battery_Ducted_Fan_Parallel_Hybrid.Battery_Ducted_Fan_Parallel_Hybrid)SUAVE.Components.Energy.Networks.Battery_Ducted_Fan_Parallel_Hybrid.Battery_Ducted_Fan_Parallel_Hybrid
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Energy.Networks.Battery_Ducted_Fan_Parallel_Hybrid.Battery_Ducted_Fan_Parallel_Hybrid)SUAVE.Components.Energy.Networks.Battery_Ducted_Fan_Parallel_Hybrid.Battery_Ducted_Fan_Parallel_Hybrid
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Ducted__Fan__Parallel__Hybrid_1_1Battc2b0401828a0427c88400fbb1bcfcf1d.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Ducted__Fan__Parallel__Hybrid_1_1Battc2b0401828a0427c88400fbb1bcfcf1d.html deleted file mode 100644 index 75ddfa7c..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Ducted__Fan__Parallel__Hybrid_1_1Battc2b0401828a0427c88400fbb1bcfcf1d.html +++ /dev/null @@ -1,279 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Components.Energy.Networks.Battery_Ducted_Fan_Parallel_Hybrid.Battery_Ducted_Fan_Parallel_Hybrid Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
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SUAVE.Components.Energy.Networks.Battery_Ducted_Fan_Parallel_Hybrid.Battery_Ducted_Fan_Parallel_Hybrid Class Reference
-
-
-
-Inheritance diagram for SUAVE.Components.Energy.Networks.Battery_Ducted_Fan_Parallel_Hybrid.Battery_Ducted_Fan_Parallel_Hybrid:
-
-
- - -SUAVE.Components.Propulsors.Propulsor.Propulsor -SUAVE.Components.Physical_Component.Physical_Component -SUAVE.Components.Component.Component - -
- - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def evaluate_thrust (self, state)
 
- Public Member Functions inherited from SUAVE.Components.Propulsors.Propulsor.Propulsor
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

propulsor
 
primary_battery
 
auxiliary_battery
 
motor_efficiency
 
tag
 
- Public Attributes inherited from SUAVE.Components.Propulsors.Propulsor.Propulsor
tag
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
-

Detailed Description

-
Uses two batteries to run a motor connected to a ducted fan; 
-    
-    Assumptions:
-    The primary_battery always runs, while the auxiliary_battery meets additional power needs
-    
-    Source:
-    None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Components.Energy.Networks.Battery_Ducted_Fan_Parallel_Hybrid.Battery_Ducted_Fan_Parallel_Hybrid.__defaults__ ( self)
-
-
This sets the default values for the network to function.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    N/A
-
-
-
- -

◆ evaluate_thrust()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Components.Energy.Networks.Battery_Ducted_Fan_Parallel_Hybrid.Battery_Ducted_Fan_Parallel_Hybrid.evaluate_thrust ( self,
 state 
)
-
-
Calculate thrust given the current state of the vehicle
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    state [state()]
-    
-    Outputs:
-    results.thrust_force_vector [newtons]
-    results.vehicle_mass_rate   [kg/s]
-    conditions.propulsion.primary_battery_draw     [watts]
-    conditions.propulsion.primary_battery_energy   [joules]
-    conditions.propulsion.auxiliary_battery_draw   [watts]
-    conditions.propulsion.auxiliary_battery_energy [joules]
-    
-    Properties Used:
-    Defaulted values
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Energy/Networks/Battery_Ducted_Fan_Parallel_Hybrid.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Ducted__Fan__Parallel__Hybrid_1_1Battc2b0401828a0427c88400fbb1bcfcf1d.js b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Ducted__Fan__Parallel__Hybrid_1_1Battc2b0401828a0427c88400fbb1bcfcf1d.js deleted file mode 100644 index 67aa7026..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Ducted__Fan__Parallel__Hybrid_1_1Battc2b0401828a0427c88400fbb1bcfcf1d.js +++ /dev/null @@ -1,10 +0,0 @@ -var classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Ducted__Fan__Parallel__Hybrid_1_1Battc2b0401828a0427c88400fbb1bcfcf1d = -[ - [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Ducted__Fan__Parallel__Hybrid_1_1Battc2b0401828a0427c88400fbb1bcfcf1d.html#a687290d12bc2f749359f4a1cce1fb1b2", null ], - [ "evaluate_thrust", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Ducted__Fan__Parallel__Hybrid_1_1Battc2b0401828a0427c88400fbb1bcfcf1d.html#a6d5b90c476592a501e96410fed1a77d8", null ], - [ "auxiliary_battery", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Ducted__Fan__Parallel__Hybrid_1_1Battc2b0401828a0427c88400fbb1bcfcf1d.html#a97968b4bfe2d75ab6d5b7a90fa4bb77c", null ], - [ "motor_efficiency", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Ducted__Fan__Parallel__Hybrid_1_1Battc2b0401828a0427c88400fbb1bcfcf1d.html#ac2a253f9d6159394e51b62e508b12138", null ], - [ "primary_battery", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Ducted__Fan__Parallel__Hybrid_1_1Battc2b0401828a0427c88400fbb1bcfcf1d.html#afa0fa5859a60c2d241d67456a23f4530", null ], - [ "propulsor", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Ducted__Fan__Parallel__Hybrid_1_1Battc2b0401828a0427c88400fbb1bcfcf1d.html#aae3f5349d0f99351fb89f167dbfffe49", null ], - [ "tag", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Ducted__Fan__Parallel__Hybrid_1_1Battc2b0401828a0427c88400fbb1bcfcf1d.html#a9da26c5f784beb335652fbe2a8519ec2", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Ducted__Fan__Parallel__Hybrid_1_1Battc2b0401828a0427c88400fbb1bcfcf1d.png b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Ducted__Fan__Parallel__Hybrid_1_1Battc2b0401828a0427c88400fbb1bcfcf1d.png deleted file mode 100644 index 567ce3b2..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Ducted__Fan__Parallel__Hybrid_1_1Battc2b0401828a0427c88400fbb1bcfcf1d.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Propeller_1_1Battery__Propeller-members.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Propeller_1_1Battery__Propeller-members.html deleted file mode 100644 index 20164f32..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Propeller_1_1Battery__Propeller-members.html +++ /dev/null @@ -1,131 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller Member List
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This is the complete list of members for SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller, including all inherited members.

- - - - - - - - - - - - - - - - - - - - -
__defaults__(self)SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller
avionics (defined in SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller)SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller
battery (defined in SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller)SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller
engine_length (defined in SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller)SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller
esc (defined in SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller)SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller
evaluate_thrust(self, state)SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
motor (defined in SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller)SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller
nacelle_diameter (defined in SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller)SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller
number_of_engines (defined in SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller)SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
payload (defined in SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller)SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller
propeller (defined in SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller)SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller
residuals(self, segment, state)SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller)SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller
thrust_angle (defined in SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller)SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller
unpack_unknowns(self, segment, state)SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller
voltage (defined in SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller)SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Propeller_1_1Battery__Propeller.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Propeller_1_1Battery__Propeller.html deleted file mode 100644 index 27b6be45..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Propeller_1_1Battery__Propeller.html +++ /dev/null @@ -1,420 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller Class Reference
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-Inheritance diagram for SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller:
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- - -SUAVE.Components.Propulsors.Propulsor.Propulsor -SUAVE.Components.Physical_Component.Physical_Component -SUAVE.Components.Component.Component - -
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-Public Member Functions

def __defaults__ (self)
 
def evaluate_thrust (self, state)
 
def unpack_unknowns (self, segment, state)
 
def residuals (self, segment, state)
 
- Public Member Functions inherited from SUAVE.Components.Propulsors.Propulsor.Propulsor
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

motor
 
propeller
 
esc
 
avionics
 
payload
 
battery
 
nacelle_diameter
 
engine_length
 
number_of_engines
 
voltage
 
thrust_angle
 
tag
 
- Public Attributes inherited from SUAVE.Components.Propulsors.Propulsor.Propulsor
tag
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
-

Detailed Description

-
This is a simple network with a battery powering a propeller through
-    an electric motor
-    
-    This network adds 2 extra unknowns to the mission. The first is
-    a voltage, to calculate the thevenin voltage drop in the pack.
-    The second is torque matching between motor and propeller.
-
-    Assumptions:
-    None
-    
-    Source:
-    None
-

Member Function Documentation

- -

◆ __defaults__()

- -
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def SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller.__defaults__ ( self)
-
-
This sets the default values for the network to function.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    N/A
-
-
-
- -

◆ evaluate_thrust()

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def SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller.evaluate_thrust ( self,
 state 
)
-
-
Calculate thrust given the current state of the vehicle
-    
-    Assumptions:
-    Caps the throttle at 110% and linearly interpolates thrust off that
-    
-    Source:
-    N/A
-    
-    Inputs:
-    state [state()]
-    
-    Outputs:
-    results.thrust_force_vector [newtons]
-    results.vehicle_mass_rate   [kg/s]
-    conditions.propulsion:
-rpm                  [radians/sec]
-current              [amps]
-battery_draw         [watts]
-battery_energy       [joules]
-voltage_open_circuit [volts]
-voltage_under_load   [volts]
-motor_torque         [N-M]
-propeller_torque     [N-M]
-    
-    Properties Used:
-    Defaulted values
-
-
-
- -

◆ residuals()

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def SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller.residuals ( self,
 segment,
 state 
)
-
-
This packs the residuals to be send to the mission solver.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    state.conditions.propulsion:
-motor_torque                          [N-m]
-propeller_torque                      [N-m]
-voltage_under_load                    [volts]
-    state.unknowns.battery_voltage_under_load [volts]
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    self.voltage                              [volts]
-
-
-
- -

◆ unpack_unknowns()

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def SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller.unpack_unknowns ( self,
 segment,
 state 
)
-
-
This is an extra set of unknowns which are unpacked from the mission solver and send to the network.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    state.unknowns.propeller_power_coefficient [None]
-    state.unknowns.battery_voltage_under_load  [volts]
-    
-    Outputs:
-    state.conditions.propulsion.propeller_power_coefficient [None]
-    state.conditions.propulsion.battery_voltage_under_load  [volts]
-    
-    Properties Used:
-    N/A
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Energy/Networks/Battery_Propeller.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Propeller_1_1Battery__Propeller.js b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Propeller_1_1Battery__Propeller.js deleted file mode 100644 index dfaa361d..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Propeller_1_1Battery__Propeller.js +++ /dev/null @@ -1,19 +0,0 @@ -var classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Propeller_1_1Battery__Propeller = -[ - [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Propeller_1_1Battery__Propeller.html#a5139599762ddccd4077654b2797e0957", null ], - [ "evaluate_thrust", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Propeller_1_1Battery__Propeller.html#ac90f964684965af5c1d2d6b936ff769c", null ], - [ "residuals", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Propeller_1_1Battery__Propeller.html#af75bca55504a4c158b844178cc3560d6", null ], - [ "unpack_unknowns", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Propeller_1_1Battery__Propeller.html#abdfc2d6560f02a7b2cf8bfb5291a321d", null ], - [ "avionics", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Propeller_1_1Battery__Propeller.html#af76a5d8fc73c74267da6634b39c667b4", null ], - [ "battery", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Propeller_1_1Battery__Propeller.html#a9aa5e4c3240b6f6ee44b77d56486639e", null ], - [ "engine_length", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Propeller_1_1Battery__Propeller.html#a683e8ecb8cd5f57e0d73f9faaabdb458", null ], - [ "esc", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Propeller_1_1Battery__Propeller.html#a69571f6df7077a072a74fac289b37b94", null ], - [ "motor", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Propeller_1_1Battery__Propeller.html#aba73ecabb3d7776324bf9a2a5f61b3f1", null ], - [ "nacelle_diameter", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Propeller_1_1Battery__Propeller.html#a3abf88a71b11fcd466d8a8dc8ad690b1", null ], - [ "number_of_engines", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Propeller_1_1Battery__Propeller.html#a7c1f68607a9955130e4f8e42cf2e25f0", null ], - [ "payload", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Propeller_1_1Battery__Propeller.html#ac733d4d41de9f7c20bf5153d3b7a5bfd", null ], - [ "propeller", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Propeller_1_1Battery__Propeller.html#a5824fa11492359db3f481fc18effc0ee", null ], - [ "tag", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Propeller_1_1Battery__Propeller.html#ac13048ae157a044a18338d455ab86c86", null ], - [ "thrust_angle", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Propeller_1_1Battery__Propeller.html#a57899f04a912f824be02d29fdc6ec5f4", null ], - [ "voltage", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Propeller_1_1Battery__Propeller.html#a6d1abaa63d86e61e8a603c175e3de56f", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Propeller_1_1Battery__Propeller.png b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Propeller_1_1Battery__Propeller.png deleted file mode 100644 index aec8eace..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Propeller_1_1Battery__Propeller.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Dual__Battery__Ducted__Fan_1_1Dual__Battery__Ducted__Fan-members.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Dual__Battery__Ducted__Fan_1_1Dual__Battery__Ducted__Fan-members.html deleted file mode 100644 index cccdf80b..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Dual__Battery__Ducted__Fan_1_1Dual__Battery__Ducted__Fan-members.html +++ /dev/null @@ -1,122 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Energy.Networks.Dual_Battery_Ducted_Fan.Dual_Battery_Ducted_Fan Member List
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- -

This is the complete list of members for SUAVE.Components.Energy.Networks.Dual_Battery_Ducted_Fan.Dual_Battery_Ducted_Fan, including all inherited members.

- - - - - - - - - - - -
__defaults__(self)SUAVE.Components.Energy.Networks.Dual_Battery_Ducted_Fan.Dual_Battery_Ducted_Fan
auxiliary_battery (defined in SUAVE.Components.Energy.Networks.Dual_Battery_Ducted_Fan.Dual_Battery_Ducted_Fan)SUAVE.Components.Energy.Networks.Dual_Battery_Ducted_Fan.Dual_Battery_Ducted_Fan
evaluate_thrust(self, state)SUAVE.Components.Energy.Networks.Dual_Battery_Ducted_Fan.Dual_Battery_Ducted_Fan
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
motor_efficiency (defined in SUAVE.Components.Energy.Networks.Dual_Battery_Ducted_Fan.Dual_Battery_Ducted_Fan)SUAVE.Components.Energy.Networks.Dual_Battery_Ducted_Fan.Dual_Battery_Ducted_Fan
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
primary_battery (defined in SUAVE.Components.Energy.Networks.Dual_Battery_Ducted_Fan.Dual_Battery_Ducted_Fan)SUAVE.Components.Energy.Networks.Dual_Battery_Ducted_Fan.Dual_Battery_Ducted_Fan
propulsor (defined in SUAVE.Components.Energy.Networks.Dual_Battery_Ducted_Fan.Dual_Battery_Ducted_Fan)SUAVE.Components.Energy.Networks.Dual_Battery_Ducted_Fan.Dual_Battery_Ducted_Fan
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Energy.Networks.Dual_Battery_Ducted_Fan.Dual_Battery_Ducted_Fan)SUAVE.Components.Energy.Networks.Dual_Battery_Ducted_Fan.Dual_Battery_Ducted_Fan
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Dual__Battery__Ducted__Fan_1_1Dual__Battery__Ducted__Fan.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Dual__Battery__Ducted__Fan_1_1Dual__Battery__Ducted__Fan.html deleted file mode 100644 index 2a74c3d4..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Dual__Battery__Ducted__Fan_1_1Dual__Battery__Ducted__Fan.html +++ /dev/null @@ -1,279 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Components.Energy.Networks.Dual_Battery_Ducted_Fan.Dual_Battery_Ducted_Fan Class Reference - - - - - - - - - - - - - - - -
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- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Energy.Networks.Dual_Battery_Ducted_Fan.Dual_Battery_Ducted_Fan Class Reference
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-
-
-Inheritance diagram for SUAVE.Components.Energy.Networks.Dual_Battery_Ducted_Fan.Dual_Battery_Ducted_Fan:
-
-
- - -SUAVE.Components.Propulsors.Propulsor.Propulsor -SUAVE.Components.Physical_Component.Physical_Component -SUAVE.Components.Component.Component - -
- - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def evaluate_thrust (self, state)
 
- Public Member Functions inherited from SUAVE.Components.Propulsors.Propulsor.Propulsor
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

propulsor
 
primary_battery
 
auxiliary_battery
 
motor_efficiency
 
tag
 
- Public Attributes inherited from SUAVE.Components.Propulsors.Propulsor.Propulsor
tag
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
-

Detailed Description

-
Uses two batteries to run a motor connected to a ducted fan; 
-    
-    Assumptions:
-    The primary_battery always runs, while the auxiliary_battery meets additional power needs
-    
-    Source:
-    None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Components.Energy.Networks.Dual_Battery_Ducted_Fan.Dual_Battery_Ducted_Fan.__defaults__ ( self)
-
-
This sets the default values for the network to function.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    N/A
-
-
-
- -

◆ evaluate_thrust()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Components.Energy.Networks.Dual_Battery_Ducted_Fan.Dual_Battery_Ducted_Fan.evaluate_thrust ( self,
 state 
)
-
-
Calculate thrust given the current state of the vehicle
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    state [state()]
-    
-    Outputs:
-    results.thrust_force_vector [newtons]
-    results.vehicle_mass_rate   [kg/s]
-    conditions.propulsion.primary_battery_draw     [watts]
-    conditions.propulsion.primary_battery_energy   [joules]
-    conditions.propulsion.auxiliary_battery_draw   [watts]
-    conditions.propulsion.auxiliary_battery_energy [joules]
-    
-    Properties Used:
-    Defaulted values
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Energy/Networks/Dual_Battery_Ducted_Fan.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Dual__Battery__Ducted__Fan_1_1Dual__Battery__Ducted__Fan.js b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Dual__Battery__Ducted__Fan_1_1Dual__Battery__Ducted__Fan.js deleted file mode 100644 index ef19e9f3..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Dual__Battery__Ducted__Fan_1_1Dual__Battery__Ducted__Fan.js +++ /dev/null @@ -1,10 +0,0 @@ -var classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Dual__Battery__Ducted__Fan_1_1Dual__Battery__Ducted__Fan = -[ - [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Dual__Battery__Ducted__Fan_1_1Dual__Battery__Ducted__Fan.html#a5dc648add76242495190b22734c71bf3", null ], - [ "evaluate_thrust", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Dual__Battery__Ducted__Fan_1_1Dual__Battery__Ducted__Fan.html#a59f813bcd082fc977fb78b763900d879", null ], - [ "auxiliary_battery", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Dual__Battery__Ducted__Fan_1_1Dual__Battery__Ducted__Fan.html#a56345ec136a6f3101e9db068808c4a9e", null ], - [ "motor_efficiency", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Dual__Battery__Ducted__Fan_1_1Dual__Battery__Ducted__Fan.html#a5a55a6d5baf29750c2895d02467c70bf", null ], - [ "primary_battery", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Dual__Battery__Ducted__Fan_1_1Dual__Battery__Ducted__Fan.html#ac6cd6c3aa3b891ada7427eb13651290c", null ], - [ "propulsor", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Dual__Battery__Ducted__Fan_1_1Dual__Battery__Ducted__Fan.html#ad93c950b7882159dc4b0222af2a74d9e", null ], - [ "tag", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Dual__Battery__Ducted__Fan_1_1Dual__Battery__Ducted__Fan.html#a8eed85d5755d8c8f16a8a13609bad30d", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Dual__Battery__Ducted__Fan_1_1Dual__Battery__Ducted__Fan.png b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Dual__Battery__Ducted__Fan_1_1Dual__Battery__Ducted__Fan.png deleted file mode 100644 index 0a1dd42b..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Dual__Battery__Ducted__Fan_1_1Dual__Battery__Ducted__Fan.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ducted__Fan_1_1Ducted__Fan-members.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ducted__Fan_1_1Ducted__Fan-members.html deleted file mode 100644 index ef7d1cf2..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ducted__Fan_1_1Ducted__Fan-members.html +++ /dev/null @@ -1,124 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Energy.Networks.Ducted_Fan.Ducted_Fan Member List
-
-
- -

This is the complete list of members for SUAVE.Components.Energy.Networks.Ducted_Fan.Ducted_Fan, including all inherited members.

- - - - - - - - - - - - - -
__defaults__(self)SUAVE.Components.Energy.Networks.Ducted_Fan.Ducted_Fan
areas (defined in SUAVE.Components.Energy.Networks.Ducted_Fan.Ducted_Fan)SUAVE.Components.Energy.Networks.Ducted_Fan.Ducted_Fan
bypass_ratio (defined in SUAVE.Components.Energy.Networks.Ducted_Fan.Ducted_Fan)SUAVE.Components.Energy.Networks.Ducted_Fan.Ducted_Fan
engine_length (defined in SUAVE.Components.Energy.Networks.Ducted_Fan.Ducted_Fan)SUAVE.Components.Energy.Networks.Ducted_Fan.Ducted_Fan
evaluate_thrust(self, state)SUAVE.Components.Energy.Networks.Ducted_Fan.Ducted_Fan
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
nacelle_diameter (defined in SUAVE.Components.Energy.Networks.Ducted_Fan.Ducted_Fan)SUAVE.Components.Energy.Networks.Ducted_Fan.Ducted_Fan
number_of_engines (defined in SUAVE.Components.Energy.Networks.Ducted_Fan.Ducted_Fan)SUAVE.Components.Energy.Networks.Ducted_Fan.Ducted_Fan
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
size(self, state)SUAVE.Components.Energy.Networks.Ducted_Fan.Ducted_Fan
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Energy.Networks.Ducted_Fan.Ducted_Fan)SUAVE.Components.Energy.Networks.Ducted_Fan.Ducted_Fan
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ducted__Fan_1_1Ducted__Fan.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ducted__Fan_1_1Ducted__Fan.html deleted file mode 100644 index a3d1bd24..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ducted__Fan_1_1Ducted__Fan.html +++ /dev/null @@ -1,333 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Components.Energy.Networks.Ducted_Fan.Ducted_Fan Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Energy.Networks.Ducted_Fan.Ducted_Fan Class Reference
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-Inheritance diagram for SUAVE.Components.Energy.Networks.Ducted_Fan.Ducted_Fan:
-
-
- - -SUAVE.Components.Propulsors.Propulsor.Propulsor -SUAVE.Components.Physical_Component.Physical_Component -SUAVE.Components.Component.Component - -
- - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def evaluate_thrust (self, state)
 
def size (self, state)
 
- Public Member Functions inherited from SUAVE.Components.Propulsors.Propulsor.Propulsor
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

tag
 
number_of_engines
 
nacelle_diameter
 
engine_length
 
bypass_ratio
 
areas
 
- Public Attributes inherited from SUAVE.Components.Propulsors.Propulsor.Propulsor
tag
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
-

Detailed Description

-
A ducted fan 
-
-    Assumptions:
-    None
-    
-    Source:
-    Most of the componentes come from this book:
-    https://web.stanford.edu/~cantwell/AA283_Course_Material/AA283_Course_Notes/
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Components.Energy.Networks.Ducted_Fan.Ducted_Fan.__defaults__ ( self)
-
-
This sets the default values for the network to function.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    N/A
-
-
-
- -

◆ evaluate_thrust()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Components.Energy.Networks.Ducted_Fan.Ducted_Fan.evaluate_thrust ( self,
 state 
)
-
-
Calculate thrust given the current state of the vehicle
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    state [state()]
-    
-    Outputs:
-    results.thrust_force_vector [newtons]
-    results.vehicle_mass_rate   [kg/s]
-    results.power               [Watts]
-    conditions.propulsion.acoustic_outputs:
-fan:
-    exit_static_temperature      
-    exit_static_pressure       
-    exit_stagnation_temperature 
-    exit_stagnation_pressure
-    exit_velocity 
-    
-    Properties Used:
-    Defaulted values
-
-
-
- -

◆ size()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Components.Energy.Networks.Ducted_Fan.Ducted_Fan.size ( self,
 state 
)
-
-
Size the turbofan
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    State [state()]
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    N/A
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Energy/Networks/Ducted_Fan.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ducted__Fan_1_1Ducted__Fan.js b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ducted__Fan_1_1Ducted__Fan.js deleted file mode 100644 index 149b89d5..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ducted__Fan_1_1Ducted__Fan.js +++ /dev/null @@ -1,12 +0,0 @@ -var classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ducted__Fan_1_1Ducted__Fan = -[ - [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ducted__Fan_1_1Ducted__Fan.html#a8d73a918891b363032abd9adbcc1c868", null ], - [ "evaluate_thrust", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ducted__Fan_1_1Ducted__Fan.html#a993ed0f38fc8b40340bf58b376461b6a", null ], - [ "size", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ducted__Fan_1_1Ducted__Fan.html#a9b5288b67f95185b4edaa1b813e4b601", null ], - [ "areas", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ducted__Fan_1_1Ducted__Fan.html#ae22f76d8cb6aeb04454643964a43aae6", null ], - [ "bypass_ratio", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ducted__Fan_1_1Ducted__Fan.html#aefa45fa7b6e4d57183e3b5788bf01d2f", null ], - [ "engine_length", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ducted__Fan_1_1Ducted__Fan.html#ae557071255a5f36a43e0db676e4f3ba2", null ], - [ "nacelle_diameter", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ducted__Fan_1_1Ducted__Fan.html#a6e44da438a79f93ae981a68895043e74", null ], - [ "number_of_engines", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ducted__Fan_1_1Ducted__Fan.html#ae845b8ec30319de8b8ced55dfa4694e8", null ], - [ "tag", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ducted__Fan_1_1Ducted__Fan.html#a8909a2f8395ae333ce6080a57c69d3d0", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ducted__Fan_1_1Ducted__Fan.png b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ducted__Fan_1_1Ducted__Fan.png deleted file mode 100644 index 87bc30c3..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ducted__Fan_1_1Ducted__Fan.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Lift__Forward__Propulsor_1_1Lift__Forward-members.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Lift__Forward__Propulsor_1_1Lift__Forward-members.html deleted file mode 100644 index 9867de85..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Lift__Forward__Propulsor_1_1Lift__Forward-members.html +++ /dev/null @@ -1,142 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward Member List
-
-
- -

This is the complete list of members for SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward, including all inherited members.

- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
__defaults__(self)SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward
avionics (defined in SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward)SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward
battery (defined in SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward)SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward
engine_length_forward (defined in SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward)SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward
engine_length_lift (defined in SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward)SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward
esc_forward (defined in SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward)SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward
esc_lift (defined in SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward)SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward
evaluate_thrust(self, state)SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
motor_forward (defined in SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward)SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward
motor_lift (defined in SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward)SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward
nacelle_diameter_forward (defined in SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward)SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward
nacelle_diameter_lift (defined in SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward)SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward
number_of_engines_forward (defined in SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward)SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward
number_of_engines_lift (defined in SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward)SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
payload (defined in SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward)SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward
propeller_forward (defined in SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward)SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward
propeller_lift (defined in SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward)SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward
residuals(self, segment, state)SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward
residuals_no_forward(self, segment, state)SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward
residuals_no_lift(self, segment, state)SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Propulsors.Propulsor.Propulsor)SUAVE.Components.Propulsors.Propulsor.Propulsor
thrust_angle_forward (defined in SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward)SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward
thrust_angle_lift (defined in SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward)SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward
unpack_unknowns(self, segment, state)SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward
unpack_unknowns_no_forward(self, segment, state)SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward
unpack_unknowns_no_lift(self, segment, state)SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward
voltage (defined in SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward)SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Lift__Forward__Propulsor_1_1Lift__Forward.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Lift__Forward__Propulsor_1_1Lift__Forward.html deleted file mode 100644 index cab106fd..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Lift__Forward__Propulsor_1_1Lift__Forward.html +++ /dev/null @@ -1,693 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward Class Reference
-
-
-
-Inheritance diagram for SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward:
-
-
- - -SUAVE.Components.Propulsors.Propulsor.Propulsor -SUAVE.Components.Physical_Component.Physical_Component -SUAVE.Components.Component.Component - -
- - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def evaluate_thrust (self, state)
 
def unpack_unknowns (self, segment, state)
 
def unpack_unknowns_no_lift (self, segment, state)
 
def unpack_unknowns_no_forward (self, segment, state)
 
def residuals (self, segment, state)
 
def residuals_no_lift (self, segment, state)
 
def residuals_no_forward (self, segment, state)
 
- Public Member Functions inherited from SUAVE.Components.Propulsors.Propulsor.Propulsor
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

motor_lift
 
motor_forward
 
propeller_lift
 
propeller_forward
 
esc_lift
 
esc_forward
 
avionics
 
payload
 
battery
 
nacelle_diameter_lift
 
nacelle_diameter_forward
 
engine_length_lift
 
engine_length_forward
 
number_of_engines_lift
 
number_of_engines_forward
 
voltage
 
thrust_angle_lift
 
thrust_angle_forward
 
- Public Attributes inherited from SUAVE.Components.Propulsors.Propulsor.Propulsor
tag
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
-

Detailed Description

-
This is a complex version of battery_propeller with a battery powering propellers through
-    electric motors. In this case we have 2 sets of motors at different motors that can be controlled seperately
-    
-    This network adds 2 extra unknowns to the mission. The first is
-    a voltage, to calculate the thevenin voltage drop in the pack.
-    The second is torque matching between motor and propeller.
-    
-    We have two inputs, the forward throttle and the lift throttle setting
-
-    Since this is an airplane first and foremost, the "throttle" will be for forward thrust
-    The new unknown will be for lift throttle, because of the assumption on throttle something needs to be done...
-
-    Want only 1 residual on voltage
-
-    Assumptions:
-    For any segment using this, body angle can't be an unknown.
-    
-    Source:
-    None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward.__defaults__ ( self)
-
-
This sets the default values for the network to function.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    N/A
-
-
-
- -

◆ evaluate_thrust()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward.evaluate_thrust ( self,
 state 
)
-
-
Calculate thrust given the current state of the vehicle
-    
-    Assumptions:
-    Caps the throttle at 110% and linearly interpolates thrust off that
-    
-    Source:
-    N/A
-    
-    Inputs:
-    state [state()]
-    
-    Outputs:
-    results.thrust_force_vector [Newtons]
-    results.vehicle_mass_rate   [kg/s]
-    conditions.propulsion:
-rpm_lift                 [radians/sec]
-rpm _forward             [radians/sec]
-current_lift             [amps]
-current_forward          [amps]
-battery_draw             [watts]
-battery_energy           [joules]
-voltage_open_circuit     [volts]
-voltage_under_load       [volts]
-motor_torque_lift        [N-M]
-motor_torque_forward     [N-M]
-propeller_torque_lift    [N-M]
-propeller_torque_forward [N-M]
-    
-    Properties Used:
-    Defaulted values
-
-
-
- -

◆ residuals()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward.residuals ( self,
 segment,
 state 
)
-
-
This packs the residuals to be send to the mission solver.
-    Use this if all motors are operational
-    
-    Assumptions:
-    All motors are operational
-    
-    Source:
-    N/A
-    
-    Inputs:
-    state.conditions.propulsion:
-motor_torque_forward                  [N-m]
-motor_torque_lift                     [N-m]
-propeller_torque_forward              [N-m]
-propeller_torque_lift                 [N-m]
-voltage_under_load                    [volts]
-    state.unknowns.battery_voltage_under_load [volts]
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    self.voltage                              [volts]
-
-
-
- -

◆ residuals_no_forward()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward.residuals_no_forward ( self,
 segment,
 state 
)
-
-
This packs the residuals to be send to the mission solver.
-    Only the lift motors are operational
-    
-    Assumptions:
-    The lift motors are operational
-    
-    Source:
-    N/A
-    
-    Inputs:
-    state.conditions.propulsion:
-motor_torque_forward                  [N-m]
-motor_torque_lift                     [N-m]
-propeller_torque_forward              [N-m]
-propeller_torque_lift                 [N-m]
-voltage_under_load                    [volts]
-    state.unknowns.battery_voltage_under_load [volts]
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    self.voltage                              [volts]
-
-
-
- -

◆ residuals_no_lift()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward.residuals_no_lift ( self,
 segment,
 state 
)
-
-
This packs the residuals to be send to the mission solver.
-    Use this if only the forward motors are operational
-    
-    Assumptions:
-    Only the forward motors are operational
-    
-    Source:
-    N/A
-    
-    Inputs:
-    state.conditions.propulsion:
-motor_torque_forward                  [N-m]
-motor_torque_lift                     [N-m]
-propeller_torque_forward              [N-m]
-propeller_torque_lift                 [N-m]
-voltage_under_load                    [volts]
-    state.unknowns.battery_voltage_under_load [volts]
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    self.voltage                              [volts]
-
-
-
- -

◆ unpack_unknowns()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward.unpack_unknowns ( self,
 segment,
 state 
)
-
-
This is an extra set of unknowns which are unpacked from the mission solver and send to the network.
-    This uses all the motors.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    state.unknowns.propeller_power_coefficient [None]
-    state.unknowns.battery_voltage_under_load  [volts]
-    state.unknowns.lift_throttle               [0-1]
-    state.unknowns.throttle                    [0-1]
-    
-    Outputs:
-    state.conditions.propulsion.propeller_power_coefficient [None]
-    state.conditions.propulsion.battery_voltage_under_load  [volts]
-    state.conditions.propulsion.lift_throttle               [0-1]
-    state.conditions.propulsion.throttle                    [0-1]
-    
-    Properties Used:
-    N/A
-
-
-
- -

◆ unpack_unknowns_no_forward()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward.unpack_unknowns_no_forward ( self,
 segment,
 state 
)
-
-
This is an extra set of unknowns which are unpacked from the mission solver and send to the network.
-    This uses only the lift motors.
-    
-    Assumptions:
-    Only the lift motors.
-    
-    Source:
-    N/A
-    
-    Inputs:
-    state.unknowns.propeller_power_coefficient [None]
-    state.unknowns.battery_voltage_under_load  [volts]
-    state.unknowns.lift_throttle               [0-1]
-    state.unknowns.throttle                    [0-1]
-    
-    Outputs:
-    state.conditions.propulsion.propeller_power_coefficient [None]
-    state.conditions.propulsion.battery_voltage_under_load  [volts]
-    state.conditions.propulsion.lift_throttle               [0-1]
-    state.conditions.propulsion.throttle                    [0-1]
-    
-    Properties Used:
-    N/A
-
-
-
- -

◆ unpack_unknowns_no_lift()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward.unpack_unknowns_no_lift ( self,
 segment,
 state 
)
-
-
This is an extra set of unknowns which are unpacked from the mission solver and send to the network.
-    This uses only the forward motors and turns the rest off.
-    
-    Assumptions:
-    Only the forward motors and turns the rest off.
-    
-    Source:
-    N/A
-    
-    Inputs:
-    state.unknowns.propeller_power_coefficient [None]
-    state.unknowns.battery_voltage_under_load  [volts]
-    state.unknowns.lift_throttle               [0-1]
-    state.unknowns.throttle                    [0-1]
-    
-    Outputs:
-    state.conditions.propulsion.propeller_power_coefficient [None]
-    state.conditions.propulsion.battery_voltage_under_load  [volts]
-    state.conditions.propulsion.lift_throttle               [0-1]
-    state.conditions.propulsion.throttle                    [0-1]
-    
-    Properties Used:
-    N/A
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Energy/Networks/Lift_Forward_Propulsor.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Lift__Forward__Propulsor_1_1Lift__Forward.js b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Lift__Forward__Propulsor_1_1Lift__Forward.js deleted file mode 100644 index 862049bb..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Lift__Forward__Propulsor_1_1Lift__Forward.js +++ /dev/null @@ -1,29 +0,0 @@ -var classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Lift__Forward__Propulsor_1_1Lift__Forward = -[ - [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Lift__Forward__Propulsor_1_1Lift__Forward.html#a70da1341e8a327f1a4647e9613601863", null ], - [ "evaluate_thrust", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Lift__Forward__Propulsor_1_1Lift__Forward.html#ada609dfe53e8ed938726421966e03a47", null ], - [ "residuals", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Lift__Forward__Propulsor_1_1Lift__Forward.html#a5c669167bb6583a6c74b014c891dd4cc", null ], - [ "residuals_no_forward", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Lift__Forward__Propulsor_1_1Lift__Forward.html#a13370553f57a134e82491c9fd28ffe1a", null ], - [ "residuals_no_lift", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Lift__Forward__Propulsor_1_1Lift__Forward.html#a2aaaa06df4872f6377df6aef529d22a6", null ], - [ "unpack_unknowns", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Lift__Forward__Propulsor_1_1Lift__Forward.html#ae28833488e1f15551c7481147726284d", null ], - [ "unpack_unknowns_no_forward", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Lift__Forward__Propulsor_1_1Lift__Forward.html#aa6ff8ff8c2b09b442860d73a9c71a7f3", null ], - [ "unpack_unknowns_no_lift", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Lift__Forward__Propulsor_1_1Lift__Forward.html#a0189fcccc5ff170b38374fd1f6631a2d", null ], - [ "avionics", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Lift__Forward__Propulsor_1_1Lift__Forward.html#a9e60dcdebe35c4633b29761b79b3de1b", null ], - [ "battery", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Lift__Forward__Propulsor_1_1Lift__Forward.html#af2ca157af33b504ffad5331268a6db38", null ], - [ "engine_length_forward", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Lift__Forward__Propulsor_1_1Lift__Forward.html#aa930858a6f7c869d7b1283b7b133daf7", null ], - [ "engine_length_lift", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Lift__Forward__Propulsor_1_1Lift__Forward.html#a5dbbae599c054a4c1b0595f28af2d309", null ], - [ "esc_forward", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Lift__Forward__Propulsor_1_1Lift__Forward.html#a43f0a6b71747bb045ee9819faf7e3ec5", null ], - [ "esc_lift", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Lift__Forward__Propulsor_1_1Lift__Forward.html#a1f69f8bcef612362d21d6151b79c75c1", null ], - [ "motor_forward", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Lift__Forward__Propulsor_1_1Lift__Forward.html#af45fc281583b6c7fc329e93810bcf67e", null ], - [ "motor_lift", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Lift__Forward__Propulsor_1_1Lift__Forward.html#ab41a35a115f49f8ca9617ea4817f18f6", null ], - [ "nacelle_diameter_forward", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Lift__Forward__Propulsor_1_1Lift__Forward.html#a953f74fdd172b24bd44b921518b699a2", null ], - [ "nacelle_diameter_lift", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Lift__Forward__Propulsor_1_1Lift__Forward.html#a6c7147181917549e44f7b0b6f142b8ba", null ], - [ "number_of_engines_forward", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Lift__Forward__Propulsor_1_1Lift__Forward.html#a1a02d2e17e737685e12044c43aff300a", null ], - [ "number_of_engines_lift", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Lift__Forward__Propulsor_1_1Lift__Forward.html#a1880338cda033740b78bf225dfd551e0", null ], - [ "payload", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Lift__Forward__Propulsor_1_1Lift__Forward.html#a6aa7c868fd51dbb06b24fa9762183be9", null ], - [ "propeller_forward", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Lift__Forward__Propulsor_1_1Lift__Forward.html#aa23be534a4e872268a8cbd2c3ab11008", null ], - [ "propeller_lift", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Lift__Forward__Propulsor_1_1Lift__Forward.html#abb971dd482411273280c33cd5cf9111f", null ], - [ "thrust_angle_forward", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Lift__Forward__Propulsor_1_1Lift__Forward.html#a7a6de6d291e84c8314b88bef6dc96e24", null ], - [ "thrust_angle_lift", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Lift__Forward__Propulsor_1_1Lift__Forward.html#a60f7d7d0ae4b9adc1114c22becbb62da", null ], - [ "voltage", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Lift__Forward__Propulsor_1_1Lift__Forward.html#ac7c75644feb40764cb254be46a4690b0", null ] -]; 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- - - - - - - - -
-
SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
-
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SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate Member List
-
-
- -

This is the complete list of members for SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate, including all inherited members.

- - - - - - - - - - - - - - - - - -
__defaults__(self)SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate
areas (defined in SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate)SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate
build_surrogate(self)SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate
engine_length (defined in SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate)SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate
evaluate_thrust(self, state)SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate
input_file (defined in SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate)SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
nacelle_diameter (defined in SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate)SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate
number_of_engines (defined in SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate)SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
sfc_surrogate (defined in SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate)SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate
surrogate_type (defined in SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate)SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate)SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate
thrust_angle (defined in SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate)SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate
thrust_surrogate (defined in SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate)SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Propulsor__Surrogate_1_1Propulsor__Surrogate.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Propulsor__Surrogate_1_1Propulsor__Surrogate.html deleted file mode 100644 index 0851622e..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Propulsor__Surrogate_1_1Propulsor__Surrogate.html +++ /dev/null @@ -1,333 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate Class Reference
-
-
-
-Inheritance diagram for SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate:
-
-
- - -SUAVE.Components.Propulsors.Propulsor.Propulsor -SUAVE.Components.Physical_Component.Physical_Component -SUAVE.Components.Component.Component - -
- - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def evaluate_thrust (self, state)
 
def build_surrogate (self)
 
- Public Member Functions inherited from SUAVE.Components.Propulsors.Propulsor.Propulsor
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

nacelle_diameter
 
engine_length
 
number_of_engines
 
tag
 
input_file
 
sfc_surrogate
 
thrust_surrogate
 
thrust_angle
 
areas
 
surrogate_type
 
- Public Attributes inherited from SUAVE.Components.Propulsors.Propulsor.Propulsor
tag
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
-

Detailed Description

-
This is a way for you to load engine data from a source.
-    A .csv file is read in, a surrogate made, that surrogate is used during the mission analysis.
-    
-    You need to use build surrogate first when setting up the vehicle to make this work.
-
-    Assumptions:
-    The input format for this should be Altitude, Mach, Throttle, Thrust, SFC
-    
-    Source:
-    None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate.__defaults__ ( self)
-
-
This sets the default values for the network to function.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    N/A
-
-
-
- -

◆ build_surrogate()

- -
-
- - - - - - - - -
def SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate.build_surrogate ( self)
-
-
Build a surrogate. Multiple options for models are available including:
-    -Gaussian Processes
-    -KNN
-    -SVR
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    state [state()]
-    
-    Outputs:
-    self.sfc_surrogate    [fun()]
-    self.thrust_surrogate [fun()]
-    
-    Properties Used:
-    Defaulted values
-
-
-
- -

◆ evaluate_thrust()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate.evaluate_thrust ( self,
 state 
)
-
-
Calculate thrust given the current state of the vehicle
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    state [state()]
-    
-    Outputs:
-    results.thrust_force_vector [newtons]
-    results.vehicle_mass_rate   [kg/s]
-    
-    Properties Used:
-    Defaulted values
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Energy/Networks/Propulsor_Surrogate.py
  • -
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Propulsor__Surrogate_1_1Propulsor__Surrogate.js b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Propulsor__Surrogate_1_1Propulsor__Surrogate.js deleted file mode 100644 index abbade27..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Propulsor__Surrogate_1_1Propulsor__Surrogate.js +++ /dev/null @@ -1,16 +0,0 @@ -var classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Propulsor__Surrogate_1_1Propulsor__Surrogate = -[ - [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Propulsor__Surrogate_1_1Propulsor__Surrogate.html#ac3623a6164073e210b9a47c9ac179675", null ], - [ "build_surrogate", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Propulsor__Surrogate_1_1Propulsor__Surrogate.html#a983089ddf1aee9c63dd67cb54be750bc", null ], - [ "evaluate_thrust", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Propulsor__Surrogate_1_1Propulsor__Surrogate.html#a0431c37a2355c55c6b956c8a0f34c117", null ], - [ "areas", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Propulsor__Surrogate_1_1Propulsor__Surrogate.html#a43a943b42a00b837368c7f0af5f5e632", null ], - [ "engine_length", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Propulsor__Surrogate_1_1Propulsor__Surrogate.html#a22f2b4329ab6cdf8b94fd2272a614225", null ], - [ "input_file", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Propulsor__Surrogate_1_1Propulsor__Surrogate.html#aa50a9643ba03f73f53e997038f24ee72", null ], - [ "nacelle_diameter", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Propulsor__Surrogate_1_1Propulsor__Surrogate.html#a319ad4cfb0f0729d1d57dd456f5cb7ac", null ], - [ "number_of_engines", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Propulsor__Surrogate_1_1Propulsor__Surrogate.html#abee949d1cdde57a683f87cbb0947c854", null ], - [ "sfc_surrogate", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Propulsor__Surrogate_1_1Propulsor__Surrogate.html#a50dd24280b7aa9da32b836fe0ca33842", null ], - [ "surrogate_type", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Propulsor__Surrogate_1_1Propulsor__Surrogate.html#adb1c55a957e8fa9e6b31853e2d61031f", null ], - [ "tag", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Propulsor__Surrogate_1_1Propulsor__Surrogate.html#ab1a2cd84ddf70535cf8be599b02c00eb", null ], - [ "thrust_angle", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Propulsor__Surrogate_1_1Propulsor__Surrogate.html#a987fb867374d30397995a8bc306c4887", null ], - [ "thrust_surrogate", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Propulsor__Surrogate_1_1Propulsor__Surrogate.html#acc030cf367c0a0aed49beb116503287d", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Propulsor__Surrogate_1_1Propulsor__Surrogate.png b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Propulsor__Surrogate_1_1Propulsor__Surrogate.png deleted file mode 100644 index c5c83d7f..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Propulsor__Surrogate_1_1Propulsor__Surrogate.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar-members.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar-members.html deleted file mode 100644 index f44ac7d0..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar-members.html +++ /dev/null @@ -1,132 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Energy.Networks.Solar.Solar Member List
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This is the complete list of members for SUAVE.Components.Energy.Networks.Solar.Solar, including all inherited members.

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__defaults__(self)SUAVE.Components.Energy.Networks.Solar.Solar
avionics (defined in SUAVE.Components.Energy.Networks.Solar.Solar)SUAVE.Components.Energy.Networks.Solar.Solar
battery (defined in SUAVE.Components.Energy.Networks.Solar.Solar)SUAVE.Components.Energy.Networks.Solar.Solar
engine_length (defined in SUAVE.Components.Energy.Networks.Solar.Solar)SUAVE.Components.Energy.Networks.Solar.Solar
esc (defined in SUAVE.Components.Energy.Networks.Solar.Solar)SUAVE.Components.Energy.Networks.Solar.Solar
evaluate_thrust(self, state)SUAVE.Components.Energy.Networks.Solar.Solar
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
motor (defined in SUAVE.Components.Energy.Networks.Solar.Solar)SUAVE.Components.Energy.Networks.Solar.Solar
nacelle_diameter (defined in SUAVE.Components.Energy.Networks.Solar.Solar)SUAVE.Components.Energy.Networks.Solar.Solar
number_of_engines (defined in SUAVE.Components.Energy.Networks.Solar.Solar)SUAVE.Components.Energy.Networks.Solar.Solar
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
payload (defined in SUAVE.Components.Energy.Networks.Solar.Solar)SUAVE.Components.Energy.Networks.Solar.Solar
propeller (defined in SUAVE.Components.Energy.Networks.Solar.Solar)SUAVE.Components.Energy.Networks.Solar.Solar
residuals(self, segment, state)SUAVE.Components.Energy.Networks.Solar.Solar
solar_flux (defined in SUAVE.Components.Energy.Networks.Solar.Solar)SUAVE.Components.Energy.Networks.Solar.Solar
solar_logic (defined in SUAVE.Components.Energy.Networks.Solar.Solar)SUAVE.Components.Energy.Networks.Solar.Solar
solar_panel (defined in SUAVE.Components.Energy.Networks.Solar.Solar)SUAVE.Components.Energy.Networks.Solar.Solar
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Energy.Networks.Solar.Solar)SUAVE.Components.Energy.Networks.Solar.Solar
unpack_unknowns(self, segment, state)SUAVE.Components.Energy.Networks.Solar.Solar
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar.html deleted file mode 100644 index e8eae18a..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar.html +++ /dev/null @@ -1,415 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Components.Energy.Networks.Solar.Solar Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Energy.Networks.Solar.Solar Class Reference
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-Inheritance diagram for SUAVE.Components.Energy.Networks.Solar.Solar:
-
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- - -SUAVE.Components.Propulsors.Propulsor.Propulsor -SUAVE.Components.Physical_Component.Physical_Component -SUAVE.Components.Component.Component - -
- - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def evaluate_thrust (self, state)
 
def unpack_unknowns (self, segment, state)
 
def residuals (self, segment, state)
 
- Public Member Functions inherited from SUAVE.Components.Propulsors.Propulsor.Propulsor
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
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-Public Attributes

solar_flux
 
solar_panel
 
motor
 
propeller
 
esc
 
avionics
 
payload
 
solar_logic
 
battery
 
nacelle_diameter
 
engine_length
 
number_of_engines
 
tag
 
- Public Attributes inherited from SUAVE.Components.Propulsors.Propulsor.Propulsor
tag
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
-

Detailed Description

-
A solar powered system with batteries and maximum power point tracking.
-    
-    This network adds an extra unknowns to the mission, the torque matching between motor and propeller.
-
-    Assumptions:
-    None
-    
-    Source:
-    None
-

Member Function Documentation

- -

◆ __defaults__()

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def SUAVE.Components.Energy.Networks.Solar.Solar.__defaults__ ( self)
-
-
This sets the default values for the network to function.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    N/A
-
-
-
- -

◆ evaluate_thrust()

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def SUAVE.Components.Energy.Networks.Solar.Solar.evaluate_thrust ( self,
 state 
)
-
-
Calculate thrust given the current state of the vehicle
-    
-    Assumptions:
-    Caps the throttle at 110% and linearly interpolates thrust off that
-    
-    Source:
-    N/A
-    
-    Inputs:
-    state [state()]
-    
-    Outputs:
-    results.thrust_force_vector [newtons]
-    results.vehicle_mass_rate   [kg/s]
-    conditions.propulsion:
-solar_flux           [watts/m^2] 
-rpm                  [radians/sec]
-current              [amps]
-battery_draw         [watts]
-battery_energy       [joules]
-motor_torque         [N-M]
-propeller_torque     [N-M]
-    
-    Properties Used:
-    Defaulted values
-
-
-
- -

◆ residuals()

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def SUAVE.Components.Energy.Networks.Solar.Solar.residuals ( self,
 segment,
 state 
)
-
-
This packs the residuals to be send to the mission solver.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    state.conditions.propulsion:
-motor_torque                          [N-m]
-propeller_torque                      [N-m]
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
- -

◆ unpack_unknowns()

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def SUAVE.Components.Energy.Networks.Solar.Solar.unpack_unknowns ( self,
 segment,
 state 
)
-
-
This is an extra set of unknowns which are unpacked from the mission solver and send to the network.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    state.unknowns.propeller_power_coefficient [None]
-    
-    Outputs:
-    state.conditions.propulsion.propeller_power_coefficient [None]
-    
-    Properties Used:
-    N/A
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Energy/Networks/Solar.py
  • -
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar.js b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar.js deleted file mode 100644 index 9ee33118..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar.js +++ /dev/null @@ -1,20 +0,0 @@ -var classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar = -[ - [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar.html#a1b845035b4dfa9e54c0487e6d9c1c55b", null ], - [ "evaluate_thrust", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar.html#a03837081f89d8b2f3e50455f44411e41", null ], - [ "residuals", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar.html#afc4852d79b60415d25511fc2a6bb1930", null ], - [ "unpack_unknowns", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar.html#a7d95eeb99fa7ca3bd14e4c5f833f09c8", null ], - [ "avionics", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar.html#a1f33f40e58f05ee58ed0669fe5302e72", null ], - [ "battery", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar.html#ac16762f88873f88419a0d851b4d7c5f0", null ], - [ "engine_length", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar.html#a9e7c3492cc016f11fd98c3a47317961f", null ], - [ "esc", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar.html#a33cfb357ddf776d510b8501cdadfc777", null ], - [ "motor", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar.html#aaedcd0dd93c8c610bdfb6760269bf3a1", null ], - [ "nacelle_diameter", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar.html#a072998c85626b49f300270c8e4b5a8c9", null ], - [ "number_of_engines", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar.html#af9d3157b48236320e321b822a10427fb", null ], - [ "payload", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar.html#ab2fe0fa4d19dc750a430fbd2d2c7fbd5", null ], - [ "propeller", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar.html#a9bfbd8f231fa46f7f693a7340556fb1a", null ], - [ "solar_flux", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar.html#ad9c27f16e7457864328b37d4111abda0", null ], - [ "solar_logic", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar.html#a70294c7d2ddd2f3b719e7777e9845d6b", null ], - [ "solar_panel", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar.html#af1a064708a49ca2d7bb64912724e69b2", null ], - [ "tag", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar.html#a28f5aacd5ba78c3de21f5af4f4808f9b", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar.png b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar.png deleted file mode 100644 index 63eb68b1..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar__Low__Fidelity_1_1Solar__Low__Fidelity-members.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar__Low__Fidelity_1_1Solar__Low__Fidelity-members.html deleted file mode 100644 index e4f3aa78..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar__Low__Fidelity_1_1Solar__Low__Fidelity-members.html +++ /dev/null @@ -1,130 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity Member List
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- -

This is the complete list of members for SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity, including all inherited members.

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__defaults__(self)SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity
avionics (defined in SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity)SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity
battery (defined in SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity)SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity
engine_length (defined in SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity)SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity
esc (defined in SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity)SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity
evaluate_thrust(self, state)SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
motor (defined in SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity)SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity
nacelle_dia (defined in SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity)SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity
number_of_engines (defined in SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity)SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
payload (defined in SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity)SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity
propeller (defined in SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity)SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity
solar_flux (defined in SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity)SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity
solar_logic (defined in SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity)SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity
solar_panel (defined in SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity)SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity)SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar__Low__Fidelity_1_1Solar__Low__Fidelity.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar__Low__Fidelity_1_1Solar__Low__Fidelity.html deleted file mode 100644 index d927870c..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar__Low__Fidelity_1_1Solar__Low__Fidelity.html +++ /dev/null @@ -1,308 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity Class Reference - - - - - - - - - - - - - - - -
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- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity Class Reference
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-
-
-Inheritance diagram for SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity:
-
-
- - -SUAVE.Components.Propulsors.Propulsor.Propulsor -SUAVE.Components.Physical_Component.Physical_Component -SUAVE.Components.Component.Component - -
- - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def evaluate_thrust (self, state)
 
- Public Member Functions inherited from SUAVE.Components.Propulsors.Propulsor.Propulsor
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

solar_flux
 
solar_panel
 
motor
 
propeller
 
esc
 
avionics
 
payload
 
solar_logic
 
battery
 
nacelle_dia
 
engine_length
 
number_of_engines
 
tag
 
- Public Attributes inherited from SUAVE.Components.Propulsors.Propulsor.Propulsor
tag
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
-

Detailed Description

-
A solar powered system with batteries and maximum power point tracking.
-    
-    This network adds an extra unknowns to the mission, the torque matching between motor and propeller.
-
-    Assumptions:
-    This model uses the low fidelity motor and propeller model to speed computation.
-    This reduces accuracy as it is assuming a simple efficiency
-    
-    Source:
-    None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity.__defaults__ ( self)
-
-
This sets the default values for the network to function.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    N/A
-
-
-
- -

◆ evaluate_thrust()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity.evaluate_thrust ( self,
 state 
)
-
-
Calculate thrust given the current state of the vehicle
-    
-    Assumptions:
-    Caps the throttle at 110% and linearly interpolates thrust off that
-    
-    Source:
-    N/A
-    
-    Inputs:
-    state [state()]
-    
-    Outputs:
-    results.thrust_force_vector [newtons]
-    results.vehicle_mass_rate   [kg/s]
-    conditions.propulsion:
-solar_flux           [watts/m^2] 
-rpm                  [radians/sec]
-current              [amps]
-battery_draw         [watts]
-battery_energy       [joules]
-
-    Properties Used:
-    Defaulted values
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Energy/Networks/Solar_Low_Fidelity.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar__Low__Fidelity_1_1Solar__Low__Fidelity.js b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar__Low__Fidelity_1_1Solar__Low__Fidelity.js deleted file mode 100644 index fd41ef09..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar__Low__Fidelity_1_1Solar__Low__Fidelity.js +++ /dev/null @@ -1,18 +0,0 @@ -var classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar__Low__Fidelity_1_1Solar__Low__Fidelity = -[ - [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar__Low__Fidelity_1_1Solar__Low__Fidelity.html#a8c234f92097f1e00d836e134236e5d33", null ], - [ "evaluate_thrust", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar__Low__Fidelity_1_1Solar__Low__Fidelity.html#ac70deccb1a3eb33088c5413488a9a4d2", null ], - [ "avionics", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar__Low__Fidelity_1_1Solar__Low__Fidelity.html#a65d53083a4146fe80ec0dfced2ca87be", null ], - [ "battery", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar__Low__Fidelity_1_1Solar__Low__Fidelity.html#ace5a5a7a2d5e6b7a5aa9ac8e0a66cf0c", null ], - [ "engine_length", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar__Low__Fidelity_1_1Solar__Low__Fidelity.html#ae59b65392146034a9b407394de7c336f", null ], - [ "esc", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar__Low__Fidelity_1_1Solar__Low__Fidelity.html#ae7fc5861cb4a944129c9749270885b0e", null ], - [ "motor", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar__Low__Fidelity_1_1Solar__Low__Fidelity.html#acae5bbd194cad986cfd52f880a22935f", null ], - [ "nacelle_dia", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar__Low__Fidelity_1_1Solar__Low__Fidelity.html#acc0224108fa8af8cf4f290ccb30c0272", null ], - [ "number_of_engines", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar__Low__Fidelity_1_1Solar__Low__Fidelity.html#a4a5ad2f9600fa7bcd88310f7f972700e", null ], - [ "payload", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar__Low__Fidelity_1_1Solar__Low__Fidelity.html#a233c717fad987512c42cb83c53e4c651", null ], - [ "propeller", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar__Low__Fidelity_1_1Solar__Low__Fidelity.html#a8e2853156ffcf1aef68eb1108d852da4", null ], - [ "solar_flux", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar__Low__Fidelity_1_1Solar__Low__Fidelity.html#aa28e2e6e7acec0716377ed10bad1392a", null ], - [ "solar_logic", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar__Low__Fidelity_1_1Solar__Low__Fidelity.html#a11fc9922ff807efcd9ef99e0c37d41c9", null ], - [ "solar_panel", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar__Low__Fidelity_1_1Solar__Low__Fidelity.html#ac02569a947e971d2287c7480544ae722", null ], - [ "tag", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar__Low__Fidelity_1_1Solar__Low__Fidelity.html#a77be18098afc3c7ce30d5e8f0e1a9b40", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar__Low__Fidelity_1_1Solar__Low__Fidelity.png b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar__Low__Fidelity_1_1Solar__Low__Fidelity.png deleted file mode 100644 index 05054854..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar__Low__Fidelity_1_1Solar__Low__Fidelity.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbofan_1_1Turbofan-members.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbofan_1_1Turbofan-members.html deleted file mode 100644 index 5baefe0c..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbofan_1_1Turbofan-members.html +++ /dev/null @@ -1,125 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Energy.Networks.Turbofan.Turbofan Member List
-
-
- -

This is the complete list of members for SUAVE.Components.Energy.Networks.Turbofan.Turbofan, including all inherited members.

- - - - - - - - - - - - - - -
__defaults__(self)SUAVE.Components.Energy.Networks.Turbofan.Turbofan
areas (defined in SUAVE.Components.Energy.Networks.Turbofan.Turbofan)SUAVE.Components.Energy.Networks.Turbofan.Turbofan
bypass_ratio (defined in SUAVE.Components.Energy.Networks.Turbofan.Turbofan)SUAVE.Components.Energy.Networks.Turbofan.Turbofan
engine_length (defined in SUAVE.Components.Energy.Networks.Turbofan.Turbofan)SUAVE.Components.Energy.Networks.Turbofan.Turbofan
engine_out(self, state)SUAVE.Components.Energy.Networks.Turbofan.Turbofan
evaluate_thrust(self, state)SUAVE.Components.Energy.Networks.Turbofan.Turbofan
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
nacelle_diameter (defined in SUAVE.Components.Energy.Networks.Turbofan.Turbofan)SUAVE.Components.Energy.Networks.Turbofan.Turbofan
number_of_engines (defined in SUAVE.Components.Energy.Networks.Turbofan.Turbofan)SUAVE.Components.Energy.Networks.Turbofan.Turbofan
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
size(self, state)SUAVE.Components.Energy.Networks.Turbofan.Turbofan
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Energy.Networks.Turbofan.Turbofan)SUAVE.Components.Energy.Networks.Turbofan.Turbofan
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbofan_1_1Turbofan.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbofan_1_1Turbofan.html deleted file mode 100644 index 36c5e384..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbofan_1_1Turbofan.html +++ /dev/null @@ -1,384 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Components.Energy.Networks.Turbofan.Turbofan Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Energy.Networks.Turbofan.Turbofan Class Reference
-
-
-
-Inheritance diagram for SUAVE.Components.Energy.Networks.Turbofan.Turbofan:
-
-
- - -SUAVE.Components.Propulsors.Propulsor.Propulsor -SUAVE.Components.Physical_Component.Physical_Component -SUAVE.Components.Component.Component - -
- - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def evaluate_thrust (self, state)
 
def size (self, state)
 
def engine_out (self, state)
 
- Public Member Functions inherited from SUAVE.Components.Propulsors.Propulsor.Propulsor
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

tag
 
number_of_engines
 
nacelle_diameter
 
engine_length
 
bypass_ratio
 
areas
 
- Public Attributes inherited from SUAVE.Components.Propulsors.Propulsor.Propulsor
tag
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
-

Detailed Description

-
This is a turbofan. 
-
-    Assumptions:
-    None
-    
-    Source:
-    Most of the componentes come from this book:
-    https://web.stanford.edu/~cantwell/AA283_Course_Material/AA283_Course_Notes/
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Components.Energy.Networks.Turbofan.Turbofan.__defaults__ ( self)
-
-
This sets the default values for the network to function.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    N/A
-
-
-
- -

◆ engine_out()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Components.Energy.Networks.Turbofan.Turbofan.engine_out ( self,
 state 
)
-
-
Lose an engine
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    N/A
-
-
-
- -

◆ evaluate_thrust()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Components.Energy.Networks.Turbofan.Turbofan.evaluate_thrust ( self,
 state 
)
-
-
Calculate thrust given the current state of the vehicle
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    state [state()]
-    
-    Outputs:
-    results.thrust_force_vector [newtons]
-    results.vehicle_mass_rate   [kg/s]
-    conditions.propulsion.acoustic_outputs:
-core:
-    exit_static_temperature      
-    exit_static_pressure       
-    exit_stagnation_temperature 
-    exit_stagnation_pressure
-    exit_velocity 
-fan:
-    exit_static_temperature      
-    exit_static_pressure       
-    exit_stagnation_temperature 
-    exit_stagnation_pressure
-    exit_velocity 
-    
-    Properties Used:
-    Defaulted values
-
-
-
- -

◆ size()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Components.Energy.Networks.Turbofan.Turbofan.size ( self,
 state 
)
-
-
Size the turbofan
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    State [state()]
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    N/A
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Energy/Networks/Turbofan.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbofan_1_1Turbofan.js b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbofan_1_1Turbofan.js deleted file mode 100644 index 34fbf304..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbofan_1_1Turbofan.js +++ /dev/null @@ -1,13 +0,0 @@ -var classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbofan_1_1Turbofan = -[ - [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbofan_1_1Turbofan.html#a4ec9fd9367a661587c9067770654e380", null ], - [ "engine_out", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbofan_1_1Turbofan.html#a60e0d2eab2e30852f0bec0a09b95920a", null ], - [ "evaluate_thrust", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbofan_1_1Turbofan.html#a756c8dc0e7bb56646703f11a74012315", null ], - [ "size", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbofan_1_1Turbofan.html#aa5b08f9f6391cfc6fae54dcd4ba64a97", null ], - [ "areas", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbofan_1_1Turbofan.html#a507a47908221e71e51bdb6edf7a6f4ab", null ], - [ "bypass_ratio", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbofan_1_1Turbofan.html#a7da8c93851aa2763d0a38f53de203619", null ], - [ "engine_length", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbofan_1_1Turbofan.html#a5985a59648a18ea778c429c5cf2ac948", null ], - [ "nacelle_diameter", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbofan_1_1Turbofan.html#a1bf3a72eac55b30fc00ddc8cdc099d26", null ], - [ "number_of_engines", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbofan_1_1Turbofan.html#ac838a4ddc129e87df7fe82977d42caad", null ], - [ "tag", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbofan_1_1Turbofan.html#a643c70b63ac983fcf945798e9cbc1bcf", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbofan_1_1Turbofan.png b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbofan_1_1Turbofan.png deleted file mode 100644 index 6f15b8a1..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbofan_1_1Turbofan.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbojet__Super_1_1Turbojet__Super-members.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbojet__Super_1_1Turbojet__Super-members.html deleted file mode 100644 index 06b5bd8e..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbojet__Super_1_1Turbojet__Super-members.html +++ /dev/null @@ -1,153 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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- - -
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SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super Member List
-
-
- -

This is the complete list of members for SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super, including all inherited members.

- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
__defaults__(self) (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super
bypass_ratio (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Superstatic
combustor (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Superstatic
compressor (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Superstatic
conditionsSUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Superstatic
core_area_ratio (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Superstatic
core_exit_velocity (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Superstatic
core_nozzle (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Superstatic
engine_length (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Superstatic
evaluate_thrust(self, state) (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super
F (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Superstatic
F (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Superstatic
F_vec (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Superstatic
flow_through_core (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Superstatic
flow_through_fan (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Superstatic
fuel_to_air_ratio (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Superstatic
high_pressure_compressor (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Superstatic
high_pressure_turbine (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Superstatic
inlet_nozzle (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Superstatic
Isp (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Superstatic
low_pressure_compressor (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Superstatic
low_pressure_turbine (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Superstatic
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
mdot (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Superstatic
nacelle_diameter (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Superstatic
number_of_engines (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Superstatic
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
output_power (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Superstatic
ram (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Superstatic
results (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Superstatic
size(self, state) (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super
stag_press_lpt_exit (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Superstatic
stag_temp_lpt_exit (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Superstatic
stagnation_pressure (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Superstatic
stagnation_temperature (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Superstatic
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tagSUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Superstatic
thrust (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Superstatic
thrust_force_vector (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Superstatic
vehicle_mass_rate (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Superstatic
working_fluid (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Superstatic
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbojet__Super_1_1Turbojet__Super.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbojet__Super_1_1Turbojet__Super.html deleted file mode 100644 index a4c934cc..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbojet__Super_1_1Turbojet__Super.html +++ /dev/null @@ -1,383 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super Class Reference - - - - - - - - - - - - - - - -
-
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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- -
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- -
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SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super Class Reference
-
-
-
-Inheritance diagram for SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super:
-
-
- - -SUAVE.Components.Propulsors.Propulsor.Propulsor -SUAVE.Components.Physical_Component.Physical_Component -SUAVE.Components.Component.Component - -
- - - - - - - - - - - - - - - - - -

-Public Member Functions

-def __defaults__ (self)
 
-def evaluate_thrust (self, state)
 
-def size (self, state)
 
- Public Member Functions inherited from SUAVE.Components.Propulsors.Propulsor.Propulsor
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Static Public Attributes

 tag
 
number_of_engines = self.number_of_engines
 
nacelle_diameter
 
engine_length
 
 conditions = state.conditions
 
ram = self.ram
 
inlet_nozzle = self.inlet_nozzle
 
low_pressure_compressor = self.low_pressure_compressor
 
high_pressure_compressor = self.high_pressure_compressor
 
combustor = self.combustor
 
high_pressure_turbine = self.high_pressure_turbine
 
low_pressure_turbine = self.low_pressure_turbine
 
core_nozzle = self.core_nozzle
 
thrust = self.thrust
 
working_fluid
 
stagnation_temperature
 
stagnation_pressure
 
fuel_to_air_ratio
 
compressor
 
bypass_ratio
 
core_exit_velocity
 
core_area_ratio
 
stag_temp_lpt_exit
 
stag_press_lpt_exit
 
flow_through_core
 
flow_through_fan
 
F = thrust.outputs.thrust*[1,0,0]
 
mdot = thrust.outputs.fuel_flow_rate
 
Isp = thrust.outputs.specific_impulse
 
output_power = thrust.outputs.power
 
-float F_vec = conditions.ones_row(3) * 0.0
 
-float F = F_vec
 
results = Data()
 
thrust_force_vector
 
vehicle_mass_rate
 
- - - - - - - - - - - - - - - - - - -

-Additional Inherited Members

- Public Attributes inherited from SUAVE.Components.Propulsors.Propulsor.Propulsor
tag
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
-

Detailed Description

-
This is a turbojet for supersonic flight.
-
-    Assumptions:
-    None
-
-    Source:
-    Most of the componentes come from this book:
-    https://web.stanford.edu/~cantwell/AA283_Course_Material/AA283_Course_Notes/
-

Member Data Documentation

- -

◆ conditions

- -
-
- - - - - -
- - - - -
SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super.conditions = state.conditions
-
-static
-
-
Calculate thrust given the current state of the vehicle
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-state [state()]
-
-Outputs:
-results.thrust_force_vector [newtons]
-results.vehicle_mass_rate   [kg/s]
-conditions.propulsion.acoustic_outputs:
-    core:
-    exit_static_temperature      
-    exit_static_pressure       
-    exit_stagnation_temperature 
-    exit_stagnation_pressure
-    exit_velocity 
-    fan:
-    exit_static_temperature      
-    exit_static_pressure       
-    exit_stagnation_temperature 
-    exit_stagnation_pressure
-    exit_velocity 
-
-Properties Used:
-Defaulted values
-
-
-
- -

◆ tag

- -
-
- - - - - -
- - - - -
SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super.tag
-
-static
-
-
This sets the default values for the network to function.
-
-    Assumptions:
-    None
-
-    Source:
-    N/A
-
-    Inputs:
-    None
-
-    Outputs:
-    None
-
-    Properties Used:
-    N/A
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Energy/Networks/Turbojet_Super.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbojet__Super_1_1Turbojet__Super.js b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbojet__Super_1_1Turbojet__Super.js deleted file mode 100644 index 4bc542f8..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbojet__Super_1_1Turbojet__Super.js +++ /dev/null @@ -1,6 +0,0 @@ -var classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbojet__Super_1_1Turbojet__Super = -[ - [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbojet__Super_1_1Turbojet__Super.html#ab4871db4337784d79070b2b52f4a1287", null ], - [ "evaluate_thrust", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbojet__Super_1_1Turbojet__Super.html#ac08d01e1cb8d375476c9363d9bc05c43", null ], - [ "size", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbojet__Super_1_1Turbojet__Super.html#a2c1031116d3527670cf4a69e55d79649", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbojet__Super_1_1Turbojet__Super.png b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbojet__Super_1_1Turbojet__Super.png deleted file mode 100644 index dc4f3d62..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbojet__Super_1_1Turbojet__Super.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Peripherals_1_1Avionics_1_1Avionics-members.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Peripherals_1_1Avionics_1_1Avionics-members.html deleted file mode 100644 index 33ff4c0e..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Peripherals_1_1Avionics_1_1Avionics-members.html +++ /dev/null @@ -1,121 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
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- - - - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Peripherals_1_1Avionics_1_1Avionics.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Peripherals_1_1Avionics_1_1Avionics.html deleted file mode 100644 index b1fdf87d..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Peripherals_1_1Avionics_1_1Avionics.html +++ /dev/null @@ -1,255 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Components.Energy.Peripherals.Avionics.Avionics Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Energy.Peripherals.Avionics.Avionics Class Reference
-
-
-
-Inheritance diagram for SUAVE.Components.Energy.Peripherals.Avionics.Avionics:
-
-
- - -SUAVE.Components.Energy.Energy_Component.Energy_Component -SUAVE.Components.Physical_Component.Physical_Component -SUAVE.Components.Component.Component - -
- - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def power (self)
 
- Public Member Functions inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
- - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

power_draw
 
- Public Attributes inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
inputs
 
outputs
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
-

Detailed Description

-
A class representing avionics.
-
-Assumptions:
-None
-
-Source:
-N/A
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Components.Energy.Peripherals.Avionics.Avionics.__defaults__ ( self)
-
-
This sets the default power draw.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
-
- -

◆ power()

- -
-
- - - - - - - - -
def SUAVE.Components.Energy.Peripherals.Avionics.Avionics.power ( self)
-
-
This gives the power draw from avionics.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-self.outputs.power_draw
-
-Properties Used:
-self.power_draw
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Energy/Peripherals/Avionics.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Peripherals_1_1Avionics_1_1Avionics.js b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Peripherals_1_1Avionics_1_1Avionics.js deleted file mode 100644 index 99603b87..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Peripherals_1_1Avionics_1_1Avionics.js +++ /dev/null @@ -1,6 +0,0 @@ -var classSUAVE_1_1Components_1_1Energy_1_1Peripherals_1_1Avionics_1_1Avionics = -[ - [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Peripherals_1_1Avionics_1_1Avionics.html#a9e84c9c15af2fee12b95f1da79a4ff79", null ], - [ "power", "classSUAVE_1_1Components_1_1Energy_1_1Peripherals_1_1Avionics_1_1Avionics.html#ac9c2993263546a5f21acbf48fa637a28", null ], - [ "power_draw", "classSUAVE_1_1Components_1_1Energy_1_1Peripherals_1_1Avionics_1_1Avionics.html#a47460105eda78a3f35e8bfa9e5ae2ca2", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Peripherals_1_1Avionics_1_1Avionics.png b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Peripherals_1_1Avionics_1_1Avionics.png deleted file mode 100644 index d27343e9..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Peripherals_1_1Avionics_1_1Avionics.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Peripherals_1_1Payload_1_1Payload-members.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Peripherals_1_1Payload_1_1Payload-members.html deleted file mode 100644 index 1ac701e2..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Peripherals_1_1Payload_1_1Payload-members.html +++ /dev/null @@ -1,121 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
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-
- - - -
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- - - - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Peripherals_1_1Payload_1_1Payload.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Peripherals_1_1Payload_1_1Payload.html deleted file mode 100644 index 09fd33c0..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Peripherals_1_1Payload_1_1Payload.html +++ /dev/null @@ -1,255 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Components.Energy.Peripherals.Payload.Payload Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
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SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
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- -
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SUAVE.Components.Energy.Peripherals.Payload.Payload Class Reference
-
-
-
-Inheritance diagram for SUAVE.Components.Energy.Peripherals.Payload.Payload:
-
-
- - -SUAVE.Components.Energy.Energy_Component.Energy_Component -SUAVE.Components.Physical_Component.Physical_Component -SUAVE.Components.Component.Component - -
- - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def power (self)
 
- Public Member Functions inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
- - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

power_draw
 
- Public Attributes inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
inputs
 
outputs
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
-

Detailed Description

-
A class representing a payload.
-
-Assumptions:
-None
-
-Source:
-N/A
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Components.Energy.Peripherals.Payload.Payload.__defaults__ ( self)
-
-
This sets the default power draw.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
-
- -

◆ power()

- -
-
- - - - - - - - -
def SUAVE.Components.Energy.Peripherals.Payload.Payload.power ( self)
-
-
This gives the power draw from a payload.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-self.outputs.power_draw
-
-Properties Used:
-self.power_draw
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Energy/Peripherals/Payload.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Peripherals_1_1Payload_1_1Payload.js b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Peripherals_1_1Payload_1_1Payload.js deleted file mode 100644 index 14b25bee..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Peripherals_1_1Payload_1_1Payload.js +++ /dev/null @@ -1,6 +0,0 @@ -var classSUAVE_1_1Components_1_1Energy_1_1Peripherals_1_1Payload_1_1Payload = -[ - [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Peripherals_1_1Payload_1_1Payload.html#abaf837c9d0bf2ad1dbee4090fa1be2dd", null ], - [ "power", "classSUAVE_1_1Components_1_1Energy_1_1Peripherals_1_1Payload_1_1Payload.html#a3d9e2f22339197b7199d5c6540edb4e2", null ], - [ "power_draw", "classSUAVE_1_1Components_1_1Energy_1_1Peripherals_1_1Payload_1_1Payload.html#ac50047f40cc72e42d7243a21850bb199", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Peripherals_1_1Payload_1_1Payload.png b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Peripherals_1_1Payload_1_1Payload.png deleted file mode 100644 index 21722403..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Peripherals_1_1Payload_1_1Payload.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Solar__Radiation_1_1Solar__Radiation-members.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Solar__Radiation_1_1Solar__Radiation-members.html deleted file mode 100644 index d6959c51..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Solar__Radiation_1_1Solar__Radiation-members.html +++ /dev/null @@ -1,120 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
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-
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- -
-
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- - - - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Solar__Radiation_1_1Solar__Radiation.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Solar__Radiation_1_1Solar__Radiation.html deleted file mode 100644 index 9b4de52c..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Solar__Radiation_1_1Solar__Radiation.html +++ /dev/null @@ -1,235 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Components.Energy.Processes.Solar_Radiation.Solar_Radiation Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Energy.Processes.Solar_Radiation.Solar_Radiation Class Reference
-
-
-
-Inheritance diagram for SUAVE.Components.Energy.Processes.Solar_Radiation.Solar_Radiation:
-
-
- - -SUAVE.Components.Energy.Energy_Component.Energy_Component -SUAVE.Components.Physical_Component.Physical_Component -SUAVE.Components.Component.Component - -
- - - - - - - - - - - - - -

-Public Member Functions

def solar_radiation (self, conditions)
 
- Public Member Functions inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
- - - - - - - - - - - - - - - - - - - - -

-Additional Inherited Members

- Public Attributes inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
inputs
 
outputs
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
-

Detailed Description

-
A class that handle solar radiation computation.
-
-Assumptions:
-None
-
-Source:
-N/A
-

Member Function Documentation

- -

◆ solar_radiation()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Components.Energy.Processes.Solar_Radiation.Solar_Radiation.solar_radiation ( self,
 conditions 
)
-
-
Computes the adjusted solar flux
-
-Assumptions:
-Solar intensity =1305 W/m^2
-Includes a diffuse component of 0% of the direct component
-Altitudes are not excessive 
-
-Source:
-N/A
-
-Inputs:
-conditions.frames.
-  planet.start_time        [s]
-  planet.latitude          [degrees]
-  planet.longitude         [degrees]
-  body.inertial_rotations  [radians]
-  inertial.time            [s]
-conditions.freestream.
-  altitude                 [m]
-
-Outputs:
-self.outputs.flux          [W/m^2]
-flux                       [W/m^2]
-
-Properties Used:
-N/A
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Energy/Processes/Solar_Radiation.py
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Solar__Radiation_1_1Solar__Radiation.js b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Solar__Radiation_1_1Solar__Radiation.js deleted file mode 100644 index d02d67bb..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Solar__Radiation_1_1Solar__Radiation.js +++ /dev/null @@ -1,4 +0,0 @@ -var classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Solar__Radiation_1_1Solar__Radiation = -[ - [ "solar_radiation", "classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Solar__Radiation_1_1Solar__Radiation.html#a0c7b7918398ad07a2d4b1d7d481e6418", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Solar__Radiation_1_1Solar__Radiation.png b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Solar__Radiation_1_1Solar__Radiation.png deleted file mode 100644 index 3582053e..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Solar__Radiation_1_1Solar__Radiation.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Thrust_1_1Thrust-members.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Thrust_1_1Thrust-members.html deleted file mode 100644 index f8041560..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Thrust_1_1Thrust-members.html +++ /dev/null @@ -1,128 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Energy.Processes.Thrust.Thrust Member List
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This is the complete list of members for SUAVE.Components.Energy.Processes.Thrust.Thrust, including all inherited members.

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__defaults__(self)SUAVE.Components.Energy.Processes.Thrust.Thrust
bypass_ratio (defined in SUAVE.Components.Energy.Processes.Thrust.Thrust)SUAVE.Components.Energy.Processes.Thrust.Thrust
compressor_nondimensional_massflow (defined in SUAVE.Components.Energy.Processes.Thrust.Thrust)SUAVE.Components.Energy.Processes.Thrust.Thrust
compute(self, conditions)SUAVE.Components.Energy.Processes.Thrust.Thrust
design_thrust (defined in SUAVE.Components.Energy.Processes.Thrust.Thrust)SUAVE.Components.Energy.Processes.Thrust.Thrust
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
mass_flow_rate_design (defined in SUAVE.Components.Energy.Processes.Thrust.Thrust)SUAVE.Components.Energy.Processes.Thrust.Thrust
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
number_of_engines (defined in SUAVE.Components.Energy.Processes.Thrust.Thrust)SUAVE.Components.Energy.Processes.Thrust.Thrust
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
reference_pressure (defined in SUAVE.Components.Energy.Processes.Thrust.Thrust)SUAVE.Components.Energy.Processes.Thrust.Thrust
reference_temperature (defined in SUAVE.Components.Energy.Processes.Thrust.Thrust)SUAVE.Components.Energy.Processes.Thrust.Thrust
size(self, conditions)SUAVE.Components.Energy.Processes.Thrust.Thrust
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Energy.Processes.Thrust.Thrust)SUAVE.Components.Energy.Processes.Thrust.Thrust
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Thrust_1_1Thrust.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Thrust_1_1Thrust.html deleted file mode 100644 index 19933870..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Thrust_1_1Thrust.html +++ /dev/null @@ -1,373 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Components.Energy.Processes.Thrust.Thrust Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Energy.Processes.Thrust.Thrust Class Reference
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-Inheritance diagram for SUAVE.Components.Energy.Processes.Thrust.Thrust:
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- - -SUAVE.Components.Energy.Energy_Component.Energy_Component -SUAVE.Components.Physical_Component.Physical_Component -SUAVE.Components.Component.Component - -
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-Public Member Functions

def __defaults__ (self)
 
def compute (self, conditions)
 
def size (self, conditions)
 
- Public Member Functions inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
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-Public Attributes

tag
 
bypass_ratio
 
compressor_nondimensional_massflow
 
reference_temperature
 
reference_pressure
 
number_of_engines
 
design_thrust
 
mass_flow_rate_design
 
- Public Attributes inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
inputs
 
outputs
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
-

Detailed Description

-
A class that handles computation of thrust and other outputs for a gas turbine engine.
-
-Assumptions:
-Perfect gas
-
-Source:
-https://web.stanford.edu/~cantwell/AA283_Course_Material/AA283_Course_Notes/
-

Member Function Documentation

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◆ __defaults__()

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def SUAVE.Components.Energy.Processes.Thrust.Thrust.__defaults__ ( self)
-
-
This sets the default value.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
-
- -

◆ compute()

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def SUAVE.Components.Energy.Processes.Thrust.Thrust.compute ( self,
 conditions 
)
-
-
Computes thrust and other properties as below.
-
-Assumptions:
-Perfect gas
-
-Source:
-https://web.stanford.edu/~cantwell/AA283_Course_Material/AA283_Course_Notes/
-
-Inputs:
-conditions.freestream.
-  isentropic_expansion_factor        [-] (gamma)
-  specific_heat_at_constant_pressure [J/(kg K)]
-  velocity                           [m/s]
-  speed_of_sound                     [m/s]
-  mach_number                        [-]
-  pressure                           [Pa]
-  gravity                            [m/s^2]
-conditions.throttle                  [-] (.1 is 10%)
-self.inputs.
-  fuel_to_air_ratio                  [-]
-  total_temperature_reference        [K]
-  total_pressure_reference           [Pa]
-  core_nozzle.
-    velocity                         [m/s]
-    static_pressure                  [Pa]
-    area_ratio                       [-]
-  fan_nozzle.
-    velocity                         [m/s]
-    static_pressure                  [Pa]
-    area_ratio                       [-]
-  number_of_engines                  [-]
-  bypass_ratio                       [-]
-  flow_through_core                  [-] percentage of total flow (.1 is 10%)
-  flow_through_fan                   [-] percentage of total flow (.1 is 10%)
-
-Outputs:
-self.outputs.
-  thrust                             [N]
-  thrust_specific_fuel_consumption   [N/N-s]
-  non_dimensional_thrust             [-]
-  core_mass_flow_rate                [kg/s]
-  fuel_flow_rate                     [kg/s]
-  power                              [W]
-
-Properties Used:
-self.
-  reference_temperature              [K]
-  reference_pressure                 [Pa]
-  compressor_nondimensional_massflow [-]
-
-
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◆ size()

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def SUAVE.Components.Energy.Processes.Thrust.Thrust.size ( self,
 conditions 
)
-
-
Sizes the core flow for the design condition.
-
-Assumptions:
-Perfect gas
-
-Source:
-https://web.stanford.edu/~cantwell/AA283_Course_Material/AA283_Course_Notes/
-
-Inputs:
-conditions.freestream.speed_of_sound [m/s] (conditions is also passed to self.compute(..))
-self.inputs.
-  bypass_ratio                       [-]
-  total_temperature_reference        [K]
-  total_pressure_reference           [Pa]
-  number_of_engines                  [-]
-
-Outputs:
-self.outputs.non_dimensional_thrust  [-]
-
-Properties Used:
-self.
-  reference_temperature              [K]
-  reference_pressure                 [Pa]
-  total_design                       [N] - Design thrust
-
-
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The documentation for this class was generated from the following file:
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  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Energy/Processes/Thrust.py
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Thrust_1_1Thrust.js b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Thrust_1_1Thrust.js deleted file mode 100644 index f57121e2..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Thrust_1_1Thrust.js +++ /dev/null @@ -1,14 +0,0 @@ -var classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Thrust_1_1Thrust = -[ - [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Thrust_1_1Thrust.html#a4a6b965d0e738d3cd7cf259b2157dfd3", null ], - [ "compute", "classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Thrust_1_1Thrust.html#a65285d08cd9bf97245c4b0933e23b9d2", null ], - [ "size", "classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Thrust_1_1Thrust.html#ae63d108105b0578e786f51d8799eb8c2", null ], - [ "bypass_ratio", "classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Thrust_1_1Thrust.html#a57203285c31d0d5df7fbb063ef566b29", null ], - [ "compressor_nondimensional_massflow", "classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Thrust_1_1Thrust.html#a1be464918920af147d428173a68853e7", null ], - [ "design_thrust", "classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Thrust_1_1Thrust.html#a0a2b78e1b59fe6be7c860c1b7972af56", null ], - [ "mass_flow_rate_design", "classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Thrust_1_1Thrust.html#a406d35e6a371cf0cfc346b253ec55563", null ], - [ "number_of_engines", "classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Thrust_1_1Thrust.html#aa048c9f61b35a2ea1b903e53d9d43a99", null ], - [ "reference_pressure", "classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Thrust_1_1Thrust.html#aa96a8f8bc7798801e719bf41f7d495d4", null ], - [ "reference_temperature", "classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Thrust_1_1Thrust.html#a6d23c79620a073c073109e0dfe4d0c69", null ], - [ "tag", "classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Thrust_1_1Thrust.html#a1dd2cf24444b3f094c0fce37fc000ac9", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Thrust_1_1Thrust.png b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Thrust_1_1Thrust.png deleted file mode 100644 index 131a7850..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Thrust_1_1Thrust.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery-members.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery-members.html deleted file mode 100644 index a0d6c232..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery-members.html +++ /dev/null @@ -1,128 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Energy.Storages.Batteries.Battery.Battery Member List
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This is the complete list of members for SUAVE.Components.Energy.Storages.Batteries.Battery.Battery, including all inherited members.

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__defaults__(self) (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
current_energy (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
discharge_model (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
energy_calc(self, numerics) (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
energy_density (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
max_energy (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
max_power (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
max_voltage (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
ragone (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
resistance (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.html deleted file mode 100644 index 0f4c4800..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.html +++ /dev/null @@ -1,209 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Components.Energy.Storages.Batteries.Battery.Battery Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Energy.Storages.Batteries.Battery.Battery Class Reference
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-Inheritance diagram for SUAVE.Components.Energy.Storages.Batteries.Battery.Battery:
-
-
- - -SUAVE.Components.Energy.Energy_Component.Energy_Component -SUAVE.Components.Physical_Component.Physical_Component -SUAVE.Components.Component.Component -SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion -SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Sulfur.Lithium_Sulfur -SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Aluminum_Air.Aluminum_Air -SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Lithium_Air.Lithium_Air - -
- - - - - - - - - - - - - - - -

-Public Member Functions

-def __defaults__ (self)
 
-def energy_calc (self, numerics)
 
- Public Member Functions inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

energy_density
 
current_energy
 
resistance
 
max_energy
 
max_power
 
max_voltage
 
discharge_model
 
ragone
 
- Public Attributes inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
inputs
 
outputs
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
-

Detailed Description

-
Energy Component object that stores energy. Contains values
-used to indicate its discharge characterics, including a model
-that calculates discharge losses
-

The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Energy/Storages/Batteries/Battery.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.js b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.js deleted file mode 100644 index 90cadf61..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.js +++ /dev/null @@ -1,13 +0,0 @@ -var classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery = -[ - [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.html#a529cffa04fba4664bd432349f14fe268", null ], - [ "energy_calc", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.html#aa65c7a1b8d7ff1b54685851fb8d8f2cd", null ], - [ "current_energy", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.html#ab75d672bb965c5aec6968c38e1fec34e", null ], - [ "discharge_model", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.html#ac1e376177175252082d5b465a7915f7a", null ], - [ "energy_density", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.html#af6ab54f2a19d11ce4b6362a21610c96c", null ], - [ "max_energy", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.html#a26fea5041ae1d5bb54a6a816420191a8", null ], - [ "max_power", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.html#a216ae6ac99fb528716599d14c64a1888", null ], - [ "max_voltage", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.html#af34d6af1003c3d903a9eef49f1a7f368", null ], - [ "ragone", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.html#acfe3bfad30bd53b5c4608a7660606832", null ], - [ "resistance", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.html#a53d46e3ffe1570d23a4423005dd608a9", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.png b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.png deleted file mode 100644 index d7fc26c8..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Constant__Mass_1_1Lithium__Ion_1_1Lithium__Ion-members.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Constant__Mass_1_1Lithium__Ion_1_1Lithium__Ion-members.html deleted file mode 100644 index 7ffa4757..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Constant__Mass_1_1Lithium__Ion_1_1Lithium__Ion-members.html +++ /dev/null @@ -1,130 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion Member List
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This is the complete list of members for SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion, including all inherited members.

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__defaults__(self) (defined in SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion
current_energy (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
discharge_model (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
energy_calc(self, numerics) (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
energy_density (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
max_energy (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
max_power (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
max_voltage (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
ragone (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
resistance (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
specific_energy (defined in SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion
specific_power (defined in SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Constant__Mass_1_1Lithium__Ion_1_1Lithium__Ion.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Constant__Mass_1_1Lithium__Ion_1_1Lithium__Ion.html deleted file mode 100644 index d176f725..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Constant__Mass_1_1Lithium__Ion_1_1Lithium__Ion.html +++ /dev/null @@ -1,216 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion Class Reference - - - - - - - - - - - - - - - -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion Class Reference
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-Inheritance diagram for SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion:
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- - -SUAVE.Components.Energy.Storages.Batteries.Battery.Battery -SUAVE.Components.Energy.Energy_Component.Energy_Component -SUAVE.Components.Physical_Component.Physical_Component -SUAVE.Components.Component.Component - -
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-Public Member Functions

-def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
-def __defaults__ (self)
 
-def energy_calc (self, numerics)
 
- Public Member Functions inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
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-Public Attributes

specific_energy
 
specific_power
 
- Public Attributes inherited from SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
energy_density
 
current_energy
 
resistance
 
max_energy
 
max_power
 
max_voltage
 
discharge_model
 
ragone
 
- Public Attributes inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
inputs
 
outputs
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
-

Detailed Description

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Specifies discharge/specific energy characteristics specific tobytes
-lithium-ion batteries
-

The documentation for this class was generated from the following file:
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  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Energy/Storages/Batteries/Constant_Mass/Lithium_Ion.py
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Constant__Mass_1_1Lithium__Ion_1_1Lithium__Ion.js b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Constant__Mass_1_1Lithium__Ion_1_1Lithium__Ion.js deleted file mode 100644 index 7d33ecf8..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Constant__Mass_1_1Lithium__Ion_1_1Lithium__Ion.js +++ /dev/null @@ -1,6 +0,0 @@ -var classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Constant__Mass_1_1Lithium__Ion_1_1Lithium__Ion = -[ - [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Constant__Mass_1_1Lithium__Ion_1_1Lithium__Ion.html#ae795b271329eaaf29ac6601954531bfc", null ], - [ "specific_energy", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Constant__Mass_1_1Lithium__Ion_1_1Lithium__Ion.html#a69a0d26fe86cdc7258bf96f2e70aef73", null ], - [ "specific_power", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Constant__Mass_1_1Lithium__Ion_1_1Lithium__Ion.html#a59313342cb39243bb18a9c4db03f5f11", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Constant__Mass_1_1Lithium__Ion_1_1Lithium__Ion.png b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Constant__Mass_1_1Lithium__Ion_1_1Lithium__Ion.png deleted file mode 100644 index cd4f7e8e..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Constant__Mass_1_1Lithium__Ion_1_1Lithium__Ion.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Constant__Mass_1_1Lithium__Sulfur_1_1Lithium__Sulfur-members.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Constant__Mass_1_1Lithium__Sulfur_1_1Lithium__Sulfur-members.html deleted file mode 100644 index 9f8cb893..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Constant__Mass_1_1Lithium__Sulfur_1_1Lithium__Sulfur-members.html +++ /dev/null @@ -1,130 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Sulfur.Lithium_Sulfur Member List
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This is the complete list of members for SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Sulfur.Lithium_Sulfur, including all inherited members.

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__defaults__(self) (defined in SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Sulfur.Lithium_Sulfur)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Sulfur.Lithium_Sulfur
current_energy (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
discharge_model (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
energy_calc(self, numerics) (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
energy_density (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
max_energy (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
max_power (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
max_voltage (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
ragone (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
resistance (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
specific_energy (defined in SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Sulfur.Lithium_Sulfur)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Sulfur.Lithium_Sulfur
specific_power (defined in SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Sulfur.Lithium_Sulfur)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Sulfur.Lithium_Sulfur
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Constant__Mass_1_1Lithium__Sulfur_1_1Lithium__Sulfur.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Constant__Mass_1_1Lithium__Sulfur_1_1Lithium__Sulfur.html deleted file mode 100644 index 3dc4ea23..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Constant__Mass_1_1Lithium__Sulfur_1_1Lithium__Sulfur.html +++ /dev/null @@ -1,216 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Sulfur.Lithium_Sulfur Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Sulfur.Lithium_Sulfur Class Reference
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-Inheritance diagram for SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Sulfur.Lithium_Sulfur:
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- - -SUAVE.Components.Energy.Storages.Batteries.Battery.Battery -SUAVE.Components.Energy.Energy_Component.Energy_Component -SUAVE.Components.Physical_Component.Physical_Component -SUAVE.Components.Component.Component - -
- - - - - - - - - - - - - - - - - - -

-Public Member Functions

-def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
-def __defaults__ (self)
 
-def energy_calc (self, numerics)
 
- Public Member Functions inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
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-Public Attributes

specific_energy
 
specific_power
 
- Public Attributes inherited from SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
energy_density
 
current_energy
 
resistance
 
max_energy
 
max_power
 
max_voltage
 
discharge_model
 
ragone
 
- Public Attributes inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
inputs
 
outputs
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
-

Detailed Description

-
Specifies discharge/specific energy characteristics specific to
-lithium-ion batteries
-

The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Energy/Storages/Batteries/Constant_Mass/Lithium_Sulfur.py
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Constant__Mass_1_1Lithium__Sulfur_1_1Lithium__Sulfur.js b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Constant__Mass_1_1Lithium__Sulfur_1_1Lithium__Sulfur.js deleted file mode 100644 index d58ebb2c..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Constant__Mass_1_1Lithium__Sulfur_1_1Lithium__Sulfur.js +++ /dev/null @@ -1,6 +0,0 @@ -var classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Constant__Mass_1_1Lithium__Sulfur_1_1Lithium__Sulfur = -[ - [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Constant__Mass_1_1Lithium__Sulfur_1_1Lithium__Sulfur.html#a379ba3c396d7a65ce7b8a02251a824f2", null ], - [ "specific_energy", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Constant__Mass_1_1Lithium__Sulfur_1_1Lithium__Sulfur.html#ae47ff0eae461618101c7e10358b5f3f6", null ], - [ "specific_power", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Constant__Mass_1_1Lithium__Sulfur_1_1Lithium__Sulfur.html#a11b840e1979e226f5fe1911cb20acf34", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Constant__Mass_1_1Lithium__Sulfur_1_1Lithium__Sulfur.png b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Constant__Mass_1_1Lithium__Sulfur_1_1Lithium__Sulfur.png deleted file mode 100644 index ff4aa026..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Constant__Mass_1_1Lithium__Sulfur_1_1Lithium__Sulfur.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Variable__Mass_1_1Aluminum__Air_1_1Aluminum__Air-members.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Variable__Mass_1_1Aluminum__Air_1_1Aluminum__Air-members.html deleted file mode 100644 index ca6e2a58..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Variable__Mass_1_1Aluminum__Air_1_1Aluminum__Air-members.html +++ /dev/null @@ -1,135 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Aluminum_Air.Aluminum_Air Member List
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This is the complete list of members for SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Aluminum_Air.Aluminum_Air, including all inherited members.

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__defaults__(self) (defined in SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Aluminum_Air.Aluminum_Air)SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Aluminum_Air.Aluminum_Air
aluminum_mass_factor (defined in SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Aluminum_Air.Aluminum_Air)SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Aluminum_Air.Aluminum_Air
current_energy (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
discharge_model (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
energy_calc(self, numerics) (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
energy_density (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
find_aluminum_mass(self, energy) (defined in SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Aluminum_Air.Aluminum_Air)SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Aluminum_Air.Aluminum_Air
find_water_mass(self, energy) (defined in SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Aluminum_Air.Aluminum_Air)SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Aluminum_Air.Aluminum_Air
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
mass_gain_factor (defined in SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Aluminum_Air.Aluminum_Air)SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Aluminum_Air.Aluminum_Air
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
max_energy (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
max_power (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
max_voltage (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
ragone (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
resistance (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
specific_energy (defined in SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Aluminum_Air.Aluminum_Air)SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Aluminum_Air.Aluminum_Air
specific_power (defined in SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Aluminum_Air.Aluminum_Air)SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Aluminum_Air.Aluminum_Air
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
water_mass_gain_factor (defined in SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Aluminum_Air.Aluminum_Air)SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Aluminum_Air.Aluminum_Air
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Variable__Mass_1_1Aluminum__Air_1_1Aluminum__Air.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Variable__Mass_1_1Aluminum__Air_1_1Aluminum__Air.html deleted file mode 100644 index 91091ea3..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Variable__Mass_1_1Aluminum__Air_1_1Aluminum__Air.html +++ /dev/null @@ -1,232 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Aluminum_Air.Aluminum_Air Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Aluminum_Air.Aluminum_Air Class Reference
-
-
-
-Inheritance diagram for SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Aluminum_Air.Aluminum_Air:
-
-
- - -SUAVE.Components.Energy.Storages.Batteries.Battery.Battery -SUAVE.Components.Energy.Energy_Component.Energy_Component -SUAVE.Components.Physical_Component.Physical_Component -SUAVE.Components.Component.Component - -
- - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

-def __defaults__ (self)
 
-def find_water_mass (self, energy)
 
-def find_aluminum_mass (self, energy)
 
- Public Member Functions inherited from SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
-def __defaults__ (self)
 
-def energy_calc (self, numerics)
 
- Public Member Functions inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

specific_energy
 
specific_power
 
mass_gain_factor
 
water_mass_gain_factor
 
aluminum_mass_factor
 
- Public Attributes inherited from SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
energy_density
 
current_energy
 
resistance
 
max_energy
 
max_power
 
max_voltage
 
discharge_model
 
ragone
 
- Public Attributes inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
inputs
 
outputs
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
-

Detailed Description

-
Specifies discharge/specific energy characteristics specific to
-aluminum-air batteries. Also includes parameters related to 
-consumption of aluminum, oxygen, and water
-

The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Energy/Storages/Batteries/Variable_Mass/Aluminum_Air.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Variable__Mass_1_1Aluminum__Air_1_1Aluminum__Air.js b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Variable__Mass_1_1Aluminum__Air_1_1Aluminum__Air.js deleted file mode 100644 index 9c0cf4a0..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Variable__Mass_1_1Aluminum__Air_1_1Aluminum__Air.js +++ /dev/null @@ -1,11 +0,0 @@ -var classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Variable__Mass_1_1Aluminum__Air_1_1Aluminum__Air = -[ - [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Variable__Mass_1_1Aluminum__Air_1_1Aluminum__Air.html#a67b26c73d23d3a45a85d210f1e7787c7", null ], - [ "find_aluminum_mass", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Variable__Mass_1_1Aluminum__Air_1_1Aluminum__Air.html#a75a314d72d1a267e9dc68156b80154fb", null ], - [ "find_water_mass", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Variable__Mass_1_1Aluminum__Air_1_1Aluminum__Air.html#ab9dc2fcecd7cf01ab408169816a739e7", null ], - [ "aluminum_mass_factor", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Variable__Mass_1_1Aluminum__Air_1_1Aluminum__Air.html#a1db53177baf8ba8774eb3272342ce7da", null ], - [ "mass_gain_factor", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Variable__Mass_1_1Aluminum__Air_1_1Aluminum__Air.html#aa5bcfff381331da45e98ebdbf5423dae", null ], - [ "specific_energy", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Variable__Mass_1_1Aluminum__Air_1_1Aluminum__Air.html#a67a1687b9151ffa4a6e1ad7c88a782fb", null ], - [ "specific_power", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Variable__Mass_1_1Aluminum__Air_1_1Aluminum__Air.html#a79f580d6edc454032aadfb11c9437383", null ], - [ "water_mass_gain_factor", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Variable__Mass_1_1Aluminum__Air_1_1Aluminum__Air.html#ac720e8d3593bf98d16606c9e33058d4f", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Variable__Mass_1_1Aluminum__Air_1_1Aluminum__Air.png b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Variable__Mass_1_1Aluminum__Air_1_1Aluminum__Air.png deleted file mode 100644 index 5961e402..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Variable__Mass_1_1Aluminum__Air_1_1Aluminum__Air.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Variable__Mass_1_1Lithium__Air_1_1Lithium__Air-members.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Variable__Mass_1_1Lithium__Air_1_1Lithium__Air-members.html deleted file mode 100644 index 3bf1261c..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Variable__Mass_1_1Lithium__Air_1_1Lithium__Air-members.html +++ /dev/null @@ -1,131 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Lithium_Air.Lithium_Air Member List
-
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- -

This is the complete list of members for SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Lithium_Air.Lithium_Air, including all inherited members.

- - - - - - - - - - - - - - - - - - - - -
__defaults__(self) (defined in SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Lithium_Air.Lithium_Air)SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Lithium_Air.Lithium_Air
current_energy (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
discharge_model (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
energy_calc(self, numerics) (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
energy_density (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
mass_gain_factor (defined in SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Lithium_Air.Lithium_Air)SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Lithium_Air.Lithium_Air
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
max_energy (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
max_power (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
max_voltage (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
ragone (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
resistance (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
specific_energy (defined in SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Lithium_Air.Lithium_Air)SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Lithium_Air.Lithium_Air
specific_power (defined in SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Lithium_Air.Lithium_Air)SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Lithium_Air.Lithium_Air
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Variable__Mass_1_1Lithium__Air_1_1Lithium__Air.html b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Variable__Mass_1_1Lithium__Air_1_1Lithium__Air.html deleted file mode 100644 index ae10b20c..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Variable__Mass_1_1Lithium__Air_1_1Lithium__Air.html +++ /dev/null @@ -1,220 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Lithium_Air.Lithium_Air Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Lithium_Air.Lithium_Air Class Reference
-
-
-
-Inheritance diagram for SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Lithium_Air.Lithium_Air:
-
-
- - -SUAVE.Components.Energy.Storages.Batteries.Battery.Battery -SUAVE.Components.Energy.Energy_Component.Energy_Component -SUAVE.Components.Physical_Component.Physical_Component -SUAVE.Components.Component.Component - -
- - - - - - - - - - - - - - - - - - -

-Public Member Functions

-def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
-def __defaults__ (self)
 
-def energy_calc (self, numerics)
 
- Public Member Functions inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

specific_energy
 
specific_power
 
mass_gain_factor
 
- Public Attributes inherited from SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
energy_density
 
current_energy
 
resistance
 
max_energy
 
max_power
 
max_voltage
 
discharge_model
 
ragone
 
- Public Attributes inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
inputs
 
outputs
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
-

Detailed Description

-
Specifies specific energy characteristics specific to
-lithium-air batteries. Also includes parameters related to 
-consumption of oxygen
-

The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Energy/Storages/Batteries/Variable_Mass/Lithium_Air.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Variable__Mass_1_1Lithium__Air_1_1Lithium__Air.js b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Variable__Mass_1_1Lithium__Air_1_1Lithium__Air.js deleted file mode 100644 index b634836e..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Variable__Mass_1_1Lithium__Air_1_1Lithium__Air.js +++ /dev/null @@ -1,7 +0,0 @@ -var classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Variable__Mass_1_1Lithium__Air_1_1Lithium__Air = -[ - [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Variable__Mass_1_1Lithium__Air_1_1Lithium__Air.html#a9e54953c1f3e45bf2d88d7b68535b541", null ], - [ "mass_gain_factor", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Variable__Mass_1_1Lithium__Air_1_1Lithium__Air.html#a6c703c31f3458e7c1df82605ddc0ff84", null ], - [ "specific_energy", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Variable__Mass_1_1Lithium__Air_1_1Lithium__Air.html#a72d675e0c2636493880c5355bc4de756", null ], - [ "specific_power", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Variable__Mass_1_1Lithium__Air_1_1Lithium__Air.html#a20bb563e6dc09928533965efa295385c", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Variable__Mass_1_1Lithium__Air_1_1Lithium__Air.png b/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Variable__Mass_1_1Lithium__Air_1_1Lithium__Air.png deleted file mode 100644 index 237a1ef0..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Variable__Mass_1_1Lithium__Air_1_1Lithium__Air.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Envelope_1_1Envelope-members.html b/_site/doxygen/classSUAVE_1_1Components_1_1Envelope_1_1Envelope-members.html deleted file mode 100644 index 3c1f11f4..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Envelope_1_1Envelope-members.html +++ /dev/null @@ -1,125 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Envelope.Envelope Class Reference
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-
-Inheritance diagram for SUAVE.Components.Envelope.Envelope:
-
-
- - -SUAVE.Components.Component.Component - -
- - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

tag
 
ultimate_load
 
limit_load
 
alpha_maximum
 
alt_vc
 
alt_gust
 
max_ceiling
 
maximum_dynamic_pressure
 
maximum_mach_operational
 
maneuver
 
gust
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
-

Detailed Description

-
Flight envelope for a vehicle
-
-    Assumptions:
-    None
-    
-    Source:
-    None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Components.Envelope.Envelope.__defaults__ ( self)
-
-
This sets the default values.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Envelope.py
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Envelope_1_1Envelope.js b/_site/doxygen/classSUAVE_1_1Components_1_1Envelope_1_1Envelope.js deleted file mode 100644 index d4fac5c9..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Envelope_1_1Envelope.js +++ /dev/null @@ -1,15 +0,0 @@ -var classSUAVE_1_1Components_1_1Envelope_1_1Envelope = -[ - [ "__defaults__", "classSUAVE_1_1Components_1_1Envelope_1_1Envelope.html#a97fc4349f99f5a137433ac92e92236ab", null ], - [ "alpha_maximum", "classSUAVE_1_1Components_1_1Envelope_1_1Envelope.html#a00d01b30172b34a30ae1262d94a558f2", null ], - [ "alt_gust", "classSUAVE_1_1Components_1_1Envelope_1_1Envelope.html#afdcb698837c07f80a6cf7765701cb30c", null ], - [ "alt_vc", "classSUAVE_1_1Components_1_1Envelope_1_1Envelope.html#a9fa1d524f7072f9d99a79b7a4960e59f", null ], - [ "gust", "classSUAVE_1_1Components_1_1Envelope_1_1Envelope.html#a817cbf39aeec6758432ee3eab3f4b882", null ], - [ "limit_load", "classSUAVE_1_1Components_1_1Envelope_1_1Envelope.html#ad9653f50cbbd9323878da353fe49e6fe", null ], - [ "maneuver", "classSUAVE_1_1Components_1_1Envelope_1_1Envelope.html#a49d434a90895935ad7a89d77db9f763e", null ], - [ "max_ceiling", "classSUAVE_1_1Components_1_1Envelope_1_1Envelope.html#a3d0278765533a69d81e74c9da73d6677", null ], - [ "maximum_dynamic_pressure", "classSUAVE_1_1Components_1_1Envelope_1_1Envelope.html#a510c802653d940134add99ab206a186c", null ], - [ "maximum_mach_operational", "classSUAVE_1_1Components_1_1Envelope_1_1Envelope.html#a0b9fb595ec7118bb22d8766d0b6ba633", null ], - [ "tag", "classSUAVE_1_1Components_1_1Envelope_1_1Envelope.html#a37803830ce866776eb6ab122d597a183", null ], - [ "ultimate_load", "classSUAVE_1_1Components_1_1Envelope_1_1Envelope.html#a802e08bf22970bc80c6ea4390dd7c135", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Envelope_1_1Envelope.png b/_site/doxygen/classSUAVE_1_1Components_1_1Envelope_1_1Envelope.png deleted file mode 100644 index 776bd617..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Envelope_1_1Envelope.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Container-members.html b/_site/doxygen/classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Container-members.html deleted file mode 100644 index 3bcb074b..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Container-members.html +++ /dev/null @@ -1,114 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Fuselages.Fuselage.Container Member List
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SUAVE.Components.Fuselages.Fuselage.Container Class Reference
-
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-Inheritance diagram for SUAVE.Components.Fuselages.Fuselage.Container:
-
-
- - -SUAVE.Components.Physical_Component.Container -SUAVE.Components.Component.Container - -
- - - - - - - -

-Static Public Attributes

Container
 
- Static Public Attributes inherited from SUAVE.Components.Component.Container
Container
 
- - - - -

-Additional Inherited Members

- Public Member Functions inherited from SUAVE.Components.Physical_Component.Container
def sum_mass (self)
 
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Fuselages/Fuselage.py
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Fuselages.Fuselage.Fuselage Member List
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This is the complete list of members for SUAVE.Components.Fuselages.Fuselage.Fuselage, including all inherited members.

- - - - - - - - - - - - - - - - - - - - - - -
__defaults__(self)SUAVE.Components.Fuselages.Fuselage.Fuselage
aerodynamic_center (defined in SUAVE.Components.Fuselages.Fuselage.Fuselage)SUAVE.Components.Fuselages.Fuselage.Fuselage
aft_centerbody_area (defined in SUAVE.Components.Fuselages.Fuselage.Fuselage)SUAVE.Components.Fuselages.Fuselage.Fuselage
aft_centerbody_taper (defined in SUAVE.Components.Fuselages.Fuselage.Fuselage)SUAVE.Components.Fuselages.Fuselage.Fuselage
areas (defined in SUAVE.Components.Fuselages.Fuselage.Fuselage)SUAVE.Components.Fuselages.Fuselage.Fuselage
cabin_area (defined in SUAVE.Components.Fuselages.Fuselage.Fuselage)SUAVE.Components.Fuselages.Fuselage.Fuselage
differential_pressure (defined in SUAVE.Components.Fuselages.Fuselage.Fuselage)SUAVE.Components.Fuselages.Fuselage.Fuselage
effective_diameter (defined in SUAVE.Components.Fuselages.Fuselage.Fuselage)SUAVE.Components.Fuselages.Fuselage.Fuselage
fineness (defined in SUAVE.Components.Fuselages.Fuselage.Fuselage)SUAVE.Components.Fuselages.Fuselage.Fuselage
heights (defined in SUAVE.Components.Fuselages.Fuselage.Fuselage)SUAVE.Components.Fuselages.Fuselage.Fuselage
lengths (defined in SUAVE.Components.Fuselages.Fuselage.Fuselage)SUAVE.Components.Fuselages.Fuselage.Fuselage
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
number_coach_seats (defined in SUAVE.Components.Fuselages.Fuselage.Fuselage)SUAVE.Components.Fuselages.Fuselage.Fuselage
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
seat_pitch (defined in SUAVE.Components.Fuselages.Fuselage.Fuselage)SUAVE.Components.Fuselages.Fuselage.Fuselage
seats_abreast (defined in SUAVE.Components.Fuselages.Fuselage.Fuselage)SUAVE.Components.Fuselages.Fuselage.Fuselage
Sections (defined in SUAVE.Components.Fuselages.Fuselage.Fuselage)SUAVE.Components.Fuselages.Fuselage.Fuselage
Segments (defined in SUAVE.Components.Fuselages.Fuselage.Fuselage)SUAVE.Components.Fuselages.Fuselage.Fuselage
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Fuselages.Fuselage.Fuselage)SUAVE.Components.Fuselages.Fuselage.Fuselage
width (defined in SUAVE.Components.Fuselages.Fuselage.Fuselage)SUAVE.Components.Fuselages.Fuselage.Fuselage
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html b/_site/doxygen/classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html deleted file mode 100644 index 52515f94..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html +++ /dev/null @@ -1,270 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Components.Fuselages.Fuselage.Fuselage Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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SUAVE.Components.Fuselages.Fuselage.Fuselage Class Reference
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-Inheritance diagram for SUAVE.Components.Fuselages.Fuselage.Fuselage:
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- - -SUAVE.Components.Lofted_Body.Lofted_Body -SUAVE.Components.Physical_Component.Physical_Component -SUAVE.Components.Component.Component - -
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-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Lofted_Body.Lofted_Body
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
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-Public Attributes

tag
 
aerodynamic_center
 
Sections
 
Segments
 
number_coach_seats
 
seats_abreast
 
seat_pitch
 
areas
 
effective_diameter
 
width
 
heights
 
lengths
 
fineness
 
differential_pressure
 
aft_centerbody_area
 
aft_centerbody_taper
 
cabin_area
 
- Public Attributes inherited from SUAVE.Components.Lofted_Body.Lofted_Body
tag
 
Segments
 
Sections
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
-

Detailed Description

-
This is a standard fuselage for a tube and wing aircraft.
-
-Assumptions:
-Conventional fuselage
-
-Source:
-N/A
-

Member Function Documentation

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◆ __defaults__()

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def SUAVE.Components.Fuselages.Fuselage.Fuselage.__defaults__ ( self)
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This sets the default values for the component to function.
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-Assumptions:
-None
-    
-Source:
-N/A
-    
-Inputs:
-None
-    
-Outputs:
-None
-    
-Properties Used:
-None
-
-
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-
The documentation for this class was generated from the following file:
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  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Fuselages/Fuselage.py
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.js b/_site/doxygen/classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.js deleted file mode 100644 index b319ebbc..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.js +++ /dev/null @@ -1,21 +0,0 @@ -var classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage = -[ - [ "__defaults__", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#a13a4cd81f10d72cd1bbfbc756d69ca25", null ], - [ "aerodynamic_center", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#a804b9a97a7090359a6ba48d636714e1f", null ], - [ "aft_centerbody_area", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#ae569f01643b85dfeb3da55275897144d", null ], - [ "aft_centerbody_taper", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#a928c49bd07c05f4e278827f08b0a976f", null ], - [ "areas", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#adb36a1b713c6460a7c4e063658ca8105", null ], - [ "cabin_area", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#a388dc3a3e1a086ccc93c3d0dbfd66e11", null ], - [ "differential_pressure", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#a60e74147869ccd496f8c8185c5d07c09", null ], - [ "effective_diameter", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#a79f6884ddd6e0ca4241194b4966d8cf1", null ], - [ "fineness", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#afb50945499974ff3306d15d9715bc8f7", null ], - [ "heights", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#ae46d1a31c166bca78400a194d3ef3686", null ], - [ "lengths", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#acc972f58e4a9f7d1632271f0ed24e1df", null ], - [ "number_coach_seats", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#acc6f517eb0fdec2c551169210492af0c", null ], - [ "seat_pitch", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#ab06ac6ecf14ab5ce6b3346d05d2e284d", null ], - [ "seats_abreast", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#a779b05b88a125d4ea57d480112384c9f", null ], - [ "Sections", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#a6214ee66b1f87414bc095f9f2587ada7", null ], - [ "Segments", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#a60d47dc740536a8703505ce95da44bb3", null ], - [ "tag", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#aeb1aab02a525f21939d7b5e5b11375f3", null ], - [ "width", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#a2d18b6bcb752bfb5d39974806c0079e8", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.png b/_site/doxygen/classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.png deleted file mode 100644 index 359aa057..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Landing__Gear_1_1Landing__Gear_1_1Landing__Gear-members.html b/_site/doxygen/classSUAVE_1_1Components_1_1Landing__Gear_1_1Landing__Gear_1_1Landing__Gear-members.html deleted file mode 100644 index ba039984..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Landing__Gear_1_1Landing__Gear_1_1Landing__Gear-members.html +++ /dev/null @@ -1,117 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE.Components.Landing_Gear.Landing_Gear.Landing_Gear Class Reference
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-Inheritance diagram for SUAVE.Components.Landing_Gear.Landing_Gear.Landing_Gear:
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- - -SUAVE.Components.Physical_Component.Physical_Component -SUAVE.Components.Component.Component -SUAVE.Components.Landing_Gear.Main_Landing_Gear.Main_Landing_Gear -SUAVE.Components.Landing_Gear.Nose_Landing_Gear.Nose_Landing_Gear - -
- - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
- - - - - - - - - - - - - - - - - -

-Public Attributes

tag
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
-

Detailed Description

-
SUAVE.Components.Landing_Gear.Landing_Gear()
-    
-    The Top Landing Gear Component Class
-    
-        Assumptions:
-        None
-        
-        Source:
-        N/A

Member Function Documentation

- -

◆ __defaults__()

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def SUAVE.Components.Landing_Gear.Landing_Gear.Landing_Gear.__defaults__ ( self)
-
-
This sets the default values for the component attributes.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
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-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Landing_Gear/Landing_Gear.py
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-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Landing__Gear_1_1Landing__Gear_1_1Landing__Gear.js b/_site/doxygen/classSUAVE_1_1Components_1_1Landing__Gear_1_1Landing__Gear_1_1Landing__Gear.js deleted file mode 100644 index e3a6827f..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Landing__Gear_1_1Landing__Gear_1_1Landing__Gear.js +++ /dev/null @@ -1,5 +0,0 @@ -var classSUAVE_1_1Components_1_1Landing__Gear_1_1Landing__Gear_1_1Landing__Gear = -[ - [ "__defaults__", "classSUAVE_1_1Components_1_1Landing__Gear_1_1Landing__Gear_1_1Landing__Gear.html#a5b545fccc3b0b5f05e8e3008d5c5a8cf", null ], - [ "tag", "classSUAVE_1_1Components_1_1Landing__Gear_1_1Landing__Gear_1_1Landing__Gear.html#aed0f1965909ce50ae9e3e79c4c802fd0", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Landing__Gear_1_1Landing__Gear_1_1Landing__Gear.png b/_site/doxygen/classSUAVE_1_1Components_1_1Landing__Gear_1_1Landing__Gear_1_1Landing__Gear.png deleted file mode 100644 index 9482d513..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Landing__Gear_1_1Landing__Gear_1_1Landing__Gear.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Landing__Gear_1_1Main__Landing__Gear_1_1Main__Landing__Gear-members.html b/_site/doxygen/classSUAVE_1_1Components_1_1Landing__Gear_1_1Main__Landing__Gear_1_1Main__Landing__Gear-members.html deleted file mode 100644 index 31d7a269..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Landing__Gear_1_1Main__Landing__Gear_1_1Main__Landing__Gear-members.html +++ /dev/null @@ -1,121 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Landing_Gear.Main_Landing_Gear.Main_Landing_Gear Class Reference
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-Inheritance diagram for SUAVE.Components.Landing_Gear.Main_Landing_Gear.Main_Landing_Gear:
-
-
- - -SUAVE.Components.Landing_Gear.Landing_Gear.Landing_Gear -SUAVE.Components.Physical_Component.Physical_Component -SUAVE.Components.Component.Component - -
- - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Landing_Gear.Landing_Gear.Landing_Gear
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

units
 
strut_length
 
tire_diameter
 
wheels
 
- Public Attributes inherited from SUAVE.Components.Landing_Gear.Landing_Gear.Landing_Gear
tag
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
-

Detailed Description

-
SUAVE.Components.Landing_Gear.Main_Landing_Gear()
-    
-    The MLG Landing Gear Component Class
-    
-        Assumptions:
-        None
-        
-        Source:
-        N/A

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Components.Landing_Gear.Main_Landing_Gear.Main_Landing_Gear.__defaults__ ( self)
-
-
This sets the default values for the component attributes.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Output:
-None
-
-Properties Used:
-N/A
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Landing_Gear/Main_Landing_Gear.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Landing__Gear_1_1Main__Landing__Gear_1_1Main__Landing__Gear.js b/_site/doxygen/classSUAVE_1_1Components_1_1Landing__Gear_1_1Main__Landing__Gear_1_1Main__Landing__Gear.js deleted file mode 100644 index 08ae7c96..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Landing__Gear_1_1Main__Landing__Gear_1_1Main__Landing__Gear.js +++ /dev/null @@ -1,8 +0,0 @@ -var classSUAVE_1_1Components_1_1Landing__Gear_1_1Main__Landing__Gear_1_1Main__Landing__Gear = -[ - [ "__defaults__", "classSUAVE_1_1Components_1_1Landing__Gear_1_1Main__Landing__Gear_1_1Main__Landing__Gear.html#a49f8c147fcead8400fbf06ba5607257c", null ], - [ "strut_length", "classSUAVE_1_1Components_1_1Landing__Gear_1_1Main__Landing__Gear_1_1Main__Landing__Gear.html#a0746446ff4e556f4bfaa8e8133269cf8", null ], - [ "tire_diameter", "classSUAVE_1_1Components_1_1Landing__Gear_1_1Main__Landing__Gear_1_1Main__Landing__Gear.html#a3fdc93cc5f4a391eeff8ce20588a422d", null ], - [ "units", "classSUAVE_1_1Components_1_1Landing__Gear_1_1Main__Landing__Gear_1_1Main__Landing__Gear.html#adf90062bd324cc58d3fa5c4165412f50", null ], - [ "wheels", "classSUAVE_1_1Components_1_1Landing__Gear_1_1Main__Landing__Gear_1_1Main__Landing__Gear.html#abcfe6aac23f12d46d7c1eaa686982d41", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Landing__Gear_1_1Main__Landing__Gear_1_1Main__Landing__Gear.png b/_site/doxygen/classSUAVE_1_1Components_1_1Landing__Gear_1_1Main__Landing__Gear_1_1Main__Landing__Gear.png deleted file mode 100644 index 301ee832..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Landing__Gear_1_1Main__Landing__Gear_1_1Main__Landing__Gear.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Landing__Gear_1_1Nose__Landing__Gear_1_1Nose__Landing__Gear-members.html b/_site/doxygen/classSUAVE_1_1Components_1_1Landing__Gear_1_1Nose__Landing__Gear_1_1Nose__Landing__Gear-members.html deleted file mode 100644 index a82cff7d..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Landing__Gear_1_1Nose__Landing__Gear_1_1Nose__Landing__Gear-members.html +++ /dev/null @@ -1,121 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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- - - - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Landing__Gear_1_1Nose__Landing__Gear_1_1Nose__Landing__Gear.html b/_site/doxygen/classSUAVE_1_1Components_1_1Landing__Gear_1_1Nose__Landing__Gear_1_1Nose__Landing__Gear.html deleted file mode 100644 index 9a44aef3..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Landing__Gear_1_1Nose__Landing__Gear_1_1Nose__Landing__Gear.html +++ /dev/null @@ -1,227 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Components.Landing_Gear.Nose_Landing_Gear.Nose_Landing_Gear Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Landing_Gear.Nose_Landing_Gear.Nose_Landing_Gear Class Reference
-
-
-
-Inheritance diagram for SUAVE.Components.Landing_Gear.Nose_Landing_Gear.Nose_Landing_Gear:
-
-
- - -SUAVE.Components.Landing_Gear.Landing_Gear.Landing_Gear -SUAVE.Components.Physical_Component.Physical_Component -SUAVE.Components.Component.Component - -
- - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Landing_Gear.Landing_Gear.Landing_Gear
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

tire_diameter
 
strut_length
 
units
 
wheels
 
- Public Attributes inherited from SUAVE.Components.Landing_Gear.Landing_Gear.Landing_Gear
tag
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
-

Detailed Description

-
SUAVE.Components.Landing_Gear.Nose_Landing_Gear()
-    
-    The NLG Landing Gear Component Class
-        
-        Assumptions:
-        None
-        
-        Source:
-        N/A        
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Components.Landing_Gear.Nose_Landing_Gear.Nose_Landing_Gear.__defaults__ ( self)
-
-
This sets the default values for the component attributes.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Output:
-None
-
-Properties Used:
-N/A
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Landing_Gear/Nose_Landing_Gear.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Landing__Gear_1_1Nose__Landing__Gear_1_1Nose__Landing__Gear.js b/_site/doxygen/classSUAVE_1_1Components_1_1Landing__Gear_1_1Nose__Landing__Gear_1_1Nose__Landing__Gear.js deleted file mode 100644 index 24071e69..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Landing__Gear_1_1Nose__Landing__Gear_1_1Nose__Landing__Gear.js +++ /dev/null @@ -1,8 +0,0 @@ -var classSUAVE_1_1Components_1_1Landing__Gear_1_1Nose__Landing__Gear_1_1Nose__Landing__Gear = -[ - [ "__defaults__", "classSUAVE_1_1Components_1_1Landing__Gear_1_1Nose__Landing__Gear_1_1Nose__Landing__Gear.html#ac5ad8f513c8037bdcafe89490ae9b771", null ], - [ "strut_length", "classSUAVE_1_1Components_1_1Landing__Gear_1_1Nose__Landing__Gear_1_1Nose__Landing__Gear.html#ab9bd2221e3bc7debc15df18403b3d039", null ], - [ "tire_diameter", "classSUAVE_1_1Components_1_1Landing__Gear_1_1Nose__Landing__Gear_1_1Nose__Landing__Gear.html#ab0f697c45997ba5b6de8021eef2850be", null ], - [ "units", "classSUAVE_1_1Components_1_1Landing__Gear_1_1Nose__Landing__Gear_1_1Nose__Landing__Gear.html#a4d7fc084dfa42ced1729cd0949e5db24", null ], - [ "wheels", "classSUAVE_1_1Components_1_1Landing__Gear_1_1Nose__Landing__Gear_1_1Nose__Landing__Gear.html#a6ba38038577df2b45650d9452cb87cda", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Landing__Gear_1_1Nose__Landing__Gear_1_1Nose__Landing__Gear.png b/_site/doxygen/classSUAVE_1_1Components_1_1Landing__Gear_1_1Nose__Landing__Gear_1_1Nose__Landing__Gear.png deleted file mode 100644 index d7600b02..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Landing__Gear_1_1Nose__Landing__Gear_1_1Nose__Landing__Gear.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Curve-members.html b/_site/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Curve-members.html deleted file mode 100644 index c422bcfb..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Curve-members.html +++ /dev/null @@ -1,116 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Lofted_Body.Curve Member List
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Curve.html b/_site/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Curve.html deleted file mode 100644 index 5d30db94..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Curve.html +++ /dev/null @@ -1,194 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Components.Lofted_Body.Curve Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Lofted_Body.Curve Class Reference
-
-
-
-Inheritance diagram for SUAVE.Components.Lofted_Body.Curve:
-
-
- - -SUAVE.Components.Component.Component - -
- - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
- - - - - - - - - - -

-Public Attributes

tag
 
points
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
-

Detailed Description

-
A class that stubs out what a curve is
-
-Assumptions:
-None
-
-Source:
-None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Components.Lofted_Body.Curve.__defaults__ ( self)
-
-
This sets the default values.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Lofted_Body.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Curve.js b/_site/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Curve.js deleted file mode 100644 index 124b4bd2..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Curve.js +++ /dev/null @@ -1,6 +0,0 @@ -var classSUAVE_1_1Components_1_1Lofted__Body_1_1Curve = -[ - [ "__defaults__", "classSUAVE_1_1Components_1_1Lofted__Body_1_1Curve.html#a843aec6fd606521a8c2336e992438158", null ], - [ "points", "classSUAVE_1_1Components_1_1Lofted__Body_1_1Curve.html#a3f471917d7e9ebdab3b61771389ddd21", null ], - [ "tag", "classSUAVE_1_1Components_1_1Lofted__Body_1_1Curve.html#aa3d06b7633c0175e5b5020576d767c89", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Curve.png b/_site/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Curve.png deleted file mode 100644 index 8eb5fdb1..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Curve.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1CurveContainer-members.html b/_site/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1CurveContainer-members.html deleted file mode 100644 index c7134012..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1CurveContainer-members.html +++ /dev/null @@ -1,116 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Lofted_Body.CurveContainer Member List
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- -
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1CurveContainer.html b/_site/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1CurveContainer.html deleted file mode 100644 index 447b605f..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1CurveContainer.html +++ /dev/null @@ -1,153 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Components.Lofted_Body.CurveContainer Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Lofted_Body.CurveContainer Class Reference
-
-
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-Inheritance diagram for SUAVE.Components.Lofted_Body.CurveContainer:
-
-
- - -SUAVE.Components.Component.Container - -
- - - - - - - - - - - - - -

-Static Public Attributes

Curve
 
Container
 
Section
 
Segment
 
- Static Public Attributes inherited from SUAVE.Components.Component.Container
Container
 
-

Detailed Description

-
This does nothing
-
-Assumptions:
-None
-
-Source:
-None
-

The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Lofted_Body.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1CurveContainer.png b/_site/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1CurveContainer.png deleted file mode 100644 index e23cea6c..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1CurveContainer.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Lofted__Body-members.html b/_site/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Lofted__Body-members.html deleted file mode 100644 index 954a2c42..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Lofted__Body-members.html +++ /dev/null @@ -1,119 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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- - - - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Lofted__Body.html b/_site/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Lofted__Body.html deleted file mode 100644 index 744e6453..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Lofted__Body.html +++ /dev/null @@ -1,212 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Components.Lofted_Body.Lofted_Body Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Lofted_Body.Lofted_Body Class Reference
-
-
-
-Inheritance diagram for SUAVE.Components.Lofted_Body.Lofted_Body:
-
-
- - -SUAVE.Components.Physical_Component.Physical_Component -SUAVE.Components.Component.Component -SUAVE.Components.Fuselages.Fuselage.Fuselage -SUAVE.Components.Wings.Control_Surface.Control_Surface -SUAVE.Components.Wings.Wing.Wing -SUAVE.Components.Wings.Horizontal_Tail.Horizontal_Tail -SUAVE.Components.Wings.Main_Wing.Main_Wing -SUAVE.Components.Wings.Vertical_Tail.Vertical_Tail - -
- - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
- - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

tag
 
Segments
 
Sections
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Components.Lofted_Body.Lofted_Body.__defaults__ ( self)
-
-
This sets the default values.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Lofted_Body.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Lofted__Body.js b/_site/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Lofted__Body.js deleted file mode 100644 index 07cc6449..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Lofted__Body.js +++ /dev/null @@ -1,7 +0,0 @@ -var classSUAVE_1_1Components_1_1Lofted__Body_1_1Lofted__Body = -[ - [ "__defaults__", "classSUAVE_1_1Components_1_1Lofted__Body_1_1Lofted__Body.html#a9a41b92aeca26b01f43527677f0f715a", null ], - [ "Sections", "classSUAVE_1_1Components_1_1Lofted__Body_1_1Lofted__Body.html#a436ac8f3ad1b562b09051693377b70df", null ], - [ "Segments", "classSUAVE_1_1Components_1_1Lofted__Body_1_1Lofted__Body.html#ad997a3fd0531a8c08fe66cd427b27391", null ], - [ "tag", "classSUAVE_1_1Components_1_1Lofted__Body_1_1Lofted__Body.html#a9be10450331f26faa3e4f6e222e12ee1", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Lofted__Body.png b/_site/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Lofted__Body.png deleted file mode 100644 index 89aacd2c..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Lofted__Body.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Section-members.html b/_site/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Section-members.html deleted file mode 100644 index 3f307f5e..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Section-members.html +++ /dev/null @@ -1,118 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
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SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Lofted_Body.Section Class Reference
-
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-
-Inheritance diagram for SUAVE.Components.Lofted_Body.Section:
-
-
- - -SUAVE.Components.Component.Component -SUAVE.Components.Wings.Airfoils.Airfoil.Airfoil -SUAVE.Components.Wings.Control_Surface.Control_Surface_Section - -
- - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
- - - - - - - - - - - - - - -

-Public Attributes

tag
 
Curves
 
prev
 
next
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
-

Detailed Description

-
A class that stubs out what a section is
-
-Assumptions:
-None
-
-Source:
-None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Components.Lofted_Body.Section.__defaults__ ( self)
-
-
This sets the default values.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Lofted_Body.py
  • -
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Section.js b/_site/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Section.js deleted file mode 100644 index 02aaa64c..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Section.js +++ /dev/null @@ -1,8 +0,0 @@ -var classSUAVE_1_1Components_1_1Lofted__Body_1_1Section = -[ - [ "__defaults__", "classSUAVE_1_1Components_1_1Lofted__Body_1_1Section.html#a18e362879f7fe5a3c64d9320eff94a07", null ], - [ "Curves", "classSUAVE_1_1Components_1_1Lofted__Body_1_1Section.html#a5fea20dce1b6cebb2ea0bde9f41d7393", null ], - [ "next", "classSUAVE_1_1Components_1_1Lofted__Body_1_1Section.html#afc04bc14b1deba0e6a9a3b7e2a7f1973", null ], - [ "prev", "classSUAVE_1_1Components_1_1Lofted__Body_1_1Section.html#a4a00ad1e29432ac6ff0a0b7a30f8e3eb", null ], - [ "tag", "classSUAVE_1_1Components_1_1Lofted__Body_1_1Section.html#adcd5d2ed1bb07f1fe5cd326c10341d85", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Section.png b/_site/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Section.png deleted file mode 100644 index 2d5246ad..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Section.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1SectionContainer-members.html b/_site/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1SectionContainer-members.html deleted file mode 100644 index 8513b331..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1SectionContainer-members.html +++ /dev/null @@ -1,113 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Lofted_Body.SectionContainer Member List
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This is the complete list of members for SUAVE.Components.Lofted_Body.SectionContainer, including all inherited members.

- - -
Container (defined in SUAVE.Components.Component.Container)SUAVE.Components.Component.Containerstatic
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1SectionContainer.html b/_site/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1SectionContainer.html deleted file mode 100644 index a35cf153..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1SectionContainer.html +++ /dev/null @@ -1,140 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Components.Lofted_Body.SectionContainer Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Lofted_Body.SectionContainer Class Reference
-
-
-
-Inheritance diagram for SUAVE.Components.Lofted_Body.SectionContainer:
-
-
- - -SUAVE.Components.Component.Container - -
- - - - - -

-Additional Inherited Members

- Static Public Attributes inherited from SUAVE.Components.Component.Container
Container
 
-

Detailed Description

-
This does nothing
-
-Assumptions:
-None
-
-Source:
-None
-

The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Lofted_Body.py
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1SectionContainer.png b/_site/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1SectionContainer.png deleted file mode 100644 index 60e0d669..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1SectionContainer.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Segment-members.html b/_site/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Segment-members.html deleted file mode 100644 index 38271d84..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Segment-members.html +++ /dev/null @@ -1,117 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Lofted_Body.Segment Member List
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Segment.html b/_site/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Segment.html deleted file mode 100644 index a39e651a..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Segment.html +++ /dev/null @@ -1,198 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Components.Lofted_Body.Segment Class Reference - - - - - - - - - - - - - - - -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Lofted_Body.Segment Class Reference
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-Inheritance diagram for SUAVE.Components.Lofted_Body.Segment:
-
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- - -SUAVE.Components.Component.Component -SUAVE.Components.Wings.Segment.Segment - -
- - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
- - - - - - - - - - - - -

-Public Attributes

tag
 
prev
 
next
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
-

Detailed Description

-
A class that stubs out what a segment is
-
-Assumptions:
-None
-
-Source:
-None
-

Member Function Documentation

- -

◆ __defaults__()

- -
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- - - - - - - - -
def SUAVE.Components.Lofted_Body.Segment.__defaults__ ( self)
-
-
This sets the default values.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Lofted_Body.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Segment.js b/_site/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Segment.js deleted file mode 100644 index 4453ae8f..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Segment.js +++ /dev/null @@ -1,7 +0,0 @@ -var classSUAVE_1_1Components_1_1Lofted__Body_1_1Segment = -[ - [ "__defaults__", "classSUAVE_1_1Components_1_1Lofted__Body_1_1Segment.html#ac5436a7b509fbcd08121af7ea5d5efe9", null ], - [ "next", "classSUAVE_1_1Components_1_1Lofted__Body_1_1Segment.html#a512e5a377fce4ebd8a395822d77fcea0", null ], - [ "prev", "classSUAVE_1_1Components_1_1Lofted__Body_1_1Segment.html#a163ef44a63095e7250091b2ae230032d", null ], - [ "tag", "classSUAVE_1_1Components_1_1Lofted__Body_1_1Segment.html#acf1b4d5f1c7eebb7b34f534899df4b01", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Segment.png b/_site/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Segment.png deleted file mode 100644 index eec13d3e..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Segment.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Mass__Properties_1_1Mass__Properties-members.html b/_site/doxygen/classSUAVE_1_1Components_1_1Mass__Properties_1_1Mass__Properties-members.html deleted file mode 100644 index 6d98bc74..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Mass__Properties_1_1Mass__Properties-members.html +++ /dev/null @@ -1,117 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Mass_Properties.Mass_Properties Class Reference
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-Inheritance diagram for SUAVE.Components.Mass_Properties.Mass_Properties:
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- - -SUAVE.Vehicle.Vehicle_Mass_Properties - -
- - - - -

-Public Member Functions

def __defaults__ (self)
 
- - - - - - - - - -

-Public Attributes

mass
 
volume
 
center_of_gravity
 
moments_of_inertia
 
-

Detailed Description

-
Mass properties for a physical component
-    
-    Assumptions:
-    None
-    
-    Source:
-    None
-

Member Function Documentation

- -

◆ __defaults__()

- -
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def SUAVE.Components.Mass_Properties.Mass_Properties.__defaults__ ( self)
-
-
This sets the default values.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Mass_Properties.py
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Mass__Properties_1_1Mass__Properties.js b/_site/doxygen/classSUAVE_1_1Components_1_1Mass__Properties_1_1Mass__Properties.js deleted file mode 100644 index 795f1ac3..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Mass__Properties_1_1Mass__Properties.js +++ /dev/null @@ -1,8 +0,0 @@ -var classSUAVE_1_1Components_1_1Mass__Properties_1_1Mass__Properties = -[ - [ "__defaults__", "classSUAVE_1_1Components_1_1Mass__Properties_1_1Mass__Properties.html#ac9cfb57a83a0c203a8d0c99b5b5202c2", null ], - [ "center_of_gravity", "classSUAVE_1_1Components_1_1Mass__Properties_1_1Mass__Properties.html#a466525e75a39a1e738884a13296c29d1", null ], - [ "mass", "classSUAVE_1_1Components_1_1Mass__Properties_1_1Mass__Properties.html#a571091a7c9a2cf736b18bc1422bb62a9", null ], - [ "moments_of_inertia", "classSUAVE_1_1Components_1_1Mass__Properties_1_1Mass__Properties.html#a1014834c653dd1ba8f8896d7eb61572b", null ], - [ "volume", "classSUAVE_1_1Components_1_1Mass__Properties_1_1Mass__Properties.html#a601be236f7556d57dcf017a002a60895", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Mass__Properties_1_1Mass__Properties.png b/_site/doxygen/classSUAVE_1_1Components_1_1Mass__Properties_1_1Mass__Properties.png deleted file mode 100644 index b734ddea..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Mass__Properties_1_1Mass__Properties.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Cargo_1_1Cargo-members.html b/_site/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Cargo_1_1Cargo-members.html deleted file mode 100644 index 0cd5efd6..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Cargo_1_1Cargo-members.html +++ /dev/null @@ -1,117 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Payloads.Cargo.Cargo Class Reference
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-Inheritance diagram for SUAVE.Components.Payloads.Cargo.Cargo:
-
-
- - -SUAVE.Components.Payloads.Payload.Payload -SUAVE.Components.Physical_Component.Physical_Component -SUAVE.Components.Component.Component - -
- - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Payloads.Payload.Payload
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
- - - - - - - - - - - - - - - - - - - - -

-Public Attributes

tag
 
- Public Attributes inherited from SUAVE.Components.Payloads.Payload.Payload
tag
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
-

Detailed Description

-
A class representing cargo.
-
-Assumptions:
-None
-
-Source:
-N/A
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Components.Payloads.Cargo.Cargo.__defaults__ ( self)
-
-
This sets the default tag for cargo.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Payloads/Cargo.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Cargo_1_1Cargo.js b/_site/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Cargo_1_1Cargo.js deleted file mode 100644 index 4c2661cb..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Cargo_1_1Cargo.js +++ /dev/null @@ -1,5 +0,0 @@ -var classSUAVE_1_1Components_1_1Payloads_1_1Cargo_1_1Cargo = -[ - [ "__defaults__", "classSUAVE_1_1Components_1_1Payloads_1_1Cargo_1_1Cargo.html#a4f97de17ea1ae1c4e6e68e3a6307952e", null ], - [ "tag", "classSUAVE_1_1Components_1_1Payloads_1_1Cargo_1_1Cargo.html#a0113edcfd4ad704eed565e3201d5a5fb", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Cargo_1_1Cargo.png b/_site/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Cargo_1_1Cargo.png deleted file mode 100644 index 0e20a305..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Cargo_1_1Cargo.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Payload_1_1Container-members.html b/_site/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Payload_1_1Container-members.html deleted file mode 100644 index da1fc359..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Payload_1_1Container-members.html +++ /dev/null @@ -1,114 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Payloads.Payload.Container Member List
-
-
- -

This is the complete list of members for SUAVE.Components.Payloads.Payload.Container, including all inherited members.

- - - -
Container (defined in SUAVE.Components.Payloads.Payload.Container)SUAVE.Components.Payloads.Payload.Containerstatic
sum_mass(self)SUAVE.Components.Physical_Component.Container
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Payload_1_1Container.html b/_site/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Payload_1_1Container.html deleted file mode 100644 index 3ae281c3..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Payload_1_1Container.html +++ /dev/null @@ -1,151 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Components.Payloads.Payload.Container Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Payloads.Payload.Container Class Reference
-
-
-
-Inheritance diagram for SUAVE.Components.Payloads.Payload.Container:
-
-
- - -SUAVE.Components.Physical_Component.Container -SUAVE.Components.Component.Container - -
- - - - - - - -

-Static Public Attributes

Container
 
- Static Public Attributes inherited from SUAVE.Components.Component.Container
Container
 
- - - - -

-Additional Inherited Members

- Public Member Functions inherited from SUAVE.Components.Physical_Component.Container
def sum_mass (self)
 
-

Detailed Description

-
The container used for payloads. No additional functionality.
-
-Assumptions:
-None
-
-Source:
-N/A
-

The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Payloads/Payload.py
  • -
-
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Payload_1_1Container.png b/_site/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Payload_1_1Container.png deleted file mode 100644 index f9b08cfc..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Payload_1_1Container.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Payload_1_1Payload-members.html b/_site/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Payload_1_1Payload-members.html deleted file mode 100644 index 595f181c..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Payload_1_1Payload-members.html +++ /dev/null @@ -1,117 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Payloads.Payload.Payload Class Reference
-
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-Inheritance diagram for SUAVE.Components.Payloads.Payload.Payload:
-
-
- - -SUAVE.Components.Physical_Component.Physical_Component -SUAVE.Components.Component.Component -SUAVE.Components.Payloads.Cargo.Cargo -SUAVE.Components.Payloads.Person.Person -SUAVE.Components.Payloads.Satellite.Satellite - -
- - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
- - - - - - - - - - - - - - - - - -

-Public Attributes

tag
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
-

Detailed Description

-
A class representing a payload.
-
-Assumptions:
-None
-
-Source:
-N/A
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Components.Payloads.Payload.Payload.__defaults__ ( self)
-
-
This sets the default tag for a payload.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Payloads/Payload.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Payload_1_1Payload.js b/_site/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Payload_1_1Payload.js deleted file mode 100644 index 8f3bbd97..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Payload_1_1Payload.js +++ /dev/null @@ -1,5 +0,0 @@ -var classSUAVE_1_1Components_1_1Payloads_1_1Payload_1_1Payload = -[ - [ "__defaults__", "classSUAVE_1_1Components_1_1Payloads_1_1Payload_1_1Payload.html#a8ab675e813585c3036cfeffcbd976f33", null ], - [ "tag", "classSUAVE_1_1Components_1_1Payloads_1_1Payload_1_1Payload.html#aa90c294700820fd00984a65f0da3417a", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Payload_1_1Payload.png b/_site/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Payload_1_1Payload.png deleted file mode 100644 index 92f742d8..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Payload_1_1Payload.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Person_1_1Person-members.html b/_site/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Person_1_1Person-members.html deleted file mode 100644 index b8e55e56..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Person_1_1Person-members.html +++ /dev/null @@ -1,117 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
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- - - -
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- - - - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Person_1_1Person.html b/_site/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Person_1_1Person.html deleted file mode 100644 index e8e484f6..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Person_1_1Person.html +++ /dev/null @@ -1,216 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Components.Payloads.Person.Person Class Reference - - - - - - - - - - - - - - - -
-
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Payloads.Person.Person Class Reference
-
-
-
-Inheritance diagram for SUAVE.Components.Payloads.Person.Person:
-
-
- - -SUAVE.Components.Payloads.Payload.Payload -SUAVE.Components.Physical_Component.Physical_Component -SUAVE.Components.Component.Component - -
- - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Payloads.Payload.Payload
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
- - - - - - - - - - - - - - - - - - - - -

-Public Attributes

tag
 
- Public Attributes inherited from SUAVE.Components.Payloads.Payload.Payload
tag
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
-

Detailed Description

-
A class representing a person.
-
-Assumptions:
-None
-
-Source:
-N/A
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Components.Payloads.Person.Person.__defaults__ ( self)
-
-
This sets the default values for a person.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Payloads/Person.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Person_1_1Person.js b/_site/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Person_1_1Person.js deleted file mode 100644 index 1ff52699..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Person_1_1Person.js +++ /dev/null @@ -1,5 +0,0 @@ -var classSUAVE_1_1Components_1_1Payloads_1_1Person_1_1Person = -[ - [ "__defaults__", "classSUAVE_1_1Components_1_1Payloads_1_1Person_1_1Person.html#a057b4069cf1182ae815f9ac23828a483", null ], - [ "tag", "classSUAVE_1_1Components_1_1Payloads_1_1Person_1_1Person.html#a8a256ceea2c9695987a0760609a2fd3a", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Person_1_1Person.png b/_site/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Person_1_1Person.png deleted file mode 100644 index dae4c78c..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Person_1_1Person.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Satellite_1_1Satellite-members.html b/_site/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Satellite_1_1Satellite-members.html deleted file mode 100644 index f8fec3b9..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Satellite_1_1Satellite-members.html +++ /dev/null @@ -1,117 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
-
- - - -
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- -
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-
- - - - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Satellite_1_1Satellite.html b/_site/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Satellite_1_1Satellite.html deleted file mode 100644 index eb66e63f..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Satellite_1_1Satellite.html +++ /dev/null @@ -1,216 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Components.Payloads.Satellite.Satellite Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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- -
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- -
- -
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-
SUAVE.Components.Payloads.Satellite.Satellite Class Reference
-
-
-
-Inheritance diagram for SUAVE.Components.Payloads.Satellite.Satellite:
-
-
- - -SUAVE.Components.Payloads.Payload.Payload -SUAVE.Components.Physical_Component.Physical_Component -SUAVE.Components.Component.Component - -
- - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Payloads.Payload.Payload
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
- - - - - - - - - - - - - - - - - - - - -

-Public Attributes

tag
 
- Public Attributes inherited from SUAVE.Components.Payloads.Payload.Payload
tag
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
-

Detailed Description

-
A class representing a satellite.
-
-Assumptions:
-None
-
-Source:
-N/A
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Components.Payloads.Satellite.Satellite.__defaults__ ( self)
-
-
This sets the default tag for a satellite.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Payloads/Satellite.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Satellite_1_1Satellite.js b/_site/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Satellite_1_1Satellite.js deleted file mode 100644 index 98406b48..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Satellite_1_1Satellite.js +++ /dev/null @@ -1,5 +0,0 @@ -var classSUAVE_1_1Components_1_1Payloads_1_1Satellite_1_1Satellite = -[ - [ "__defaults__", "classSUAVE_1_1Components_1_1Payloads_1_1Satellite_1_1Satellite.html#a0dd0be04f50f34e19e8c5130a4d38956", null ], - [ "tag", "classSUAVE_1_1Components_1_1Payloads_1_1Satellite_1_1Satellite.html#a11c080c0b8112d73fe2eb41668bf5809", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Satellite_1_1Satellite.png b/_site/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Satellite_1_1Satellite.png deleted file mode 100644 index 5d3a5456..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Satellite_1_1Satellite.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Physical__Component_1_1Container-members.html b/_site/doxygen/classSUAVE_1_1Components_1_1Physical__Component_1_1Container-members.html deleted file mode 100644 index dd39bbb4..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Physical__Component_1_1Container-members.html +++ /dev/null @@ -1,114 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Physical_Component.Container Member List
-
-
- -

This is the complete list of members for SUAVE.Components.Physical_Component.Container, including all inherited members.

- - - -
Container (defined in SUAVE.Components.Component.Container)SUAVE.Components.Component.Containerstatic
sum_mass(self)SUAVE.Components.Physical_Component.Container
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Physical__Component_1_1Container.html b/_site/doxygen/classSUAVE_1_1Components_1_1Physical__Component_1_1Container.html deleted file mode 100644 index aab4175c..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Physical__Component_1_1Container.html +++ /dev/null @@ -1,186 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Components.Physical_Component.Container Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
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SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
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- - - - - - -
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-
- - - -
-
- -
-
-
- -
- -
-
- - -
- -
- -
- -
-
SUAVE.Components.Physical_Component.Container Class Reference
-
-
-
-Inheritance diagram for SUAVE.Components.Physical_Component.Container:
-
-
- - -SUAVE.Components.Component.Container -SUAVE.Components.Energy.Energy.ComponentContainer -SUAVE.Components.Fuselages.Fuselage.Container -SUAVE.Components.Payloads.Payload.Container -SUAVE.Components.Propulsors.Propulsor.Container - -
- - - - -

-Public Member Functions

def sum_mass (self)
 
- - - - -

-Additional Inherited Members

- Static Public Attributes inherited from SUAVE.Components.Component.Container
Container
 
-

Detailed Description

-
A container of physical components
-    
-    Assumptions:
-    None
-    
-    Source:
-    None
-

Member Function Documentation

- -

◆ sum_mass()

- -
-
- - - - - - - - -
def SUAVE.Components.Physical_Component.Container.sum_mass ( self)
-
-
will recursively search the data tree and sum
-    any Comp.Mass_Properties.mass, and return the total sum
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Physical_Component.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Physical__Component_1_1Container.js b/_site/doxygen/classSUAVE_1_1Components_1_1Physical__Component_1_1Container.js deleted file mode 100644 index 0d9c75f7..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Physical__Component_1_1Container.js +++ /dev/null @@ -1,4 +0,0 @@ -var classSUAVE_1_1Components_1_1Physical__Component_1_1Container = -[ - [ "sum_mass", "classSUAVE_1_1Components_1_1Physical__Component_1_1Container.html#ae51f620275537cac1c60ba136c68735e", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Physical__Component_1_1Container.png b/_site/doxygen/classSUAVE_1_1Components_1_1Physical__Component_1_1Container.png deleted file mode 100644 index 764c7e63..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Physical__Component_1_1Container.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Physical__Component_1_1Physical__Component-members.html b/_site/doxygen/classSUAVE_1_1Components_1_1Physical__Component_1_1Physical__Component-members.html deleted file mode 100644 index 26b29aba..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Physical__Component_1_1Physical__Component-members.html +++ /dev/null @@ -1,117 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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- - - - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Physical__Component_1_1Physical__Component.html b/_site/doxygen/classSUAVE_1_1Components_1_1Physical__Component_1_1Physical__Component.html deleted file mode 100644 index a85bd10b..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Physical__Component_1_1Physical__Component.html +++ /dev/null @@ -1,249 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Components.Physical_Component.Physical_Component Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Physical_Component.Physical_Component Class Reference
-
-
-
-Inheritance diagram for SUAVE.Components.Physical_Component.Physical_Component:
-
-
- - -SUAVE.Components.Component.Component -SUAVE.Components.Energy.Energy.Component -SUAVE.Components.Energy.Energy.Energy -SUAVE.Components.Energy.Energy_Component.Energy_Component -SUAVE.Components.Landing_Gear.Landing_Gear.Landing_Gear -SUAVE.Components.Lofted_Body.Lofted_Body -SUAVE.Components.Payloads.Payload.Payload -SUAVE.Components.Propulsors.Propulsor.Propulsor -SUAVE.Components.Energy.Converters.Combustor.Combustor -SUAVE.Components.Energy.Converters.Compression_Nozzle.Compression_Nozzle -SUAVE.Components.Energy.Converters.Compressor.Compressor -SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle -SUAVE.Components.Energy.Converters.Fan.Fan -SUAVE.Components.Energy.Converters.Fuel_Cell.Fuel_Cell -SUAVE.Components.Energy.Converters.Gearbox.Gearbox -SUAVE.Components.Energy.Converters.Motor.Motor -SUAVE.Components.Energy.Converters.Motor_Lo_Fid.Motor_Lo_Fid -SUAVE.Components.Energy.Converters.Propeller.Propeller -SUAVE.Components.Energy.Converters.Propeller_Lo_Fid.Propeller_Lo_Fid -SUAVE.Components.Energy.Converters.Ram.Ram -SUAVE.Components.Energy.Converters.Shaft_Power_Off_Take.Shaft_Power_Off_Take -SUAVE.Components.Energy.Converters.Solar_Panel.Solar_Panel -SUAVE.Components.Energy.Converters.Supersonic_Nozzle.Supersonic_Nozzle -SUAVE.Components.Energy.Converters.Turbine.Turbine -SUAVE.Components.Energy.Distributors.Electronic_Speed_Controller.Electronic_Speed_Controller -SUAVE.Components.Energy.Distributors.Solar_Logic.Solar_Logic -SUAVE.Components.Energy.Peripherals.Avionics.Avionics -SUAVE.Components.Energy.Peripherals.Payload.Payload -SUAVE.Components.Energy.Processes.Solar_Radiation.Solar_Radiation -SUAVE.Components.Energy.Processes.Thrust.Thrust -SUAVE.Components.Energy.Storages.Batteries.Battery.Battery -SUAVE.Components.Landing_Gear.Main_Landing_Gear.Main_Landing_Gear -SUAVE.Components.Landing_Gear.Nose_Landing_Gear.Nose_Landing_Gear -SUAVE.Components.Fuselages.Fuselage.Fuselage -SUAVE.Components.Wings.Control_Surface.Control_Surface -SUAVE.Components.Wings.Wing.Wing -SUAVE.Components.Payloads.Cargo.Cargo -SUAVE.Components.Payloads.Person.Person -SUAVE.Components.Payloads.Satellite.Satellite -SUAVE.Components.Energy.Networks.Battery_Ducted_Fan.Battery_Ducted_Fan -SUAVE.Components.Energy.Networks.Battery_Ducted_Fan_Parallel_Hybrid.Battery_Ducted_Fan_Parallel_Hybrid -SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller -SUAVE.Components.Energy.Networks.Dual_Battery_Ducted_Fan.Dual_Battery_Ducted_Fan -SUAVE.Components.Energy.Networks.Ducted_Fan.Ducted_Fan -SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward -SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate -SUAVE.Components.Energy.Networks.Solar.Solar -SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity -SUAVE.Components.Energy.Networks.Turbofan.Turbofan -SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super - -
- - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
- - - - - - - - - - - - - - -

-Public Attributes

tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
-

Detailed Description

-
A component that has a Mass_Properties Data
-    
-    Assumptions:
-    None
-    
-    Source:
-    None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Components.Physical_Component.Physical_Component.__defaults__ ( self)
-
-
This sets the default values.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Physical_Component.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Physical__Component_1_1Physical__Component.js b/_site/doxygen/classSUAVE_1_1Components_1_1Physical__Component_1_1Physical__Component.js deleted file mode 100644 index d3b24f11..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Physical__Component_1_1Physical__Component.js +++ /dev/null @@ -1,8 +0,0 @@ -var classSUAVE_1_1Components_1_1Physical__Component_1_1Physical__Component = -[ - [ "__defaults__", "classSUAVE_1_1Components_1_1Physical__Component_1_1Physical__Component.html#a3106f384175b0db34f6189d699dcd158", null ], - [ "mass_properties", "classSUAVE_1_1Components_1_1Physical__Component_1_1Physical__Component.html#ab1924562e5ca2455dd716d184e518f71", null ], - [ "origin", "classSUAVE_1_1Components_1_1Physical__Component_1_1Physical__Component.html#a1aff33ef99efa2fd64d9226210a036db", null ], - [ "symmetric", "classSUAVE_1_1Components_1_1Physical__Component_1_1Physical__Component.html#a758e782a149c79c487fd88da24d9fe6d", null ], - [ "tag", "classSUAVE_1_1Components_1_1Physical__Component_1_1Physical__Component.html#a262d78a38d51f7f484f930155843edff", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Physical__Component_1_1Physical__Component.png b/_site/doxygen/classSUAVE_1_1Components_1_1Physical__Component_1_1Physical__Component.png deleted file mode 100644 index 55282b5e..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Physical__Component_1_1Physical__Component.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Container-members.html b/_site/doxygen/classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Container-members.html deleted file mode 100644 index cfc27e7f..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Container-members.html +++ /dev/null @@ -1,115 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Propulsors.Propulsor.Container Member List
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Propulsors.Propulsor.Container Class Reference
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-Inheritance diagram for SUAVE.Components.Propulsors.Propulsor.Container:
-
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- - -SUAVE.Components.Physical_Component.Container -SUAVE.Components.Component.Container - -
- - - - - - - -

-Public Member Functions

def evaluate_thrust (self, state)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Container
def sum_mass (self)
 
- - - - -

-Additional Inherited Members

- Static Public Attributes inherited from SUAVE.Components.Component.Container
Container
 
-

Detailed Description

-
SUAVE.Components.Propulsor.Container()
-    
-    The Propulsor Container Class
-
-        Assumptions:
-        None
-        
-        Source:
-        N/A

Member Function Documentation

- -

◆ evaluate_thrust()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Components.Propulsors.Propulsor.Container.evaluate_thrust ( self,
 state 
)
-
-
This is used to evaluate the thrust produced by the propulsor.
-
-Assumptions:
-Propulsor has "evaluate_thrust" method
-
-Source:
-N/A
-
-Inputs:
-State variables
-
-Outputs:
-Results of the "evaluate_thrust" method
-
-Properties Used:
-N/A
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Propulsors/Propulsor.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Container.js b/_site/doxygen/classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Container.js deleted file mode 100644 index 5fb1f3ec..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Container.js +++ /dev/null @@ -1,4 +0,0 @@ -var classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Container = -[ - [ "evaluate_thrust", "classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Container.html#a42e24eef8ee7108c8f99379060824724", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Container.png b/_site/doxygen/classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Container.png deleted file mode 100644 index 80648b18..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Container.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Propulsor-members.html b/_site/doxygen/classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Propulsor-members.html deleted file mode 100644 index 8104ad46..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Propulsor-members.html +++ /dev/null @@ -1,117 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Propulsors.Propulsor.Propulsor Class Reference
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-Inheritance diagram for SUAVE.Components.Propulsors.Propulsor.Propulsor:
-
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- - -SUAVE.Components.Physical_Component.Physical_Component -SUAVE.Components.Component.Component -SUAVE.Components.Energy.Networks.Battery_Ducted_Fan.Battery_Ducted_Fan -SUAVE.Components.Energy.Networks.Battery_Ducted_Fan_Parallel_Hybrid.Battery_Ducted_Fan_Parallel_Hybrid -SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller -SUAVE.Components.Energy.Networks.Dual_Battery_Ducted_Fan.Dual_Battery_Ducted_Fan -SUAVE.Components.Energy.Networks.Ducted_Fan.Ducted_Fan -SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward -SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate -SUAVE.Components.Energy.Networks.Solar.Solar -SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity -SUAVE.Components.Energy.Networks.Turbofan.Turbofan -SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super - -
- - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
- - - - - - - - - - - - - - - - - -

-Public Attributes

tag
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
-

Detailed Description

-
SUAVE.Components.Propulsor()
-
-    The Top Level Propulsor Class
-        
-        Assumptions:
-        None
-        
-        Source:
-        N/As

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Components.Propulsors.Propulsor.Propulsor.__defaults__ ( self)
-
-
This sets the default attributes for the propulsor.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Propulsors/Propulsor.py
  • -
-
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Propulsor.js b/_site/doxygen/classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Propulsor.js deleted file mode 100644 index b46c5843..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Propulsor.js +++ /dev/null @@ -1,5 +0,0 @@ -var classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Propulsor = -[ - [ "__defaults__", "classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Propulsor.html#a1a13b12fb63990dcd51c6ecc46c83f21", null ], - [ "tag", "classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Propulsor.html#a297d16d03533b9da160be9d970073588", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Propulsor.png b/_site/doxygen/classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Propulsor.png deleted file mode 100644 index ccf944e5..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Propulsor.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Systems_1_1System_1_1Container-members.html b/_site/doxygen/classSUAVE_1_1Components_1_1Systems_1_1System_1_1Container-members.html deleted file mode 100644 index f0868e8a..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Systems_1_1System_1_1Container-members.html +++ /dev/null @@ -1,113 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE.Components.Systems.System.Container Member List
-
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- -

This is the complete list of members for SUAVE.Components.Systems.System.Container, including all inherited members.

- - -
Container (defined in SUAVE.Components.Systems.System.Container)SUAVE.Components.Systems.System.Containerstatic
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Systems_1_1System_1_1Container.html b/_site/doxygen/classSUAVE_1_1Components_1_1Systems_1_1System_1_1Container.html deleted file mode 100644 index 25ed45db..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Systems_1_1System_1_1Container.html +++ /dev/null @@ -1,146 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Components.Systems.System.Container Class Reference - - - - - - - - - - - - - - - -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Systems.System.Container Class Reference
-
-
-
-Inheritance diagram for SUAVE.Components.Systems.System.Container:
-
-
- - -SUAVE.Components.Component.Container - -
- - - - - - - -

-Static Public Attributes

Container
 
- Static Public Attributes inherited from SUAVE.Components.Component.Container
Container
 
-

Detailed Description

-
SUAVE.Components.Systems.Container()
-
-    The Systems Container Class
-    
-        Assumptions:
-        None
-        
-        Source:
-        N/A
-

The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Systems/System.py
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Systems.System.System Class Reference
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-Inheritance diagram for SUAVE.Components.Systems.System.System:
-
-
- - -SUAVE.Components.Component.Component - -
- - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
- - - - - - - - - - - - - - - - -

-Public Attributes

tag
 
mass_properties
 
position
 
control
 
accessories
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
-

Detailed Description

-
SUAVE.Components.Systems.System()
-
-    The Top Level System Class
-    
-        Assumptions:
-        None
-        
-        Source:
-        N/A
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Components.Systems.System.System.__defaults__ ( self)
-
-
This sets the default values for the system.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Systems/System.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Systems_1_1System_1_1System.js b/_site/doxygen/classSUAVE_1_1Components_1_1Systems_1_1System_1_1System.js deleted file mode 100644 index ee63ae2c..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Systems_1_1System_1_1System.js +++ /dev/null @@ -1,9 +0,0 @@ -var classSUAVE_1_1Components_1_1Systems_1_1System_1_1System = -[ - [ "__defaults__", "classSUAVE_1_1Components_1_1Systems_1_1System_1_1System.html#afc1811095781c3b874ab279c8449b53a", null ], - [ "accessories", "classSUAVE_1_1Components_1_1Systems_1_1System_1_1System.html#a22ad3a5dc4d33c9c53a2d01897173e99", null ], - [ "control", "classSUAVE_1_1Components_1_1Systems_1_1System_1_1System.html#adb487ae49fd4892c42ef0cd2ffdd9530", null ], - [ "mass_properties", "classSUAVE_1_1Components_1_1Systems_1_1System_1_1System.html#ac257d2d78c0da7c92ddd9cf16256bfe5", null ], - [ "position", "classSUAVE_1_1Components_1_1Systems_1_1System_1_1System.html#ae3836f93b6ac5c6bab29ec4074b8ff38", null ], - [ "tag", "classSUAVE_1_1Components_1_1Systems_1_1System_1_1System.html#a4fa86faee2bbe57bbd444c14417e1e76", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Systems_1_1System_1_1System.png b/_site/doxygen/classSUAVE_1_1Components_1_1Systems_1_1System_1_1System.png deleted file mode 100644 index b7e8e600..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Systems_1_1System_1_1System.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Airfoils_1_1Airfoil_1_1Airfoil-members.html b/_site/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Airfoils_1_1Airfoil_1_1Airfoil-members.html deleted file mode 100644 index 919f5b9d..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Airfoils_1_1Airfoil_1_1Airfoil-members.html +++ /dev/null @@ -1,122 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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- - - - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Airfoils_1_1Airfoil_1_1Airfoil.html b/_site/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Airfoils_1_1Airfoil_1_1Airfoil.html deleted file mode 100644 index d8685696..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Airfoils_1_1Airfoil_1_1Airfoil.html +++ /dev/null @@ -1,245 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Components.Wings.Airfoils.Airfoil.Airfoil Class Reference - - - - - - - - - - - - - - - -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Wings.Airfoils.Airfoil.Airfoil Class Reference
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-
-Inheritance diagram for SUAVE.Components.Wings.Airfoils.Airfoil.Airfoil:
-
-
- - -SUAVE.Components.Lofted_Body.Section -SUAVE.Components.Component.Component - -
- - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def import_airfoil_dat (self)
 
- Public Member Functions inherited from SUAVE.Components.Lofted_Body.Section
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
- - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

tag
 
thickness_to_chord
 
coordinate_file
 
points
 
- Public Attributes inherited from SUAVE.Components.Lofted_Body.Section
tag
 
Curves
 
prev
 
next
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Components.Wings.Airfoils.Airfoil.Airfoil.__defaults__ ( self)
-
-
This sets the default values of a airfoil defined in SUAVE.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
-
- -

◆ import_airfoil_dat()

- -
-
- - - - - - - - -
def SUAVE.Components.Wings.Airfoils.Airfoil.Airfoil.import_airfoil_dat ( self)
-
-
Imports airfoil data
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Wings/Airfoils/Airfoil.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Airfoils_1_1Airfoil_1_1Airfoil.js b/_site/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Airfoils_1_1Airfoil_1_1Airfoil.js deleted file mode 100644 index 49ca67b5..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Airfoils_1_1Airfoil_1_1Airfoil.js +++ /dev/null @@ -1,9 +0,0 @@ -var classSUAVE_1_1Components_1_1Wings_1_1Airfoils_1_1Airfoil_1_1Airfoil = -[ - [ "__defaults__", "classSUAVE_1_1Components_1_1Wings_1_1Airfoils_1_1Airfoil_1_1Airfoil.html#aebc33642fbd2cee33d7238535c4ed955", null ], - [ "import_airfoil_dat", "classSUAVE_1_1Components_1_1Wings_1_1Airfoils_1_1Airfoil_1_1Airfoil.html#a2fa4f8f73f27a56e42ae3ea2df7584a8", null ], - [ "coordinate_file", "classSUAVE_1_1Components_1_1Wings_1_1Airfoils_1_1Airfoil_1_1Airfoil.html#ad622a4ec18682cda7a5392a9a190f1e3", null ], - [ "points", "classSUAVE_1_1Components_1_1Wings_1_1Airfoils_1_1Airfoil_1_1Airfoil.html#a17ef2e1e3e857a5397db8b47044092d3", null ], - [ "tag", "classSUAVE_1_1Components_1_1Wings_1_1Airfoils_1_1Airfoil_1_1Airfoil.html#ab960bdfdc567919896007568600ce750", null ], - [ "thickness_to_chord", "classSUAVE_1_1Components_1_1Wings_1_1Airfoils_1_1Airfoil_1_1Airfoil.html#a23f121ba0dabb98693c6b5881d01a028", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Airfoils_1_1Airfoil_1_1Airfoil.png b/_site/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Airfoils_1_1Airfoil_1_1Airfoil.png deleted file mode 100644 index 659ce64f..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Airfoils_1_1Airfoil_1_1Airfoil.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surface_1_1Control__Surface-members.html b/_site/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surface_1_1Control__Surface-members.html deleted file mode 100644 index 875ecf9f..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surface_1_1Control__Surface-members.html +++ /dev/null @@ -1,126 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Wings.Control_Surface.Control_Surface Member List
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This is the complete list of members for SUAVE.Components.Wings.Control_Surface.Control_Surface, including all inherited members.

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__defaults__(self)SUAVE.Components.Wings.Control_Surface.Control_Surface
append_section(self, section)SUAVE.Components.Wings.Control_Surface.Control_Surface
chord_fraction (defined in SUAVE.Components.Wings.Control_Surface.Control_Surface)SUAVE.Components.Wings.Control_Surface.Control_Surface
deflection_symmetry (defined in SUAVE.Components.Wings.Control_Surface.Control_Surface)SUAVE.Components.Wings.Control_Surface.Control_Surface
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
origin (defined in SUAVE.Components.Wings.Control_Surface.Control_Surface)SUAVE.Components.Wings.Control_Surface.Control_Surface
Sections (defined in SUAVE.Components.Lofted_Body.Lofted_Body)SUAVE.Components.Lofted_Body.Lofted_Body
sections (defined in SUAVE.Components.Wings.Control_Surface.Control_Surface)SUAVE.Components.Wings.Control_Surface.Control_Surface
Segments (defined in SUAVE.Components.Lofted_Body.Lofted_Body)SUAVE.Components.Lofted_Body.Lofted_Body
span (defined in SUAVE.Components.Wings.Control_Surface.Control_Surface)SUAVE.Components.Wings.Control_Surface.Control_Surface
span_fraction (defined in SUAVE.Components.Wings.Control_Surface.Control_Surface)SUAVE.Components.Wings.Control_Surface.Control_Surface
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Wings.Control_Surface.Control_Surface)SUAVE.Components.Wings.Control_Surface.Control_Surface
transformation_matrix (defined in SUAVE.Components.Wings.Control_Surface.Control_Surface)SUAVE.Components.Wings.Control_Surface.Control_Surface
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surface_1_1Control__Surface.html b/_site/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surface_1_1Control__Surface.html deleted file mode 100644 index 65d3904b..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surface_1_1Control__Surface.html +++ /dev/null @@ -1,281 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Components.Wings.Control_Surface.Control_Surface Class Reference - - - - - - - - - - - - - - - -
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SUAVE.Components.Wings.Control_Surface.Control_Surface Class Reference
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-Inheritance diagram for SUAVE.Components.Wings.Control_Surface.Control_Surface:
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-Public Member Functions

def __defaults__ (self)
 
def append_section (self, section)
 
- Public Member Functions inherited from SUAVE.Components.Lofted_Body.Lofted_Body
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
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-Public Attributes

tag
 
span
 
span_fraction
 
chord_fraction
 
deflection_symmetry
 
origin
 
transformation_matrix
 
sections
 
- Public Attributes inherited from SUAVE.Components.Lofted_Body.Lofted_Body
tag
 
Segments
 
Sections
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
-

Member Function Documentation

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◆ __defaults__()

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def SUAVE.Components.Wings.Control_Surface.Control_Surface.__defaults__ ( self)
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This sets the default values of control surfaces defined in SUAVE.
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-Assumptions:
-None
-
-Source:
-N/A
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-Inputs:
-None
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-Outputs:
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-Properties Used:
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◆ append_section()

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def SUAVE.Components.Wings.Control_Surface.Control_Surface.append_section ( self,
 section 
)
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Adds a section
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-Assumptions:
-None
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-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
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The documentation for this class was generated from the following file:
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  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Wings/Control_Surface.py
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surface_1_1Control__Surface.js b/_site/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surface_1_1Control__Surface.js deleted file mode 100644 index fd6716ea..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surface_1_1Control__Surface.js +++ /dev/null @@ -1,13 +0,0 @@ -var classSUAVE_1_1Components_1_1Wings_1_1Control__Surface_1_1Control__Surface = -[ - [ "__defaults__", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surface_1_1Control__Surface.html#a3a781f5847d12f2774321c3ef8b2247c", null ], - [ "append_section", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surface_1_1Control__Surface.html#ac0a1c6961466410eaa6bd591ad1fca87", null ], - [ "chord_fraction", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surface_1_1Control__Surface.html#abd6a13a3747efe88025a3277287b4479", null ], - [ "deflection_symmetry", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surface_1_1Control__Surface.html#a6908765e912ce272389bda3146169344", null ], - [ "origin", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surface_1_1Control__Surface.html#a74db06d548ae7e82b4dd48054a754fbb", null ], - [ "sections", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surface_1_1Control__Surface.html#afb80fcb8c180feaf713cfedef57c2c36", null ], - [ "span", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surface_1_1Control__Surface.html#a936396e8d7bdfbcafdccdc4c39856f07", null ], - [ "span_fraction", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surface_1_1Control__Surface.html#af1eddf963b206c1a6674362635cd6599", null ], - [ "tag", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surface_1_1Control__Surface.html#a0a059df92df4d4f8128ceb506e493857", null ], - [ "transformation_matrix", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surface_1_1Control__Surface.html#a2789056b29248fdcfa03622e6b3b4543", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surface_1_1Control__Surface.png b/_site/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surface_1_1Control__Surface.png deleted file mode 100644 index e379b9ca..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surface_1_1Control__Surface.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surface_1_1Control__Surface__Section-members.html b/_site/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surface_1_1Control__Surface__Section-members.html deleted file mode 100644 index 1925e676..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surface_1_1Control__Surface__Section-members.html +++ /dev/null @@ -1,123 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE.Components.Wings.Control_Surface.Control_Surface_Section Member List
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SUAVE.Components.Wings.Control_Surface.Control_Surface_Section Class Reference
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-Inheritance diagram for SUAVE.Components.Wings.Control_Surface.Control_Surface_Section:
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-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Lofted_Body.Section
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
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-Public Attributes

tag
 
chord
 
chord_fraction
 
twist
 
origins
 
points
 
- Public Attributes inherited from SUAVE.Components.Lofted_Body.Section
tag
 
Curves
 
prev
 
next
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
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Member Function Documentation

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◆ __defaults__()

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def SUAVE.Components.Wings.Control_Surface.Control_Surface_Section.__defaults__ ( self)
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This sets the default values control surface sections defined in SUAVE.
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-Assumptions:
-None
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-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
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-Properties Used:
-N/A
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The documentation for this class was generated from the following file:
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  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Wings/Control_Surface.py
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Wings.Horizontal_Tail.Horizontal_Tail Member List
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This is the complete list of members for SUAVE.Components.Wings.Horizontal_Tail.Horizontal_Tail, including all inherited members.

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__defaults__(self)SUAVE.Components.Wings.Horizontal_Tail.Horizontal_Tail
aerodynamic_center (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
Airfoil (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
append_airfoil(self, airfoil)SUAVE.Components.Wings.Wing.Wing
append_control_surface(self, control_surface)SUAVE.Components.Wings.Wing.Wing
append_segment(self, segment)SUAVE.Components.Wings.Wing.Wing
areas (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
aspect_ratio (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
chords (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
control_surfaces (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
dihedral (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
exposed_root_chord_offset (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
flaps (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
high_lift (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
high_mach (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
mass_properties (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
position (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
Sections (defined in SUAVE.Components.Lofted_Body.Lofted_Body)SUAVE.Components.Lofted_Body.Lofted_Body
Segments (defined in SUAVE.Components.Lofted_Body.Lofted_Body)SUAVE.Components.Lofted_Body.Lofted_Body
slats (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
span_efficiency (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
spans (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
sweeps (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
symmetric (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
t_tail (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
tag (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
taper (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
thickness_to_chord (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
transition_x_lower (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
transition_x_upper (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
twists (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
vertical (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
vortex_lift (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Wings.Horizontal_Tail.Horizontal_Tail Class Reference
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-Inheritance diagram for SUAVE.Components.Wings.Horizontal_Tail.Horizontal_Tail:
-
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- - -SUAVE.Components.Wings.Wing.Wing -SUAVE.Components.Lofted_Body.Lofted_Body -SUAVE.Components.Physical_Component.Physical_Component -SUAVE.Components.Component.Component - -
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-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Wings.Wing.Wing
def __defaults__ (self)
 
def append_segment (self, segment)
 
def append_airfoil (self, airfoil)
 
def append_control_surface (self, control_surface)
 
- Public Member Functions inherited from SUAVE.Components.Lofted_Body.Lofted_Body
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Additional Inherited Members

- Public Attributes inherited from SUAVE.Components.Wings.Wing.Wing
tag
 
mass_properties
 
position
 
symmetric
 
vertical
 
t_tail
 
taper
 
dihedral
 
aspect_ratio
 
thickness_to_chord
 
span_efficiency
 
aerodynamic_center
 
exposed_root_chord_offset
 
spans
 
areas
 
chords
 
sweeps
 
twists
 
control_surfaces
 
flaps
 
slats
 
high_lift
 
high_mach
 
vortex_lift
 
transition_x_upper
 
transition_x_lower
 
Airfoil
 
- Public Attributes inherited from SUAVE.Components.Lofted_Body.Lofted_Body
tag
 
Segments
 
Sections
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
-

Detailed Description

-
This class is used to define horiontal tails SUAVE
-
-    Assumptions:
-    None
-
-    Source:
-    N/A
-
-    Inputs:
-    None
-
-    Outputs:
-    None
-
-    Properties Used:
-    N/A

Member Function Documentation

- -

◆ __defaults__()

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def SUAVE.Components.Wings.Horizontal_Tail.Horizontal_Tail.__defaults__ ( self)
-
-
This sets the default for horizontal tails in SUAVE.
-    
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Wings/Horizontal_Tail.py
  • -
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Horizontal__Tail_1_1Horizontal__Tail.js b/_site/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Horizontal__Tail_1_1Horizontal__Tail.js deleted file mode 100644 index 36a689c5..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Horizontal__Tail_1_1Horizontal__Tail.js +++ /dev/null @@ -1,4 +0,0 @@ -var classSUAVE_1_1Components_1_1Wings_1_1Horizontal__Tail_1_1Horizontal__Tail = -[ - [ "__defaults__", "classSUAVE_1_1Components_1_1Wings_1_1Horizontal__Tail_1_1Horizontal__Tail.html#a674bb83b6f89d403ae41c506caaedc1d", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Horizontal__Tail_1_1Horizontal__Tail.png b/_site/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Horizontal__Tail_1_1Horizontal__Tail.png deleted file mode 100644 index adfa3a00..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Horizontal__Tail_1_1Horizontal__Tail.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Main__Wing_1_1Main__Wing-members.html b/_site/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Main__Wing_1_1Main__Wing-members.html deleted file mode 100644 index d7b694de..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Main__Wing_1_1Main__Wing-members.html +++ /dev/null @@ -1,146 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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SUAVE.Components.Wings.Main_Wing.Main_Wing Member List
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This is the complete list of members for SUAVE.Components.Wings.Main_Wing.Main_Wing, including all inherited members.

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__defaults__(self)SUAVE.Components.Wings.Main_Wing.Main_Wing
aerodynamic_center (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
Airfoil (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
append_airfoil(self, airfoil)SUAVE.Components.Wings.Wing.Wing
append_control_surface(self, control_surface)SUAVE.Components.Wings.Wing.Wing
append_segment(self, segment)SUAVE.Components.Wings.Wing.Wing
areas (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
aspect_ratio (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
chords (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
control_surfaces (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
dihedral (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
exposed_root_chord_offset (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
flaps (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
high_lift (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
high_mach (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
mass_properties (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
position (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
Sections (defined in SUAVE.Components.Lofted_Body.Lofted_Body)SUAVE.Components.Lofted_Body.Lofted_Body
Segments (defined in SUAVE.Components.Lofted_Body.Lofted_Body)SUAVE.Components.Lofted_Body.Lofted_Body
slats (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
span_efficiency (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
spans (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
sweeps (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
symmetric (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
t_tail (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
tag (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
taper (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
thickness_to_chord (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
transition_x_lower (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
transition_x_upper (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
twists (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
vertical (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
vortex_lift (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
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SUAVE.Components.Wings.Main_Wing.Main_Wing Class Reference
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-Inheritance diagram for SUAVE.Components.Wings.Main_Wing.Main_Wing:
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def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Wings.Wing.Wing
def __defaults__ (self)
 
def append_segment (self, segment)
 
def append_airfoil (self, airfoil)
 
def append_control_surface (self, control_surface)
 
- Public Member Functions inherited from SUAVE.Components.Lofted_Body.Lofted_Body
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
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-Additional Inherited Members

- Public Attributes inherited from SUAVE.Components.Wings.Wing.Wing
tag
 
mass_properties
 
position
 
symmetric
 
vertical
 
t_tail
 
taper
 
dihedral
 
aspect_ratio
 
thickness_to_chord
 
span_efficiency
 
aerodynamic_center
 
exposed_root_chord_offset
 
spans
 
areas
 
chords
 
sweeps
 
twists
 
control_surfaces
 
flaps
 
slats
 
high_lift
 
high_mach
 
vortex_lift
 
transition_x_upper
 
transition_x_lower
 
Airfoil
 
- Public Attributes inherited from SUAVE.Components.Lofted_Body.Lofted_Body
tag
 
Segments
 
Sections
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
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tag
 
origin
 
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Detailed Description

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This class is used to define main wings SUAVE
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Member Function Documentation

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◆ __defaults__()

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def SUAVE.Components.Wings.Main_Wing.Main_Wing.__defaults__ ( self)
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This sets the default for main wings in SUAVE.
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SUAVE.Components.Wings.Segment.Segment Class Reference
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def __defaults__ (self)
 
def append_airfoil (self, airfoil)
 
- Public Member Functions inherited from SUAVE.Components.Lofted_Body.Segment
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
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tag
 
percent_span_location
 
twist
 
root_chord_percent
 
dihedral_outboard
 
sweeps
 
Airfoil
 
control_surfaces
 
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origin
 
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Member Function Documentation

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◆ __defaults__()

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def SUAVE.Components.Wings.Segment.Segment.__defaults__ ( self)
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This sets the default for wing segments in SUAVE.
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def SUAVE.Components.Wings.Segment.Segment.append_airfoil ( self,
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Adds an airfoil to the segment
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SUAVE.Components.Wings.Segment.SegmentContainer Class Reference
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Detailed Description

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Container for wing segment
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-Assumptions:
-None
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-Source:
-N/A
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-None
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-Properties Used:
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The documentation for this class was generated from the following file:
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SUAVE.Components.Wings.Vertical_Tail.Vertical_Tail Member List
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This is the complete list of members for SUAVE.Components.Wings.Vertical_Tail.Vertical_Tail, including all inherited members.

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__defaults__(self)SUAVE.Components.Wings.Vertical_Tail.Vertical_Tail
aerodynamic_center (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
Airfoil (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
append_airfoil(self, airfoil)SUAVE.Components.Wings.Wing.Wing
append_control_surface(self, control_surface)SUAVE.Components.Wings.Wing.Wing
append_segment(self, segment)SUAVE.Components.Wings.Wing.Wing
areas (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
aspect_ratio (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
chords (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
control_surfaces (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
dihedral (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
exposed_root_chord_offset (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
flaps (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
high_lift (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
high_mach (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
mass_properties (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
position (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
Sections (defined in SUAVE.Components.Lofted_Body.Lofted_Body)SUAVE.Components.Lofted_Body.Lofted_Body
Segments (defined in SUAVE.Components.Lofted_Body.Lofted_Body)SUAVE.Components.Lofted_Body.Lofted_Body
slats (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
span_efficiency (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
spans (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
sweeps (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
symmetric (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
t_tail (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
tag (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
taper (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
thickness_to_chord (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
transition_x_lower (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
transition_x_upper (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
twists (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
vertical (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
vortex_lift (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
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SUAVE.Components.Wings.Vertical_Tail.Vertical_Tail Class Reference
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-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Wings.Wing.Wing
def __defaults__ (self)
 
def append_segment (self, segment)
 
def append_airfoil (self, airfoil)
 
def append_control_surface (self, control_surface)
 
- Public Member Functions inherited from SUAVE.Components.Lofted_Body.Lofted_Body
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
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-Additional Inherited Members

- Public Attributes inherited from SUAVE.Components.Wings.Wing.Wing
tag
 
mass_properties
 
position
 
symmetric
 
vertical
 
t_tail
 
taper
 
dihedral
 
aspect_ratio
 
thickness_to_chord
 
span_efficiency
 
aerodynamic_center
 
exposed_root_chord_offset
 
spans
 
areas
 
chords
 
sweeps
 
twists
 
control_surfaces
 
flaps
 
slats
 
high_lift
 
high_mach
 
vortex_lift
 
transition_x_upper
 
transition_x_lower
 
Airfoil
 
- Public Attributes inherited from SUAVE.Components.Lofted_Body.Lofted_Body
tag
 
Segments
 
Sections
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
-

Detailed Description

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This class is used to define vertical tails SUAVE
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-Assumptions:
-None
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-Source:
-N/A
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-Inputs:
-None
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-Outputs:
-None
-
-Properties Used:
-N/A
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Components.Wings.Vertical_Tail.Vertical_Tail.__defaults__ ( self)
-
-
This sets the default for vertical tails in SUAVE.
-    
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Wings/Vertical_Tail.py
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Vertical__Tail_1_1Vertical__Tail.js b/_site/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Vertical__Tail_1_1Vertical__Tail.js deleted file mode 100644 index 37eeafea..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Vertical__Tail_1_1Vertical__Tail.js +++ /dev/null @@ -1,4 +0,0 @@ -var classSUAVE_1_1Components_1_1Wings_1_1Vertical__Tail_1_1Vertical__Tail = -[ - [ "__defaults__", "classSUAVE_1_1Components_1_1Wings_1_1Vertical__Tail_1_1Vertical__Tail.html#a140e95184807806f674ada3a7f7d783a", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Vertical__Tail_1_1Vertical__Tail.png b/_site/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Vertical__Tail_1_1Vertical__Tail.png deleted file mode 100644 index a3937a4e..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Vertical__Tail_1_1Vertical__Tail.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Container-members.html b/_site/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Container-members.html deleted file mode 100644 index 3917259e..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Container-members.html +++ /dev/null @@ -1,113 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Wings.Wing.Container Member List
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This is the complete list of members for SUAVE.Components.Wings.Wing.Container, including all inherited members.

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Container (defined in SUAVE.Components.Wings.Wing.Container)SUAVE.Components.Wings.Wing.Containerstatic
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Container.html b/_site/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Container.html deleted file mode 100644 index 0ca7de6b..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Container.html +++ /dev/null @@ -1,153 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Components.Wings.Wing.Container Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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SUAVE.Components.Wings.Wing.Container Class Reference
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-Inheritance diagram for SUAVE.Components.Wings.Wing.Container:
-
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- - -SUAVE.Components.Component.Container - -
- - - - - - - -

-Static Public Attributes

Container
 
- Static Public Attributes inherited from SUAVE.Components.Component.Container
Container
 
-

Detailed Description

-
Container for wing
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-

The documentation for this class was generated from the following file:
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  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Wings/Wing.py
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-
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Container.png b/_site/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Container.png deleted file mode 100644 index f881e6ab..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Container.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing-members.html b/_site/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing-members.html deleted file mode 100644 index 0203b58c..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing-members.html +++ /dev/null @@ -1,146 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
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SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Wings.Wing.Wing Member List
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This is the complete list of members for SUAVE.Components.Wings.Wing.Wing, including all inherited members.

- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
__defaults__(self)SUAVE.Components.Wings.Wing.Wing
aerodynamic_center (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
Airfoil (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
append_airfoil(self, airfoil)SUAVE.Components.Wings.Wing.Wing
append_control_surface(self, control_surface)SUAVE.Components.Wings.Wing.Wing
append_segment(self, segment)SUAVE.Components.Wings.Wing.Wing
areas (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
aspect_ratio (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
chords (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
control_surfaces (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
dihedral (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
exposed_root_chord_offset (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
flaps (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
high_lift (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
high_mach (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
mass_properties (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
position (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
Sections (defined in SUAVE.Components.Lofted_Body.Lofted_Body)SUAVE.Components.Lofted_Body.Lofted_Body
Segments (defined in SUAVE.Components.Lofted_Body.Lofted_Body)SUAVE.Components.Lofted_Body.Lofted_Body
slats (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
span_efficiency (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
spans (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
sweeps (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
symmetric (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
t_tail (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
tag (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
taper (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
thickness_to_chord (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
transition_x_lower (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
transition_x_upper (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
twists (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
vertical (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
vortex_lift (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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- -
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SUAVE.Components.Wings.Wing.Wing Class Reference
-
-
-
-Inheritance diagram for SUAVE.Components.Wings.Wing.Wing:
-
-
- - -SUAVE.Components.Lofted_Body.Lofted_Body -SUAVE.Components.Physical_Component.Physical_Component -SUAVE.Components.Component.Component -SUAVE.Components.Wings.Horizontal_Tail.Horizontal_Tail -SUAVE.Components.Wings.Main_Wing.Main_Wing -SUAVE.Components.Wings.Vertical_Tail.Vertical_Tail - -
- - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def append_segment (self, segment)
 
def append_airfoil (self, airfoil)
 
def append_control_surface (self, control_surface)
 
- Public Member Functions inherited from SUAVE.Components.Lofted_Body.Lofted_Body
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

tag
 
mass_properties
 
position
 
symmetric
 
vertical
 
t_tail
 
taper
 
dihedral
 
aspect_ratio
 
thickness_to_chord
 
span_efficiency
 
aerodynamic_center
 
exposed_root_chord_offset
 
spans
 
areas
 
chords
 
sweeps
 
twists
 
control_surfaces
 
flaps
 
slats
 
high_lift
 
high_mach
 
vortex_lift
 
transition_x_upper
 
transition_x_lower
 
Airfoil
 
- Public Attributes inherited from SUAVE.Components.Lofted_Body.Lofted_Body
tag
 
Segments
 
Sections
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
-

Detailed Description

-
This class defines the wing in SUAVE
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Components.Wings.Wing.Wing.__defaults__ ( self)
-
-
This sets the default values of a wing defined in SUAVE.
-    
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
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-Outputs:
-None
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-Properties Used:
-N/A
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◆ append_airfoil()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Components.Wings.Wing.Wing.append_airfoil ( self,
 airfoil 
)
-
-
Adds an airfoil to the segment 
-    
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
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-Properties Used:
-N/A
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- -

◆ append_control_surface()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Components.Wings.Wing.Wing.append_control_surface ( self,
 control_surface 
)
-
-
Adds a component to vehicle 
-    
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
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-Outputs:
-None
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-Properties Used:
-N/A
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◆ append_segment()

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def SUAVE.Components.Wings.Wing.Wing.append_segment ( self,
 segment 
)
-
-
Adds a segment to the wing 
-    
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Components/Wings/Wing.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.js b/_site/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.js deleted file mode 100644 index a8fa3a70..00000000 --- a/_site/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.js +++ /dev/null @@ -1,34 +0,0 @@ -var classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing = -[ - [ "__defaults__", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html#ab53e649ccbbc13673b6aacc081dc59dc", null ], - [ "append_airfoil", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html#aae7e3c4e26c570a1df378ae24e537713", null ], - [ "append_control_surface", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html#aadd013ca1ee42a79fdd1c5c0a1b92506", null ], - [ "append_segment", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html#a6af83046c14d3a0ef4d4d21fbd4be086", null ], - [ "aerodynamic_center", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html#a571c1dc8eb5821ad559d01dbb4574076", null ], - [ "Airfoil", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html#a4b25ac0ada709189458bd5cbf5098421", null ], - [ "areas", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html#a3286136578a7fce8b37ef16f306fcb89", null ], - [ "aspect_ratio", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html#ab405e3638ee9de58fed53bb2d9f33d3d", null ], - [ "chords", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html#a7eef52d56996afb3d5745eb608ee138b", null ], - [ "control_surfaces", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html#aafa1c4446e778b2adf84925c96c45df0", null ], - [ "dihedral", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html#a122fc4a8b8195bc82e8988eae413638c", null ], - [ "exposed_root_chord_offset", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html#aa65cca0ac4c258e0fd48d851468ec25e", null ], - [ "flaps", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html#ade2666acf39d8ab9d0f0452380432722", null ], - [ "high_lift", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html#a54b2922197121a8e144c864052addbc1", null ], - [ "high_mach", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html#a39814d7d0a9045ecc4b52a90602d2eb5", null ], - [ "mass_properties", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html#a734345ca36c535557e19cf72afb2dec3", null ], - [ "position", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html#a9dc4902e77f1210d8ff622c9cc663d3a", null ], - [ "slats", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html#a62971f29066998a4cecd60c373a5ce47", null ], - [ "span_efficiency", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html#ab9486856c8849049ee532753f2f28d34", null ], - [ "spans", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html#a9c8581500143469644736a6a346fb574", null ], - [ "sweeps", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html#a9c95d8e5232adf728ae14f240d20e37a", null ], - [ "symmetric", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html#a868aa0c0bd1e95b99eebe899c0e68c27", null ], - [ "t_tail", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html#ac02d70ef5a4c6491d94ef4ceb6bdd8a6", null ], - [ "tag", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html#a82a4410a681cbee9d280a7742d3f8f21", null ], - [ "taper", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html#ab95ccc5960b40df6a1c1cf23106be252", null ], - [ "thickness_to_chord", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html#a13a5cf4a4553b887e2686dc253f54f80", null ], - [ "transition_x_lower", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html#a7fae8d960f7f53c9c158a8b5eeacc4f0", null ], - [ "transition_x_upper", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html#ab9ac0e252a2cd2a169acf061c555059d", null ], - [ "twists", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html#a0e4556318f06695584f96db46c226211", null ], - [ "vertical", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html#ab9ad1ec9e6ded8c581c6d8df09ae9e40", null ], - [ "vortex_lift", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html#a485b7de08ab568d8945d7543809b75b0", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.png b/_site/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.png deleted file mode 100644 index 252c646b..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Core_1_1ContainerOrdered_1_1ContainerOrdered-members.html b/_site/doxygen/classSUAVE_1_1Core_1_1ContainerOrdered_1_1ContainerOrdered-members.html deleted file mode 100644 index 9cb788d8..00000000 --- a/_site/doxygen/classSUAVE_1_1Core_1_1ContainerOrdered_1_1ContainerOrdered-members.html +++ /dev/null @@ -1,144 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
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- - - -
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- -
- -
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SUAVE.Core.ContainerOrdered.ContainerOrdered Member List
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This is the complete list of members for SUAVE.Core.ContainerOrdered.ContainerOrdered, including all inherited members.

- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
__defaults__(self)SUAVE.Core.ContainerOrdered.ContainerOrdered
__delattr__(self, key)SUAVE.Core.DataOrdered.DataOrdered
__eq__(self, other)SUAVE.Core.DataOrdered.DataOrdered
__getitem__(self, k)SUAVE.Core.DataOrdered.DataOrdered
__init__(self, args, kwarg)SUAVE.Core.ContainerOrdered.ContainerOrdered
__iter__(self)SUAVE.Core.DataOrdered.DataOrdered
__iter__(self)SUAVE.Core.DataOrdered.DataOrdered
__len__(self)SUAVE.Core.DataOrdered.DataOrdered
__new__(cls, args, kwarg)SUAVE.Core.DataOrdered.DataOrdered
__reduce__(self)SUAVE.Core.DataOrdered.DataOrdered
__repr__(self)SUAVE.Core.DataOrdered.DataOrdered
__setattr__(self, key, value)SUAVE.Core.DataOrdered.DataOrdered
__setitem__(self, k, v)SUAVE.Core.DataOrdered.DataOrdered
__str__(self, indent='')SUAVE.Core.DataOrdered.DataOrdered
append(self, val)SUAVE.Core.ContainerOrdered.ContainerOrdered
SUAVE::Core::DataOrdered::DataOrdered.append(self, value, key=None)SUAVE.Core.DataOrdered.DataOrdered
clear(self)SUAVE.Core.DataOrdered.DataOrdered
dataname(self)SUAVE.Core.DataOrdered.DataOrdered
deep_get(self, keys)SUAVE.Core.DataOrdered.DataOrdered
deep_set(self, keys, val)SUAVE.Core.DataOrdered.DataOrdered
extend(self, vals)SUAVE.Core.ContainerOrdered.ContainerOrdered
get(self, k, d=None)SUAVE.Core.DataOrdered.DataOrdered
get_bases(self)SUAVE.Core.DataOrdered.DataOrdered
has_key(self, k)SUAVE.Core.DataOrdered.DataOrdered
items(self)SUAVE.Core.DataOrdered.DataOrdered
iteritems(self)SUAVE.Core.DataOrdered.DataOrdered
iterkeys(self)SUAVE.Core.DataOrdered.DataOrdered
itervalues(self)SUAVE.Core.DataOrdered.DataOrdered
keys(self)SUAVE.Core.DataOrdered.DataOrdered
typestring(self)SUAVE.Core.DataOrdered.DataOrdered
update(self, other)SUAVE.Core.DataOrdered.DataOrdered
values(self)SUAVE.Core.DataOrdered.DataOrdered
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Core.ContainerOrdered.ContainerOrdered Class Reference
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-Inheritance diagram for SUAVE.Core.ContainerOrdered.ContainerOrdered:
-
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- - -SUAVE.Core.DataOrdered.DataOrdered - -
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-Public Member Functions

def __defaults__ (self)
 
def __init__ (self, args, kwarg)
 
def append (self, val)
 
def extend (self, vals)
 
- Public Member Functions inherited from SUAVE.Core.DataOrdered.DataOrdered
def append (self, value, key=None)
 
def __defaults__ (self)
 
def __getitem__ (self, k)
 
def __new__ (cls, args, kwarg)
 
def __init__ (self, args, kwarg)
 
def __iter__ (self)
 
def __str__ (self, indent='')
 
def __repr__ (self)
 
def get_bases (self)
 
def typestring (self)
 
def dataname (self)
 
def deep_set (self, keys, val)
 
def deep_get (self, keys)
 
def update (self, other)
 
def __delattr__ (self, key)
 
def __eq__ (self, other)
 
def __len__ (self)
 
def __iter__ (self)
 
def __reduce__ (self)
 
def __setattr__ (self, key, value)
 
def __setitem__ (self, k, v)
 
def clear (self)
 
def get (self, k, d=None)
 
def has_key (self, k)
 
def keys (self)
 
def values (self)
 
def items (self)
 
def iterkeys (self)
 
def itervalues (self)
 
def iteritems (self)
 
-

Detailed Description

-
A dict-type container with attribute, item and index style access
-    intended to hold a attribute-accessible list of DataOrdered(). This is unordered.
-    
-    Assumptions:
-    N/A
-    
-    Source:
-    N/A

Constructor & Destructor Documentation

- -

◆ __init__()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Core.ContainerOrdered.ContainerOrdered.__init__ ( self,
 args,
 kwarg 
)
-
-
Initialization that builds the container
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    self
-    
-    Outputs:
-    N/A
-    
-    Properties Used:
-    N/A
-
-
-

Member Function Documentation

- -

◆ __defaults__()

- -
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- - - - - - - - -
def SUAVE.Core.ContainerOrdered.ContainerOrdered.__defaults__ ( self)
-
-
Defaults function
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    N/A
-    
-    Outputs:
-    N/A
-    
-    Properties Used:
-    N/A
-
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◆ append()

- -
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def SUAVE.Core.ContainerOrdered.ContainerOrdered.append ( self,
 val 
)
-
-
Appends the value to the containers
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    self
-    
-    Outputs:
-    N/A
-    
-    Properties Used:
-    N/A
-
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◆ extend()

- -
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def SUAVE.Core.ContainerOrdered.ContainerOrdered.extend ( self,
 vals 
)
-
-
Append things regressively depending on what is inside.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    self
-    
-    Outputs:
-    N/A
-    
-    Properties Used:
-    N/A
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Core/ContainerOrdered.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Core_1_1ContainerOrdered_1_1ContainerOrdered.js b/_site/doxygen/classSUAVE_1_1Core_1_1ContainerOrdered_1_1ContainerOrdered.js deleted file mode 100644 index d97c28bc..00000000 --- a/_site/doxygen/classSUAVE_1_1Core_1_1ContainerOrdered_1_1ContainerOrdered.js +++ /dev/null @@ -1,7 +0,0 @@ -var classSUAVE_1_1Core_1_1ContainerOrdered_1_1ContainerOrdered = -[ - [ "__init__", "classSUAVE_1_1Core_1_1ContainerOrdered_1_1ContainerOrdered.html#aed0a64ed7ae49700963351f337d3efa3", null ], - [ "__defaults__", "classSUAVE_1_1Core_1_1ContainerOrdered_1_1ContainerOrdered.html#ad4208e02ac70e846604b536c4f654c66", null ], - [ "append", "classSUAVE_1_1Core_1_1ContainerOrdered_1_1ContainerOrdered.html#a7011a4af617cd2242a9dfb98e36e2a24", null ], - [ "extend", "classSUAVE_1_1Core_1_1ContainerOrdered_1_1ContainerOrdered.html#a9c2614dcd055d49735be64e500c3baaa", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Core_1_1ContainerOrdered_1_1ContainerOrdered.png b/_site/doxygen/classSUAVE_1_1Core_1_1ContainerOrdered_1_1ContainerOrdered.png deleted file mode 100644 index 078b02cd..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Core_1_1ContainerOrdered_1_1ContainerOrdered.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Core_1_1Container_1_1Container-members.html b/_site/doxygen/classSUAVE_1_1Core_1_1Container_1_1Container-members.html deleted file mode 100644 index 1a5e15d4..00000000 --- a/_site/doxygen/classSUAVE_1_1Core_1_1Container_1_1Container-members.html +++ /dev/null @@ -1,134 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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- - - - - - diff --git a/_site/doxygen/classSUAVE_1_1Core_1_1Container_1_1Container.html b/_site/doxygen/classSUAVE_1_1Core_1_1Container_1_1Container.html deleted file mode 100644 index 3485fada..00000000 --- a/_site/doxygen/classSUAVE_1_1Core_1_1Container_1_1Container.html +++ /dev/null @@ -1,360 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Core.Container.Container Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Core.Container.Container Class Reference
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-Public Member Functions

def __defaults__ (self)
 
def __init__ (self, args, kwarg)
 
def append (self, val)
 
def extend (self, vals)
 
- Public Member Functions inherited from SUAVE.Core.Data.Data
def __getattribute__ (self, k)
 
def __setattr__ (self, k, v)
 
def __delattr__ (self, k)
 
def __defaults__ (self)
 
def __new__ (cls, args, kwarg)
 
def typestring (self)
 
def dataname (self)
 
def __str__ (self, indent='')
 
def __init__ (self, args, kwarg)
 
def __iter__ (self)
 
def itervalues (self)
 
def values (self)
 
def update (self, other)
 
def get_bases (self)
 
def append (self, value, key=None)
 
def deep_set (self, keys, val)
 
def deep_get (self, keys)
 
def pack_array (self, output='vector')
 
def unpack_array (self, M)
 
def do_recursive (self, method, other=None, default=None)
 
-

Detailed Description

-
A dict-type container with attribute, item and index style access
-    intended to hold a attribute-accessible list of Data(). This is unordered.
-    
-    Assumptions:
-    N/A
-    
-    Source:
-    N/A

Constructor & Destructor Documentation

- -

◆ __init__()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Core.Container.Container.__init__ ( self,
 args,
 kwarg 
)
-
-
Initialization that builds the container
-
-    Assumptions:
-    None
-
-    Source:
-    N/A
-
-    Inputs:
-    self
-
-    Outputs:
-    N/A
-    
-    Properties Used:
-    N/A
-
-
-
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Core.Container.Container.__defaults__ ( self)
-
-
Defaults function
-    
-    Assumptions:
-    None
-
-    Source:
-    N/A
-
-    Inputs:
-    N/A
-
-    Outputs:
-    N/A
-    
-    Properties Used:
-    N/A
-
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-
- -

◆ append()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Core.Container.Container.append ( self,
 val 
)
-
-
Appends the value to the containers
-
-    Assumptions:
-    None
-
-    Source:
-    N/A
-
-    Inputs:
-    self
-
-    Outputs:
-    N/A
-    
-    Properties Used:
-    N/A
-
-
-
- -

◆ extend()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Core.Container.Container.extend ( self,
 vals 
)
-
-
Append things regressively depending on what is inside.
-    
-    Assumptions:
-    None
-
-    Source:
-    N/A
-
-    Inputs:
-    self
-
-    Outputs:
-    N/A
-    
-    Properties Used:
-    N/A
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Core/Container.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Core_1_1Container_1_1Container.js b/_site/doxygen/classSUAVE_1_1Core_1_1Container_1_1Container.js deleted file mode 100644 index d65466be..00000000 --- a/_site/doxygen/classSUAVE_1_1Core_1_1Container_1_1Container.js +++ /dev/null @@ -1,7 +0,0 @@ -var classSUAVE_1_1Core_1_1Container_1_1Container = -[ - [ "__init__", "classSUAVE_1_1Core_1_1Container_1_1Container.html#a7cbac1bbad1dd3279655f10d8315ffb2", null ], - [ "__defaults__", "classSUAVE_1_1Core_1_1Container_1_1Container.html#a566ffa56d67a534512525e5212065568", null ], - [ "append", "classSUAVE_1_1Core_1_1Container_1_1Container.html#a0f2652c760244b0128b854b9dce9a774", null ], - [ "extend", "classSUAVE_1_1Core_1_1Container_1_1Container.html#a6e9b7dbfa8ffa88162d698d32318b22d", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Core_1_1Container_1_1Container.png b/_site/doxygen/classSUAVE_1_1Core_1_1Container_1_1Container.png deleted file mode 100644 index b134f913..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Core_1_1Container_1_1Container.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Core_1_1DataOrdered_1_1DataOrdered-members.html b/_site/doxygen/classSUAVE_1_1Core_1_1DataOrdered_1_1DataOrdered-members.html deleted file mode 100644 index f0232994..00000000 --- a/_site/doxygen/classSUAVE_1_1Core_1_1DataOrdered_1_1DataOrdered-members.html +++ /dev/null @@ -1,142 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Core.DataOrdered.DataOrdered Member List
-
-
- -

This is the complete list of members for SUAVE.Core.DataOrdered.DataOrdered, including all inherited members.

- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
__defaults__(self)SUAVE.Core.DataOrdered.DataOrdered
__delattr__(self, key)SUAVE.Core.DataOrdered.DataOrdered
__eq__(self, other)SUAVE.Core.DataOrdered.DataOrdered
__getitem__(self, k)SUAVE.Core.DataOrdered.DataOrdered
__init__(self, args, kwarg)SUAVE.Core.DataOrdered.DataOrdered
__iter__(self)SUAVE.Core.DataOrdered.DataOrdered
__iter__(self)SUAVE.Core.DataOrdered.DataOrdered
__len__(self)SUAVE.Core.DataOrdered.DataOrdered
__new__(cls, args, kwarg)SUAVE.Core.DataOrdered.DataOrdered
__reduce__(self)SUAVE.Core.DataOrdered.DataOrdered
__repr__(self)SUAVE.Core.DataOrdered.DataOrdered
__setattr__(self, key, value)SUAVE.Core.DataOrdered.DataOrdered
__setitem__(self, k, v)SUAVE.Core.DataOrdered.DataOrdered
__str__(self, indent='')SUAVE.Core.DataOrdered.DataOrdered
append(self, value, key=None)SUAVE.Core.DataOrdered.DataOrdered
clear(self)SUAVE.Core.DataOrdered.DataOrdered
dataname(self)SUAVE.Core.DataOrdered.DataOrdered
deep_get(self, keys)SUAVE.Core.DataOrdered.DataOrdered
deep_set(self, keys, val)SUAVE.Core.DataOrdered.DataOrdered
get(self, k, d=None)SUAVE.Core.DataOrdered.DataOrdered
get_bases(self)SUAVE.Core.DataOrdered.DataOrdered
has_key(self, k)SUAVE.Core.DataOrdered.DataOrdered
items(self)SUAVE.Core.DataOrdered.DataOrdered
iteritems(self)SUAVE.Core.DataOrdered.DataOrdered
iterkeys(self)SUAVE.Core.DataOrdered.DataOrdered
itervalues(self)SUAVE.Core.DataOrdered.DataOrdered
keys(self)SUAVE.Core.DataOrdered.DataOrdered
typestring(self)SUAVE.Core.DataOrdered.DataOrdered
update(self, other)SUAVE.Core.DataOrdered.DataOrdered
values(self)SUAVE.Core.DataOrdered.DataOrdered
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Core_1_1DataOrdered_1_1DataOrdered.html b/_site/doxygen/classSUAVE_1_1Core_1_1DataOrdered_1_1DataOrdered.html deleted file mode 100644 index b5ef8472..00000000 --- a/_site/doxygen/classSUAVE_1_1Core_1_1DataOrdered_1_1DataOrdered.html +++ /dev/null @@ -1,1409 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Core.DataOrdered.DataOrdered Class Reference - - - - - - - - - - - - - - - -
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- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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- -
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- -
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SUAVE.Core.DataOrdered.DataOrdered Class Reference
-
-
-
-Inheritance diagram for SUAVE.Core.DataOrdered.DataOrdered:
-
-
- - -SUAVE.Core.ContainerOrdered.ContainerOrdered -SUAVE.Input_Output.D3JS.Tree_Element.Tree_Element -SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Container - -
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-Public Member Functions

def append (self, value, key=None)
 
def __defaults__ (self)
 
def __getitem__ (self, k)
 
def __new__ (cls, args, kwarg)
 
def __init__ (self, args, kwarg)
 
def __iter__ (self)
 
def __str__ (self, indent='')
 
def __repr__ (self)
 
def get_bases (self)
 
def typestring (self)
 
def dataname (self)
 
def deep_set (self, keys, val)
 
def deep_get (self, keys)
 
def update (self, other)
 
def __delattr__ (self, key)
 
def __eq__ (self, other)
 
def __len__ (self)
 
def __iter__ (self)
 
def __reduce__ (self)
 
def __setattr__ (self, key, value)
 
def __setitem__ (self, k, v)
 
def clear (self)
 
def get (self, k, d=None)
 
def has_key (self, k)
 
def keys (self)
 
def values (self)
 
def items (self)
 
def iterkeys (self)
 
def itervalues (self)
 
def iteritems (self)
 
-

Detailed Description

-
An extension of the Python dict which allows for both tag and '.' usage.
-    This is an unordered dictionary. So indexing it will not produce deterministic results.
-    This has less overhead than ordering. If ordering is needed use DataOrdered().
-   
-    Assumptions:
-    N/A
-    
-    Source:
-    N/A
-

Constructor & Destructor Documentation

- -

◆ __init__()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Core.DataOrdered.DataOrdered.__init__ ( self,
 args,
 kwarg 
)
-
-
Initializes a new Data() class
-    
-    Assumptions:
-    N/A
-    
-    Source:
-    N/A
-    
-    Inputs:
-    N/A
-    
-    Outputs:
-    N/A
-    
-    Properties Used:
-    N/A    
-
-
-
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Core.DataOrdered.DataOrdered.__defaults__ ( self)
-
-
A stub for all classes that come later
-    
-    Assumptions:
-    N/A
-    
-    Source:
-    N/A
-    
-    Inputs:
-    N/A
-    
-    Outputs:
-    N/A
-    
-    Properties Used:
-    N/A    
-
-
-
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◆ __delattr__()

- -
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def SUAVE.Core.DataOrdered.DataOrdered.__delattr__ ( self,
 key 
)
-
-
An override of the standard __delattr_ in Python. This deletes whatever is called by k
-    
-    Assumptions:
-    This one tries to treat k as an object, if that fails it treats it as a key.
-    
-    Source:
-    N/A
-    
-    Inputs:
-    N/A
-    
-    Outputs:
-    N/A
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◆ __eq__()

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def SUAVE.Core.DataOrdered.DataOrdered.__eq__ ( self,
 other 
)
-
-
This is overrides the Python function for checking for equality
-    
-    Assumptions:
-    N/A
-    
-    Source:
-    N/A
-    
-    Inputs:
-    N/A
-    
-    Outputs:
-    N/A
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-    Properties Used:
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◆ __getitem__()

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def SUAVE.Core.DataOrdered.DataOrdered.__getitem__ ( self,
 k 
)
-
-
Retrieves an attribute set by a key k
-    
-    Assumptions:
-    N/A
-    
-    Source:
-    N/A
-    
-    Inputs:
-    N/A
-    
-    Outputs:
-    N/A
-    
-    Properties Used:
-    N/A    
-
-
-
- -

◆ __iter__() [1/2]

- -
-
- - - - - - - - -
def SUAVE.Core.DataOrdered.DataOrdered.__iter__ ( self)
-
-
Returns all the iterable values. Can be used in a for loop.
-    
-    Assumptions:
-    N/A
-    
-    Source:
-    N/A
-    
-    Inputs:
-    N/A
-    
-    Outputs:
-    N/A
-    
-    Properties Used:
-    N/A    
-
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◆ __iter__() [2/2]

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def SUAVE.Core.DataOrdered.DataOrdered.__iter__ ( self)
-
-
Returns all the iterable values. Can be used in a for loop.
-    
-    Assumptions:
-    N/A
-    
-    Source:
-    N/A
-    
-    Inputs:
-    N/A
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-    Outputs:
-    N/A
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◆ __len__()

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def SUAVE.Core.DataOrdered.DataOrdered.__len__ ( self)
-
-
This is overrides the Python function for checking length
-    
-    Assumptions:
-    N/A
-    
-    Source:
-    N/A
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-    Inputs:
-    N/A
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-    Outputs:
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◆ __new__()

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def SUAVE.Core.DataOrdered.DataOrdered.__new__ ( cls,
 args,
 kwarg 
)
-
-
Creates a new Data() class
-    
-    Assumptions:
-    N/A
-    
-    Source:
-    N/A
-    
-    Inputs:
-    N/A
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◆ __reduce__()

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def SUAVE.Core.DataOrdered.DataOrdered.__reduce__ ( self)
-
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Reduction function used for pickling data
-    
-    Assumptions:
-    N/A
-    
-    Source:
-    N/A
-    
-    Inputs:
-    N/A
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◆ __repr__()

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def SUAVE.Core.DataOrdered.DataOrdered.__repr__ ( self)
-
-
This function is used for printing the dataname of the class
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-    Assumptions:
-    N/A
-    
-    Source:
-    N/A
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-    Inputs:
-    N/A
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◆ __setattr__()

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def SUAVE.Core.DataOrdered.DataOrdered.__setattr__ ( self,
 key,
 value 
)
-
-
An override of the standard __setattr_ in Python.
-    
-    Assumptions:
-    This one tries to treat k as an object, if that fails it treats it as a key.
-    
-    Source:
-    N/A
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-    Inputs:
-    k        [key]
-    v        [value]
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-    N/A
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◆ __setitem__()

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def SUAVE.Core.DataOrdered.DataOrdered.__setitem__ ( self,
 k,
 v 
)
-
-
An override of the standard __setattr_ in Python.
-    
-    Assumptions:
-    This one tries to treat k as an object, if that fails it treats it as a key.
-    
-    Source:
-    N/A
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-    Inputs:
-    k        [key]
-    v        [value]
-    
-    Outputs:
-    N/A
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-    N/A    
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◆ __str__()

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def SUAVE.Core.DataOrdered.DataOrdered.__str__ ( self,
 indent = '' 
)
-
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This function is used for printing the class. This starts the first line of printing.
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-    Assumptions:
-    N/A
-    
-    Source:
-    N/A
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◆ append()

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def SUAVE.Core.DataOrdered.DataOrdered.append ( self,
 value,
 key = None 
)
-
-
Adds new values to the classes. Can also change an already appended key
-    
-    Assumptions:
-    N/A
-    
-    Source:
-    N/A
-    
-    Inputs:
-    value
-    key
-    
-    Outputs:
-    N/A
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-    Properties Used:
-    N/A    
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◆ clear()

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def SUAVE.Core.DataOrdered.DataOrdered.clear ( self)
-
-
Empties a dictionary
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-    Assumptions:
-    N/A
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-    Source:
-    N/A
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-    Inputs:
-    N/A
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-    Outputs:
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-    N/A    
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◆ dataname()

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def SUAVE.Core.DataOrdered.DataOrdered.dataname ( self)
-
-
This function is used for printing the class
-    
-    Assumptions:
-    N/A
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-    Source:
-    N/A
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-    Inputs:
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-    Outputs:
-    N/A
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-
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-
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◆ deep_get()

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def SUAVE.Core.DataOrdered.DataOrdered.deep_get ( self,
 keys 
)
-
-
Regresses through a list of keys to pull a specific value out
-    
-    Assumptions:
-    N/A
-    
-    Source:
-    N/A
-    
-    Inputs:
-    keys  - The keys to iterate over
-    
-    Outputs:
-    value - The value to be retrieved
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-    Properties Used:
-    N/A    
-
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◆ deep_set()

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def SUAVE.Core.DataOrdered.DataOrdered.deep_set ( self,
 keys,
 val 
)
-
-
Regresses through a list of keys the same value in various places in a dictionary.
-    
-    Assumptions:
-    N/A
-    
-    Source:
-    N/A
-    
-    Inputs:
-    keys  - The keys to iterate over
-    val   - The value to be set
-    
-    Outputs:
-    N/A
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-    Properties Used:
-    N/A    
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-
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◆ get()

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def SUAVE.Core.DataOrdered.DataOrdered.get ( self,
 k,
 d = None 
)
-
-
Returns the values from k
-    
-    Assumptions:
-    N/A
-    
-    Source:
-    N/A
-    
-    Inputs:
-    k
-    
-    Outputs:
-    N/A
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-    Properties Used:
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-
-
-
- -

◆ get_bases()

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def SUAVE.Core.DataOrdered.DataOrdered.get_bases ( self)
-
-
Finds the higher classes that may be built off of data
-    
-    Assumptions:
-    N/A
-    
-    Source:
-    N/A
-    
-    Inputs:
-    N/A
-    
-    Outputs:
-    klasses
-    
-    Properties Used:
-    N/A    
-
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-
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◆ has_key()

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def SUAVE.Core.DataOrdered.DataOrdered.has_key ( self,
 k 
)
-
-
Checks if the dictionary has the key, k
-    
-    Assumptions:
-    N/A
-    
-    Source:
-    N/A
-    
-    Inputs:
-    k
-    
-    Outputs:
-    N/A
-    
-    Properties Used:
-    N/A    
-
-
-
- -

◆ items()

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-
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def SUAVE.Core.DataOrdered.DataOrdered.items ( self)
-
-
Returns all the items inside the data class
-    
-    Assumptions:
-    N/A
-    
-    Source:
-    N/A
-    
-    Inputs:
-    N/A
-    
-    Outputs:
-    values
-    
-    Properties Used:
-    N/A    
-
-
-
- -

◆ iteritems()

- -
-
- - - - - - - - -
def SUAVE.Core.DataOrdered.DataOrdered.iteritems ( self)
-
-
All items that may be iterated over
-    
-    Assumptions:
-    N/A
-    
-    Source:
-    N/A
-    
-    Inputs:
-    N/A
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-    Outputs:
-    N/A
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-
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◆ iterkeys()

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def SUAVE.Core.DataOrdered.DataOrdered.iterkeys ( self)
-
-
Returns all the keys which may be iterated over
-    
-    Assumptions:
-    N/A
-    
-    Source:
-    N/A
-    
-    Inputs:
-    N/A
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-    Outputs:
-    N/A
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-    N/A    
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-
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◆ itervalues()

- -
-
- - - - - - - - -
def SUAVE.Core.DataOrdered.DataOrdered.itervalues ( self)
-
-
Finds all the values that can be iterated over.
-    
-    Assumptions:
-    N/A
-    
-    Source:
-    N/A
-    
-    Inputs:
-    N/A
-    
-    Outputs:
-    N/A
-    
-    Properties Used:
-    N/A    
-
-
-
- -

◆ keys()

- -
-
- - - - - - - - -
def SUAVE.Core.DataOrdered.DataOrdered.keys ( self)
-
-
Returns a list of keys
-    
-    Assumptions:
-    N/A
-    
-    Source:
-    N/A
-    
-    Inputs:
-    N/A
-    
-    Outputs:
-    N/A
-    
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-    N/A    
-
-
-
- -

◆ typestring()

- -
-
- - - - - - - - -
def SUAVE.Core.DataOrdered.DataOrdered.typestring ( self)
-
-
This function makes the .key.key structure in string form of Data()
-    
-    Assumptions:
-    N/A
-    
-    Source:
-    N/A
-    
-    Inputs:
-    N/A
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-    Outputs:
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◆ update()

- -
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def SUAVE.Core.DataOrdered.DataOrdered.update ( self,
 other 
)
-
-
Updates the internal values of a dictionary with given data
-    
-    Assumptions:
-    N/A
-    
-    Source:
-    N/A
-    
-    Inputs:
-    other
-    
-    Outputs:
-    N/A
-    
-    Properties Used:
-    N/A    
-
-
-
- -

◆ values()

- -
-
- - - - - - - - -
def SUAVE.Core.DataOrdered.DataOrdered.values ( self)
-
-
Returns all values inside the Data() class.
-    
-    Assumptions:
-    N/A
-    
-    Source:
-    N/A
-    
-    Inputs:
-    N/A
-    
-    Outputs:
-    values
-    
-    Properties Used:
-    N/A    
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Core/DataOrdered.py
  • -
-
-
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- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Core.DataOrdered.Property Member List
-
-
- -

This is the complete list of members for SUAVE.Core.DataOrdered.Property, including all inherited members.

- - - - - -
__delete__(self, obj)SUAVE.Core.DataOrdered.Property
__get__(self, obj, kls=None)SUAVE.Core.DataOrdered.Property
__init__(self, key=None)SUAVE.Core.DataOrdered.Property
__set__(self, obj, val)SUAVE.Core.DataOrdered.Property
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Core_1_1DataOrdered_1_1Property.html b/_site/doxygen/classSUAVE_1_1Core_1_1DataOrdered_1_1Property.html deleted file mode 100644 index bc06565e..00000000 --- a/_site/doxygen/classSUAVE_1_1Core_1_1DataOrdered_1_1Property.html +++ /dev/null @@ -1,335 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Core.DataOrdered.Property Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
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-
- - - -
-
- -
-
-
- -
- -
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SUAVE.Core.DataOrdered.Property Class Reference
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-Inheritance diagram for SUAVE.Core.DataOrdered.Property:
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- - - -
- - - - - - - - - - -

-Public Member Functions

def __init__ (self, key=None)
 
def __get__ (self, obj, kls=None)
 
def __set__ (self, obj, val)
 
def __delete__ (self, obj)
 
-

Detailed Description

-
Used to create the root map essential to the linking in DataOrdered()
-   
-    Assumptions:
-    N/A
-    
-    Source:
-    N/A
-

Constructor & Destructor Documentation

- -

◆ __init__()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Core.DataOrdered.Property.__init__ ( self,
 key = None 
)
-
-
Initializes a property
-    
-    Assumptions:
-    N/A
-    
-    Source:
-    N/A
-    
-    Inputs:
-    N/A
-    
-    Outputs:
-    N/A
-    
-    Properties Used:
-    N/A    
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-
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-

Member Function Documentation

- -

◆ __delete__()

- -
-
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def SUAVE.Core.DataOrdered.Property.__delete__ ( self,
 obj 
)
-
-
Deletes a property
-    
-    Assumptions:
-    N/A
-    
-    Source:
-    N/A
-    
-    Inputs:
-    N/A
-    
-    Outputs:
-    N/A
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◆ __get__()

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def SUAVE.Core.DataOrdered.Property.__get__ ( self,
 obj,
 kls = None 
)
-
-
Gets a property
-    
-    Assumptions:
-    N/A
-    
-    Source:
-    N/A
-    
-    Inputs:
-    obj
-    
-    Outputs:
-    self.key
-    
-    Properties Used:
-    N/A    
-
-
-
- -

◆ __set__()

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def SUAVE.Core.DataOrdered.Property.__set__ ( self,
 obj,
 val 
)
-
-
Sets a property
-    
-    Assumptions:
-    N/A
-    
-    Source:
-    N/A
-    
-    Inputs:
-    obj
-    value
-    
-    Outputs:
-    N/A
-    
-    Properties Used:
-    N/A    
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Core/DataOrdered.py
  • -
-
-
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- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Core.Data.Data Member List
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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-
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- - -
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SUAVE.Core.Data.Data Class Reference
-
-
-
-Inheritance diagram for SUAVE.Core.Data.Data:
-
-
- - -SUAVE.Core.Container.Container -SUAVE.Core.Diffed_Data.Diffed_Data -SUAVE.Methods.Aerodynamics.AVL.Data.Aircraft.Aircraft -SUAVE.Methods.Aerodynamics.AVL.Data.Body.Body -SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Run_Case -SUAVE.Methods.Aerodynamics.AVL.Data.Configuration.Configuration -SUAVE.Methods.Aerodynamics.AVL.Data.Inputs.Inputs -SUAVE.Methods.Aerodynamics.AVL.Data.Results.Results -SUAVE.Methods.Aerodynamics.AVL.Data.Settings.AVL_Discretization_Settings -SUAVE.Methods.Aerodynamics.AVL.Data.Settings.Settings -SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface -SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Section -SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing -SUAVE.Optimization.Nexus.Nexus -SUAVE.Optimization.Package_Setups.TRMM.Trust_Region.Trust_Region -SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization -SUAVE.Optimization.Surrogate_Optimization.Surrogate_Optimization -SUAVE.Sizing.Sizing_Loop.Sizing_Loop -SUAVE.Surrogate.Surrogate_Problem.Surrogate_Problem -SUAVE.Vehicle.Costs -SUAVE.Vehicle.Vehicle - -
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __getattribute__ (self, k)
 
def __setattr__ (self, k, v)
 
def __delattr__ (self, k)
 
def __defaults__ (self)
 
def __new__ (cls, args, kwarg)
 
def typestring (self)
 
def dataname (self)
 
def __str__ (self, indent='')
 
def __init__ (self, args, kwarg)
 
def __iter__ (self)
 
def itervalues (self)
 
def values (self)
 
def update (self, other)
 
def get_bases (self)
 
def append (self, value, key=None)
 
def deep_set (self, keys, val)
 
def deep_get (self, keys)
 
def pack_array (self, output='vector')
 
def unpack_array (self, M)
 
def do_recursive (self, method, other=None, default=None)
 
-

Detailed Description

-
An extension of the Python dict which allows for both tag and '.' usage.
-    This is an unordered dictionary. So indexing it will not produce deterministic results.
-    This has less overhead than ordering. If ordering is needed use DataOrdered().
-   
-    Assumptions:
-    N/A
-    
-    Source:
-    N/A
-

Constructor & Destructor Documentation

- -

◆ __init__()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Core.Data.Data.__init__ ( self,
 args,
 kwarg 
)
-
-
Initializes a new Data() class
-    
-    Assumptions:
-    N/A
-    
-    Source:
-    N/A
-    
-    Inputs:
-    N/A
-    
-    Outputs:
-    N/A
-    
-    Properties Used:
-    N/A    
-
-
-
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Core.Data.Data.__defaults__ ( self)
-
-
A stub for all classes that come later
-    
-    Assumptions:
-    N/A
-    
-    Source:
-    N/A
-    
-    Inputs:
-    N/A
-    
-    Outputs:
-    N/A
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-    Properties Used:
-    N/A    
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- -

◆ __delattr__()

- -
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- - - - - - - - - - - - - - - - - - -
def SUAVE.Core.Data.Data.__delattr__ ( self,
 k 
)
-
-
An override of the standard __delattr_ in Python. This deletes whatever is called by k
-    
-    Assumptions:
-    This one tries to treat k as an object, if that fails it treats it as a key.
-    
-    Source:
-    N/A
-    
-    Inputs:
-    N/A
-    
-    Outputs:
-    N/A
-    
-    Properties Used:
-    N/A    
-
-
-
- -

◆ __getattribute__()

- -
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- - - - - - - - - - - - - - - - - - -
def SUAVE.Core.Data.Data.__getattribute__ ( self,
 k 
)
-
-
Retrieves an attribute set by a key k
-    
-    Assumptions:
-    Does a try if it is a dict, but if that fails treats it as an object
-    
-    Source:
-    N/A
-    
-    Inputs:
-    k
-    
-    Outputs:
-    whatever is found by k
-    
-    Properties Used:
-    N/A
-
-
- -

◆ __iter__()

- -
-
- - - - - - - - -
def SUAVE.Core.Data.Data.__iter__ ( self)
-
-
Returns all the iterable values. Can be used in a for loop.
-    
-    Assumptions:
-    N/A
-    
-    Source:
-    N/A
-    
-    Inputs:
-    N/A
-    
-    Outputs:
-    N/A
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-    Properties Used:
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- -

◆ __new__()

- -
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def SUAVE.Core.Data.Data.__new__ ( cls,
 args,
 kwarg 
)
-
-
Creates a new Data() class
-    
-    Assumptions:
-    N/A
-    
-    Source:
-    N/A
-    
-    Inputs:
-    N/A
-    
-    Outputs:
-    N/A
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◆ __setattr__()

- -
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def SUAVE.Core.Data.Data.__setattr__ ( self,
 k,
 v 
)
-
-
An override of the standard __setattr_ in Python.
-    
-    Assumptions:
-    This one tries to treat k as an object, if that fails it treats it as a key.
-    
-    Source:
-    N/A
-    
-    Inputs:
-    k        [key]
-    v        [value]
-    
-    Outputs:
-    N/A
-    
-    Properties Used:
-    N/A    
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-
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- -

◆ __str__()

- -
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def SUAVE.Core.Data.Data.__str__ ( self,
 indent = '' 
)
-
-
This function is used for printing the class. This starts the first line of printing.
-    
-    Assumptions:
-    N/A
-    
-    Source:
-    N/A
-    
-    Inputs:
-    N/A
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◆ append()

- -
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def SUAVE.Core.Data.Data.append ( self,
 value,
 key = None 
)
-
-
Adds new values to the classes. Can also change an already appended key
-    
-    Assumptions:
-    N/A
-    
-    Source:
-    N/A
-    
-    Inputs:
-    value
-    key
-    
-    Outputs:
-    N/A
-    
-    Properties Used:
-    N/A    
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◆ dataname()

- -
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def SUAVE.Core.Data.Data.dataname ( self)
-
-
This function is used for printing the class
-    
-    Assumptions:
-    N/A
-    
-    Source:
-    N/A
-    
-    Inputs:
-    N/A
-    
-    Outputs:
-    N/A
-    
-    Properties Used:
-    N/A    
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-
- -

◆ deep_get()

- -
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def SUAVE.Core.Data.Data.deep_get ( self,
 keys 
)
-
-
Regresses through a list of keys to pull a specific value out
-    
-    Assumptions:
-    N/A
-    
-    Source:
-    N/A
-    
-    Inputs:
-    keys  - The keys to iterate over
-    
-    Outputs:
-    value - The value to be retrieved
-    
-    Properties Used:
-    N/A    
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- -

◆ deep_set()

- -
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def SUAVE.Core.Data.Data.deep_set ( self,
 keys,
 val 
)
-
-
Regresses through a list of keys the same value in various places in a dictionary.
-    
-    Assumptions:
-    N/A
-    
-    Source:
-    N/A
-    
-    Inputs:
-    keys  - The keys to iterate over
-    val   - The value to be set
-    
-    Outputs:
-    N/A
-    
-    Properties Used:
-    N/A    
-
-
-
- -

◆ do_recursive()

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def SUAVE.Core.Data.Data.do_recursive ( self,
 method,
 other = None,
 default = None 
)
-
-
Recursively applies a method of the class.
-    
-    Assumptions:
-    N/A
-    
-    Source:
-    N/A
-    
-    Inputs:
-    method  - name of the method to access
-    
-    Outputs:
-    Result  - the results of the method
-    
-    Properties Used:
-    N/A    
-
-
-
- -

◆ get_bases()

- -
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- - - - - - - - -
def SUAVE.Core.Data.Data.get_bases ( self)
-
-
Finds the higher classes that may be built off of data
-    
-    Assumptions:
-    N/A
-    
-    Source:
-    N/A
-    
-    Inputs:
-    N/A
-    
-    Outputs:
-    klasses
-    
-    Properties Used:
-    N/A    
-
-
-
- -

◆ itervalues()

- -
-
- - - - - - - - -
def SUAVE.Core.Data.Data.itervalues ( self)
-
-
Finds all the values that can be iterated over.
-    
-    Assumptions:
-    N/A
-    
-    Source:
-    N/A
-    
-    Inputs:
-    N/A
-    
-    Outputs:
-    N/A
-    
-    Properties Used:
-    N/A    
-
-
-
- -

◆ pack_array()

- -
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def SUAVE.Core.Data.Data.pack_array ( self,
 output = 'vector' 
)
-
-
maps the data dict to a 1D vector or 2D column array
-
-    Assumptions:
-will only pack int, float, np.array and np.matrix (max rank 2)
-if using output = 'matrix', all data values must have 
-same length (if 1D) or number of rows (if 2D), otherwise is skipped
-    
-    Source:
-    N/A
-    
-    Inputs:
-output - either 'vector' (default), or 'array'
-         chooses whether to output a 1d vector or 
-         2d column array
-    
-    Outputs:
-array - the packed array
-    
-    Properties Used:
-    N/A  
-
-
- -

◆ typestring()

- -
-
- - - - - - - - -
def SUAVE.Core.Data.Data.typestring ( self)
-
-
This function makes the .key.key structure in string form of Data()
-    
-    Assumptions:
-    N/A
-    
-    Source:
-    N/A
-    
-    Inputs:
-    N/A
-    
-    Outputs:
-    N/A
-    
-    Properties Used:
-    N/A    
-
-
-
- -

◆ unpack_array()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Core.Data.Data.unpack_array ( self,
 M 
)
-
-
unpacks an input 1d vector or 2d column array into the data dictionary
-    important that the structure of the data dictionary, and the shapes
-    of the contained values are the same as the data from which the array was packed
-    
-    Assumptions:
-    N/A
-    
-    Source:
-    N/A
-    
-    Inputs:
-    M - either a 1D vector or 2D column array
-    
-    Outputs:
-    a reference to self, updates self in place
-    
-    Properties Used:
-    N/A    
-
-
-
- -

◆ update()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Core.Data.Data.update ( self,
 other 
)
-
-
Updates the internal values of a dictionary with given data
-    
-    Assumptions:
-    N/A
-    
-    Source:
-    N/A
-    
-    Inputs:
-    other
-    
-    Outputs:
-    N/A
-    
-    Properties Used:
-    N/A    
-
-
-
- -

◆ values()

- -
-
- - - - - - - - -
def SUAVE.Core.Data.Data.values ( self)
-
-
Returns all values inside the Data() class.
-    
-    Assumptions:
-    N/A
-    
-    Source:
-    N/A
-    
-    Inputs:
-    N/A
-    
-    Outputs:
-    values
-    
-    Properties Used:
-    N/A    
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Core/Data.py
  • -
-
-
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Core.Diffed_Data.Container Member List
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Core.Diffed_Data.Container Class Reference
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-Inheritance diagram for SUAVE.Core.Diffed_Data.Container:
-
-
- - - -
- - - - - - - - - - -

-Public Member Functions

def append (self, value)
 
def pull_base (self)
 
def store_diff (self)
 
def finalize (self)
 
-

Detailed Description

-
A dict-type container with attribute, item and index style access
-    intended to hold a attribute-accessible list of Data(). This is unordered.
-    
-    Assumptions:
-    N/A
-    
-    Source:
-    N/A

Member Function Documentation

- -

◆ append()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Core.Diffed_Data.Container.append ( self,
 value 
)
-
-
Appends the value to the containers
-
-    Assumptions:
-    None
-
-    Source:
-    N/A
-
-    Inputs:
-    self
-
-    Outputs:
-    N/A
-    
-    Properties Used:
-    N/A
-
-
-
- -

◆ finalize()

- -
-
- - - - - - - - -
def SUAVE.Core.Diffed_Data.Container.finalize ( self)
-
-
This just does a pull_base()
-    
-    Assumptions:
-    N/A
-    
-    Source:
-    N/A
-    
-    Inputs:
-    N/A
-    
-    Outputs:
-    N/A
-    
-    Properties Used:
-    N/A    
-
-
-
- -

◆ pull_base()

- -
-
- - - - - - - - -
def SUAVE.Core.Diffed_Data.Container.pull_base ( self)
-
-
Updates the differences
-    
-    Assumptions:
-    N/A
-    
-    Source:
-    N/A
-    
-    Inputs:
-    N/A
-    
-    Outputs:
-    N/A
-    
-    Properties Used:
-    N/A    
-
-
-
- -

◆ store_diff()

- -
-
- - - - - - - - -
def SUAVE.Core.Diffed_Data.Container.store_diff ( self)
-
-
Finds the differences and saves them
-    
-    Assumptions:
-    N/A
-    
-    Source:
-    N/A
-    
-    Inputs:
-    N/A
-    
-    Outputs:
-    N/A
-    
-    Properties Used:
-    N/A    
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Core/Diffed_Data.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Core_1_1Diffed__Data_1_1Container.js b/_site/doxygen/classSUAVE_1_1Core_1_1Diffed__Data_1_1Container.js deleted file mode 100644 index fb459b0a..00000000 --- a/_site/doxygen/classSUAVE_1_1Core_1_1Diffed__Data_1_1Container.js +++ /dev/null @@ -1,7 +0,0 @@ -var classSUAVE_1_1Core_1_1Diffed__Data_1_1Container = -[ - [ "append", "classSUAVE_1_1Core_1_1Diffed__Data_1_1Container.html#a9328520507f3fc021ea2a18804769fe4", null ], - [ "finalize", "classSUAVE_1_1Core_1_1Diffed__Data_1_1Container.html#a85ed1a65b349fba00dc5d1611ef128cc", null ], - [ "pull_base", "classSUAVE_1_1Core_1_1Diffed__Data_1_1Container.html#af9bd7385c66e21f06ec75d4869be4a10", null ], - [ "store_diff", "classSUAVE_1_1Core_1_1Diffed__Data_1_1Container.html#aee149ee0e2174680ff180d53f548d25c", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Core_1_1Diffed__Data_1_1Container.png b/_site/doxygen/classSUAVE_1_1Core_1_1Diffed__Data_1_1Container.png deleted file mode 100644 index 6cee15ab..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Core_1_1Diffed__Data_1_1Container.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Core_1_1Diffed__Data_1_1Diffed__Data-members.html b/_site/doxygen/classSUAVE_1_1Core_1_1Diffed__Data_1_1Diffed__Data-members.html deleted file mode 100644 index 286b6505..00000000 --- a/_site/doxygen/classSUAVE_1_1Core_1_1Diffed__Data_1_1Diffed__Data-members.html +++ /dev/null @@ -1,137 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
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- - - - - - diff --git a/_site/doxygen/classSUAVE_1_1Core_1_1Diffed__Data_1_1Diffed__Data.html b/_site/doxygen/classSUAVE_1_1Core_1_1Diffed__Data_1_1Diffed__Data.html deleted file mode 100644 index 8ed9daa6..00000000 --- a/_site/doxygen/classSUAVE_1_1Core_1_1Diffed__Data_1_1Diffed__Data.html +++ /dev/null @@ -1,424 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Core.Diffed_Data.Diffed_Data Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
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- -
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-
SUAVE.Core.Diffed_Data.Diffed_Data Class Reference
-
-
-
-Inheritance diagram for SUAVE.Core.Diffed_Data.Diffed_Data:
-
-
- - -SUAVE.Core.Data.Data - -
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def __init__ (self, base=None)
 
def store_diff (self)
 
def pull_base (self)
 
def __str__ (self, indent='')
 
def finalize (self)
 
- Public Member Functions inherited from SUAVE.Core.Data.Data
def __getattribute__ (self, k)
 
def __setattr__ (self, k, v)
 
def __delattr__ (self, k)
 
def __defaults__ (self)
 
def __new__ (cls, args, kwarg)
 
def typestring (self)
 
def dataname (self)
 
def __str__ (self, indent='')
 
def __init__ (self, args, kwarg)
 
def __iter__ (self)
 
def itervalues (self)
 
def values (self)
 
def update (self, other)
 
def get_bases (self)
 
def append (self, value, key=None)
 
def deep_set (self, keys, val)
 
def deep_get (self, keys)
 
def pack_array (self, output='vector')
 
def unpack_array (self, M)
 
def do_recursive (self, method, other=None, default=None)
 
- - - -

-Public Attributes

tag
 
-

Detailed Description

-
This is for creating a data new class where a different copy is saved.
-    This is useful for creating a new configuration of a vehicle.
-
-    Assumptions:
-    N/A
-
-    Source:
-    N/A
-

Constructor & Destructor Documentation

- -

◆ __init__()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Core.Diffed_Data.Diffed_Data.__init__ ( self,
 base = None 
)
-
-
Initializes the new Diffed_Data() class through a deepcopy
-    
-    Assumptions:
-    N/A
-    
-    Source:
-    N/A
-    
-    Inputs:
-    N/A
-    
-    Outputs:
-    N/A
-    
-    Properties Used:
-    N/A    
-
-
-
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Core.Diffed_Data.Diffed_Data.__defaults__ ( self)
-
-
A stub for all classes that come later
-    
-    Assumptions:
-    N/A
-    
-    Source:
-    N/A
-    
-    Inputs:
-    N/A
-    
-    Outputs:
-    N/A
-    
-    Properties Used:
-    N/A    
-
-
-
- -

◆ __str__()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Core.Diffed_Data.Diffed_Data.__str__ ( self,
 indent = '' 
)
-
-
This function is used for printing the class.
-    
-    Assumptions:
-    N/A
-    
-    Source:
-    N/A
-    
-    Inputs:
-    N/A
-    
-    Outputs:
-    N/A
-    
-    Properties Used:
-    N/A    
-
-
-
- -

◆ finalize()

- -
-
- - - - - - - - -
def SUAVE.Core.Diffed_Data.Diffed_Data.finalize ( self)
-
-
This just does a pull_base()
-    
-    Assumptions:
-    N/A
-    
-    Source:
-    N/A
-    
-    Inputs:
-    N/A
-    
-    Outputs:
-    N/A
-    
-    Properties Used:
-    N/A    
-
-
-
- -

◆ pull_base()

- -
-
- - - - - - - - -
def SUAVE.Core.Diffed_Data.Diffed_Data.pull_base ( self)
-
-
Updates the differences
-    
-    Assumptions:
-    N/A
-    
-    Source:
-    N/A
-    
-    Inputs:
-    N/A
-    
-    Outputs:
-    N/A
-    
-    Properties Used:
-    N/A    
-
-
-
- -

◆ store_diff()

- -
-
- - - - - - - - -
def SUAVE.Core.Diffed_Data.Diffed_Data.store_diff ( self)
-
-
Finds the differences and saves them
-    
-    Assumptions:
-    N/A
-    
-    Source:
-    N/A
-    
-    Inputs:
-    N/A
-    
-    Outputs:
-    N/A
-    
-    Properties Used:
-    N/A    
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Core/Diffed_Data.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Core_1_1Diffed__Data_1_1Diffed__Data.js b/_site/doxygen/classSUAVE_1_1Core_1_1Diffed__Data_1_1Diffed__Data.js deleted file mode 100644 index c65fcb46..00000000 --- a/_site/doxygen/classSUAVE_1_1Core_1_1Diffed__Data_1_1Diffed__Data.js +++ /dev/null @@ -1,10 +0,0 @@ -var classSUAVE_1_1Core_1_1Diffed__Data_1_1Diffed__Data = -[ - [ "__init__", "classSUAVE_1_1Core_1_1Diffed__Data_1_1Diffed__Data.html#a5189a8561ed465fd3eee205ee03adbc7", null ], - [ "__defaults__", "classSUAVE_1_1Core_1_1Diffed__Data_1_1Diffed__Data.html#a42f788eee3fdf0b91a57214e87d14319", null ], - [ "__str__", "classSUAVE_1_1Core_1_1Diffed__Data_1_1Diffed__Data.html#acad2ec656ea1a3ab4165ad6e187f722c", null ], - [ "finalize", "classSUAVE_1_1Core_1_1Diffed__Data_1_1Diffed__Data.html#a208551ba84d56d7f6142fd73ab8a7814", null ], - [ "pull_base", "classSUAVE_1_1Core_1_1Diffed__Data_1_1Diffed__Data.html#ac954509f24fa414208851dd82f262e8b", null ], - [ "store_diff", "classSUAVE_1_1Core_1_1Diffed__Data_1_1Diffed__Data.html#a753bc71826eb55734e8c31d7c2e6a5d2", null ], - [ "tag", "classSUAVE_1_1Core_1_1Diffed__Data_1_1Diffed__Data.html#aa628ee6a83534bce567dd638fda62b68", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Core_1_1Diffed__Data_1_1Diffed__Data.png b/_site/doxygen/classSUAVE_1_1Core_1_1Diffed__Data_1_1Diffed__Data.png deleted file mode 100644 index 3f3f5f20..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Core_1_1Diffed__Data_1_1Diffed__Data.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Core_1_1redirect_1_1folder-members.html b/_site/doxygen/classSUAVE_1_1Core_1_1redirect_1_1folder-members.html deleted file mode 100644 index 8dea84fc..00000000 --- a/_site/doxygen/classSUAVE_1_1Core_1_1redirect_1_1folder-members.html +++ /dev/null @@ -1,121 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
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-
SUAVE.Core.redirect.folder Member List
-
-
- -

This is the complete list of members for SUAVE.Core.redirect.folder, including all inherited members.

- - - - - - - - - - -
__enter__(self) (defined in SUAVE.Core.redirect.folder)SUAVE.Core.redirect.folder
__exit__(self, exc_type, exc_value, traceback) (defined in SUAVE.Core.redirect.folder)SUAVE.Core.redirect.folder
__init__(self, folder, pull=None, link=None, force=True)SUAVE.Core.redirect.folder
folder (defined in SUAVE.Core.redirect.folder)SUAVE.Core.redirect.folder
force (defined in SUAVE.Core.redirect.folder)SUAVE.Core.redirect.folder
link (defined in SUAVE.Core.redirect.folder)SUAVE.Core.redirect.folder
origin (defined in SUAVE.Core.redirect.folder)SUAVE.Core.redirect.folder
pull (defined in SUAVE.Core.redirect.folder)SUAVE.Core.redirect.folder
push (defined in SUAVE.Core.redirect.folder)SUAVE.Core.redirect.folder
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Core_1_1redirect_1_1folder.html b/_site/doxygen/classSUAVE_1_1Core_1_1redirect_1_1folder.html deleted file mode 100644 index 1b3b4b04..00000000 --- a/_site/doxygen/classSUAVE_1_1Core_1_1redirect_1_1folder.html +++ /dev/null @@ -1,244 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Core.redirect.folder Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
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-
- - - -
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- -
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SUAVE.Core.redirect.folder Class Reference
-
-
-
-Inheritance diagram for SUAVE.Core.redirect.folder:
-
-
- - - -
- - - - - - - - -

-Public Member Functions

def __init__ (self, folder, pull=None, link=None, force=True)
 
-def __enter__ (self)
 
-def __exit__ (self, exc_type, exc_value, traceback)
 
- - - - - - - - - - - - - -

-Public Attributes

origin
 
folder
 
pull
 
push
 
link
 
force
 
-

Detailed Description

-
Temporarily redirects to a working folder, pulling 
-    and pushing needed files
-    
-    Example:
-    
-    folder = 'temp'                    
-    pull   = ['file1.txt','file2.txt'] 
-    link   = ['file3.big']             
-    force  = True                      
-    
-    # original path
-    import os
-    print os.getcwd()
-    
-    # enter folder
-    with SU2.io.redirect_folder(folder,pull,link,force) as push:
-        print os.getcwd()
-        # code
-        push.append('file4.txt')
-    #: with folder redirection
-    
-    # returned to original path
-    print os.getcwd()
-    
-    Inputs:
-        folder - working folder, relative or absolute
-        pull   - list of files to pull (copy to working folder)
-        link   - list of files to link (symbolic link in working folder)
-        force  - True/False overwrite existing files in working folder
-    
-    Targets:
-        push   - list of files to push (copy to originating path)
-    
-    Notes:
-        push must be appended or extended, not overwritten
-        links in Windows not supported, will simply copy
-

Constructor & Destructor Documentation

- -

◆ __init__()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Core.redirect.folder.__init__ ( self,
 folder,
 pull = None,
 link = None,
 force = True 
)
-
-
folder redirection initialization
-    see help( folder ) for more info
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Core/redirect.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Core_1_1redirect_1_1folder.js b/_site/doxygen/classSUAVE_1_1Core_1_1redirect_1_1folder.js deleted file mode 100644 index 4bc9d2ce..00000000 --- a/_site/doxygen/classSUAVE_1_1Core_1_1redirect_1_1folder.js +++ /dev/null @@ -1,12 +0,0 @@ -var classSUAVE_1_1Core_1_1redirect_1_1folder = -[ - [ "__init__", "classSUAVE_1_1Core_1_1redirect_1_1folder.html#aa5667c9c1c87940bd3a45c19b6ad5c74", null ], - [ "__enter__", "classSUAVE_1_1Core_1_1redirect_1_1folder.html#a1318626860a67d19a9d4d65b1eecf288", null ], - [ "__exit__", "classSUAVE_1_1Core_1_1redirect_1_1folder.html#ac9a4641c45c24e738b710a110077d608", null ], - [ "folder", "classSUAVE_1_1Core_1_1redirect_1_1folder.html#af76d93f69e0ad58913af7b98b37b7704", null ], - [ "force", "classSUAVE_1_1Core_1_1redirect_1_1folder.html#a62c79e2d9d2da764ab1a6417b4c490fd", null ], - [ "link", "classSUAVE_1_1Core_1_1redirect_1_1folder.html#a6eeffc2ddcf5f1350df4a0c130e19407", null ], - [ "origin", "classSUAVE_1_1Core_1_1redirect_1_1folder.html#a0272b78e6d94ac47bdefa45a77a586c9", null ], - [ "pull", "classSUAVE_1_1Core_1_1redirect_1_1folder.html#aad3daec21784bc33f5200b2b55331696", null ], - [ "push", "classSUAVE_1_1Core_1_1redirect_1_1folder.html#aa62e5156869cca5e34e92f8ccc2ae3e7", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Core_1_1redirect_1_1folder.png b/_site/doxygen/classSUAVE_1_1Core_1_1redirect_1_1folder.png deleted file mode 100644 index 02754e3d..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Core_1_1redirect_1_1folder.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Core_1_1redirect_1_1output-members.html b/_site/doxygen/classSUAVE_1_1Core_1_1redirect_1_1output-members.html deleted file mode 100644 index 201903a8..00000000 --- a/_site/doxygen/classSUAVE_1_1Core_1_1redirect_1_1output-members.html +++ /dev/null @@ -1,116 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
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-
-
- - - -
-
- -
-
-
- -
- -
-
- - -
- -
- -
-
-
SUAVE.Core.redirect.output Member List
-
-
- -

This is the complete list of members for SUAVE.Core.redirect.output, including all inherited members.

- - - - - -
__enter__(self) (defined in SUAVE.Core.redirect.output)SUAVE.Core.redirect.output
__exit__(self, exc_type, exc_value, traceback) (defined in SUAVE.Core.redirect.output)SUAVE.Core.redirect.output
__init__(self, stdout=None, stderr=None)SUAVE.Core.redirect.output
old_stderr (defined in SUAVE.Core.redirect.output)SUAVE.Core.redirect.output
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Core_1_1redirect_1_1output.html b/_site/doxygen/classSUAVE_1_1Core_1_1redirect_1_1output.html deleted file mode 100644 index b23ca96f..00000000 --- a/_site/doxygen/classSUAVE_1_1Core_1_1redirect_1_1output.html +++ /dev/null @@ -1,211 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Core.redirect.output Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Core.redirect.output Class Reference
-
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-
-Inheritance diagram for SUAVE.Core.redirect.output:
-
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- - - - - - - - -

-Public Member Functions

def __init__ (self, stdout=None, stderr=None)
 
-def __enter__ (self)
 
-def __exit__ (self, exc_type, exc_value, traceback)
 
- - - -

-Public Attributes

old_stderr
 
-

Detailed Description

-
Temporarily redirects sys.stdout and sys.stderr when used in
-    a 'with' contextmanager
-    
-    Example:
-    with SU2.io.redirect_output('stdout.txt','stderr.txt'):
-        sys.stdout.write("standard out")
-        sys.stderr.write("stanrard error")
-        # code
-    #: with output redirection
-    
-    Inputs:
-        stdout - None, a filename, or a file stream
-        stderr - None, a filename, or a file stream
-    None will not redirect outptut
-    
-    Source:
-    http://stackoverflow.com/questions/6796492/python-temporarily-redirect-stdout-stderr

Constructor & Destructor Documentation

- -

◆ __init__()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Core.redirect.output.__init__ ( self,
 stdout = None,
 stderr = None 
)
-
-
Initializes a new output() class
-    
-    Assumptions:
-    N/A
-    
-    Source:
-    N/A
-    
-    Inputs:
-    N/A
-    
-    Outputs:
-    N/A
-    
-    Properties Used:
-    N/A    
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Core/redirect.py
  • -
-
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Input_Output.D3JS.Tree_Element.Tree_Element Member List
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This is the complete list of members for SUAVE.Input_Output.D3JS.Tree_Element.Tree_Element, including all inherited members.

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__defaults__(self)SUAVE.Core.DataOrdered.DataOrdered
__delattr__(self, key)SUAVE.Core.DataOrdered.DataOrdered
__eq__(self, other)SUAVE.Core.DataOrdered.DataOrdered
__getitem__(self, k)SUAVE.Core.DataOrdered.DataOrdered
__init__(self, name)SUAVE.Input_Output.D3JS.Tree_Element.Tree_Element
SUAVE::Core::DataOrdered::DataOrdered.__init__(self, args, kwarg)SUAVE.Core.DataOrdered.DataOrdered
__iter__(self)SUAVE.Core.DataOrdered.DataOrdered
__iter__(self)SUAVE.Core.DataOrdered.DataOrdered
__len__(self)SUAVE.Core.DataOrdered.DataOrdered
__new__(cls, args, kwarg)SUAVE.Core.DataOrdered.DataOrdered
__reduce__(self)SUAVE.Core.DataOrdered.DataOrdered
__repr__(self)SUAVE.Core.DataOrdered.DataOrdered
__setattr__(self, key, value)SUAVE.Core.DataOrdered.DataOrdered
__setitem__(self, k, v)SUAVE.Core.DataOrdered.DataOrdered
__str__(self, indent='')SUAVE.Core.DataOrdered.DataOrdered
append(self, element)SUAVE.Input_Output.D3JS.Tree_Element.Tree_Element
SUAVE::Core::DataOrdered::DataOrdered.append(self, value, key=None)SUAVE.Core.DataOrdered.DataOrdered
children (defined in SUAVE.Input_Output.D3JS.Tree_Element.Tree_Element)SUAVE.Input_Output.D3JS.Tree_Element.Tree_Element
clear(self)SUAVE.Core.DataOrdered.DataOrdered
dataname(self)SUAVE.Core.DataOrdered.DataOrdered
deep_get(self, keys)SUAVE.Core.DataOrdered.DataOrdered
deep_set(self, keys, val)SUAVE.Core.DataOrdered.DataOrdered
get(self, k, d=None)SUAVE.Core.DataOrdered.DataOrdered
get_bases(self)SUAVE.Core.DataOrdered.DataOrdered
has_key(self, k)SUAVE.Core.DataOrdered.DataOrdered
items(self)SUAVE.Core.DataOrdered.DataOrdered
iteritems(self)SUAVE.Core.DataOrdered.DataOrdered
iterkeys(self)SUAVE.Core.DataOrdered.DataOrdered
itervalues(self)SUAVE.Core.DataOrdered.DataOrdered
keys(self)SUAVE.Core.DataOrdered.DataOrdered
name (defined in SUAVE.Input_Output.D3JS.Tree_Element.Tree_Element)SUAVE.Input_Output.D3JS.Tree_Element.Tree_Element
typestring(self)SUAVE.Core.DataOrdered.DataOrdered
update(self, other)SUAVE.Core.DataOrdered.DataOrdered
values(self)SUAVE.Core.DataOrdered.DataOrdered
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Input__Output_1_1D3JS_1_1Tree__Element_1_1Tree__Element.html b/_site/doxygen/classSUAVE_1_1Input__Output_1_1D3JS_1_1Tree__Element_1_1Tree__Element.html deleted file mode 100644 index ab843ad5..00000000 --- a/_site/doxygen/classSUAVE_1_1Input__Output_1_1D3JS_1_1Tree__Element_1_1Tree__Element.html +++ /dev/null @@ -1,302 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Input_Output.D3JS.Tree_Element.Tree_Element Class Reference - - - - - - - - - - - - - - - -
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SUAVE.Input_Output.D3JS.Tree_Element.Tree_Element Class Reference
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-Public Member Functions

def __init__ (self, name)
 
def append (self, element)
 
- Public Member Functions inherited from SUAVE.Core.DataOrdered.DataOrdered
def append (self, value, key=None)
 
def __defaults__ (self)
 
def __getitem__ (self, k)
 
def __new__ (cls, args, kwarg)
 
def __init__ (self, args, kwarg)
 
def __iter__ (self)
 
def __str__ (self, indent='')
 
def __repr__ (self)
 
def get_bases (self)
 
def typestring (self)
 
def dataname (self)
 
def deep_set (self, keys, val)
 
def deep_get (self, keys)
 
def update (self, other)
 
def __delattr__ (self, key)
 
def __eq__ (self, other)
 
def __len__ (self)
 
def __iter__ (self)
 
def __reduce__ (self)
 
def __setattr__ (self, key, value)
 
def __setitem__ (self, k, v)
 
def clear (self)
 
def get (self, k, d=None)
 
def has_key (self, k)
 
def keys (self)
 
def values (self)
 
def items (self)
 
def iterkeys (self)
 
def itervalues (self)
 
def iteritems (self)
 
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-Public Attributes

name
 
children
 
-

Detailed Description

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This is a tree element used in D3JS trees.
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-Assumptions:
-None
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-Source:
-N/A
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Constructor & Destructor Documentation

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◆ __init__()

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def SUAVE.Input_Output.D3JS.Tree_Element.Tree_Element.__init__ ( self,
 name 
)
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This sets default values.
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-Assumptions:
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-Source:
-N/A
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-Inputs:
-name    <string>
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-None
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Member Function Documentation

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◆ append()

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def SUAVE.Input_Output.D3JS.Tree_Element.Tree_Element.append ( self,
 element 
)
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This adds an element to self.children
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-Assumptions:
-None
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-Source:
-N/A
-    
-Inputs:
-element - an element to be added to self.children
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-Outputs:
-None
-    
-Properties Used:
-self.children (created if not already available)
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The documentation for this class was generated from the following file:
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  • /home/tim/Documents/SUAVE/trunk/SUAVE/Input_Output/D3JS/Tree_Element.py
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Input_Output.XML.Data.Attributes Class Reference
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Detailed Description

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Placeholder class. No functionality.
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-Assumptions:
-None
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-Source:
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The documentation for this class was generated from the following file:
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SUAVE.Input_Output.XML.Data.Data Class Reference
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-Public Member Functions

def __defaults__ (self)
 
def get_elements (self, tag)
 
def new_element (self, tag)
 
def __str__ (self, indent='')
 
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-Static Public Member Functions

def from_dict (data)
 
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-Public Attributes

tag
 
attributes
 
content
 
elements
 
-

Detailed Description

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This the XML data class used in SUAVE.
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-Assumptions:
-None
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-Source:
-N/A
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Member Function Documentation

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◆ __defaults__()

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def SUAVE.Input_Output.XML.Data.Data.__defaults__ ( self)
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Defaults for the data class.
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-Assumptions:
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◆ __str__()

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def SUAVE.Input_Output.XML.Data.Data.__str__ ( self,
 indent = '' 
)
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-
Determines how the class is shown in a string.
-    
-Assumptions:
-None
-    
-Source:
-N/A
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-Inputs:
-indent  <string> indent to be used
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-Outputs:
-args    <string>
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-Properties Used:
-N/A
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◆ from_dict()

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def SUAVE.Input_Output.XML.Data.Data.from_dict ( data)
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Gives a list of elements from data.
-    
-Assumptions:
-None
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-Source:
-N/A
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-Inputs:
-data    - data class to read
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-Outputs:
-results - list of elements
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-Properties Used:
-N/A
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def SUAVE.Input_Output.XML.Data.Data.get_elements ( self,
 tag 
)
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Gets elements with a given tag.
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-Assumptions:
-None
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-Source:
-N/A
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-Inputs:
-tag     - used to check which elements to return
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-Outputs:
-output  - list of matching elements
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-Properties Used:
-N/A
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◆ new_element()

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def SUAVE.Input_Output.XML.Data.Data.new_element ( self,
 tag 
)
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Creates a new element.
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-Assumptions:
-None
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-Source:
-N/A
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-Inputs:
-tag   - tag of the new element
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-Outputs:
-elem  - the new element
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-Properties Used:
-N/A
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The documentation for this class was generated from the following file:
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  • /home/tim/Documents/SUAVE/trunk/SUAVE/Input_Output/XML/Data.py
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-Public Member Functions

def __init__ (self)
 
def startElement (self, name, attrs)
 
def endElement (self, name)
 
def characters (self, content)
 
- - - - - - - - - -

-Public Attributes

root
 
stack
 
current
 
text_parts
 
-

Detailed Description

-
A class used to build the tree in an XML data structure
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-Assumptions:
-None
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-Source:
-N/A
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Constructor & Destructor Documentation

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◆ __init__()

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def SUAVE.Input_Output.XML.load.TreeBuilder.__init__ ( self)
-
-
Base values for the class to function.
-    
-Assumptions:
-None
-    
-Source:
-N/A
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-Inputs:
-None
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-Outputs:
-None
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-Properties Used:
-N/A
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Member Function Documentation

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◆ characters()

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def SUAVE.Input_Output.XML.load.TreeBuilder.characters ( self,
 content 
)
-
-
Appends content. This is used by an external package.
-    
-Assumptions:
-None
-    
-Source:
-N/A
-    
-Inputs:
-content
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-Outputs:
-None
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-Properties Used:
-self.text_parts
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◆ endElement()

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def SUAVE.Input_Output.XML.load.TreeBuilder.endElement ( self,
 name 
)
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-
End a new element. This is used by an external package.
-    
-Assumptions:
-None
-    
-Source:
-N/A
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-Inputs:
-None used
-    
-Outputs:
-None
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-Properties Used:
-self.
-  stack
-  current.
-    content
-    elements
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◆ startElement()

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def SUAVE.Input_Output.XML.load.TreeBuilder.startElement ( self,
 name,
 attrs 
)
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Starts a new element. This is used by an external package.
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-Assumptions:
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-
-
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The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Input_Output/XML/load.py
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- - - - - - - - -
-
SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Methods.Aerodynamics.AVL.Data.Aircraft.Aircraft Member List
-
-
- -

This is the complete list of members for SUAVE.Methods.Aerodynamics.AVL.Data.Aircraft.Aircraft, including all inherited members.

- - - - - - - - - - - - - - - - - - - - - - - - - - -
__defaults__(self)SUAVE.Methods.Aerodynamics.AVL.Data.Aircraft.Aircraft
__delattr__(self, k)SUAVE.Core.Data.Data
__getattribute__(self, k)SUAVE.Core.Data.Data
__init__(self, args, kwarg)SUAVE.Core.Data.Data
__iter__(self)SUAVE.Core.Data.Data
__new__(cls, args, kwarg)SUAVE.Core.Data.Data
__setattr__(self, k, v)SUAVE.Core.Data.Data
__str__(self, indent='')SUAVE.Core.Data.Data
append(self, value, key=None)SUAVE.Core.Data.Data
append_body(self, body)SUAVE.Methods.Aerodynamics.AVL.Data.Aircraft.Aircraft
append_wing(self, wing)SUAVE.Methods.Aerodynamics.AVL.Data.Aircraft.Aircraft
bodies (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Aircraft.Aircraft)SUAVE.Methods.Aerodynamics.AVL.Data.Aircraft.Aircraft
dataname(self)SUAVE.Core.Data.Data
deep_get(self, keys)SUAVE.Core.Data.Data
deep_set(self, keys, val)SUAVE.Core.Data.Data
do_recursive(self, method, other=None, default=None)SUAVE.Core.Data.Data
get_bases(self)SUAVE.Core.Data.Data
itervalues(self)SUAVE.Core.Data.Data
pack_array(self, output='vector')SUAVE.Core.Data.Data
tag (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Aircraft.Aircraft)SUAVE.Methods.Aerodynamics.AVL.Data.Aircraft.Aircraft
typestring(self)SUAVE.Core.Data.Data
unpack_array(self, M)SUAVE.Core.Data.Data
update(self, other)SUAVE.Core.Data.Data
values(self)SUAVE.Core.Data.Data
wings (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Aircraft.Aircraft)SUAVE.Methods.Aerodynamics.AVL.Data.Aircraft.Aircraft
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Aircraft_1_1Aircraft.html b/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Aircraft_1_1Aircraft.html deleted file mode 100644 index 7dcc9cf4..00000000 --- a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Aircraft_1_1Aircraft.html +++ /dev/null @@ -1,329 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Methods.Aerodynamics.AVL.Data.Aircraft.Aircraft Class Reference - - - - - - - - - - - - - - - -
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- - - - - - - - -
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SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
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- -
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- -
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SUAVE.Methods.Aerodynamics.AVL.Data.Aircraft.Aircraft Class Reference
-
-
-
-Inheritance diagram for SUAVE.Methods.Aerodynamics.AVL.Data.Aircraft.Aircraft:
-
-
- - -SUAVE.Core.Data.Data - -
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def append_wing (self, wing)
 
def append_body (self, body)
 
- Public Member Functions inherited from SUAVE.Core.Data.Data
def __getattribute__ (self, k)
 
def __setattr__ (self, k, v)
 
def __delattr__ (self, k)
 
def __defaults__ (self)
 
def __new__ (cls, args, kwarg)
 
def typestring (self)
 
def dataname (self)
 
def __str__ (self, indent='')
 
def __init__ (self, args, kwarg)
 
def __iter__ (self)
 
def itervalues (self)
 
def values (self)
 
def update (self, other)
 
def get_bases (self)
 
def append (self, value, key=None)
 
def deep_set (self, keys, val)
 
def deep_get (self, keys)
 
def pack_array (self, output='vector')
 
def unpack_array (self, M)
 
def do_recursive (self, method, other=None, default=None)
 
- - - - - - - -

-Public Attributes

tag
 
wings
 
bodies
 
-

Detailed Description

-
A data class defining the entire AVL aircraft geometry
-
-Assumptions:
-    None
-
-Source:
-    None
-
-Inputs:
-    None
-
-Outputs:
-    None
-
-Properties Used:
-    N/A
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Methods.Aerodynamics.AVL.Data.Aircraft.Aircraft.__defaults__ ( self)
-
-
Defines the data structure and defaults of aircraft classes
-
-Assumptions:
-    None
-
-Source:
-    None
-
-Inputs:
-    None
-
-Outputs:
-    None
-
-Properties Used:
-    N/A
-
-
-
- -

◆ append_body()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Aerodynamics.AVL.Data.Aircraft.Aircraft.append_body ( self,
 body 
)
-
-
Appends body geometry onto aircraft class
-
-Assumptions:
-    None
-
-Source:
-    None
-
-Inputs:
-    None
-
-Outputs:
-    None
-
-Properties Used:
-    N/A
-
-
-
- -

◆ append_wing()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Aerodynamics.AVL.Data.Aircraft.Aircraft.append_wing ( self,
 wing 
)
-
-
Appends wing geometry onto aircraft class
-
-Assumptions:
-    None
-
-Source:
-    None
-
-Inputs:
-    None
-
-Outputs:
-    None
-
-Properties Used:
-    N/A
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Methods/Aerodynamics/AVL/Data/Aircraft.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Aircraft_1_1Aircraft.js b/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Aircraft_1_1Aircraft.js deleted file mode 100644 index d7308d80..00000000 --- a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Aircraft_1_1Aircraft.js +++ /dev/null @@ -1,9 +0,0 @@ -var classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Aircraft_1_1Aircraft = -[ - [ "__defaults__", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Aircraft_1_1Aircraft.html#a8f24d7640e88f242ffece9f7f877ada1", null ], - [ "append_body", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Aircraft_1_1Aircraft.html#af02fd813837694b85b3b1634b880527e", null ], - [ "append_wing", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Aircraft_1_1Aircraft.html#a79ebe6aa92ad545d307639d3d6cd05a7", null ], - [ "bodies", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Aircraft_1_1Aircraft.html#a423b44bdf62a70909503f2a25a9a6a3e", null ], - [ "tag", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Aircraft_1_1Aircraft.html#adcd5f96656a2f6207669d96bba31bafa", null ], - [ "wings", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Aircraft_1_1Aircraft.html#a831c6646bbbf90fabf65189030d70d49", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Aircraft_1_1Aircraft.png b/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Aircraft_1_1Aircraft.png deleted file mode 100644 index 8e27e9e3..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Aircraft_1_1Aircraft.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Body_1_1Body-members.html b/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Body_1_1Body-members.html deleted file mode 100644 index 3b60c818..00000000 --- a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Body_1_1Body-members.html +++ /dev/null @@ -1,141 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Methods.Aerodynamics.AVL.Data.Body.Body Member List
-
-
- -

This is the complete list of members for SUAVE.Methods.Aerodynamics.AVL.Data.Body.Body, including all inherited members.

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__defaults__(self)SUAVE.Methods.Aerodynamics.AVL.Data.Body.Body
__delattr__(self, k)SUAVE.Core.Data.Data
__getattribute__(self, k)SUAVE.Core.Data.Data
__init__(self, args, kwarg)SUAVE.Core.Data.Data
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append_section(self, section, orientation='Horizontal')SUAVE.Methods.Aerodynamics.AVL.Data.Body.Body
configuration (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Body.Body)SUAVE.Methods.Aerodynamics.AVL.Data.Body.Body
dataname(self)SUAVE.Core.Data.Data
deep_get(self, keys)SUAVE.Core.Data.Data
deep_set(self, keys, val)SUAVE.Core.Data.Data
do_recursive(self, method, other=None, default=None)SUAVE.Core.Data.Data
get_bases(self)SUAVE.Core.Data.Data
heights (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Body.Body)SUAVE.Methods.Aerodynamics.AVL.Data.Body.Body
itervalues(self)SUAVE.Core.Data.Data
lengths (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Body.Body)SUAVE.Methods.Aerodynamics.AVL.Data.Body.Body
origin (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Body.Body)SUAVE.Methods.Aerodynamics.AVL.Data.Body.Body
pack_array(self, output='vector')SUAVE.Core.Data.Data
sections (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Body.Body)SUAVE.Methods.Aerodynamics.AVL.Data.Body.Body
symmetric (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Body.Body)SUAVE.Methods.Aerodynamics.AVL.Data.Body.Body
tag (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Body.Body)SUAVE.Methods.Aerodynamics.AVL.Data.Body.Body
typestring(self)SUAVE.Core.Data.Data
unpack_array(self, M)SUAVE.Core.Data.Data
update(self, other)SUAVE.Core.Data.Data
values(self)SUAVE.Core.Data.Data
widths (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Body.Body)SUAVE.Methods.Aerodynamics.AVL.Data.Body.Body
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Body_1_1Body.html b/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Body_1_1Body.html deleted file mode 100644 index 66689a77..00000000 --- a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Body_1_1Body.html +++ /dev/null @@ -1,306 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Methods.Aerodynamics.AVL.Data.Body.Body Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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-
- -
-
-
- -
- -
-
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- -
-
SUAVE.Methods.Aerodynamics.AVL.Data.Body.Body Class Reference
-
-
-
-Inheritance diagram for SUAVE.Methods.Aerodynamics.AVL.Data.Body.Body:
-
-
- - -SUAVE.Core.Data.Data - -
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def append_section (self, section, orientation='Horizontal')
 
- Public Member Functions inherited from SUAVE.Core.Data.Data
def __getattribute__ (self, k)
 
def __setattr__ (self, k, v)
 
def __delattr__ (self, k)
 
def __defaults__ (self)
 
def __new__ (cls, args, kwarg)
 
def typestring (self)
 
def dataname (self)
 
def __str__ (self, indent='')
 
def __init__ (self, args, kwarg)
 
def __iter__ (self)
 
def itervalues (self)
 
def values (self)
 
def update (self, other)
 
def get_bases (self)
 
def append (self, value, key=None)
 
def deep_set (self, keys, val)
 
def deep_get (self, keys)
 
def pack_array (self, output='vector')
 
def unpack_array (self, M)
 
def do_recursive (self, method, other=None, default=None)
 
- - - - - - - - - - - - - - - - - -

-Public Attributes

tag
 
symmetric
 
origin
 
lengths
 
widths
 
heights
 
sections
 
configuration
 
-

Detailed Description

-
A data class defining the parameters of a fuselage or other body modeled
-by side and planform projections arranged in a plus (+) shape (when viewed from
-the front).
-        
-Assumptions:
-    None
-    
-Source:
-    None
-
-Inputs:
-    None
-
-Outputs:
-    None
-
-Properties Used:
-    N/A
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Methods.Aerodynamics.AVL.Data.Body.Body.__defaults__ ( self)
-
-
Defines the data structure and defaults for aircraft body geometry 
-    
-Assumptions:
-    None
-
-Source:
-    None
-
-Inputs:
-    None
-
-Outputs:
-    None
-
-Properties Used:
-    N/A
-
-
-
- -

◆ append_section()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Aerodynamics.AVL.Data.Body.Body.append_section ( self,
 section,
 orientation = 'Horizontal' 
)
-
-
Adds a section to the body vertical or horizontal segment 
-    
-Assumptions:
-    None
-
-Source:
-    None
-
-Inputs:
-    None
-
-Outputs:
-    None
-
-Properties Used:
-    N/A
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Methods/Aerodynamics/AVL/Data/Body.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Body_1_1Body.js b/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Body_1_1Body.js deleted file mode 100644 index 0b1f3bfb..00000000 --- a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Body_1_1Body.js +++ /dev/null @@ -1,13 +0,0 @@ -var classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Body_1_1Body = -[ - [ "__defaults__", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Body_1_1Body.html#a34f75c1e2e5a28f604d15b09beaf2a15", null ], - [ "append_section", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Body_1_1Body.html#a64fb80a7b9d208ad13679085aa264a57", null ], - [ "configuration", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Body_1_1Body.html#af9e8e12ba0881bffbb07afb16d616f68", null ], - [ "heights", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Body_1_1Body.html#ada7e11962bdb536a2cf5af95a515b9b3", null ], - [ "lengths", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Body_1_1Body.html#ad4d098f93ed20734c6bef3badfebbfc8", null ], - [ "origin", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Body_1_1Body.html#a185da31a1271ef73878185f0a902d0c9", null ], - [ "sections", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Body_1_1Body.html#a6c2ea2b797ff297724b0baa3bb60227a", null ], - [ "symmetric", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Body_1_1Body.html#a8fb35cc86ed4023e6808d124f79d947c", null ], - [ "tag", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Body_1_1Body.html#a9df357e14851637f29218a1254c1909a", null ], - [ "widths", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Body_1_1Body.html#a476ac73c5a34ec5b6b1f77e2b71d95e9", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Body_1_1Body.png b/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Body_1_1Body.png deleted file mode 100644 index cb4ded0e..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Body_1_1Body.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Container-members.html b/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Container-members.html deleted file mode 100644 index 863174f4..00000000 --- a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Container-members.html +++ /dev/null @@ -1,143 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Container Member List
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- -

This is the complete list of members for SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Container, including all inherited members.

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__defaults__(self)SUAVE.Core.DataOrdered.DataOrdered
__delattr__(self, key)SUAVE.Core.DataOrdered.DataOrdered
__eq__(self, other)SUAVE.Core.DataOrdered.DataOrdered
__getitem__(self, k)SUAVE.Core.DataOrdered.DataOrdered
__init__(self, args, kwarg)SUAVE.Core.DataOrdered.DataOrdered
__iter__(self)SUAVE.Core.DataOrdered.DataOrdered
__iter__(self)SUAVE.Core.DataOrdered.DataOrdered
__len__(self)SUAVE.Core.DataOrdered.DataOrdered
__new__(cls, args, kwarg)SUAVE.Core.DataOrdered.DataOrdered
__reduce__(self)SUAVE.Core.DataOrdered.DataOrdered
__repr__(self)SUAVE.Core.DataOrdered.DataOrdered
__setattr__(self, key, value)SUAVE.Core.DataOrdered.DataOrdered
__setitem__(self, k, v)SUAVE.Core.DataOrdered.DataOrdered
__str__(self, indent='')SUAVE.Core.DataOrdered.DataOrdered
append(self, value, key=None)SUAVE.Core.DataOrdered.DataOrdered
append_case(self, case)SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Container
clear(self)SUAVE.Core.DataOrdered.DataOrdered
dataname(self)SUAVE.Core.DataOrdered.DataOrdered
deep_get(self, keys)SUAVE.Core.DataOrdered.DataOrdered
deep_set(self, keys, val)SUAVE.Core.DataOrdered.DataOrdered
get(self, k, d=None)SUAVE.Core.DataOrdered.DataOrdered
get_bases(self)SUAVE.Core.DataOrdered.DataOrdered
has_key(self, k)SUAVE.Core.DataOrdered.DataOrdered
items(self)SUAVE.Core.DataOrdered.DataOrdered
iteritems(self)SUAVE.Core.DataOrdered.DataOrdered
iterkeys(self)SUAVE.Core.DataOrdered.DataOrdered
itervalues(self)SUAVE.Core.DataOrdered.DataOrdered
keys(self)SUAVE.Core.DataOrdered.DataOrdered
typestring(self)SUAVE.Core.DataOrdered.DataOrdered
update(self, other)SUAVE.Core.DataOrdered.DataOrdered
values(self)SUAVE.Core.DataOrdered.DataOrdered
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Container.html b/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Container.html deleted file mode 100644 index 1eced67e..00000000 --- a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Container.html +++ /dev/null @@ -1,253 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Container Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Container Class Reference
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-
-Inheritance diagram for SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Container:
-
-
- - -SUAVE.Core.DataOrdered.DataOrdered - -
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def append_case (self, case)
 
- Public Member Functions inherited from SUAVE.Core.DataOrdered.DataOrdered
def append (self, value, key=None)
 
def __defaults__ (self)
 
def __getitem__ (self, k)
 
def __new__ (cls, args, kwarg)
 
def __init__ (self, args, kwarg)
 
def __iter__ (self)
 
def __str__ (self, indent='')
 
def __repr__ (self)
 
def get_bases (self)
 
def typestring (self)
 
def dataname (self)
 
def deep_set (self, keys, val)
 
def deep_get (self, keys)
 
def update (self, other)
 
def __delattr__ (self, key)
 
def __eq__ (self, other)
 
def __len__ (self)
 
def __iter__ (self)
 
def __reduce__ (self)
 
def __setattr__ (self, key, value)
 
def __setitem__ (self, k, v)
 
def clear (self)
 
def get (self, k, d=None)
 
def has_key (self, k)
 
def keys (self)
 
def values (self)
 
def items (self)
 
def iterkeys (self)
 
def itervalues (self)
 
def iteritems (self)
 
-

Detailed Description

-
A data class for the addition of a cases to the set of run cases
-
-Assumptions:
-    None
-    
-Source:
-    None
-
-Inputs:
-    None
-
-Outputs:
-    None
-
-Properties Used:
-    N/A
-

Member Function Documentation

- -

◆ append_case()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Container.append_case ( self,
 case 
)
-
-
Adds a case to the set of run cases "
-
-    Assumptions:
-None
-    
-    Source:
-None
-    
-    Inputs:
-None
-    
-    Outputs:
-None
-    
-    Properties Used:
-N/A
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Methods/Aerodynamics/AVL/Data/Cases.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Container.js b/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Container.js deleted file mode 100644 index 753e9d3f..00000000 --- a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Container.js +++ /dev/null @@ -1,4 +0,0 @@ -var classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Container = -[ - [ "append_case", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Container.html#aff65fa3e29a58d9023c79b30da40d2df", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Container.png b/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Container.png deleted file mode 100644 index 4d0ee189..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Container.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Run__Case-members.html b/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Run__Case-members.html deleted file mode 100644 index 8d277032..00000000 --- a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Run__Case-members.html +++ /dev/null @@ -1,140 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Run_Case Member List
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This is the complete list of members for SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Run_Case, including all inherited members.

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__defaults__(self)SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Run_Case
__delattr__(self, k)SUAVE.Core.Data.Data
__getattribute__(self, k)SUAVE.Core.Data.Data
__init__(self, args, kwarg)SUAVE.Core.Data.Data
__iter__(self)SUAVE.Core.Data.Data
__new__(cls, args, kwarg)SUAVE.Core.Data.Data
__setattr__(self, k, v)SUAVE.Core.Data.Data
__str__(self, indent='')SUAVE.Core.Data.Data
append(self, value, key=None)SUAVE.Core.Data.Data
append_control_deflection(self, control_tag, deflection)SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Run_Case
conditions (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Run_Case)SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Run_Case
dataname(self)SUAVE.Core.Data.Data
deep_get(self, keys)SUAVE.Core.Data.Data
deep_set(self, keys, val)SUAVE.Core.Data.Data
do_recursive(self, method, other=None, default=None)SUAVE.Core.Data.Data
eigen_result_filename (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Run_Case)SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Run_Case
get_bases(self)SUAVE.Core.Data.Data
index (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Run_Case)SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Run_Case
itervalues(self)SUAVE.Core.Data.Data
mass (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Run_Case)SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Run_Case
pack_array(self, output='vector')SUAVE.Core.Data.Data
result_filename (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Run_Case)SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Run_Case
stability_and_control (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Run_Case)SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Run_Case
tag (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Run_Case)SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Run_Case
typestring(self)SUAVE.Core.Data.Data
unpack_array(self, M)SUAVE.Core.Data.Data
update(self, other)SUAVE.Core.Data.Data
values(self)SUAVE.Core.Data.Data
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Run__Case.html b/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Run__Case.html deleted file mode 100644 index faba50b6..00000000 --- a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Run__Case.html +++ /dev/null @@ -1,302 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Run_Case Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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- -
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SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Run_Case Class Reference
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-
-Inheritance diagram for SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Run_Case:
-
-
- - -SUAVE.Core.Data.Data - -
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def append_control_deflection (self, control_tag, deflection)
 
- Public Member Functions inherited from SUAVE.Core.Data.Data
def __getattribute__ (self, k)
 
def __setattr__ (self, k, v)
 
def __delattr__ (self, k)
 
def __defaults__ (self)
 
def __new__ (cls, args, kwarg)
 
def typestring (self)
 
def dataname (self)
 
def __str__ (self, indent='')
 
def __init__ (self, args, kwarg)
 
def __iter__ (self)
 
def itervalues (self)
 
def values (self)
 
def update (self, other)
 
def get_bases (self)
 
def append (self, value, key=None)
 
def deep_set (self, keys, val)
 
def deep_get (self, keys)
 
def pack_array (self, output='vector')
 
def unpack_array (self, M)
 
def do_recursive (self, method, other=None, default=None)
 
- - - - - - - - - - - - - - - -

-Public Attributes

index
 
tag
 
mass
 
conditions
 
stability_and_control
 
result_filename
 
eigen_result_filename
 
-

Detailed Description

-
A data class defining the parameters for the analysis cases 
-including angle of attack and mach number 
-
-Assumptions:
-    None
-    
-Source:
-    None
-
-Inputs:
-    None
-
-Outputs:
-    None
-
-Properties Used:
-    N/A
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Run_Case.__defaults__ ( self)
-
-
Defines the data structure and defaults of aerodynamics coefficients, 
-body derivatives and stability derivatives   
-
-Assumptions:
-    None
-    
-Source:
-    None
-    
-Inputs:
-    None
-    
-Outputs:
-    None
-    
-Properties Used:
-    N/A
-
-
-
- -

◆ append_control_deflection()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Run_Case.append_control_deflection ( self,
 control_tag,
 deflection 
)
-
-
Adds a control deflection case 
-
-    Assumptions:
-None
-    
-    Source:
-None
-    
-    Inputs:
-None
-    
-    Outputs:
-None
-    
-    Properties Used:
-N/A
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Methods/Aerodynamics/AVL/Data/Cases.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Run__Case.js b/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Run__Case.js deleted file mode 100644 index c8c72c46..00000000 --- a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Run__Case.js +++ /dev/null @@ -1,12 +0,0 @@ -var classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Run__Case = -[ - [ "__defaults__", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Run__Case.html#a6a9108165be8c60598d8040c1b3c5203", null ], - [ "append_control_deflection", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Run__Case.html#a0204b074d5dad2d32d5b221ad922dc2a", null ], - [ "conditions", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Run__Case.html#a3eddb7985cac1df2f93fd4c90b5d14f2", null ], - [ "eigen_result_filename", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Run__Case.html#ae88894a124bdf653ae64543605114198", null ], - [ "index", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Run__Case.html#a5271bb99f849f5f6dca450f1f293023a", null ], - [ "mass", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Run__Case.html#a92517a94d9e4bb763fceaca80c3a4b25", null ], - [ "result_filename", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Run__Case.html#a8cbb7d2798c08a5e631204180b4bd9c2", null ], - [ "stability_and_control", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Run__Case.html#a5958cefee53f8e33db6a32520c7b7f91", null ], - [ "tag", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Run__Case.html#a94540c93dbd0009db6b3b022c9a3fbdc", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Run__Case.png b/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Run__Case.png deleted file mode 100644 index 1a3e6ce8..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Run__Case.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Configuration_1_1Configuration-members.html b/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Configuration_1_1Configuration-members.html deleted file mode 100644 index d3027098..00000000 --- a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Configuration_1_1Configuration-members.html +++ /dev/null @@ -1,137 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Methods.Aerodynamics.AVL.Data.Configuration.Configuration Member List
-
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- -

This is the complete list of members for SUAVE.Methods.Aerodynamics.AVL.Data.Configuration.Configuration, including all inherited members.

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__defaults__(self)SUAVE.Methods.Aerodynamics.AVL.Data.Configuration.Configuration
__delattr__(self, k)SUAVE.Core.Data.Data
__getattribute__(self, k)SUAVE.Core.Data.Data
__init__(self, args, kwarg)SUAVE.Core.Data.Data
__iter__(self)SUAVE.Core.Data.Data
__new__(cls, args, kwarg)SUAVE.Core.Data.Data
__setattr__(self, k, v)SUAVE.Core.Data.Data
__str__(self, indent='')SUAVE.Core.Data.Data
append(self, value, key=None)SUAVE.Core.Data.Data
dataname(self)SUAVE.Core.Data.Data
deep_get(self, keys)SUAVE.Core.Data.Data
deep_set(self, keys, val)SUAVE.Core.Data.Data
do_recursive(self, method, other=None, default=None)SUAVE.Core.Data.Data
get_bases(self)SUAVE.Core.Data.Data
itervalues(self)SUAVE.Core.Data.Data
mass_properties (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Configuration.Configuration)SUAVE.Methods.Aerodynamics.AVL.Data.Configuration.Configuration
pack_array(self, output='vector')SUAVE.Core.Data.Data
parasite_drag (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Configuration.Configuration)SUAVE.Methods.Aerodynamics.AVL.Data.Configuration.Configuration
reference_values (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Configuration.Configuration)SUAVE.Methods.Aerodynamics.AVL.Data.Configuration.Configuration
symmetry_settings (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Configuration.Configuration)SUAVE.Methods.Aerodynamics.AVL.Data.Configuration.Configuration
tag (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Configuration.Configuration)SUAVE.Methods.Aerodynamics.AVL.Data.Configuration.Configuration
typestring(self)SUAVE.Core.Data.Data
unpack_array(self, M)SUAVE.Core.Data.Data
update(self, other)SUAVE.Core.Data.Data
values(self)SUAVE.Core.Data.Data
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Configuration_1_1Configuration.html b/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Configuration_1_1Configuration.html deleted file mode 100644 index 3f300b3f..00000000 --- a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Configuration_1_1Configuration.html +++ /dev/null @@ -1,245 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Methods.Aerodynamics.AVL.Data.Configuration.Configuration Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
-
- - - -
-
- -
-
-
- -
- -
-
- - -
- -
- -
- -
-
SUAVE.Methods.Aerodynamics.AVL.Data.Configuration.Configuration Class Reference
-
-
-
-Inheritance diagram for SUAVE.Methods.Aerodynamics.AVL.Data.Configuration.Configuration:
-
-
- - -SUAVE.Core.Data.Data - -
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Core.Data.Data
def __getattribute__ (self, k)
 
def __setattr__ (self, k, v)
 
def __delattr__ (self, k)
 
def __defaults__ (self)
 
def __new__ (cls, args, kwarg)
 
def typestring (self)
 
def dataname (self)
 
def __str__ (self, indent='')
 
def __init__ (self, args, kwarg)
 
def __iter__ (self)
 
def itervalues (self)
 
def values (self)
 
def update (self, other)
 
def get_bases (self)
 
def append (self, value, key=None)
 
def deep_set (self, keys, val)
 
def deep_get (self, keys)
 
def pack_array (self, output='vector')
 
def unpack_array (self, M)
 
def do_recursive (self, method, other=None, default=None)
 
- - - - - - - - - - - -

-Public Attributes

tag
 
parasite_drag
 
reference_values
 
mass_properties
 
symmetry_settings
 
-

Detailed Description

-
A data class defining the reference parameters of the aircraft geoemtry and 
-flight configuration 
-
-Assumptions:
-    None
-
-Source:
-    None
-
-Inputs:
-    None
-
-Outputs:
-    None
-
-Properties Used:
-    N/A
-

Member Function Documentation

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◆ __defaults__()

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def SUAVE.Methods.Aerodynamics.AVL.Data.Configuration.Configuration.__defaults__ ( self)
-
-
Defines the data structure and defaults for mass properties of the aircraft 
-in AVL
-
-Assumptions:
-    None
-
-Source:
-    None
-
-Inputs:
-    None
-
-Outputs:
-    None
-
-Properties Used:
-    N/A
-
-
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-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Methods/Aerodynamics/AVL/Data/Configuration.py
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Configuration_1_1Configuration.js b/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Configuration_1_1Configuration.js deleted file mode 100644 index a09a5597..00000000 --- a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Configuration_1_1Configuration.js +++ /dev/null @@ -1,9 +0,0 @@ -var classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Configuration_1_1Configuration = -[ - [ "__defaults__", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Configuration_1_1Configuration.html#ac0e5a8864eb37a4ee4d838e8ff0adcc7", null ], - [ "mass_properties", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Configuration_1_1Configuration.html#ac29cde4fac6d7c7975ce525ea50d82ca", null ], - [ "parasite_drag", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Configuration_1_1Configuration.html#ad6317e87913bc6e77b45884faa900d50", null ], - [ "reference_values", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Configuration_1_1Configuration.html#ab7fd500649104731b3aebd87b351b500", null ], - [ "symmetry_settings", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Configuration_1_1Configuration.html#a8ab4b95690bfba68e9b1be72d70e4f9f", null ], - [ "tag", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Configuration_1_1Configuration.html#aa98f6f29b565c1e59f3b9790ae55a8f0", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Configuration_1_1Configuration.png b/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Configuration_1_1Configuration.png deleted file mode 100644 index 9fdb1a04..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Configuration_1_1Configuration.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Inputs_1_1Inputs-members.html b/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Inputs_1_1Inputs-members.html deleted file mode 100644 index 24aea5db..00000000 --- a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Inputs_1_1Inputs-members.html +++ /dev/null @@ -1,137 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Methods.Aerodynamics.AVL.Data.Inputs.Inputs Member List
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This is the complete list of members for SUAVE.Methods.Aerodynamics.AVL.Data.Inputs.Inputs, including all inherited members.

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__defaults__(self)SUAVE.Methods.Aerodynamics.AVL.Data.Inputs.Inputs
__delattr__(self, k)SUAVE.Core.Data.Data
__getattribute__(self, k)SUAVE.Core.Data.Data
__init__(self, args, kwarg)SUAVE.Core.Data.Data
__iter__(self)SUAVE.Core.Data.Data
__new__(cls, args, kwarg)SUAVE.Core.Data.Data
__setattr__(self, k, v)SUAVE.Core.Data.Data
__str__(self, indent='')SUAVE.Core.Data.Data
aircraft (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Inputs.Inputs)SUAVE.Methods.Aerodynamics.AVL.Data.Inputs.Inputs
append(self, value, key=None)SUAVE.Core.Data.Data
avl_bin_path (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Inputs.Inputs)SUAVE.Methods.Aerodynamics.AVL.Data.Inputs.Inputs
cases (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Inputs.Inputs)SUAVE.Methods.Aerodynamics.AVL.Data.Inputs.Inputs
configuration (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Inputs.Inputs)SUAVE.Methods.Aerodynamics.AVL.Data.Inputs.Inputs
dataname(self)SUAVE.Core.Data.Data
deep_get(self, keys)SUAVE.Core.Data.Data
deep_set(self, keys, val)SUAVE.Core.Data.Data
do_recursive(self, method, other=None, default=None)SUAVE.Core.Data.Data
get_bases(self)SUAVE.Core.Data.Data
input_files (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Inputs.Inputs)SUAVE.Methods.Aerodynamics.AVL.Data.Inputs.Inputs
itervalues(self)SUAVE.Core.Data.Data
pack_array(self, output='vector')SUAVE.Core.Data.Data
typestring(self)SUAVE.Core.Data.Data
unpack_array(self, M)SUAVE.Core.Data.Data
update(self, other)SUAVE.Core.Data.Data
values(self)SUAVE.Core.Data.Data
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Inputs_1_1Inputs.html b/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Inputs_1_1Inputs.html deleted file mode 100644 index eda9c7b0..00000000 --- a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Inputs_1_1Inputs.html +++ /dev/null @@ -1,243 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Methods.Aerodynamics.AVL.Data.Inputs.Inputs Class Reference - - - - - - - - - - - - - - - -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Methods.Aerodynamics.AVL.Data.Inputs.Inputs Class Reference
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-Inheritance diagram for SUAVE.Methods.Aerodynamics.AVL.Data.Inputs.Inputs:
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-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Core.Data.Data
def __getattribute__ (self, k)
 
def __setattr__ (self, k, v)
 
def __delattr__ (self, k)
 
def __defaults__ (self)
 
def __new__ (cls, args, kwarg)
 
def typestring (self)
 
def dataname (self)
 
def __str__ (self, indent='')
 
def __init__ (self, args, kwarg)
 
def __iter__ (self)
 
def itervalues (self)
 
def values (self)
 
def update (self, other)
 
def get_bases (self)
 
def append (self, value, key=None)
 
def deep_set (self, keys, val)
 
def deep_get (self, keys)
 
def pack_array (self, output='vector')
 
def unpack_array (self, M)
 
def do_recursive (self, method, other=None, default=None)
 
- - - - - - - - - - - -

-Public Attributes

configuration
 
aircraft
 
cases
 
avl_bin_path
 
input_files
 
-

Detailed Description

-
A data class defining filenames for the AVL executable
-
-Assumptions:
-    None
-
-Source:
-    None
-
-Inputs:
-    None
-
-Outputs:
-    None
-
-Properties Used:
-    N/A
-

Member Function Documentation

- -

◆ __defaults__()

- -
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- - - - - - - - -
def SUAVE.Methods.Aerodynamics.AVL.Data.Inputs.Inputs.__defaults__ ( self)
-
-
Defines the data structure  and defaults of aircraft configuration and cases 
-    
-Assumptions:
-    None
-
-Source:
-    None
-
-Inputs:
-    None
-
-Outputs:
-    None
-
-Properties Used:
-    N/A
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Methods/Aerodynamics/AVL/Data/Inputs.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Inputs_1_1Inputs.js b/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Inputs_1_1Inputs.js deleted file mode 100644 index be9d16ec..00000000 --- a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Inputs_1_1Inputs.js +++ /dev/null @@ -1,9 +0,0 @@ -var classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Inputs_1_1Inputs = -[ - [ "__defaults__", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Inputs_1_1Inputs.html#a4158c4be1d0ce919aa33641b1ae084a8", null ], - [ "aircraft", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Inputs_1_1Inputs.html#a805ced1f4d58c5341853aabc5271f46c", null ], - [ "avl_bin_path", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Inputs_1_1Inputs.html#aada0cea25029e415f155fe0480fec1c6", null ], - [ "cases", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Inputs_1_1Inputs.html#a50e474dcbb9e39e91e2799586fe2cfa5", null ], - [ "configuration", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Inputs_1_1Inputs.html#ab55d4b081fa697bd8c74c7fccd00d3b8", null ], - [ "input_files", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Inputs_1_1Inputs.html#a95c24e5276665b97da9a46f0417ee3f4", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Inputs_1_1Inputs.png b/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Inputs_1_1Inputs.png deleted file mode 100644 index b32fc4bf..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Inputs_1_1Inputs.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Results_1_1Results-members.html b/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Results_1_1Results-members.html deleted file mode 100644 index 34eab824..00000000 --- a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Results_1_1Results-members.html +++ /dev/null @@ -1,134 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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- - - - - - diff --git a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Results_1_1Results.html b/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Results_1_1Results.html deleted file mode 100644 index 5bc78de9..00000000 --- a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Results_1_1Results.html +++ /dev/null @@ -1,234 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Methods.Aerodynamics.AVL.Data.Results.Results Class Reference - - - - - - - - - - - - - - - -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Methods.Aerodynamics.AVL.Data.Results.Results Class Reference
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-Inheritance diagram for SUAVE.Methods.Aerodynamics.AVL.Data.Results.Results:
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-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Core.Data.Data
def __getattribute__ (self, k)
 
def __setattr__ (self, k, v)
 
def __delattr__ (self, k)
 
def __defaults__ (self)
 
def __new__ (cls, args, kwarg)
 
def typestring (self)
 
def dataname (self)
 
def __str__ (self, indent='')
 
def __init__ (self, args, kwarg)
 
def __iter__ (self)
 
def itervalues (self)
 
def values (self)
 
def update (self, other)
 
def get_bases (self)
 
def append (self, value, key=None)
 
def deep_set (self, keys, val)
 
def deep_get (self, keys)
 
def pack_array (self, output='vector')
 
def unpack_array (self, M)
 
def do_recursive (self, method, other=None, default=None)
 
- - - - - -

-Public Attributes

aerodynamics
 
stability
 
-

Detailed Description

-
A data class defining aerodynamics and stability results 
-
-Assumptions:
-    None
-    
-Source:
-    None
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-Inputs:
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-Outputs:
-    None
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-Properties Used:
-    N/A
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Member Function Documentation

- -

◆ __defaults__()

- -
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def SUAVE.Methods.Aerodynamics.AVL.Data.Results.Results.__defaults__ ( self)
-
-
Defining data structure  and defaults for aerodynamics and stabilty results 
-    
-Assumptions:
-    None
-    
-Source:
-    None
-    
-Inputs:
-    None
-    
-Outputs:
-    None
-    
-Properties Used:
-    N/A
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Methods/Aerodynamics/AVL/Data/Results.py
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-
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Results_1_1Results.js b/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Results_1_1Results.js deleted file mode 100644 index de9b47d5..00000000 --- a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Results_1_1Results.js +++ /dev/null @@ -1,6 +0,0 @@ -var classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Results_1_1Results = -[ - [ "__defaults__", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Results_1_1Results.html#a89aecce3b18d27e1c19ec3ca3f4d382f", null ], - [ "aerodynamics", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Results_1_1Results.html#a4ad2c8f107349d23d3e0422d55c3b42e", null ], - [ "stability", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Results_1_1Results.html#a430468bfa01067a3d3873fdbb4f107fe", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Results_1_1Results.png b/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Results_1_1Results.png deleted file mode 100644 index 1b6e1a9e..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Results_1_1Results.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Settings_1_1AVL__Discretization__Settings-members.html b/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Settings_1_1AVL__Discretization__Settings-members.html deleted file mode 100644 index e47c0883..00000000 --- a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Settings_1_1AVL__Discretization__Settings-members.html +++ /dev/null @@ -1,136 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Methods.Aerodynamics.AVL.Data.Settings.AVL_Discretization_Settings Member List
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This is the complete list of members for SUAVE.Methods.Aerodynamics.AVL.Data.Settings.AVL_Discretization_Settings, including all inherited members.

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__defaults__(self)SUAVE.Methods.Aerodynamics.AVL.Data.Settings.AVL_Discretization_Settings
__delattr__(self, k)SUAVE.Core.Data.Data
__getattribute__(self, k)SUAVE.Core.Data.Data
__init__(self, args, kwarg)SUAVE.Core.Data.Data
__iter__(self)SUAVE.Core.Data.Data
__new__(cls, args, kwarg)SUAVE.Core.Data.Data
__setattr__(self, k, v)SUAVE.Core.Data.Data
__str__(self, indent='')SUAVE.Core.Data.Data
append(self, value, key=None)SUAVE.Core.Data.Data
chordwise_elements (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Settings.AVL_Discretization_Settings)SUAVE.Methods.Aerodynamics.AVL.Data.Settings.AVL_Discretization_Settings
chordwise_spacing_scheme (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Settings.AVL_Discretization_Settings)SUAVE.Methods.Aerodynamics.AVL.Data.Settings.AVL_Discretization_Settings
dataname(self)SUAVE.Core.Data.Data
deep_get(self, keys)SUAVE.Core.Data.Data
deep_set(self, keys, val)SUAVE.Core.Data.Data
do_recursive(self, method, other=None, default=None)SUAVE.Core.Data.Data
get_bases(self)SUAVE.Core.Data.Data
itervalues(self)SUAVE.Core.Data.Data
pack_array(self, output='vector')SUAVE.Core.Data.Data
spanwise_elements (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Settings.AVL_Discretization_Settings)SUAVE.Methods.Aerodynamics.AVL.Data.Settings.AVL_Discretization_Settings
spanwise_spacing_scheme (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Settings.AVL_Discretization_Settings)SUAVE.Methods.Aerodynamics.AVL.Data.Settings.AVL_Discretization_Settings
typestring(self)SUAVE.Core.Data.Data
unpack_array(self, M)SUAVE.Core.Data.Data
update(self, other)SUAVE.Core.Data.Data
values(self)SUAVE.Core.Data.Data
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Settings_1_1AVL__Discretization__Settings.html b/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Settings_1_1AVL__Discretization__Settings.html deleted file mode 100644 index 98bf4257..00000000 --- a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Settings_1_1AVL__Discretization__Settings.html +++ /dev/null @@ -1,245 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Methods.Aerodynamics.AVL.Data.Settings.AVL_Discretization_Settings Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Methods.Aerodynamics.AVL.Data.Settings.AVL_Discretization_Settings Class Reference
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-Inheritance diagram for SUAVE.Methods.Aerodynamics.AVL.Data.Settings.AVL_Discretization_Settings:
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-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Core.Data.Data
def __getattribute__ (self, k)
 
def __setattr__ (self, k, v)
 
def __delattr__ (self, k)
 
def __defaults__ (self)
 
def __new__ (cls, args, kwarg)
 
def typestring (self)
 
def dataname (self)
 
def __str__ (self, indent='')
 
def __init__ (self, args, kwarg)
 
def __iter__ (self)
 
def itervalues (self)
 
def values (self)
 
def update (self, other)
 
def get_bases (self)
 
def append (self, value, key=None)
 
def deep_set (self, keys, val)
 
def deep_get (self, keys)
 
def pack_array (self, output='vector')
 
def unpack_array (self, M)
 
def do_recursive (self, method, other=None, default=None)
 
- - - - - - - - - -

-Public Attributes

chordwise_elements
 
chordwise_spacing_scheme
 
spanwise_elements
 
spanwise_spacing_scheme
 
-

Detailed Description

-
A class that defines discretization of vortices on the aircraft wing
-
-Assumptions:
-    None
-    
-Source:
-    None
-    
-Inputs:
-    None
-    
-Outputs:
-    None
-    
-Properties Used:
-    N/A
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Methods.Aerodynamics.AVL.Data.Settings.AVL_Discretization_Settings.__defaults__ ( self)
-
-
Defines the spacing of vortices on lifting surface in AVL
-SPACING SCHEMES:
-    - 'cosine' : ||  |    |      |      |    |  || (bunched at both ends)
-    - '+sine'  : || |  |   |    |    |     |     | (bunched at start)
-    - 'equal'  : |   |   |   |   |   |   |   |   | (equally spaced)
-    - '-sine'  : |     |     |    |    |   |  | || (bunched at end)
-               
-Assumptions:
-    None
-
-Source:
-    None
-
-Inputs:
-    None
-
-Outputs:
-    None
-
-Properties Used:
-    N/A
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Methods/Aerodynamics/AVL/Data/Settings.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Settings_1_1AVL__Discretization__Settings.js b/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Settings_1_1AVL__Discretization__Settings.js deleted file mode 100644 index 3211b482..00000000 --- a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Settings_1_1AVL__Discretization__Settings.js +++ /dev/null @@ -1,8 +0,0 @@ -var classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Settings_1_1AVL__Discretization__Settings = -[ - [ "__defaults__", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Settings_1_1AVL__Discretization__Settings.html#adccbf59a4db06215311385b49df11865", null ], - [ "chordwise_elements", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Settings_1_1AVL__Discretization__Settings.html#a1d8433619c928a46f38cbef5d1a5127c", null ], - [ "chordwise_spacing_scheme", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Settings_1_1AVL__Discretization__Settings.html#a1c119a7150b756431cc71a402081c5b4", null ], - [ "spanwise_elements", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Settings_1_1AVL__Discretization__Settings.html#a486fb3c32e70c27583d57980c7b28af6", null ], - [ "spanwise_spacing_scheme", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Settings_1_1AVL__Discretization__Settings.html#a64c8834ecdd841e2185678e63578f5f6", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Settings_1_1AVL__Discretization__Settings.png b/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Settings_1_1AVL__Discretization__Settings.png deleted file mode 100644 index 3bed82bf..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Settings_1_1AVL__Discretization__Settings.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Settings_1_1Settings-members.html b/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Settings_1_1Settings-members.html deleted file mode 100644 index 62dd6316..00000000 --- a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Settings_1_1Settings-members.html +++ /dev/null @@ -1,137 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Methods.Aerodynamics.AVL.Data.Settings.Settings Member List
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This is the complete list of members for SUAVE.Methods.Aerodynamics.AVL.Data.Settings.Settings, including all inherited members.

- - - - - - - - - - - - - - - - - - - - - - - - - - -
__defaults__(self)SUAVE.Methods.Aerodynamics.AVL.Data.Settings.Settings
__delattr__(self, k)SUAVE.Core.Data.Data
__getattribute__(self, k)SUAVE.Core.Data.Data
__init__(self, args, kwarg)SUAVE.Core.Data.Data
__iter__(self)SUAVE.Core.Data.Data
__new__(cls, args, kwarg)SUAVE.Core.Data.Data
__setattr__(self, k, v)SUAVE.Core.Data.Data
__str__(self, indent='')SUAVE.Core.Data.Data
append(self, value, key=None)SUAVE.Core.Data.Data
dataname(self)SUAVE.Core.Data.Data
deep_get(self, keys)SUAVE.Core.Data.Data
deep_set(self, keys, val)SUAVE.Core.Data.Data
discretization (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Settings.Settings)SUAVE.Methods.Aerodynamics.AVL.Data.Settings.Settings
do_recursive(self, method, other=None, default=None)SUAVE.Core.Data.Data
filenames (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Settings.Settings)SUAVE.Methods.Aerodynamics.AVL.Data.Settings.Settings
flow_symmetry (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Settings.Settings)SUAVE.Methods.Aerodynamics.AVL.Data.Settings.Settings
get_bases(self)SUAVE.Core.Data.Data
itervalues(self)SUAVE.Core.Data.Data
num_control_surfaces (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Settings.Settings)SUAVE.Methods.Aerodynamics.AVL.Data.Settings.Settings
pack_array(self, output='vector')SUAVE.Core.Data.Data
run_cases (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Settings.Settings)SUAVE.Methods.Aerodynamics.AVL.Data.Settings.Settings
typestring(self)SUAVE.Core.Data.Data
unpack_array(self, M)SUAVE.Core.Data.Data
update(self, other)SUAVE.Core.Data.Data
values(self)SUAVE.Core.Data.Data
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Settings_1_1Settings.html b/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Settings_1_1Settings.html deleted file mode 100644 index 70b5d9c0..00000000 --- a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Settings_1_1Settings.html +++ /dev/null @@ -1,244 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Methods.Aerodynamics.AVL.Data.Settings.Settings Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Methods.Aerodynamics.AVL.Data.Settings.Settings Class Reference
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-Inheritance diagram for SUAVE.Methods.Aerodynamics.AVL.Data.Settings.Settings:
-
-
- - -SUAVE.Core.Data.Data - -
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Core.Data.Data
def __getattribute__ (self, k)
 
def __setattr__ (self, k, v)
 
def __delattr__ (self, k)
 
def __defaults__ (self)
 
def __new__ (cls, args, kwarg)
 
def typestring (self)
 
def dataname (self)
 
def __str__ (self, indent='')
 
def __init__ (self, args, kwarg)
 
def __iter__ (self)
 
def itervalues (self)
 
def values (self)
 
def update (self, other)
 
def get_bases (self)
 
def append (self, value, key=None)
 
def deep_set (self, keys, val)
 
def deep_get (self, keys)
 
def pack_array (self, output='vector')
 
def unpack_array (self, M)
 
def do_recursive (self, method, other=None, default=None)
 
- - - - - - - - - - - -

-Public Attributes

run_cases
 
filenames
 
flow_symmetry
 
discretization
 
num_control_surfaces
 
-

Detailed Description

-
A class that defines important settings that call the AVL executable in addition to the 
-format of the result, batch and geometry filenames
-
-Assumptions:
-    None
-    
-Source:
-    None
-    
-Inputs:
-    None
-    
-Outputs:
-    None
-    
-Properties Used:
-    N/A
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Methods.Aerodynamics.AVL.Data.Settings.Settings.__defaults__ ( self)
-
-
Defines naming convention for files created/used by AVL to compute analysus
-        
-Assumptions:
-    None
-        
-Source:
-    None
-        
-Inputs:
-    None
-        
-Outputs:
-    None
-        
-Properties Used:
-    N/A
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Methods/Aerodynamics/AVL/Data/Settings.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Settings_1_1Settings.js b/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Settings_1_1Settings.js deleted file mode 100644 index 44fd83f5..00000000 --- a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Settings_1_1Settings.js +++ /dev/null @@ -1,9 +0,0 @@ -var classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Settings_1_1Settings = -[ - [ "__defaults__", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Settings_1_1Settings.html#a79d49c59a2bf93ffbb3fc030d4a0e0e4", null ], - [ "discretization", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Settings_1_1Settings.html#a4079c122f98eef755e4fe7758070ead0", null ], - [ "filenames", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Settings_1_1Settings.html#a23d7675f5d82f81dabaa0b43787cdb30", null ], - [ "flow_symmetry", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Settings_1_1Settings.html#a21260b2f900e83e052b5e9c566f6da13", null ], - [ "num_control_surfaces", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Settings_1_1Settings.html#ac691e98b5c4c257afddd332eff988449", null ], - [ "run_cases", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Settings_1_1Settings.html#a56dd550b4e50698cc5792ab8a9b50ec5", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Settings_1_1Settings.png b/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Settings_1_1Settings.png deleted file mode 100644 index 612d89d7..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Settings_1_1Settings.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface-members.html b/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface-members.html deleted file mode 100644 index 077cb527..00000000 --- a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface-members.html +++ /dev/null @@ -1,137 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
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SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface Member List
-
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- -

This is the complete list of members for SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface, including all inherited members.

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__defaults__(self)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface
__delattr__(self, k)SUAVE.Core.Data.Data
__getattribute__(self, k)SUAVE.Core.Data.Data
__init__(self, args, kwarg)SUAVE.Core.Data.Data
__iter__(self)SUAVE.Core.Data.Data
__new__(cls, args, kwarg)SUAVE.Core.Data.Data
__setattr__(self, k, v)SUAVE.Core.Data.Data
__str__(self, indent='')SUAVE.Core.Data.Data
append(self, value, key=None)SUAVE.Core.Data.Data
dataname(self)SUAVE.Core.Data.Data
deep_get(self, keys)SUAVE.Core.Data.Data
deep_set(self, keys, val)SUAVE.Core.Data.Data
do_recursive(self, method, other=None, default=None)SUAVE.Core.Data.Data
gain (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface
get_bases(self)SUAVE.Core.Data.Data
hinge_vector (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface
itervalues(self)SUAVE.Core.Data.Data
pack_array(self, output='vector')SUAVE.Core.Data.Data
sign_duplicate (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface
tag (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface
typestring(self)SUAVE.Core.Data.Data
unpack_array(self, M)SUAVE.Core.Data.Data
update(self, other)SUAVE.Core.Data.Data
values(self)SUAVE.Core.Data.Data
x_hinge (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface.html b/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface.html deleted file mode 100644 index 0e7e24f3..00000000 --- a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface.html +++ /dev/null @@ -1,245 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface Class Reference
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-
-Inheritance diagram for SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface:
-
-
- - -SUAVE.Core.Data.Data - -
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Core.Data.Data
def __getattribute__ (self, k)
 
def __setattr__ (self, k, v)
 
def __delattr__ (self, k)
 
def __defaults__ (self)
 
def __new__ (cls, args, kwarg)
 
def typestring (self)
 
def dataname (self)
 
def __str__ (self, indent='')
 
def __init__ (self, args, kwarg)
 
def __iter__ (self)
 
def itervalues (self)
 
def values (self)
 
def update (self, other)
 
def get_bases (self)
 
def append (self, value, key=None)
 
def deep_set (self, keys, val)
 
def deep_get (self, keys)
 
def pack_array (self, output='vector')
 
def unpack_array (self, M)
 
def do_recursive (self, method, other=None, default=None)
 
- - - - - - - - - - - -

-Public Attributes

tag
 
gain
 
x_hinge
 
hinge_vector
 
sign_duplicate
 
-

Detailed Description

-
A class that defines the control surface geometry and deflection
-on the aircraft wing in AVL
-
-Assumptions:
-    None
-
-Source:
-    None
-
-Inputs:
-    None
-
-Outputs:
-    None
-
-Properties Used:
-    N/A
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface.__defaults__ ( self)
-
-
Sets the defaults of the control surface on the aircraft wing
-in AVL
-    
-Assumptions:
-    None
-    
-Source:
-    None
-    
-Inputs:
-    None
-    
-Outputs:
-    None
-    
-Properties Used:
-    N/A
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Methods/Aerodynamics/AVL/Data/Wing.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface.js b/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface.js deleted file mode 100644 index 47e5548e..00000000 --- a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface.js +++ /dev/null @@ -1,9 +0,0 @@ -var classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface = -[ - [ "__defaults__", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface.html#ac6c75479876eeb8f1e1b0fa6427c75dd", null ], - [ "gain", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface.html#aa1cc6c9fc9019988b3ddbb82a95b2dd2", null ], - [ "hinge_vector", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface.html#a4ffdcdedc2d6b764687c9e42940587e2", null ], - [ "sign_duplicate", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface.html#a89515ef6de21cda9f08ac9dc4de0f5ba", null ], - [ "tag", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface.html#abeb4f1f85e07b0428ac7d8399dcc05ee", null ], - [ "x_hinge", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface.html#a7be2cca6ca757661e7704efa36b405d2", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface.png b/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface.png deleted file mode 100644 index 6eba8b3e..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Section-members.html b/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Section-members.html deleted file mode 100644 index 0b346a55..00000000 --- a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Section-members.html +++ /dev/null @@ -1,139 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
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SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Section Member List
-
-
- -

This is the complete list of members for SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Section, including all inherited members.

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__defaults__(self)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Section
__delattr__(self, k)SUAVE.Core.Data.Data
__getattribute__(self, k)SUAVE.Core.Data.Data
__init__(self, args, kwarg)SUAVE.Core.Data.Data
__iter__(self)SUAVE.Core.Data.Data
__new__(cls, args, kwarg)SUAVE.Core.Data.Data
__setattr__(self, k, v)SUAVE.Core.Data.Data
__str__(self, indent='')SUAVE.Core.Data.Data
airfoil_coord_file (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Section)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Section
append(self, value, key=None)SUAVE.Core.Data.Data
append_control_surface(self, control)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Section
chord (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Section)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Section
control_surfaces (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Section)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Section
dataname(self)SUAVE.Core.Data.Data
deep_get(self, keys)SUAVE.Core.Data.Data
deep_set(self, keys, val)SUAVE.Core.Data.Data
do_recursive(self, method, other=None, default=None)SUAVE.Core.Data.Data
get_bases(self)SUAVE.Core.Data.Data
itervalues(self)SUAVE.Core.Data.Data
origin (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Section)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Section
pack_array(self, output='vector')SUAVE.Core.Data.Data
tag (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Section)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Section
twist (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Section)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Section
typestring(self)SUAVE.Core.Data.Data
unpack_array(self, M)SUAVE.Core.Data.Data
update(self, other)SUAVE.Core.Data.Data
values(self)SUAVE.Core.Data.Data
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Section.html b/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Section.html deleted file mode 100644 index 8921cffa..00000000 --- a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Section.html +++ /dev/null @@ -1,293 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Section Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Section Class Reference
-
-
-
-Inheritance diagram for SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Section:
-
-
- - -SUAVE.Core.Data.Data - -
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def append_control_surface (self, control)
 
- Public Member Functions inherited from SUAVE.Core.Data.Data
def __getattribute__ (self, k)
 
def __setattr__ (self, k, v)
 
def __delattr__ (self, k)
 
def __defaults__ (self)
 
def __new__ (cls, args, kwarg)
 
def typestring (self)
 
def dataname (self)
 
def __str__ (self, indent='')
 
def __init__ (self, args, kwarg)
 
def __iter__ (self)
 
def itervalues (self)
 
def values (self)
 
def update (self, other)
 
def get_bases (self)
 
def append (self, value, key=None)
 
def deep_set (self, keys, val)
 
def deep_get (self, keys)
 
def pack_array (self, output='vector')
 
def unpack_array (self, M)
 
def do_recursive (self, method, other=None, default=None)
 
- - - - - - - - - - - - - -

-Public Attributes

tag
 
origin
 
chord
 
twist
 
airfoil_coord_file
 
control_surfaces
 
-

Detailed Description

-
A class that defines the sections of the aircraft wing in AVL.
-Each section can be thought of as a trapezoid
-
-Assumptions:
-    None
-
-Source:
-    None
-
-Inputs:
-    None
-
-Outputs:
-    None
-
-Properties Used:
-    N/A
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Section.__defaults__ ( self)
-
-
Sets the defaunts of the aircraft wing geometry 
-    
-Assumptions:
-    None
-    
-Source:
-    None
-    
-Inputs:
-    None
-    
-Outputs:
-    None
-    
-Properties Used:
-    N/A
-
-
-
- -

◆ append_control_surface()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Section.append_control_surface ( self,
 control 
)
-
-
Adds a control_surface to the wing section in AVL
-    
-Assumptions:
-    None
-    
-Source:
-    None
-    
-Inputs:
-    None
-    
-Outputs:
-    None
-    
-Properties Used:
-    N/A
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Methods/Aerodynamics/AVL/Data/Wing.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Section.js b/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Section.js deleted file mode 100644 index 7762420c..00000000 --- a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Section.js +++ /dev/null @@ -1,11 +0,0 @@ -var classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Section = -[ - [ "__defaults__", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Section.html#a8e1e0ac259353e0ce2a1b672ed9bee71", null ], - [ "append_control_surface", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Section.html#a1db4b8c7983b9f3ee477eb6e479caedc", null ], - [ "airfoil_coord_file", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Section.html#abd0183b7faac5f2c02397afb471aa667", null ], - [ "chord", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Section.html#a7b76228bb44c3a1e477439185e428af6", null ], - [ "control_surfaces", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Section.html#afc85152833f0c6c44bc1cf9bd960b756", null ], - [ "origin", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Section.html#a1e74b5c3cbee04e629ebf425b6ee75d4", null ], - [ "tag", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Section.html#a2e01bb6c59e37d1e6b37571b0709da36", null ], - [ "twist", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Section.html#ab9c9fb32b0c7178626a8b105e696064d", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Section.png b/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Section.png deleted file mode 100644 index 74d3efd6..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Section.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Wing-members.html b/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Wing-members.html deleted file mode 100644 index d348114e..00000000 --- a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Wing-members.html +++ /dev/null @@ -1,142 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
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- - - -
-
- -
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- -
- -
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- - -
- -
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SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing Member List
-
-
- -

This is the complete list of members for SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing, including all inherited members.

- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
__defaults__(self) (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing
__delattr__(self, k)SUAVE.Core.Data.Data
__getattribute__(self, k)SUAVE.Core.Data.Data
__init__(self, args, kwarg)SUAVE.Core.Data.Data
__iter__(self)SUAVE.Core.Data.Data
__new__(cls, args, kwarg)SUAVE.Core.Data.Data
__setattr__(self, k, v)SUAVE.Core.Data.Data
__str__(self, indent='')SUAVE.Core.Data.Data
append(self, value, key=None)SUAVE.Core.Data.Data
append_section(self, section)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing
configuration (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing
control_surfaces (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing
dataname(self)SUAVE.Core.Data.Data
deep_get(self, keys)SUAVE.Core.Data.Data
deep_set(self, keys, val)SUAVE.Core.Data.Data
dihedral (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing
do_recursive(self, method, other=None, default=None)SUAVE.Core.Data.Data
get_bases(self)SUAVE.Core.Data.Data
itervalues(self)SUAVE.Core.Data.Data
origin (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing
pack_array(self, output='vector')SUAVE.Core.Data.Data
sections (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing
sweep (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing
symmetric (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing
tag (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing
typestring(self)SUAVE.Core.Data.Data
unpack_array(self, M)SUAVE.Core.Data.Data
update(self, other)SUAVE.Core.Data.Data
values(self)SUAVE.Core.Data.Data
vertical (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Wing.html b/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Wing.html deleted file mode 100644 index df3d875c..00000000 --- a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Wing.html +++ /dev/null @@ -1,252 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
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SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
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SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing Class Reference
-
-
-
-Inheritance diagram for SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing:
-
-
- - -SUAVE.Core.Data.Data - -
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

-def __defaults__ (self)
 
def append_section (self, section)
 
- Public Member Functions inherited from SUAVE.Core.Data.Data
def __getattribute__ (self, k)
 
def __setattr__ (self, k, v)
 
def __delattr__ (self, k)
 
def __defaults__ (self)
 
def __new__ (cls, args, kwarg)
 
def typestring (self)
 
def dataname (self)
 
def __str__ (self, indent='')
 
def __init__ (self, args, kwarg)
 
def __iter__ (self)
 
def itervalues (self)
 
def values (self)
 
def update (self, other)
 
def get_bases (self)
 
def append (self, value, key=None)
 
def deep_set (self, keys, val)
 
def deep_get (self, keys)
 
def pack_array (self, output='vector')
 
def unpack_array (self, M)
 
def do_recursive (self, method, other=None, default=None)
 
- - - - - - - - - - - - - - - - - - - -

-Public Attributes

tag
 
symmetric
 
vertical
 
origin
 
sweep
 
dihedral
 
sections
 
configuration
 
control_surfaces
 
-

Detailed Description

-
A class that defines parameters of the AVL aircraft wing
-
-Assumptions:
-    None
-
-Source:
-    None
-
-Inputs:
-    None
-
-Outputs:
-    None
-
-Properties Used:
-    N/A
-

Member Function Documentation

- -

◆ append_section()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing.append_section ( self,
 section 
)
-
-
adds a segment to the wing 
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Methods/Aerodynamics/AVL/Data/Wing.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Wing.js b/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Wing.js deleted file mode 100644 index aba0d3f7..00000000 --- a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Wing.js +++ /dev/null @@ -1,14 +0,0 @@ -var classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Wing = -[ - [ "__defaults__", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Wing.html#a90ddc0380e1cae8fab5c9f0f6c2a839d", null ], - [ "append_section", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Wing.html#a294eba3444d1f5bb9a2fb165386b82b2", null ], - [ "configuration", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Wing.html#ade730cc2e7854e3ed46ee21e7fb054a4", null ], - [ "control_surfaces", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Wing.html#a9c990fc2abe3003b85d81c64fa8fe64d", null ], - [ "dihedral", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Wing.html#a7d1569249e630a11584b5ce0713418cb", null ], - [ "origin", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Wing.html#a46ec9bf3092f3c38f9636fcf18fd2828", null ], - [ "sections", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Wing.html#a26183260ee90b15ff56b057dea9a2ea2", null ], - [ "sweep", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Wing.html#a824e062760f9fdca7a3810da74e52d07", null ], - [ "symmetric", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Wing.html#ac3908bc32ce3dfa73a6b4f3bf063ad6c", null ], - [ "tag", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Wing.html#a8548663fbf09da789fcc8058c77f329b", null ], - [ "vertical", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Wing.html#ad5826318001245a0f478465591870de4", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Wing.png b/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Wing.png deleted file mode 100644 index d140cd4d..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Wing.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Optimization_1_1Nexus_1_1Nexus-members.html b/_site/doxygen/classSUAVE_1_1Optimization_1_1Nexus_1_1Nexus-members.html deleted file mode 100644 index 76642cd8..00000000 --- a/_site/doxygen/classSUAVE_1_1Optimization_1_1Nexus_1_1Nexus-members.html +++ /dev/null @@ -1,152 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Optimization.Nexus.Nexus Member List
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This is the complete list of members for SUAVE.Optimization.Nexus.Nexus, including all inherited members.

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__defaults__(self)SUAVE.Optimization.Nexus.Nexus
__delattr__(self, k)SUAVE.Core.Data.Data
__getattribute__(self, k)SUAVE.Core.Data.Data
__init__(self, args, kwarg)SUAVE.Core.Data.Data
__iter__(self)SUAVE.Core.Data.Data
__new__(cls, args, kwarg)SUAVE.Core.Data.Data
__setattr__(self, k, v)SUAVE.Core.Data.Data
__str__(self, indent='')SUAVE.Core.Data.Data
all_constraints(self, x=None)SUAVE.Optimization.Nexus.Nexus
analyses (defined in SUAVE.Optimization.Nexus.Nexus)SUAVE.Optimization.Nexus.Nexus
append(self, value, key=None)SUAVE.Core.Data.Data
constraints_individual(self, x=None)SUAVE.Optimization.Nexus.Nexus
dataname(self)SUAVE.Core.Data.Data
deep_get(self, keys)SUAVE.Core.Data.Data
deep_set(self, keys, val)SUAVE.Core.Data.Data
do_recursive(self, method, other=None, default=None)SUAVE.Core.Data.Data
equality_constraint(self, x=None)SUAVE.Optimization.Nexus.Nexus
evaluate(self, x=None)SUAVE.Optimization.Nexus.Nexus
evaluation_count (defined in SUAVE.Optimization.Nexus.Nexus)SUAVE.Optimization.Nexus.Nexus
fidelity_level (defined in SUAVE.Optimization.Nexus.Nexus)SUAVE.Optimization.Nexus.Nexus
finite_difference(self, x, diff_interval=1e-8)SUAVE.Optimization.Nexus.Nexus
get_bases(self)SUAVE.Core.Data.Data
inequality_constraint(self, x=None)SUAVE.Optimization.Nexus.Nexus
itervalues(self)SUAVE.Core.Data.Data
last_fidelity (defined in SUAVE.Optimization.Nexus.Nexus)SUAVE.Optimization.Nexus.Nexus
last_inputs (defined in SUAVE.Optimization.Nexus.Nexus)SUAVE.Optimization.Nexus.Nexus
missions (defined in SUAVE.Optimization.Nexus.Nexus)SUAVE.Optimization.Nexus.Nexus
objective(self, x=None)SUAVE.Optimization.Nexus.Nexus
optimization_problem (defined in SUAVE.Optimization.Nexus.Nexus)SUAVE.Optimization.Nexus.Nexus
pack_array(self, output='vector')SUAVE.Core.Data.Data
procedure (defined in SUAVE.Optimization.Nexus.Nexus)SUAVE.Optimization.Nexus.Nexus
results (defined in SUAVE.Optimization.Nexus.Nexus)SUAVE.Optimization.Nexus.Nexus
summary (defined in SUAVE.Optimization.Nexus.Nexus)SUAVE.Optimization.Nexus.Nexus
translate(self, x=None)SUAVE.Optimization.Nexus.Nexus
typestring(self)SUAVE.Core.Data.Data
unpack_array(self, M)SUAVE.Core.Data.Data
unpack_inputs(self, x=None)SUAVE.Optimization.Nexus.Nexus
update(self, other)SUAVE.Core.Data.Data
values(self)SUAVE.Core.Data.Data
vehicle_configurations (defined in SUAVE.Optimization.Nexus.Nexus)SUAVE.Optimization.Nexus.Nexus
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Optimization_1_1Nexus_1_1Nexus.html b/_site/doxygen/classSUAVE_1_1Optimization_1_1Nexus_1_1Nexus.html deleted file mode 100644 index 4effcba8..00000000 --- a/_site/doxygen/classSUAVE_1_1Optimization_1_1Nexus_1_1Nexus.html +++ /dev/null @@ -1,681 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Optimization.Nexus.Nexus Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
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-
- - - -
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- -
-
-
- -
- -
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SUAVE.Optimization.Nexus.Nexus Class Reference
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-
-
-Inheritance diagram for SUAVE.Optimization.Nexus.Nexus:
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-
- - -SUAVE.Core.Data.Data - -
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def evaluate (self, x=None)
 
def objective (self, x=None)
 
def inequality_constraint (self, x=None)
 
def equality_constraint (self, x=None)
 
def all_constraints (self, x=None)
 
def unpack_inputs (self, x=None)
 
def constraints_individual (self, x=None)
 
def finite_difference (self, x, diff_interval=1e-8)
 
def translate (self, x=None)
 
- Public Member Functions inherited from SUAVE.Core.Data.Data
def __getattribute__ (self, k)
 
def __setattr__ (self, k, v)
 
def __delattr__ (self, k)
 
def __defaults__ (self)
 
def __new__ (cls, args, kwarg)
 
def typestring (self)
 
def dataname (self)
 
def __str__ (self, indent='')
 
def __init__ (self, args, kwarg)
 
def __iter__ (self)
 
def itervalues (self)
 
def values (self)
 
def update (self, other)
 
def get_bases (self)
 
def append (self, value, key=None)
 
def deep_set (self, keys, val)
 
def deep_get (self, keys)
 
def pack_array (self, output='vector')
 
def unpack_array (self, M)
 
def do_recursive (self, method, other=None, default=None)
 
- - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

vehicle_configurations
 
analyses
 
missions
 
procedure
 
results
 
summary
 
optimization_problem
 
fidelity_level
 
last_inputs
 
last_fidelity
 
evaluation_count
 
-

Detailed Description

-
noun (plural same or nexuses)
-    -a connection or series of connections linking two or more things
-    -a connected group or series: a nexus of ideas.
-    -the central and most important point or place
-    
-    This is the class that makes optimization possible. We put all the data and functions together to make
-    your future dreams come true.
-    
-    Assumptions:
-    You like SUAVE
-    
-    Source:
-    Oxford English Dictionary
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Optimization.Nexus.Nexus.__defaults__ ( self)
-
-
This sets the default values.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
- -

◆ all_constraints()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Optimization.Nexus.Nexus.all_constraints ( self,
 x = None 
)
-
-
Returns both the inequality and equality constraint values for your function
-    
-    Assumptions:
-    N/A
-    
-    Source:
-    N/A
-    
-    Inputs:
-    x                  [vector]
-    
-    Outputs:
-    scaled_constraints [vector]
-    
-    Properties Used:
-    None
-
-
-
- -

◆ constraints_individual()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Optimization.Nexus.Nexus.constraints_individual ( self,
 x = None 
)
-
-
Put's the values of the problem in the right place.
-    
-    Assumptions:
-    N/A
-    
-    Source:
-    N/A
-    
-    Inputs:
-    x                  [vector]
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
- -

◆ equality_constraint()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Optimization.Nexus.Nexus.equality_constraint ( self,
 x = None 
)
-
-
Retrieve the equality constraint values for your function
-    
-    Assumptions:
-    N/A
-    
-    Source:
-    N/A
-    
-    Inputs:
-    x                  [vector]
-    
-    Outputs:
-    scaled_constraints [vector]
-    
-    Properties Used:
-    None
-
-
-
- -

◆ evaluate()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Optimization.Nexus.Nexus.evaluate ( self,
 x = None 
)
-
-
This function runs the problem you setup in SUAVE.
-    If the last time you ran this the inputs were the same, a cache is used.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    x       [vector]
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
- -

◆ finite_difference()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Optimization.Nexus.Nexus.finite_difference ( self,
 x,
 diff_interval = 1e-8 
)
-
-
Finite difference gradients and jacobians of the problem.
-    
-    Assumptions:
-    N/A
-    
-    Source:
-    N/A
-    
-    Inputs:
-    x                  [vector]
-    diff_interval      [float]
-    
-    Outputs:
-    grad_obj           [vector]
-    jac_con            [array]
-    
-    Properties Used:
-    None
-
-
-
- -

◆ inequality_constraint()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Optimization.Nexus.Nexus.inequality_constraint ( self,
 x = None 
)
-
-
Retrieve the inequality constraint values for your function
-    
-    Assumptions:
-    N/A
-    
-    Source:
-    N/A
-    
-    Inputs:
-    x                  [vector]
-    
-    Outputs:
-    scaled_constraints [vector]
-    
-    Properties Used:
-    None
-
-
- -

◆ objective()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Optimization.Nexus.Nexus.objective ( self,
 x = None 
)
-
-
Retrieve the objective value for your function
-    
-    Assumptions:
-    N/A
-    
-    Source:
-    N/A
-    
-    Inputs:
-    x       [vector]
-    
-    Outputs:
-    scaled_objective [float]
-    
-    Properties Used:
-    None
-
-
-
- -

◆ translate()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Optimization.Nexus.Nexus.translate ( self,
 x = None 
)
-
-
Make a pretty table view of the problem with objective and constraints at the current inputs
-    
-    Assumptions:
-    N/A
-    
-    Source:
-    N/A
-    
-    Inputs:
-    x                  [vector]
-    
-    Outputs:
-    inpu               [array]
-    const_table        [array]
-    
-    Properties Used:
-    None
-
-
-
- -

◆ unpack_inputs()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Optimization.Nexus.Nexus.unpack_inputs ( self,
 x = None 
)
-
-
Put's the values of the problem in the right place.
-    
-    Assumptions:
-    N/A
-    
-    Source:
-    N/A
-    
-    Inputs:
-    x                  [vector]
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Optimization/Nexus.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Optimization_1_1Nexus_1_1Nexus.js b/_site/doxygen/classSUAVE_1_1Optimization_1_1Nexus_1_1Nexus.js deleted file mode 100644 index e7829923..00000000 --- a/_site/doxygen/classSUAVE_1_1Optimization_1_1Nexus_1_1Nexus.js +++ /dev/null @@ -1,24 +0,0 @@ -var classSUAVE_1_1Optimization_1_1Nexus_1_1Nexus = -[ - [ "__defaults__", "classSUAVE_1_1Optimization_1_1Nexus_1_1Nexus.html#aa322d3e87229966ab24c85f885ab3570", null ], - [ "all_constraints", "classSUAVE_1_1Optimization_1_1Nexus_1_1Nexus.html#a283bba67ee91bdc858cca6a317a578f5", null ], - [ "constraints_individual", "classSUAVE_1_1Optimization_1_1Nexus_1_1Nexus.html#a47f18af949a54d34571cf342d9bc07f3", null ], - [ "equality_constraint", "classSUAVE_1_1Optimization_1_1Nexus_1_1Nexus.html#ab53543f4eaa1f6c9e9fa34dc568b4192", null ], - [ "evaluate", "classSUAVE_1_1Optimization_1_1Nexus_1_1Nexus.html#a2ccf05f1c95dd06c8e3e03fc444a73fa", null ], - [ "finite_difference", "classSUAVE_1_1Optimization_1_1Nexus_1_1Nexus.html#af25ebc8a76e541e3bb18d412c5284b7a", null ], - [ "inequality_constraint", "classSUAVE_1_1Optimization_1_1Nexus_1_1Nexus.html#a6c0d456823c899efeb87947690801f29", null ], - [ "objective", "classSUAVE_1_1Optimization_1_1Nexus_1_1Nexus.html#a1eda3512dfde03334eff1fff6c8d5784", null ], - [ "translate", "classSUAVE_1_1Optimization_1_1Nexus_1_1Nexus.html#a39fd2614a9089eaf48e84e4c748bbfa5", null ], - [ "unpack_inputs", "classSUAVE_1_1Optimization_1_1Nexus_1_1Nexus.html#a2eeced272b32579d028038e434083de0", null ], - [ "analyses", "classSUAVE_1_1Optimization_1_1Nexus_1_1Nexus.html#a7540bae0fa705aedd67732e6a4f2fd03", null ], - [ "evaluation_count", "classSUAVE_1_1Optimization_1_1Nexus_1_1Nexus.html#a0e0a0b0d2ba3e3cd1381569156f1f2ff", null ], - [ "fidelity_level", "classSUAVE_1_1Optimization_1_1Nexus_1_1Nexus.html#aea9b128c29d6dc551ac15263d0e2267c", null ], - [ "last_fidelity", "classSUAVE_1_1Optimization_1_1Nexus_1_1Nexus.html#ac4c2045d9bc469e48c23a7b5f96ecb84", null ], - [ "last_inputs", "classSUAVE_1_1Optimization_1_1Nexus_1_1Nexus.html#a4a62b5f7d690c3b4390ccd4f54fd6a45", null ], - [ "missions", "classSUAVE_1_1Optimization_1_1Nexus_1_1Nexus.html#a3b13fe94b3835bb58af3aca92ec95a16", null ], - [ "optimization_problem", "classSUAVE_1_1Optimization_1_1Nexus_1_1Nexus.html#a62cd9c40fc4f8c623ec937b4aecefc0d", null ], - [ "procedure", "classSUAVE_1_1Optimization_1_1Nexus_1_1Nexus.html#a8d5a4c85ca10966b274f9d25101b4015", null ], - [ "results", "classSUAVE_1_1Optimization_1_1Nexus_1_1Nexus.html#a070abc2a7311764ba5e1a1946d87b144", null ], - [ "summary", "classSUAVE_1_1Optimization_1_1Nexus_1_1Nexus.html#a58bc82420728a14e4d00573f5297d55e", null ], - [ "vehicle_configurations", "classSUAVE_1_1Optimization_1_1Nexus_1_1Nexus.html#a155e65f06b8a8426f9e168661934fed6", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Optimization_1_1Nexus_1_1Nexus.png b/_site/doxygen/classSUAVE_1_1Optimization_1_1Nexus_1_1Nexus.png deleted file mode 100644 index 0f6ff235..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Optimization_1_1Nexus_1_1Nexus.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region_1_1Trust__Region-members.html b/_site/doxygen/classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region_1_1Trust__Region-members.html deleted file mode 100644 index dcb9c848..00000000 --- a/_site/doxygen/classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region_1_1Trust__Region-members.html +++ /dev/null @@ -1,140 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
-
- - - -
-
- -
-
-
- -
- -
-
- - -
- -
- -
-
-
SUAVE.Optimization.Package_Setups.TRMM.Trust_Region.Trust_Region Member List
-
-
- -

This is the complete list of members for SUAVE.Optimization.Package_Setups.TRMM.Trust_Region.Trust_Region, including all inherited members.

- - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
__defaults__(self)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region.Trust_Region
__delattr__(self, k)SUAVE.Core.Data.Data
__getattribute__(self, k)SUAVE.Core.Data.Data
__init__(self, args, kwarg)SUAVE.Core.Data.Data
__iter__(self)SUAVE.Core.Data.Data
__new__(cls, args, kwarg)SUAVE.Core.Data.Data
__setattr__(self, k, v)SUAVE.Core.Data.Data
__str__(self, indent='')SUAVE.Core.Data.Data
append(self, value, key=None)SUAVE.Core.Data.Data
contract_threshold (defined in SUAVE.Optimization.Package_Setups.TRMM.Trust_Region.Trust_Region)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region.Trust_Region
contraction_factor (defined in SUAVE.Optimization.Package_Setups.TRMM.Trust_Region.Trust_Region)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region.Trust_Region
dataname(self)SUAVE.Core.Data.Data
deep_get(self, keys)SUAVE.Core.Data.Data
deep_set(self, keys, val)SUAVE.Core.Data.Data
do_recursive(self, method, other=None, default=None)SUAVE.Core.Data.Data
evaluate_function(self, f, gviol)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region.Trust_Region
expand_threshold (defined in SUAVE.Optimization.Package_Setups.TRMM.Trust_Region.Trust_Region)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region.Trust_Region
expansion_factor (defined in SUAVE.Optimization.Package_Setups.TRMM.Trust_Region.Trust_Region)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region.Trust_Region
get_bases(self)SUAVE.Core.Data.Data
initial_size (defined in SUAVE.Optimization.Package_Setups.TRMM.Trust_Region.Trust_Region)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region.Trust_Region
itervalues(self)SUAVE.Core.Data.Data
minimum_size (defined in SUAVE.Optimization.Package_Setups.TRMM.Trust_Region.Trust_Region)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region.Trust_Region
pack_array(self, output='vector')SUAVE.Core.Data.Data
size (defined in SUAVE.Optimization.Package_Setups.TRMM.Trust_Region.Trust_Region)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region.Trust_Region
typestring(self)SUAVE.Core.Data.Data
unpack_array(self, M)SUAVE.Core.Data.Data
update(self, other)SUAVE.Core.Data.Data
values(self)SUAVE.Core.Data.Data
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region_1_1Trust__Region.html b/_site/doxygen/classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region_1_1Trust__Region.html deleted file mode 100644 index caeca7e4..00000000 --- a/_site/doxygen/classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region_1_1Trust__Region.html +++ /dev/null @@ -1,292 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Optimization.Package_Setups.TRMM.Trust_Region.Trust_Region Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
-
- - - -
-
- -
-
-
- -
- -
-
- - -
- -
- -
- -
-
SUAVE.Optimization.Package_Setups.TRMM.Trust_Region.Trust_Region Class Reference
-
-
-
-Inheritance diagram for SUAVE.Optimization.Package_Setups.TRMM.Trust_Region.Trust_Region:
-
-
- - -SUAVE.Core.Data.Data - -
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def evaluate_function (self, f, gviol)
 
- Public Member Functions inherited from SUAVE.Core.Data.Data
def __getattribute__ (self, k)
 
def __setattr__ (self, k, v)
 
def __delattr__ (self, k)
 
def __defaults__ (self)
 
def __new__ (cls, args, kwarg)
 
def typestring (self)
 
def dataname (self)
 
def __str__ (self, indent='')
 
def __init__ (self, args, kwarg)
 
def __iter__ (self)
 
def itervalues (self)
 
def values (self)
 
def update (self, other)
 
def get_bases (self)
 
def append (self, value, key=None)
 
def deep_set (self, keys, val)
 
def deep_get (self, keys)
 
def pack_array (self, output='vector')
 
def unpack_array (self, M)
 
def do_recursive (self, method, other=None, default=None)
 
- - - - - - - - - - - - - - - -

-Public Attributes

initial_size
 
size
 
minimum_size
 
contract_threshold
 
expand_threshold
 
contraction_factor
 
expansion_factor
 
-

Detailed Description

-
A trust region class
-
-Assumptions:
-None
-
-Source:
-None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Optimization.Package_Setups.TRMM.Trust_Region.Trust_Region.__defaults__ ( self)
-
-
This sets the default values.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
- -

◆ evaluate_function()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Optimization.Package_Setups.TRMM.Trust_Region.Trust_Region.evaluate_function ( self,
 f,
 gviol 
)
-
-
Evaluates the function
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    self    
-    f         []
-    gviol     []
-    
-    Outputs:
-    phi       []
-    
-    Properties Used:
-    None
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Optimization/Package_Setups/TRMM/Trust_Region.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region_1_1Trust__Region.js b/_site/doxygen/classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region_1_1Trust__Region.js deleted file mode 100644 index ffb98d87..00000000 --- a/_site/doxygen/classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region_1_1Trust__Region.js +++ /dev/null @@ -1,12 +0,0 @@ -var classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region_1_1Trust__Region = -[ - [ "__defaults__", "classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region_1_1Trust__Region.html#aed3de6e47f3e4f368d486a111ccd5cd1", null ], - [ "evaluate_function", "classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region_1_1Trust__Region.html#ada04fa2510437fb9fd138f90fc1e6811", null ], - [ "contract_threshold", "classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region_1_1Trust__Region.html#afc8b4e2c078bc4cbc3cc3185302a5c24", null ], - [ "contraction_factor", "classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region_1_1Trust__Region.html#a3dbb3e29efc86cf9e2cdd99200ac9e17", null ], - [ "expand_threshold", "classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region_1_1Trust__Region.html#aa8f96e181d55261200eabe78edf30fe1", null ], - [ "expansion_factor", "classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region_1_1Trust__Region.html#a1084a7a71558fd414bbd66e71a5c1d1e", null ], - [ "initial_size", "classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region_1_1Trust__Region.html#af2e818dba7358535c2e8010bd5bc1fb9", null ], - [ "minimum_size", "classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region_1_1Trust__Region.html#a6d1dea7c1d30249410f673d6f5771cb2", null ], - [ "size", "classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region_1_1Trust__Region.html#ac79b00658ad489ef82a8667253f3b085", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region_1_1Trust__Region.png b/_site/doxygen/classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region_1_1Trust__Region.png deleted file mode 100644 index 76ad25f3..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region_1_1Trust__Region.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region__Optimization_1_1Trust__Region__Optimization-members.html b/_site/doxygen/classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region__Optimization_1_1Trust__Region__Optimization-members.html deleted file mode 100644 index 7f59f1f1..00000000 --- a/_site/doxygen/classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region__Optimization_1_1Trust__Region__Optimization-members.html +++ /dev/null @@ -1,154 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
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-
-
- - - -
-
- -
-
-
- -
- -
-
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- -
- -
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-
SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization Member List
-
-
- -

This is the complete list of members for SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization, including all inherited members.

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__defaults__(self)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization
__delattr__(self, k)SUAVE.Core.Data.Data
__getattribute__(self, k)SUAVE.Core.Data.Data
__init__(self, args, kwarg)SUAVE.Core.Data.Data
__iter__(self)SUAVE.Core.Data.Data
__new__(cls, args, kwarg)SUAVE.Core.Data.Data
__setattr__(self, k, v)SUAVE.Core.Data.Data
__str__(self, indent='')SUAVE.Core.Data.Data
accuracy_ratio(self, f_center, f_hi, f_corr, g_viol_center, g_viol_hi, g_viol_corr, tr)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization
append(self, value, key=None)SUAVE.Core.Data.Data
calculate_constraint_violation(self, gval, lb, ub)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization
calculate_correction(self, f, df, g, dg, tr)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization
convergence_tolerance (defined in SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization
dataname(self)SUAVE.Core.Data.Data
deep_get(self, keys)SUAVE.Core.Data.Data
deep_set(self, keys, val)SUAVE.Core.Data.Data
difference_interval (defined in SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization
do_recursive(self, method, other=None, default=None)SUAVE.Core.Data.Data
evaluate_constraints(self, x, problem=None, corrections=None, tr=None, lb=None, ub=None)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization
evaluate_corrected_model(self, x, problem=None, corrections=None, tr=None)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization
evaluate_model(self, problem, x, der_flag=True)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization
evaluation_order (defined in SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization
fidelity_levels (defined in SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization
get_bases(self)SUAVE.Core.Data.Data
itervalues(self)SUAVE.Core.Data.Data
optimize(self, problem, print_output=False)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization
optimizer (defined in SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization
optimizer_constraint_tolerance (defined in SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization
optimizer_convergence_tolerance (defined in SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization
optimizer_function_precision (defined in SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization
optimizer_max_iterations (defined in SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization
optimizer_verify_level (defined in SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization
pack_array(self, output='vector')SUAVE.Core.Data.Data
scale_vals(self, inp, con, ini, bnd, scl)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization
tag (defined in SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization
trust_region_function_precision (defined in SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization
trust_region_max_iterations (defined in SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization
typestring(self)SUAVE.Core.Data.Data
unpack_array(self, M)SUAVE.Core.Data.Data
update(self, other)SUAVE.Core.Data.Data
update_tr_size(self, rho, tr, accepted)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization
values(self)SUAVE.Core.Data.Data
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region__Optimization_1_1Trust__Region__Optimization.html b/_site/doxygen/classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region__Optimization_1_1Trust__Region__Optimization.html deleted file mode 100644 index 9e35e7ad..00000000 --- a/_site/doxygen/classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region__Optimization_1_1Trust__Region__Optimization.html +++ /dev/null @@ -1,925 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization Class Reference
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-Inheritance diagram for SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization:
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- - -SUAVE.Core.Data.Data - -
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-Public Member Functions

def __defaults__ (self)
 
def optimize (self, problem, print_output=False)
 
def evaluate_model (self, problem, x, der_flag=True)
 
def evaluate_corrected_model (self, x, problem=None, corrections=None, tr=None)
 
def evaluate_constraints (self, x, problem=None, corrections=None, tr=None, lb=None, ub=None)
 
def calculate_constraint_violation (self, gval, lb, ub)
 
def calculate_correction (self, f, df, g, dg, tr)
 
def scale_vals (self, inp, con, ini, bnd, scl)
 
def accuracy_ratio (self, f_center, f_hi, f_corr, g_viol_center, g_viol_hi, g_viol_corr, tr)
 
def update_tr_size (self, rho, tr, accepted)
 
- Public Member Functions inherited from SUAVE.Core.Data.Data
def __getattribute__ (self, k)
 
def __setattr__ (self, k, v)
 
def __delattr__ (self, k)
 
def __defaults__ (self)
 
def __new__ (cls, args, kwarg)
 
def typestring (self)
 
def dataname (self)
 
def __str__ (self, indent='')
 
def __init__ (self, args, kwarg)
 
def __iter__ (self)
 
def itervalues (self)
 
def values (self)
 
def update (self, other)
 
def get_bases (self)
 
def append (self, value, key=None)
 
def deep_set (self, keys, val)
 
def deep_get (self, keys)
 
def pack_array (self, output='vector')
 
def unpack_array (self, M)
 
def do_recursive (self, method, other=None, default=None)
 
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-Public Attributes

tag
 
trust_region_max_iterations
 
optimizer_max_iterations
 
convergence_tolerance
 
optimizer_convergence_tolerance
 
optimizer_constraint_tolerance
 
difference_interval
 
optimizer_function_precision
 
trust_region_function_precision
 
optimizer_verify_level
 
fidelity_levels
 
evaluation_order
 
optimizer
 
-

Detailed Description

-
A trust region optimization
-
-Assumptions:
-Only SNOPT is implemented
-
-Source:
-None
-

Member Function Documentation

- -

◆ __defaults__()

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def SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization.__defaults__ ( self)
-
-
This sets the default values.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-None
-
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- -

◆ accuracy_ratio()

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def SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization.accuracy_ratio ( self,
 f_center,
 f_hi,
 f_corr,
 g_viol_center,
 g_viol_hi,
 g_viol_corr,
 tr 
)
-
-
Compute the trust region accuracy ratio.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-f_center                   Objective value at the center of the trust region
-f_hi                       High-fidelity objective value at the expected optimum
-f_corr                     Corrected low-fidelity objective value at the expected optimum
-g_viol_center              Constraint violation at the center of the trust region
-g_viol_hi                  High-fidelity constraint violation at the expected optimum
-g_viol_corr                Corrected low-fidelity constraint violation at the expected optimum
-tr.evaluation_function(..)
-
-Outputs:
-rho                        [-] accuracy ratio
-
-Properties Used:
-self.trust_region_function_precision [-]
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◆ calculate_constraint_violation()

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def SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization.calculate_constraint_violation ( self,
 gval,
 lb,
 ub 
)
-
-
Calculates the constraint violation using a 2-norm of the violated constraint values.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-gval                     <numpy array> constraint values
-lb                       <numpy array> lower bounds on the constraints
-up                       <numpy array> upper bounds on the constraints
-
-Outputs:
-constraint violation     [-]
-
-Properties Used:
-None
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◆ calculate_correction()

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def SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization.calculate_correction ( self,
 f,
 df,
 g,
 dg,
 tr 
)
-
-
Calculates additive correction factors.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-f  - function value      <float>
-df - derivative of f     <numpy array>
-g  - constraint value    <numpy array> (only returned if der_flag is True)
-dg - jacobian of g       <numpy array> (only returned if der_flag is True)
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-Outputs:
-corr                     <tuple> correction factors
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-Properties Used:
-None
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◆ evaluate_constraints()

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def SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization.evaluate_constraints ( self,
 x,
 problem = None,
 corrections = None,
 tr = None,
 lb = None,
 ub = None 
)
-
-
Evaluates the SUAVE nexus problem provides an objective value based on constraint violation.
-Correction factors are applied to the evaluation results.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-problem.                 <Nexus class>
-  objective(..)
-  all_constraints(..)
-corrections              <tuple> Contains correction factors
-tr.center                <numpy array>
-lb                       <numpy array> lower bounds on the constraints
-up                       <numpy array> upper bounds on the constraints
-
-Outputs:
-obj_cons                 objective based on constraint violation
-cons                     list of contraint values
-fail                     indicates if the evaluation was successful
-
-Properties Used:
-self.calculate_constraint_violation(..)
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◆ evaluate_corrected_model()

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def SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization.evaluate_corrected_model ( self,
 x,
 problem = None,
 corrections = None,
 tr = None 
)
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Evaluates the SUAVE nexus problem and applies corrections to the results.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-problem.                 <Nexus class>
-  objective(..)
-  all_constraints(..)
-corrections              <tuple> Contains correction factors
-tr.center                <array>
-
-Outputs:
-obj                      function objective
-cons                     list of contraint values
-fail                     indicates if the evaluation was successful
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-Properties Used:
-None
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◆ evaluate_model()

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def SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization.evaluate_model ( self,
 problem,
 x,
 der_flag = True 
)
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Evaluates the SUAVE nexus problem. This is often a mission evaluation.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-problem.                 <Nexus class>
-  objective(..)
-  all_constraints(..)
-  finite difference(..)
-x                        <numpy array>
-der_flag                 <boolean>  Determines if finite differencing is done
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-Outputs:
-f  - function value      <float>
-df - derivative of f     <numpy array>
-g  - constraint value    <numpy array> (only returned if der_flag is True)
-dg - jacobian of g       <numpy array> (only returned if der_flag is True)
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-Properties Used:
-self.difference_interval [-]
-
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◆ optimize()

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def SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization.optimize ( self,
 problem,
 print_output = False 
)
-
-
Optimizes the problem
-
-Assumptions:
-Currently only works with SNOPT
-
-Source:
-"A trust-region framework for managing the use of approximation models in optimization," Alexandrov et. al., 1998
-Details do not follow exactly.
-
-Inputs:
-problem.                 <Nexus class> (also passed into other functions)
-  optimization_problem. 
-    inputs               Numpy array matching standard SUAVE optimization setup
-    objective            Numpy array matching standard SUAVE optimization setup
-    constraints          Numpy array matching standard SUAVE optimization setup
-  fidelity_level         [-]
-print_output             <boolean> Determines if output is printed during the optimization run
-
-Outputs:
-(fOpt_corr,xOpt_corr,str):
-    fOpt_corr            <float>
-    xOpt_corr            <numpy array>
-    str                  Varies depending on the result of the optimization
-    
-
-Properties Used:
-self.
-  trust_region_max_iterations         [-]    
-  fidelity_levels                     [-]
-  evaluation_order                    List of the fidelity level order
-  evaluate_model(..)
-  calculate_correction(..)
-  calculate_constraint_violation(..)
-  optimizer                           <string> Determines what optimizer is used
-  evaluate_corrected_model(..)
-  optimizer_max_iterations            [-]
-  optimizer_convergence_tolerance     [-]
-  optimizer_constraint_tolerance      [-]
-  optimizer_function_precision        [-]
-  optimizer_verify_level              Int determining if SNOPT will verify that the minimum is level
-  accuracy_ratio(..)
-  update_tr_size(..)
-  convergance_tolerance               [-]
-
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◆ scale_vals()

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def SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization.scale_vals ( self,
 inp,
 con,
 ini,
 bnd,
 scl 
)
-
-
Scales inputs, constraints, and their bounds.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-(all SUAVE format specific numpy arrays)
-inp                 Design variables
-con                 Constraint limits
-ini                 Initial values
-bnd                 Variable bounds
-scl                 Scaling factors
-
-Outputs:
-x                   <numpy array> Scaled design variables
-scaled_constraints  <numpy array>
-x_low_bound         <numpy array>
-x_up_bound          <numpy array>
-con_up_edge         <numpy array>
-con_low_edge        <numpy array>
-name                <list of strings> List of variable names
-
-Properties Used:
-None
-
-
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- -

◆ update_tr_size()

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def SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization.update_tr_size ( self,
 rho,
 tr,
 accepted 
)
-
-
Updates the trust region size based on the accuracy ratio and if it has been accepted.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-rho                  [-] accuracy ratio
-tr. 
-  size               [-]
-  contraction_factor [-]
-  contract_threshold [-]
-  expand_threshold   [-]
-  expansion_factor   [-]
-
-Outputs:
-tr_action            [-] number indicating the type of action done by the trust region
-
-Properties Used:
-None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Optimization/Package_Setups/TRMM/Trust_Region_Optimization.py
  • -
-
-
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- - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Optimization.Surrogate_Optimization.Surrogate_Optimization Member List
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- -

This is the complete list of members for SUAVE.Optimization.Surrogate_Optimization.Surrogate_Optimization, including all inherited members.

- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
__defaults__(self)SUAVE.Optimization.Surrogate_Optimization.Surrogate_Optimization
__delattr__(self, k)SUAVE.Core.Data.Data
__getattribute__(self, k)SUAVE.Core.Data.Data
__init__(self, args, kwarg)SUAVE.Core.Data.Data
__iter__(self)SUAVE.Core.Data.Data
__new__(cls, args, kwarg)SUAVE.Core.Data.Data
__setattr__(self, k, v)SUAVE.Core.Data.Data
__str__(self, indent='')SUAVE.Core.Data.Data
append(self, value, key=None)SUAVE.Core.Data.Data
build_surrogate(self)SUAVE.Optimization.Surrogate_Optimization.Surrogate_Optimization
dataname(self)SUAVE.Core.Data.Data
deep_get(self, keys)SUAVE.Core.Data.Data
deep_set(self, keys, val)SUAVE.Core.Data.Data
do_recursive(self, method, other=None, default=None)SUAVE.Core.Data.Data
get_bases(self)SUAVE.Core.Data.Data
iterative_optimization(self)SUAVE.Optimization.Surrogate_Optimization.Surrogate_Optimization
itervalues(self)SUAVE.Core.Data.Data
max_iterations (defined in SUAVE.Optimization.Surrogate_Optimization.Surrogate_Optimization)SUAVE.Optimization.Surrogate_Optimization.Surrogate_Optimization
number_of_points (defined in SUAVE.Optimization.Surrogate_Optimization.Surrogate_Optimization)SUAVE.Optimization.Surrogate_Optimization.Surrogate_Optimization
optimization_filename (defined in SUAVE.Optimization.Surrogate_Optimization.Surrogate_Optimization)SUAVE.Optimization.Surrogate_Optimization.Surrogate_Optimization
optimizer (defined in SUAVE.Optimization.Surrogate_Optimization.Surrogate_Optimization)SUAVE.Optimization.Surrogate_Optimization.Surrogate_Optimization
pack_array(self, output='vector')SUAVE.Core.Data.Data
problem (defined in SUAVE.Optimization.Surrogate_Optimization.Surrogate_Optimization)SUAVE.Optimization.Surrogate_Optimization.Surrogate_Optimization
sample_plan (defined in SUAVE.Optimization.Surrogate_Optimization.Surrogate_Optimization)SUAVE.Optimization.Surrogate_Optimization.Surrogate_Optimization
surrogate_model (defined in SUAVE.Optimization.Surrogate_Optimization.Surrogate_Optimization)SUAVE.Optimization.Surrogate_Optimization.Surrogate_Optimization
typestring(self)SUAVE.Core.Data.Data
unpack_array(self, M)SUAVE.Core.Data.Data
update(self, other)SUAVE.Core.Data.Data
values(self)SUAVE.Core.Data.Data
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Optimization_1_1Surrogate__Optimization_1_1Surrogate__Optimization.html b/_site/doxygen/classSUAVE_1_1Optimization_1_1Surrogate__Optimization_1_1Surrogate__Optimization.html deleted file mode 100644 index 49db88e8..00000000 --- a/_site/doxygen/classSUAVE_1_1Optimization_1_1Surrogate__Optimization_1_1Surrogate__Optimization.html +++ /dev/null @@ -1,315 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Optimization.Surrogate_Optimization.Surrogate_Optimization Class Reference - - - - - - - - - - - - - - - -
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- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Optimization.Surrogate_Optimization.Surrogate_Optimization Class Reference
-
-
-
-Inheritance diagram for SUAVE.Optimization.Surrogate_Optimization.Surrogate_Optimization:
-
-
- - -SUAVE.Core.Data.Data - -
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def build_surrogate (self)
 
def iterative_optimization (self)
 
- Public Member Functions inherited from SUAVE.Core.Data.Data
def __getattribute__ (self, k)
 
def __setattr__ (self, k, v)
 
def __delattr__ (self, k)
 
def __defaults__ (self)
 
def __new__ (cls, args, kwarg)
 
def typestring (self)
 
def dataname (self)
 
def __str__ (self, indent='')
 
def __init__ (self, args, kwarg)
 
def __iter__ (self)
 
def itervalues (self)
 
def values (self)
 
def update (self, other)
 
def get_bases (self)
 
def append (self, value, key=None)
 
def deep_set (self, keys, val)
 
def deep_get (self, keys)
 
def pack_array (self, output='vector')
 
def unpack_array (self, M)
 
def do_recursive (self, method, other=None, default=None)
 
- - - - - - - - - - - - - - - -

-Public Attributes

sample_plan
 
problem
 
optimizer
 
surrogate_model
 
optimization_filename
 
number_of_points
 
max_iterations
 
-

Detailed Description

-
Takes a SUAVE Optimization problem, builds a surrogate around it, 
-    and iteratively finds the optimum of the surrogate, then samples at that point.
-    Stops when you hit max_iterations or it converges
-    
-    Assumptions:
-    You're okay with represeting your problem with a surrogate
-    
-    Source:
-    N/A
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Optimization.Surrogate_Optimization.Surrogate_Optimization.__defaults__ ( self)
-
-
This sets the default values.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
- -

◆ build_surrogate()

- -
-
- - - - - - - - -
def SUAVE.Optimization.Surrogate_Optimization.Surrogate_Optimization.build_surrogate ( self)
-
-
Builds a surrogate for the problem
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
- -

◆ iterative_optimization()

- -
-
- - - - - - - - -
def SUAVE.Optimization.Surrogate_Optimization.Surrogate_Optimization.iterative_optimization ( self)
-
-
Optimizes iteratively 
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    output_real        [float]
-    surrogate_problem  [surrogate]
-    
-    Properties Used:
-    None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Optimization/Surrogate_Optimization.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Optimization_1_1Surrogate__Optimization_1_1Surrogate__Optimization.js b/_site/doxygen/classSUAVE_1_1Optimization_1_1Surrogate__Optimization_1_1Surrogate__Optimization.js deleted file mode 100644 index a9991bb7..00000000 --- a/_site/doxygen/classSUAVE_1_1Optimization_1_1Surrogate__Optimization_1_1Surrogate__Optimization.js +++ /dev/null @@ -1,13 +0,0 @@ -var classSUAVE_1_1Optimization_1_1Surrogate__Optimization_1_1Surrogate__Optimization = -[ - [ "__defaults__", "classSUAVE_1_1Optimization_1_1Surrogate__Optimization_1_1Surrogate__Optimization.html#ae8ce39024fb5917c848d91c5add786ce", null ], - [ "build_surrogate", "classSUAVE_1_1Optimization_1_1Surrogate__Optimization_1_1Surrogate__Optimization.html#a63e93b8ba59c2d6bbb07aa814236f61a", null ], - [ "iterative_optimization", "classSUAVE_1_1Optimization_1_1Surrogate__Optimization_1_1Surrogate__Optimization.html#a56fa475f7dc914e93945ec4b3e3af438", null ], - [ "max_iterations", "classSUAVE_1_1Optimization_1_1Surrogate__Optimization_1_1Surrogate__Optimization.html#ad98abbf7bb6c0a6e4e023473728ced2e", null ], - [ "number_of_points", "classSUAVE_1_1Optimization_1_1Surrogate__Optimization_1_1Surrogate__Optimization.html#a8f4c1f2cecad013cb541b60318df008b", null ], - [ "optimization_filename", "classSUAVE_1_1Optimization_1_1Surrogate__Optimization_1_1Surrogate__Optimization.html#abb9a78d20b3137abee2f6f2405bffeaf", null ], - [ "optimizer", "classSUAVE_1_1Optimization_1_1Surrogate__Optimization_1_1Surrogate__Optimization.html#a2cb5764be64a11fbb024dc84faedb7fb", null ], - [ "problem", "classSUAVE_1_1Optimization_1_1Surrogate__Optimization_1_1Surrogate__Optimization.html#a4a97c733a972daf4410a23200582da34", null ], - [ "sample_plan", "classSUAVE_1_1Optimization_1_1Surrogate__Optimization_1_1Surrogate__Optimization.html#a3c78ec269e1836c9cf26ce4e6fad5a4f", null ], - [ "surrogate_model", "classSUAVE_1_1Optimization_1_1Surrogate__Optimization_1_1Surrogate__Optimization.html#afdcd53b3cd62007eefa0df27a4e75ae6", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Optimization_1_1Surrogate__Optimization_1_1Surrogate__Optimization.png b/_site/doxygen/classSUAVE_1_1Optimization_1_1Surrogate__Optimization_1_1Surrogate__Optimization.png deleted file mode 100644 index 575fb41e..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Optimization_1_1Surrogate__Optimization_1_1Surrogate__Optimization.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1compat_1_1ChainMap-members.html b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1compat_1_1ChainMap-members.html deleted file mode 100644 index 90bd8843..00000000 --- a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1compat_1_1ChainMap-members.html +++ /dev/null @@ -1,131 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
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SUAVE.Plugins.pint.compat.ChainMap Member List
-
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- -

This is the complete list of members for SUAVE.Plugins.pint.compat.ChainMap, including all inherited members.

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__bool__(self) (defined in SUAVE.Plugins.pint.compat.ChainMap)SUAVE.Plugins.pint.compat.ChainMap
__contains__(self, key) (defined in SUAVE.Plugins.pint.compat.ChainMap)SUAVE.Plugins.pint.compat.ChainMap
__delitem__(self, key) (defined in SUAVE.Plugins.pint.compat.ChainMap)SUAVE.Plugins.pint.compat.ChainMap
__getitem__(self, key) (defined in SUAVE.Plugins.pint.compat.ChainMap)SUAVE.Plugins.pint.compat.ChainMap
__init__(self, maps)SUAVE.Plugins.pint.compat.ChainMap
__iter__(self) (defined in SUAVE.Plugins.pint.compat.ChainMap)SUAVE.Plugins.pint.compat.ChainMap
__len__(self) (defined in SUAVE.Plugins.pint.compat.ChainMap)SUAVE.Plugins.pint.compat.ChainMap
__missing__(self, key) (defined in SUAVE.Plugins.pint.compat.ChainMap)SUAVE.Plugins.pint.compat.ChainMap
__repr__(self) (defined in SUAVE.Plugins.pint.compat.ChainMap)SUAVE.Plugins.pint.compat.ChainMap
__setitem__(self, key, value) (defined in SUAVE.Plugins.pint.compat.ChainMap)SUAVE.Plugins.pint.compat.ChainMap
clear(self) (defined in SUAVE.Plugins.pint.compat.ChainMap)SUAVE.Plugins.pint.compat.ChainMap
copy(self) (defined in SUAVE.Plugins.pint.compat.ChainMap)SUAVE.Plugins.pint.compat.ChainMap
fromkeys(cls, iterable, args) (defined in SUAVE.Plugins.pint.compat.ChainMap)SUAVE.Plugins.pint.compat.ChainMap
get(self, key, default=None) (defined in SUAVE.Plugins.pint.compat.ChainMap)SUAVE.Plugins.pint.compat.ChainMap
maps (defined in SUAVE.Plugins.pint.compat.ChainMap)SUAVE.Plugins.pint.compat.ChainMap
new_child(self, m=None)SUAVE.Plugins.pint.compat.ChainMap
parents(self) (defined in SUAVE.Plugins.pint.compat.ChainMap)SUAVE.Plugins.pint.compat.ChainMap
pop(self, key, args) (defined in SUAVE.Plugins.pint.compat.ChainMap)SUAVE.Plugins.pint.compat.ChainMap
popitem(self) (defined in SUAVE.Plugins.pint.compat.ChainMap)SUAVE.Plugins.pint.compat.ChainMap
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1compat_1_1ChainMap.html b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1compat_1_1ChainMap.html deleted file mode 100644 index 289ccc9b..00000000 --- a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1compat_1_1ChainMap.html +++ /dev/null @@ -1,258 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Plugins.pint.compat.ChainMap Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
-
- - - -
-
- -
-
-
- -
- -
-
- - -
- -
- -
- -
-
SUAVE.Plugins.pint.compat.ChainMap Class Reference
-
-
-
-Inheritance diagram for SUAVE.Plugins.pint.compat.ChainMap:
-
-
- - -SUAVE.Plugins.pint.context.ContextChain - -
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __init__ (self, maps)
 
-def __missing__ (self, key)
 
-def __getitem__ (self, key)
 
-def get (self, key, default=None)
 
-def __len__ (self)
 
-def __iter__ (self)
 
-def __contains__ (self, key)
 
-def __bool__ (self)
 
-def __repr__ (self)
 
-def fromkeys (cls, iterable, args)
 
-def copy (self)
 
def new_child (self, m=None)
 
-def parents (self)
 
-def __setitem__ (self, key, value)
 
-def __delitem__ (self, key)
 
-def popitem (self)
 
-def pop (self, key, args)
 
-def clear (self)
 
- - - -

-Public Attributes

maps
 
-

Detailed Description

-
A ChainMap groups multiple dicts (or other mappings) together
-to create a single, updateable view.
-
-The underlying mappings are stored in a list.  That list is public and can
-accessed or updated using the *maps* attribute.  There is no other state.
-
-Lookups search the underlying mappings successively until a key is found.
-In contrast, writes, updates, and deletions only operate on the first
-mapping.

Constructor & Destructor Documentation

- -

◆ __init__()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Plugins.pint.compat.ChainMap.__init__ ( self,
 maps 
)
-
-
Initialize a ChainMap by setting *maps* to the given mappings.
-If no mappings are provided, a single empty dictionary is used.
-
-
-

Member Function Documentation

- -

◆ new_child()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Plugins.pint.compat.ChainMap.new_child ( self,
 m = None 
)
-
-
New ChainMap with a new map followed by all previous maps. If no
-map is provided, an empty dict is used.
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Plugins/pint/compat.py
  • -
-
-
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-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
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SUAVE.Plugins.pint.context.Context Member List
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- -
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1context_1_1Context.html b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1context_1_1Context.html deleted file mode 100644 index d547731c..00000000 --- a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1context_1_1Context.html +++ /dev/null @@ -1,355 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Plugins.pint.context.Context Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Plugins.pint.context.Context Class Reference
-
-
-
-Inheritance diagram for SUAVE.Plugins.pint.context.Context:
-
-
- - - -
- - - - - - - - - - - - - - -

-Public Member Functions

-def __init__ (self, name, aliases=(), defaults=None)
 
def from_context (cls, context, defaults)
 
-def from_lines (cls, lines, to_base_func=None)
 
def add_transformation (self, src, dst, func)
 
def remove_transformation (self, src, dst)
 
def transform (self, src, dst, registry, value)
 
- - - -

-Static Public Member Functions

-def __keytransform__ (src, dst)
 
- - - - - - - - - - - -

-Public Attributes

name
 
aliases
 
funcs
 
defaults
 
relation_to_context
 
-

Detailed Description

-
A specialized container that defines transformation functions from
-one dimension to another. Each Dimension are specified using a UnitsContainer.
-Simple transformation are given with a function taking a single parameter.
-
-    >>> timedim = UnitsContainer({'[time]': 1})
-    >>> spacedim = UnitsContainer({'[length]': 1})
-    >>> def f(time):
-    ...     'Time to length converter'
-    ...     return 3. * time
-    >>> c = Context()
-    >>> c.add_transformation(timedim, spacedim, f)
-    >>> c.transform(timedim, spacedim, 2)
-    6
-
-Conversion functions may take optional keyword arguments and the context can
-have default values for these arguments.
-
-    >>> def f(time, n):
-    ...     'Time to length converter, n is the index of refraction of the material'
-    ...     return 3. * time / n
-    >>> c = Context(n=3)
-    >>> c.add_transformation(timedim, spacedim, f)
-    >>> c.transform(timedim, spacedim, 2)
-    2

Member Function Documentation

- -

◆ add_transformation()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Plugins.pint.context.Context.add_transformation ( self,
 src,
 dst,
 func 
)
-
-
Add a transformation function to the context.
-
-
-
- -

◆ from_context()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Plugins.pint.context.Context.from_context ( cls,
 context,
 defaults 
)
-
-
Creates a new context that shares the funcs dictionary with the original
-context. The default values are copied from the original context and updated
-with the new defaults.
-
-If defaults is empty, return the same context.
-
-
-
- -

◆ remove_transformation()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Plugins.pint.context.Context.remove_transformation ( self,
 src,
 dst 
)
-
-
Add a transformation function to the context.
-
-
-
- -

◆ transform()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Plugins.pint.context.Context.transform ( self,
 src,
 dst,
 registry,
 value 
)
-
-
Transform a value.
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Plugins/pint/context.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1context_1_1Context.js b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1context_1_1Context.js deleted file mode 100644 index e2ad58b9..00000000 --- a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1context_1_1Context.js +++ /dev/null @@ -1,14 +0,0 @@ -var classSUAVE_1_1Plugins_1_1pint_1_1context_1_1Context = -[ - [ "__init__", "classSUAVE_1_1Plugins_1_1pint_1_1context_1_1Context.html#a711c56099d5f4a057c17a2e291271ee2", null ], - [ "add_transformation", "classSUAVE_1_1Plugins_1_1pint_1_1context_1_1Context.html#a6c6e5ca70615d646dc9aa6f42c606d58", null ], - [ "from_context", "classSUAVE_1_1Plugins_1_1pint_1_1context_1_1Context.html#a66f98a4dd9ae08e15b32961914f5641b", null ], - [ "from_lines", "classSUAVE_1_1Plugins_1_1pint_1_1context_1_1Context.html#aeb8be96e54ea025d281ab6ce89656295", null ], - [ "remove_transformation", "classSUAVE_1_1Plugins_1_1pint_1_1context_1_1Context.html#a9289ff4f315744f7d3f72ba5e0af1a98", null ], - [ "transform", "classSUAVE_1_1Plugins_1_1pint_1_1context_1_1Context.html#abb6b6f8bbf8264656eb0d35a0a6be9b2", null ], - [ "aliases", "classSUAVE_1_1Plugins_1_1pint_1_1context_1_1Context.html#a95e4e35e488c8bbfd43ca0295b1a484b", null ], - [ "defaults", "classSUAVE_1_1Plugins_1_1pint_1_1context_1_1Context.html#a6a4f0e82e92994c3d08ca36cab5278cc", null ], - [ "funcs", "classSUAVE_1_1Plugins_1_1pint_1_1context_1_1Context.html#a24acde1a712ceff4eaed00ec94f9a7e2", null ], - [ "name", "classSUAVE_1_1Plugins_1_1pint_1_1context_1_1Context.html#a005a8858ee14e54c6b6cf804a70add56", null ], - [ "relation_to_context", "classSUAVE_1_1Plugins_1_1pint_1_1context_1_1Context.html#a01b58f6e684af0667b8e400eb0ce4cf6", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1context_1_1Context.png b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1context_1_1Context.png deleted file mode 100644 index d4457382..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1context_1_1Context.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1context_1_1ContextChain-members.html b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1context_1_1ContextChain-members.html deleted file mode 100644 index b29b406b..00000000 --- a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1context_1_1ContextChain-members.html +++ /dev/null @@ -1,137 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
-
- - - -
-
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-
-
- -
- -
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SUAVE.Plugins.pint.context.ContextChain Member List
-
-
- -

This is the complete list of members for SUAVE.Plugins.pint.context.ContextChain, including all inherited members.

- - - - - - - - - - - - - - - - - - - - - - - - - - -
__bool__(self) (defined in SUAVE.Plugins.pint.compat.ChainMap)SUAVE.Plugins.pint.compat.ChainMap
__contains__(self, key) (defined in SUAVE.Plugins.pint.compat.ChainMap)SUAVE.Plugins.pint.compat.ChainMap
__delitem__(self, key) (defined in SUAVE.Plugins.pint.compat.ChainMap)SUAVE.Plugins.pint.compat.ChainMap
__getitem__(self, key) (defined in SUAVE.Plugins.pint.compat.ChainMap)SUAVE.Plugins.pint.compat.ChainMap
__init__(self, args, kwargs) (defined in SUAVE.Plugins.pint.context.ContextChain)SUAVE.Plugins.pint.context.ContextChain
SUAVE::Plugins::pint::compat::ChainMap.__init__(self, maps)SUAVE.Plugins.pint.compat.ChainMap
__iter__(self) (defined in SUAVE.Plugins.pint.compat.ChainMap)SUAVE.Plugins.pint.compat.ChainMap
__len__(self) (defined in SUAVE.Plugins.pint.compat.ChainMap)SUAVE.Plugins.pint.compat.ChainMap
__missing__(self, key) (defined in SUAVE.Plugins.pint.compat.ChainMap)SUAVE.Plugins.pint.compat.ChainMap
__repr__(self) (defined in SUAVE.Plugins.pint.compat.ChainMap)SUAVE.Plugins.pint.compat.ChainMap
__setitem__(self, key, value) (defined in SUAVE.Plugins.pint.compat.ChainMap)SUAVE.Plugins.pint.compat.ChainMap
clear(self) (defined in SUAVE.Plugins.pint.compat.ChainMap)SUAVE.Plugins.pint.compat.ChainMap
copy(self) (defined in SUAVE.Plugins.pint.compat.ChainMap)SUAVE.Plugins.pint.compat.ChainMap
defaults(self) (defined in SUAVE.Plugins.pint.context.ContextChain)SUAVE.Plugins.pint.context.ContextChain
fromkeys(cls, iterable, args) (defined in SUAVE.Plugins.pint.compat.ChainMap)SUAVE.Plugins.pint.compat.ChainMap
get(self, key, default=None) (defined in SUAVE.Plugins.pint.compat.ChainMap)SUAVE.Plugins.pint.compat.ChainMap
graph(self)SUAVE.Plugins.pint.context.ContextChain
insert_contexts(self, contexts)SUAVE.Plugins.pint.context.ContextChain
maps (defined in SUAVE.Plugins.pint.context.ContextChain)SUAVE.Plugins.pint.context.ContextChain
new_child(self, m=None)SUAVE.Plugins.pint.compat.ChainMap
parents(self) (defined in SUAVE.Plugins.pint.compat.ChainMap)SUAVE.Plugins.pint.compat.ChainMap
pop(self, key, args) (defined in SUAVE.Plugins.pint.compat.ChainMap)SUAVE.Plugins.pint.compat.ChainMap
popitem(self) (defined in SUAVE.Plugins.pint.compat.ChainMap)SUAVE.Plugins.pint.compat.ChainMap
remove_contexts(self, n)SUAVE.Plugins.pint.context.ContextChain
transform(self, src, dst, registry, value)SUAVE.Plugins.pint.context.ContextChain
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1context_1_1ContextChain.html b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1context_1_1ContextChain.html deleted file mode 100644 index 1d78fb89..00000000 --- a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1context_1_1ContextChain.html +++ /dev/null @@ -1,342 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Plugins.pint.context.ContextChain Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
-
- - - -
-
- -
-
-
- -
- -
-
- - -
- -
- -
- -
-
SUAVE.Plugins.pint.context.ContextChain Class Reference
-
-
-
-Inheritance diagram for SUAVE.Plugins.pint.context.ContextChain:
-
-
- - -SUAVE.Plugins.pint.compat.ChainMap - -
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

-def __init__ (self, args, kwargs)
 
def insert_contexts (self, contexts)
 
def remove_contexts (self, n)
 
-def defaults (self)
 
def graph (self)
 
def transform (self, src, dst, registry, value)
 
- Public Member Functions inherited from SUAVE.Plugins.pint.compat.ChainMap
def __init__ (self, maps)
 
-def __missing__ (self, key)
 
-def __getitem__ (self, key)
 
-def get (self, key, default=None)
 
-def __len__ (self)
 
-def __iter__ (self)
 
-def __contains__ (self, key)
 
-def __bool__ (self)
 
-def __repr__ (self)
 
-def fromkeys (cls, iterable, args)
 
-def copy (self)
 
def new_child (self, m=None)
 
-def parents (self)
 
-def __setitem__ (self, key, value)
 
-def __delitem__ (self, key)
 
-def popitem (self)
 
-def pop (self, key, args)
 
-def clear (self)
 
- - - - - - -

-Public Attributes

maps
 
- Public Attributes inherited from SUAVE.Plugins.pint.compat.ChainMap
maps
 
-

Detailed Description

-
A specialized ChainMap for contexts that simplifies finding rules
-to transform from one dimension to another.
-

Member Function Documentation

- -

◆ graph()

- -
-
- - - - - - - - -
def SUAVE.Plugins.pint.context.ContextChain.graph ( self)
-
-
The graph relating
-
-
-
- -

◆ insert_contexts()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Plugins.pint.context.ContextChain.insert_contexts ( self,
 contexts 
)
-
-
Insert one or more contexts in reversed order the chained map.
-(A rule in last context will take precedence)
-
-To facilitate the identification of the context with the matching rule,
-the *relation_to_context* dictionary of the context is used.
-
-
-
- -

◆ remove_contexts()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Plugins.pint.context.ContextChain.remove_contexts ( self,
 n 
)
-
-
Remove the last n inserted contexts from the chain.
-
-
-
- -

◆ transform()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Plugins.pint.context.ContextChain.transform ( self,
 src,
 dst,
 registry,
 value 
)
-
-
Transform the value, finding the rule in the chained context.
-(A rule in last context will take precedence)
-
-:raises: KeyError if the rule is not found.
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Plugins/pint/context.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1context_1_1ContextChain.js b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1context_1_1ContextChain.js deleted file mode 100644 index 318cc48f..00000000 --- a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1context_1_1ContextChain.js +++ /dev/null @@ -1,10 +0,0 @@ -var classSUAVE_1_1Plugins_1_1pint_1_1context_1_1ContextChain = -[ - [ "__init__", "classSUAVE_1_1Plugins_1_1pint_1_1context_1_1ContextChain.html#a9af3606e14dd2ca683a6dfb088d7d6e2", null ], - [ "defaults", "classSUAVE_1_1Plugins_1_1pint_1_1context_1_1ContextChain.html#ae480e50e871f32994f9bee8ca90f9328", null ], - [ "graph", "classSUAVE_1_1Plugins_1_1pint_1_1context_1_1ContextChain.html#ad1f3b9b56633a6940846b225b4e7025d", null ], - [ "insert_contexts", "classSUAVE_1_1Plugins_1_1pint_1_1context_1_1ContextChain.html#a3cfbdc06d4624200eabf3f5be9409d18", null ], - [ "remove_contexts", "classSUAVE_1_1Plugins_1_1pint_1_1context_1_1ContextChain.html#a5f6e660044e5ca4e2abe5459f71b0741", null ], - [ "transform", "classSUAVE_1_1Plugins_1_1pint_1_1context_1_1ContextChain.html#a133967cefcb49a5c012dbd97dbd204e0", null ], - [ "maps", "classSUAVE_1_1Plugins_1_1pint_1_1context_1_1ContextChain.html#a59fa2befb0e787b0f3d61a9b03977225", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1context_1_1ContextChain.png b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1context_1_1ContextChain.png deleted file mode 100644 index c918bb97..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1context_1_1ContextChain.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1measurement_1_1Measurement-members.html b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1measurement_1_1Measurement-members.html deleted file mode 100644 index 211d88a0..00000000 --- a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1measurement_1_1Measurement-members.html +++ /dev/null @@ -1,124 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
-
- - - -
-
- -
-
-
- -
- -
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- - -
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SUAVE.Plugins.pint.measurement.Measurement Member List
-
-
- -

This is the complete list of members for SUAVE.Plugins.pint.measurement.Measurement, including all inherited members.

- - - - - - - - - - - - - -
__add__(self, other) (defined in SUAVE.Plugins.pint.measurement.Measurement)SUAVE.Plugins.pint.measurement.Measurement
__floordiv__(self, other) (defined in SUAVE.Plugins.pint.measurement.Measurement)SUAVE.Plugins.pint.measurement.Measurement
__format__(self, spec) (defined in SUAVE.Plugins.pint.measurement.Measurement)SUAVE.Plugins.pint.measurement.Measurement
__init__(self, value, error) (defined in SUAVE.Plugins.pint.measurement.Measurement)SUAVE.Plugins.pint.measurement.Measurement
__mul__(self, other) (defined in SUAVE.Plugins.pint.measurement.Measurement)SUAVE.Plugins.pint.measurement.Measurement
__repr__(self) (defined in SUAVE.Plugins.pint.measurement.Measurement)SUAVE.Plugins.pint.measurement.Measurement
__str__(self) (defined in SUAVE.Plugins.pint.measurement.Measurement)SUAVE.Plugins.pint.measurement.Measurement
__sub__(self, other) (defined in SUAVE.Plugins.pint.measurement.Measurement)SUAVE.Plugins.pint.measurement.Measurement
__truediv__(self, other) (defined in SUAVE.Plugins.pint.measurement.Measurement)SUAVE.Plugins.pint.measurement.Measurement
error(self) (defined in SUAVE.Plugins.pint.measurement.Measurement)SUAVE.Plugins.pint.measurement.Measurement
rel(self) (defined in SUAVE.Plugins.pint.measurement.Measurement)SUAVE.Plugins.pint.measurement.Measurement
value(self) (defined in SUAVE.Plugins.pint.measurement.Measurement)SUAVE.Plugins.pint.measurement.Measurement
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1measurement_1_1Measurement.html b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1measurement_1_1Measurement.html deleted file mode 100644 index 67898721..00000000 --- a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1measurement_1_1Measurement.html +++ /dev/null @@ -1,171 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Plugins.pint.measurement.Measurement Class Reference - - - - - - - - - - - - - - - -
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SUAVE.Plugins.pint.measurement.Measurement Class Reference
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-Public Member Functions

-def __init__ (self, value, error)
 
-def value (self)
 
-def error (self)
 
-def rel (self)
 
-def __add__ (self, other)
 
-def __sub__ (self, other)
 
-def __mul__ (self, other)
 
-def __truediv__ (self, other)
 
-def __floordiv__ (self, other)
 
-def __str__ (self)
 
-def __repr__ (self)
 
-def __format__ (self, spec)
 
-

Detailed Description

-
Implements a class to describe a quantity with uncertainty.
-
-:param value: The most likely value of the measurement.
-:type value: Quantity or Number
-:param error: The error or uncertainty of the measurement.
-:type value: Quantity or Number
-

The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Plugins/pint/measurement.py
  • -
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1measurement_1_1Measurement.js b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1measurement_1_1Measurement.js deleted file mode 100644 index 4b457d89..00000000 --- a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1measurement_1_1Measurement.js +++ /dev/null @@ -1,15 +0,0 @@ -var classSUAVE_1_1Plugins_1_1pint_1_1measurement_1_1Measurement = -[ - [ "__init__", "classSUAVE_1_1Plugins_1_1pint_1_1measurement_1_1Measurement.html#ae6f33f88d6cf091d7b492c6b0ce1551f", null ], - [ "__add__", "classSUAVE_1_1Plugins_1_1pint_1_1measurement_1_1Measurement.html#a083f335d365203b25009998323fd85a7", null ], - [ "__floordiv__", "classSUAVE_1_1Plugins_1_1pint_1_1measurement_1_1Measurement.html#ac19fb202ae05caad48cffcaee3c02591", null ], - [ "__format__", "classSUAVE_1_1Plugins_1_1pint_1_1measurement_1_1Measurement.html#a7e3a629553e14066347b36a981f506ba", null ], - [ "__mul__", "classSUAVE_1_1Plugins_1_1pint_1_1measurement_1_1Measurement.html#ad7675af2e52abacaeeb2fc1b3489e69a", null ], - [ "__repr__", "classSUAVE_1_1Plugins_1_1pint_1_1measurement_1_1Measurement.html#a3e74d9d9bbba22fb842ee745d68338dd", null ], - [ "__str__", "classSUAVE_1_1Plugins_1_1pint_1_1measurement_1_1Measurement.html#ab4635b80141e9f09067adc6d41233ad2", null ], - [ "__sub__", "classSUAVE_1_1Plugins_1_1pint_1_1measurement_1_1Measurement.html#a085f00193c7672906eeb02be89bd411c", null ], - [ "__truediv__", "classSUAVE_1_1Plugins_1_1pint_1_1measurement_1_1Measurement.html#a157d50839cc97e38e994d4aa352ef004", null ], - [ "error", "classSUAVE_1_1Plugins_1_1pint_1_1measurement_1_1Measurement.html#a791a3f3ba1a42537c79ccfb7b439eb58", null ], - [ "rel", "classSUAVE_1_1Plugins_1_1pint_1_1measurement_1_1Measurement.html#a1e816d7de765ba5e24107f4afcfb1128", null ], - [ "value", "classSUAVE_1_1Plugins_1_1pint_1_1measurement_1_1Measurement.html#a4c16e18ce3d78fe827ba1733c6e6d0d0", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1measurement_1_1Measurement.png b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1measurement_1_1Measurement.png deleted file mode 100644 index e61708be..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1measurement_1_1Measurement.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1quantity_1_1__Exception-members.html b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1quantity_1_1__Exception-members.html deleted file mode 100644 index b7adb9a7..00000000 --- a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1quantity_1_1__Exception-members.html +++ /dev/null @@ -1,114 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE.Plugins.pint.quantity._Exception Member List
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This is the complete list of members for SUAVE.Plugins.pint.quantity._Exception, including all inherited members.

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__init__(self, internal) (defined in SUAVE.Plugins.pint.quantity._Exception)SUAVE.Plugins.pint.quantity._Exception
internal (defined in SUAVE.Plugins.pint.quantity._Exception)SUAVE.Plugins.pint.quantity._Exception
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1quantity_1_1__Exception.html b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1quantity_1_1__Exception.html deleted file mode 100644 index dca23754..00000000 --- a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1quantity_1_1__Exception.html +++ /dev/null @@ -1,138 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Plugins.pint.quantity._Exception Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Plugins.pint.quantity._Exception Class Reference
-
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-Inheritance diagram for SUAVE.Plugins.pint.quantity._Exception:
-
-
- - - -
- - - - -

-Public Member Functions

-def __init__ (self, internal)
 
- - - -

-Public Attributes

internal
 
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Plugins/pint/quantity.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1quantity_1_1__Exception.js b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1quantity_1_1__Exception.js deleted file mode 100644 index 8cbd13cb..00000000 --- a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1quantity_1_1__Exception.js +++ /dev/null @@ -1,5 +0,0 @@ -var classSUAVE_1_1Plugins_1_1pint_1_1quantity_1_1__Exception = -[ - [ "__init__", "classSUAVE_1_1Plugins_1_1pint_1_1quantity_1_1__Exception.html#a28ec68beb1c8e5689f06665d39a9bfab", null ], - [ "internal", "classSUAVE_1_1Plugins_1_1pint_1_1quantity_1_1__Exception.html#a084976d64b2ebf7dd6232658c533a2e4", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1quantity_1_1__Exception.png b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1quantity_1_1__Exception.png deleted file mode 100644 index d6606d83..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1quantity_1_1__Exception.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1quantity_1_1__Quantity-members.html b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1quantity_1_1__Quantity-members.html deleted file mode 100644 index 593ccb2c..00000000 --- a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1quantity_1_1__Quantity-members.html +++ /dev/null @@ -1,170 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Plugins.pint.quantity._Quantity Member List
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This is the complete list of members for SUAVE.Plugins.pint.quantity._Quantity, including all inherited members.

- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
__abs__(self) (defined in SUAVE.Plugins.pint.quantity._Quantity)SUAVE.Plugins.pint.quantity._Quantity
__add__(self, other) (defined in SUAVE.Plugins.pint.quantity._Quantity)SUAVE.Plugins.pint.quantity._Quantity
__array_prepare__(self, obj, context=None) (defined in SUAVE.Plugins.pint.quantity._Quantity)SUAVE.Plugins.pint.quantity._Quantity
__array_wrap__(self, obj, context=None) (defined in SUAVE.Plugins.pint.quantity._Quantity)SUAVE.Plugins.pint.quantity._Quantity
__bool__(self) (defined in SUAVE.Plugins.pint.quantity._Quantity)SUAVE.Plugins.pint.quantity._Quantity
__complex__(self) (defined in SUAVE.Plugins.pint.quantity._Quantity)SUAVE.Plugins.pint.quantity._Quantity
__copy__(self) (defined in SUAVE.Plugins.pint.quantity._Quantity)SUAVE.Plugins.pint.quantity._Quantity
__eq__(self, other) (defined in SUAVE.Plugins.pint.quantity._Quantity)SUAVE.Plugins.pint.quantity._Quantity
__float__(self) (defined in SUAVE.Plugins.pint.quantity._Quantity)SUAVE.Plugins.pint.quantity._Quantity
__floordiv__(self, other) (defined in SUAVE.Plugins.pint.quantity._Quantity)SUAVE.Plugins.pint.quantity._Quantity
__format__(self, spec) (defined in SUAVE.Plugins.pint.quantity._Quantity)SUAVE.Plugins.pint.quantity._Quantity
__getattr__(self, item) (defined in SUAVE.Plugins.pint.quantity._Quantity)SUAVE.Plugins.pint.quantity._Quantity
__getitem__(self, key) (defined in SUAVE.Plugins.pint.quantity._Quantity)SUAVE.Plugins.pint.quantity._Quantity
__iadd__(self, other) (defined in SUAVE.Plugins.pint.quantity._Quantity)SUAVE.Plugins.pint.quantity._Quantity
__ifloordiv__(self, other) (defined in SUAVE.Plugins.pint.quantity._Quantity)SUAVE.Plugins.pint.quantity._Quantity
__imul__(self, other) (defined in SUAVE.Plugins.pint.quantity._Quantity)SUAVE.Plugins.pint.quantity._Quantity
__ipow__(self, other) (defined in SUAVE.Plugins.pint.quantity._Quantity)SUAVE.Plugins.pint.quantity._Quantity
__isub__(self, other) (defined in SUAVE.Plugins.pint.quantity._Quantity)SUAVE.Plugins.pint.quantity._Quantity
__iter__(self) (defined in SUAVE.Plugins.pint.quantity._Quantity)SUAVE.Plugins.pint.quantity._Quantity
__itruediv__(self, other) (defined in SUAVE.Plugins.pint.quantity._Quantity)SUAVE.Plugins.pint.quantity._Quantity
__len__(self) (defined in SUAVE.Plugins.pint.quantity._Quantity)SUAVE.Plugins.pint.quantity._Quantity
__mul__(self, other) (defined in SUAVE.Plugins.pint.quantity._Quantity)SUAVE.Plugins.pint.quantity._Quantity
__ne__(self, other) (defined in SUAVE.Plugins.pint.quantity._Quantity)SUAVE.Plugins.pint.quantity._Quantity
__neg__(self) (defined in SUAVE.Plugins.pint.quantity._Quantity)SUAVE.Plugins.pint.quantity._Quantity
__new__(cls, value, units=None) (defined in SUAVE.Plugins.pint.quantity._Quantity)SUAVE.Plugins.pint.quantity._Quantity
__pos__(self) (defined in SUAVE.Plugins.pint.quantity._Quantity)SUAVE.Plugins.pint.quantity._Quantity
__pow__(self, other) (defined in SUAVE.Plugins.pint.quantity._Quantity)SUAVE.Plugins.pint.quantity._Quantity
__reduce__(self) (defined in SUAVE.Plugins.pint.quantity._Quantity)SUAVE.Plugins.pint.quantity._Quantity
__repr__(self) (defined in SUAVE.Plugins.pint.quantity._Quantity)SUAVE.Plugins.pint.quantity._Quantity
__rfloordiv__(self, other) (defined in SUAVE.Plugins.pint.quantity._Quantity)SUAVE.Plugins.pint.quantity._Quantity
__round__(self, ndigits=0) (defined in SUAVE.Plugins.pint.quantity._Quantity)SUAVE.Plugins.pint.quantity._Quantity
__rsub__(self, other) (defined in SUAVE.Plugins.pint.quantity._Quantity)SUAVE.Plugins.pint.quantity._Quantity
__rtruediv__(self, other) (defined in SUAVE.Plugins.pint.quantity._Quantity)SUAVE.Plugins.pint.quantity._Quantity
__setitem__(self, key, value) (defined in SUAVE.Plugins.pint.quantity._Quantity)SUAVE.Plugins.pint.quantity._Quantity
__str__(self) (defined in SUAVE.Plugins.pint.quantity._Quantity)SUAVE.Plugins.pint.quantity._Quantity
__sub__(self, other) (defined in SUAVE.Plugins.pint.quantity._Quantity)SUAVE.Plugins.pint.quantity._Quantity
__truediv__(self, other) (defined in SUAVE.Plugins.pint.quantity._Quantity)SUAVE.Plugins.pint.quantity._Quantity
add_sub(self, other, op) (defined in SUAVE.Plugins.pint.quantity._Quantity)SUAVE.Plugins.pint.quantity._Quantity
clip(self, first=None, second=None, out=None, kwargs) (defined in SUAVE.Plugins.pint.quantity._Quantity)SUAVE.Plugins.pint.quantity._Quantity
compare(self, other, op) (defined in SUAVE.Plugins.pint.quantity._Quantity)SUAVE.Plugins.pint.quantity._Quantity
default_format (defined in SUAVE.Plugins.pint.quantity._Quantity)SUAVE.Plugins.pint.quantity._Quantitystatic
dimensionality (defined in SUAVE.Plugins.pint.quantity._Quantity)SUAVE.Plugins.pint.quantity._Quantity
dimensionality(self)SUAVE.Plugins.pint.quantity._Quantity
dimensionless(self)SUAVE.Plugins.pint.quantity._Quantity
fill(self, value) (defined in SUAVE.Plugins.pint.quantity._Quantity)SUAVE.Plugins.pint.quantity._Quantity
iadd_sub(self, other, op) (defined in SUAVE.Plugins.pint.quantity._Quantity)SUAVE.Plugins.pint.quantity._Quantity
ito(self, other=None, contexts, ctx_kwargs)SUAVE.Plugins.pint.quantity._Quantity
ito_base_units(self)SUAVE.Plugins.pint.quantity._Quantity
magnitude(self)SUAVE.Plugins.pint.quantity._Quantity
plus_minus(self, error, relative=False) (defined in SUAVE.Plugins.pint.quantity._Quantity)SUAVE.Plugins.pint.quantity._Quantity
put(self, indices, values, mode='raise') (defined in SUAVE.Plugins.pint.quantity._Quantity)SUAVE.Plugins.pint.quantity._Quantity
searchsorted(self, v, side='left') (defined in SUAVE.Plugins.pint.quantity._Quantity)SUAVE.Plugins.pint.quantity._Quantity
to(self, other=None, contexts, ctx_kwargs)SUAVE.Plugins.pint.quantity._Quantity
to_base_units(self)SUAVE.Plugins.pint.quantity._Quantity
tolist(self) (defined in SUAVE.Plugins.pint.quantity._Quantity)SUAVE.Plugins.pint.quantity._Quantity
unitless(self)SUAVE.Plugins.pint.quantity._Quantity
units (defined in SUAVE.Plugins.pint.quantity._Quantity)SUAVE.Plugins.pint.quantity._Quantity
units(self)SUAVE.Plugins.pint.quantity._Quantity
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1quantity_1_1__Quantity.html b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1quantity_1_1__Quantity.html deleted file mode 100644 index baa8d277..00000000 --- a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1quantity_1_1__Quantity.html +++ /dev/null @@ -1,533 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Plugins.pint.quantity._Quantity Class Reference - - - - - - - - - - - - - - - -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Plugins.pint.quantity._Quantity Class Reference
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-Inheritance diagram for SUAVE.Plugins.pint.quantity._Quantity:
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- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

-def __reduce__ (self)
 
-def __new__ (cls, value, units=None)
 
-def __copy__ (self)
 
-def __str__ (self)
 
-def __repr__ (self)
 
-def __format__ (self, spec)
 
def magnitude (self)
 
def units (self)
 
def unitless (self)
 
def dimensionless (self)
 
def dimensionality (self)
 
def ito (self, other=None, contexts, ctx_kwargs)
 
def to (self, other=None, contexts, ctx_kwargs)
 
def ito_base_units (self)
 
def to_base_units (self)
 
-def __float__ (self)
 
-def __complex__ (self)
 
-def iadd_sub (self, other, op)
 
-def add_sub (self, other, op)
 
-def __iadd__ (self, other)
 
-def __add__ (self, other)
 
-def __isub__ (self, other)
 
-def __sub__ (self, other)
 
-def __rsub__ (self, other)
 
-def __imul__ (self, other)
 
-def __mul__ (self, other)
 
-def __itruediv__ (self, other)
 
-def __truediv__ (self, other)
 
-def __rtruediv__ (self, other)
 
-def __ifloordiv__ (self, other)
 
-def __floordiv__ (self, other)
 
-def __rfloordiv__ (self, other)
 
-def __ipow__ (self, other)
 
-def __pow__ (self, other)
 
-def __abs__ (self)
 
-def __round__ (self, ndigits=0)
 
-def __pos__ (self)
 
-def __neg__ (self)
 
-def __eq__ (self, other)
 
-def __ne__ (self, other)
 
-def compare (self, other, op)
 
-def __bool__ (self)
 
-def clip (self, first=None, second=None, out=None, kwargs)
 
-def fill (self, value)
 
-def put (self, indices, values, mode='raise')
 
-def searchsorted (self, v, side='left')
 
-def __len__ (self)
 
-def __iter__ (self)
 
-def __getattr__ (self, item)
 
-def __getitem__ (self, key)
 
-def __setitem__ (self, key, value)
 
-def tolist (self)
 
-def __array_prepare__ (self, obj, context=None)
 
-def __array_wrap__ (self, obj, context=None)
 
-def plus_minus (self, error, relative=False)
 
- - - - - -

-Public Attributes

dimensionality
 
units
 
- - - -

-Static Public Attributes

-string default_format = ''
 
-

Detailed Description

-
Implements a class to describe a physical quantities:
-the product of a numerical value and a unit of measurement.
-
-:param value: value of the physical quantity to be created.
-:type value: str, Quantity or any numeric type.
-:param units: units of the physical quantity to be created.
-:type units: UnitsContainer, str or Quantity.
-

Member Function Documentation

- -

◆ dimensionality()

- -
-
- - - - - - - - -
def SUAVE.Plugins.pint.quantity._Quantity.dimensionality ( self)
-
-
Quantity's dimensionality (e.g. {length: 1, time: -1})
-
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-
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◆ dimensionless()

- -
-
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def SUAVE.Plugins.pint.quantity._Quantity.dimensionless ( self)
-
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Return true if the quantity is dimensionless.
-
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◆ ito()

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def SUAVE.Plugins.pint.quantity._Quantity.ito ( self,
 other = None,
 contexts,
 ctx_kwargs 
)
-
-
Inplace rescale to different units.
-
-:param other: destination units.
-:type other: Quantity, str or dict
-
-
-
- -

◆ ito_base_units()

- -
-
- - - - - - - - -
def SUAVE.Plugins.pint.quantity._Quantity.ito_base_units ( self)
-
-
Return Quantity rescaled to base units
-
-
-
- -

◆ magnitude()

- -
-
- - - - - - - - -
def SUAVE.Plugins.pint.quantity._Quantity.magnitude ( self)
-
-
Quantity's magnitude.
-
-
-
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◆ to()

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def SUAVE.Plugins.pint.quantity._Quantity.to ( self,
 other = None,
 contexts,
 ctx_kwargs 
)
-
-
Return Quantity rescaled to different units.
-
-:param other: destination units.
-:type other: Quantity, str or dict
-
-
-
- -

◆ to_base_units()

- -
-
- - - - - - - - -
def SUAVE.Plugins.pint.quantity._Quantity.to_base_units ( self)
-
-
Return Quantity rescaled to base units
-
-
-
- -

◆ unitless()

- -
-
- - - - - - - - -
def SUAVE.Plugins.pint.quantity._Quantity.unitless ( self)
-
-
Return true if the quantity does not have units.
-
-
-
- -

◆ units()

- -
-
- - - - - - - - -
def SUAVE.Plugins.pint.quantity._Quantity.units ( self)
-
-
Quantity's units.
-
-:rtype: UnitContainer
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Plugins/pint/quantity.py
  • -
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SUAVE.Plugins.pint.testsuite.TestCase Member List
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assertAlmostEqual(self, first, second, places=None, msg=None, delta=None) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
assertAlmostEqualRelError(self, first, second, rel, msg=None) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
assertSequenceEqual(self, seq1, seq2, msg=None, seq_type=None) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
Q_ (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
setUpClass(cls) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
ureg (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
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SUAVE.Plugins.pint.testsuite.TestCase Class Reference
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-Public Member Functions

-def setUpClass (cls)
 
-def assertSequenceEqual (self, seq1, seq2, msg=None, seq_type=None)
 
-def assertAlmostEqual (self, first, second, places=None, msg=None, delta=None)
 
-def assertAlmostEqualRelError (self, first, second, rel, msg=None)
 
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-Public Attributes

ureg
 
Q_
 
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The documentation for this class was generated from the following file:
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SUAVE.Plugins.pint.testsuite.test_contexts.TestContexts Member List
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This is the complete list of members for SUAVE.Plugins.pint.testsuite.test_contexts.TestContexts, including all inherited members.

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test_context_with_arg(self) (defined in SUAVE.Plugins.pint.testsuite.test_contexts.TestContexts)SUAVE.Plugins.pint.testsuite.test_contexts.TestContexts
test_context_with_arg_def(self) (defined in SUAVE.Plugins.pint.testsuite.test_contexts.TestContexts)SUAVE.Plugins.pint.testsuite.test_contexts.TestContexts
test_context_with_sharedarg_def(self) (defined in SUAVE.Plugins.pint.testsuite.test_contexts.TestContexts)SUAVE.Plugins.pint.testsuite.test_contexts.TestContexts
test_enable_context_with_arg(self) (defined in SUAVE.Plugins.pint.testsuite.test_contexts.TestContexts)SUAVE.Plugins.pint.testsuite.test_contexts.TestContexts
test_graph(self) (defined in SUAVE.Plugins.pint.testsuite.test_contexts.TestContexts)SUAVE.Plugins.pint.testsuite.test_contexts.TestContexts
test_graph_enable(self) (defined in SUAVE.Plugins.pint.testsuite.test_contexts.TestContexts)SUAVE.Plugins.pint.testsuite.test_contexts.TestContexts
test_known_context(self) (defined in SUAVE.Plugins.pint.testsuite.test_contexts.TestContexts)SUAVE.Plugins.pint.testsuite.test_contexts.TestContexts
test_known_context_enable(self) (defined in SUAVE.Plugins.pint.testsuite.test_contexts.TestContexts)SUAVE.Plugins.pint.testsuite.test_contexts.TestContexts
test_known_nested_context(self) (defined in SUAVE.Plugins.pint.testsuite.test_contexts.TestContexts)SUAVE.Plugins.pint.testsuite.test_contexts.TestContexts
test_multiple_context(self) (defined in SUAVE.Plugins.pint.testsuite.test_contexts.TestContexts)SUAVE.Plugins.pint.testsuite.test_contexts.TestContexts
test_nested_context(self) (defined in SUAVE.Plugins.pint.testsuite.test_contexts.TestContexts)SUAVE.Plugins.pint.testsuite.test_contexts.TestContexts
test_one_context(self) (defined in SUAVE.Plugins.pint.testsuite.test_contexts.TestContexts)SUAVE.Plugins.pint.testsuite.test_contexts.TestContexts
test_parse_auto_inverse(self) (defined in SUAVE.Plugins.pint.testsuite.test_contexts.TestContexts)SUAVE.Plugins.pint.testsuite.test_contexts.TestContexts
test_parse_define(self) (defined in SUAVE.Plugins.pint.testsuite.test_contexts.TestContexts)SUAVE.Plugins.pint.testsuite.test_contexts.TestContexts
test_parse_parameterized(self) (defined in SUAVE.Plugins.pint.testsuite.test_contexts.TestContexts)SUAVE.Plugins.pint.testsuite.test_contexts.TestContexts
test_parse_simple(self) (defined in SUAVE.Plugins.pint.testsuite.test_contexts.TestContexts)SUAVE.Plugins.pint.testsuite.test_contexts.TestContexts
test_unknown_context(self) (defined in SUAVE.Plugins.pint.testsuite.test_contexts.TestContexts)SUAVE.Plugins.pint.testsuite.test_contexts.TestContexts
test_unknown_nested_context(self) (defined in SUAVE.Plugins.pint.testsuite.test_contexts.TestContexts)SUAVE.Plugins.pint.testsuite.test_contexts.TestContexts
test_warnings(self) (defined in SUAVE.Plugins.pint.testsuite.test_contexts.TestContexts)SUAVE.Plugins.pint.testsuite.test_contexts.TestContexts
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-def test_known_context_enable (self)
 
-def test_graph (self)
 
-def test_graph_enable (self)
 
-def test_known_nested_context (self)
 
-def test_unknown_context (self)
 
-def test_unknown_nested_context (self)
 
-def test_one_context (self)
 
-def test_multiple_context (self)
 
-def test_nested_context (self)
 
-def test_context_with_arg (self)
 
-def test_enable_context_with_arg (self)
 
-def test_context_with_arg_def (self)
 
-def test_context_with_sharedarg_def (self)
 
-def test_parse_simple (self)
 
-def test_parse_auto_inverse (self)
 
-def test_parse_define (self)
 
-def test_parse_parameterized (self)
 
-def test_warnings (self)
 
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The documentation for this class was generated from the following file:
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SUAVE.Plugins.pint.testsuite.test_contexts.TestDefinedContexts Class Reference
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-Public Member Functions

-def test_defined (self)
 
-def test_spectroscopy (self)
 
- Public Member Functions inherited from SUAVE.Plugins.pint.testsuite.TestCase
-def setUpClass (cls)
 
-def assertSequenceEqual (self, seq1, seq2, msg=None, seq_type=None)
 
-def assertAlmostEqual (self, first, second, places=None, msg=None, delta=None)
 
-def assertAlmostEqualRelError (self, first, second, rel, msg=None)
 
- - - -

-Static Public Attributes

-bool FORCE_NDARRAY = False
 
- - - - - - -

-Additional Inherited Members

- Public Attributes inherited from SUAVE.Plugins.pint.testsuite.TestCase
ureg
 
Q_
 
-
The documentation for this class was generated from the following file:
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  • /home/tim/Documents/SUAVE/trunk/SUAVE/Plugins/pint/testsuite/test_contexts.py
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__contexts_1_1TestDefinedContexts.js b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__contexts_1_1TestDefinedContexts.js deleted file mode 100644 index 26792af9..00000000 --- a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__contexts_1_1TestDefinedContexts.js +++ /dev/null @@ -1,5 +0,0 @@ -var classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__contexts_1_1TestDefinedContexts = -[ - [ "test_defined", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__contexts_1_1TestDefinedContexts.html#adb3d389628becf7062d80f81ca39d638", null ], - [ "test_spectroscopy", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__contexts_1_1TestDefinedContexts.html#af7b69df3fb2460093364b5a5c09e9aed", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__contexts_1_1TestDefinedContexts.png b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__contexts_1_1TestDefinedContexts.png deleted file mode 100644 index a29fdeb7..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__contexts_1_1TestDefinedContexts.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__contexts_1_1TestHandler-members.html b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__contexts_1_1TestHandler-members.html deleted file mode 100644 index 53a73884..00000000 --- a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__contexts_1_1TestHandler-members.html +++ /dev/null @@ -1,115 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Plugins.pint.testsuite.test_contexts.TestHandler Member List
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Plugins.pint.testsuite.test_contexts.TestHandler Class Reference
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-Public Member Functions

-def __init__ (self)
 
-def shouldFlush (self)
 
-def emit (self, record)
 
-
The documentation for this class was generated from the following file:
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  • /home/tim/Documents/SUAVE/trunk/SUAVE/Plugins/pint/testsuite/test_contexts.py
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__contexts_1_1TestHandler.js b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__contexts_1_1TestHandler.js deleted file mode 100644 index d2aa6ebf..00000000 --- a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__contexts_1_1TestHandler.js +++ /dev/null @@ -1,6 +0,0 @@ -var classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__contexts_1_1TestHandler = -[ - [ "__init__", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__contexts_1_1TestHandler.html#ab95b93df50ee0e994e249a1ec3882335", null ], - [ "emit", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__contexts_1_1TestHandler.html#abc3855046e7933ea2b342023ea043329", null ], - [ "shouldFlush", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__contexts_1_1TestHandler.html#aa2da76f25bb809f7f6aebffa65cbf2d0", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__contexts_1_1TestHandler.png b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__contexts_1_1TestHandler.png deleted file mode 100644 index bcadb943..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__contexts_1_1TestHandler.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__issues_1_1TestIssues-members.html b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__issues_1_1TestIssues-members.html deleted file mode 100644 index 2038ff25..00000000 --- a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__issues_1_1TestIssues-members.html +++ /dev/null @@ -1,122 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE.Plugins.pint.testsuite.test_issues.TestIssues Member List
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This is the complete list of members for SUAVE.Plugins.pint.testsuite.test_issues.TestIssues, including all inherited members.

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test_issue25(self) (defined in SUAVE.Plugins.pint.testsuite.test_issues.TestIssues)SUAVE.Plugins.pint.testsuite.test_issues.TestIssues
test_issue29(self) (defined in SUAVE.Plugins.pint.testsuite.test_issues.TestIssues)SUAVE.Plugins.pint.testsuite.test_issues.TestIssues
test_issue52(self) (defined in SUAVE.Plugins.pint.testsuite.test_issues.TestIssues)SUAVE.Plugins.pint.testsuite.test_issues.TestIssues
test_issue54(self) (defined in SUAVE.Plugins.pint.testsuite.test_issues.TestIssues)SUAVE.Plugins.pint.testsuite.test_issues.TestIssues
test_issue54_related(self) (defined in SUAVE.Plugins.pint.testsuite.test_issues.TestIssues)SUAVE.Plugins.pint.testsuite.test_issues.TestIssues
test_issue61(self) (defined in SUAVE.Plugins.pint.testsuite.test_issues.TestIssues)SUAVE.Plugins.pint.testsuite.test_issues.TestIssues
test_issue61_notNP(self) (defined in SUAVE.Plugins.pint.testsuite.test_issues.TestIssues)SUAVE.Plugins.pint.testsuite.test_issues.TestIssues
test_issue66(self) (defined in SUAVE.Plugins.pint.testsuite.test_issues.TestIssues)SUAVE.Plugins.pint.testsuite.test_issues.TestIssues
test_issue66b(self) (defined in SUAVE.Plugins.pint.testsuite.test_issues.TestIssues)SUAVE.Plugins.pint.testsuite.test_issues.TestIssues
test_issue69(self) (defined in SUAVE.Plugins.pint.testsuite.test_issues.TestIssues)SUAVE.Plugins.pint.testsuite.test_issues.TestIssues
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__issues_1_1TestIssues.html b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__issues_1_1TestIssues.html deleted file mode 100644 index 31e47219..00000000 --- a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__issues_1_1TestIssues.html +++ /dev/null @@ -1,158 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Plugins.pint.testsuite.test_issues.TestIssues Class Reference - - - - - - - - - - - - - - - -
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SUAVE.Plugins.pint.testsuite.test_issues.TestIssues Class Reference
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-Public Member Functions

-def test_issue25 (self)
 
-def test_issue29 (self)
 
-def test_issue52 (self)
 
-def test_issue54 (self)
 
-def test_issue54_related (self)
 
-def test_issue61 (self)
 
-def test_issue61_notNP (self)
 
-def test_issue66 (self)
 
-def test_issue66b (self)
 
-def test_issue69 (self)
 
-
The documentation for this class was generated from the following file:
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  • /home/tim/Documents/SUAVE/trunk/SUAVE/Plugins/pint/testsuite/test_issues.py
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SUAVE -  1.0.0 -
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assertAlmostEqual(self, first, second, places=None, msg=None, delta=None) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
assertAlmostEqualRelError(self, first, second, rel, msg=None) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
assertSequenceEqual(self, seq1, seq2, msg=None, seq_type=None) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
FORCE_NDARRAY (defined in SUAVE.Plugins.pint.testsuite.test_issues.TestIssuesNP)SUAVE.Plugins.pint.testsuite.test_issues.TestIssuesNPstatic
Q_ (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
setUpClass(cls) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
test_issue37(self) (defined in SUAVE.Plugins.pint.testsuite.test_issues.TestIssuesNP)SUAVE.Plugins.pint.testsuite.test_issues.TestIssuesNP
test_issue39(self) (defined in SUAVE.Plugins.pint.testsuite.test_issues.TestIssuesNP)SUAVE.Plugins.pint.testsuite.test_issues.TestIssuesNP
test_issue44(self) (defined in SUAVE.Plugins.pint.testsuite.test_issues.TestIssuesNP)SUAVE.Plugins.pint.testsuite.test_issues.TestIssuesNP
test_issue45(self) (defined in SUAVE.Plugins.pint.testsuite.test_issues.TestIssuesNP)SUAVE.Plugins.pint.testsuite.test_issues.TestIssuesNP
test_issue45b(self) (defined in SUAVE.Plugins.pint.testsuite.test_issues.TestIssuesNP)SUAVE.Plugins.pint.testsuite.test_issues.TestIssuesNP
test_issue50(self) (defined in SUAVE.Plugins.pint.testsuite.test_issues.TestIssuesNP)SUAVE.Plugins.pint.testsuite.test_issues.TestIssuesNP
test_issue62(self) (defined in SUAVE.Plugins.pint.testsuite.test_issues.TestIssuesNP)SUAVE.Plugins.pint.testsuite.test_issues.TestIssuesNP
test_issue74(self) (defined in SUAVE.Plugins.pint.testsuite.test_issues.TestIssuesNP)SUAVE.Plugins.pint.testsuite.test_issues.TestIssuesNP
test_issue75(self) (defined in SUAVE.Plugins.pint.testsuite.test_issues.TestIssuesNP)SUAVE.Plugins.pint.testsuite.test_issues.TestIssuesNP
ureg (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
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SUAVE.Plugins.pint.testsuite.test_issues.TestIssuesNP Class Reference
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-Public Member Functions

-def test_issue37 (self)
 
-def test_issue39 (self)
 
-def test_issue44 (self)
 
-def test_issue45 (self)
 
-def test_issue45b (self)
 
-def test_issue50 (self)
 
-def test_issue62 (self)
 
-def test_issue74 (self)
 
-def test_issue75 (self)
 
- Public Member Functions inherited from SUAVE.Plugins.pint.testsuite.TestCase
-def setUpClass (cls)
 
-def assertSequenceEqual (self, seq1, seq2, msg=None, seq_type=None)
 
-def assertAlmostEqual (self, first, second, places=None, msg=None, delta=None)
 
-def assertAlmostEqualRelError (self, first, second, rel, msg=None)
 
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-bool FORCE_NDARRAY = False
 
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-Additional Inherited Members

- Public Attributes inherited from SUAVE.Plugins.pint.testsuite.TestCase
ureg
 
Q_
 
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The documentation for this class was generated from the following file:
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SUAVE.Plugins.pint.testsuite.test_measurement.TestMeasurement Member List
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This is the complete list of members for SUAVE.Plugins.pint.testsuite.test_measurement.TestMeasurement, including all inherited members.

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assertAlmostEqual(self, first, second, places=None, msg=None, delta=None) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
assertAlmostEqualRelError(self, first, second, rel, msg=None) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
assertSequenceEqual(self, seq1, seq2, msg=None, seq_type=None) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
FORCE_NDARRAY (defined in SUAVE.Plugins.pint.testsuite.test_measurement.TestMeasurement)SUAVE.Plugins.pint.testsuite.test_measurement.TestMeasurementstatic
Q_ (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
setUpClass(cls) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
test_build(self) (defined in SUAVE.Plugins.pint.testsuite.test_measurement.TestMeasurement)SUAVE.Plugins.pint.testsuite.test_measurement.TestMeasurement
test_propagate_linear(self) (defined in SUAVE.Plugins.pint.testsuite.test_measurement.TestMeasurement)SUAVE.Plugins.pint.testsuite.test_measurement.TestMeasurement
test_propagate_product(self) (defined in SUAVE.Plugins.pint.testsuite.test_measurement.TestMeasurement)SUAVE.Plugins.pint.testsuite.test_measurement.TestMeasurement
test_raise_build(self) (defined in SUAVE.Plugins.pint.testsuite.test_measurement.TestMeasurement)SUAVE.Plugins.pint.testsuite.test_measurement.TestMeasurement
ureg (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Plugins.pint.testsuite.test_measurement.TestMeasurement Class Reference
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-Public Member Functions

-def test_build (self)
 
-def test_raise_build (self)
 
-def test_propagate_linear (self)
 
-def test_propagate_product (self)
 
- Public Member Functions inherited from SUAVE.Plugins.pint.testsuite.TestCase
-def setUpClass (cls)
 
-def assertSequenceEqual (self, seq1, seq2, msg=None, seq_type=None)
 
-def assertAlmostEqual (self, first, second, places=None, msg=None, delta=None)
 
-def assertAlmostEqualRelError (self, first, second, rel, msg=None)
 
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-Static Public Attributes

-bool FORCE_NDARRAY = False
 
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-Additional Inherited Members

- Public Attributes inherited from SUAVE.Plugins.pint.testsuite.TestCase
ureg
 
Q_
 
-
The documentation for this class was generated from the following file:
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  • /home/tim/Documents/SUAVE/trunk/SUAVE/Plugins/pint/testsuite/test_measurement.py
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__measurement_1_1TestMeasurement.js b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__measurement_1_1TestMeasurement.js deleted file mode 100644 index 4272f7ae..00000000 --- a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__measurement_1_1TestMeasurement.js +++ /dev/null @@ -1,7 +0,0 @@ -var classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__measurement_1_1TestMeasurement = -[ - [ "test_build", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__measurement_1_1TestMeasurement.html#aa1a558d8d38c7481fe6a1a6f8e37f178", null ], - [ "test_propagate_linear", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__measurement_1_1TestMeasurement.html#acf5a966c2d01239405aa01176cad8246", null ], - [ "test_propagate_product", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__measurement_1_1TestMeasurement.html#a73fe64815d083b3bcbf89a6e8463f68c", null ], - [ "test_raise_build", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__measurement_1_1TestMeasurement.html#ae2926d7be3595e8da2dc4f7d2b646002", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__measurement_1_1TestMeasurement.png b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__measurement_1_1TestMeasurement.png deleted file mode 100644 index 02203849..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__measurement_1_1TestMeasurement.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__numpy_1_1TestBitTwiddlingUfuncs-members.html b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__numpy_1_1TestBitTwiddlingUfuncs-members.html deleted file mode 100644 index 91388faf..00000000 --- a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__numpy_1_1TestBitTwiddlingUfuncs-members.html +++ /dev/null @@ -1,133 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE.Plugins.pint.testsuite.test_numpy.TestBitTwiddlingUfuncs Member List
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This is the complete list of members for SUAVE.Plugins.pint.testsuite.test_numpy.TestBitTwiddlingUfuncs, including all inherited members.

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assertAlmostEqual(self, first, second, places=None, msg=None, delta=None) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
assertAlmostEqualRelError(self, first, second, rel, msg=None) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
assertEqual(self, first, second, msg=None) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs
assertRaisesMsg(self, msg, ExcType, func, args, kwargs) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs
assertSequenceEqual(self, seq1, seq2, msg=None, seq_type=None) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
FORCE_NDARRAY (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncsstatic
q1(self) (defined in SUAVE.Plugins.pint.testsuite.test_numpy.TestBitTwiddlingUfuncs)SUAVE.Plugins.pint.testsuite.test_numpy.TestBitTwiddlingUfuncs
q2(self) (defined in SUAVE.Plugins.pint.testsuite.test_numpy.TestBitTwiddlingUfuncs)SUAVE.Plugins.pint.testsuite.test_numpy.TestBitTwiddlingUfuncs
Q_ (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
qi(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs
qless(self) (defined in SUAVE.Plugins.pint.testsuite.test_numpy.TestBitTwiddlingUfuncs)SUAVE.Plugins.pint.testsuite.test_numpy.TestBitTwiddlingUfuncs
qm(self) (defined in SUAVE.Plugins.pint.testsuite.test_numpy.TestBitTwiddlingUfuncs)SUAVE.Plugins.pint.testsuite.test_numpy.TestBitTwiddlingUfuncs
qs(self) (defined in SUAVE.Plugins.pint.testsuite.test_numpy.TestBitTwiddlingUfuncs)SUAVE.Plugins.pint.testsuite.test_numpy.TestBitTwiddlingUfuncs
setUpClass(cls) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
test_bitwise_and(self) (defined in SUAVE.Plugins.pint.testsuite.test_numpy.TestBitTwiddlingUfuncs)SUAVE.Plugins.pint.testsuite.test_numpy.TestBitTwiddlingUfuncs
test_bitwise_or(self) (defined in SUAVE.Plugins.pint.testsuite.test_numpy.TestBitTwiddlingUfuncs)SUAVE.Plugins.pint.testsuite.test_numpy.TestBitTwiddlingUfuncs
test_bitwise_xor(self) (defined in SUAVE.Plugins.pint.testsuite.test_numpy.TestBitTwiddlingUfuncs)SUAVE.Plugins.pint.testsuite.test_numpy.TestBitTwiddlingUfuncs
test_invert(self) (defined in SUAVE.Plugins.pint.testsuite.test_numpy.TestBitTwiddlingUfuncs)SUAVE.Plugins.pint.testsuite.test_numpy.TestBitTwiddlingUfuncs
test_left_shift(self) (defined in SUAVE.Plugins.pint.testsuite.test_numpy.TestBitTwiddlingUfuncs)SUAVE.Plugins.pint.testsuite.test_numpy.TestBitTwiddlingUfuncs
test_right_shift(self) (defined in SUAVE.Plugins.pint.testsuite.test_numpy.TestBitTwiddlingUfuncs)SUAVE.Plugins.pint.testsuite.test_numpy.TestBitTwiddlingUfuncs
ureg (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Plugins.pint.testsuite.test_numpy.TestBitTwiddlingUfuncs Class Reference
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-Public Member Functions

-def qless (self)
 
-def qs (self)
 
-def q1 (self)
 
-def q2 (self)
 
-def qm (self)
 
-def test_bitwise_and (self)
 
-def test_bitwise_or (self)
 
-def test_bitwise_xor (self)
 
-def test_invert (self)
 
-def test_left_shift (self)
 
-def test_right_shift (self)
 
- Public Member Functions inherited from SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs
-def qless (self)
 
-def qs (self)
 
-def q1 (self)
 
-def q2 (self)
 
-def qm (self)
 
-def qi (self)
 
-def assertEqual (self, first, second, msg=None)
 
-def assertRaisesMsg (self, msg, ExcType, func, args, kwargs)
 
- Public Member Functions inherited from SUAVE.Plugins.pint.testsuite.TestCase
-def setUpClass (cls)
 
-def assertSequenceEqual (self, seq1, seq2, msg=None, seq_type=None)
 
-def assertAlmostEqual (self, first, second, places=None, msg=None, delta=None)
 
-def assertAlmostEqualRelError (self, first, second, rel, msg=None)
 
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-Additional Inherited Members

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ureg
 
Q_
 
- Static Public Attributes inherited from SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs
-bool FORCE_NDARRAY = True
 
-

Detailed Description

-
Universal functions (ufuncs) >  Bittwiddling functions
-
-http://docs.scipy.org/doc/numpy/reference/ufuncs.html#bittwiddlingfunctions
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-bitwise_and(x1, x2[, out])         Compute the bitwise AND of two arrays elementwise.
-bitwise_or(x1, x2[, out])  Compute the bitwise OR of two arrays elementwise.
-bitwise_xor(x1, x2[, out])         Compute the bitwise XOR of two arrays elementwise.
-invert(x[, out])   Compute bitwise inversion, or bitwise NOT, elementwise.
-left_shift(x1, x2[, out])  Shift the bits of an integer to the left.
-right_shift(x1, x2[, out])         Shift the bits of an integer to the right.
-

The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Plugins/pint/testsuite/test_numpy.py
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SUAVE -  1.0.0 -
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SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods Member List
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This is the complete list of members for SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods, including all inherited members.

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assertAlmostEqual(self, first, second, places=None, msg=None, delta=None) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
assertAlmostEqualRelError(self, first, second, rel, msg=None) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
assertSequenceEqual(self, seq1, seq2, msg=None, seq_type=None) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
FORCE_NDARRAY (defined in SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods)SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethodsstatic
q(self) (defined in SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods)SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods
Q_ (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
setUpClass(cls) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
test_argmax(self) (defined in SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods)SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods
test_argmin(self) (defined in SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods)SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods
test_argsort(self) (defined in SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods)SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods
test_clip(self) (defined in SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods)SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods
test_compress(self) (defined in SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods)SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods
test_conj(self) (defined in SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods)SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods
test_cumprod(self) (defined in SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods)SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods
test_cumsum(self) (defined in SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods)SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods
test_diagonal(self) (defined in SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods)SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods
test_equal(self) (defined in SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods)SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods
test_fill(self) (defined in SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods)SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods
test_flatten(self) (defined in SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods)SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods
test_getitem(self) (defined in SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods)SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods
test_iterator(self) (defined in SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods)SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods
test_max(self) (defined in SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods)SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods
test_mean(self) (defined in SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods)SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods
test_min(self) (defined in SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods)SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods
test_nonzero(self) (defined in SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods)SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods
test_pickle(self) (defined in SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods)SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods
test_prod(self) (defined in SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods)SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods
test_ptp(self) (defined in SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods)SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods
test_put(self) (defined in SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods)SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods
test_ravel(self) (defined in SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods)SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods
test_repeat(self) (defined in SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods)SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods
test_reshape(self) (defined in SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods)SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods
test_reversible_op(self)SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods
test_round(self) (defined in SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods)SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods
test_searchsorted(self) (defined in SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods)SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods
test_setitem(self) (defined in SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods)SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods
test_sort(self) (defined in SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods)SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods
test_squeeze(self) (defined in SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods)SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods
test_std(self) (defined in SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods)SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods
test_sum(self) (defined in SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods)SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods
test_take(self) (defined in SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods)SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods
test_tolist(self) (defined in SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods)SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods
test_trace(self) (defined in SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods)SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods
test_transpose(self) (defined in SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods)SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods
test_var(self) (defined in SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods)SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods
ureg (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
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SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods Class Reference
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-Inheritance diagram for SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods:
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-Public Member Functions

-def q (self)
 
-def test_tolist (self)
 
-def test_sum (self)
 
-def test_fill (self)
 
-def test_reshape (self)
 
-def test_transpose (self)
 
-def test_flatten (self)
 
-def test_ravel (self)
 
-def test_squeeze (self)
 
-def test_take (self)
 
-def test_put (self)
 
-def test_repeat (self)
 
-def test_sort (self)
 
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-def test_diagonal (self)
 
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-def test_searchsorted (self)
 
-def test_nonzero (self)
 
-def test_max (self)
 
-def test_argmax (self)
 
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-def test_ptp (self)
 
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-def test_setitem (self)
 
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def test_reversible_op (self)
 
-def test_pickle (self)
 
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- Public Member Functions inherited from SUAVE.Plugins.pint.testsuite.TestCase
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-def assertAlmostEqual (self, first, second, places=None, msg=None, delta=None)
 
-def assertAlmostEqualRelError (self, first, second, rel, msg=None)
 
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-Static Public Attributes

-bool FORCE_NDARRAY = True
 
- - - - - - -

-Additional Inherited Members

- Public Attributes inherited from SUAVE.Plugins.pint.testsuite.TestCase
ureg
 
Q_
 
-

Member Function Documentation

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◆ test_reversible_op()

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def SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods.test_reversible_op ( self)
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The documentation for this class was generated from the following file:
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  • /home/tim/Documents/SUAVE/trunk/SUAVE/Plugins/pint/testsuite/test_numpy.py
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SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyNotSupported Member List
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assertAlmostEqual(self, first, second, places=None, msg=None, delta=None) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
assertAlmostEqualRelError(self, first, second, rel, msg=None) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
assertEqual(self, first, second, msg=None) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs
assertRaisesMsg(self, msg, ExcType, func, args, kwargs) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs
assertSequenceEqual(self, seq1, seq2, msg=None, seq_type=None) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
FORCE_NDARRAY (defined in SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyNotSupported)SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyNotSupportedstatic
q1(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs
q2(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs
Q_ (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
qi(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs
qless(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs
qm(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs
qs(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs
setUpClass(cls) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
test_cross(self)SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyNotSupported
test_diff(self)SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyNotSupported
test_ediff1d(self)SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyNotSupported
test_fix(self)SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyNotSupported
test_gradient(self)SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyNotSupported
test_ones_like(self)SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyNotSupported
test_power(self)SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyNotSupported
test_trapz(self)SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyNotSupported
test_unwrap(self)SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyNotSupported
ureg (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
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SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyNotSupported Class Reference
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-Inheritance diagram for SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyNotSupported:
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def test_unwrap (self)
 
def test_trapz (self)
 
def test_diff (self)
 
def test_ediff1d (self)
 
def test_fix (self)
 
def test_gradient (self)
 
def test_cross (self)
 
def test_power (self)
 
def test_ones_like (self)
 
- Public Member Functions inherited from SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs
-def qless (self)
 
-def qs (self)
 
-def q1 (self)
 
-def q2 (self)
 
-def qm (self)
 
-def qi (self)
 
-def assertEqual (self, first, second, msg=None)
 
-def assertRaisesMsg (self, msg, ExcType, func, args, kwargs)
 
- Public Member Functions inherited from SUAVE.Plugins.pint.testsuite.TestCase
-def setUpClass (cls)
 
-def assertSequenceEqual (self, seq1, seq2, msg=None, seq_type=None)
 
-def assertAlmostEqual (self, first, second, places=None, msg=None, delta=None)
 
-def assertAlmostEqualRelError (self, first, second, rel, msg=None)
 
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-Static Public Attributes

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-bool FORCE_NDARRAY = True
 
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-Additional Inherited Members

- Public Attributes inherited from SUAVE.Plugins.pint.testsuite.TestCase
ureg
 
Q_
 
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Member Function Documentation

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◆ test_cross()

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def SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyNotSupported.test_cross ( self)
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◆ test_diff()

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def SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyNotSupported.test_diff ( self)
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◆ test_ediff1d()

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def SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyNotSupported.test_ediff1d ( self)
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def SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyNotSupported.test_fix ( self)
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◆ test_gradient()

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def SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyNotSupported.test_gradient ( self)
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◆ test_ones_like()

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def SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyNotSupported.test_ones_like ( self)
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◆ test_power()

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def SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyNotSupported.test_power ( self)
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This is not supported as different elements might end up with different units
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◆ test_trapz()

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def SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyNotSupported.test_trapz ( self)
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◆ test_unwrap()

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def SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyNotSupported.test_unwrap ( self)
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unwrap depends on diff
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The documentation for this class was generated from the following file:
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SUAVE.Plugins.pint.testsuite.test_pitheorem.TestPiTheorem Class Reference
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- Public Member Functions inherited from SUAVE.Plugins.pint.testsuite.TestCase
-def setUpClass (cls)
 
-def assertSequenceEqual (self, seq1, seq2, msg=None, seq_type=None)
 
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ureg
 
Q_
 
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The documentation for this class was generated from the following file:
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Plugins.pint.testsuite.test_quantity.TestDimensions Class Reference
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-Public Member Functions

-def test_get_dimensionality (self)
 
-def test_dimensionality (self)
 
- Public Member Functions inherited from SUAVE.Plugins.pint.testsuite.TestCase
-def setUpClass (cls)
 
-def assertSequenceEqual (self, seq1, seq2, msg=None, seq_type=None)
 
-def assertAlmostEqual (self, first, second, places=None, msg=None, delta=None)
 
-def assertAlmostEqualRelError (self, first, second, rel, msg=None)
 
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-bool FORCE_NDARRAY = False
 
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-Additional Inherited Members

- Public Attributes inherited from SUAVE.Plugins.pint.testsuite.TestCase
ureg
 
Q_
 
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The documentation for this class was generated from the following file:
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__quantity_1_1TestDimensions.js b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__quantity_1_1TestDimensions.js deleted file mode 100644 index 5a2a1363..00000000 --- a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__quantity_1_1TestDimensions.js +++ /dev/null @@ -1,5 +0,0 @@ -var classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__quantity_1_1TestDimensions = -[ - [ "test_dimensionality", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__quantity_1_1TestDimensions.html#ad68c728669073feee11a55771153b92b", null ], - [ "test_get_dimensionality", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__quantity_1_1TestDimensions.html#a806eb9eace72667d22bf2def20984140", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__quantity_1_1TestDimensions.png b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__quantity_1_1TestDimensions.png deleted file mode 100644 index cc39a61b..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__quantity_1_1TestDimensions.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__quantity_1_1TestQuantity-members.html b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__quantity_1_1TestQuantity-members.html deleted file mode 100644 index ecb83bea..00000000 --- a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__quantity_1_1TestQuantity-members.html +++ /dev/null @@ -1,141 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Plugins.pint.testsuite.test_quantity.TestQuantity Member List
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This is the complete list of members for SUAVE.Plugins.pint.testsuite.test_quantity.TestQuantity, including all inherited members.

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assertAlmostEqual(self, first, second, places=None, msg=None, delta=None) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
assertAlmostEqualRelError(self, first, second, rel, msg=None) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
assertSequenceEqual(self, seq1, seq2, msg=None, seq_type=None) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
FORCE_NDARRAY (defined in SUAVE.Plugins.pint.testsuite.test_quantity.TestQuantity)SUAVE.Plugins.pint.testsuite.test_quantity.TestQuantitystatic
Q_ (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
setUpClass(cls) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
test_both_symbol(self) (defined in SUAVE.Plugins.pint.testsuite.test_quantity.TestQuantity)SUAVE.Plugins.pint.testsuite.test_quantity.TestQuantity
test_context_attr(self) (defined in SUAVE.Plugins.pint.testsuite.test_quantity.TestQuantity)SUAVE.Plugins.pint.testsuite.test_quantity.TestQuantity
test_convert(self) (defined in SUAVE.Plugins.pint.testsuite.test_quantity.TestQuantity)SUAVE.Plugins.pint.testsuite.test_quantity.TestQuantity
test_default_formatting(self) (defined in SUAVE.Plugins.pint.testsuite.test_quantity.TestQuantity)SUAVE.Plugins.pint.testsuite.test_quantity.TestQuantity
test_dimensionless_units(self) (defined in SUAVE.Plugins.pint.testsuite.test_quantity.TestQuantity)SUAVE.Plugins.pint.testsuite.test_quantity.TestQuantity
test_offset(self) (defined in SUAVE.Plugins.pint.testsuite.test_quantity.TestQuantity)SUAVE.Plugins.pint.testsuite.test_quantity.TestQuantity
test_offset_delta(self) (defined in SUAVE.Plugins.pint.testsuite.test_quantity.TestQuantity)SUAVE.Plugins.pint.testsuite.test_quantity.TestQuantity
test_pickle(self) (defined in SUAVE.Plugins.pint.testsuite.test_quantity.TestQuantity)SUAVE.Plugins.pint.testsuite.test_quantity.TestQuantity
test_quantity_abs_round(self) (defined in SUAVE.Plugins.pint.testsuite.test_quantity.TestQuantity)SUAVE.Plugins.pint.testsuite.test_quantity.TestQuantity
test_quantity_add_sub(self) (defined in SUAVE.Plugins.pint.testsuite.test_quantity.TestQuantity)SUAVE.Plugins.pint.testsuite.test_quantity.TestQuantity
test_quantity_bool(self) (defined in SUAVE.Plugins.pint.testsuite.test_quantity.TestQuantity)SUAVE.Plugins.pint.testsuite.test_quantity.TestQuantity
test_quantity_comparison(self) (defined in SUAVE.Plugins.pint.testsuite.test_quantity.TestQuantity)SUAVE.Plugins.pint.testsuite.test_quantity.TestQuantity
test_quantity_comparison_convert(self) (defined in SUAVE.Plugins.pint.testsuite.test_quantity.TestQuantity)SUAVE.Plugins.pint.testsuite.test_quantity.TestQuantity
test_quantity_creation(self) (defined in SUAVE.Plugins.pint.testsuite.test_quantity.TestQuantity)SUAVE.Plugins.pint.testsuite.test_quantity.TestQuantity
test_quantity_float_complex(self) (defined in SUAVE.Plugins.pint.testsuite.test_quantity.TestQuantity)SUAVE.Plugins.pint.testsuite.test_quantity.TestQuantity
test_quantity_floordiv(self) (defined in SUAVE.Plugins.pint.testsuite.test_quantity.TestQuantity)SUAVE.Plugins.pint.testsuite.test_quantity.TestQuantity
test_quantity_format(self) (defined in SUAVE.Plugins.pint.testsuite.test_quantity.TestQuantity)SUAVE.Plugins.pint.testsuite.test_quantity.TestQuantity
test_quantity_iadd_isub(self) (defined in SUAVE.Plugins.pint.testsuite.test_quantity.TestQuantity)SUAVE.Plugins.pint.testsuite.test_quantity.TestQuantity
test_quantity_imul_idiv(self) (defined in SUAVE.Plugins.pint.testsuite.test_quantity.TestQuantity)SUAVE.Plugins.pint.testsuite.test_quantity.TestQuantity
test_quantity_mul_div(self) (defined in SUAVE.Plugins.pint.testsuite.test_quantity.TestQuantity)SUAVE.Plugins.pint.testsuite.test_quantity.TestQuantity
test_quantity_repr(self) (defined in SUAVE.Plugins.pint.testsuite.test_quantity.TestQuantity)SUAVE.Plugins.pint.testsuite.test_quantity.TestQuantity
test_to_base_units(self) (defined in SUAVE.Plugins.pint.testsuite.test_quantity.TestQuantity)SUAVE.Plugins.pint.testsuite.test_quantity.TestQuantity
ureg (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__quantity_1_1TestQuantity.html b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__quantity_1_1TestQuantity.html deleted file mode 100644 index 3b167071..00000000 --- a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__quantity_1_1TestQuantity.html +++ /dev/null @@ -1,225 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Plugins.pint.testsuite.test_quantity.TestQuantity Class Reference - - - - - - - - - - - - - - - -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Plugins.pint.testsuite.test_quantity.TestQuantity Class Reference
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-Public Member Functions

-def test_quantity_creation (self)
 
-def test_quantity_bool (self)
 
-def test_quantity_comparison (self)
 
-def test_quantity_comparison_convert (self)
 
-def test_quantity_repr (self)
 
-def test_quantity_format (self)
 
-def test_default_formatting (self)
 
-def test_quantity_add_sub (self)
 
-def test_quantity_iadd_isub (self)
 
-def test_quantity_mul_div (self)
 
-def test_quantity_imul_idiv (self)
 
-def test_quantity_floordiv (self)
 
-def test_quantity_abs_round (self)
 
-def test_quantity_float_complex (self)
 
-def test_to_base_units (self)
 
-def test_convert (self)
 
-def test_context_attr (self)
 
-def test_both_symbol (self)
 
-def test_dimensionless_units (self)
 
-def test_offset (self)
 
-def test_offset_delta (self)
 
-def test_pickle (self)
 
- Public Member Functions inherited from SUAVE.Plugins.pint.testsuite.TestCase
-def setUpClass (cls)
 
-def assertSequenceEqual (self, seq1, seq2, msg=None, seq_type=None)
 
-def assertAlmostEqual (self, first, second, places=None, msg=None, delta=None)
 
-def assertAlmostEqualRelError (self, first, second, rel, msg=None)
 
- - - -

-Static Public Attributes

-bool FORCE_NDARRAY = False
 
- - - - - - -

-Additional Inherited Members

- Public Attributes inherited from SUAVE.Plugins.pint.testsuite.TestCase
ureg
 
Q_
 
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Plugins/pint/testsuite/test_quantity.py
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__quantity_1_1TestQuantity.js b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__quantity_1_1TestQuantity.js deleted file mode 100644 index 879c452d..00000000 --- a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__quantity_1_1TestQuantity.js +++ /dev/null @@ -1,25 +0,0 @@ -var classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__quantity_1_1TestQuantity = -[ - [ "test_both_symbol", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__quantity_1_1TestQuantity.html#ac5c77cc68ac19d606165d54a2152925f", null ], - [ "test_context_attr", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__quantity_1_1TestQuantity.html#a0ead3af30557e5727b4591989dc6c9fd", null ], - [ "test_convert", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__quantity_1_1TestQuantity.html#a0e0dde1942c41525ff1089169dad961b", null ], - [ "test_default_formatting", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__quantity_1_1TestQuantity.html#a86d2a288f95539c63e85707d6ee8220e", null ], - [ "test_dimensionless_units", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__quantity_1_1TestQuantity.html#a4a635aeb13bbf190c100b8253b7a5be0", null ], - [ "test_offset", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__quantity_1_1TestQuantity.html#af3513cd8cf6c767d32dc019d1d2723fd", null ], - [ "test_offset_delta", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__quantity_1_1TestQuantity.html#aa5993fcff267b138ff0834c015faf616", null ], - [ "test_pickle", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__quantity_1_1TestQuantity.html#aed959a7c8a715776b44cf002edfd3f32", null ], - [ "test_quantity_abs_round", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__quantity_1_1TestQuantity.html#a62e4db16150d7214fd8339ab0171f3a4", null ], - [ "test_quantity_add_sub", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__quantity_1_1TestQuantity.html#ab540911863b9e361c63b7c3e7336c9ee", null ], - [ "test_quantity_bool", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__quantity_1_1TestQuantity.html#a339e853253a8553be86b8eccc4fc0d50", null ], - [ "test_quantity_comparison", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__quantity_1_1TestQuantity.html#afe333f48591b19f91f66d4f663e91f83", null ], - [ "test_quantity_comparison_convert", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__quantity_1_1TestQuantity.html#a793b9074548e1592e4724333f48299aa", null ], - [ "test_quantity_creation", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__quantity_1_1TestQuantity.html#aa401f2859aa1d95595db47cab868d281", null ], - [ "test_quantity_float_complex", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__quantity_1_1TestQuantity.html#a3314f501b1f79de62fdfa22be4328e57", null ], - [ "test_quantity_floordiv", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__quantity_1_1TestQuantity.html#a573d3af6deb9f1bdef6ad6105deb7c23", null ], - [ "test_quantity_format", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__quantity_1_1TestQuantity.html#aef24ff8d848120a943427b19570dde4f", null ], - [ "test_quantity_iadd_isub", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__quantity_1_1TestQuantity.html#a20008227ec8a6c15c43977a629ef11d2", null ], - [ "test_quantity_imul_idiv", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__quantity_1_1TestQuantity.html#afb5ec1fea8942fed1f187dafc2409c51", null ], - [ "test_quantity_mul_div", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__quantity_1_1TestQuantity.html#a93ff685b642da10d8dfbd57e55cd3d30", null ], - [ "test_quantity_repr", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__quantity_1_1TestQuantity.html#a2458f7631a1adb1caa43fae017c4a347", null ], - [ "test_to_base_units", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__quantity_1_1TestQuantity.html#a5a06a02cb876806479e430e83b9d8103", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__quantity_1_1TestQuantity.png b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__quantity_1_1TestQuantity.png deleted file mode 100644 index 08a155c9..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__quantity_1_1TestQuantity.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestComparisonUfuncs-members.html b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestComparisonUfuncs-members.html deleted file mode 100644 index ee964a6f..00000000 --- a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestComparisonUfuncs-members.html +++ /dev/null @@ -1,133 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Plugins.pint.testsuite.test_umath.TestComparisonUfuncs Member List
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This is the complete list of members for SUAVE.Plugins.pint.testsuite.test_umath.TestComparisonUfuncs, including all inherited members.

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assertAlmostEqual(self, first, second, places=None, msg=None, delta=None) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
assertAlmostEqualRelError(self, first, second, rel, msg=None) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
assertEqual(self, first, second, msg=None) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs
assertRaisesMsg(self, msg, ExcType, func, args, kwargs) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs
assertSequenceEqual(self, seq1, seq2, msg=None, seq_type=None) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
FORCE_NDARRAY (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncsstatic
q1(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs
q2(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs
Q_ (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
qi(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs
qless(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs
qm(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs
qs(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs
setUpClass(cls) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
test_equal(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestComparisonUfuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestComparisonUfuncs
test_greater(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestComparisonUfuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestComparisonUfuncs
test_greater_equal(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestComparisonUfuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestComparisonUfuncs
test_less(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestComparisonUfuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestComparisonUfuncs
test_less_equal(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestComparisonUfuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestComparisonUfuncs
test_not_equal(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestComparisonUfuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestComparisonUfuncs
ureg (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestComparisonUfuncs.html b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestComparisonUfuncs.html deleted file mode 100644 index fbbd507a..00000000 --- a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestComparisonUfuncs.html +++ /dev/null @@ -1,211 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Plugins.pint.testsuite.test_umath.TestComparisonUfuncs Class Reference - - - - - - - - - - - - - - - -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Plugins.pint.testsuite.test_umath.TestComparisonUfuncs Class Reference
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-Inheritance diagram for SUAVE.Plugins.pint.testsuite.test_umath.TestComparisonUfuncs:
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-Public Member Functions

-def test_greater (self)
 
-def test_greater_equal (self)
 
-def test_less (self)
 
-def test_less_equal (self)
 
-def test_not_equal (self)
 
-def test_equal (self)
 
- Public Member Functions inherited from SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs
-def qless (self)
 
-def qs (self)
 
-def q1 (self)
 
-def q2 (self)
 
-def qm (self)
 
-def qi (self)
 
-def assertEqual (self, first, second, msg=None)
 
-def assertRaisesMsg (self, msg, ExcType, func, args, kwargs)
 
- Public Member Functions inherited from SUAVE.Plugins.pint.testsuite.TestCase
-def setUpClass (cls)
 
-def assertSequenceEqual (self, seq1, seq2, msg=None, seq_type=None)
 
-def assertAlmostEqual (self, first, second, places=None, msg=None, delta=None)
 
-def assertAlmostEqualRelError (self, first, second, rel, msg=None)
 
- - - - - - - - - -

-Additional Inherited Members

- Public Attributes inherited from SUAVE.Plugins.pint.testsuite.TestCase
ureg
 
Q_
 
- Static Public Attributes inherited from SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs
-bool FORCE_NDARRAY = True
 
-

Detailed Description

-
Universal functions (ufunc) > Comparison functions
-
-http://docs.scipy.org/doc/numpy/reference/ufuncs.html#comparison-functions
-
-greater(x1, x2[, out])  Return the truth value of (x1 > x2) element-wise.
-greater_equal(x1, x2[, out])    Return the truth value of (x1 >= x2) element-wise.
-less(x1, x2[, out])     Return the truth value of (x1 < x2) element-wise.
-less_equal(x1, x2[, out])   Return the truth value of (x1 =< x2) element-wise.
-not_equal(x1, x2[, out])    Return (x1 != x2) element-wise.
-equal(x1, x2[, out])    Return (x1 == x2) element-wise.
-

The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Plugins/pint/testsuite/test_umath.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestComparisonUfuncs.js b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestComparisonUfuncs.js deleted file mode 100644 index 08d124cf..00000000 --- a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestComparisonUfuncs.js +++ /dev/null @@ -1,9 +0,0 @@ -var classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestComparisonUfuncs = -[ - [ "test_equal", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestComparisonUfuncs.html#a9411862dba24e8d965e9affc76b21f32", null ], - [ "test_greater", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestComparisonUfuncs.html#aa76eba0f5e06529ac1bf3d3b376c01ef", null ], - [ "test_greater_equal", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestComparisonUfuncs.html#a8b5d5b5f9b88c8d73e3a48893cf3090e", null ], - [ "test_less", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestComparisonUfuncs.html#a408015048d033e220401e099007341c4", null ], - [ "test_less_equal", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestComparisonUfuncs.html#ab1a1d2fe4449303e7caaa1785be6382c", null ], - [ "test_not_equal", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestComparisonUfuncs.html#aabc777009b14c59c700ae82fc657cc87", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestComparisonUfuncs.png b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestComparisonUfuncs.png deleted file mode 100644 index c45812b5..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestComparisonUfuncs.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestFloatingUfuncs-members.html b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestFloatingUfuncs-members.html deleted file mode 100644 index f7c4dce7..00000000 --- a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestFloatingUfuncs-members.html +++ /dev/null @@ -1,142 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Plugins.pint.testsuite.test_umath.TestFloatingUfuncs Member List
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This is the complete list of members for SUAVE.Plugins.pint.testsuite.test_umath.TestFloatingUfuncs, including all inherited members.

- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
assertAlmostEqual(self, first, second, places=None, msg=None, delta=None) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
assertAlmostEqualRelError(self, first, second, rel, msg=None) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
assertEqual(self, first, second, msg=None) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs
assertRaisesMsg(self, msg, ExcType, func, args, kwargs) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs
assertSequenceEqual(self, seq1, seq2, msg=None, seq_type=None) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
FORCE_NDARRAY (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncsstatic
q1(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs
q2(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs
Q_ (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
qi(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs
qless(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs
qm(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs
qs(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs
setUpClass(cls) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
test_ceil(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestFloatingUfuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestFloatingUfuncs
test_copysign(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestFloatingUfuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestFloatingUfuncs
test_floor(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestFloatingUfuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestFloatingUfuncs
test_fmod(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestFloatingUfuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestFloatingUfuncs
test_frexp(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestFloatingUfuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestFloatingUfuncs
test_iscomplex(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestFloatingUfuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestFloatingUfuncs
test_isfinite(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestFloatingUfuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestFloatingUfuncs
test_isinf(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestFloatingUfuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestFloatingUfuncs
test_isnan(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestFloatingUfuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestFloatingUfuncs
test_isreal(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestFloatingUfuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestFloatingUfuncs
test_ldexp(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestFloatingUfuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestFloatingUfuncs
test_modf(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestFloatingUfuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestFloatingUfuncs
test_nextafter(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestFloatingUfuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestFloatingUfuncs
test_signbit(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestFloatingUfuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestFloatingUfuncs
test_trunc(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestFloatingUfuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestFloatingUfuncs
ureg (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestFloatingUfuncs.html b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestFloatingUfuncs.html deleted file mode 100644 index b998f7e3..00000000 --- a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestFloatingUfuncs.html +++ /dev/null @@ -1,247 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Plugins.pint.testsuite.test_umath.TestFloatingUfuncs Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Plugins.pint.testsuite.test_umath.TestFloatingUfuncs Class Reference
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-Inheritance diagram for SUAVE.Plugins.pint.testsuite.test_umath.TestFloatingUfuncs:
-
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- - -SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs -SUAVE.Plugins.pint.testsuite.TestCase - -
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

-def test_isreal (self)
 
-def test_iscomplex (self)
 
-def test_isfinite (self)
 
-def test_isinf (self)
 
-def test_isnan (self)
 
-def test_signbit (self)
 
-def test_copysign (self)
 
-def test_nextafter (self)
 
-def test_modf (self)
 
-def test_ldexp (self)
 
-def test_frexp (self)
 
-def test_fmod (self)
 
-def test_floor (self)
 
-def test_ceil (self)
 
-def test_trunc (self)
 
- Public Member Functions inherited from SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs
-def qless (self)
 
-def qs (self)
 
-def q1 (self)
 
-def q2 (self)
 
-def qm (self)
 
-def qi (self)
 
-def assertEqual (self, first, second, msg=None)
 
-def assertRaisesMsg (self, msg, ExcType, func, args, kwargs)
 
- Public Member Functions inherited from SUAVE.Plugins.pint.testsuite.TestCase
-def setUpClass (cls)
 
-def assertSequenceEqual (self, seq1, seq2, msg=None, seq_type=None)
 
-def assertAlmostEqual (self, first, second, places=None, msg=None, delta=None)
 
-def assertAlmostEqualRelError (self, first, second, rel, msg=None)
 
- - - - - - - - - -

-Additional Inherited Members

- Public Attributes inherited from SUAVE.Plugins.pint.testsuite.TestCase
ureg
 
Q_
 
- Static Public Attributes inherited from SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs
-bool FORCE_NDARRAY = True
 
-

Detailed Description

-
Universal functions (ufunc) > Floating functions
-
-http://docs.scipy.org/doc/numpy/reference/ufuncs.html#floating-functions
-
-isreal(x)   Returns a bool array, where True if input element is real.
-iscomplex(x)    Returns a bool array, where True if input element is complex.
-isfinite(x[, out])  Test element-wise for finite-ness (not infinity or not Not a Number).
-isinf(x[, out])     Test element-wise for positive or negative infinity.
-isnan(x[, out])     Test element-wise for Not a Number (NaN), return result as a bool array.
-signbit(x[, out])   Returns element-wise True where signbit is set (less than zero).
-copysign(x1, x2[, out])     Change the sign of x1 to that of x2, element-wise.
-nextafter(x1, x2[, out])    Return the next representable floating-point value after x1 in the direction of x2 element-wise.
-modf(x[, out1, out2])   Return the fractional and integral parts of an array, element-wise.
-ldexp(x1, x2[, out])    Compute y = x1 * 2**x2.
-frexp(x[, out1, out2])  Split the number, x, into a normalized fraction (y1) and exponent (y2)
-fmod(x1, x2[, out])     Return the element-wise remainder of division.
-floor(x[, out])     Return the floor of the input, element-wise.
-ceil(x[, out])  Return the ceiling of the input, element-wise.
-trunc(x[, out])     Return the truncated value of the input, element-wise.
-

The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Plugins/pint/testsuite/test_umath.py
  • -
-
-
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- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Plugins.pint.testsuite.test_umath.TestMathUfuncs Member List
-
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- -

This is the complete list of members for SUAVE.Plugins.pint.testsuite.test_umath.TestMathUfuncs, including all inherited members.

- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
assertAlmostEqual(self, first, second, places=None, msg=None, delta=None) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
assertAlmostEqualRelError(self, first, second, rel, msg=None) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
assertEqual(self, first, second, msg=None) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs
assertRaisesMsg(self, msg, ExcType, func, args, kwargs) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs
assertSequenceEqual(self, seq1, seq2, msg=None, seq_type=None) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
FORCE_NDARRAY (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncsstatic
q1(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs
q2(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs
Q_ (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
qi(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs
qless(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs
qm(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs
qs(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs
setUpClass(cls) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
test_absolute(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestMathUfuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestMathUfuncs
test_add(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestMathUfuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestMathUfuncs
test_conj(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestMathUfuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestMathUfuncs
test_divide(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestMathUfuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestMathUfuncs
test_exp(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestMathUfuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestMathUfuncs
test_exp2(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestMathUfuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestMathUfuncs
test_expm1(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestMathUfuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestMathUfuncs
test_floor_divide(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestMathUfuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestMathUfuncs
test_fmod(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestMathUfuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestMathUfuncs
test_log(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestMathUfuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestMathUfuncs
test_log10(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestMathUfuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestMathUfuncs
test_log2(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestMathUfuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestMathUfuncs
test_logaddexp(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestMathUfuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestMathUfuncs
test_logaddexp2(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestMathUfuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestMathUfuncs
test_mod(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestMathUfuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestMathUfuncs
test_multiply(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestMathUfuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestMathUfuncs
test_negative(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestMathUfuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestMathUfuncs
test_reciprocal(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestMathUfuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestMathUfuncs
test_remainder(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestMathUfuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestMathUfuncs
test_rint(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestMathUfuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestMathUfuncs
test_sqrt(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestMathUfuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestMathUfuncs
test_square(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestMathUfuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestMathUfuncs
test_subtract(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestMathUfuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestMathUfuncs
test_true_divide(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestMathUfuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestMathUfuncs
ureg (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestMathUfuncs.html b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestMathUfuncs.html deleted file mode 100644 index 0aa12fcc..00000000 --- a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestMathUfuncs.html +++ /dev/null @@ -1,287 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Plugins.pint.testsuite.test_umath.TestMathUfuncs Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Plugins.pint.testsuite.test_umath.TestMathUfuncs Class Reference
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-Inheritance diagram for SUAVE.Plugins.pint.testsuite.test_umath.TestMathUfuncs:
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- - -SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs -SUAVE.Plugins.pint.testsuite.TestCase - -
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

-def test_add (self)
 
-def test_subtract (self)
 
-def test_multiply (self)
 
-def test_divide (self)
 
-def test_logaddexp (self)
 
-def test_logaddexp2 (self)
 
-def test_true_divide (self)
 
-def test_floor_divide (self)
 
-def test_negative (self)
 
-def test_remainder (self)
 
-def test_mod (self)
 
-def test_fmod (self)
 
-def test_absolute (self)
 
-def test_rint (self)
 
-def test_conj (self)
 
-def test_exp (self)
 
-def test_exp2 (self)
 
-def test_log (self)
 
-def test_log2 (self)
 
-def test_log10 (self)
 
-def test_expm1 (self)
 
-def test_sqrt (self)
 
-def test_square (self)
 
-def test_reciprocal (self)
 
- Public Member Functions inherited from SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs
-def qless (self)
 
-def qs (self)
 
-def q1 (self)
 
-def q2 (self)
 
-def qm (self)
 
-def qi (self)
 
-def assertEqual (self, first, second, msg=None)
 
-def assertRaisesMsg (self, msg, ExcType, func, args, kwargs)
 
- Public Member Functions inherited from SUAVE.Plugins.pint.testsuite.TestCase
-def setUpClass (cls)
 
-def assertSequenceEqual (self, seq1, seq2, msg=None, seq_type=None)
 
-def assertAlmostEqual (self, first, second, places=None, msg=None, delta=None)
 
-def assertAlmostEqualRelError (self, first, second, rel, msg=None)
 
- - - - - - - - - -

-Additional Inherited Members

- Public Attributes inherited from SUAVE.Plugins.pint.testsuite.TestCase
ureg
 
Q_
 
- Static Public Attributes inherited from SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs
-bool FORCE_NDARRAY = True
 
-

Detailed Description

-
Universal functions (ufunc) > Math operations
-
-http://docs.scipy.org/doc/numpy/reference/ufuncs.html#math-operations
-
-add(x1, x2[, out])  Add arguments element-wise.
-subtract(x1, x2[, out])     Subtract arguments, element-wise.
-multiply(x1, x2[, out])     Multiply arguments element-wise.
-divide(x1, x2[, out])   Divide arguments element-wise.
-logaddexp(x1, x2[, out])    Logarithm of the sum of exponentiations of the inputs.
-logaddexp2(x1, x2[, out])   Logarithm of the sum of exponentiations of the inputs in base-2.
-true_divide(x1, x2[, out])  Returns a true division of the inputs, element-wise.
-floor_divide(x1, x2[, out])     Return the largest integer smaller or equal to the division of the inputs.
-negative(x[, out])  Returns an array with the negative of each element of the original array.
-power(x1, x2[, out])    First array elements raised to powers from second array, element-wise. NOT IMPLEMENTED
-remainder(x1, x2[, out])    Return element-wise remainder of division.
-mod(x1, x2[, out])  Return element-wise remainder of division.
-fmod(x1, x2[, out])     Return the element-wise remainder of division.
-absolute(x[, out])  Calculate the absolute value element-wise.
-rint(x[, out])  Round elements of the array to the nearest integer.
-sign(x[, out])  Returns an element-wise indication of the sign of a number.
-conj(x[, out])  Return the complex conjugate, element-wise.
-exp(x[, out])   Calculate the exponential of all elements in the input array.
-exp2(x[, out])  Calculate 2**p for all p in the input array.
-log(x[, out])   Natural logarithm, element-wise.
-log2(x[, out])  Base-2 logarithm of x.
-log10(x[, out])     Return the base 10 logarithm of the input array, element-wise.
-expm1(x[, out])     Calculate exp(x) - 1 for all elements in the array.
-log1p(x[, out])     Return the natural logarithm of one plus the input array, element-wise.
-sqrt(x[, out])  Return the positive square-root of an array, element-wise.
-square(x[, out])    Return the element-wise square of the input.
-reciprocal(x[, out])    Return the reciprocal of the argument, element-wise.
-ones_like(x[, out])     Returns an array of ones with the same shape and type as a given array.
-

The documentation for this class was generated from the following file:
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  • /home/tim/Documents/SUAVE/trunk/SUAVE/Plugins/pint/testsuite/test_umath.py
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Plugins.pint.testsuite.test_umath.TestTrigUfuncs Member List
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This is the complete list of members for SUAVE.Plugins.pint.testsuite.test_umath.TestTrigUfuncs, including all inherited members.

- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
assertAlmostEqual(self, first, second, places=None, msg=None, delta=None) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
assertAlmostEqualRelError(self, first, second, rel, msg=None) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
assertEqual(self, first, second, msg=None) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs
assertRaisesMsg(self, msg, ExcType, func, args, kwargs) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs
assertSequenceEqual(self, seq1, seq2, msg=None, seq_type=None) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
FORCE_NDARRAY (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncsstatic
q1(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs
q2(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs
Q_ (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
qi(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs
qless(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs
qm(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs
qs(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs
setUpClass(cls) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
test_arccos(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestTrigUfuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestTrigUfuncs
test_arccosh(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestTrigUfuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestTrigUfuncs
test_arcsin(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestTrigUfuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestTrigUfuncs
test_arcsinh(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestTrigUfuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestTrigUfuncs
test_arctan(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestTrigUfuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestTrigUfuncs
test_arctan2(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestTrigUfuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestTrigUfuncs
test_arctanh(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestTrigUfuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestTrigUfuncs
test_cos(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestTrigUfuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestTrigUfuncs
test_cosh(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestTrigUfuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestTrigUfuncs
test_deg2rad(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestTrigUfuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestTrigUfuncs
test_hypot(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestTrigUfuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestTrigUfuncs
test_rad2deg(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestTrigUfuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestTrigUfuncs
test_sin(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestTrigUfuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestTrigUfuncs
test_sinh(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestTrigUfuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestTrigUfuncs
test_tan(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestTrigUfuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestTrigUfuncs
test_tanh(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestTrigUfuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestTrigUfuncs
ureg (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Plugins.pint.testsuite.test_umath.TestTrigUfuncs Class Reference
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-Inheritance diagram for SUAVE.Plugins.pint.testsuite.test_umath.TestTrigUfuncs:
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- - -SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs -SUAVE.Plugins.pint.testsuite.TestCase - -
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-Public Member Functions

-def test_sin (self)
 
-def test_cos (self)
 
-def test_tan (self)
 
-def test_arcsin (self)
 
-def test_arccos (self)
 
-def test_arctan (self)
 
-def test_arctan2 (self)
 
-def test_hypot (self)
 
-def test_sinh (self)
 
-def test_cosh (self)
 
-def test_tanh (self)
 
-def test_arcsinh (self)
 
-def test_arccosh (self)
 
-def test_arctanh (self)
 
-def test_deg2rad (self)
 
-def test_rad2deg (self)
 
- Public Member Functions inherited from SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs
-def qless (self)
 
-def qs (self)
 
-def q1 (self)
 
-def q2 (self)
 
-def qm (self)
 
-def qi (self)
 
-def assertEqual (self, first, second, msg=None)
 
-def assertRaisesMsg (self, msg, ExcType, func, args, kwargs)
 
- Public Member Functions inherited from SUAVE.Plugins.pint.testsuite.TestCase
-def setUpClass (cls)
 
-def assertSequenceEqual (self, seq1, seq2, msg=None, seq_type=None)
 
-def assertAlmostEqual (self, first, second, places=None, msg=None, delta=None)
 
-def assertAlmostEqualRelError (self, first, second, rel, msg=None)
 
- - - - - - - - - -

-Additional Inherited Members

- Public Attributes inherited from SUAVE.Plugins.pint.testsuite.TestCase
ureg
 
Q_
 
- Static Public Attributes inherited from SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs
-bool FORCE_NDARRAY = True
 
-

Detailed Description

-
Universal functions (ufunc) > Trigonometric functions
-
-http://docs.scipy.org/doc/numpy/reference/ufuncs.html#trigonometric-functions
-
-sin(x[, out])   Trigonometric sine, element-wise.
-cos(x[, out])   Cosine elementwise.
-tan(x[, out])   Compute tangent element-wise.
-arcsin(x[, out])    Inverse sine, element-wise.
-arccos(x[, out])    Trigonometric inverse cosine, element-wise.
-arctan(x[, out])    Trigonometric inverse tangent, element-wise.
-arctan2(x1, x2[, out])  Element-wise arc tangent of x1/x2 choosing the quadrant correctly.
-hypot(x1, x2[, out])    Given the “legs” of a right triangle, return its hypotenuse.
-sinh(x[, out])  Hyperbolic sine, element-wise.
-cosh(x[, out])  Hyperbolic cosine, element-wise.
-tanh(x[, out])  Compute hyperbolic tangent element-wise.
-arcsinh(x[, out])   Inverse hyperbolic sine elementwise.
-arccosh(x[, out])   Inverse hyperbolic cosine, elementwise.
-arctanh(x[, out])   Inverse hyperbolic tangent elementwise.
-deg2rad(x[, out])   Convert angles from degrees to radians.
-rad2deg(x[, out])   Convert angles from radians to degrees.
-

The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Plugins/pint/testsuite/test_umath.py
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestTrigUfuncs.js b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestTrigUfuncs.js deleted file mode 100644 index fd6502b1..00000000 --- a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestTrigUfuncs.js +++ /dev/null @@ -1,19 +0,0 @@ -var classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestTrigUfuncs = -[ - [ "test_arccos", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestTrigUfuncs.html#ad093bfe64204bc51f3bee11f91a7176a", null ], - [ "test_arccosh", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestTrigUfuncs.html#abb699dc3b7eae3bdccb9773c77d588fd", null ], - [ "test_arcsin", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestTrigUfuncs.html#a5866eb33f084cd69ae67c2963f83d4fe", null ], - [ "test_arcsinh", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestTrigUfuncs.html#a5caa282bf17890fa619aba118a7efda2", null ], - [ "test_arctan", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestTrigUfuncs.html#ad78a265602bb65133f7ab45b0e4bef2f", null ], - [ "test_arctan2", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestTrigUfuncs.html#affb9c2b7a01d1f68b53a6e4856a15cd7", null ], - [ "test_arctanh", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestTrigUfuncs.html#a96ed400fd926f1145d4f98bba67e1946", null ], - [ "test_cos", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestTrigUfuncs.html#a38c2baebbbb35047bb0fcce7fcf65232", null ], - [ "test_cosh", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestTrigUfuncs.html#a771f4b7fb1ff66c49ac304d7415f0667", null ], - [ "test_deg2rad", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestTrigUfuncs.html#a6c017bccc6cfb639e2c6e63fa3cd7373", null ], - [ "test_hypot", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestTrigUfuncs.html#a66bfce456505419abc4091bf8e51dc90", null ], - [ "test_rad2deg", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestTrigUfuncs.html#a1ced998a471f5a487b36ef2aba0467cb", null ], - [ "test_sin", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestTrigUfuncs.html#a4a9b63e4eecdd804abfec9e975501f99", null ], - [ "test_sinh", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestTrigUfuncs.html#a36885ad798f9373f7bbf9233e4fbf675", null ], - [ "test_tan", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestTrigUfuncs.html#a43de3248cf35f9d892aa6ef5844e06d8", null ], - [ "test_tanh", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestTrigUfuncs.html#ae9278f14287a827974aabbb489f51dfe", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestTrigUfuncs.png b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestTrigUfuncs.png deleted file mode 100644 index 8bf6fc7e..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestTrigUfuncs.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestUFuncs-members.html b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestUFuncs-members.html deleted file mode 100644 index 2f5afda6..00000000 --- a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestUFuncs-members.html +++ /dev/null @@ -1,127 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs Member List
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This is the complete list of members for SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs, including all inherited members.

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assertAlmostEqual(self, first, second, places=None, msg=None, delta=None) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
assertAlmostEqualRelError(self, first, second, rel, msg=None) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
assertEqual(self, first, second, msg=None) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs
assertRaisesMsg(self, msg, ExcType, func, args, kwargs) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs
assertSequenceEqual(self, seq1, seq2, msg=None, seq_type=None) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
FORCE_NDARRAY (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncsstatic
q1(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs
q2(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs
Q_ (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
qi(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs
qless(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs
qm(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs
qs(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs
setUpClass(cls) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
ureg (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestUFuncs.html b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestUFuncs.html deleted file mode 100644 index 48560c82..00000000 --- a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestUFuncs.html +++ /dev/null @@ -1,189 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs Class Reference
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-Inheritance diagram for SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs:
-
-
- - -SUAVE.Plugins.pint.testsuite.TestCase -SUAVE.Plugins.pint.testsuite.test_numpy.TestBitTwiddlingUfuncs -SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyNotSupported -SUAVE.Plugins.pint.testsuite.test_umath.TestComparisonUfuncs -SUAVE.Plugins.pint.testsuite.test_umath.TestFloatingUfuncs -SUAVE.Plugins.pint.testsuite.test_umath.TestMathUfuncs -SUAVE.Plugins.pint.testsuite.test_umath.TestTrigUfuncs - -
- - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

-def qless (self)
 
-def qs (self)
 
-def q1 (self)
 
-def q2 (self)
 
-def qm (self)
 
-def qi (self)
 
-def assertEqual (self, first, second, msg=None)
 
-def assertRaisesMsg (self, msg, ExcType, func, args, kwargs)
 
- Public Member Functions inherited from SUAVE.Plugins.pint.testsuite.TestCase
-def setUpClass (cls)
 
-def assertSequenceEqual (self, seq1, seq2, msg=None, seq_type=None)
 
-def assertAlmostEqual (self, first, second, places=None, msg=None, delta=None)
 
-def assertAlmostEqualRelError (self, first, second, rel, msg=None)
 
- - - -

-Static Public Attributes

-bool FORCE_NDARRAY = True
 
- - - - - - -

-Additional Inherited Members

- Public Attributes inherited from SUAVE.Plugins.pint.testsuite.TestCase
ureg
 
Q_
 
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Plugins/pint/testsuite/test_umath.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestUFuncs.js b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestUFuncs.js deleted file mode 100644 index f086140c..00000000 --- a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestUFuncs.js +++ /dev/null @@ -1,11 +0,0 @@ -var classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestUFuncs = -[ - [ "assertEqual", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestUFuncs.html#a0c0e2b1e640261526b45d75815041eed", null ], - [ "assertRaisesMsg", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestUFuncs.html#af0f187e9627726c315aa2addfc3372b8", null ], - [ "q1", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestUFuncs.html#a369fea855eac711f52da20a83b2c42f7", null ], - [ "q2", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestUFuncs.html#ad738197b70e5b38c835aa534e623fa0d", null ], - [ "qi", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestUFuncs.html#acaa99eee28562bc9eeb3b5a925ad7cf1", null ], - [ "qless", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestUFuncs.html#a0e98847c2df97eaf685917395a434e52", null ], - [ "qm", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestUFuncs.html#a59413842a804440522080cb06b9d5a98", null ], - [ "qs", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestUFuncs.html#aa01bd01693bd30e183b9584faf00060c", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestUFuncs.png b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestUFuncs.png deleted file mode 100644 index c3ca058c..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestUFuncs.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestConverter-members.html b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestConverter-members.html deleted file mode 100644 index cb1fafe5..00000000 --- a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestConverter-members.html +++ /dev/null @@ -1,114 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Plugins.pint.testsuite.test_unit.TestConverter Member List
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This is the complete list of members for SUAVE.Plugins.pint.testsuite.test_unit.TestConverter, including all inherited members.

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test_multiplicative_converter(self) (defined in SUAVE.Plugins.pint.testsuite.test_unit.TestConverter)SUAVE.Plugins.pint.testsuite.test_unit.TestConverter
test_offset_converter(self) (defined in SUAVE.Plugins.pint.testsuite.test_unit.TestConverter)SUAVE.Plugins.pint.testsuite.test_unit.TestConverter
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SUAVE.Plugins.pint.testsuite.test_unit.TestConverter Class Reference
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-Public Member Functions

-def test_multiplicative_converter (self)
 
-def test_offset_converter (self)
 
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Plugins/pint/testsuite/test_unit.py
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-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestConverter.js b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestConverter.js deleted file mode 100644 index 2aa905e5..00000000 --- a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestConverter.js +++ /dev/null @@ -1,5 +0,0 @@ -var classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestConverter = -[ - [ "test_multiplicative_converter", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestConverter.html#a95f6d7aade373aa6b74230d3396b4b64", null ], - [ "test_offset_converter", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestConverter.html#a78a5067c77568fad55b91f0b992be22c", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestConverter.png b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestConverter.png deleted file mode 100644 index a1e7ff11..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestConverter.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestDefinition-members.html b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestDefinition-members.html deleted file mode 100644 index 2239ff19..00000000 --- a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestDefinition-members.html +++ /dev/null @@ -1,116 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Plugins.pint.testsuite.test_unit.TestDefinition Class Reference
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-Public Member Functions

-def test_prefix_definition (self)
 
-def test_baseunit_definition (self)
 
-def test_unit_definition (self)
 
-def test_dimension_definition (self)
 
-
The documentation for this class was generated from the following file:
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  • /home/tim/Documents/SUAVE/trunk/SUAVE/Plugins/pint/testsuite/test_unit.py
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Plugins.pint.testsuite.test_unit.TestRegistry Member List
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assertAlmostEqual(self, first, second, places=None, msg=None, delta=None) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
assertAlmostEqualRelError(self, first, second, rel, msg=None) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
assertSequenceEqual(self, seq1, seq2, msg=None, seq_type=None) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
FORCE_NDARRAY (defined in SUAVE.Plugins.pint.testsuite.test_unit.TestRegistry)SUAVE.Plugins.pint.testsuite.test_unit.TestRegistrystatic
Q_ (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
setUpClass(cls) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
test_delta_in_diff(self)SUAVE.Plugins.pint.testsuite.test_unit.TestRegistry
test_parse_alias(self) (defined in SUAVE.Plugins.pint.testsuite.test_unit.TestRegistry)SUAVE.Plugins.pint.testsuite.test_unit.TestRegistry
test_parse_complex(self) (defined in SUAVE.Plugins.pint.testsuite.test_unit.TestRegistry)SUAVE.Plugins.pint.testsuite.test_unit.TestRegistry
test_parse_factor(self) (defined in SUAVE.Plugins.pint.testsuite.test_unit.TestRegistry)SUAVE.Plugins.pint.testsuite.test_unit.TestRegistry
test_parse_mul_div(self) (defined in SUAVE.Plugins.pint.testsuite.test_unit.TestRegistry)SUAVE.Plugins.pint.testsuite.test_unit.TestRegistry
test_parse_number(self) (defined in SUAVE.Plugins.pint.testsuite.test_unit.TestRegistry)SUAVE.Plugins.pint.testsuite.test_unit.TestRegistry
test_parse_plural(self) (defined in SUAVE.Plugins.pint.testsuite.test_unit.TestRegistry)SUAVE.Plugins.pint.testsuite.test_unit.TestRegistry
test_parse_prefix(self) (defined in SUAVE.Plugins.pint.testsuite.test_unit.TestRegistry)SUAVE.Plugins.pint.testsuite.test_unit.TestRegistry
test_parse_single(self) (defined in SUAVE.Plugins.pint.testsuite.test_unit.TestRegistry)SUAVE.Plugins.pint.testsuite.test_unit.TestRegistry
test_pint(self) (defined in SUAVE.Plugins.pint.testsuite.test_unit.TestRegistry)SUAVE.Plugins.pint.testsuite.test_unit.TestRegistry
test_rep_and_parse(self) (defined in SUAVE.Plugins.pint.testsuite.test_unit.TestRegistry)SUAVE.Plugins.pint.testsuite.test_unit.TestRegistry
test_str_errors(self) (defined in SUAVE.Plugins.pint.testsuite.test_unit.TestRegistry)SUAVE.Plugins.pint.testsuite.test_unit.TestRegistry
test_symbol(self) (defined in SUAVE.Plugins.pint.testsuite.test_unit.TestRegistry)SUAVE.Plugins.pint.testsuite.test_unit.TestRegistry
test_to_delta(self) (defined in SUAVE.Plugins.pint.testsuite.test_unit.TestRegistry)SUAVE.Plugins.pint.testsuite.test_unit.TestRegistry
test_wraps(self) (defined in SUAVE.Plugins.pint.testsuite.test_unit.TestRegistry)SUAVE.Plugins.pint.testsuite.test_unit.TestRegistry
ureg (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestRegistry.html b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestRegistry.html deleted file mode 100644 index 0db1865a..00000000 --- a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestRegistry.html +++ /dev/null @@ -1,223 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Plugins.pint.testsuite.test_unit.TestRegistry Class Reference - - - - - - - - - - - - - - - -
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SUAVE.Plugins.pint.testsuite.test_unit.TestRegistry Class Reference
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-Public Member Functions

-def test_parse_number (self)
 
-def test_parse_single (self)
 
-def test_parse_alias (self)
 
-def test_parse_plural (self)
 
-def test_parse_prefix (self)
 
-def test_parse_complex (self)
 
-def test_str_errors (self)
 
-def test_parse_mul_div (self)
 
-def test_parse_factor (self)
 
-def test_rep_and_parse (self)
 
-def test_to_delta (self)
 
-def test_symbol (self)
 
def test_delta_in_diff (self)
 
-def test_pint (self)
 
-def test_wraps (self)
 
- Public Member Functions inherited from SUAVE.Plugins.pint.testsuite.TestCase
-def setUpClass (cls)
 
-def assertSequenceEqual (self, seq1, seq2, msg=None, seq_type=None)
 
-def assertAlmostEqual (self, first, second, places=None, msg=None, delta=None)
 
-def assertAlmostEqualRelError (self, first, second, rel, msg=None)
 
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-Static Public Attributes

-bool FORCE_NDARRAY = False
 
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-Additional Inherited Members

- Public Attributes inherited from SUAVE.Plugins.pint.testsuite.TestCase
ureg
 
Q_
 
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Member Function Documentation

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◆ test_delta_in_diff()

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def SUAVE.Plugins.pint.testsuite.test_unit.TestRegistry.test_delta_in_diff ( self)
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This might be supported in future versions
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The documentation for this class was generated from the following file:
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestRegistry.js b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestRegistry.js deleted file mode 100644 index 98a24a8f..00000000 --- a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestRegistry.js +++ /dev/null @@ -1,18 +0,0 @@ -var classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestRegistry = -[ - [ "test_delta_in_diff", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestRegistry.html#a2def4266754e60e07017f5dc73044002", null ], - [ "test_parse_alias", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestRegistry.html#a9cbcea59a857cbb44f0b9035db31646c", null ], - [ "test_parse_complex", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestRegistry.html#ae82f05a7137b633b329086fd8bb61546", null ], - [ "test_parse_factor", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestRegistry.html#acca55ef1f2a657596df6650427388a91", null ], - [ "test_parse_mul_div", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestRegistry.html#ad3b8cbb7dc6ad8929be229a9f8d0d238", null ], - [ "test_parse_number", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestRegistry.html#a07c858087451c81e552524c547bcf503", null ], - [ "test_parse_plural", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestRegistry.html#ae134de7640645ef9c5dd8c4bac9a03e3", null ], - [ "test_parse_prefix", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestRegistry.html#a860afc6c6fc2439c6607d328390cca53", null ], - [ "test_parse_single", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestRegistry.html#ae2c8277612ad205ce7f40f1af2dbcd43", null ], - [ "test_pint", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestRegistry.html#afa65f233351009566465a7b22798d33b", null ], - [ "test_rep_and_parse", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestRegistry.html#af81b871c40c0b9db45ea961fbd4ada7e", null ], - [ "test_str_errors", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestRegistry.html#a6e554da38995139a818157bd313638f7", null ], - [ "test_symbol", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestRegistry.html#a8d4f268288358fe2b12487712d590f96", null ], - [ "test_to_delta", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestRegistry.html#a993a0a073dca0deb9d41b7bf63cb4c2f", null ], - [ "test_wraps", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestRegistry.html#a3a5263650f2915b9cda20e7090a058e5", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestRegistry.png b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestRegistry.png deleted file mode 100644 index 73ad0ef7..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestRegistry.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestUnitsContainer-members.html b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestUnitsContainer-members.html deleted file mode 100644 index e5fb78c8..00000000 --- a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestUnitsContainer-members.html +++ /dev/null @@ -1,118 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE.Plugins.pint.testsuite.test_unit.TestUnitsContainer Class Reference
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-Public Member Functions

-def test_unitcontainer_creation (self)
 
-def test_unitcontainer_repr (self)
 
-def test_unitcontainer_bool (self)
 
-def test_unitcontainer_comp (self)
 
-def test_unitcontainer_arithmetic (self)
 
-def test_string_comparison (self)
 
-
The documentation for this class was generated from the following file:
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestUnitsContainer.js b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestUnitsContainer.js deleted file mode 100644 index e6b89881..00000000 --- a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestUnitsContainer.js +++ /dev/null @@ -1,9 +0,0 @@ -var classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestUnitsContainer = -[ - [ "test_string_comparison", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestUnitsContainer.html#aeecae30b5298e34591a39240b244c7e4", null ], - [ "test_unitcontainer_arithmetic", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestUnitsContainer.html#a874f9ec2151c24b5dc2d8b8a8456264b", null ], - [ "test_unitcontainer_bool", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestUnitsContainer.html#a5b182783e38f3a50b4f85770631ed00f", null ], - [ "test_unitcontainer_comp", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestUnitsContainer.html#a869604a9d64b4a2ecfe63746147212c0", null ], - [ "test_unitcontainer_creation", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestUnitsContainer.html#a3f4f84c114782db6c52289ba5536fa1a", null ], - [ "test_unitcontainer_repr", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestUnitsContainer.html#aa066f1b5e714a98c6a275f0bcf3c7daf", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestUnitsContainer.png b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestUnitsContainer.png deleted file mode 100644 index 4351104a..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestUnitsContainer.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__util_1_1TestStringProcessor-members.html b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__util_1_1TestStringProcessor-members.html deleted file mode 100644 index 35c188d2..00000000 --- a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__util_1_1TestStringProcessor-members.html +++ /dev/null @@ -1,114 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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-def test_rules (self)
 
-def test_shortest_path (self)
 
-
The documentation for this class was generated from the following file:
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__util_1_1TestStringProcessor.js b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__util_1_1TestStringProcessor.js deleted file mode 100644 index a3e837b2..00000000 --- a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__util_1_1TestStringProcessor.js +++ /dev/null @@ -1,5 +0,0 @@ -var classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__util_1_1TestStringProcessor = -[ - [ "test_rules", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__util_1_1TestStringProcessor.html#a67f3bbf5febe825a789ddc0ee57c04e3", null ], - [ "test_shortest_path", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__util_1_1TestStringProcessor.html#a7fa27ea05b1bfa940b6a00cdd9190adb", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__util_1_1TestStringProcessor.png b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__util_1_1TestStringProcessor.png deleted file mode 100644 index 58b3c5f5..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__util_1_1TestStringProcessor.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1Converter-members.html b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1Converter-members.html deleted file mode 100644 index 261410c3..00000000 --- a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1Converter-members.html +++ /dev/null @@ -1,114 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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from_reference(self, value) (defined in SUAVE.Plugins.pint.unit.Converter)SUAVE.Plugins.pint.unit.Converter
to_reference(self, value) (defined in SUAVE.Plugins.pint.unit.Converter)SUAVE.Plugins.pint.unit.Converter
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1Converter.html b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1Converter.html deleted file mode 100644 index 80a22d6f..00000000 --- a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1Converter.html +++ /dev/null @@ -1,138 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Plugins.pint.unit.Converter Class Reference - - - - - - - - - - - - - - - -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Plugins.pint.unit.Converter Class Reference
-
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-Inheritance diagram for SUAVE.Plugins.pint.unit.Converter:
-
-
- - -SUAVE.Plugins.pint.unit.OffsetConverter -SUAVE.Plugins.pint.unit.ScaleConverter - -
- - - - - - -

-Public Member Functions

-def to_reference (self, value)
 
-def from_reference (self, value)
 
-

Detailed Description

-
Base class for value converters.
-

The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Plugins/pint/unit.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1Converter.js b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1Converter.js deleted file mode 100644 index df8aff4a..00000000 --- a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1Converter.js +++ /dev/null @@ -1,5 +0,0 @@ -var classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1Converter = -[ - [ "from_reference", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1Converter.html#abb183047ca0f04d38818035b1ca99a22", null ], - [ "to_reference", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1Converter.html#aa41d798c876b22cb05ce41008f9011e3", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1Converter.png b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1Converter.png deleted file mode 100644 index 4c5b82c5..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1Converter.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1Definition-members.html b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1Definition-members.html deleted file mode 100644 index e8fe48b0..00000000 --- a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1Definition-members.html +++ /dev/null @@ -1,119 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Plugins.pint.unit.Definition Member List
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1Definition.html b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1Definition.html deleted file mode 100644 index dff47ef0..00000000 --- a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1Definition.html +++ /dev/null @@ -1,188 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Plugins.pint.unit.Definition Class Reference - - - - - - - - - - - - - - - -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Plugins.pint.unit.Definition Class Reference
-
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-Inheritance diagram for SUAVE.Plugins.pint.unit.Definition:
-
-
- - -SUAVE.Plugins.pint.unit.DimensionDefinition -SUAVE.Plugins.pint.unit.PrefixDefinition -SUAVE.Plugins.pint.unit.UnitDefinition - -
- - - - - - - - - - - - - - - - -

-Public Member Functions

-def __init__ (self, name, symbol, aliases, converter)
 
def from_string (cls, definition)
 
-def name (self)
 
-def symbol (self)
 
-def aliases (self)
 
-def converter (self)
 
-def __str__ (self)
 
-

Detailed Description

-
Base class for definitions.
-
-:param name: name.
-:param symbol: a short name or symbol for the definition
-:param aliases: iterable of other names.
-:param converter: an instance of Converter.
-

Member Function Documentation

- -

◆ from_string()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Plugins.pint.unit.Definition.from_string ( cls,
 definition 
)
-
-
Parse a definition
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Plugins/pint/unit.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1Definition.js b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1Definition.js deleted file mode 100644 index e381c543..00000000 --- a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1Definition.js +++ /dev/null @@ -1,10 +0,0 @@ -var classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1Definition = -[ - [ "__init__", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1Definition.html#a8e93d837c170c5c91818f3ac2d862a6b", null ], - [ "__str__", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1Definition.html#aec6e23e5d1c93b362097c0686bb9b591", null ], - [ "aliases", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1Definition.html#a78e8cf07fb369840d6861791aaba6588", null ], - [ "converter", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1Definition.html#aa7d5b4434e32ccab229e5f53911d7c46", null ], - [ "from_string", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1Definition.html#ab9ab5af6145178c7047d04937b4e9f85", null ], - [ "name", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1Definition.html#adf9a57efddcc5e787d447c6bb535e787", null ], - [ "symbol", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1Definition.html#abe829a6aa6c46c17c1da831afed25a41", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1Definition.png b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1Definition.png deleted file mode 100644 index 6cb99f93..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1Definition.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1DimensionDefinition-members.html b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1DimensionDefinition-members.html deleted file mode 100644 index 10824ef9..00000000 --- a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1DimensionDefinition-members.html +++ /dev/null @@ -1,122 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE.Plugins.pint.unit.DimensionDefinition Member List
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SUAVE.Plugins.pint.unit.DimensionDefinition Class Reference
-
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-Inheritance diagram for SUAVE.Plugins.pint.unit.DimensionDefinition:
-
-
- - -SUAVE.Plugins.pint.unit.Definition - -
- - - - - - - - - - - - - - - - - - - -

-Public Member Functions

-def __init__ (self, name, symbol, aliases, converter, reference=None, is_base=False)
 
- Public Member Functions inherited from SUAVE.Plugins.pint.unit.Definition
-def __init__ (self, name, symbol, aliases, converter)
 
def from_string (cls, definition)
 
-def name (self)
 
-def symbol (self)
 
-def aliases (self)
 
-def converter (self)
 
-def __str__ (self)
 
- - - - - -

-Public Attributes

reference
 
is_base
 
-

Detailed Description

-
Definition of a dimension.
-

The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Plugins/pint/unit.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1DimensionDefinition.js b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1DimensionDefinition.js deleted file mode 100644 index aeef63b5..00000000 --- a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1DimensionDefinition.js +++ /dev/null @@ -1,6 +0,0 @@ -var classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1DimensionDefinition = -[ - [ "__init__", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1DimensionDefinition.html#a6c98bd712d82d14f337b90f2614b60ca", null ], - [ "is_base", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1DimensionDefinition.html#a9386248e21b934271fd3f76772a69c36", null ], - [ "reference", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1DimensionDefinition.html#ada4791383fd5b41c248b16b3f3493a24", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1DimensionDefinition.png b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1DimensionDefinition.png deleted file mode 100644 index 46ae64bf..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1DimensionDefinition.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1DimensionalityError-members.html b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1DimensionalityError-members.html deleted file mode 100644 index d8c1243f..00000000 --- a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1DimensionalityError-members.html +++ /dev/null @@ -1,118 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Plugins.pint.unit.DimensionalityError Class Reference
-
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-Inheritance diagram for SUAVE.Plugins.pint.unit.DimensionalityError:
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-Public Member Functions

-def __init__ (self, units1, units2, dim1=None, dim2=None)
 
-def __str__ (self)
 
- - - - - - - - - -

-Public Attributes

units1
 
units2
 
dim1
 
dim2
 
-

Detailed Description

-
Raised when trying to convert between incompatible units.
-

The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Plugins/pint/unit.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1DimensionalityError.js b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1DimensionalityError.js deleted file mode 100644 index d2cb7288..00000000 --- a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1DimensionalityError.js +++ /dev/null @@ -1,9 +0,0 @@ -var classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1DimensionalityError = -[ - [ "__init__", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1DimensionalityError.html#ad34b06e26687e0d194cbdc3089688379", null ], - [ "__str__", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1DimensionalityError.html#ab802f398669bde7acf206769fc2d6da8", null ], - [ "dim1", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1DimensionalityError.html#aec5f2ada5b8f844f239aa27565557640", null ], - [ "dim2", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1DimensionalityError.html#a90f4b1b018ebf838fe753e376ecab606", null ], - [ "units1", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1DimensionalityError.html#ae4f965df43f98339b1f734439dcf968b", null ], - [ "units2", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1DimensionalityError.html#a3b3c56f399f2d5b514be24e65815fbe2", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1DimensionalityError.png b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1DimensionalityError.png deleted file mode 100644 index b0d0b07e..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1DimensionalityError.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1OffsetConverter-members.html b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1OffsetConverter-members.html deleted file mode 100644 index 069826db..00000000 --- a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1OffsetConverter-members.html +++ /dev/null @@ -1,117 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Plugins.pint.unit.OffsetConverter Member List
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SUAVE.Plugins.pint.unit.OffsetConverter Class Reference
-
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-Inheritance diagram for SUAVE.Plugins.pint.unit.OffsetConverter:
-
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- - -SUAVE.Plugins.pint.unit.Converter - -
- - - - - - - - - - - - - -

-Public Member Functions

-def __init__ (self, scale, offset)
 
-def to_reference (self, value)
 
-def from_reference (self, value)
 
- Public Member Functions inherited from SUAVE.Plugins.pint.unit.Converter
-def to_reference (self, value)
 
-def from_reference (self, value)
 
- - - - - -

-Public Attributes

scale
 
offset
 
-

Detailed Description

-
An affine transformation
-

The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Plugins/pint/unit.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1OffsetConverter.js b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1OffsetConverter.js deleted file mode 100644 index b3cf939b..00000000 --- a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1OffsetConverter.js +++ /dev/null @@ -1,8 +0,0 @@ -var classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1OffsetConverter = -[ - [ "__init__", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1OffsetConverter.html#ad89fd685aa61274fb8a7cf219b6aad45", null ], - [ "from_reference", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1OffsetConverter.html#a3412d40ca0461f765a6448fbf122acc8", null ], - [ "to_reference", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1OffsetConverter.html#ac764b50cf2742cc725e013a28f0aa09d", null ], - [ "offset", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1OffsetConverter.html#a48ec8b1fbe460e245365cccd655ecbd0", null ], - [ "scale", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1OffsetConverter.html#aeab2b5908af76fd141e8bc42f80522ce", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1OffsetConverter.png b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1OffsetConverter.png deleted file mode 100644 index 903e72c9..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1OffsetConverter.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1PrefixDefinition-members.html b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1PrefixDefinition-members.html deleted file mode 100644 index a053263f..00000000 --- a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1PrefixDefinition-members.html +++ /dev/null @@ -1,119 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE.Plugins.pint.unit.PrefixDefinition Member List
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SUAVE.Plugins.pint.unit.PrefixDefinition Class Reference
-
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-Inheritance diagram for SUAVE.Plugins.pint.unit.PrefixDefinition:
-
-
- - -SUAVE.Plugins.pint.unit.Definition - -
- - - - - - - - - - - - - - - - - - - -

-Public Member Functions

-def __init__ (self, name, symbol, aliases, converter)
 
- Public Member Functions inherited from SUAVE.Plugins.pint.unit.Definition
-def __init__ (self, name, symbol, aliases, converter)
 
def from_string (cls, definition)
 
-def name (self)
 
-def symbol (self)
 
-def aliases (self)
 
-def converter (self)
 
-def __str__ (self)
 
-

Detailed Description

-
Definition of a prefix.
-

The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Plugins/pint/unit.py
  • -
-
-
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SUAVE.Plugins.pint.unit.ScaleConverter Class Reference
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-Inheritance diagram for SUAVE.Plugins.pint.unit.ScaleConverter:
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- - -SUAVE.Plugins.pint.unit.Converter - -
- - - - - - - - - - - - - -

-Public Member Functions

-def __init__ (self, scale)
 
-def to_reference (self, value)
 
-def from_reference (self, value)
 
- Public Member Functions inherited from SUAVE.Plugins.pint.unit.Converter
-def to_reference (self, value)
 
-def from_reference (self, value)
 
- - - -

-Public Attributes

scale
 
-

Detailed Description

-
A linear transformation
-

The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Plugins/pint/unit.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1ScaleConverter.js b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1ScaleConverter.js deleted file mode 100644 index 23715c90..00000000 --- a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1ScaleConverter.js +++ /dev/null @@ -1,7 +0,0 @@ -var classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1ScaleConverter = -[ - [ "__init__", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1ScaleConverter.html#ac8af1bf3a07abadb42b7928adb047c5f", null ], - [ "from_reference", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1ScaleConverter.html#aa1e500c68c39e06eb969ed33cc157691", null ], - [ "to_reference", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1ScaleConverter.html#afcbf75c7795e8a43a95f9b68d7cd0c44", null ], - [ "scale", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1ScaleConverter.html#aa7cd2503a28d31add246b594ac3025ce", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1ScaleConverter.png b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1ScaleConverter.png deleted file mode 100644 index be31b137..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1ScaleConverter.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UndefinedUnitError-members.html b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UndefinedUnitError-members.html deleted file mode 100644 index 9d6f68c9..00000000 --- a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UndefinedUnitError-members.html +++ /dev/null @@ -1,115 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE.Plugins.pint.unit.UndefinedUnitError Member List
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SUAVE.Plugins.pint.unit.UndefinedUnitError Class Reference
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-Inheritance diagram for SUAVE.Plugins.pint.unit.UndefinedUnitError:
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- - - - - - -

-Public Member Functions

-def __init__ (self, unit_names)
 
-def __str__ (self)
 
- - - -

-Public Attributes

unit_names
 
-

Detailed Description

-
Raised when the units are not defined in the unit registry.
-

The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Plugins/pint/unit.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UndefinedUnitError.js b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UndefinedUnitError.js deleted file mode 100644 index 79e46f29..00000000 --- a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UndefinedUnitError.js +++ /dev/null @@ -1,6 +0,0 @@ -var classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UndefinedUnitError = -[ - [ "__init__", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UndefinedUnitError.html#ad29e3be1dc3b37ee48854ebbc811f0cf", null ], - [ "__str__", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UndefinedUnitError.html#aa03f02c70f34e46fd4db831b5a26b04c", null ], - [ "unit_names", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UndefinedUnitError.html#a314867d48b585a790985c5fa9c62420e", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UndefinedUnitError.png b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UndefinedUnitError.png deleted file mode 100644 index 5fc443d9..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UndefinedUnitError.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitDefinition-members.html b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitDefinition-members.html deleted file mode 100644 index 68ff3a7f..00000000 --- a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitDefinition-members.html +++ /dev/null @@ -1,122 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE.Plugins.pint.unit.UnitDefinition Member List
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SUAVE.Plugins.pint.unit.UnitDefinition Class Reference
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-
-
- - -SUAVE.Plugins.pint.unit.Definition - -
- - - - - - - - - - - - - - - - - - - -

-Public Member Functions

-def __init__ (self, name, symbol, aliases, converter, reference=None, is_base=False)
 
- Public Member Functions inherited from SUAVE.Plugins.pint.unit.Definition
-def __init__ (self, name, symbol, aliases, converter)
 
def from_string (cls, definition)
 
-def name (self)
 
-def symbol (self)
 
-def aliases (self)
 
-def converter (self)
 
-def __str__ (self)
 
- - - - - -

-Public Attributes

reference
 
is_base
 
-

Detailed Description

-
Definition of a unit.
-
-:param reference: Units container with reference units.
-:param is_base: indicates if it is a base unit.
-

The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Plugins/pint/unit.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitDefinition.js b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitDefinition.js deleted file mode 100644 index 523df96b..00000000 --- a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitDefinition.js +++ /dev/null @@ -1,6 +0,0 @@ -var classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitDefinition = -[ - [ "__init__", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitDefinition.html#a4b1da95b87d14db876c467927292f4d6", null ], - [ "is_base", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitDefinition.html#aaf4e388ea261c7b3365ee4ffdb5a1e2b", null ], - [ "reference", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitDefinition.html#a35d7a7f400dd660b9075261f36610bf6", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitDefinition.png b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitDefinition.png deleted file mode 100644 index d83602bc..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitDefinition.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry-members.html b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry-members.html deleted file mode 100644 index fac69bf9..00000000 --- a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry-members.html +++ /dev/null @@ -1,138 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE.Plugins.pint.unit.UnitRegistry Member List
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This is the complete list of members for SUAVE.Plugins.pint.unit.UnitRegistry, including all inherited members.

- - - - - - - - - - - - - - - - - - - - - - - - - - - -
__dir__(self) (defined in SUAVE.Plugins.pint.unit.UnitRegistry)SUAVE.Plugins.pint.unit.UnitRegistry
__getattr__(self, item) (defined in SUAVE.Plugins.pint.unit.UnitRegistry)SUAVE.Plugins.pint.unit.UnitRegistry
__getitem__(self, item) (defined in SUAVE.Plugins.pint.unit.UnitRegistry)SUAVE.Plugins.pint.unit.UnitRegistry
__init__(self, filename='', force_ndarray=False, default_to_delta=True) (defined in SUAVE.Plugins.pint.unit.UnitRegistry)SUAVE.Plugins.pint.unit.UnitRegistry
add_context(self, context)SUAVE.Plugins.pint.unit.UnitRegistry
context(self, names, kwargs)SUAVE.Plugins.pint.unit.UnitRegistry
convert(self, value, src, dst)SUAVE.Plugins.pint.unit.UnitRegistry
default_format(self)SUAVE.Plugins.pint.unit.UnitRegistry
default_format(self, value) (defined in SUAVE.Plugins.pint.unit.UnitRegistry)SUAVE.Plugins.pint.unit.UnitRegistry
default_to_delta (defined in SUAVE.Plugins.pint.unit.UnitRegistry)SUAVE.Plugins.pint.unit.UnitRegistry
define(self, definition)SUAVE.Plugins.pint.unit.UnitRegistry
disable_contexts(self, n=None)SUAVE.Plugins.pint.unit.UnitRegistry
enable_contexts(self, names_or_contexts, kwargs)SUAVE.Plugins.pint.unit.UnitRegistry
get_base_units(self, input_units)SUAVE.Plugins.pint.unit.UnitRegistry
get_dimensionality(self, input_units)SUAVE.Plugins.pint.unit.UnitRegistry
get_name(self, name_or_alias)SUAVE.Plugins.pint.unit.UnitRegistry
get_symbol(self, name_or_alias)SUAVE.Plugins.pint.unit.UnitRegistry
load_definitions(self, file, is_resource=False)SUAVE.Plugins.pint.unit.UnitRegistry
parse_expression(self, input_string, values)SUAVE.Plugins.pint.unit.UnitRegistry
parse_unit_name(self, unit_name)SUAVE.Plugins.pint.unit.UnitRegistry
parse_units(self, input_string, to_delta=None)SUAVE.Plugins.pint.unit.UnitRegistry
pi_theorem(self, quantities)SUAVE.Plugins.pint.unit.UnitRegistry
Quantity (defined in SUAVE.Plugins.pint.unit.UnitRegistry)SUAVE.Plugins.pint.unit.UnitRegistry
remove_context(self, name_or_alias)SUAVE.Plugins.pint.unit.UnitRegistry
validate(self)SUAVE.Plugins.pint.unit.UnitRegistry
wraps(self, ret, args, strict=True)SUAVE.Plugins.pint.unit.UnitRegistry
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry.html b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry.html deleted file mode 100644 index 20c6b6da..00000000 --- a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry.html +++ /dev/null @@ -1,881 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Plugins.pint.unit.UnitRegistry Class Reference - - - - - - - - - - - - - - - -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Plugins.pint.unit.UnitRegistry Class Reference
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-Inheritance diagram for SUAVE.Plugins.pint.unit.UnitRegistry:
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- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

-def __init__ (self, filename='', force_ndarray=False, default_to_delta=True)
 
-def __getattr__ (self, item)
 
-def __getitem__ (self, item)
 
-def __dir__ (self)
 
def default_format (self)
 
-def default_format (self, value)
 
def add_context (self, context)
 
def remove_context (self, name_or_alias)
 
def enable_contexts (self, names_or_contexts, kwargs)
 
def disable_contexts (self, n=None)
 
def context (self, names, kwargs)
 
def define (self, definition)
 
def load_definitions (self, file, is_resource=False)
 
def validate (self)
 
def get_name (self, name_or_alias)
 
def get_symbol (self, name_or_alias)
 
def get_dimensionality (self, input_units)
 
def get_base_units (self, input_units)
 
def convert (self, value, src, dst)
 
def pi_theorem (self, quantities)
 
def parse_unit_name (self, unit_name)
 
def parse_units (self, input_string, to_delta=None)
 
def parse_expression (self, input_string, values)
 
def wraps (self, ret, args, strict=True)
 
- - - - - -

-Public Attributes

Quantity
 
default_to_delta
 
-

Detailed Description

-
The unit registry stores the definitions and relationships between
-units.
-
-:param filename: path of the units definition file to load.
-                 Empty to load the default definition file.
-                 None to leave the UnitRegistry empty.
-:param force_ndarray: convert any input, scalar or not to a numpy.ndarray.
-:param default_to_delta: In the context of a multiplication of units, interpret
-                         non-multiplicative units as their *delta* counterparts.
-

Member Function Documentation

- -

◆ add_context()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Plugins.pint.unit.UnitRegistry.add_context ( self,
 context 
)
-
-
Add a context object to the registry.
-
-The context will be accessible by its name and aliases.
-
-Notice that this method will NOT enable the context. Use `enable_contexts`.
-
-
-
- -

◆ context()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Plugins.pint.unit.UnitRegistry.context ( self,
 names,
 kwargs 
)
-
-
Used as a context manager, this function enables to activate a context
-which is removed after usage.
-
-:param names: name of the context.
-:param kwargs: keyword arguments for the contexts.
-
-Context are called by their name::
-
-    >>> with ureg.context('one'):
-    ...     pass
-
-If the context has an argument, you can specify it's value as a keyword
-argument::
-
-    >>> with ureg.context('one', n=1):
-    ...     pass
-
-Multiple contexts can be entered in single call:
-
-    >>> with ureg.context('one', 'two', n=1):
-    ...     pass
-
-or nested allowing you to give different values to the same keyword argument::
-
-    >>> with ureg.context('one', n=1):
-    ...     with ureg.context('two', n=2):
-    ...         pass
-
-A nested context inherits the defaults from the containing context::
-
-    >>> with ureg.context('one', n=1):
-    ...     with ureg.context('two'): # Here n takes the value of the upper context
-    ...         pass
-
-
- -

◆ convert()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Plugins.pint.unit.UnitRegistry.convert ( self,
 value,
 src,
 dst 
)
-
-
Convert value from some source to destination units.
-
-:param value: value
-:param src: source units.
-:type src: UnitsContainer or str
-:param dst: destination units.
-:type dst: UnitsContainer or str
-
-:return: converted value
-
-
-
- -

◆ default_format()

- -
-
- - - - - - - - -
def SUAVE.Plugins.pint.unit.UnitRegistry.default_format ( self)
-
-
Default formatting string for quantities.
-
-
-
- -

◆ define()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Plugins.pint.unit.UnitRegistry.define ( self,
 definition 
)
-
-
Add unit to the registry.
-
-
-
- -

◆ disable_contexts()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Plugins.pint.unit.UnitRegistry.disable_contexts ( self,
 n = None 
)
-
-
Disable the last n enabled contexts.
-
-
-
- -

◆ enable_contexts()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Plugins.pint.unit.UnitRegistry.enable_contexts ( self,
 names_or_contexts,
 kwargs 
)
-
-
Enable contexts provided by name or by object.
-
-:param names_or_contexts: sequence of the contexts or contexts names/alias
-:param kwargs: keyword arguments for the context
-
-
-
- -

◆ get_base_units()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Plugins.pint.unit.UnitRegistry.get_base_units ( self,
 input_units 
)
-
-
Convert unit or dict of units to the base units.
-
-If the unit is non multiplicative, None is returned as
-the multiplicative factor.
-
-:param input_units:
-:return: multiplicative factor, base units
-
-
-
- -

◆ get_dimensionality()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Plugins.pint.unit.UnitRegistry.get_dimensionality ( self,
 input_units 
)
-
-
Convert unit or dict of units or dimensions to a dict of base dimensions
-
-:param input_units:
-:return: dimensionality
-
-
-
- -

◆ get_name()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Plugins.pint.unit.UnitRegistry.get_name ( self,
 name_or_alias 
)
-
-
Return the canonical name of a unit.
-
-
-
- -

◆ get_symbol()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Plugins.pint.unit.UnitRegistry.get_symbol ( self,
 name_or_alias 
)
-
-
Return the preferred alias for a unit
-
-
-
- -

◆ load_definitions()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Plugins.pint.unit.UnitRegistry.load_definitions ( self,
 file,
 is_resource = False 
)
-
-
Add units and prefixes defined in a definition text file.
-
-
-
- -

◆ parse_expression()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Plugins.pint.unit.UnitRegistry.parse_expression ( self,
 input_string,
 values 
)
-
-
Parse a mathematical expression including units and return a quantity object.
-
-Numerical constants can be specified as keyword arguments and will take precedence
-over the names defined in the registry.
-
-
-
- -

◆ parse_unit_name()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Plugins.pint.unit.UnitRegistry.parse_unit_name ( self,
 unit_name 
)
-
-
Parse a unit to identify prefix, unit name and suffix
-by walking the list of prefix and suffix.
-
-
-
- -

◆ parse_units()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Plugins.pint.unit.UnitRegistry.parse_units ( self,
 input_string,
 to_delta = None 
)
-
-
Parse a units expression and returns a UnitContainer with
-the canonical names.
-
-The expression can only contain products, ratios and powers of units.
-
-:param to_delta: if the expression has multiple units, the parser will
-         interpret non multiplicative units as their `delta_` counterparts.
-
-:raises:
-    :class:`pint.UndefinedUnitError` if a unit is not in the registry
-    :class:`ValueError` if the expression is invalid.
-
-
-
- -

◆ pi_theorem()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Plugins.pint.unit.UnitRegistry.pi_theorem ( self,
 quantities 
)
-
-
Builds dimensionless quantities using the Buckingham π theorem
-
-:param quantities: mapping between variable name and units
-:type quantities: dict
-:return: a list of dimensionless quantities expressed as dicts
-
-
-
- -

◆ remove_context()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Plugins.pint.unit.UnitRegistry.remove_context ( self,
 name_or_alias 
)
-
-
Remove a context from the registry and return it.
-
-Notice that this methods will not disable the context. Use `disable_contexts`.
-
-
-
- -

◆ validate()

- -
-
- - - - - - - - -
def SUAVE.Plugins.pint.unit.UnitRegistry.validate ( self)
-
-
Walk the registry and calculate for each unit definition
-the corresponding base units and dimensionality.
-
-
-
- -

◆ wraps()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Plugins.pint.unit.UnitRegistry.wraps ( self,
 ret,
 args,
 strict = True 
)
-
-
Wraps a function to become pint-aware.
-
-Use it when a function requires a numerical value but in some specific
-units. The wrapper function will take a pint quantity, convert to the units
-specified in `args` and then call the wrapped function with the resulting
-magnitude.
-
-The value returned by the wrapped function will be converted to the units
-specified in `ret`.
-
-Use None to skip argument conversion.
-Set strict to False, to accept also numerical values.
-
-:param ret: output units.
-:param args: iterable of input units.
-:param strict: boolean to indicate that only quantities are accepted.
-:return: the wrapped function.
-:raises:
-    :class:`ValueError` if strict and one of the arguments is not a Quantity.
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Plugins/pint/unit.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry.js b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry.js deleted file mode 100644 index 50a27be8..00000000 --- a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry.js +++ /dev/null @@ -1,29 +0,0 @@ -var classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry = -[ - [ "__init__", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry.html#a5e38e28e66c741a9ac672b6f30ce3f6b", null ], - [ "__dir__", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry.html#a7a620ec7e3bc2a9ef549ab8e7212a074", null ], - [ "__getattr__", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry.html#ac33b542eb0eeea598bae96697b189a43", null ], - [ "__getitem__", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry.html#a11e5efd5afad852f9682b4deea4bf137", null ], - [ "add_context", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry.html#ad8dae43dc3a09546da8da6bc5999c12f", null ], - [ "context", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry.html#aeff4a616272690ba06ee479f8e22ce8e", null ], - [ "convert", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry.html#a82fa3e84687f39f5dd80025393e92379", null ], - [ "default_format", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry.html#add51f2c695a5642f18b8e8c1bfe18b92", null ], - [ "default_format", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry.html#a066a3b0927b04e46fc8c41033291b5af", null ], - [ "define", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry.html#ad425bb5f74509eb34c5719e602973151", null ], - [ "disable_contexts", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry.html#a0bb62e9743a85b15186679308dda1c13", null ], - [ "enable_contexts", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry.html#a36d3fc68e8e142fd5f9a0c687cd61b60", null ], - [ "get_base_units", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry.html#a7efb7e1108fc7b043804b80c54605f4f", null ], - [ "get_dimensionality", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry.html#addb56049afe22c3ee7700905c1d35559", null ], - [ "get_name", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry.html#a52fc0919e39a5ed8fe52b74db841ad2f", null ], - [ "get_symbol", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry.html#a231bac0fb58eed32470c45563c97525d", null ], - [ "load_definitions", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry.html#af207ae7d1ba346823ca5cf012db5fde0", null ], - [ "parse_expression", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry.html#acd7fda180374b5f9e201f3d912cd472d", null ], - [ "parse_unit_name", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry.html#ad6d0be3333825fca3e8899da06caa654", null ], - [ "parse_units", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry.html#a4686109f23abf7863f7a5f13f5b3b910", null ], - [ "pi_theorem", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry.html#abcaeffa218bba609463a749926fa070f", null ], - [ "remove_context", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry.html#a6f605d51cf518aef11fbf1e3cd84eb4a", null ], - [ "validate", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry.html#a4db5878b3a4d60864f04f91f9b1dcc9e", null ], - [ "wraps", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry.html#a2ede2984b7a1e8ca34a8ecbb9f0e503e", null ], - [ "default_to_delta", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry.html#aa94d393c138854dd1e229246d6da53ca", null ], - [ "Quantity", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry.html#ab5ff75e5065677bde4d201e0e2e4207b", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry.png b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry.png deleted file mode 100644 index 2ed7fb64..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitsContainer-members.html b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitsContainer-members.html deleted file mode 100644 index fdca7577..00000000 --- a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitsContainer-members.html +++ /dev/null @@ -1,128 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
-
- - - -
-
- -
-
-
- -
- -
-
- - -
- -
- -
-
-
SUAVE.Plugins.pint.unit.UnitsContainer Member List
-
-
- -

This is the complete list of members for SUAVE.Plugins.pint.unit.UnitsContainer, including all inherited members.

- - - - - - - - - - - - - - - - - -
__copy__(self) (defined in SUAVE.Plugins.pint.unit.UnitsContainer)SUAVE.Plugins.pint.unit.UnitsContainer
__eq__(self, other) (defined in SUAVE.Plugins.pint.unit.UnitsContainer)SUAVE.Plugins.pint.unit.UnitsContainer
__format__(self, spec) (defined in SUAVE.Plugins.pint.unit.UnitsContainer)SUAVE.Plugins.pint.unit.UnitsContainer
__imul__(self, other) (defined in SUAVE.Plugins.pint.unit.UnitsContainer)SUAVE.Plugins.pint.unit.UnitsContainer
__init__(self, args, kwargs) (defined in SUAVE.Plugins.pint.unit.UnitsContainer)SUAVE.Plugins.pint.unit.UnitsContainer
__ipow__(self, other) (defined in SUAVE.Plugins.pint.unit.UnitsContainer)SUAVE.Plugins.pint.unit.UnitsContainer
__itruediv__(self, other) (defined in SUAVE.Plugins.pint.unit.UnitsContainer)SUAVE.Plugins.pint.unit.UnitsContainer
__missing__(self, key) (defined in SUAVE.Plugins.pint.unit.UnitsContainer)SUAVE.Plugins.pint.unit.UnitsContainer
__mul__(self, other) (defined in SUAVE.Plugins.pint.unit.UnitsContainer)SUAVE.Plugins.pint.unit.UnitsContainer
__pow__(self, other) (defined in SUAVE.Plugins.pint.unit.UnitsContainer)SUAVE.Plugins.pint.unit.UnitsContainer
__repr__(self) (defined in SUAVE.Plugins.pint.unit.UnitsContainer)SUAVE.Plugins.pint.unit.UnitsContainer
__rtruediv__(self, other) (defined in SUAVE.Plugins.pint.unit.UnitsContainer)SUAVE.Plugins.pint.unit.UnitsContainer
__setitem__(self, key, value) (defined in SUAVE.Plugins.pint.unit.UnitsContainer)SUAVE.Plugins.pint.unit.UnitsContainer
__str__(self) (defined in SUAVE.Plugins.pint.unit.UnitsContainer)SUAVE.Plugins.pint.unit.UnitsContainer
__truediv__(self, other) (defined in SUAVE.Plugins.pint.unit.UnitsContainer)SUAVE.Plugins.pint.unit.UnitsContainer
add(self, key, value) (defined in SUAVE.Plugins.pint.unit.UnitsContainer)SUAVE.Plugins.pint.unit.UnitsContainer
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitsContainer.html b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitsContainer.html deleted file mode 100644 index 814a05cb..00000000 --- a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitsContainer.html +++ /dev/null @@ -1,179 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Plugins.pint.unit.UnitsContainer Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
-
- - - -
-
- -
-
-
- -
- -
-
- - -
- -
- -
- -
-
SUAVE.Plugins.pint.unit.UnitsContainer Class Reference
-
-
-
-Inheritance diagram for SUAVE.Plugins.pint.unit.UnitsContainer:
-
-
- - - -
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

-def __init__ (self, args, kwargs)
 
-def __missing__ (self, key)
 
-def __setitem__ (self, key, value)
 
-def add (self, key, value)
 
-def __eq__ (self, other)
 
-def __str__ (self)
 
-def __repr__ (self)
 
-def __format__ (self, spec)
 
-def __copy__ (self)
 
-def __imul__ (self, other)
 
-def __mul__ (self, other)
 
-def __ipow__ (self, other)
 
-def __pow__ (self, other)
 
-def __itruediv__ (self, other)
 
-def __truediv__ (self, other)
 
-def __rtruediv__ (self, other)
 
-

Detailed Description

-
The UnitsContainer stores the product of units and their respective
-exponent and implements the corresponding operations
-

The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Plugins/pint/unit.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitsContainer.js b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitsContainer.js deleted file mode 100644 index c634ffe3..00000000 --- a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitsContainer.js +++ /dev/null @@ -1,19 +0,0 @@ -var classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitsContainer = -[ - [ "__init__", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitsContainer.html#abd5b9d529b8ac7790cef30323dd7733a", null ], - [ "__copy__", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitsContainer.html#a3d53d1f6aa698a55f153920d76f3c0a6", null ], - [ "__eq__", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitsContainer.html#a1eddb87e46ff10130f0f129e9f14455e", null ], - [ "__format__", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitsContainer.html#abafa11b17931a1f2fa64551686e2837a", null ], - [ "__imul__", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitsContainer.html#a4a40d47742c7e5eac36142568c04e486", null ], - [ "__ipow__", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitsContainer.html#aeacaa80f6589e549d5046df99d2b1a47", null ], - [ "__itruediv__", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitsContainer.html#a94fe54b0d860980da43d4d90828a6ea1", null ], - [ "__missing__", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitsContainer.html#aabea6beaed7208c5f5d1059f6ff2afcb", null ], - [ "__mul__", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitsContainer.html#a746037092d0c1a4e74ae16b849d3d364", null ], - [ "__pow__", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitsContainer.html#a51a968d0b23843f96db43b230e2db695", null ], - [ "__repr__", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitsContainer.html#a13c38858cbad193228146b4e7c4c5ed5", null ], - [ "__rtruediv__", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitsContainer.html#ab9d28d6265496fd9d17ecca6d6e9f1e5", null ], - [ "__setitem__", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitsContainer.html#a861bbcb10f69ec8b3e5637215b808e24", null ], - [ "__str__", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitsContainer.html#ac7fc90fdb50b20924e0620bb90d597c6", null ], - [ "__truediv__", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitsContainer.html#ac61f54469ff6f5e9f1ff19b7526ff428", null ], - [ "add", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitsContainer.html#ad9dcb8b8d4f4235ee580e1b553fbf449", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitsContainer.png b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitsContainer.png deleted file mode 100644 index 1fc45a94..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitsContainer.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1util_1_1ParserHelper-members.html b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1util_1_1ParserHelper-members.html deleted file mode 100644 index abe44797..00000000 --- a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1util_1_1ParserHelper-members.html +++ /dev/null @@ -1,125 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
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SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
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- - - - - - -
-
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- - - -
-
- -
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SUAVE.Plugins.pint.util.ParserHelper Member List
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- -
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1util_1_1ParserHelper.html b/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1util_1_1ParserHelper.html deleted file mode 100644 index b87dafb6..00000000 --- a/_site/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1util_1_1ParserHelper.html +++ /dev/null @@ -1,232 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Plugins.pint.util.ParserHelper Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
-
- - - -
-
- -
-
-
- -
- -
-
- - -
- -
- -
- -
-
SUAVE.Plugins.pint.util.ParserHelper Class Reference
-
-
-
-Inheritance diagram for SUAVE.Plugins.pint.util.ParserHelper:
-
-
- - - -
- - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

-def __init__ (self, scale=1, args, kwargs)
 
def from_word (cls, input_word)
 
def from_string (cls, input_string)
 
-def __missing__ (self, key)
 
-def add (self, key, value)
 
-def operate (self, items, op=operator.iadd, cleanup=True)
 
-def __str__ (self)
 
-def __repr__ (self)
 
-def __mul__ (self, other)
 
-def __pow__ (self, other)
 
-def __truediv__ (self, other)
 
-def __rtruediv__ (self, other)
 
- - - -

-Public Attributes

scale
 
-

Detailed Description

-
The ParserHelper stores in place the product of variables and
-their respective exponent and implements the corresponding operations.
-

Member Function Documentation

- -

◆ from_string()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Plugins.pint.util.ParserHelper.from_string ( cls,
 input_string 
)
-
-
Parse linear expression mathematical units and return a quantity object.
-
-
-
- -

◆ from_word()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Plugins.pint.util.ParserHelper.from_word ( cls,
 input_word 
)
-
-
Creates a ParserHelper object with a single variable with exponent one.
-
-Equivalent to: ParserHelper({'word': 1})
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Plugins/pint/util.py
  • -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Plugins.pint.util.ndarray Class Reference
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-Inheritance diagram for SUAVE.Plugins.pint.util.ndarray:
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The documentation for this class was generated from the following file:
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  • /home/tim/Documents/SUAVE/trunk/SUAVE/Plugins/pint/util.py
  • -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Sizing.Sizing_Loop.Sizing_Loop Member List
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This is the complete list of members for SUAVE.Sizing.Sizing_Loop.Sizing_Loop, including all inherited members.

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__defaults__(self)SUAVE.Sizing.Sizing_Loop.Sizing_Loop
__delattr__(self, k)SUAVE.Core.Data.Data
__getattribute__(self, k)SUAVE.Core.Data.Data
__init__(self, args, kwarg)SUAVE.Core.Data.Data
__iter__(self)SUAVE.Core.Data.Data
__new__(cls, args, kwarg)SUAVE.Core.Data.Data
__setattr__(self, k, v)SUAVE.Core.Data.Data
__str__(self, indent='')SUAVE.Core.Data.Data
append(self, value, key=None)SUAVE.Core.Data.Data
broyden_update(self, y, err, sizing_evaluation, nexus, scaling, iter, iteration_options)SUAVE.Sizing.Sizing_Loop.Sizing_Loop
damped_newton_update(self, y, err, sizing_evaluation, nexus, scaling, iter, iteration_options) (defined in SUAVE.Sizing.Sizing_Loop.Sizing_Loop)SUAVE.Sizing.Sizing_Loop.Sizing_Loop
dataname(self)SUAVE.Core.Data.Data
deep_get(self, keys)SUAVE.Core.Data.Data
deep_set(self, keys, val)SUAVE.Core.Data.Data
default_scaling (defined in SUAVE.Sizing.Sizing_Loop.Sizing_Loop)SUAVE.Sizing.Sizing_Loop.Sizing_Loop
default_y (defined in SUAVE.Sizing.Sizing_Loop.Sizing_Loop)SUAVE.Sizing.Sizing_Loop.Sizing_Loop
do_recursive(self, method, other=None, default=None)SUAVE.Core.Data.Data
evaluate(self, nexus) (defined in SUAVE.Sizing.Sizing_Loop.Sizing_Loop)SUAVE.Sizing.Sizing_Loop.Sizing_Loop
get_bases(self)SUAVE.Core.Data.Data
initial_step (defined in SUAVE.Sizing.Sizing_Loop.Sizing_Loop)SUAVE.Sizing.Sizing_Loop.Sizing_Loop
iteration_options (defined in SUAVE.Sizing.Sizing_Loop.Sizing_Loop)SUAVE.Sizing.Sizing_Loop.Sizing_Loop
itervalues(self)SUAVE.Core.Data.Data
maximum_iterations (defined in SUAVE.Sizing.Sizing_Loop.Sizing_Loop)SUAVE.Sizing.Sizing_Loop.Sizing_Loop
newton_raphson_update(self, y, err, sizing_evaluation, nexus, scaling, iter, iteration_options)SUAVE.Sizing.Sizing_Loop.Sizing_Loop
output_filename (defined in SUAVE.Sizing.Sizing_Loop.Sizing_Loop)SUAVE.Sizing.Sizing_Loop.Sizing_Loop
pack_array(self, output='vector')SUAVE.Core.Data.Data
sizing_evaluation (defined in SUAVE.Sizing.Sizing_Loop.Sizing_Loop)SUAVE.Sizing.Sizing_Loop.Sizing_Loop
successive_substitution_update(self, y, err, sizing_evaluation, nexus, scaling, iter, iteration_options)SUAVE.Sizing.Sizing_Loop.Sizing_Loop
tolerance (defined in SUAVE.Sizing.Sizing_Loop.Sizing_Loop)SUAVE.Sizing.Sizing_Loop.Sizing_Loop
typestring(self)SUAVE.Core.Data.Data
unpack_array(self, M)SUAVE.Core.Data.Data
update(self, other)SUAVE.Core.Data.Data
update_method (defined in SUAVE.Sizing.Sizing_Loop.Sizing_Loop)SUAVE.Sizing.Sizing_Loop.Sizing_Loop
values(self)SUAVE.Core.Data.Data
write_threshhold (defined in SUAVE.Sizing.Sizing_Loop.Sizing_Loop)SUAVE.Sizing.Sizing_Loop.Sizing_Loop
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Sizing.Sizing_Loop.Sizing_Loop Class Reference
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-Inheritance diagram for SUAVE.Sizing.Sizing_Loop.Sizing_Loop:
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- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
-def evaluate (self, nexus)
 
def successive_substitution_update (self, y, err, sizing_evaluation, nexus, scaling, iter, iteration_options)
 
def newton_raphson_update (self, y, err, sizing_evaluation, nexus, scaling, iter, iteration_options)
 
def broyden_update (self, y, err, sizing_evaluation, nexus, scaling, iter, iteration_options)
 
-def damped_newton_update (self, y, err, sizing_evaluation, nexus, scaling, iter, iteration_options)
 
- Public Member Functions inherited from SUAVE.Core.Data.Data
def __getattribute__ (self, k)
 
def __setattr__ (self, k, v)
 
def __delattr__ (self, k)
 
def __defaults__ (self)
 
def __new__ (cls, args, kwarg)
 
def typestring (self)
 
def dataname (self)
 
def __str__ (self, indent='')
 
def __init__ (self, args, kwarg)
 
def __iter__ (self)
 
def itervalues (self)
 
def values (self)
 
def update (self, other)
 
def get_bases (self)
 
def append (self, value, key=None)
 
def deep_set (self, keys, val)
 
def deep_get (self, keys)
 
def pack_array (self, output='vector')
 
def unpack_array (self, M)
 
def do_recursive (self, method, other=None, default=None)
 
- - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

tolerance
 
initial_step
 
update_method
 
default_y
 
default_scaling
 
maximum_iterations
 
output_filename
 
sizing_evaluation
 
write_threshhold
 
iteration_options
 
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Sizing.Sizing_Loop.Sizing_Loop.__defaults__ ( self)
-
-
Data class that solves a fixed point iteration problem to size the aircraft. Includes
-a variety of methods to solve the subproblem, including successive substitution, newton-raphson,
-broyden's method, as well as a damped newton method. Also includes machine learning algorithms
-from scikit-learn to aid in finding a good initial guess for your sizing parameters.
-
-
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- -

◆ broyden_update()

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def SUAVE.Sizing.Sizing_Loop.Sizing_Loop.broyden_update ( self,
 y,
 err,
 sizing_evaluation,
 nexus,
 scaling,
 iter,
 iteration_options 
)
-
-
uses an approximation to update the Jacobian without
-the use of finite differencing
-
-
- -

◆ newton_raphson_update()

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def SUAVE.Sizing.Sizing_Loop.Sizing_Loop.newton_raphson_update ( self,
 y,
 err,
 sizing_evaluation,
 nexus,
 scaling,
 iter,
 iteration_options 
)
-
-
Finite differences the problem to calculate the Jacobian, then
-tries to use that to zero the residual
-
-
-
- -

◆ successive_substitution_update()

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def SUAVE.Sizing.Sizing_Loop.Sizing_Loop.successive_substitution_update ( self,
 y,
 err,
 sizing_evaluation,
 nexus,
 scaling,
 iter,
 iteration_options 
)
-
-
Uses a successive substitution update to try to zero the residual
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Sizing/Sizing_Loop.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.js b/_site/doxygen/classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.js deleted file mode 100644 index a25366f3..00000000 --- a/_site/doxygen/classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.js +++ /dev/null @@ -1,19 +0,0 @@ -var classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop = -[ - [ "__defaults__", "classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.html#a178ec5c05131960d4fa8d5ad6e3c3e11", null ], - [ "broyden_update", "classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.html#a52d275bd606778420dde57df5c710ced", null ], - [ "damped_newton_update", "classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.html#a5942e4cd16b9a18ed372e79d4e8dbd70", null ], - [ "evaluate", "classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.html#a153a6ac6de2d18f130320b5e871756de", null ], - [ "newton_raphson_update", "classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.html#afee06f0c84b5023393a68b8163024939", null ], - [ "successive_substitution_update", "classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.html#a4222e0b4efa8045836ef6fb1ba94a6f3", null ], - [ "default_scaling", "classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.html#addd0442dc00517c1db5c0de356e75e68", null ], - [ "default_y", "classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.html#ac3d271509f69df8f90e10e2bf709413e", null ], - [ "initial_step", "classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.html#a5afe4453cdff685473f8f94cb6f054df", null ], - [ "iteration_options", "classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.html#af4d73d77d7b7748b08cd8e5f6cedf4fd", null ], - [ "maximum_iterations", "classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.html#a880e2af1ba6856fd9ba640aaa2b78136", null ], - [ "output_filename", "classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.html#a8bd8cbf5a638d448371e44a2f59fb4bd", null ], - [ "sizing_evaluation", "classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.html#aa9f5e946792b134387052287be34a531", null ], - [ "tolerance", "classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.html#ab945e6e09e3783f41580e291da29559f", null ], - [ "update_method", "classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.html#a82aceccafa7e1f519154a06057f02fe9", null ], - [ "write_threshhold", "classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.html#afb271146361bd7c3157ded88876df9e9", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.png b/_site/doxygen/classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.png deleted file mode 100644 index 1a60e12c..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Surrogate_1_1Surrogate__Problem_1_1Surrogate__Problem-members.html b/_site/doxygen/classSUAVE_1_1Surrogate_1_1Surrogate__Problem_1_1Surrogate__Problem-members.html deleted file mode 100644 index 8449d94c..00000000 --- a/_site/doxygen/classSUAVE_1_1Surrogate_1_1Surrogate__Problem_1_1Surrogate__Problem-members.html +++ /dev/null @@ -1,135 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE.Surrogate.Surrogate_Problem.Surrogate_Problem Member List
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Surrogate.Surrogate_Problem.Surrogate_Problem Class Reference
-
-
-
-Inheritance diagram for SUAVE.Surrogate.Surrogate_Problem.Surrogate_Problem:
-
-
- - -SUAVE.Core.Data.Data - -
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

-def __defaults__ (self)
 
def compute (self, x)
 
- Public Member Functions inherited from SUAVE.Core.Data.Data
def __getattribute__ (self, k)
 
def __setattr__ (self, k, v)
 
def __delattr__ (self, k)
 
def __defaults__ (self)
 
def __new__ (cls, args, kwarg)
 
def typestring (self)
 
def dataname (self)
 
def __str__ (self, indent='')
 
def __init__ (self, args, kwarg)
 
def __iter__ (self)
 
def itervalues (self)
 
def values (self)
 
def update (self, other)
 
def get_bases (self)
 
def append (self, value, key=None)
 
def deep_set (self, keys, val)
 
def deep_get (self, keys)
 
def pack_array (self, output='vector')
 
def unpack_array (self, M)
 
def do_recursive (self, method, other=None, default=None)
 
- - - - - -

-Public Attributes

obj_surrogate
 
constraints_surrogates
 
-

Detailed Description

-
Callable data structure that computes a surrogate 
-prediction of the problem vs. a point x
-

Member Function Documentation

- -

◆ compute()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Surrogate.Surrogate_Problem.Surrogate_Problem.compute ( self,
 x 
)
-
-
Inputs: 
-x    [array]
-
-Outputs:
-f    [float]
-g    [array]
-fail [int]
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Surrogate/Surrogate_Problem.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Surrogate_1_1Surrogate__Problem_1_1Surrogate__Problem.js b/_site/doxygen/classSUAVE_1_1Surrogate_1_1Surrogate__Problem_1_1Surrogate__Problem.js deleted file mode 100644 index 72d3f5bf..00000000 --- a/_site/doxygen/classSUAVE_1_1Surrogate_1_1Surrogate__Problem_1_1Surrogate__Problem.js +++ /dev/null @@ -1,7 +0,0 @@ -var classSUAVE_1_1Surrogate_1_1Surrogate__Problem_1_1Surrogate__Problem = -[ - [ "__defaults__", "classSUAVE_1_1Surrogate_1_1Surrogate__Problem_1_1Surrogate__Problem.html#a01369a3a73449c9e32b85f7ced1a24d6", null ], - [ "compute", "classSUAVE_1_1Surrogate_1_1Surrogate__Problem_1_1Surrogate__Problem.html#ae2f195b54e2c25ed08009ba54272ecfa", null ], - [ "constraints_surrogates", "classSUAVE_1_1Surrogate_1_1Surrogate__Problem_1_1Surrogate__Problem.html#aa9100b4649696cd28f63c3875c6c2ef3", null ], - [ "obj_surrogate", "classSUAVE_1_1Surrogate_1_1Surrogate__Problem_1_1Surrogate__Problem.html#ac78ab6ca32dd1abe9c4a105f6ca738b9", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Surrogate_1_1Surrogate__Problem_1_1Surrogate__Problem.png b/_site/doxygen/classSUAVE_1_1Surrogate_1_1Surrogate__Problem_1_1Surrogate__Problem.png deleted file mode 100644 index e7e86a15..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Surrogate_1_1Surrogate__Problem_1_1Surrogate__Problem.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Vehicle_1_1Costs-members.html b/_site/doxygen/classSUAVE_1_1Vehicle_1_1Costs-members.html deleted file mode 100644 index b2bbca83..00000000 --- a/_site/doxygen/classSUAVE_1_1Vehicle_1_1Costs-members.html +++ /dev/null @@ -1,135 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Vehicle.Costs Member List
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Vehicle.Costs Class Reference
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-Inheritance diagram for SUAVE.Vehicle.Costs:
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- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Core.Data.Data
def __getattribute__ (self, k)
 
def __setattr__ (self, k, v)
 
def __delattr__ (self, k)
 
def __defaults__ (self)
 
def __new__ (cls, args, kwarg)
 
def typestring (self)
 
def dataname (self)
 
def __str__ (self, indent='')
 
def __init__ (self, args, kwarg)
 
def __iter__ (self)
 
def itervalues (self)
 
def values (self)
 
def update (self, other)
 
def get_bases (self)
 
def append (self, value, key=None)
 
def deep_set (self, keys, val)
 
def deep_get (self, keys)
 
def pack_array (self, output='vector')
 
def unpack_array (self, M)
 
def do_recursive (self, method, other=None, default=None)
 
- - - - - - - -

-Public Attributes

tag
 
industrial
 
operating
 
-

Detailed Description

-
Costs class for organizing the costs of things
-
-Assumptions:
-None
-
-Source:
-None
-

Member Function Documentation

- -

◆ __defaults__()

- -
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- - - - - - - - -
def SUAVE.Vehicle.Costs.__defaults__ ( self)
-
-
This sets the default values.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Vehicle.py
  • -
-
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Vehicle.Vehicle Member List
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This is the complete list of members for SUAVE.Vehicle.Vehicle, including all inherited members.

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__defaults__(self)SUAVE.Vehicle.Vehicle
__delattr__(self, k)SUAVE.Core.Data.Data
__getattribute__(self, k)SUAVE.Core.Data.Data
__init__(self, args, kwarg)SUAVE.Vehicle.Vehicle
__iter__(self)SUAVE.Core.Data.Data
__new__(cls, args, kwarg)SUAVE.Core.Data.Data
__setattr__(self, k, v)SUAVE.Core.Data.Data
__str__(self, indent='')SUAVE.Core.Data.Data
append(self, value, key=None)SUAVE.Core.Data.Data
append_component(self, component)SUAVE.Vehicle.Vehicle
costs (defined in SUAVE.Vehicle.Vehicle)SUAVE.Vehicle.Vehicle
dataname(self)SUAVE.Core.Data.Data
deep_get(self, keys)SUAVE.Core.Data.Data
deep_set(self, keys, val)SUAVE.Core.Data.Data
do_recursive(self, method, other=None, default=None)SUAVE.Core.Data.Data
energy (defined in SUAVE.Vehicle.Vehicle)SUAVE.Vehicle.Vehicle
envelope (defined in SUAVE.Vehicle.Vehicle)SUAVE.Vehicle.Vehicle
find_component_root(self, component)SUAVE.Vehicle.Vehicle
fuselages (defined in SUAVE.Vehicle.Vehicle)SUAVE.Vehicle.Vehicle
get_bases(self)SUAVE.Core.Data.Data
itervalues(self)SUAVE.Core.Data.Data
mass_properties (defined in SUAVE.Vehicle.Vehicle)SUAVE.Vehicle.Vehicle
max_lift_coefficient_factor (defined in SUAVE.Vehicle.Vehicle)SUAVE.Vehicle.Vehicle
pack_array(self, output='vector')SUAVE.Core.Data.Data
passengers (defined in SUAVE.Vehicle.Vehicle)SUAVE.Vehicle.Vehicle
propulsors (defined in SUAVE.Vehicle.Vehicle)SUAVE.Vehicle.Vehicle
reference_area (defined in SUAVE.Vehicle.Vehicle)SUAVE.Vehicle.Vehicle
systems (defined in SUAVE.Vehicle.Vehicle)SUAVE.Vehicle.Vehicle
tag (defined in SUAVE.Vehicle.Vehicle)SUAVE.Vehicle.Vehicle
typestring(self)SUAVE.Core.Data.Data
unpack_array(self, M)SUAVE.Core.Data.Data
update(self, other)SUAVE.Core.Data.Data
values(self)SUAVE.Core.Data.Data
wings (defined in SUAVE.Vehicle.Vehicle)SUAVE.Vehicle.Vehicle
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- - - - diff --git a/_site/doxygen/classSUAVE_1_1Vehicle_1_1Vehicle.html b/_site/doxygen/classSUAVE_1_1Vehicle_1_1Vehicle.html deleted file mode 100644 index 8907d24b..00000000 --- a/_site/doxygen/classSUAVE_1_1Vehicle_1_1Vehicle.html +++ /dev/null @@ -1,399 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Vehicle.Vehicle Class Reference - - - - - - - - - - - - - - - -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Vehicle.Vehicle Class Reference
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-Inheritance diagram for SUAVE.Vehicle.Vehicle:
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-Public Member Functions

def __defaults__ (self)
 
def __init__ (self, args, kwarg)
 
def find_component_root (self, component)
 
def append_component (self, component)
 
- Public Member Functions inherited from SUAVE.Core.Data.Data
def __getattribute__ (self, k)
 
def __setattr__ (self, k, v)
 
def __delattr__ (self, k)
 
def __defaults__ (self)
 
def __new__ (cls, args, kwarg)
 
def typestring (self)
 
def dataname (self)
 
def __str__ (self, indent='')
 
def __init__ (self, args, kwarg)
 
def __iter__ (self)
 
def itervalues (self)
 
def values (self)
 
def update (self, other)
 
def get_bases (self)
 
def append (self, value, key=None)
 
def deep_set (self, keys, val)
 
def deep_get (self, keys)
 
def pack_array (self, output='vector')
 
def unpack_array (self, M)
 
def do_recursive (self, method, other=None, default=None)
 
- - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

tag
 
fuselages
 
wings
 
propulsors
 
energy
 
systems
 
mass_properties
 
costs
 
envelope
 
reference_area
 
passengers
 
max_lift_coefficient_factor
 
-

Detailed Description

-
SUAVE Vehicle container class with database + input / output functionality
-
-Assumptions:
-None
-
-Source:
-None
-

Constructor & Destructor Documentation

- -

◆ __init__()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Vehicle.Vehicle.__init__ ( self,
 args,
 kwarg 
)
-
-
Sets up the component hierarchy for a vehicle
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Vehicle.Vehicle.__defaults__ ( self)
-
-
This sets the default values.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
- -

◆ append_component()

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-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Vehicle.Vehicle.append_component ( self,
 component 
)
-
-
adds a component to vehicle
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
- -

◆ find_component_root()

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def SUAVE.Vehicle.Vehicle.find_component_root ( self,
 component 
)
-
-
find pointer to component data root.
-
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Vehicle.py
  • -
-
-
- - - - diff --git a/_site/doxygen/classSUAVE_1_1Vehicle_1_1Vehicle.js b/_site/doxygen/classSUAVE_1_1Vehicle_1_1Vehicle.js deleted file mode 100644 index f7a3c59c..00000000 --- a/_site/doxygen/classSUAVE_1_1Vehicle_1_1Vehicle.js +++ /dev/null @@ -1,19 +0,0 @@ -var classSUAVE_1_1Vehicle_1_1Vehicle = -[ - [ "__init__", "classSUAVE_1_1Vehicle_1_1Vehicle.html#ae6908bd99e7d8f4708f4fbcf64ec821d", null ], - [ "__defaults__", "classSUAVE_1_1Vehicle_1_1Vehicle.html#ab279ed6a6b71a4a34fd5e07595b5d640", null ], - [ "append_component", "classSUAVE_1_1Vehicle_1_1Vehicle.html#a33e2631545860ec0f2d89affae0569e7", null ], - [ "find_component_root", "classSUAVE_1_1Vehicle_1_1Vehicle.html#aa5f8c6794e64be4f87f2fc5848d1c5bf", null ], - [ "costs", "classSUAVE_1_1Vehicle_1_1Vehicle.html#a5a86ec750966687ee01ecd04f18f9b61", null ], - [ "energy", "classSUAVE_1_1Vehicle_1_1Vehicle.html#a8dd71874edebf03de72c240406ef6fed", null ], - [ "envelope", "classSUAVE_1_1Vehicle_1_1Vehicle.html#af627044c07d1d292a963abafad9ad4f8", null ], - [ "fuselages", "classSUAVE_1_1Vehicle_1_1Vehicle.html#aa5a1c52d2f0be67663a3a84b5f918182", null ], - [ "mass_properties", "classSUAVE_1_1Vehicle_1_1Vehicle.html#aa8694bc77300ae2ff815e9d59f3775e3", null ], - [ "max_lift_coefficient_factor", "classSUAVE_1_1Vehicle_1_1Vehicle.html#a763d9473ea2c6f89f8da5f07a8521adc", null ], - [ "passengers", "classSUAVE_1_1Vehicle_1_1Vehicle.html#afc67cdf2695b8ecc92f5f067639c3ada", null ], - [ "propulsors", "classSUAVE_1_1Vehicle_1_1Vehicle.html#a50c78d84e282ec3b88d50d5596cdba2c", null ], - [ "reference_area", "classSUAVE_1_1Vehicle_1_1Vehicle.html#a60668c7b9710b4df0a667ec8e9c0d7dd", null ], - [ "systems", "classSUAVE_1_1Vehicle_1_1Vehicle.html#ab8b0b39ab3b930928b161151cacfdc59", null ], - [ "tag", "classSUAVE_1_1Vehicle_1_1Vehicle.html#a91d0af7fac13cf22c95a7d085ec96dbf", null ], - [ "wings", "classSUAVE_1_1Vehicle_1_1Vehicle.html#aecfdeb1df5bdcea1e38d1b9e1a5dce70", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Vehicle_1_1Vehicle.png b/_site/doxygen/classSUAVE_1_1Vehicle_1_1Vehicle.png deleted file mode 100644 index d50776ed..00000000 Binary files a/_site/doxygen/classSUAVE_1_1Vehicle_1_1Vehicle.png and /dev/null differ diff --git a/_site/doxygen/classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties-members.html b/_site/doxygen/classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties-members.html deleted file mode 100644 index 8b515e68..00000000 --- a/_site/doxygen/classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties-members.html +++ /dev/null @@ -1,132 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Vehicle.Vehicle_Mass_Properties Member List
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This is the complete list of members for SUAVE.Vehicle.Vehicle_Mass_Properties, including all inherited members.

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__defaults__(self)SUAVE.Vehicle.Vehicle_Mass_Properties
cargo (defined in SUAVE.Vehicle.Vehicle_Mass_Properties)SUAVE.Vehicle.Vehicle_Mass_Properties
center_of_gravity (defined in SUAVE.Vehicle.Vehicle_Mass_Properties)SUAVE.Vehicle.Vehicle_Mass_Properties
crew (defined in SUAVE.Vehicle.Vehicle_Mass_Properties)SUAVE.Vehicle.Vehicle_Mass_Properties
fuel (defined in SUAVE.Vehicle.Vehicle_Mass_Properties)SUAVE.Vehicle.Vehicle_Mass_Properties
landing (defined in SUAVE.Vehicle.Vehicle_Mass_Properties)SUAVE.Vehicle.Vehicle_Mass_Properties
mass (defined in SUAVE.Components.Mass_Properties.Mass_Properties)SUAVE.Components.Mass_Properties.Mass_Properties
max_cargo (defined in SUAVE.Vehicle.Vehicle_Mass_Properties)SUAVE.Vehicle.Vehicle_Mass_Properties
max_fuel (defined in SUAVE.Vehicle.Vehicle_Mass_Properties)SUAVE.Vehicle.Vehicle_Mass_Properties
max_landing (defined in SUAVE.Vehicle.Vehicle_Mass_Properties)SUAVE.Vehicle.Vehicle_Mass_Properties
max_payload (defined in SUAVE.Vehicle.Vehicle_Mass_Properties)SUAVE.Vehicle.Vehicle_Mass_Properties
max_takeoff (defined in SUAVE.Vehicle.Vehicle_Mass_Properties)SUAVE.Vehicle.Vehicle_Mass_Properties
max_zero_fuel (defined in SUAVE.Vehicle.Vehicle_Mass_Properties)SUAVE.Vehicle.Vehicle_Mass_Properties
moments_of_inertia (defined in SUAVE.Components.Mass_Properties.Mass_Properties)SUAVE.Components.Mass_Properties.Mass_Properties
operating_empty (defined in SUAVE.Vehicle.Vehicle_Mass_Properties)SUAVE.Vehicle.Vehicle_Mass_Properties
passenger (defined in SUAVE.Vehicle.Vehicle_Mass_Properties)SUAVE.Vehicle.Vehicle_Mass_Properties
payload (defined in SUAVE.Vehicle.Vehicle_Mass_Properties)SUAVE.Vehicle.Vehicle_Mass_Properties
takeoff (defined in SUAVE.Vehicle.Vehicle_Mass_Properties)SUAVE.Vehicle.Vehicle_Mass_Properties
volume (defined in SUAVE.Components.Mass_Properties.Mass_Properties)SUAVE.Components.Mass_Properties.Mass_Properties
zero_fuel_center_of_gravity (defined in SUAVE.Vehicle.Vehicle_Mass_Properties)SUAVE.Vehicle.Vehicle_Mass_Properties
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Vehicle.Vehicle_Mass_Properties Class Reference
-
-
-
-Inheritance diagram for SUAVE.Vehicle.Vehicle_Mass_Properties:
-
-
- - -SUAVE.Components.Mass_Properties.Mass_Properties - -
- - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Mass_Properties.Mass_Properties
def __defaults__ (self)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

operating_empty
 
max_takeoff
 
takeoff
 
max_landing
 
landing
 
max_cargo
 
cargo
 
max_payload
 
payload
 
passenger
 
crew
 
max_fuel
 
fuel
 
max_zero_fuel
 
center_of_gravity
 
zero_fuel_center_of_gravity
 
- Public Attributes inherited from SUAVE.Components.Mass_Properties.Mass_Properties
mass
 
volume
 
center_of_gravity
 
moments_of_inertia
 
-

Detailed Description

-
Vehicle_Mass_Properties():
-    The vehicle's mass properties.
-
-
-Assumptions:
-None
-
-Source:
-None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Vehicle.Vehicle_Mass_Properties.__defaults__ ( self)
-
-
This sets the default values.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Vehicle.py
  • -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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Constant_Speed_Constant_Altitude_Loiter (SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude_Loiter)   Fidelity_One (SUAVE.Analyses.Noise.Fidelity_One)   output (SUAVE.Core.redirect)   Surrogate_Problem (SUAVE.Surrogate.Surrogate_Problem)   
Constant_Speed_Constant_Angle (SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle)   Fidelity_Zero (SUAVE.Analyses.Aerodynamics.Fidelity_Zero)   
  p  
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System (SUAVE.Components.Systems.System)   
_Exception (SUAVE.Plugins.pint.quantity)   Constant_Speed_Constant_Angle (SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle)   Fidelity_Zero (SUAVE.Analyses.Stability.Fidelity_Zero)   
  t  
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_Quantity (SUAVE.Plugins.pint.quantity)   Constant_Speed_Constant_Angle_Noise (SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle_Noise)   folder (SUAVE.Core.redirect)   ParserHelper (SUAVE.Plugins.pint.util)   
  a  
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Constant_Speed_Constant_Angle_Noise (SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle_Noise)   Fuel_Cell (SUAVE.Components.Energy.Converters.Fuel_Cell)   Payload (SUAVE.Components.Energy.Peripherals.Payload)   Takeoff (SUAVE.Analyses.Mission.Segments.Ground.Takeoff)   
Constant_Speed_Constant_Rate (SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Rate)   Fuselage (SUAVE.Components.Fuselages.Fuselage)   Payload (SUAVE.Components.Payloads.Payload)   TestBitTwiddlingUfuncs (SUAVE.Plugins.pint.testsuite.test_numpy)   
AERODAS (SUAVE.Analyses.Aerodynamics.AERODAS)   Constant_Speed_Constant_Rate (SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Rate)   
  g  
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Person (SUAVE.Components.Payloads.Person)   TestCase (SUAVE.Plugins.pint.testsuite)   
Aerodynamic (SUAVE.Analyses.Mission.Segments.Aerodynamic)   Constant_Speed_Linear_Altitude (SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Linear_Altitude)   Physical_Component (SUAVE.Components.Physical_Component)   TestComparisonUfuncs (SUAVE.Plugins.pint.testsuite.test_umath)   
Aerodynamics (SUAVE.Analyses.Aerodynamics.Aerodynamics)   Constant_Temperature (SUAVE.Analyses.Atmospheric.Constant_Temperature)   Gas (SUAVE.Attributes.Gases.Gas)   Planet (SUAVE.Analyses.Planets.Planet)   TestContexts (SUAVE.Plugins.pint.testsuite.test_contexts)   
Aerodynamics (SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics)   Constant_Temperature (SUAVE.Attributes.Atmospheres.Earth.Constant_Temperature)   Gaseous_H2 (SUAVE.Attributes.Propellants.Gaseous_H2)   Planet (SUAVE.Attributes.Planets.Planet)   TestConverter (SUAVE.Plugins.pint.testsuite.test_unit)   
Air (SUAVE.Attributes.Gases.Air)   Constant_Throttle_Constant_Altitude (SUAVE.Analyses.Mission.Segments.Cruise.Constant_Throttle_Constant_Altitude)   Gearbox (SUAVE.Components.Energy.Converters.Gearbox)   PrefixDefinition (SUAVE.Plugins.pint.unit)   TestDefinedContexts (SUAVE.Plugins.pint.testsuite.test_contexts)   
Aircraft (SUAVE.Methods.Aerodynamics.AVL.Data.Aircraft)   Constant_Throttle_Constant_Speed (SUAVE.Analyses.Mission.Segments.Climb.Constant_Throttle_Constant_Speed)   Geometry (SUAVE.Analyses.Geometry.Geometry)   Process (SUAVE.Analyses.Process)   TestDefinition (SUAVE.Plugins.pint.testsuite.test_unit)   
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All_At_Once (SUAVE.Analyses.Mission.All_At_Once)   Container (SUAVE.Analyses.Mission.Segments.Segment)   
  h  
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Propeller (SUAVE.Components.Energy.Converters.Propeller)   TestHandler (SUAVE.Plugins.pint.testsuite.test_contexts)   
Aluminum_Air (SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Aluminum_Air)   Container (SUAVE.Analyses.Mission.Segments.Simple)   Propeller_Lo_Fid (SUAVE.Components.Energy.Converters.Propeller_Lo_Fid)   TestIssues (SUAVE.Plugins.pint.testsuite.test_issues)   
Analysis (SUAVE.Analyses.Analysis)   Container (SUAVE.Analyses.Mission.Sequential_Segments)   Horizontal_Tail (SUAVE.Components.Wings.Horizontal_Tail)   Property (SUAVE.Core.DataOrdered)   TestIssuesNP (SUAVE.Plugins.pint.testsuite.test_issues)   
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  i  
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Propulsor_Surrogate (SUAVE.Components.Energy.Networks.Propulsor_Surrogate)   TestMeasurement (SUAVE.Plugins.pint.testsuite.test_measurement)   
Attributes (SUAVE.Input_Output.XML.Data)   Container (SUAVE.Components.Payloads.Payload)   
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TestNumpyMethods (SUAVE.Plugins.pint.testsuite.test_numpy)   
Aviation_Gasoline (SUAVE.Attributes.Propellants.Aviation_Gasoline)   Container (SUAVE.Components.Propulsors.Propulsor)   Industrial_Costs (SUAVE.Components.Costs.Costs)   TestNumpyNotSupported (SUAVE.Plugins.pint.testsuite.test_numpy)   
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AVL (SUAVE.Analyses.Stability.AVL)   Container (SUAVE.Components.Systems.System)   
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Residuals (SUAVE.Analyses.Mission.Segments.Conditions.Residuals)   TestQuantity (SUAVE.Plugins.pint.testsuite.test_quantity)   
AVL (SUAVE.Analyses.Aerodynamics.AVL)   Container (SUAVE.Analyses.Mission.Segments.Conditions.State)   Results (SUAVE.Analyses.Aerodynamics.Results)   TestRegistry (SUAVE.Plugins.pint.testsuite.test_unit)   
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  l  
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Run_Case (SUAVE.Methods.Aerodynamics.AVL.Data.Cases)   TestUFuncs (SUAVE.Plugins.pint.testsuite.test_umath)   
  b  
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Container (SUAVE.Core.Diffed_Data)   Runway (SUAVE.Attributes.Airports.Runway)   TestUnitsContainer (SUAVE.Plugins.pint.testsuite.test_unit)   
Container (SUAVE.Attributes.Constants.Constant)   Landing (SUAVE.Analyses.Mission.Segments.Ground.Landing)   
  s  
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Thrust (SUAVE.Components.Energy.Processes.Thrust)   
Basic (SUAVE.Analyses.Mission.Segments.Conditions.Basic)   Container (SUAVE.Methods.Aerodynamics.AVL.Data.Cases)   Landing_Gear (SUAVE.Components.Landing_Gear.Landing_Gear)   Tree_Element (SUAVE.Input_Output.D3JS.Tree_Element)   
Battery (SUAVE.Components.Energy.Storages.Batteries.Battery)   Container (SUAVE.Components.Component)   Lift_Forward (SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor)   Satellite (SUAVE.Components.Payloads.Satellite)   TreeBuilder (SUAVE.Input_Output.XML.load)   
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Battery_Propeller (SUAVE.Components.Energy.Networks.Battery_Propeller)   ContextChain (SUAVE.Plugins.pint.context)   Linear_Speed_Constant_Rate (SUAVE.Analyses.Mission.Segments.Climb.Linear_Speed_Constant_Rate)   Section (SUAVE.Methods.Aerodynamics.AVL.Data.Wing)   Turbine (SUAVE.Components.Energy.Converters.Turbine)   
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Control_Surface (SUAVE.Methods.Aerodynamics.AVL.Data.Wing)   Liquid_H2 (SUAVE.Attributes.Propellants.Liquid_H2)   Segment (SUAVE.Components.Lofted_Body)   Turbojet_Super (SUAVE.Components.Energy.Networks.Turbojet_Super)   
Control_Surface_Section (SUAVE.Components.Wings.Control_Surface)   Liquid_Natural_Gas (SUAVE.Attributes.Propellants.Liquid_Natural_Gas)   Segment (SUAVE.Analyses.Mission.Segments.Segment)   
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Cargo (SUAVE.Components.Payloads.Cargo)   Converter (SUAVE.Plugins.pint.unit)   Lithium_Air (SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Lithium_Air)   Segment (SUAVE.Components.Wings.Segment)   
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Climb (SUAVE.Analyses.Mission.Segments.Hover.Climb)   Costs (SUAVE.Analyses.Costs.Costs)   Lithium_Sulfur (SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Sulfur)   Sequential_Segments (SUAVE.Analyses.Mission.Sequential_Segments)   UnitDefinition (SUAVE.Plugins.pint.unit)   
CO2 (SUAVE.Attributes.Gases.CO2)   Curve (SUAVE.Components.Lofted_Body)   Loads (SUAVE.Analyses.Loads.Loads)   Set_Speed_Set_Altitude (SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude)   UnitRegistry (SUAVE.Plugins.pint.unit)   
Combustor (SUAVE.Components.Energy.Converters.Combustor)   CurveContainer (SUAVE.Components.Lofted_Body)   Lofted_Body (SUAVE.Components.Lofted_Body)   Set_Speed_Set_Throttle (SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Throttle)   UnitsContainer (SUAVE.Plugins.pint.unit)   
Component (SUAVE.Components.Energy.Energy)   
  d  
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  m  
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Settings (SUAVE.Analyses.Settings)   Unknown_Throttle (SUAVE.Analyses.Mission.Segments.Descent.Unknown_Throttle)   
Component (SUAVE.Components.Component)   Settings (SUAVE.Methods.Aerodynamics.AVL.Data.Settings)   Unknown_Throttle (SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle)   
ComponentContainer (SUAVE.Components.Energy.Energy)   Data (SUAVE.Core.Data)   Main_Landing_Gear (SUAVE.Components.Landing_Gear.Main_Landing_Gear)   Shaft_Power_Off_Take (SUAVE.Components.Energy.Converters.Shaft_Power_Off_Take)   Unknowns (SUAVE.Analyses.Mission.Segments.Conditions.Unknowns)   
Composition (SUAVE.Attributes.Constants.Composition)   Data (SUAVE.Input_Output.XML.Data)   Main_Wing (SUAVE.Components.Wings.Main_Wing)   Simple (SUAVE.Analyses.Mission.Segments.Simple)   US_Standard_1976 (SUAVE.Attributes.Atmospheres.Earth.US_Standard_1976)   
Compression_Nozzle (SUAVE.Components.Energy.Converters.Compression_Nozzle)   DataOrdered (SUAVE.Core.DataOrdered)   Markup (SUAVE.Analyses.Aerodynamics.Markup)   Sizing (SUAVE.Analyses.Sizing.Sizing)   US_Standard_1976 (SUAVE.Analyses.Atmospheric.US_Standard_1976)   
Compressor (SUAVE.Components.Energy.Converters.Compressor)   Definition (SUAVE.Plugins.pint.unit)   Mars (SUAVE.Attributes.Planets.Mars)   Sizing_Loop (SUAVE.Sizing.Sizing_Loop)   
  v  
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Conditions (SUAVE.Analyses.Mission.Segments.Conditions.Conditions)   Descent (SUAVE.Analyses.Mission.Segments.Hover.Descent)   Mass_Properties (SUAVE.Components.Mass_Properties)   Solar (SUAVE.Components.Energy.Networks.Solar)   
Config (SUAVE.Components.Configs.Config)   Diffed_Data (SUAVE.Core.Diffed_Data)   Measurement (SUAVE.Plugins.pint.measurement)   Solar_Logic (SUAVE.Components.Energy.Distributors.Solar_Logic)   Vehicle (SUAVE.Analyses.Vehicle)   
Configuration (SUAVE.Methods.Aerodynamics.AVL.Data.Configuration)   DimensionalityError (SUAVE.Plugins.pint.unit)   Mission (SUAVE.Analyses.Mission.Mission)   Solar_Low_Fidelity (SUAVE.Components.Energy.Networks.Solar_Low_Fidelity)   Vehicle (SUAVE.Vehicle)   
Constant (SUAVE.Attributes.Constants.Constant)   DimensionDefinition (SUAVE.Plugins.pint.unit)   Motor (SUAVE.Components.Energy.Converters.Motor)   Solar_Panel (SUAVE.Components.Energy.Converters.Solar_Panel)   Vehicle_Mass_Properties (SUAVE.Vehicle)   
Constant_Acceleration_Constant_Altitude (SUAVE.Analyses.Mission.Segments.Cruise.Constant_Acceleration_Constant_Altitude)   Dual_Battery_Ducted_Fan (SUAVE.Components.Energy.Networks.Dual_Battery_Ducted_Fan)   Motor_Lo_Fid (SUAVE.Components.Energy.Converters.Motor_Lo_Fid)   Solar_Radiation (SUAVE.Components.Energy.Processes.Solar_Radiation)   Vertical_Tail (SUAVE.Components.Wings.Vertical_Tail)   
Constant_Dynamic_Pressure_Constant_Altitude (SUAVE.Analyses.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude)   Ducted_Fan (SUAVE.Components.Energy.Networks.Ducted_Fan)   
  n  
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Stability (SUAVE.Analyses.Stability.Stability)   Vortex_Lattice (SUAVE.Analyses.Aerodynamics.Vortex_Lattice)   
Constant_Dynamic_Pressure_Constant_Altitude_Loiter (SUAVE.Analyses.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude_Loiter)   
  e  
-
State (SUAVE.Analyses.Mission.Segments.Conditions.State)   
  w  
-
Constant_Dynamic_Pressure_Constant_Angle (SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Angle)   ndarray (SUAVE.Plugins.pint.util)   Steam (SUAVE.Attributes.Gases.Steam)   
Constant_Dynamic_Pressure_Constant_Rate (SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Rate)   Earth (SUAVE.Attributes.Planets.Earth)   ndarray (SUAVE.Plugins.pint.testsuite)   Structures (SUAVE.Analyses.Structures.Structures)   Water (SUAVE.Attributes.Liquids.Water)   
Constant_EAS_Constant_Rate (SUAVE.Analyses.Mission.Segments.Descent.Constant_EAS_Constant_Rate)   Electronic_Speed_Controller (SUAVE.Components.Energy.Distributors.Electronic_Speed_Controller)   Nexus (SUAVE.Optimization.Nexus)   SU2_Euler (SUAVE.Analyses.Aerodynamics.SU2_Euler)   Weights (SUAVE.Analyses.Weights.Weights)   
Constant_EAS_Constant_Rate (SUAVE.Analyses.Mission.Segments.Climb.Constant_EAS_Constant_Rate)   Energy (SUAVE.Components.Energy.Energy)   Noise (SUAVE.Analyses.Noise.Noise)   SU2_Euler_Super (SUAVE.Analyses.Aerodynamics.SU2_Euler_Super)   Weights_BWB (SUAVE.Analyses.Weights.Weights_BWB)   
Constant_Mach_Constant_Altitude (SUAVE.Analyses.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude)   Energy (SUAVE.Analyses.Energy.Energy)   Nose_Landing_Gear (SUAVE.Components.Landing_Gear.Nose_Landing_Gear)   SU2_inviscid (SUAVE.Analyses.Aerodynamics.SU2_inviscid)   Weights_Tube_Wing (SUAVE.Analyses.Weights.Weights_Tube_Wing)   
Constant_Mach_Constant_Altitude_Loiter (SUAVE.Analyses.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude_Loiter)   Energy_Component (SUAVE.Components.Energy.Energy_Component)   Numerics (SUAVE.Analyses.Mission.Segments.Conditions.Numerics)   SU2_inviscid_Super (SUAVE.Analyses.Aerodynamics.SU2_inviscid_Super)   Weights_UAV (SUAVE.Analyses.Weights.Weights_UAV)   
Constant_Mach_Constant_Angle (SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Angle)   Envelope (SUAVE.Components.Envelope)   
  o  
-
Supersonic_Nozzle (SUAVE.Components.Energy.Converters.Supersonic_Nozzle)   Wing (SUAVE.Components.Wings.Wing)   
Constant_Mach_Constant_Rate (SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Rate)   Expansion_Nozzle (SUAVE.Components.Energy.Converters.Expansion_Nozzle)   Supersonic_OpenVSP_Wave_Drag (SUAVE.Analyses.Aerodynamics.Supersonic_OpenVSP_Wave_Drag)   Wing (SUAVE.Methods.Aerodynamics.AVL.Data.Wing)   
Constant_Mach_Linear_Altitude (SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Linear_Altitude)   
  f  
-
OffsetConverter (SUAVE.Plugins.pint.unit)   Supersonic_Zero (SUAVE.Analyses.Aerodynamics.Supersonic_Zero)   
Constant_Pitch_Rate_Constant_Altitude (SUAVE.Analyses.Mission.Segments.Cruise.Constant_Pitch_Rate_Constant_Altitude)   Operating_Costs (SUAVE.Components.Costs.Costs)   Surrogate (SUAVE.Analyses.Surrogate)   
Constant_Speed_Constant_Altitude (SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude)   Fan (SUAVE.Components.Energy.Converters.Fan)   Optimized (SUAVE.Analyses.Mission.Segments.Climb.Optimized)   Surrogate_Optimization (SUAVE.Optimization.Surrogate_Optimization)   
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SUAVE -  1.0.0 -
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-
- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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Conditions
-
-
- -

These are analyses files that help setup a mission. -More...

- - - - - - - - - - - - - - - - - - -

-Classes

class  SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics
 
class  SUAVE.Analyses.Mission.Segments.Conditions.Basic.Basic
 
class  SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
 
class  SUAVE.Analyses.Mission.Segments.Conditions.Numerics.Numerics
 
class  SUAVE.Analyses.Mission.Segments.Conditions.Residuals.Residuals
 
class  SUAVE.Analyses.Mission.Segments.Conditions.State.State
 
class  SUAVE.Analyses.Mission.Segments.Conditions.State.Container
 
class  SUAVE.Analyses.Mission.Segments.Conditions.Unknowns.Unknowns
 
- - - -

-Functions

def SUAVE.Analyses.Mission.Segments.Conditions.State.append_array (A, B=None)
 
-

Detailed Description

-

These are analyses files that help setup a mission.

-

They create the data structure. They're not something the user normally toucbes.

-

Function Documentation

- -

◆ append_array()

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def SUAVE.Analyses.Mission.Segments.Conditions.State.append_array ( A,
 B = None 
)
-
-
A stacking operation used by merged to put together data structures
-
-    Assumptions:
-    None
-
-    Source:
-    N/A
-
-    Inputs:
-    A [array]
-    B [array]
-
-    Outputs:
-    array
-
-    Properties Used:
-    None
-
-
-
-
-
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Single_Point
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Single point segments. -More...

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Detailed Description

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Single point segments.

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These are simple snapshots in time.

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Segment
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Segment analyses to setup each part of a mission to fly. -More...

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 Segments for climbing flight.
 
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 Segments for cruise flight.
 
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 Segments for descending flight.
 
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 Segments for ground operations.
 
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 Single point segments.
 
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-

Detailed Description

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Segment analyses to setup each part of a mission to fly.

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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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Vary_Cruise
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Variable cruise mission setups. -More...

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Detailed Description

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Variable cruise mission setups.

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Mission
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Mission Analyses to setup each part of a mission to fly. -More...

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-Modules

 Segment
 Segment analyses to setup each part of a mission to fly.
 
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 Variable cruise mission setups.
 
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Detailed Description

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Mission Analyses to setup each part of a mission to fly.

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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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These are the analyses that control noise evaluations. -More...

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-Classes

class  SUAVE.Analyses.Noise.Fidelity_One.Fidelity_One
 
class  SUAVE.Analyses.Noise.Noise.Noise
 
-

Detailed Description

-

These are the analyses that control noise evaluations.

-
-
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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Sizing
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This is the analysis that controls vehicle sizing evaluations. -More...

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-Classes

class  SUAVE.Analyses.Sizing.Sizing.Sizing
 
-

Detailed Description

-

This is the analysis that controls vehicle sizing evaluations.

-
-
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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Stability
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-
- - - - - - - - -
-
SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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Structures
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This is the analysis that controls vehicle structure evaluations. -More...

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-Classes

class  SUAVE.Analyses.Structures.Structures.Structures
 
-

Detailed Description

-

This is the analysis that controls vehicle structure evaluations.

-
-
- - - - diff --git a/_site/doxygen/group__Analyses-Structures.js b/_site/doxygen/group__Analyses-Structures.js deleted file mode 100644 index f99db1d0..00000000 --- a/_site/doxygen/group__Analyses-Structures.js +++ /dev/null @@ -1,10 +0,0 @@ -var group__Analyses_Structures = -[ - [ "Structures", "classSUAVE_1_1Analyses_1_1Structures_1_1Structures_1_1Structures.html", [ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Structures_1_1Structures_1_1Structures.html#af4900ed36ae06effa0ecb10080e0a667", null ], - [ "evaluate", "classSUAVE_1_1Analyses_1_1Structures_1_1Structures_1_1Structures.html#ab08fe047a6db230f0029c0d99f8d44f7", null ], - [ "features", "classSUAVE_1_1Analyses_1_1Structures_1_1Structures_1_1Structures.html#a4de2b7356404f1e4d38b3509bf8dc9ad", null ], - [ "settings", "classSUAVE_1_1Analyses_1_1Structures_1_1Structures_1_1Structures.html#a7010fe6e6c8eee4c11c401441855d3ae", null ], - [ "tag", "classSUAVE_1_1Analyses_1_1Structures_1_1Structures_1_1Structures.html#a8a7a57d3440fa99c345d107250296f5e", null ] - ] ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Analyses-Weights.html b/_site/doxygen/group__Analyses-Weights.html deleted file mode 100644 index 4acd706f..00000000 --- a/_site/doxygen/group__Analyses-Weights.html +++ /dev/null @@ -1,128 +0,0 @@ - - - - - - - -SUAVE: Weights - - - - - - - - - - - - - - - -
-
- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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Weights
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Classes that represent the types of aircraft configuration weight computations. -More...

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-Classes

class  SUAVE.Analyses.Weights.Weights.Weights
 
class  SUAVE.Analyses.Weights.Weights_BWB.Weights_BWB
 
class  SUAVE.Analyses.Weights.Weights_Tube_Wing.Weights_Tube_Wing
 
class  SUAVE.Analyses.Weights.Weights_UAV.Weights_UAV
 
-

Detailed Description

-

Classes that represent the types of aircraft configuration weight computations.

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-
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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Analyses
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Analyses are classes that are comprised of several methods. -More...

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-Modules

 Aerodynamics
 These are the analyses that control aerodynamic evaluations.
 
 Atmospheric
 Classes that represent the different types of atmospheres that may be used for analysis.
 
 Costs
 Cost Analysis.
 
 Energy
 This is the analysis that controls energy network evaluations.
 
 Geometry
 This is the analysis that controls vehicle geometry evaluations.
 
 Loads
 This is the analysis that controls vehicle load evaluations.
 
 Mission
 Mission Analyses to setup each part of a mission to fly.
 
 Noise
 These are the analyses that control noise evaluations.
 
 Sizing
 This is the analysis that controls vehicle sizing evaluations.
 
 Stability
 
 Structures
 This is the analysis that controls vehicle structure evaluations.
 
 Weights
 Classes that represent the types of aircraft configuration weight computations.
 
- - - - - - - - - - - - - - - -

-Classes

class  SUAVE.Analyses.Analysis.Analysis
 
class  SUAVE.Analyses.Analysis.Container
 
class  SUAVE.Analyses.Process.Process
 
class  SUAVE.Analyses.Settings.Settings
 
class  SUAVE.Analyses.Settings.Container
 
class  SUAVE.Analyses.Surrogate.Surrogate
 
class  SUAVE.Analyses.Vehicle.Vehicle
 
-

Detailed Description

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Analyses are classes that are comprised of several methods.

-

Methods operate on attributes. This process and structure is described here.

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- - - - diff --git a/_site/doxygen/group__Analyses.js b/_site/doxygen/group__Analyses.js deleted file mode 100644 index e821bcb3..00000000 --- a/_site/doxygen/group__Analyses.js +++ /dev/null @@ -1,67 +0,0 @@ -var group__Analyses = -[ - [ "Aerodynamics", "group__Analyses-Aerodynamics.html", "group__Analyses-Aerodynamics" ], - [ "Atmospheric", "group__Analyses-Atmospheric.html", "group__Analyses-Atmospheric" ], - [ "Costs", "group__Analyses-Costs.html", "group__Analyses-Costs" ], - [ "Energy", "group__Analyses-Energy.html", "group__Analyses-Energy" ], - [ "Geometry", "group__Analyses-Geometry.html", "group__Analyses-Geometry" ], - [ "Loads", "group__Analyses-Loads.html", "group__Analyses-Loads" ], - [ "Mission", "group__Analyses-Mission.html", "group__Analyses-Mission" ], - [ "Noise", "group__Analyses-Noise.html", "group__Analyses-Noise" ], - [ "Sizing", "group__Analyses-Sizing.html", "group__Analyses-Sizing" ], - [ "Stability", "group__Analyses-Stability.html", "group__Analyses-Stability" ], - 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- - - - - - -SUAVE: Airports - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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Airports
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These are airport related classes. -More...

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-Classes

class  SUAVE.Attributes.Airports.Airport.Airport
 
class  SUAVE.Attributes.Airports.Runway.Runway
 
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Detailed Description

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These are airport related classes.

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-
- - - - diff --git a/_site/doxygen/group__Attributes-Airports.js b/_site/doxygen/group__Attributes-Airports.js deleted file mode 100644 index 083a090a..00000000 --- a/_site/doxygen/group__Attributes-Airports.js +++ /dev/null @@ -1,14 +0,0 @@ -var group__Attributes_Airports = -[ - [ "Airport", "classSUAVE_1_1Attributes_1_1Airports_1_1Airport_1_1Airport.html", [ - [ "__defaults__", "classSUAVE_1_1Attributes_1_1Airports_1_1Airport_1_1Airport.html#a87751519698b56e2366bf388d21052d1", null ], - [ "altitude", "classSUAVE_1_1Attributes_1_1Airports_1_1Airport_1_1Airport.html#afeb3e603029ff1b68262205550dfd4aa", null ], - [ "atmosphere", "classSUAVE_1_1Attributes_1_1Airports_1_1Airport_1_1Airport.html#a67a9bede56cdd73aa673e5a1b36f7790", null ], - [ "delta_isa", "classSUAVE_1_1Attributes_1_1Airports_1_1Airport_1_1Airport.html#a62abe14755e7944ad08f587861c17452", null ], - [ "tag", "classSUAVE_1_1Attributes_1_1Airports_1_1Airport_1_1Airport.html#a1cf3dc8bf593783283bf1a807385fb31", null ] - ] ], - [ "Runway", "classSUAVE_1_1Attributes_1_1Airports_1_1Runway_1_1Runway.html", [ - [ "__defaults__", "classSUAVE_1_1Attributes_1_1Airports_1_1Runway_1_1Runway.html#a952b090516a9563fc9f040c891493737", null ], - [ "tag", "classSUAVE_1_1Attributes_1_1Airports_1_1Runway_1_1Runway.html#a90f4ba576b4d5091fb0ce8caf86bf9e3", null ] - ] ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Attributes-Atmospheres-Earth.html b/_site/doxygen/group__Attributes-Atmospheres-Earth.html deleted file mode 100644 index ae11e39c..00000000 --- a/_site/doxygen/group__Attributes-Atmospheres-Earth.html +++ /dev/null @@ -1,124 +0,0 @@ - - - - - - - -SUAVE: Earth - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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Contains basic data for specific Earth atmosphere types. -More...

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class  SUAVE.Attributes.Atmospheres.Earth.Constant_Temperature.Constant_Temperature
 
class  SUAVE.Attributes.Atmospheres.Earth.US_Standard_1976.US_Standard_1976
 
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Detailed Description

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Contains basic data for specific Earth atmosphere types.

-
-
- - - - diff --git a/_site/doxygen/group__Attributes-Atmospheres-Earth.js b/_site/doxygen/group__Attributes-Atmospheres-Earth.js deleted file mode 100644 index ac4d3d61..00000000 --- a/_site/doxygen/group__Attributes-Atmospheres-Earth.js +++ /dev/null @@ -1,16 +0,0 @@ -var group__Attributes_Atmospheres_Earth = -[ - [ "Constant_Temperature", "classSUAVE_1_1Attributes_1_1Atmospheres_1_1Earth_1_1Constant__Temperature_1_1Constant__Temperature.html", [ - [ "__defaults__", "classSUAVE_1_1Attributes_1_1Atmospheres_1_1Earth_1_1Constant__Temperature_1_1Constant__Temperature.html#a92622bef320a1c81d3af37c7596f6c1d", null ], - [ "breaks", "classSUAVE_1_1Attributes_1_1Atmospheres_1_1Earth_1_1Constant__Temperature_1_1Constant__Temperature.html#a38e7bf852e905f3fb8fe792a17fb214a", null ], - [ "fluid_properties", "classSUAVE_1_1Attributes_1_1Atmospheres_1_1Earth_1_1Constant__Temperature_1_1Constant__Temperature.html#ae1c49eaf59f3dab65e6765b11db601b2", null ], - [ "planet", "classSUAVE_1_1Attributes_1_1Atmospheres_1_1Earth_1_1Constant__Temperature_1_1Constant__Temperature.html#affc343bce9f9d20caed0a663c773eb36", null ] - ] ], - [ "US_Standard_1976", "classSUAVE_1_1Attributes_1_1Atmospheres_1_1Earth_1_1US__Standard__1976_1_1US__Standard__1976.html", [ - [ "__defaults__", "classSUAVE_1_1Attributes_1_1Atmospheres_1_1Earth_1_1US__Standard__1976_1_1US__Standard__1976.html#ac126d272ade6b9e6cdf4676fa1a74481", null ], - [ "breaks", "classSUAVE_1_1Attributes_1_1Atmospheres_1_1Earth_1_1US__Standard__1976_1_1US__Standard__1976.html#a1f5d0138162f34940d6c70708f60ec3d", null ], - [ "fluid_properties", "classSUAVE_1_1Attributes_1_1Atmospheres_1_1Earth_1_1US__Standard__1976_1_1US__Standard__1976.html#aafe591a742dabc7c30eb0102e36e0e6f", null ], - [ "planet", "classSUAVE_1_1Attributes_1_1Atmospheres_1_1Earth_1_1US__Standard__1976_1_1US__Standard__1976.html#a1d06e1096c3fd570851ab5d70c85842a", null ], - [ "tag", "classSUAVE_1_1Attributes_1_1Atmospheres_1_1Earth_1_1US__Standard__1976_1_1US__Standard__1976.html#a282283c9824da8bfaabc7fb112ef47a5", null ] - ] ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Attributes-Atmospheres.html b/_site/doxygen/group__Attributes-Atmospheres.html deleted file mode 100644 index d9a01a17..00000000 --- a/_site/doxygen/group__Attributes-Atmospheres.html +++ /dev/null @@ -1,129 +0,0 @@ - - - - - - - -SUAVE: Atmospheres - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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Atmospheres
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Contains basic data for atmospheres. -More...

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 Earth
 Contains basic data for specific Earth atmosphere types.
 
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-Classes

class  SUAVE.Attributes.Atmospheres.Atmosphere.Atmosphere
 
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Detailed Description

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Contains basic data for atmospheres.

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-
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- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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Constants
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- -

Contains basic data for atmospheres. -More...

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-Classes

class  SUAVE.Attributes.Constants.Composition.Composition
 
class  SUAVE.Attributes.Constants.Constant.Constant
 
-

Detailed Description

-

Contains basic data for atmospheres.

-

classes

-
-
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SUAVE -  1.0.0 -
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Common gasesclasses. -More...

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class  SUAVE.Attributes.Gases.Air.Air
 
class  SUAVE.Attributes.Gases.CO2.CO2
 
class  SUAVE.Attributes.Gases.Gas.Gas
 
class  SUAVE.Attributes.Gases.Steam.Steam
 
-

Detailed Description

-

Common gases

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classes.

-
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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Liquids
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Common liquidsclasses. -More...

- - - - - - -

-Classes

class  SUAVE.Attributes.Liquids.Liquid.Liquid
 
class  SUAVE.Attributes.Liquids.Water.Water
 
-

Detailed Description

-

Common liquids

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classes.

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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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Planets
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Available planetsclasses. -More...

- - - - - - - - -

-Classes

class  SUAVE.Attributes.Planets.Earth.Earth
 
class  SUAVE.Attributes.Planets.Mars.Mars
 
class  SUAVE.Attributes.Planets.Planet.Planet
 
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Detailed Description

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Available planets

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classes.

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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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Attributes
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Attributes provide objects that can be attached to various analyses. -More...

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-Modules

 Airports
 These are airport related classes.
 
 Atmospheres
 Contains basic data for atmospheres.
 
 Constants
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 Gases
 Common gasesclasses.
 
 Liquids
 Common liquidsclasses.
 
 Planets
 Available planetsclasses.
 
 Propellants
 Common propellantsclasses.
 
-

Detailed Description

-

Attributes provide objects that can be attached to various analyses.

-
-
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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Configs
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This is the component that defines the template for vehicle configurations. -More...

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class  SUAVE.Components.Configs.Config.Config
 
class  SUAVE.Components.Configs.Config.Container
 
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Detailed Description

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This is the component that defines the template for vehicle configurations.

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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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Cost component. -More...

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class  SUAVE.Components.Costs.Costs.Operating_Costs
 
class  SUAVE.Components.Costs.Costs.Industrial_Costs
 
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Detailed Description

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Cost component.

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Converters
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] ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Components-Energy-Distributors.html b/_site/doxygen/group__Components-Energy-Distributors.html deleted file mode 100644 index 68177594..00000000 --- a/_site/doxygen/group__Components-Energy-Distributors.html +++ /dev/null @@ -1,124 +0,0 @@ - - - - - - - -SUAVE: Distributors - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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Distributors
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Components that move energy/control energy/power in a network. -More...

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class  SUAVE.Components.Energy.Distributors.Electronic_Speed_Controller.Electronic_Speed_Controller
 
class  SUAVE.Components.Energy.Distributors.Solar_Logic.Solar_Logic
 
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Detailed Description

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Components that move energy/control energy/power in a network.

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Variable_Mass
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-
- -

Contains different battery types that don't change mass, such as lithium-air and aluminum-air batteries. -More...

- - - - - - -

-Classes

class  SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Aluminum_Air.Aluminum_Air
 
class  SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Lithium_Air.Lithium_Air
 
-

Detailed Description

-

Contains different battery types that don't change mass, such as lithium-air and aluminum-air batteries.

-
-
- - - - diff --git a/_site/doxygen/group__Components-Energy-Storages-Batteries-Variable__Mass.js b/_site/doxygen/group__Components-Energy-Storages-Batteries-Variable__Mass.js deleted file mode 100644 index fa1e0271..00000000 --- a/_site/doxygen/group__Components-Energy-Storages-Batteries-Variable__Mass.js +++ /dev/null @@ -1,19 +0,0 @@ -var group__Components_Energy_Storages_Batteries_Variable__Mass = -[ - [ "Aluminum_Air", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Variable__Mass_1_1Aluminum__Air_1_1Aluminum__Air.html", [ - [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Variable__Mass_1_1Aluminum__Air_1_1Aluminum__Air.html#a67b26c73d23d3a45a85d210f1e7787c7", null ], - [ "find_aluminum_mass", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Variable__Mass_1_1Aluminum__Air_1_1Aluminum__Air.html#a75a314d72d1a267e9dc68156b80154fb", null ], - [ "find_water_mass", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Variable__Mass_1_1Aluminum__Air_1_1Aluminum__Air.html#ab9dc2fcecd7cf01ab408169816a739e7", null ], - [ "aluminum_mass_factor", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Variable__Mass_1_1Aluminum__Air_1_1Aluminum__Air.html#a1db53177baf8ba8774eb3272342ce7da", null ], - [ "mass_gain_factor", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Variable__Mass_1_1Aluminum__Air_1_1Aluminum__Air.html#aa5bcfff381331da45e98ebdbf5423dae", null ], - [ "specific_energy", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Variable__Mass_1_1Aluminum__Air_1_1Aluminum__Air.html#a67a1687b9151ffa4a6e1ad7c88a782fb", null ], - [ "specific_power", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Variable__Mass_1_1Aluminum__Air_1_1Aluminum__Air.html#a79f580d6edc454032aadfb11c9437383", null ], - [ "water_mass_gain_factor", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Variable__Mass_1_1Aluminum__Air_1_1Aluminum__Air.html#ac720e8d3593bf98d16606c9e33058d4f", null ] - ] ], - [ "Lithium_Air", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Variable__Mass_1_1Lithium__Air_1_1Lithium__Air.html", [ - [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Variable__Mass_1_1Lithium__Air_1_1Lithium__Air.html#a9e54953c1f3e45bf2d88d7b68535b541", null ], - [ "mass_gain_factor", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Variable__Mass_1_1Lithium__Air_1_1Lithium__Air.html#a6c703c31f3458e7c1df82605ddc0ff84", null ], - [ "specific_energy", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Variable__Mass_1_1Lithium__Air_1_1Lithium__Air.html#a72d675e0c2636493880c5355bc4de756", null ], - [ "specific_power", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Variable__Mass_1_1Lithium__Air_1_1Lithium__Air.html#a20bb563e6dc09928533965efa295385c", null ] - ] ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Components-Energy-Storages-Batteries.html b/_site/doxygen/group__Components-Energy-Storages-Batteries.html deleted file mode 100644 index a8d9dd9f..00000000 --- a/_site/doxygen/group__Components-Energy-Storages-Batteries.html +++ /dev/null @@ -1,132 +0,0 @@ - - - - - - - -SUAVE: Batteries - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
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-
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Batteries
-
-
- -

Contains different battery types, separated into variable mass (metal-air) and constant mass batteries. -More...

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-Modules

 Constant_Mass
 Contains different battery types that don't change mass, such as lithium-ion and lithium-sulfur batteries.
 
 Variable_Mass
 Contains different battery types that don't change mass, such as lithium-air and aluminum-air batteries.
 
- - - -

-Classes

class  SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
 
-

Detailed Description

-

Contains different battery types, separated into variable mass (metal-air) and constant mass batteries.

-
-
- - - - diff --git a/_site/doxygen/group__Components-Energy-Storages-Batteries.js b/_site/doxygen/group__Components-Energy-Storages-Batteries.js deleted file mode 100644 index bd3902f2..00000000 --- a/_site/doxygen/group__Components-Energy-Storages-Batteries.js +++ /dev/null @@ -1,17 +0,0 @@ -var group__Components_Energy_Storages_Batteries = -[ - [ "Constant_Mass", "group__Components-Energy-Storages-Batteries-Constant__Mass.html", "group__Components-Energy-Storages-Batteries-Constant__Mass" ], - [ "Variable_Mass", "group__Components-Energy-Storages-Batteries-Variable__Mass.html", "group__Components-Energy-Storages-Batteries-Variable__Mass" ], - [ "Battery", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.html", [ - [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.html#a529cffa04fba4664bd432349f14fe268", null ], - [ "energy_calc", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.html#aa65c7a1b8d7ff1b54685851fb8d8f2cd", null ], - [ "current_energy", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.html#ab75d672bb965c5aec6968c38e1fec34e", null ], - [ "discharge_model", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.html#ac1e376177175252082d5b465a7915f7a", null ], - [ "energy_density", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.html#af6ab54f2a19d11ce4b6362a21610c96c", null ], - [ "max_energy", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.html#a26fea5041ae1d5bb54a6a816420191a8", null ], - [ "max_power", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.html#a216ae6ac99fb528716599d14c64a1888", null ], - [ "max_voltage", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.html#af34d6af1003c3d903a9eef49f1a7f368", null ], - [ "ragone", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.html#acfe3bfad30bd53b5c4608a7660606832", null ], - [ "resistance", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.html#a53d46e3ffe1570d23a4423005dd608a9", null ] - ] ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Components-Energy-Storages.html b/_site/doxygen/group__Components-Energy-Storages.html deleted file mode 100644 index 06883e2d..00000000 --- a/_site/doxygen/group__Components-Energy-Storages.html +++ /dev/null @@ -1,123 +0,0 @@ - - - - - - - -SUAVE: Storages - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
-
- - - -
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- -
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Storages
-
-
- -

Energy components that store energy (such as batteries) -More...

- - - - - -

-Modules

 Batteries
 Contains different battery types, separated into variable mass (metal-air) and constant mass batteries.
 
-

Detailed Description

-

Energy components that store energy (such as batteries)

-
-
- - - - diff --git a/_site/doxygen/group__Components-Energy-Storages.js b/_site/doxygen/group__Components-Energy-Storages.js deleted file mode 100644 index 8a91c41f..00000000 --- a/_site/doxygen/group__Components-Energy-Storages.js +++ /dev/null @@ -1,4 +0,0 @@ -var group__Components_Energy_Storages = -[ - [ "Batteries", "group__Components-Energy-Storages-Batteries.html", "group__Components-Energy-Storages-Batteries" ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Components-Energy.html b/_site/doxygen/group__Components-Energy.html deleted file mode 100644 index cf9c3b94..00000000 --- a/_site/doxygen/group__Components-Energy.html +++ /dev/null @@ -1,139 +0,0 @@ - - - - - - - -SUAVE: Energy - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
-
- - - -
-
- -
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- -
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- -
- -
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- -

Components used in energy networks. -More...

- - - - - - - - - - - - - - - - - - - - -

-Modules

 Converters
 Energy components meant to be used within an energy network.
 
 Distributors
 Components that move energy/control energy/power in a network.
 
 Networks
 Components used in energy networks.
 
 Peripherals
 These are components that use energy but are otherwise not part of a network.
 
 Processes
 These are components that use energy to perform a process.
 
 Storages
 Energy components that store energy (such as batteries)
 
-

Detailed Description

-

Components used in energy networks.

-

The classes representing these components typically contain input and output data as part of the class structure.

-
-
- - - - diff --git a/_site/doxygen/group__Components-Energy.js b/_site/doxygen/group__Components-Energy.js deleted file mode 100644 index a873683e..00000000 --- a/_site/doxygen/group__Components-Energy.js +++ /dev/null @@ -1,9 +0,0 @@ -var group__Components_Energy = -[ - [ "Converters", "group__Components-Energy-Converters.html", "group__Components-Energy-Converters" ], - [ "Distributors", "group__Components-Energy-Distributors.html", "group__Components-Energy-Distributors" ], - [ "Networks", "group__Components-Energy-Networks.html", "group__Components-Energy-Networks" ], - [ "Peripherals", "group__Components-Energy-Peripherals.html", "group__Components-Energy-Peripherals" ], - [ "Processes", "group__Components-Energy-Processes.html", "group__Components-Energy-Processes" ], - [ "Storages", "group__Components-Energy-Storages.html", "group__Components-Energy-Storages" ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Components-Payloads.html b/_site/doxygen/group__Components-Payloads.html deleted file mode 100644 index 40972a19..00000000 --- a/_site/doxygen/group__Components-Payloads.html +++ /dev/null @@ -1,132 +0,0 @@ - - - - - - - -SUAVE: Payloads - - - - - - - - - - - - - - - -
-
- - - - - - - - -
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SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
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Payloads
-
-
- -

Available payload componentsinit.py. -More...

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-Classes

class  SUAVE.Components.Payloads.Cargo.Cargo
 
class  SUAVE.Components.Payloads.Payload.Payload
 
class  SUAVE.Components.Payloads.Payload.Container
 
class  SUAVE.Components.Payloads.Person.Person
 
class  SUAVE.Components.Payloads.Satellite.Satellite
 
-

Detailed Description

-

Available payload components

-

init.py.

-

Created: Modified: Feb 2016, T. MacDonald

-
-
- - - - diff --git a/_site/doxygen/group__Components-Payloads.js b/_site/doxygen/group__Components-Payloads.js deleted file mode 100644 index 34bb390a..00000000 --- a/_site/doxygen/group__Components-Payloads.js +++ /dev/null @@ -1,20 +0,0 @@ -var group__Components_Payloads = -[ - [ "Cargo", "classSUAVE_1_1Components_1_1Payloads_1_1Cargo_1_1Cargo.html", [ - [ "__defaults__", "classSUAVE_1_1Components_1_1Payloads_1_1Cargo_1_1Cargo.html#a4f97de17ea1ae1c4e6e68e3a6307952e", null ], - [ "tag", "classSUAVE_1_1Components_1_1Payloads_1_1Cargo_1_1Cargo.html#a0113edcfd4ad704eed565e3201d5a5fb", null ] - ] ], - [ "Payload", "classSUAVE_1_1Components_1_1Payloads_1_1Payload_1_1Payload.html", [ - [ "__defaults__", "classSUAVE_1_1Components_1_1Payloads_1_1Payload_1_1Payload.html#a8ab675e813585c3036cfeffcbd976f33", null ], - [ "tag", "classSUAVE_1_1Components_1_1Payloads_1_1Payload_1_1Payload.html#aa90c294700820fd00984a65f0da3417a", null ] - ] ], - [ "Container", "classSUAVE_1_1Components_1_1Payloads_1_1Payload_1_1Container.html", null ], - [ "Person", "classSUAVE_1_1Components_1_1Payloads_1_1Person_1_1Person.html", [ - [ "__defaults__", "classSUAVE_1_1Components_1_1Payloads_1_1Person_1_1Person.html#a057b4069cf1182ae815f9ac23828a483", null ], - [ "tag", "classSUAVE_1_1Components_1_1Payloads_1_1Person_1_1Person.html#a8a256ceea2c9695987a0760609a2fd3a", null ] - ] ], - [ "Satellite", "classSUAVE_1_1Components_1_1Payloads_1_1Satellite_1_1Satellite.html", [ - [ "__defaults__", "classSUAVE_1_1Components_1_1Payloads_1_1Satellite_1_1Satellite.html#a0dd0be04f50f34e19e8c5130a4d38956", null ], - [ "tag", "classSUAVE_1_1Components_1_1Payloads_1_1Satellite_1_1Satellite.html#a11c080c0b8112d73fe2eb41668bf5809", null ] - ] ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Components-Propulsors.html b/_site/doxygen/group__Components-Propulsors.html deleted file mode 100644 index b5c27bfb..00000000 --- a/_site/doxygen/group__Components-Propulsors.html +++ /dev/null @@ -1,124 +0,0 @@ - - - - - - - -SUAVE: Propulsors - - - - - - - - - - - - - - - -
-
- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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Propulsors
-
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- -

These are the components used to provide thrust to a vehicle. -More...

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-Classes

class  SUAVE.Components.Propulsors.Propulsor.Propulsor
 
class  SUAVE.Components.Propulsors.Propulsor.Container
 
-

Detailed Description

-

These are the components used to provide thrust to a vehicle.

-
-
- - - - diff --git a/_site/doxygen/group__Components-Propulsors.js b/_site/doxygen/group__Components-Propulsors.js deleted file mode 100644 index 82e6f1cf..00000000 --- a/_site/doxygen/group__Components-Propulsors.js +++ /dev/null @@ -1,10 +0,0 @@ -var group__Components_Propulsors = -[ - [ "Propulsor", "classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Propulsor.html", [ - [ "__defaults__", "classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Propulsor.html#a1a13b12fb63990dcd51c6ecc46c83f21", null ], - [ "tag", "classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Propulsor.html#a297d16d03533b9da160be9d970073588", null ] - ] ], - [ "Container", "classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Container.html", [ - [ "evaluate_thrust", "classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Container.html#a42e24eef8ee7108c8f99379060824724", null ] - ] ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Components-Systems.html b/_site/doxygen/group__Components-Systems.html deleted file mode 100644 index 493377dd..00000000 --- a/_site/doxygen/group__Components-Systems.html +++ /dev/null @@ -1,124 +0,0 @@ - - - - - - - -SUAVE: Systems - - - - - - - - - - - - - - - -
-
- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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Systems
-
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- -

These are the components which define a vehicle's onboard systems. -More...

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-Classes

class  SUAVE.Components.Systems.System.System
 
class  SUAVE.Components.Systems.System.Container
 
-

Detailed Description

-

These are the components which define a vehicle's onboard systems.

-
-
- - - - diff --git a/_site/doxygen/group__Components-Systems.js b/_site/doxygen/group__Components-Systems.js deleted file mode 100644 index e0858ea5..00000000 --- a/_site/doxygen/group__Components-Systems.js +++ /dev/null @@ -1,12 +0,0 @@ -var group__Components_Systems = -[ - [ "System", "classSUAVE_1_1Components_1_1Systems_1_1System_1_1System.html", [ - [ "__defaults__", "classSUAVE_1_1Components_1_1Systems_1_1System_1_1System.html#afc1811095781c3b874ab279c8449b53a", null ], - [ "accessories", "classSUAVE_1_1Components_1_1Systems_1_1System_1_1System.html#a22ad3a5dc4d33c9c53a2d01897173e99", null ], - [ "control", "classSUAVE_1_1Components_1_1Systems_1_1System_1_1System.html#adb487ae49fd4892c42ef0cd2ffdd9530", null ], - [ "mass_properties", "classSUAVE_1_1Components_1_1Systems_1_1System_1_1System.html#ac257d2d78c0da7c92ddd9cf16256bfe5", null ], - [ "position", "classSUAVE_1_1Components_1_1Systems_1_1System_1_1System.html#ae3836f93b6ac5c6bab29ec4074b8ff38", null ], - [ "tag", "classSUAVE_1_1Components_1_1Systems_1_1System_1_1System.html#a4fa86faee2bbe57bbd444c14417e1e76", null ] - ] ], - [ "Container", "classSUAVE_1_1Components_1_1Systems_1_1System_1_1Container.html", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Components-Wings-Airfoils.html b/_site/doxygen/group__Components-Wings-Airfoils.html deleted file mode 100644 index 50a77681..00000000 --- a/_site/doxygen/group__Components-Wings-Airfoils.html +++ /dev/null @@ -1,174 +0,0 @@ - - - - - - - -SUAVE: Airfoils - - - - - - - - - - - - - - - -
-
- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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Airfoils
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init.py -More...

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class  SUAVE.Components.Wings.Airfoils.Airfoil.Airfoil
 
- - - -

-Functions

def SUAVE.Components.Wings.Airfoils.load_airfoils.load_airfoils (directory, extension='.dat')
 
-

Detailed Description

-

init.py

-

Created: Modified: Feb 2016, T. MacDonald

-

Function Documentation

- -

◆ load_airfoils()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Components.Wings.Airfoils.load_airfoils.load_airfoils ( directory,
 extension = '.dat' 
)
-
-
Loads airfoil cooridinate points from .dat file
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
-
-
-
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-
- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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Components
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Components are classes that represent objects that are put together to form a vehicle. -More...

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-Modules

 Configs
 This is the component that defines the template for vehicle configurations.
 
 Costs
 Cost component.
 
 Energy
 Components used in energy networks.
 
 Fuselages
 Components traditionally considered to be the fuselage of a vehicle.
 
 Landing Gear
 Components considered are the Main and Nose Landing Gear.
 
 Payloads
 Available payload componentsinit.py.
 
 Propulsors
 These are the components used to provide thrust to a vehicle.
 
 Systems
 These are the components which define a vehicle's onboard systems.
 
 Wings
 init.py
 
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-Classes

class  SUAVE.Components.Component.Component
 
class  SUAVE.Components.Component.Container
 
class  SUAVE.Components.Envelope.Envelope
 
class  SUAVE.Components.Lofted_Body.Lofted_Body
 
class  SUAVE.Components.Lofted_Body.Segment
 
class  SUAVE.Components.Lofted_Body.Section
 
class  SUAVE.Components.Lofted_Body.Curve
 
class  SUAVE.Components.Lofted_Body.SectionContainer
 
class  SUAVE.Components.Lofted_Body.CurveContainer
 
class  SUAVE.Components.Mass_Properties.Mass_Properties
 
class  SUAVE.Components.Physical_Component.Physical_Component
 
class  SUAVE.Components.Physical_Component.Container
 
-

Detailed Description

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Components are classes that represent objects that are put together to form a vehicle.

-

They contain default variables and may contain functions that operate on these variables.

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- - - - - - -SUAVE: Core - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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Core
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- -

Core is all the under the hood magic that makes SUAVE work. -More...

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-Classes

class  SUAVE.Core.Container.Container
 
class  SUAVE.Core.Data.Data
 
class  SUAVE.Core.DataOrdered.DataOrdered
 
class  SUAVE.Core.Diffed_Data.Diffed_Data
 
class  SUAVE.Core.redirect.output
 
class  SUAVE.Core.redirect.folder
 
- - - - - - - - - - - -

-Functions

def SUAVE.Core.Arrays.atleast_2d_col (A)
 
def SUAVE.Core.Arrays.atleast_2d_row (A)
 
def SUAVE.Core.Arrays.atleast_2d (A, oned_as='row')
 
def SUAVE.Core.Units.__rmul__ (self, other)
 
def SUAVE.Core.Units.__rdiv__ (self, other)
 
-

Detailed Description

-

Core is all the under the hood magic that makes SUAVE work.

-

Function Documentation

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◆ __rdiv__()

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def SUAVE.Core.Units.__rdiv__ ( self,
 other 
)
-
-
Override the basic python division for Units
-
-    Assumptions:
-    N/A
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-    Source:
-    N/A
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-    Inputs:
-    Other
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-    Outputs:
-    Converted from Base Units!
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-    Properties Used:
-    N/A    
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◆ __rmul__()

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def SUAVE.Core.Units.__rmul__ ( self,
 other 
)
-
-
Override the basic python multiplication for Units
-
-    Assumptions:
-    N/A
-
-    Source:
-    N/A
-
-    Inputs:
-    Other
-
-    Outputs:
-    Converted into Base Units!
-
-    Properties Used:
-    N/A    
-
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- -

◆ atleast_2d()

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def SUAVE.Core.Arrays.atleast_2d ( A,
 oned_as = 'row' 
)
-
-
ensures A is an array and at least of rank 2
-
-Assumptions:
-Defaults as row
-
-Source:
-N/A
-
-Inputs:
-A      [1-D Array]
-
-Outputs:
-A      [2-D Array]
-
-Properties Used:
-N/A
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◆ atleast_2d_col()

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def SUAVE.Core.Arrays.atleast_2d_col ( A)
-
-
Makes a 2D array in column format
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-A      [1-D Array]
-
-Outputs:
-A      [2-D Array]
-
-Properties Used:
-N/A
-
-
-
- -

◆ atleast_2d_row()

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def SUAVE.Core.Arrays.atleast_2d_row ( A)
-
-
Makes a 2D array in row format
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-A      [1-D Array]
-
-Outputs:
-A      [2-D Array]
-
-Properties Used:
-N/A
-
-
-
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-
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- - - - - - -SUAVE: D3JS - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
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- -
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- -

Files to handle D3JS output. -More...

- - - - -

-Classes

class  SUAVE.Input_Output.D3JS.Tree_Element.Tree_Element
 
- - - - - -

-Functions

def SUAVE.Input_Output.D3JS.save_tree.save_tree (data, filename, root_name=None)
 
def SUAVE.Input_Output.D3JS.save_tree.to_d3 (tree, data)
 
-

Detailed Description

-

Files to handle D3JS output.

-

Function Documentation

- -

◆ save_tree()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Input_Output.D3JS.save_tree.save_tree ( data,
 filename,
 root_name = None 
)
-
-
This creates a D3JS file based on a SUAVE data structure.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-data       SUAVE data structure
-filename   <string> name of the output file
-root_name  (optional) root name for the data structure in the output, default is data.tag
-
-Outputs:
-D3JS file with name as specified by filename
-
-Properties Used:
-N/A
-
-
-
- -

◆ to_d3()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Input_Output.D3JS.save_tree.to_d3 ( tree,
 data 
)
-
-
This puts data for a SUAVE data structure into the needed format for D3JS
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-tree     upper level data structure
-data     SUAVE data structure
-
-Outputs:
-None - modifies tree
-
-Properties Used:
-N/A
-
-
-
-
-
- - - - diff --git a/_site/doxygen/group__Input__Output-D3JS.js b/_site/doxygen/group__Input__Output-D3JS.js deleted file mode 100644 index cc177393..00000000 --- a/_site/doxygen/group__Input__Output-D3JS.js +++ /dev/null @@ -1,11 +0,0 @@ -var group__Input__Output_D3JS = -[ - [ "Tree_Element", "classSUAVE_1_1Input__Output_1_1D3JS_1_1Tree__Element_1_1Tree__Element.html", [ - [ "__init__", "classSUAVE_1_1Input__Output_1_1D3JS_1_1Tree__Element_1_1Tree__Element.html#aa5f6d142e31e3aac7c040e0dac3b09e5", null ], - [ "append", "classSUAVE_1_1Input__Output_1_1D3JS_1_1Tree__Element_1_1Tree__Element.html#a1dd154f0ca79a9c5ee280021d48777b7", null ], - [ "children", "classSUAVE_1_1Input__Output_1_1D3JS_1_1Tree__Element_1_1Tree__Element.html#a1db41112fe73b652f98ab4918a8a9c04", null ], - [ "name", "classSUAVE_1_1Input__Output_1_1D3JS_1_1Tree__Element_1_1Tree__Element.html#a754e229777651f5aab5f3b3a797d386e", null ] - ] ], - [ "save_tree", "group__Input__Output-D3JS.html#gaa0e7d36fab0664e9d57a4d52548e51a9", null ], - [ "to_d3", "group__Input__Output-D3JS.html#ga9bc8f9958b66a34948ab0e91b0c0f34b", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Input__Output-FreeMind.html b/_site/doxygen/group__Input__Output-FreeMind.html deleted file mode 100644 index a6162d06..00000000 --- a/_site/doxygen/group__Input__Output-FreeMind.html +++ /dev/null @@ -1,215 +0,0 @@ - - - - - - - -SUAVE: FreeMind - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
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FreeMind
-
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Function to save FreeMind output. -More...

- - - - - - -

-Functions

def SUAVE.Input_Output.FreeMind.save.save (data, filename)
 
def SUAVE.Input_Output.FreeMind.save.new_fm_node (node, text)
 
-

Detailed Description

-

Function to save FreeMind output.

-

Function Documentation

- -

◆ new_fm_node()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Input_Output.FreeMind.save.new_fm_node ( node,
 text 
)
-
-
This creates a FreeMind node.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-node    The node to be modified
-text    <string> The text to be added
-
-Outputs:
-node    The modified node
-
-Properties Used:
-N/A
-
-
-
- -

◆ save()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Input_Output.FreeMind.save.save ( data,
 filename 
)
-
-
This creates a FreeMind file based on a SUAVE data structure.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-data       SUAVE data structure
-filename   <string> name of the output file
-
-Outputs:
-FreeMind file with name as specified by filename
-
-Properties Used:
-N/A
-
-
-
-
-
- - - - diff --git a/_site/doxygen/group__Input__Output-FreeMind.js b/_site/doxygen/group__Input__Output-FreeMind.js deleted file mode 100644 index 8070b61e..00000000 --- a/_site/doxygen/group__Input__Output-FreeMind.js +++ /dev/null @@ -1,5 +0,0 @@ -var group__Input__Output_FreeMind = -[ - [ "new_fm_node", "group__Input__Output-FreeMind.html#gaf43ad7381411b769d5f77845db310576", null ], - [ "save", "group__Input__Output-FreeMind.html#gac4e5a1949a337e8c1061ed2745547bf8", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Input__Output-GMSH.html b/_site/doxygen/group__Input__Output-GMSH.html deleted file mode 100644 index b99d4b7d..00000000 --- a/_site/doxygen/group__Input__Output-GMSH.html +++ /dev/null @@ -1,235 +0,0 @@ - - - - - - - -SUAVE: GMSH - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
-
- - - -
-
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- - -
-
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Functions needed to work with GMSH. -More...

- - - - - - - - -

-Functions

def SUAVE.Input_Output.GMSH.mesh_geo_file.mesh_geo_file (tag)
 
def SUAVE.Input_Output.GMSH.write_geo_file.write_geo_file (tag)
 
def SUAVE.Input_Output.GMSH.write_geo_file.read_keys (tag)
 
-

Detailed Description

-

Functions needed to work with GMSH.

-

GMSH is an open-source meshing tool.

-

Function Documentation

- -

◆ mesh_geo_file()

- -
-
- - - - - - - - -
def SUAVE.Input_Output.GMSH.mesh_geo_file.mesh_geo_file ( tag)
-
-
This calls GMSH to create a volume mesh based on a previously created .geo file.
-The volume mesh can be read by SU2.
-
-Assumptions:
-.geo file created with write_geo_file function in this folder
-
-Source:
-N/A
-
-Inputs:
-tag        <string>  This corresponds to a configuration from SUAVE
-
-Outputs:
-<tag>.su2  This is a mesh file in SU2 format
-
-Properties Used:
-N/A
-
-
-
- -

◆ read_keys()

- -
-
- - - - - - - - -
def SUAVE.Input_Output.GMSH.write_geo_file.read_keys ( tag)
-
-
This reads the corresponding OpenVSP .key file to check which surfaces
-exist in the .stl file for the vehicle.
-
-Assumptions:
-N/A
-
-Source:
-N/A
-
-Inputs:
-tag          <string>  This corresponds to a configuration from SUAVE
-
-Outputs:
-vehicle_nums [-] the numbers corresponding to surfaces on the vehicle
-farfield_num [-] the number corresponding to the farfield, -1 if not available
-symmetry_num [-] the number corresponding to the symmetry plane, -1 if not available
-
-Properties Used:
-N/A
-
-
-
- -

◆ write_geo_file()

- -
-
- - - - - - - - -
def SUAVE.Input_Output.GMSH.write_geo_file.write_geo_file ( tag)
-
-
This reads an .stl file output from OpenVSP using the SUAVE interface and builds
-a .geo file that can be read to GMSH to produce a volume mesh.
-
-Assumptions:
-The OpenVSP .stl has a farfield surface
-
-Source:
-N/A
-
-Inputs:
-tag        <string>  This corresponds to a configuration from SUAVE
-
-Outputs:
-<tag>.geo
-
-Properties Used:
-N/A
-
-
-
-
-
- - - - diff --git a/_site/doxygen/group__Input__Output-GMSH.js b/_site/doxygen/group__Input__Output-GMSH.js deleted file mode 100644 index 8d90b450..00000000 --- a/_site/doxygen/group__Input__Output-GMSH.js +++ /dev/null @@ -1,6 +0,0 @@ -var group__Input__Output_GMSH = -[ - [ "mesh_geo_file", "group__Input__Output-GMSH.html#ga722552e63f29eff42eb73450392c99b8", null ], - [ "read_keys", "group__Input__Output-GMSH.html#gaa484f4d146a301568057e11512616e75", null ], - [ "write_geo_file", "group__Input__Output-GMSH.html#gadc73c8bff11857535a1863ff21e9c96f", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Input__Output-OpenVSP.html b/_site/doxygen/group__Input__Output-OpenVSP.html deleted file mode 100644 index b667c7b8..00000000 --- a/_site/doxygen/group__Input__Output-OpenVSP.html +++ /dev/null @@ -1,469 +0,0 @@ - - - - - - - -SUAVE: OpenVSP - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
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-
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Functions needed to work with OpenVSP. -More...

- - - - - - - - - - - - -

-Functions

def SUAVE.Input_Output.OpenVSP.get_vsp_areas.get_vsp_areas (tag)
 
def SUAVE.Input_Output.OpenVSP.vsp_write.write (vehicle, tag)
 
def SUAVE.Input_Output.OpenVSP.write_vsp_mesh.write_vsp_mesh (geometry, tag, half_mesh_flag, growth_ratio, growth_limiting_flag)
 
def SUAVE.Input_Output.OpenVSP.write_vsp_mesh.set_sources (geometry)
 
def SUAVE.Input_Output.OpenVSP.write_vsp_mesh.add_segment_sources (comp, cr, ct, ii, u_start, num_secs, custom_flag, wingtip_flag, seg)
 
-

Detailed Description

-

Functions needed to work with OpenVSP.

-

Function Documentation

- -

◆ add_segment_sources()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Input_Output.OpenVSP.write_vsp_mesh.add_segment_sources ( comp,
 cr,
 ct,
 ii,
 u_start,
 num_secs,
 custom_flag,
 wingtip_flag,
 seg 
)
-
-
This sets meshing sources for the wing segments according to their size and position.
-
-Assumptions:
-None
-
-Source:
-https://github.com/OpenVSP/OpenVSP (with some modifications)
-
-Inputs:
-comp             <string> - OpenVSP component ID
-cr               [m]      - root chord
-ct               [m]      - tip chord
-ii               [-]      - segment index
-u_start          [-]      - OpenVSP parameter determining the u dimensional start point
-num_secs         [-]      - number of segments on the corresponding wing
-custom_flag      <boolean> - determines if custom source settings are to be used
-wingtip_flag     <boolean> - indicates if the current segment is a wingtip
-seg.vsp_mesh.    (only used if custom_flag is True)
-  inner_length   [m]       - length of inboard element edge
-  outer_length   [m]       - length of outboard element edge
-  inner_radius   [m]       - radius of influence for inboard source
-  outer_radius   [m]       - radius of influence for outboard source
-
-Outputs:
-None - sources are added to OpenVSP instance                             
-
-Properties Used:
-N/A
-
-
-
- -

◆ get_vsp_areas()

- -
-
- - - - - - - - -
def SUAVE.Input_Output.OpenVSP.get_vsp_areas.get_vsp_areas ( tag)
-
-
This calls OpenVSP to compute the wetted areas of a previously written vehicle.
-
-Assumptions:
-Vehicle must be open in OpenVSP (via recently used vsp_write)
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-wetted_areas   [m^2] - Dictionary with wetted areas for each component, with component tags as the keys.
-
-Properties Used:
-N/A
-
-
-
- -

◆ set_sources()

- -
-
- - - - - - - - -
def SUAVE.Input_Output.OpenVSP.write_vsp_mesh.set_sources ( geometry)
-
-
This sets meshing sources in a way similar to the OpenVSP default. Some source values can
-also be optionally specified as below.
-
-Assumptions:
-None
-
-Source:
-https://github.com/OpenVSP/OpenVSP (with some modifications)
-
-Inputs:
-geometry.
-  wings.*.                              (passed to add_segment_sources())
-    tag                                 <string>
-    Segments.*.percent_span_location    [-] (.1 is 10%)
-    Segments.*.root_chord_percent       [-] (.1 is 10%)
-    chords.root                         [m]
-    chords.tip                          [m]
-    vsp_mesh                            (optional) - This holds settings that are used in add_segment_sources
-  fuselages.*.
-    tag                                 <string>
-    vsp_mesh.                           (optional)
-      length                            [m]
-      radius                            [m]
-    lengths.total                       (only used if vsp_mesh is not defined for the fuselage)
-
-Outputs:
-<tag>.stl                               
-
-Properties Used:
-N/A
-
-
-
- -

◆ write()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Input_Output.OpenVSP.vsp_write.write ( vehicle,
 tag 
)
-
-
This writes a SUAVE vehicle to OpenVSP format. It will take wing segments into account
-if they are specified in the vehicle setup file.
-
-Assumptions:
-Vehicle is composed of conventional shape fuselages, wings, and propulsors. Any propulsor
-that should be created in tagged as 'turbofan'.
-
-Source:
-N/A
-
-Inputs:
-wings.*.    (* is all keys)
-  origin                                  [m] in all three dimensions
-  spans.projected                         [m]
-  chords.root                             [m]
-  chords.tip                              [m]
-  sweeps.quarter_chord                    [radians]
-  twists.root                             [radians]
-  twists.tip                              [radians]
-  thickness_to_chord                      [-]
-  dihedral                                [radians]
-  tag                                     <string>
-  Segments.*. (optional)
-    twist                                 [radians]
-    percent_span_location                 [-]  .1 is 10%
-    root_chord_percent                    [-]  .1 is 10%
-    dihedral_outboard                     [radians]
-    sweeps.quarter_chord                  [radians]
-    thickness_to_chord                    [-]
-propulsors.turbofan. (optional)
-  number_of_engines                       [-]
-  engine_length                           [m]
-  nacelle_diameter                        [m]
-  origin                                  [m] in all three dimension, should have as many origins as engines
-  OpenVSP_simple (optional)               <boolean> if False (default) create a flow through nacelle, if True creates a roughly biparabolic shape
-fuselages.fuselage (optional)
-  width                                   [m]
-  lengths.total                           [m]
-  heights.
-    maximum                               [m]
-    at_quarter_length                     [m]
-    at_wing_root_quarter_chord            [m]
-    at_three_quarters_length              [m]
-  effective_diameter                      [m]
-  fineness.nose                           [-] ratio of nose section length to fuselage width
-  fineness.tail                           [-] ratio of tail section length to fuselage width
-  tag                                     <string>
-  OpenVSP_values.  (optional)
-    nose.top.angle                        [degrees]
-    nose.top.strength                     [-] this determines how much the specified angle influences that shape
-    nose.side.angle                       [degrees]
-    nose.side.strength                    [-]
-    nose.TB_Sym                           <boolean> determines if top angle is mirrored on bottom
-    nose.z_pos                            [-] z position of the nose as a percentage of fuselage length (.1 is 10%)
-    tail.top.angle                        [degrees]
-    tail.top.strength                     [-]
-    tail.z_pos (optional, 0.02 default)   [-] z position of the tail as a percentage of fuselage length (.1 is 10%)
-
-
-Outputs:
-<tag>.vsp3           This is the OpenVSP representation of the aircraft
-
-Properties Used:
-N/A
-
-
-
- -

◆ write_vsp_mesh()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Input_Output.OpenVSP.write_vsp_mesh.write_vsp_mesh ( geometry,
 tag,
 half_mesh_flag,
 growth_ratio,
 growth_limiting_flag 
)
-
-
This create an .stl surface mesh based on a vehicle stored in a .vsp3 file.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-geometry.                                 - Also passed to set_sources
-  wings.main_wing.chords.mean_aerodynamic [m]
-half_mesh_flag                            <boolean>  determines if a symmetry plane is created
-growth_ratio                              [-]        growth ratio for the mesh
-growth_limiting_flag                      <boolean>  determines if 3D growth limiting is used
-
-Outputs:
-<tag>.stl                               
-
-Properties Used:
-N/A
-
-
-
-
-
- - - - diff --git a/_site/doxygen/group__Input__Output-OpenVSP.js b/_site/doxygen/group__Input__Output-OpenVSP.js deleted file mode 100644 index fcb19ec0..00000000 --- a/_site/doxygen/group__Input__Output-OpenVSP.js +++ /dev/null @@ -1,8 +0,0 @@ -var group__Input__Output_OpenVSP = -[ - [ "add_segment_sources", "group__Input__Output-OpenVSP.html#ga16150de691a986c7c5cbcfdc732157db", null ], - [ "get_vsp_areas", "group__Input__Output-OpenVSP.html#gacb89d921dd366956d67db9579ac2d04f", null ], - [ "set_sources", "group__Input__Output-OpenVSP.html#ga3d040856a17af007a55afcf7774c6c5d", null ], - [ "write", "group__Input__Output-OpenVSP.html#ga491b5dce0cfd2be891897829311b1bd5", null ], - [ "write_vsp_mesh", "group__Input__Output-OpenVSP.html#ga6310bb25b22c674e0942d9f616031a26", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Input__Output-Results.html b/_site/doxygen/group__Input__Output-Results.html deleted file mode 100644 index 4286cd59..00000000 --- a/_site/doxygen/group__Input__Output-Results.html +++ /dev/null @@ -1,448 +0,0 @@ - - - - - - - -SUAVE: Results - - - - - - - - - - - - - - - -
-
- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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Miscellaneous functions to print results. -More...

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-Functions

def SUAVE.Input_Output.Results.print_compress_drag.print_compress_drag (vehicle, analyses, filename='compress_drag.dat')
 
def SUAVE.Input_Output.Results.print_engine_data.print_engine_data (vehicle, filename='engine_data.dat', units="imperial")
 
def SUAVE.Input_Output.Results.print_mission_breakdown.print_mission_breakdown (results, filename='mission_breakdown.dat', units="imperial")
 
def SUAVE.Input_Output.Results.print_parasite_drag.print_parasite_drag (ref_condition, vehicle, analyses, filename='parasite_drag.dat')
 
def SUAVE.Input_Output.Results.print_weights.print_weight_breakdown (config, filename='weight_breakdown.dat')
 print_weights.py More...
 
-

Detailed Description

-

Miscellaneous functions to print results.

-

Function Documentation

- -

◆ print_compress_drag()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Input_Output.Results.print_compress_drag.print_compress_drag ( vehicle,
 analyses,
 filename = 'compress_drag.dat' 
)
-
-
This creates a file showing a breakdown of compressibility drag for the vehicle.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-vehicle.wings.main_wing.
-  sweeps.quarter_chord     [-]
-vehicle.wings.*.
-  tag                     <string>
-  thickness_to_chord      [-]
-vehicle.
-  tag                     <string>
-  reference_area          [m^2]
-analyses.configs.cruise.aerodynamics.settings    Used in called function:
-analyses.configs.cruise.aerodynamics.process.compute.drag.compressibility.wings.wing(state,settings,wing)
-filename                  Sets file name to save (optional)
-
-
-Outputs:
-filename                  Saved file with name as above
-
-Properties Used:
-N/A
-
-
-
- -

◆ print_engine_data()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Input_Output.Results.print_engine_data.print_engine_data ( vehicle,
 filename = 'engine_data.dat',
 units = "imperial" 
)
-
-
This creates a file showing engine information.
-
-Assumptions:
-One propulsor (can be multiple engines) with 'turbofan' tag.
-
-Source:
-N/A
-
-Inputs:
-vehicle.
-  tag
-  turbofan()              Function to compute thrust and fuel burn rate
-  propulsors.turbofan.
-    design_thrust         [N]
-    engine_length         [m]
-    nacelle_diameter      [m]
-    thrust.bypass_ratio   [-]
-filename (optional)       <string> Determines the name of the saved file
-units (optional)          <string> Determines the type of units used in the output, options are imperial and si
-
-Outputs:
-filename                  Saved file with name as above
-
-Properties Used:
-N/A
-
-
-
- -

◆ print_mission_breakdown()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Input_Output.Results.print_mission_breakdown.print_mission_breakdown ( results,
 filename = 'mission_breakdown.dat',
 units = "imperial" 
)
-
-
This creates a file showing mission information.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-results.segments.*.conditions.
-  frames.
-    inertial.position_vector     [m]
-    inertial.time                [s]
-  aerodynamics.lift_coefficient  [-]
-  weights.total                  [kg]
-  freestream.  
-    mach_number                  [-]
-    pressure                     [Pa]
-filename (optional)       <string> Determines the name of the saved file
-units (option)            <string> Determines the type of units used in the output, options are imperial and si
-
-Outputs:
-filename                  Saved file with name as above
-
-Properties Used:
-N/A
-
-
-
- -

◆ print_parasite_drag()

- -
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def SUAVE.Input_Output.Results.print_parasite_drag.print_parasite_drag ( ref_condition,
 vehicle,
 analyses,
 filename = 'parasite_drag.dat' 
)
-
-
This creates a file showing a breakdown of compressibility drag for the vehicle. Esimates
-altitude based on reference conditions.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-ref_condition.
-  mach_number
-  reynolds_number
-vehicle.wings.main_wing.
-  chords.mean_aerodynamic
-  aspect_ratio
-  sweeps.quarter_chord     [-]
-  thickness_to_chord
-  taper
-vehicle.wings.*.
-  tag                     <string>
-vehicle.reference_area    [m^2]
-analyses.configs.cruise.aerodynamics.settings    Used in called functions:
-  compute.parasite.wings.wing(state,settings,wing)                (for all wings)
-  compute.parasite.fuselages.fuselage(state,settings,fuselage)    (for all fuselages)
-  compute.parasite.propulsors.propulsor(state,settings,propulsor) (for all propulsors)
-  compute.parasite.pylons(state,settings,vehicle) 
-  compute.miscellaneous(state,settings,vehicle)
-  compute.parasite.total(state,settings,vehicle)
-  compute.induced(state,settings,vehicle)    
-    with compute = analyses.configs.cruise.aerodynamics.process.compute.drag
-filename                  Sets file name to save (optional)
-
-
-Outputs:
-filename                  Saved file with name as above
-
-Properties Used:
-N/A
-
-
-
- -

◆ print_weight_breakdown()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Input_Output.Results.print_weights.print_weight_breakdown ( config,
 filename = 'weight_breakdown.dat' 
)
-
- -

print_weights.py

-
This creates a file showing weight information.
-
-Assumptions:
-One propulsor (can be multiple engines) with 'turbofan' tag.
-
-Source:
-N/A
-
-Inputs:
-config.
-  weight_breakdown.
-    empty
-    *.tag            <string>
-    systems.*.tag    <string>
-  mass_properties.
-    max_takeoff      [kg]
-max_landing      [kg]
-max_zero_fuel    [kg]
-max_fuel         [kg]
-max_payload      [kg]
-filename (optional)  <string> Determines the name of the saved file
-
-Outputs:
-filename              Saved file with name as above
-
-Properties Used:
-N/A
-
-
-
-
-
- - - - diff --git a/_site/doxygen/group__Input__Output-Results.js b/_site/doxygen/group__Input__Output-Results.js deleted file mode 100644 index 0e9eeef6..00000000 --- a/_site/doxygen/group__Input__Output-Results.js +++ /dev/null @@ -1,8 +0,0 @@ -var group__Input__Output_Results = -[ - [ "print_compress_drag", "group__Input__Output-Results.html#gac30a069241ff0dae53534160e6fcbc90", null ], - [ "print_engine_data", "group__Input__Output-Results.html#ga880ccca63140ef4e5e5164bcd8c4369f", null ], - [ "print_mission_breakdown", "group__Input__Output-Results.html#ga136ef61dc415d6b8979e72cdc7431533", null ], - [ "print_parasite_drag", "group__Input__Output-Results.html#gaa252f45d1c331a593f1a5f6831599544", null ], - [ "print_weight_breakdown", "group__Input__Output-Results.html#ga5455b4820972640dcf423077e2d4eb28", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Input__Output-SU2.html b/_site/doxygen/group__Input__Output-SU2.html deleted file mode 100644 index db7bf83c..00000000 --- a/_site/doxygen/group__Input__Output-SU2.html +++ /dev/null @@ -1,231 +0,0 @@ - - - - - - - -SUAVE: SU2 - - - - - - - - - - - - - - - -
-
- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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Functions needed to interface with SU2. -More...

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def SUAVE.Input_Output.SU2.call_SU2_CFD.call_SU2_CFD (tag, parallel=False, processors=1)
 
def SUAVE.Input_Output.SU2.write_SU2_cfg.write_SU2_cfg (tag, SU2_settings)
 write_SU2_cfg.py More...
 
-

Detailed Description

-

Functions needed to interface with SU2.

-

Function Documentation

- -

◆ call_SU2_CFD()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Input_Output.SU2.call_SU2_CFD.call_SU2_CFD ( tag,
 parallel = False,
 processors = 1 
)
-
-
This calls SU2 to perform an analysis according to the related .cfg file.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-tag                          <string>  This determines what .cfg is used and what the output file is called.
-parallel   (optional)        <boolean> This determines if SU2 will be run in parallel. This setting requires that SU2 has been built to allow this.
-processors (optional)        [-]       The number of processors used for a parallel computation.
-
-Outputs:
-<tag>._forces_breakdown.dat  This file has standard SU2 run information.
-CL                           [-]
-CD                           [-]
-
-Properties Used:
-N/A
-
-
-
- -

◆ write_SU2_cfg()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Input_Output.SU2.write_SU2_cfg.write_SU2_cfg ( tag,
 SU2_settings 
)
-
- -

write_SU2_cfg.py

-

Created: Oct 2016, T. MacDonald Modified: Jan 2017, T. MacDonald

Creates an SU2 .cfg file that can be used for an SU2 run.
-
-Assumptions:
-Almost all settings are current hard coded.
-
-Source:
-N/A
-
-Inputs:
-tag                          <string>  This determines the name of the .cfg
-SU2_settings.
-  reference_area            [m^2]
-  mach_number               [-]
-  angle_of_attack           [degrees]
-  maximum_iterations        [-]
-
-Outputs:
-<tag>.cfg
-
-Properties Used:
-N/A
-
-
-
-
-
- - - - diff --git a/_site/doxygen/group__Input__Output-SU2.js b/_site/doxygen/group__Input__Output-SU2.js deleted file mode 100644 index 43a6536d..00000000 --- a/_site/doxygen/group__Input__Output-SU2.js +++ /dev/null @@ -1,5 +0,0 @@ -var group__Input__Output_SU2 = -[ - [ "call_SU2_CFD", "group__Input__Output-SU2.html#ga0fac27fc1c50f2c799af7698a607bd0f", null ], - [ "write_SU2_cfg", "group__Input__Output-SU2.html#ga3498cecf92e392df970ed51cc087f6a6", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Input__Output-SUAVE.html b/_site/doxygen/group__Input__Output-SUAVE.html deleted file mode 100644 index fee2face..00000000 --- a/_site/doxygen/group__Input__Output-SUAVE.html +++ /dev/null @@ -1,351 +0,0 @@ - - - - - - - -SUAVE: SUAVE - - - - - - - - - - - - - - - -
-
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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Functions needed to save SUAVE data structures in JSON form. -More...

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def SUAVE.Input_Output.SUAVE.archive.archive (data, filename)
 
def SUAVE.Input_Output.SUAVE.archive.build_dict_base (base)
 
def SUAVE.Input_Output.SUAVE.archive.build_dict_r (v)
 
def SUAVE.Input_Output.SUAVE.load.load (filename)
 
def SUAVE.Input_Output.SUAVE.load.read_SUAVE_json_dict (res_dict)
 
def SUAVE.Input_Output.SUAVE.load.build_data_r (v)
 
-

Detailed Description

-

Functions needed to save SUAVE data structures in JSON form.

-

Function Documentation

- -

◆ archive()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Input_Output.SUAVE.archive.archive ( data,
 filename 
)
-
-
Converts a SUAVE data structure to a JSON file for storage. 
-
-Assumptions:
-Data must be numpy arrays, strings, booleans, floats, ints, or lists.
-Functions are ignored and all other data raises an error.
-
-Source:
-N/A
-
-Inputs:
-data       SUAVE data structure
-filename   <string> - file to be output
-
-Outputs:
-filename   File as specified in JSON format
-
-Properties Used:
-N/A
-
-
-
- -

◆ build_data_r()

- -
-
- - - - - - - - -
def SUAVE.Input_Output.SUAVE.load.build_data_r ( v)
-
-
Builds a SUAVE data structure based on a dictionary from a JSON file. This is recursive step.
-
-Assumptions:
-Dictionary was created based on a previously saved SUAVE data structure.
-
-Source:
-N/A
-
-Inputs:
-v     generic value
-
-Outputs:
-ret   value converted to needed format
-
-Properties Used:
-N/A
-
-
-
- -

◆ build_dict_base()

- -
-
- - - - - - - - -
def SUAVE.Input_Output.SUAVE.archive.build_dict_base ( base)
-
-
Builds a dictionary based on a SUAVE data structure. This is initial case.
-
-Assumptions:
-Data must be numpy arrays, strings, booleans, floats, ints, or lists.
-Functions are ignored and all other data raises an error.
-
-Source:
-N/A
-
-Inputs:
-data       SUAVE data structure
-
-Outputs:
-base_dict  Dictionary built on the data structure.
-
-Properties Used:
-N/A
-
-
-
- -

◆ build_dict_r()

- -
-
- - - - - - - - -
def SUAVE.Input_Output.SUAVE.archive.build_dict_r ( v)
-
-
Builds a dictionary based on a SUAVE data structure. This the recursive step.
-
-Assumptions:
-Data must be numpy arrays, strings, booleans, floats, ints, or lists.
-Functions are ignored and all other data raises an error.
-
-Source:
-N/A
-
-Inputs:
-v       value in a data structure
-
-Outputs:
-ret     value based on type of v
-
-Properties Used:
-N/A
-
-
-
- -

◆ load()

- -
-
- - - - - - - - -
def SUAVE.Input_Output.SUAVE.load.load ( filename)
-
-
Converts a JSON file into a SUAVE data structure.
-
-Assumptions:
-JSON file was a previously saved SUAVE data structure.
-
-Source:
-N/A
-
-Inputs:
-filename   <string> - file to be loaded
-
-Outputs:
-data       SUAVE data structure
-
-Properties Used:
-N/A
-
-
-
- -

◆ read_SUAVE_json_dict()

- -
-
- - - - - - - - -
def SUAVE.Input_Output.SUAVE.load.read_SUAVE_json_dict ( res_dict)
-
-
Builds a SUAVE data structure based on a dictionary from a JSON file. This is initial case.
-
-Assumptions:
-Dictionary was created based on a previously saved SUAVE data structure.
-
-Source:
-N/A
-
-Inputs:
-res_dict    Dictionary based on the SUAVE data structure
-
-Outputs:
-SUAVE_data  SUAVE data structure
-
-Properties Used:
-N/A
-
-
-
-
-
- - - - diff --git a/_site/doxygen/group__Input__Output-SUAVE.js b/_site/doxygen/group__Input__Output-SUAVE.js deleted file mode 100644 index ef517887..00000000 --- a/_site/doxygen/group__Input__Output-SUAVE.js +++ /dev/null @@ -1,9 +0,0 @@ -var group__Input__Output_SUAVE = -[ - [ "archive", "group__Input__Output-SUAVE.html#gaa157805d609d1c688a0cd1356c2e7d06", null ], - [ "build_data_r", "group__Input__Output-SUAVE.html#ga83836ae9cd07eb3f83bfddb99cedb5bb", null ], - [ "build_dict_base", "group__Input__Output-SUAVE.html#ga434b0ad84d4811df563a1fee054eb88f", null ], - [ "build_dict_r", "group__Input__Output-SUAVE.html#ga3649f6517cdcefde39dc79e47ae499bc", null ], - [ "load", "group__Input__Output-SUAVE.html#gad7d8acfe6d92d6fd5c57ac85b0119d77", null ], - [ "read_SUAVE_json_dict", "group__Input__Output-SUAVE.html#ga61c7ff6f78f784c40163d57c60b370bf", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Input__Output-XML.html b/_site/doxygen/group__Input__Output-XML.html deleted file mode 100644 index 3efa5b0f..00000000 --- a/_site/doxygen/group__Input__Output-XML.html +++ /dev/null @@ -1,262 +0,0 @@ - - - - - - - -SUAVE: XML - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
-
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-Classes

class  SUAVE.Input_Output.XML.Data.Data
 
class  SUAVE.Input_Output.XML.Data.Attributes
 
class  SUAVE.Input_Output.XML.load.TreeBuilder
 
- - - - - - - -

-Functions

def SUAVE.Input_Output.XML.load.load (file_in)
 
def SUAVE.Input_Output.XML.save.save (xml_data, filename)
 
def SUAVE.Input_Output.XML.save.indent (elem, level=0)
 
-

Detailed Description

-

Files to handle XML input and output.

-

These are not directly used with SUAVE data structures but are required for using FreeMind.

-

Function Documentation

- -

◆ indent()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Input_Output.XML.save.indent ( elem,
 level = 0 
)
-
-
Indentation helper.
-
-Assumptions:
-None
-
-Source:
-http://effbot.org/zone/element-lib.htm
-
-Inputs:
-elem             The element to be used
-level (optional) The indentation level
-
-Outputs:
-Modifies elem
-
-Properties Used:
-N/A
-
-
-
- -

◆ load()

- -
-
- - - - - - - - -
def SUAVE.Input_Output.XML.load.load ( file_in)
-
-
Converts an XML file into an XML data structure.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-file_in  - The XML file
-
-Outputs:
-xml_data - The XML data structure
-
-Properties Used:
-N/A
-
-
-
- -

◆ save()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Input_Output.XML.save.save ( xml_data,
 filename 
)
-
-
This creates an XML file based on an XML data structure.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-xml_data   The XML data structure to be saved
-filename   The name of the saved file
-
-Outputs:
-XML file with name as specified by filename
-
-Properties Used:
-N/A
-
-
-
-
-
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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Input_Output
-
-
- -

These functions provide SUAVE data storage capabilities and capabilities to work with files for other programs. -More...

- - - - - - - - - - - - - - - - - - - - - - - - - - -

-Modules

 D3JS
 Files to handle D3JS output.
 
 FreeMind
 Function to save FreeMind output.
 
 GMSH
 Functions needed to work with GMSH.
 
 OpenVSP
 Functions needed to work with OpenVSP.
 
 Results
 Miscellaneous functions to print results.
 
 SU2
 Functions needed to interface with SU2.
 
 SUAVE
 Functions needed to save SUAVE data structures in JSON form.
 
 XML
 Files to handle XML input and output.
 
-

Detailed Description

-

These functions provide SUAVE data storage capabilities and capabilities to work with files for other programs.

-
-
- - - - diff --git a/_site/doxygen/group__Input__Output.js b/_site/doxygen/group__Input__Output.js deleted file mode 100644 index b197ebb2..00000000 --- a/_site/doxygen/group__Input__Output.js +++ /dev/null @@ -1,11 +0,0 @@ -var group__Input__Output = -[ - [ "D3JS", "group__Input__Output-D3JS.html", "group__Input__Output-D3JS" ], - [ "FreeMind", "group__Input__Output-FreeMind.html", "group__Input__Output-FreeMind" ], - [ "GMSH", "group__Input__Output-GMSH.html", "group__Input__Output-GMSH" ], - [ "OpenVSP", "group__Input__Output-OpenVSP.html", "group__Input__Output-OpenVSP" ], - [ "Results", "group__Input__Output-Results.html", "group__Input__Output-Results" ], - [ "SU2", "group__Input__Output-SU2.html", "group__Input__Output-SU2" ], - [ "SUAVE", "group__Input__Output-SUAVE.html", "group__Input__Output-SUAVE" ], - [ "XML", "group__Input__Output-XML.html", "group__Input__Output-XML" ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Methods-Aerodynamics-AERODAS.html b/_site/doxygen/group__Methods-Aerodynamics-AERODAS.html deleted file mode 100644 index 92518c32..00000000 --- a/_site/doxygen/group__Methods-Aerodynamics-AERODAS.html +++ /dev/null @@ -1,534 +0,0 @@ - - - - - - - -SUAVE: AERODAS - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
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-
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Functions to perform calculations according to AERODAS models. -More...

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-Functions

def SUAVE.Methods.Aerodynamics.AERODAS.AERODAS_setup.setup_data (state, settings, geometry)
 
def SUAVE.Methods.Aerodynamics.AERODAS.AERODAS_setup.lift_drag_total (state, settings, geometry)
 
def SUAVE.Methods.Aerodynamics.AERODAS.AERODAS_setup.lift_total (state, settings, geometry)
 
def SUAVE.Methods.Aerodynamics.AERODAS.AERODAS_setup.drag_total (state, settings, geometry)
 
def SUAVE.Methods.Aerodynamics.AERODAS.finite_aspect_ratio.finite_aspect_ratio (state, settings, geometry)
 
def SUAVE.Methods.Aerodynamics.AERODAS.post_stall_coefficients.post_stall_coefficients (state, settings, geometry)
 
def SUAVE.Methods.Aerodynamics.AERODAS.pre_stall_coefficients.pre_stall_coefficients (state, settings, geometry)
 
-

Detailed Description

-

Functions to perform calculations according to AERODAS models.

-

Function Documentation

- -

◆ drag_total()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Aerodynamics.AERODAS.AERODAS_setup.drag_total ( state,
 settings,
 geometry 
)
-
-
Extract the drag coefficient
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-state.conditions.aerodynamics.drag_coefficient [Unitless]
-
-Outputs:
-CD (coefficient of drag)                       [Unitless]
-
-Properties Used:
-N/A
-
-
-
- -

◆ finite_aspect_ratio()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Aerodynamics.AERODAS.finite_aspect_ratio.finite_aspect_ratio ( state,
 settings,
 geometry 
)
-
-
Uses the AERODAS method to prestall parameters for lift and drag.
-
-Assumptions:
-None
-
-Source:
-NASA TR: "Models of Lift and Drag Coefficients of Stalled and Unstalled Airfoils in
-  Wind Turbines and Wind Tunnels" by D. A. Spera
-
-Inputs:
-geometry.
-  aspect_ratio                                [Unitless]
-  section.
-    maximum_coefficient_lift                  [Unitless]
-    angle_attack_max_prestall_lift            [radians]
-    pre_stall_maximum_drag_coefficient_angle  [radians]
-    pre_stall_maximum_drag_coefficient        [Unitless]
-settings.section_lift_curve_slope             [radians]
-
-Outputs:
-pre_stall_maximum_lift_coefficient            [Unitless]
-pre_stall_maximum_lift_drag_coefficient       [Unitless]
-pre_stall_lift_curve_slope                    [radians]
-pre_stall_maximum_drag_coefficient_angle      [Unitless]
-(these are also packed into geometry.)
-
-Properties Used:
-N/A
-
-
-
- -

◆ lift_drag_total()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Aerodynamics.AERODAS.AERODAS_setup.lift_drag_total ( state,
 settings,
 geometry 
)
-
-
This sums lift and drag contributions from all of the wings.
-
-Assumptions:
-None
-
-Source:
-NASA TR: "Models of Lift and Drag Coefficients of Stalled and Unstalled Airfoils in
-  Wind Turbines and Wind Tunnels" by D. A. Spera
-
-Inputs:
-geometry.
-  reference_area                                                      [m^2]
-  wings
-state.conditions.aerodynamics.
-  angle_of_attack                                                     [radians]
-  pre_stall_coefficients[wing.tag].lift_coefficient (for each wing)   [Unitless]
-  pre_stall_coefficients[wing.tag].drag_coefficient (for each wing)   [Unitless]
-  post_stall_coefficients[wing.tag].lift_coefficient (for each wing)  [Unitless]
-  post_stall_coefficients[wing.tag].drag_coefficient (for each wing)  [Unitless]
-settings.section_zero_lift_angle_of_attack                            [radians]
-
-Outputs:
-state.conditions.aerodynamics.
-  lift_coefficient                                                    [Unitless]
-  drag_coefficient                                                    [Unitless]
-
-Properties Used:
-N/A
-
-
-
- -

◆ lift_total()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Aerodynamics.AERODAS.AERODAS_setup.lift_total ( state,
 settings,
 geometry 
)
-
-
Extract the lift coefficient
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-state.conditions.aerodynamics.lift_coefficient [Unitless]
-
-Outputs:
-CL (coefficient of lift)                       [Unitless]
-
-Properties Used:
-N/A
-
-
-
- -

◆ post_stall_coefficients()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Aerodynamics.AERODAS.post_stall_coefficients.post_stall_coefficients ( state,
 settings,
 geometry 
)
-
-
Uses the AERODAS method to determine poststall parameters for lift and drag for a single wing
-
-Assumptions:
-None
-
-Source:
-NASA TR: "Models of Lift and Drag Coefficients of Stalled and Unstalled Airfoils in
-  Wind Turbines and Wind Tunnels" by D. A. Spera
-
-Inputs:
-settings.section_zero_lift_angle_of_attack      [radians]
-geometry.
-  aspect_ratio                                  [Unitless]
-  thickness_to_chord                            [Unitless]
-  section.angle_attack_max_prestall_lift        [radians]
-  pre_stall_maximum_lift_drag_coefficient       [Unitless]
-  pre_stall_maximum_drag_coefficient_angle      [Unitless]
-state.conditions.aerodynamics.angle_of_attack   [radians]
-  
-
-Outputs:
-CL2 (coefficient of lift)                       [Unitless]
-CD2 (coefficient of drag)                       [Unitless]
-(packed in state.conditions.aerodynamics.post_stall_coefficients[geometry.tag])
-
-Properties Used:
-N/A
-
-
-
- -

◆ pre_stall_coefficients()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Aerodynamics.AERODAS.pre_stall_coefficients.pre_stall_coefficients ( state,
 settings,
 geometry 
)
-
-
Uses the AERODAS method to determine prestall parameters for lift and drag for a single wing
-
-Assumptions:
-None
-
-Source:
-NASA TR: "Models of Lift and Drag Coefficients of Stalled and Unstalled Airfoils in
-  Wind Turbines and Wind Tunnels" by D. A. Spera
-
-Inputs:
-state.conditions.aerodynamics.angle_of_attack
-settings.section_zero_lift_angle_of_attack
-geometry.
-  section.
-    angle_attack_max_prestall_lift
-    zero_lift_drag_coefficient
-  pre_stall_maximum_drag_coefficient_angle
-  pre_stall_maximum_lift_coefficient
-  pre_stall_lift_curve_slope 
-  pre_stall_maximum_lift_drag_coefficient
-
-Outputs:
-CL1 (coefficient of lift)                       [Unitless]
-CD1 (coefficient of drag)                       [Unitless]
-(packed in state.conditions.aerodynamics.pre_stall_coefficients[geometry.tag])
-
-Properties Used:
-N/A
-
-
-
- -

◆ setup_data()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Aerodynamics.AERODAS.AERODAS_setup.setup_data ( state,
 settings,
 geometry 
)
-
-
This sets up the data structure for pre and post stall coefficients
-that will be generated by the AERODAS model.
-
-Assumptions:
-None
-
-Source:
-NASA TR: "Models of Lift and Drag Coefficients of Stalled and Unstalled Airfoils in
-  Wind Turbines and Wind Tunnels" by D. A. Spera
-
-Inputs:
-state.conditions.aerodynamics (to be modified)
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
-
-
-
- - - - diff --git a/_site/doxygen/group__Methods-Aerodynamics-AERODAS.js b/_site/doxygen/group__Methods-Aerodynamics-AERODAS.js deleted file mode 100644 index 96c07ff5..00000000 --- a/_site/doxygen/group__Methods-Aerodynamics-AERODAS.js +++ /dev/null @@ -1,10 +0,0 @@ -var group__Methods_Aerodynamics_AERODAS = -[ - [ "drag_total", "group__Methods-Aerodynamics-AERODAS.html#ga49ea8af4f8a59c3a756eac1e498732b2", null ], - [ "finite_aspect_ratio", "group__Methods-Aerodynamics-AERODAS.html#gae7e52dd4b672379f9c0afbe09240bae4", null ], - [ "lift_drag_total", "group__Methods-Aerodynamics-AERODAS.html#ga6032a9f6ae0e3752d9c9bd6a21e3e4a9", null ], - [ "lift_total", "group__Methods-Aerodynamics-AERODAS.html#gaf53aab33266492f2539410472b12c741", null ], - [ "post_stall_coefficients", "group__Methods-Aerodynamics-AERODAS.html#gab68aa24147438640549d3d874e2efb23", null ], - [ "pre_stall_coefficients", "group__Methods-Aerodynamics-AERODAS.html#ga2609e27444a2910b337330e56c3bac1d", null ], - [ "setup_data", "group__Methods-Aerodynamics-AERODAS.html#ga2d66acd2994d49d3f58eb3899a52729a", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Methods-Aerodynamics-AVL-Data.html b/_site/doxygen/group__Methods-Aerodynamics-AVL-Data.html deleted file mode 100644 index 0b570922..00000000 --- a/_site/doxygen/group__Methods-Aerodynamics-AVL-Data.html +++ /dev/null @@ -1,132 +0,0 @@ - - - - - - - -SUAVE: Data - - - - - - - - - - - - - - - -
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- - - - - - -SUAVE: AVL - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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Functions to AVL calculations. -More...

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-Modules

 Data
 
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-Functions

def SUAVE.Methods.Aerodynamics.AVL.create_avl_datastructure.create_avl_datastructure (geometry, conditions)
 
def SUAVE.Methods.Aerodynamics.AVL.initialize_inputs.initialize_inputs (geometry, configuration, conditions)
 
def SUAVE.Methods.Aerodynamics.AVL.purge_directory.purge_directory (path, purge_subdirectories=False)
 
def SUAVE.Methods.Aerodynamics.AVL.purge_files.purge_files (filenames_array, directory='')
 
def SUAVE.Methods.Aerodynamics.AVL.read_results.read_results (avl_object)
 
def SUAVE.Methods.Aerodynamics.AVL.run_analysis.run_analysis (avl_object)
 
def SUAVE.Methods.Aerodynamics.AVL.translate_data.translate_conditions_to_cases (avl, conditions)
 
def SUAVE.Methods.Aerodynamics.AVL.untrimmed.untrimmed (state, settings, geometry)
 untrimmed.py More...
 
def SUAVE.Methods.Aerodynamics.AVL.write_geometry.write_geometry (avl_object)
 
def SUAVE.Methods.Aerodynamics.AVL.write_input_deck.write_input_deck (avl_object)
 
def SUAVE.Methods.Aerodynamics.AVL.write_run_cases.write_run_cases (avl_object)
 
-

Detailed Description

-

Functions to AVL calculations.

-

Function Documentation

- -

◆ create_avl_datastructure()

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def SUAVE.Methods.Aerodynamics.AVL.create_avl_datastructure.create_avl_datastructure ( geometry,
 conditions 
)
-
-
This translates the aircraft geometry into the format used in the AVL run file
-
-Assumptions:
-    None
-    
-Source:
-    Drela, M. and Youngren, H., AVL, http://web.mit.edu/drela/Public/web/avle
-    
-Inputs:
-    geometry    
-    
-Outputs:
-    avl_inputs
-    
-Properties Used:
-    N/A
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◆ initialize_inputs()

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def SUAVE.Methods.Aerodynamics.AVL.initialize_inputs.initialize_inputs ( geometry,
 configuration,
 conditions 
)
-
-
This intializes the functions used in the AVL class
-
-Assumptions:
-        None
-
-Source:
-        None
-
-Inputs:
-        avl_inputs - passed into the write_geometry, write_run_cases and write_input_deck functions
-
-Outputs:
-        avl_imputs
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-Properties Used:
-        N/A
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◆ purge_directory()

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def SUAVE.Methods.Aerodynamics.AVL.purge_directory.purge_directory ( path,
 purge_subdirectories = False 
)
-
-
Deletes the contents of a directory, then the directory itself.
-If purge_subdirectories is True, subdirectories of the directory will also
-be purged, recursively. In this case, the directory specified in the 'path'
-argument will always be removed at the end of this function. 
-However, if purge_subdirectories is False, files in 'path' will be deleted,
-but subdirectories and their contents will be left untouched. In this case, 
-the directory ('path' argument) will only be removed if it contains no
-subdirectories.
-
-
-Assumptions:
-        None
-    
-Source:
-    None
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-Inputs:
-    None
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-Outputs:
-    None
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-Properties Used:
-    N/A
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◆ purge_files()

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def SUAVE.Methods.Aerodynamics.AVL.purge_files.purge_files ( filenames_array,
 directory = '' 
)
-
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Purges folder folder of conflicting files
-
-Assumptions:
-        None
- 
-Source:
-    Drela, M. and Youngren, H., AVL, http://web.mit.edu/drela/Public/web/avl
-
-Inputs:
-    None
-
-Outputs:
-        None
-
-Properties Used:
-    N/A
-
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◆ read_results()

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def SUAVE.Methods.Aerodynamics.AVL.read_results.read_results ( avl_object)
-
-
This functions reads the results from the results text file created 
-at the end of an AVL function call
-
-Assumptions:
-    None
-    
-Source:
-    Drela, M. and Youngren, H., AVL, http://web.mit.edu/drela/Public/web/avl
-
-Inputs:
-    None
-
-Outputs:
-    results     
-
-Properties Used:
-    N/A
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◆ run_analysis()

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def SUAVE.Methods.Aerodynamics.AVL.run_analysis.run_analysis ( avl_object)
-
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This calls the AVL executable and runs an analysis
-
-Assumptions:
-    None
-    
-Source:
-    None
-
-Inputs:
-    avl_object - passed into the  call_avl function  
-    
-Outputs:
-    results
-
-Properties Used:
-    N/A
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◆ translate_conditions_to_cases()

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def SUAVE.Methods.Aerodynamics.AVL.translate_data.translate_conditions_to_cases ( avl,
 conditions 
)
-
-
Takes SUAVE Conditions() data structure and translates to a Container of
-avl Run_Case()s.
-
-Assumptions:
-    None
-    
-Source:
-    Drela, M. and Youngren, H., AVL, http://web.mit.edu/drela/Public/web/avl
-
-Inputs:
-    conditions.aerodynamics.angle_of_attack  [radians] 
-    conditions.freestream.mach_number        [-]
-    conditions.freestream.density            [kilograms per meters**3]
-    conditions.freestream.gravity            [meters per second**2]
-
-Outputs:
-    cases                                    [data structur]
-
-Properties Used:
-    N/A
-
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◆ untrimmed()

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def SUAVE.Methods.Aerodynamics.AVL.untrimmed.untrimmed ( state,
 settings,
 geometry 
)
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- -

untrimmed.py

-

Created: Jan 2014, T. Orra (base file in low fidelity) Modified: May 2017, T. MacDonald

Computes untrimmed drag of the aircraft
-
-Assumptions:
-    None
-    
-Source:
-    None
-
-Inputs:
-    state
-    settings
-    geometry
-
-Outputs:
-    aircraft_untrimmed
-
-Properties Used:
-    N/A
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◆ write_geometry()

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def SUAVE.Methods.Aerodynamics.AVL.write_geometry.write_geometry ( avl_object)
-
-
This function writes the translated aircraft geometry into text file read 
-by AVL when it is called
-
-Assumptions:
-    None
-    
-Source:
-    Drela, M. and Youngren, H., AVL, http://web.mit.edu/drela/Public/web/avl
-
-Inputs:
-    avl_object
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-Outputs:
-    None
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-Properties Used:
-    N/A
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◆ write_input_deck()

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def SUAVE.Methods.Aerodynamics.AVL.write_input_deck.write_input_deck ( avl_object)
-
-
This fucntions writes the execution steps used in the AVL call
-
-Assumptions:
-    None
-    
-Source:
-    Drela, M. and Youngren, H., AVL, http://web.mit.edu/drela/Public/web/avl
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-Inputs:
-    avl_object
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-Outputs:
-    None
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-Properties Used:
-    N/A
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◆ write_run_cases()

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def SUAVE.Methods.Aerodynamics.AVL.write_run_cases.write_run_cases ( avl_object)
-
-
This function writes the run cases used in the AVL batch analysis
-
-Assumptions:
-    None
-    
-Source:
-    Drela, M. and Youngren, H., AVL, http://web.mit.edu/drela/Public/web/avl
-
-Inputs:
-    avl_object.current_status.batch_file                    [-]
-    avl_object.geometry.mass_properties.center_of_gravity   [meters]
-
-Outputs:
-    None
-
-Properties Used:
-    N/A
-
-
-
-
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- - - - diff --git a/_site/doxygen/group__Methods-Aerodynamics-AVL.js b/_site/doxygen/group__Methods-Aerodynamics-AVL.js deleted file mode 100644 index 5c3a3be3..00000000 --- a/_site/doxygen/group__Methods-Aerodynamics-AVL.js +++ /dev/null @@ -1,15 +0,0 @@ -var group__Methods_Aerodynamics_AVL = -[ - [ "Data", "group__Methods-Aerodynamics-AVL-Data.html", "group__Methods-Aerodynamics-AVL-Data" ], - [ "create_avl_datastructure", "group__Methods-Aerodynamics-AVL.html#gac8a412b08b68fa155f5bd1d066f527e6", null ], - [ "initialize_inputs", "group__Methods-Aerodynamics-AVL.html#gaf1b797405da7d00146eac597e13280ea", null ], - [ "purge_directory", "group__Methods-Aerodynamics-AVL.html#ga1c0662bfaf8c7d1512dae0ad94fbda27", null ], - [ "purge_files", "group__Methods-Aerodynamics-AVL.html#ga51c715bd682c9cda6dca2b017265218f", null ], - [ "read_results", "group__Methods-Aerodynamics-AVL.html#ga111943e9a93d2fb37656998659a3a5f0", null ], - [ "run_analysis", "group__Methods-Aerodynamics-AVL.html#ga6c754c0ccd7480bbb1a9cc8bacf3f696", null ], - [ "translate_conditions_to_cases", "group__Methods-Aerodynamics-AVL.html#ga7b721494da52b639d291d6fb7b9b8bf6", null ], - [ "untrimmed", "group__Methods-Aerodynamics-AVL.html#ga7c71f08e28c210a3cb355a8b43f7b5f7", null ], - [ "write_geometry", "group__Methods-Aerodynamics-AVL.html#ga2d8dde8c597e20fc1a4ef7d6c966c939", null ], - [ "write_input_deck", "group__Methods-Aerodynamics-AVL.html#ga5b4b731f90586149f6889a0ba256040a", null ], - [ "write_run_cases", "group__Methods-Aerodynamics-AVL.html#ga3aa7cb9305ca87e3ab5655d63d805f9e", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Methods-Aerodynamics-Fidelity__Zero-Drag.html b/_site/doxygen/group__Methods-Aerodynamics-Fidelity__Zero-Drag.html deleted file mode 100644 index 5fa858ac..00000000 --- a/_site/doxygen/group__Methods-Aerodynamics-Fidelity__Zero-Drag.html +++ /dev/null @@ -1,1219 +0,0 @@ - - - - - - - -SUAVE: Drag - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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Functions to perform low-fidelity drag calculations. -More...

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def SUAVE.Methods.Aerodynamics.Fidelity_Zero.Drag.asymmetry_drag.asymmetry_drag (state, geometry, windmilling_drag_coefficient=0.)
 
def SUAVE.Methods.Aerodynamics.Fidelity_Zero.Drag.compressibility_drag_wing.compressibility_drag_wing (state, settings, geometry)
 
def SUAVE.Methods.Aerodynamics.Fidelity_Zero.Drag.compressibility_drag_wing_total.compressibility_drag_wing_total (state, settings, geometry)
 
def SUAVE.Methods.Aerodynamics.Fidelity_Zero.Drag.compressible_mixed_flat_plate.compressible_mixed_flat_plate (Re, Ma, Tc, xt)
 
def SUAVE.Methods.Aerodynamics.Fidelity_Zero.Drag.compressible_turbulent_flat_plate.compressible_turbulent_flat_plate (Re, Ma, Tc)
 
def SUAVE.Methods.Aerodynamics.Fidelity_Zero.Drag.estimate_2ndseg_lift_drag_ratio.estimate_2ndseg_lift_drag_ratio (config)
 
def SUAVE.Methods.Aerodynamics.Fidelity_Zero.Drag.induced_drag_aircraft.induced_drag_aircraft (state, settings, geometry)
 
def SUAVE.Methods.Aerodynamics.Fidelity_Zero.Drag.miscellaneous_drag_aircraft.miscellaneous_drag_aircraft (conditions, configuration, geometry)
 
def SUAVE.Methods.Aerodynamics.Fidelity_Zero.Drag.miscellaneous_drag_aircraft_ESDU.miscellaneous_drag_aircraft_ESDU (state, settings, geometry)
 
def SUAVE.Methods.Aerodynamics.Fidelity_Zero.Drag.parasite_drag_fuselage.parasite_drag_fuselage (state, settings, geometry)
 
def SUAVE.Methods.Aerodynamics.Fidelity_Zero.Drag.parasite_drag_propulsor.parasite_drag_propulsor (state, settings, geometry)
 
def SUAVE.Methods.Aerodynamics.Fidelity_Zero.Drag.parasite_drag_pylon.parasite_drag_pylon (state, settings, geometry)
 
def SUAVE.Methods.Aerodynamics.Fidelity_Zero.Drag.parasite_drag_wing.parasite_drag_wing (state, settings, geometry)
 
def SUAVE.Methods.Aerodynamics.Fidelity_Zero.Drag.parasite_total.parasite_total (state, settings, geometry)
 
def SUAVE.Methods.Aerodynamics.Fidelity_Zero.Drag.spoiler_drag.spoiler_drag (state, settings, geometry)
 
def SUAVE.Methods.Aerodynamics.Fidelity_Zero.Drag.total_aircraft.total_aircraft (state, settings, geometry)
 
def SUAVE.Methods.Aerodynamics.Fidelity_Zero.Drag.trim.trim (state, settings, geometry)
 trim.py More...
 
def SUAVE.Methods.Aerodynamics.Fidelity_Zero.Drag.untrimmed.untrimmed (state, settings, geometry)
 untrimmed.py More...
 
def SUAVE.Methods.Aerodynamics.Fidelity_Zero.Drag.windmilling_drag.windmilling_drag (geometry, state)
 
-

Detailed Description

-

Functions to perform low-fidelity drag calculations.

-

Function Documentation

- -

◆ asymmetry_drag()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Aerodynamics.Fidelity_Zero.Drag.asymmetry_drag.asymmetry_drag ( state,
 geometry,
 windmilling_drag_coefficient = 0. 
)
-
-
Computes asymmetry drag due to engine failure
-
-Assumptions:
-Two engine aircraft
-
-Source:
-Unknown source
-
-Inputs:
-state.conditions.freestream.dynamic_pressure                                                [Pa]
-state.conditions.aerodynamics.drag_breakdown.windmilling_drag.windmilling_drag_coefficient  [Unitless]
-geometry.
-  mass_properties.center_of_gravity                                                         [m]
-  propulsors. 
-    number_of_engines                                                                       [Unitless]
-  wings.
-    tag                                                                                     
-    sref (this function probably doesn't run)                                               [m^2]
-spans.projected                                                                         [m]
-  reference_area                                                                            [m^2]
-
-Outputs:
-asymm_trim_drag_coefficient                                                                 [Unitless]
-(packed in state.conditions.aerodynamics.drag_breakdown.asymmetry_trim_coefficient)
-
-Properties Used:
-N/A
-
-
-
- -

◆ compressibility_drag_wing()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Aerodynamics.Fidelity_Zero.Drag.compressibility_drag_wing.compressibility_drag_wing ( state,
 settings,
 geometry 
)
-
-
Computes compressibility drag for a wing
-
-Assumptions:
-Subsonic to low transonic
-Supercritical airfoil
-
-Source:
-adg.stanford.edu (Stanford AA241 A/B Course Notes)
-
-Inputs:
-state.conditions.
-  freestream.mach_number                         [Unitless]
-  aerodynamics.lift_breakdown.compressible_wings [Unitless]
-geometry.thickness_to_chord                      [Unitless]
-geometry.sweeps.quarter_chord                    [radians]
-
-Outputs:
-total_compressibility_drag                       [Unitless]
-
-Properties Used:
-N/A
-
-
-
- -

◆ compressibility_drag_wing_total()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Aerodynamics.Fidelity_Zero.Drag.compressibility_drag_wing_total.compressibility_drag_wing_total ( state,
 settings,
 geometry 
)
-
-
Sums compressibility drag for all wings combined
-
-Assumptions:
-None
-
-Source:
-adg.stanford.edu (Stanford AA241 A/B Course Notes)
-
-Inputs:
-state.conditions.aerodynamics.drag_breakdown.compressible[wing.tag].compressibility_drag  [Unitless]
-geometry.wings.areas.reference                                                            [m^2]
-geometry.reference_area                                                                   [m^2]
-
-Outputs:
-total_compressibility_drag                                                                [Unitless]
-
-Properties Used:
-N/A
-
-
-
- -

◆ compressible_mixed_flat_plate()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Aerodynamics.Fidelity_Zero.Drag.compressible_mixed_flat_plate.compressible_mixed_flat_plate ( Re,
 Ma,
 Tc,
 xt 
)
-
-
Computes the coefficient of friction for a flat plate given the 
-input parameters. Also returns the correction terms used in the
-computation.
-
-Assumptions:
-Reynolds number between 10e5 and 10e9
-xt between 0 and 1
-
-Source:
-adg.stanford.edu (Stanford AA241 A/B Course Notes)
-
-Inputs:
-Re (Reynolds number)                                             [Unitless]
-Ma (Mach number)                                                 [Unitless]
-Tc (temperature)                                                 [K]
-xt (turbulent transition point as a proportion of chord length)  [Unitless]
-
-Outputs:
-cf_comp (coefficient of friction)                                [Unitless]
-k_comp (compressibility correction)                              [Unitless]
-k_reyn (Reynolds number correction)                              [Unitless]
-
-Properties Used:
-N/A
-
-
-
- -

◆ compressible_turbulent_flat_plate()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Aerodynamics.Fidelity_Zero.Drag.compressible_turbulent_flat_plate.compressible_turbulent_flat_plate ( Re,
 Ma,
 Tc 
)
-
-
Computes the coefficient of friction for a flat plate given the 
-input parameters. Also returns the correction terms used in the
-computation.
-
-Assumptions:
-Reynolds number between 10e5 and 10e9
-Fully turbulent
-
-Source:
-adg.stanford.edu (Stanford AA241 A/B Course Notes)
-
-Inputs:
-Re (Reynolds number)                                             [Unitless]
-Ma (Mach number)                                                 [Unitless]
-Tc (temperature)                                                 [K]
-
-Outputs:
-cf_comp (coefficient of friction)                                [Unitless]
-k_comp (compressibility correction)                              [Unitless]
-k_reyn (Reynolds number correction)                              [Unitless]
-
-Properties Used:
-N/A
-
-
-
- -

◆ estimate_2ndseg_lift_drag_ratio()

- -
-
- - - - - - - - -
def SUAVE.Methods.Aerodynamics.Fidelity_Zero.Drag.estimate_2ndseg_lift_drag_ratio.estimate_2ndseg_lift_drag_ratio ( config)
-
-
Estimates the 2nd segment climb lift to drag ratio (all engine operating)
-
-Assumptions:
-All engines operating
-
-Source:
-Fig. 27.34 of "Aerodynamic Design of Transport Airplane" - Obert
-
-Inputs:
-config.
-  V2_VS_ratio              [Unitless]
-  wings.
-    areas.reference        [m^2]
-spans.projected        [m]
-aspect_ratio           [Unitless]
-  maximum_lift_coefficient [Unitless]
-
-Outputs:
-lift_drag_ratio            [Unitless]
-
-Properties Used:
-N/A
-
-
-
- -

◆ induced_drag_aircraft()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Aerodynamics.Fidelity_Zero.Drag.induced_drag_aircraft.induced_drag_aircraft ( state,
 settings,
 geometry 
)
-
-
Determines induced drag for the full aircraft
-
-Assumptions:
-Based on fits
-
-Source:
-adg.stanford.edu (Stanford AA241 A/B Course Notes)
-
-Inputs:
-state.conditions.aerodynamics.lift_coefficient               [Unitless]
-state.conditions.aerodynamics.drag_breakdown.parasite.total  [Unitless]
-configuration.oswald_efficiency_factor                       [Unitless]
-configuration.viscous_lift_dependent_drag_factor             [Unitless]
-geometry.wings['main_wing'].span_efficiency                  [Unitless]
-geometry.wings['main_wing'].aspect_ratio                     [Unitless]
-
-Outputs:
-total_induced_drag                                           [Unitless]
-
-Properties Used:
-N/A
-
-
-
- -

◆ miscellaneous_drag_aircraft()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Aerodynamics.Fidelity_Zero.Drag.miscellaneous_drag_aircraft.miscellaneous_drag_aircraft ( conditions,
 configuration,
 geometry 
)
-
-
Computes the miscellaneous drag associated with an aircraft
-
-Assumptions:
-Basic fit
-
-Source:
-adg.stanford.edu (Stanford AA241 A/B Course Notes)
-
-Inputs:
-configuration.trim_drag_correction_factor  [Unitless]
-geometry.propulsors.nacelle_diameter       [m]
-geometry.reference_area                    [m^2]
-geometry.wings['main_wing'].aspect_ratio   [Unitless]
-state.conditions.freestream.mach_number    [Unitless] (actual values are not used)
-
-Outputs:
-total_miscellaneous_drag                   [Unitless]
-
-Properties Used:
-N/A
-
-
-
- -

◆ miscellaneous_drag_aircraft_ESDU()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Aerodynamics.Fidelity_Zero.Drag.miscellaneous_drag_aircraft_ESDU.miscellaneous_drag_aircraft_ESDU ( state,
 settings,
 geometry 
)
-
-
Computes the miscellaneous drag associated with an aircraft
-
-Assumptions:
-Basic fit
-
-Source:
-ESDU 94044, figure 1
-
-Inputs:
-state.conditions.freestream.mach_number    [Unitless] (actual values not used)
-geometry.reference_area                    [m^2]
-geometry.wings.areas.wetted                [m^2]
-geometry.fuselages.areas.wetted            [m^2]
-geometry.propulsor.areas.wetted            [m^2]
-geometry.propulsor.number_of_engines       [Unitless]
-
-Outputs:
-cd_excrescence (drag)                      [Unitless]
-
-Properties Used:
-N/A
-
-
-
- -

◆ parasite_drag_fuselage()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Aerodynamics.Fidelity_Zero.Drag.parasite_drag_fuselage.parasite_drag_fuselage ( state,
 settings,
 geometry 
)
-
-
Computes the parasite drag due to the fuselage
-
-Assumptions:
-Basic fit
-
-Source:
-adg.stanford.edu (Stanford AA241 A/B Course Notes)
-
-Inputs:
-state.conditions.freestream.
-  mach_number                                [Unitless]
-  temperature                                [K]
-  reynolds_number                            [Unitless]
-settings.fuselage_parasite_drag_form_factor  [Unitless]
-geometry.fuselage.       
-  areas.front_projected                      [m^2]
-  areas.wetted                               [m^2]
-  lengths.total                              [m]
-  effective_diameter                         [m]
-
-Outputs:
-fuselage_parasite_drag                       [Unitless]
-
-Properties Used:
-N/A
-
-
-
- -

◆ parasite_drag_propulsor()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Aerodynamics.Fidelity_Zero.Drag.parasite_drag_propulsor.parasite_drag_propulsor ( state,
 settings,
 geometry 
)
-
-
Computes the parasite drag due to the propulsor
-
-Assumptions:
-Basic fit
-
-Source:
-adg.stanford.edu (Stanford AA241 A/B Course Notes)
-
-Inputs:
-state.conditions.freestream.
-  mach_number                                [Unitless]
-  temperature                                [K]
-  reynolds_number                            [Unitless]
-geometry.      
-  nacelle_diameter                           [m^2]
-  areas.wetted                               [m^2]
-  engine_length                              [m]
-
-Outputs:
-propulsor_parasite_drag                      [Unitless]
-
-Properties Used:
-N/A
-
-
-
- -

◆ parasite_drag_pylon()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Aerodynamics.Fidelity_Zero.Drag.parasite_drag_pylon.parasite_drag_pylon ( state,
 settings,
 geometry 
)
-
-
Computes the parasite drag due to pylons as a proportion of the propulsor drag
-
-Assumptions:
-Basic fit
-
-Source:
-adg.stanford.edu (Stanford AA241 A/B Course Notes)
-
-Inputs:
-conditions.aerodynamics.drag_breakdown.parasite[propulsor.tag].
-  form_factor                                                   [Unitless]
-  compressibility_factor                                        [Unitless]
-  skin_friction_coefficient                                     [Unitless]
-  wetted_area                                                   [m^2]
-  parasite_drag_coefficient                                     [Unitless]
-  reynolds_number                                               [Unitless]
-geometry.reference_area                                         [m^2]
-geometry.propulsors. 
-  nacelle_diameter                                              [m]
-  number_of_engines                                             [Unitless]
-
-Outputs:
-propulsor_parasite_drag                                         [Unitless]
-
-Properties Used:
-N/A
-
-
-
- -

◆ parasite_drag_wing()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Aerodynamics.Fidelity_Zero.Drag.parasite_drag_wing.parasite_drag_wing ( state,
 settings,
 geometry 
)
-
-
Computes the parasite drag due to wings
-
-Assumptions:
-Basic fit
-
-Source:
-adg.stanford.edu (Stanford AA241 A/B Course Notes)
-
-Inputs:
-settings.wing_parasite_drag_form_factor      [Unitless]
-state.conditions.freestream.
-  mach_number                                [Unitless]
-  temperature                                [K]
-  reynolds_number                            [Unitless]
-geometry.
-  areas.reference                            [m^2]
-  chords.mean_aerodynamic                    [m]
-  thickness_to_chord                         [Unitless]
-  sweeps.quarter_chord                       [radians]
-  aspect_ratio                               [Unitless]
-  spans.projected                            [m]
-  areas.exposed                              [m^2]
-  areas.affected                             [m^2]
-  areas.wetted                               [m^2]
-  transition_x_upper                         [Unitless]
-  transition_x_lower                         [Unitless]
-  
-  
-Outputs:
-wing_parasite_drag                           [Unitless]
-
-Properties Used:
-N/A
-
-
-
- -

◆ parasite_total()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Aerodynamics.Fidelity_Zero.Drag.parasite_total.parasite_total ( state,
 settings,
 geometry 
)
-
-
Sums component parasite drag
-
-Assumptions:
-None
-
-Source:
-None
-
-Inputs:
-geometry.reference_area                             [m^2]
-geometry.wings.areas.reference                      [m^2]
-geometry.fuselages.areas.front_projected            [m^2]
-geometry.propulsors.number_of_engines               [Unitless]
-geometry.propulsors.nacelle_diameter                [m]
-conditions.aerodynamics.drag_breakdown.
-  parasite[wing.tag].parasite_drag_coefficient      [Unitless]
-  parasite[fuselage.tag].parasite_drag_coefficient  [Unitless]
-  parasite[propulsor.tag].parasite_drag_coefficient [Unitless]
-
-
-Outputs:
-total_parasite_drag                                 [Unitless]
-
-Properties Used:
-N/A
-
-
-
- -

◆ spoiler_drag()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Aerodynamics.Fidelity_Zero.Drag.spoiler_drag.spoiler_drag ( state,
 settings,
 geometry 
)
-
-
Adds a spoiler drag increment
-
-Assumptions:
-None
-
-Source:
-None
-
-Inputs:
-settings.spoiler_drag_increment  [Unitless]
-
-Outputs:
-spoiler_drag                     [Unitless]
-
-Properties Used:
-N/A
-
-
-
- -

◆ total_aircraft()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Aerodynamics.Fidelity_Zero.Drag.total_aircraft.total_aircraft ( state,
 settings,
 geometry 
)
-
-
Computes the total drag for an aircraft
-
-Assumptions:
-None
-
-Source:
-None
-
-Inputs:
-state.conditions.aerodynamics.drag_breakdown.
-  trim_corrected_drag                    [Unitless]
-  spoiler_drag                           [Unitless]
-settings.drag_coefficient_increment      [Unitless]
-
-Outputs:
-aircraft_total_drag                      [Unitless]
-
-Properties Used:
-N/A
-
-
-
- -

◆ trim()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Aerodynamics.Fidelity_Zero.Drag.trim.trim ( state,
 settings,
 geometry 
)
-
- -

trim.py

-

Created: Jan 2014, T. Orra Modified: Jan 2016, E. Botero

Adjusts aircraft drag based on a trim correction
-
-Assumptions:
-None
-
-Source:
-Unknown
-
-Inputs:
-settings.trim_drag_correction_factor                   [Unitless]
-state.conditions.aerodynamics.drag_breakdown.untrimmed [Unitless]
-
-Outputs:
-aircraft_total_drag_trim_corrected                     [Unitless]
-
-Properties Used:
-N/A
-
-
-
- -

◆ untrimmed()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Aerodynamics.Fidelity_Zero.Drag.untrimmed.untrimmed ( state,
 settings,
 geometry 
)
-
- -

untrimmed.py

-

Created: Jan 2014, T. Orra Modified: Jan 2016, E. Botero

Sums aircraft drag before trim correction
-
-Assumptions:
-None
-
-Source:
-None
-
-Inputs:
-state.conditions.aerodynamics.drag_breakdown.
-  parasite.total                              [Unitless]
-  induced.total                               [Unitless]
-  compressible.total                          [Unitless]
-  miscellaneous.total                         [Unitless]
-
-Outputs:
-aircraft_untrimmed                            [Unitless]
-
-Properties Used:
-N/A
-
-
-
- -

◆ windmilling_drag()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Aerodynamics.Fidelity_Zero.Drag.windmilling_drag.windmilling_drag ( geometry,
 state 
)
-
-
Computes windmilling drag for turbofan engines
-
-Assumptions:
-None
-
-Source:
-http://www.dept.aoe.vt.edu/~mason/Mason_f/AskinThesis2002_13.pdf
-
-Inputs:
-geometry.
-  max_mach_operational        [Unitless]
-  reference_area              [m^2]
-  wings.sref                  [m^2]
-  propulsors. 
-    areas.wetted              [m^2]
-    nacelle_diameter          [m^2]
-    engine_length             [m^2]
-
-Outputs:
-windmilling_drag_coefficient  [Unitless]
-
-Properties Used:
-N/A
-
-
-
-
-
- - - - diff --git a/_site/doxygen/group__Methods-Aerodynamics-Fidelity__Zero-Drag.js b/_site/doxygen/group__Methods-Aerodynamics-Fidelity__Zero-Drag.js deleted file mode 100644 index b4fe4eda..00000000 --- a/_site/doxygen/group__Methods-Aerodynamics-Fidelity__Zero-Drag.js +++ /dev/null @@ -1,22 +0,0 @@ -var group__Methods_Aerodynamics_Fidelity__Zero_Drag = -[ - [ "asymmetry_drag", "group__Methods-Aerodynamics-Fidelity__Zero-Drag.html#ga1425e3cb3803cd08ac82ad0582820ab0", null ], - [ "compressibility_drag_wing", "group__Methods-Aerodynamics-Fidelity__Zero-Drag.html#ga15cfb5895590cc05b9040fec2a9e8ee0", null ], - [ "compressibility_drag_wing_total", "group__Methods-Aerodynamics-Fidelity__Zero-Drag.html#gaa0825fcdca85b2ff0ce48db7827568c4", null ], - [ "compressible_mixed_flat_plate", "group__Methods-Aerodynamics-Fidelity__Zero-Drag.html#gab1408af68123351f7c93f2286cf60c5a", null ], - [ "compressible_turbulent_flat_plate", "group__Methods-Aerodynamics-Fidelity__Zero-Drag.html#gac955f63f19536a7a9a2e2bf3a708c400", null ], - [ "estimate_2ndseg_lift_drag_ratio", "group__Methods-Aerodynamics-Fidelity__Zero-Drag.html#ga52582c76e2e1bc618dcab2cf5e3a592a", null ], - [ "induced_drag_aircraft", "group__Methods-Aerodynamics-Fidelity__Zero-Drag.html#gab7df58f47780322f76c60e6533de133f", null ], - [ "miscellaneous_drag_aircraft", "group__Methods-Aerodynamics-Fidelity__Zero-Drag.html#gae377a9f7fafb6859a3064eff39bee640", null ], - [ "miscellaneous_drag_aircraft_ESDU", "group__Methods-Aerodynamics-Fidelity__Zero-Drag.html#gab56594aae55befd02a21fc4d7cc7b974", null ], - [ "parasite_drag_fuselage", "group__Methods-Aerodynamics-Fidelity__Zero-Drag.html#gaab60e449bfe1d8714543d7facc5a33bb", null ], - [ "parasite_drag_propulsor", "group__Methods-Aerodynamics-Fidelity__Zero-Drag.html#ga227fa20bdd86f2ade29beced8d711eb8", null ], - [ "parasite_drag_pylon", "group__Methods-Aerodynamics-Fidelity__Zero-Drag.html#ga509c1c4a93e12c621ada831e0ef92ce9", null ], - [ "parasite_drag_wing", "group__Methods-Aerodynamics-Fidelity__Zero-Drag.html#ga765562bc65f4161759faa51483956db1", null ], - [ "parasite_total", "group__Methods-Aerodynamics-Fidelity__Zero-Drag.html#gaa694d9bcfa61e8bad38ccfad7e572f2a", null ], - [ "spoiler_drag", "group__Methods-Aerodynamics-Fidelity__Zero-Drag.html#ga0854dfaf40aa9456333e0980f7f7df68", null ], - [ "total_aircraft", "group__Methods-Aerodynamics-Fidelity__Zero-Drag.html#ga9d1747b3764db03b46e6c11329c4f834", null ], - [ "trim", "group__Methods-Aerodynamics-Fidelity__Zero-Drag.html#ga219b77caea5184e898ed1287cad07b81", null ], - [ "untrimmed", "group__Methods-Aerodynamics-Fidelity__Zero-Drag.html#gaba921ece6489a49aab681815ed23c38b", null ], - [ "windmilling_drag", "group__Methods-Aerodynamics-Fidelity__Zero-Drag.html#ga90c0067d34075668f4deac91ca6ad4e8", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Methods-Aerodynamics-Fidelity__Zero-Lift.html b/_site/doxygen/group__Methods-Aerodynamics-Fidelity__Zero-Lift.html deleted file mode 100644 index ebc61d82..00000000 --- a/_site/doxygen/group__Methods-Aerodynamics-Fidelity__Zero-Lift.html +++ /dev/null @@ -1,700 +0,0 @@ - - - - - - - -SUAVE: Lift - - - - - - - - - - - - - - - -
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- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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Functions to perform low-fidelity lift calculations. -More...

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-Functions

def SUAVE.Methods.Aerodynamics.Fidelity_Zero.Lift.aircraft_total.aircraft_total (state, settings, geometry)
 aircraft_total.py More...
 
def SUAVE.Methods.Aerodynamics.Fidelity_Zero.Lift.compute_flap_lift.compute_flap_lift (t_c, flap_type, flap_chord, flap_angle, sweep, wing_Sref, wing_affected_area)
 
def SUAVE.Methods.Aerodynamics.Fidelity_Zero.Lift.compute_max_lift_coeff.compute_max_lift_coeff (vehicle, conditions=None)
 
def SUAVE.Methods.Aerodynamics.Fidelity_Zero.Lift.compute_slat_lift.compute_slat_lift (slat_angle, sweep_angle)
 
def SUAVE.Methods.Aerodynamics.Fidelity_Zero.Lift.fuselage_correction.fuselage_correction (state, settings, geometry)
 fuselage_correction.py More...
 
def SUAVE.Methods.Aerodynamics.Fidelity_Zero.Lift.linear_inviscid_wing.linear_inviscid_wing (state, settings, geometry)
 
def SUAVE.Methods.Aerodynamics.Fidelity_Zero.Lift.linear_supersonic_lift.linear_supersonic_lift (conditions, configuration, wing)
 
def SUAVE.Methods.Aerodynamics.Fidelity_Zero.Lift.vortex_lift.vortex_lift (AoA, configuration, wing)
 
def SUAVE.Methods.Aerodynamics.Fidelity_Zero.Lift.weissinger_vortex_lattice.weissinger_vortex_lattice (conditions, configuration, wing)
 
def SUAVE.Methods.Aerodynamics.Fidelity_Zero.Lift.wing_compressibility_correction.wing_compressibility_correction (state, settings, geometry)
 
-

Detailed Description

-

Functions to perform low-fidelity lift calculations.

-

Function Documentation

- -

◆ aircraft_total()

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- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Aerodynamics.Fidelity_Zero.Lift.aircraft_total.aircraft_total ( state,
 settings,
 geometry 
)
-
- -

aircraft_total.py

-

Created: Dec 2013, A. Variyar, Modified: Feb 2014, A. Variyar, T. Lukaczyk, T. Orra Apr 2014, A. Variyar Jan 2016, E. Botero

Returns total aircraft lift and stores values
-
-Assumptions:
-None
-
-Source:
-None
-
-Inputs:
-settings.fuselage_lift_correction  [Unitless]
-state.conditions.
-  freestream.mach_number           [Unitless]
-  aerodynamics.angle_of_attack     [radians]
-  aerodynamics.lift_coefficient    [Unitless]
-
-Outputs:
-aircraft_lift_total                [Unitless]
-
-Properties Used:
-N/A
-
-
-
- -

◆ compute_flap_lift()

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def SUAVE.Methods.Aerodynamics.Fidelity_Zero.Lift.compute_flap_lift.compute_flap_lift ( t_c,
 flap_type,
 flap_chord,
 flap_angle,
 sweep,
 wing_Sref,
 wing_affected_area 
)
-
-
Computes the increase of lift due to trailing edge flap deployment
-
-Assumptions:
-None
-
-Source:
-Unknown
-
-Inputs:
-t_c                 (wing thickness ratio)                 [Unitless]
-flap_type                                                  [string]
-flap_c_chord        (flap chord as fraction of wing chord) [Unitless]
-flap_angle          (flap deflection)                      [radians]
-sweep               (Wing sweep angle)                     [radians]
-wing_Sref           (Wing reference area)                  [m^2]
-wing_affected_area  (Wing area affected by flaps)          [m^2]
-
-Outputs:
-dcl_max_flaps       (Lift coefficient increase)            [Unitless]
-
-Properties Used:
-N/A
-
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-
- -

◆ compute_max_lift_coeff()

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def SUAVE.Methods.Aerodynamics.Fidelity_Zero.Lift.compute_max_lift_coeff.compute_max_lift_coeff ( vehicle,
 conditions = None 
)
-
-
Computes the maximum lift coefficient associated with an aircraft high lift system
-
-Assumptions:
-None
-
-Source:
-Unknown
-
-Inputs:
-vehicle.max_lift_coefficient_factor [Unitless]
-vehicle.reference_area              [m^2]
-vehicle.wings. 
-  areas.reference                   [m^2]
-  thickness_to_chord                [Unitless]
-  chords.mean_aerodynamic           [m]
-  sweeps.quarter_chord              [radians]
-  taper                             [Unitless]
-  flaps.chord                       [m]
-  flaps.angle                       [radians]
-  slats.angle                       [radians]
-  areas.affected                    [m^2]
-  flaps.type                        [string]
-conditions.freestream.
-  velocity                          [m/s]
-  density                           [kg/m^3]
-  dynamic_viscosity                 [N s/m^2]
-
-Outputs:
-Cl_max_ls (maximum CL)              [Unitless]
-Cd_ind    (induced drag)            [Unitless]
-
-Properties Used:
-N/A
-
-
-
- -

◆ compute_slat_lift()

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- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Aerodynamics.Fidelity_Zero.Lift.compute_slat_lift.compute_slat_lift ( slat_angle,
 sweep_angle 
)
-
-
Computes the increase in lift due to slats
-
-Assumptions:
-None
-
-Source:
-adg.stanford.edu (Stanford AA241 A/B Course Notes)
-
-Inputs:
-slat_angle   [radians]
-sweep_angle  [radians]
-
-Outputs:
-dcl_slat     [Unitless]
-
-Properties Used:
-N/A
-
-
-
- -

◆ fuselage_correction()

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def SUAVE.Methods.Aerodynamics.Fidelity_Zero.Lift.fuselage_correction.fuselage_correction ( state,
 settings,
 geometry 
)
-
- -

fuselage_correction.py

-

Created: Dec 2013, A. Variyar Modified: Feb 2014, A. Variyar, T. Lukaczyk, T. Orra Apr 2014, A. Variyar Jan 2015, E. Botero

Corrects aircraft lift based on fuselage effects
-
-Assumptions:
-None
-
-Source:
-adg.stanford.edu (Stanford AA241 A/B Course Notes)
-
-Inputs:
-settings.fuselage_lift_correction  [Unitless]
-state.conditions.
-  freestream.mach_number           [Unitless]
-  aerodynamics.angle_of_attack     [radians]
-  aerodynamics.lift_coefficient    [Unitless]
-
-Outputs:
-aircraft_lift_total                [Unitless]
-
-Properties Used:
-N/A
-
-
-
- -

◆ linear_inviscid_wing()

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def SUAVE.Methods.Aerodynamics.Fidelity_Zero.Lift.linear_inviscid_wing.linear_inviscid_wing ( state,
 settings,
 geometry 
)
-
-
Computes wing lift base on simple linear theory
-
-Assumptions:
-Linear airfoil theory
-
-Source:
-Linear airfoil theory
-
-Inputs:
-state.conditions.freestream.mach_number        [Unitless]
-state.conditions.aerodynamics.angle_of_attack  [Unitless]
-
-Outputs:
-wings_lift                                     [Unitless]
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-Properties Used:
-N/A
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◆ linear_supersonic_lift()

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def SUAVE.Methods.Aerodynamics.Fidelity_Zero.Lift.linear_supersonic_lift.linear_supersonic_lift ( conditions,
 configuration,
 wing 
)
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-
This function is outdated and not used in Fidelity_Zero
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◆ vortex_lift()

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def SUAVE.Methods.Aerodynamics.Fidelity_Zero.Lift.vortex_lift.vortex_lift ( AoA,
 configuration,
 wing 
)
-
-
Computes vortex lift
-
-Assumptions:
-wing capable of vortex lift
-
-Source:
-adg.stanford.edu (Stanford AA241 A/B Course Notes)
-
-Inputs:
-wing.aspect_ratio         [Unitless]
-wing.sweeps.quarter_chord [radians]
-
-Outputs:
-CL_prime  (added CL)      [Unitless]
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-Properties Used:
-N/A
-
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- -

◆ weissinger_vortex_lattice()

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def SUAVE.Methods.Aerodynamics.Fidelity_Zero.Lift.weissinger_vortex_lattice.weissinger_vortex_lattice ( conditions,
 configuration,
 wing 
)
-
-
Uses the vortex lattice method to compute the lift coefficient and induced drag component
-
-Assumptions:
-None
-
-Source:
-Unknown
-
-Inputs:
-wing.
-  spans.projected                       [m]
-  chords.root                           [m]
-  chords.tip                            [m]
-  sweeps.quarter_chord                  [radians]
-  taper                                 [Unitless]
-  twists.root                           [radians]
-  twists.tip                            [radians]
-  symmetric                             [Boolean]
-  aspect_ratio                          [Unitless]
-  areas.reference                       [m^2]
-  vertical                              [Boolean]
-configuration.number_panels_spanwise    [Unitless]
-configuration.number_panels_chordwise   [Unitless]
-conditions.aerodynamics.angle_of_attack [radians]
-
-Outputs:
-Cl                                      [Unitless]
-Cd                                      [Unitless]
-
-Properties Used:
-N/A
-
-
-
- -

◆ wing_compressibility_correction()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Aerodynamics.Fidelity_Zero.Lift.wing_compressibility_correction.wing_compressibility_correction ( state,
 settings,
 geometry 
)
-
-
Corrects a wings lift based on compressibility
-
-Assumptions:
-subsonic
-
-Source:
-https://stanford.edu/~cantwell/AA200_Course_Material/AA200_Course_Notes/
-
-Inputs:
-settings.fuselage_lift_correction  [-]
-state.conditions.
-  freestream.mach_number           [-]
-  aerodynamics.angle_of_attack     [radians]
-  aerodynamics.lift_coefficient    [-]
-
-Outputs:
-state.conditions.aerodynamics.
-  lift_breakdown.compressible_wings [-] CL for the wings
-  lift_coefficient                  [-]
-wings_lift_comp                     [-]
-
-Properties Used:
-N/A
-
-
-
-
-
- - - - diff --git a/_site/doxygen/group__Methods-Aerodynamics-Fidelity__Zero-Lift.js b/_site/doxygen/group__Methods-Aerodynamics-Fidelity__Zero-Lift.js deleted file mode 100644 index a4407cf7..00000000 --- a/_site/doxygen/group__Methods-Aerodynamics-Fidelity__Zero-Lift.js +++ /dev/null @@ -1,13 +0,0 @@ -var group__Methods_Aerodynamics_Fidelity__Zero_Lift = -[ - [ "aircraft_total", "group__Methods-Aerodynamics-Fidelity__Zero-Lift.html#ga00e00000a6d73d937ea680f2849c7cc6", null ], - [ "compute_flap_lift", "group__Methods-Aerodynamics-Fidelity__Zero-Lift.html#gaba1f06c8eee68017b66b4f853272463b", null ], - [ "compute_max_lift_coeff", "group__Methods-Aerodynamics-Fidelity__Zero-Lift.html#ga4adc3f3425f18c8b914194a7b233fe31", null ], - [ "compute_slat_lift", "group__Methods-Aerodynamics-Fidelity__Zero-Lift.html#ga0f976657004084baf27a29d8bbf567be", null ], - [ "fuselage_correction", "group__Methods-Aerodynamics-Fidelity__Zero-Lift.html#gabad425792a86b9a28caf9506a59b2e33", null ], - [ "linear_inviscid_wing", "group__Methods-Aerodynamics-Fidelity__Zero-Lift.html#ga3605a53bc1d9beca71cec3e7b0afd604", null ], - [ "linear_supersonic_lift", "group__Methods-Aerodynamics-Fidelity__Zero-Lift.html#gafc2074250fc349852603f0accb7f3679", null ], - [ "vortex_lift", "group__Methods-Aerodynamics-Fidelity__Zero-Lift.html#ga647c5ae1f94ea7da69ac179f7b47467e", null ], - [ "weissinger_vortex_lattice", "group__Methods-Aerodynamics-Fidelity__Zero-Lift.html#ga903b6ae4c0e0196d2a50643efe73dfb1", null ], - [ "wing_compressibility_correction", "group__Methods-Aerodynamics-Fidelity__Zero-Lift.html#ga987c51069000f6e459d2754ed2533125", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Methods-Aerodynamics-Fidelity__Zero.html b/_site/doxygen/group__Methods-Aerodynamics-Fidelity__Zero.html deleted file mode 100644 index 809b0389..00000000 --- a/_site/doxygen/group__Methods-Aerodynamics-Fidelity__Zero.html +++ /dev/null @@ -1,126 +0,0 @@ - - - - - - - -SUAVE: Fidelity_Zero - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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Fidelity_Zero
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Functions to perform low-fidelity calculations. -More...

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-Modules

 Drag
 Functions to perform low-fidelity drag calculations.
 
 Lift
 Functions to perform low-fidelity lift calculations.
 
-

Detailed Description

-

Functions to perform low-fidelity calculations.

-
-
- - - - diff --git a/_site/doxygen/group__Methods-Aerodynamics-Fidelity__Zero.js b/_site/doxygen/group__Methods-Aerodynamics-Fidelity__Zero.js deleted file mode 100644 index b89966bb..00000000 --- a/_site/doxygen/group__Methods-Aerodynamics-Fidelity__Zero.js +++ /dev/null @@ -1,5 +0,0 @@ -var group__Methods_Aerodynamics_Fidelity__Zero = -[ - [ "Drag", "group__Methods-Aerodynamics-Fidelity__Zero-Drag.html", "group__Methods-Aerodynamics-Fidelity__Zero-Drag" ], - [ "Lift", "group__Methods-Aerodynamics-Fidelity__Zero-Lift.html", "group__Methods-Aerodynamics-Fidelity__Zero-Lift" ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Methods-Aerodynamics-OpenVSP__Wave__Drag.html b/_site/doxygen/group__Methods-Aerodynamics-OpenVSP__Wave__Drag.html deleted file mode 100644 index 517c20c7..00000000 --- a/_site/doxygen/group__Methods-Aerodynamics-OpenVSP__Wave__Drag.html +++ /dev/null @@ -1,460 +0,0 @@ - - - - - - - -SUAVE: OpenVSP_Wave_Drag - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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Functions to perform wave drag calculations using OpenVSP. -More...

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-Functions

def SUAVE.Methods.Aerodynamics.OpenVSP_Wave_Drag.compressibility_drag_total.compressibility_drag_total (state, settings, geometry)
 
def SUAVE.Methods.Aerodynamics.OpenVSP_Wave_Drag.compressibility_drag_total.drag_div (Mc_ii, wing, k, cl, Sref_main)
 
def SUAVE.Methods.Aerodynamics.OpenVSP_Wave_Drag.compressibility_drag_total.lift_wave_drag (conditions, configuration, wing, k, Sref_main, flag105)
 
def SUAVE.Methods.Aerodynamics.OpenVSP_Wave_Drag.wave_drag_lift.wave_drag_lift (conditions, configuration, wing)
 
def SUAVE.Methods.Aerodynamics.OpenVSP_Wave_Drag.wave_drag_volume.wave_drag_volume (conditions, geometry, flag105, num_slices=20, num_rots=10)
 
-

Detailed Description

-

Functions to perform wave drag calculations using OpenVSP.

-

Function Documentation

- -

◆ compressibility_drag_total()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Aerodynamics.OpenVSP_Wave_Drag.compressibility_drag_total.compressibility_drag_total ( state,
 settings,
 geometry 
)
-
-
Computes compressibility drag for full aircraft including volume drag through OpenVSP
-
-Assumptions:
-None
-
-Source:
-adg.stanford.edu (Stanford AA241 A/B Course Notes)
-
-Inputs:
-settings.number_slices
-settings.number_rotations
-state.conditions.aerodynamics.
-  lift_breakdown.compressible_wings      [-]
-state.conditions.freestream.mach_number  [-]
-geometry.wings.*.tag                       
-
-Outputs:
-drag_breakdown.compressible[wing.tag].
-  divergence_mach                        [-]
-drag_breakdown.compressible.total        [-]                    
-drag_breakdown.compressible.total_volume [-]
-drag_breakdown.compressible.total_lift   [-]
-cd_c                                     [-] Total compressibility drag
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-Properties Used:
-N/A
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◆ drag_div()

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def SUAVE.Methods.Aerodynamics.OpenVSP_Wave_Drag.compressibility_drag_total.drag_div ( Mc_ii,
 wing,
 k,
 cl,
 Sref_main 
)
-
-
Use drag divergence mach number to determine drag for subsonic speeds
-
-Assumptions:
-Basic fit, subsonic
-
-Source:
-adg.stanford.edu (Stanford AA241 A/B Course Notes)
-
-Inputs:
-wing.
-  thickness_to_chord    [-]     
-  sweeps.quarter_chord  [radians]
-  high_mach             [Boolean]
-  areas.reference       [m^2]
-
-Outputs:
-cd_c                    [-]
-mcc                     [-]
-MDiv                    [-]
-
-Properties Used:
-N/A
-
-
-
- -

◆ lift_wave_drag()

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-
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Aerodynamics.OpenVSP_Wave_Drag.compressibility_drag_total.lift_wave_drag ( conditions,
 configuration,
 wing,
 k,
 Sref_main,
 flag105 
)
-
-
Determine lift wave drag for supersonic speeds
-
-Assumptions:
-Basic fit
-
-Source:
-adg.stanford.edu (Stanford AA241 A/B Course Notes)
-
-Inputs:
-conditions.freestream.mach_number [-]
-configuration                     (passed to another function)
-wing.areas.reference              [m^2]
-k                                 (unused)
-Sref_main                         [m^2] Main reference area
-flag105                           <boolean> Check if calcs are for Mach 1.05
-
-Outputs:
-cd_c_l                            [-] Wave drag CD due to lift
-
-Properties Used:
-N/A
-
-
-
- -

◆ wave_drag_lift()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Aerodynamics.OpenVSP_Wave_Drag.wave_drag_lift.wave_drag_lift ( conditions,
 configuration,
 wing 
)
-
-
Determine lift wave drag for supersonic speeds
-
-Assumptions:
-Basic fit
-
-Source:
-adg.stanford.edu (Stanford AA241 A/B Course Notes)
-
-Inputs:
-conditions.
-  freestream.mach_number          [-]
-  aerodynamics.lift_coefficient   [-] Used to build a dummy array if wing is vertical
-  aerodynamics.lift_breakdown.   
-    inviscid_wings_lift           [-] Used for lift otherwise
-configuration                     (unused)
-wing.total_length                 [m]
-wing.areas.reference              [m^2]
-wing.vertical                     <boolean> Indicates if the wing is vertical
-wing.tag                          <string>
-
-Outputs:
-wave_drag_lift                    [-] Wave drag CD due to lift (for the wing)
-
-Properties Used:
-N/A
-
-
-
- -

◆ wave_drag_volume()

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def SUAVE.Methods.Aerodynamics.OpenVSP_Wave_Drag.wave_drag_volume.wave_drag_volume ( conditions,
 geometry,
 flag105,
 num_slices = 20,
 num_rots = 10 
)
-
-
Determine volume wave drag for supersonic speeds using OpenVSP
-
-Assumptions:
-None
-
-Source:
-adg.stanford.edu (Stanford AA241 A/B Course Notes)
-
-Inputs:
-conditions.
-  freestream.mach_number [-]
-geometry.
-  reference_area         [m^2]
-  tag                    <string>
-flag105                  <boolean> determines is Mach = 1.05 is used
-num_slices               [-] Slices used by OpenVSP (optional - defaults to 20)
-num_rots                 [-] Rotations used by OpenVSP (optional - defaults to 10)
-
-Outputs:
-cd_w_all
-
-Properties Used:
-N/A
-
-
-
-
-
- - - - diff --git a/_site/doxygen/group__Methods-Aerodynamics-OpenVSP__Wave__Drag.js b/_site/doxygen/group__Methods-Aerodynamics-OpenVSP__Wave__Drag.js deleted file mode 100644 index 6dcdb2ab..00000000 --- a/_site/doxygen/group__Methods-Aerodynamics-OpenVSP__Wave__Drag.js +++ /dev/null @@ -1,8 +0,0 @@ -var group__Methods_Aerodynamics_OpenVSP__Wave__Drag = -[ - [ "compressibility_drag_total", "group__Methods-Aerodynamics-OpenVSP__Wave__Drag.html#ga3971e900ca810e4db94e8345fb615643", null ], - [ "drag_div", "group__Methods-Aerodynamics-OpenVSP__Wave__Drag.html#ga697d7e84b46b7d70e96850f01ecf053c", null ], - [ "lift_wave_drag", "group__Methods-Aerodynamics-OpenVSP__Wave__Drag.html#ga8211c1791c6d45ae77451ab5a4f29cef", null ], - [ "wave_drag_lift", "group__Methods-Aerodynamics-OpenVSP__Wave__Drag.html#gab749cbd101a432408842f749d77273be", null ], - [ "wave_drag_volume", "group__Methods-Aerodynamics-OpenVSP__Wave__Drag.html#ga28cf2bc6d8103e77ee2b67793899d0b8", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Methods-Aerodynamics-SU2__Euler.html b/_site/doxygen/group__Methods-Aerodynamics-SU2__Euler.html deleted file mode 100644 index 48442e5e..00000000 --- a/_site/doxygen/group__Methods-Aerodynamics-SU2__Euler.html +++ /dev/null @@ -1,234 +0,0 @@ - - - - - - - -SUAVE: SU2_Euler - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
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SU2_Euler
-
-
- -

SU2_Euler contains the function needed to run the SU2 Euler Analysis. -More...

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-Functions

def SUAVE.Methods.Aerodynamics.SU2_Euler.total_aircraft_drag.total_aircraft_drag (state, settings, geometry)
 
def SUAVE.Methods.Aerodynamics.SU2_Euler.untrimmed.untrimmed (state, settings, geometry)
 
-

Detailed Description

-

SU2_Euler contains the function needed to run the SU2 Euler Analysis.

-

Function Documentation

- -

◆ total_aircraft_drag()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Aerodynamics.SU2_Euler.total_aircraft_drag.total_aircraft_drag ( state,
 settings,
 geometry 
)
-
-
This computes the total drag of an aircraft and stores
-that data in the conditions structure.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-settings.drag_coefficient_increment            [Unitless]
-state.conditions.aerodynamics.drag_breakdown.
-  trim_corrected_drag                          [Unitless]
-  spoiler_drag                                 [Unitless]
-  
-Outputs:
-aircraft_total_drag                            [Unitless]
-
-Properties Used:
-N/A
-
-
-
- -

◆ untrimmed()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Aerodynamics.SU2_Euler.untrimmed.untrimmed ( state,
 settings,
 geometry 
)
-
-
This computes the total drag of an aircraft without trim
-and stores that data in the conditions structure.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-state.conditions.aerodynamics.drag_breakdown.
-  parasite.total                               [Unitless]
-  induced.total                                [Unitless]
-  compressible.total                           [Unitless]
-  miscellaneous.total                          [Unitless]
-
-Outputs:
-aircraft_untrimmed                             [Unitless]
-
-Properties Used:
-N/A
-
-
-
-
-
- - - - diff --git a/_site/doxygen/group__Methods-Aerodynamics-SU2__Euler.js b/_site/doxygen/group__Methods-Aerodynamics-SU2__Euler.js deleted file mode 100644 index aa627520..00000000 --- a/_site/doxygen/group__Methods-Aerodynamics-SU2__Euler.js +++ /dev/null @@ -1,5 +0,0 @@ -var group__Methods_Aerodynamics_SU2__Euler = -[ - [ "total_aircraft_drag", "group__Methods-Aerodynamics-SU2__Euler.html#ga0b09ae08d2258da031018d6d287bef31", null ], - [ "untrimmed", "group__Methods-Aerodynamics-SU2__Euler.html#ga2177b80d030f75bc4e2e0fad6a68abb7", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Methods-Aerodynamics-Supersonic__Zero-Drag.html b/_site/doxygen/group__Methods-Aerodynamics-Supersonic__Zero-Drag.html deleted file mode 100644 index 385544d6..00000000 --- a/_site/doxygen/group__Methods-Aerodynamics-Supersonic__Zero-Drag.html +++ /dev/null @@ -1,1333 +0,0 @@ - - - - - - - -SUAVE: Drag - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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Functions to perform low-fidelity drag calculations including supersonic. -More...

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-Functions

def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.compressibility_drag_total.compressibility_drag_total (state, settings, geometry)
 
def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.compressibility_drag_total.drag_div (Mc_ii, wing, k, cl, Sref_main)
 
def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.compressibility_drag_total.wave_drag (conditions, configuration, main_fuselage, propulsor, wing, num_engines, k, Sref_main, flag105)
 
def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.compressibility_drag_total.wave_drag_body_of_rev (total_length, Rmax, Sref)
 
def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.compressible_mixed_flat_plate.compressible_mixed_flat_plate (Re, Ma, Tc, xt)
 
def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.compressible_turbulent_flat_plate.compressible_turbulent_flat_plate (Re, Ma, Tc)
 
def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.compute_aircraft_drag.compute_aircraft_drag (conditions, configuration, geometry=None)
 compute_aircraft_drag.py More...
 
def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.induced_drag_aircraft.induced_drag_aircraft (state, settings, geometry)
 
def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.miscellaneous_drag_aircraft.miscellaneous_drag_aircraft (state, settings, geometry)
 
def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.parasite_drag_aircraft.parasite_drag_aircraft (conditions, configuration, geometry)
 
def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.parasite_drag_fuselage.parasite_drag_fuselage (state, settings, geometry)
 
def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.parasite_drag_propulsor.parasite_drag_propulsor (state, settings, geometry)
 
def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.parasite_drag_wing.parasite_drag_wing (state, settings, geometry)
 
def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.parasite_total.parasite_total (state, settings, geometry)
 
def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.total_aircraft.total_aircraft (state, settings, geometry)
 total_aircraft_drag.py More...
 
def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.trim.trim (state, settings, geometry)
 
def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.untrimmed.untrimmed (state, settings, geometry)
 untrimmed.py More...
 
def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.wave_drag_body_of_rev.wave_drag_body_of_rev (total_length, Rmax, Sref)
 wave_drag_body_of_rev.py More...
 
def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.wave_drag_lift.wave_drag_lift (conditions, configuration, wing)
 
def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.wave_drag_volume.wave_drag_volume (conditions, configuration, wing)
 
-

Detailed Description

-

Functions to perform low-fidelity drag calculations including supersonic.

-

Function Documentation

- -

◆ compressibility_drag_total()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.compressibility_drag_total.compressibility_drag_total ( state,
 settings,
 geometry 
)
-
-
Computes compressibility drag for full aircraft
-
-Assumptions:
-Drag is only calculated for the wings, main fuselage, and propulsors
-Main fuselage must have tag 'fuselage'
-No lift on wings other than main wing
-
-Source:
-adg.stanford.edu (Stanford AA241 A/B Course Notes)
-
-Inputs:
-state.conditions.aerodynamics.lift_breakdown.compressible_wings  [Unitless]
-state.conditions.freestream.mach_number                          [Unitless]
-geometry.wings                             
-geometry.fuselages['fuselage'].length_total                      [m]
-geometry.fuselages['fuselage'].effective_diameter                [m]
-geometry.propulsors[geometry.propulsors.keys()[0]].
-  nacelle_diameter                                               [m]
-  engine_length                                                  [m]
-  number_of_engines                                              [m]
-
-Outputs:
-total_compressibility_drag                                       [Unitless]
-
-Properties Used:
-N/A
-
-
-
- -

◆ compressible_mixed_flat_plate()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.compressible_mixed_flat_plate.compressible_mixed_flat_plate ( Re,
 Ma,
 Tc,
 xt 
)
-
-
Computes the coefficient of friction for a flat plate given the 
-input parameters. Also returns the correction terms used in the
-computation.
-
-Assumptions:
-Reynolds number between 10e5 and 10e9
-xt between 0 and 1
-
-Source:
-adg.stanford.edu (Stanford AA241 A/B Course Notes)
-
-Inputs:
-Re (Reynolds number)                                             [Unitless]
-Ma (Mach number)                                                 [Unitless]
-Tc (temperature)                                                 [K]
-xt (turbulent transition point as a proportion of chord length)  [Unitless]
-
-Outputs:
-cf_comp (coefficient of friction)                                [Unitless]
-k_comp (compressibility correction)                              [Unitless]
-k_reyn (Reynolds number correction)                              [Unitless]
-
-Properties Used:
-N/A
-
-
-
- -

◆ compressible_turbulent_flat_plate()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.compressible_turbulent_flat_plate.compressible_turbulent_flat_plate ( Re,
 Ma,
 Tc 
)
-
-
Computes the coefficient of friction for a flat plate given the 
-input parameters. Also returns the correction terms used in the
-computation.
-
-Assumptions:
-Reynolds number between 10e5 and 10e9
-Fully turbulent
-
-Source:
-adg.stanford.edu (Stanford AA241 A/B Course Notes)
-
-Inputs:
-Re (Reynolds number)                                             [Unitless]
-Ma (Mach number)                                                 [Unitless]
-Tc (temperature)                                                 [K]
-
-Outputs:
-cf_comp (coefficient of friction)                                [Unitless]
-k_comp (compressibility correction)                              [Unitless]
-k_reyn (Reynolds number correction)                              [Unitless]
-
-Properties Used:
-N/A
-
-
-
- -

◆ compute_aircraft_drag()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.compute_aircraft_drag.compute_aircraft_drag ( conditions,
 configuration,
 geometry = None 
)
-
- -

compute_aircraft_drag.py

-

Created: Dec 2013, A. Variyar Modified: Aug 2014, T. MacDonald Jan 2016, E. Botero

Unused function
-
-
-
- -

◆ drag_div()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.compressibility_drag_total.drag_div ( Mc_ii,
 wing,
 k,
 cl,
 Sref_main 
)
-
-
Use drag divergence mach number to determine drag for subsonic speeds
-
-Assumptions:
-Basic fit, subsonic
-
-Source:
-adg.stanford.edu (Stanford AA241 A/B Course Notes)
-
-Inputs:
-wing.
-  thickness_to_chord    [Unitless]     
-  sweeps.quarter_chord  [radians]
-  high_mach             [Boolean]
-  areas.reference       [m^2]
-
-Outputs:
-cd_c                    [Unitless]
-mcc                     [Unitless]
-MDiv                    [Unitless]
-
-Properties Used:
-N/A
-
-
-
- -

◆ induced_drag_aircraft()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.induced_drag_aircraft.induced_drag_aircraft ( state,
 settings,
 geometry 
)
-
-
Determines induced drag for the full aircraft
-
-Assumptions:
-Based on fits
-
-Source:
-adg.stanford.edu (Stanford AA241 A/B Course Notes)
-
-Inputs:
-state.conditions.aerodynamics.lift_coefficient               [Unitless]
-state.conditions.aerodynamics.drag_breakdown.parasite.total  [Unitless]
-configuration.oswald_efficiency_factor                       [Unitless]
-configuration.viscous_lift_dependent_drag_factor             [Unitless]
-geometry.wings['main_wing'].span_efficiency                  [Unitless]
-geometry.wings['main_wing'].aspect_ratio                     [Unitless]
-
-Outputs:
-total_induced_drag                                           [Unitless]
-
-Properties Used:
-N/A
-
-
-
- -

◆ miscellaneous_drag_aircraft()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.miscellaneous_drag_aircraft.miscellaneous_drag_aircraft ( state,
 settings,
 geometry 
)
-
-
Computes the miscellaneous drag associated with an aircraft
-
-Assumptions:
-Basic fit
-
-Source:
-adg.stanford.edu (Stanford AA241 A/B Course Notes)
-
-Inputs:
-configuration.trim_drag_correction_factor  [Unitless]
-geometry.propulsors.nacelle_diameter       [m]
-geometry.reference_area                    [m^2]
-geometry.wings['main_wing'].aspect_ratio   [Unitless]
-state.conditions.freestream.mach_number    [Unitless] (actual values are not used)
-
-Outputs:
-total_miscellaneous_drag                   [Unitless]
-
-Properties Used:
-N/A
-
-
-
- -

◆ parasite_drag_aircraft()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.parasite_drag_aircraft.parasite_drag_aircraft ( conditions,
 configuration,
 geometry 
)
-
-
Sums component parasite drag
-
-Assumptions:
-None
-
-Source:
-None
-
-Inputs:
-geometry.reference_area                             [m^2]
-geometry.wings.areas.reference                      [m^2]
-geometry.fuselages.areas.front_projected            [m^2]
-geometry.propulsors.number_of_engines               [Unitless]
-geometry.propulsors.nacelle_diameter                [m]
-conditions.aerodynamics.drag_breakdown.
-  parasite[wing.tag].parasite_drag_coefficient      [Unitless]
-  parasite[fuselage.tag].parasite_drag_coefficient  [Unitless]
-  parasite[propulsor.tag].parasite_drag_coefficient [Unitless]
-
-
-Outputs:
-total_parasite_drag                                                                      [Unitless]
-
-Properties Used:
-N/A
-
-
-
- -

◆ parasite_drag_fuselage()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.parasite_drag_fuselage.parasite_drag_fuselage ( state,
 settings,
 geometry 
)
-
-
Computes the parasite drag due to the fuselage
-
-Assumptions:
-Basic fit
-
-Source:
-adg.stanford.edu (Stanford AA241 A/B Course Notes)
-
-Inputs:
-state.conditions.freestream.
-  mach_number                                [Unitless]
-  temperature                                [K]
-  reynolds_number                            [Unitless]
-settings.fuselage_parasite_drag_form_factor  [Unitless]
-geometry.fuselage.       
-  areas.front_projected                      [m^2]
-  areas.wetted                               [m^2]
-  lengths.total                              [m]
-  effective_diameter                         [m]
-
-Outputs:
-fuselage_parasite_drag                       [Unitless]
-
-Properties Used:
-N/A
-
-
-
- -

◆ parasite_drag_propulsor()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.parasite_drag_propulsor.parasite_drag_propulsor ( state,
 settings,
 geometry 
)
-
-
Computes the parasite drag due to the propulsor
-
-Assumptions:
-Basic fit
-
-Source:
-Raymer equation (pg 283 of Aircraft Design: A Conceptual Approach) (subsonic)
-http://adg.stanford.edu/aa241/drag/BODYFORMFACTOR.HTML (supersonic)
-
-Inputs:
-state.conditions.freestream.
-  mach_number                                [Unitless]
-  temperature                                [K]
-  reynolds_number                            [Unitless]
-geometry.      
-  nacelle_diameter                           [m^2]
-  areas.wetted                               [m^2]
-  engine_length                              [m]
-state.conditions.aerodynamics.drag_breakdown.
-  compressible.main_wing.divergence_mach     [Unitless]
-
-Outputs:
-propulsor_parasite_drag                      [Unitless]
-
-Properties Used:
-N/A
-
-
-
- -

◆ parasite_drag_wing()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.parasite_drag_wing.parasite_drag_wing ( state,
 settings,
 geometry 
)
-
-
Computes the parasite drag due to wings
-
-Assumptions:
-Basic fit
-
-Source:
-adg.stanford.edu (Stanford AA241 A/B Course Notes)
-
-Inputs:
-settings.wing_parasite_drag_form_factor      [Unitless]
-state.conditions.freestream.
-  mach_number                                [Unitless]
-  temperature                                [K]
-  reynolds_number                            [Unitless]
-geometry.
-  areas.reference                            [m^2]
-  chords.mean_aerodynamic                    [m]
-  thickness_to_chord                         [Unitless]
-  sweeps.quarter_chord                       [radians]
-  aspect_ratio                               [Unitless]
-  spans.projected                            [m]
-  areas.exposed                              [m^2]
-  areas.affected                             [m^2]
-  areas.wetted                               [m^2]
-  transition_x_upper                         [Unitless]
-  transition_x_lower                         [Unitless]
-
-
-Outputs:
-wing_parasite_drag                           [Unitless]
-
-Properties Used:
-N/A
-
-
-
- -

◆ parasite_total()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.parasite_total.parasite_total ( state,
 settings,
 geometry 
)
-
-
Sums component parasite drag
-
-Assumptions:
-None
-
-Source:
-None
-
-Inputs:
-geometry.reference_area                             [m^2]
-geometry.wings.areas.reference                      [m^2]
-geometry.fuselages.areas.front_projected            [m^2]
-geometry.propulsors.number_of_engines               [Unitless]
-conditions.aerodynamics.drag_breakdown.
-  parasite[wing.tag].parasite_drag_coefficient      [Unitless]
-  parasite[fuselage.tag].parasite_drag_coefficient  [Unitless]
-  parasite[propulsor.tag].parasite_drag_coefficient [Unitless]
-
-
-Outputs:
-total_parasite_drag                                 [Unitless]
-
-Properties Used:
-N/A
-
-
-
- -

◆ total_aircraft()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.total_aircraft.total_aircraft ( state,
 settings,
 geometry 
)
-
- -

total_aircraft_drag.py

-

Created: Dec 2013, A. Variyar Modified: Feb 2014, A. Variyar, T. Lukaczyk, T. Orra Jan 2016, E. Botero

Computes the total drag for an aircraft
-
-Assumptions:
-None
-
-Source:
-None
-
-Inputs:
-state.conditions.aerodynamics.drag_breakdown.
-  trim_corrected_drag                    [Unitless]
-settings.drag_coefficient_increment      [Unitless]
-
-Outputs:
-aircraft_total_drag                      [Unitless]
-
-Properties Used:
-N/A
-
-
-
- -

◆ trim()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.trim.trim ( state,
 settings,
 geometry 
)
-
-
Adjusts aircraft drag based on a trim correction
-
-Assumptions:
-None
-
-Source:
-Unknown
-
-Inputs:
-settings.trim_drag_correction_factor                   [Unitless]
-state.conditions.aerodynamics.drag_breakdown.untrimmed [Unitless]
-
-Outputs:
-aircraft_total_drag_trim_corrected                     [Unitless]
-
-Properties Used:
-N/A
-
-
-
- -

◆ untrimmed()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.untrimmed.untrimmed ( state,
 settings,
 geometry 
)
-
- -

untrimmed.py

-

Created: Aug 2014, T. MacDonald Modified: Nov 2016, T. MacDonald

Sums aircraft drag before trim correction
-
-Assumptions:
-None
-
-Source:
-None
-
-Inputs:
-state.conditions.aerodynamics.drag_breakdown.
-  parasite.total                              [Unitless]
-  induced.total                               [Unitless]
-  compressible.total                          [Unitless]
-  miscellaneous.total                         [Unitless]
-
-Outputs:
-aircraft_untrimmed                            [Unitless]
-
-Properties Used:
-N/A
-
-
-
- -

◆ wave_drag()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.compressibility_drag_total.wave_drag ( conditions,
 configuration,
 main_fuselage,
 propulsor,
 wing,
 num_engines,
 k,
 Sref_main,
 flag105 
)
-
-
Use wave drag to determine compressibility drag for supersonic speeds
-
-Assumptions:
-Basic fit
-
-Source:
-adg.stanford.edu (Stanford AA241 A/B Course Notes)
-
-Inputs:
-conditions.freestream.mach_number            [Unitless]
-configuration
-main_fuselage (unused)
-propulsor     (unused)
-wing.areas.reference                         [m^2]
-num_engines   (unused)
-k             (tag for wing)                 [String]
-Sref_main (main reference area)              [m^2]
-flag105   (check if calcs are for Mach 1.05) [Boolean]
-
-
-Outputs:
-cd_c                    [Unitless]
-mcc                     [Unitless]
-MDiv                    [Unitless]
-
-Properties Used:
-N/A
-
-
-
- -

◆ wave_drag_body_of_rev() [1/2]

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.wave_drag_body_of_rev.wave_drag_body_of_rev ( total_length,
 Rmax,
 Sref 
)
-
- -

wave_drag_body_of_rev.py

-

Created: Jun 2014, T. Macdonald Modified: Jan 2016, E. Botero

Use wave drag to determine compressibility drag a body of revolution
-
-Assumptions:
-Corrected Sear-Haack body 
-
-Source:
-adg.stanford.edu (Stanford AA241 A/B Course Notes)
-
-Inputs:
-total_length                    [m]
-Rmax (max radius)               [m]
-Sref (main wing reference area) [m^2]
-
-Outputs:
-wave_drag_body_of_rev*1.15      [Unitless]
-
-Properties Used:
-N/A
-
-
-
- -

◆ wave_drag_body_of_rev() [2/2]

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.compressibility_drag_total.wave_drag_body_of_rev ( total_length,
 Rmax,
 Sref 
)
-
-
Use wave drag to determine compressibility drag a body of revolution
-
-Assumptions:
-Corrected Sear-Haack body 
-
-Source:
-adg.stanford.edu (Stanford AA241 A/B Course Notes)
-
-Inputs:
-total_length                    [m]
-Rmax (max radius)               [m]
-Sref (main wing reference area) [m^2]
-
-Outputs:
-wave_drag_body_of_rev*1.15      [Unitless]
-
-Properties Used:
-N/A
-
-
-
- -

◆ wave_drag_lift()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.wave_drag_lift.wave_drag_lift ( conditions,
 configuration,
 wing 
)
-
-
Computes wave drag due to lift
-
-Assumptions:
-Simplified equations
-
-Source:
-http://adg.stanford.edu/aa241/drag/ssdragcalc.html
-
-Inputs:
-conditions.freestream.mach_number        [Unitless]
-conditions.aerodynamics.lift_coefficient [Unitless]
-wing.total_length                        [m]
-wing.areas.reference                     [m^2]
-
-Outputs:
-wave_drag_lift                           [Unitless]
-
-Properties Used:
-N/A
-
-
-
- -

◆ wave_drag_volume()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.wave_drag_volume.wave_drag_volume ( conditions,
 configuration,
 wing 
)
-
-
Computes wave drag due to volume
-
-Assumptions:
-Simplified equations for wing
-
-Source:
-http://adg.stanford.edu/aa241/drag/ssdragcalc.html
-
-Inputs:
-conditions.freestream.mach_number        [Unitless]
-wing.thickness_to_chord                  [Unitless]
-wing.total_length                        [m]
-wing.areas.reference                     [m^2]
-
-Outputs:
-wave_drag_volume                         [Unitless]
-
-Properties Used:
-N/A
-
-
-
-
-
- - - - diff --git a/_site/doxygen/group__Methods-Aerodynamics-Supersonic__Zero-Drag.js b/_site/doxygen/group__Methods-Aerodynamics-Supersonic__Zero-Drag.js deleted file mode 100644 index b01513b5..00000000 --- a/_site/doxygen/group__Methods-Aerodynamics-Supersonic__Zero-Drag.js +++ /dev/null @@ -1,23 +0,0 @@ -var group__Methods_Aerodynamics_Supersonic__Zero_Drag = -[ - [ "compressibility_drag_total", "group__Methods-Aerodynamics-Supersonic__Zero-Drag.html#ga219e16acafc09082cf24afad213e82a3", null ], - [ "compressible_mixed_flat_plate", "group__Methods-Aerodynamics-Supersonic__Zero-Drag.html#gae028d793071e90526843e96073322abe", null ], - [ "compressible_turbulent_flat_plate", "group__Methods-Aerodynamics-Supersonic__Zero-Drag.html#gad4a3d80a2b0a3ed06b38b7ae54ed52cc", null ], - [ "compute_aircraft_drag", "group__Methods-Aerodynamics-Supersonic__Zero-Drag.html#gaa2f89ce4e9c94c24ebfeea083f5afedf", null ], - [ "drag_div", "group__Methods-Aerodynamics-Supersonic__Zero-Drag.html#gabe93280aa4a398fe7f4a846f320b6cfc", null ], - [ "induced_drag_aircraft", "group__Methods-Aerodynamics-Supersonic__Zero-Drag.html#gab4d68efaf1c50a05d83f084e6fec811f", null ], - [ "miscellaneous_drag_aircraft", "group__Methods-Aerodynamics-Supersonic__Zero-Drag.html#ga857987b93648989ca62534896beef377", null ], - [ "parasite_drag_aircraft", "group__Methods-Aerodynamics-Supersonic__Zero-Drag.html#ga0dc6cc8bc296b06ba06440ee91c7a936", null ], - [ "parasite_drag_fuselage", "group__Methods-Aerodynamics-Supersonic__Zero-Drag.html#ga6bc7488251858a1e1526f90cb0ff59cc", null ], - [ "parasite_drag_propulsor", "group__Methods-Aerodynamics-Supersonic__Zero-Drag.html#ga7d6bc8c6cc09e29a2ad852bea76a7318", null ], - [ "parasite_drag_wing", "group__Methods-Aerodynamics-Supersonic__Zero-Drag.html#ga25e58f6ecf24e75602421b9f16dc7763", null ], - [ "parasite_total", "group__Methods-Aerodynamics-Supersonic__Zero-Drag.html#gab05d24dd4747b0b10729b167c01c614c", null ], - [ "total_aircraft", "group__Methods-Aerodynamics-Supersonic__Zero-Drag.html#ga8e55ecce4122931457e1f450a95abf98", null ], - [ "trim", "group__Methods-Aerodynamics-Supersonic__Zero-Drag.html#ga27503e2b2183ed30137b281200c96650", null ], - [ "untrimmed", "group__Methods-Aerodynamics-Supersonic__Zero-Drag.html#gae62d8c47392754e9cd072b8fab7e97e7", null ], - [ "wave_drag", "group__Methods-Aerodynamics-Supersonic__Zero-Drag.html#ga72a66acea89fccf56d981b5e0c50ff91", null ], - [ "wave_drag_body_of_rev", "group__Methods-Aerodynamics-Supersonic__Zero-Drag.html#ga9e79d1f0b6914e56f64ca54283e787d2", null ], - [ "wave_drag_body_of_rev", "group__Methods-Aerodynamics-Supersonic__Zero-Drag.html#gac6d270a8abdc9f999bcbd75cfaf8a498", null ], - [ "wave_drag_lift", "group__Methods-Aerodynamics-Supersonic__Zero-Drag.html#ga725df02201031e5d83aa0f62ad26acfb", null ], - [ "wave_drag_volume", "group__Methods-Aerodynamics-Supersonic__Zero-Drag.html#ga610ad17cff3812c5993409c65a40df99", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Methods-Aerodynamics-Supersonic__Zero-Lift.html b/_site/doxygen/group__Methods-Aerodynamics-Supersonic__Zero-Lift.html deleted file mode 100644 index b885ce46..00000000 --- a/_site/doxygen/group__Methods-Aerodynamics-Supersonic__Zero-Lift.html +++ /dev/null @@ -1,354 +0,0 @@ - - - - - - - -SUAVE: Lift - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
-
- - - -
-
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-
-
- -
- -
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- - -
- -
- - -
- -

Functions to perform low-fidelity lift calculations for supersonics. -More...

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-Functions

def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Lift.aircraft_total.aircraft_total (state, settings, geometry)
 compute_aircraft_lift.py More...
 
def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Lift.fuselage_correction.fuselage_correction (state, settings, geometry)
 
def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Lift.vortex_lift.vortex_lift (state, settings, geometry)
 
def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Lift.wing_compressibility.wing_compressibility (state, settings, geometry)
 
-

Detailed Description

-

Functions to perform low-fidelity lift calculations for supersonics.

-

Function Documentation

- -

◆ aircraft_total()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Lift.aircraft_total.aircraft_total ( state,
 settings,
 geometry 
)
-
- -

compute_aircraft_lift.py

-

Created: Dec 2013, A. Variyar, Modified: Feb 2014, A. Variyar, T. Lukaczyk, T. Orra Apr 2014, A. Variyar Aug 2014, T. Macdonald Jan 2016, E. Botero

Returns total aircraft lift and stores values
-
-Assumptions:
-None
-
-Source:
-None
-
-Inputs:
-settings.fuselage_lift_correction  [Unitless]
-state.conditions.
-  freestream.mach_number           [Unitless]
-  aerodynamics.angle_of_attack     [radians]
-  aerodynamics.lift_coefficient    [Unitless]
-
-Outputs:
-aircraft_lift_total                [Unitless]
-
-Properties Used:
-N/A
-
-
-
- -

◆ fuselage_correction()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Lift.fuselage_correction.fuselage_correction ( state,
 settings,
 geometry 
)
-
-
Corrects aircraft lift based on fuselage effects
-
-Assumptions:
-None
-
-Source:
-adg.stanford.edu (Stanford AA241 A/B Course Notes)
-
-Inputs:
-settings.fuselage_lift_correction  [Unitless]
-state.conditions.
-  freestream.mach_number           [Unitless]
-  aerodynamics.angle_of_attack     [radians]
-  aerodynamics.lift_coefficient    [Unitless]
-
-Outputs:
-aircraft_lift_total                [Unitless]
-
-Properties Used:
-N/A
-
-
-
- -

◆ vortex_lift()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Lift.vortex_lift.vortex_lift ( state,
 settings,
 geometry 
)
-
-
Computes vortex lift
-
-Assumptions:
-wing capable of vortex lift
-
-Source:
-http://adg.stanford.edu/aa241/highlift/sstclmax.html
-
-Inputs:
-states.conditions.
-  freestream.mach_number              [-]
-  aerodynamics.angle_of_attack        [radians]
-  aerodynamics.lift_coefficient       [-]
-geometry.wings.*.aspect_ratio         [Unitless]
-geometry.wings.*.sweeps.quarter_chord [radians]
-
-Outputs:
-state.conditions.aerodynamics.
-  lift_breakdown.vortex_lift          [-] CL due to vortex lift
-wings_lift                            [-] Total CL at this point
-
-Properties Used:
-N/A
-
-
-
- -

◆ wing_compressibility()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Lift.wing_compressibility.wing_compressibility ( state,
 settings,
 geometry 
)
-
-
Corrects a wings lift based on compressibility, allow supersonic mach number
-
-Assumptions:
-wing capable of vortex lift
-
-Source:
-https://stanford.edu/~cantwell/AA200_Course_Material/AA200_Course_Notes/
-
-Inputs:
-settings.fuselage_lift_correction  [-]
-state.conditions.
-  freestream.mach_number           [-]
-  aerodynamics.angle_of_attack     [radians]
-  aerodynamics.lift_coefficient    [-]
-
-Outputs:
-state.conditions.aerodynamics.
-  lift_breakdown.compressible_wings [-] CL for the wings
-  lift_coefficient                  [-]
-wings_lift_comp                     [-]
-
-Properties Used:
-N/A
-
-
-
-
-
- - - - diff --git a/_site/doxygen/group__Methods-Aerodynamics-Supersonic__Zero-Lift.js b/_site/doxygen/group__Methods-Aerodynamics-Supersonic__Zero-Lift.js deleted file mode 100644 index 4003f1f6..00000000 --- a/_site/doxygen/group__Methods-Aerodynamics-Supersonic__Zero-Lift.js +++ /dev/null @@ -1,7 +0,0 @@ -var group__Methods_Aerodynamics_Supersonic__Zero_Lift = -[ - [ "aircraft_total", "group__Methods-Aerodynamics-Supersonic__Zero-Lift.html#ga6194e9c123af92b6c94e891c8031c06f", null ], - [ "fuselage_correction", "group__Methods-Aerodynamics-Supersonic__Zero-Lift.html#ga871e39e2de52770c340d4bc24f716d74", null ], - [ "vortex_lift", "group__Methods-Aerodynamics-Supersonic__Zero-Lift.html#gaf1caf451d7ebd8f7449065933f6e1bf5", null ], - [ "wing_compressibility", "group__Methods-Aerodynamics-Supersonic__Zero-Lift.html#ga16916def179bf2c8fb842f664aaefd36", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Methods-Aerodynamics-Supersonic__Zero.html b/_site/doxygen/group__Methods-Aerodynamics-Supersonic__Zero.html deleted file mode 100644 index 80718f46..00000000 --- a/_site/doxygen/group__Methods-Aerodynamics-Supersonic__Zero.html +++ /dev/null @@ -1,126 +0,0 @@ - - - - - - - -SUAVE: Supersonic_Zero - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
-
- - - -
-
- -
-
-
- -
- -
-
- - -
- -
- -
- -
-
Supersonic_Zero
-
-
- -

Functions to perform low-fidelity calculations including supersonics. -More...

- - - - - - - - -

-Modules

 Drag
 Functions to perform low-fidelity drag calculations including supersonic.
 
 Lift
 Functions to perform low-fidelity lift calculations for supersonics.
 
-

Detailed Description

-

Functions to perform low-fidelity calculations including supersonics.

-
-
- - - - diff --git a/_site/doxygen/group__Methods-Aerodynamics-Supersonic__Zero.js b/_site/doxygen/group__Methods-Aerodynamics-Supersonic__Zero.js deleted file mode 100644 index 85073599..00000000 --- a/_site/doxygen/group__Methods-Aerodynamics-Supersonic__Zero.js +++ /dev/null @@ -1,5 +0,0 @@ -var group__Methods_Aerodynamics_Supersonic__Zero = -[ - [ "Drag", "group__Methods-Aerodynamics-Supersonic__Zero-Drag.html", "group__Methods-Aerodynamics-Supersonic__Zero-Drag" ], - [ "Lift", "group__Methods-Aerodynamics-Supersonic__Zero-Lift.html", "group__Methods-Aerodynamics-Supersonic__Zero-Lift" ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Methods-Aerodynamics.html b/_site/doxygen/group__Methods-Aerodynamics.html deleted file mode 100644 index 1a725ed0..00000000 --- a/_site/doxygen/group__Methods-Aerodynamics.html +++ /dev/null @@ -1,138 +0,0 @@ - - - - - - - -SUAVE: Aerodynamics - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
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-
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- -
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Aerodynamics
-
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- -

Aerodynamic methods contain the functions for the aerodynamic analyses. -More...

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-Modules

 AERODAS
 Functions to perform calculations according to AERODAS models.
 
 AVL
 Functions to AVL calculations.
 
 Fidelity_Zero
 Functions to perform low-fidelity calculations.
 
 OpenVSP_Wave_Drag
 Functions to perform wave drag calculations using OpenVSP.
 
 SU2_Euler
 SU2_Euler contains the function needed to run the SU2 Euler Analysis.
 
 Supersonic_Zero
 Functions to perform low-fidelity calculations including supersonics.
 
-

Detailed Description

-

Aerodynamic methods contain the functions for the aerodynamic analyses.

-
-
- - - - diff --git a/_site/doxygen/group__Methods-Aerodynamics.js b/_site/doxygen/group__Methods-Aerodynamics.js deleted file mode 100644 index e2328ec1..00000000 --- a/_site/doxygen/group__Methods-Aerodynamics.js +++ /dev/null @@ -1,9 +0,0 @@ -var group__Methods_Aerodynamics = -[ - [ "AERODAS", "group__Methods-Aerodynamics-AERODAS.html", "group__Methods-Aerodynamics-AERODAS" ], - [ "AVL", "group__Methods-Aerodynamics-AVL.html", "group__Methods-Aerodynamics-AVL" ], - [ "Fidelity_Zero", "group__Methods-Aerodynamics-Fidelity__Zero.html", "group__Methods-Aerodynamics-Fidelity__Zero" ], - [ "OpenVSP_Wave_Drag", "group__Methods-Aerodynamics-OpenVSP__Wave__Drag.html", "group__Methods-Aerodynamics-OpenVSP__Wave__Drag" ], - [ "SU2_Euler", "group__Methods-Aerodynamics-SU2__Euler.html", "group__Methods-Aerodynamics-SU2__Euler" ], - [ "Supersonic_Zero", "group__Methods-Aerodynamics-Supersonic__Zero.html", "group__Methods-Aerodynamics-Supersonic__Zero" ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Methods-Center__of__Gravity.html b/_site/doxygen/group__Methods-Center__of__Gravity.html deleted file mode 100644 index 8360860f..00000000 --- a/_site/doxygen/group__Methods-Center__of__Gravity.html +++ /dev/null @@ -1,267 +0,0 @@ - - - - - - - -SUAVE: Center_of_Gravity - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
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Center_of_Gravity
-
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Description. -More...

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-Functions

def SUAVE.Methods.Center_of_Gravity.compute_aircraft_center_of_gravity.compute_aircraft_center_of_gravity (vehicle, nose_load_fraction=.06)
 
def SUAVE.Methods.Center_of_Gravity.compute_component_centers_of_gravity.compute_component_centers_of_gravity (vehicle, compute_propulsor_origin=False)
 
def SUAVE.Methods.Center_of_Gravity.compute_mission_center_of_gravity.compute_mission_center_of_gravity (vehicle, mission_fuel_weight)
 compute_mission_center_of_gravity.py More...
 
-

Detailed Description

-

Description.

-

Function Documentation

- -

◆ compute_aircraft_center_of_gravity()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Center_of_Gravity.compute_aircraft_center_of_gravity.compute_aircraft_center_of_gravity ( vehicle,
 nose_load_fraction = .06 
)
-
-
This computes the CG for the vehicle from the assigned vehicle mass 
-properties and locations
-    
-Assumptions:
-None
-    
-Source:
-N/A
-    
-Inputs:
-vehicle
-nose_load_fraction
-    
-Outputs:
-vehicle.mass_properties.center_of_gravity      [meters]
-    
-Properties Used:
-N/A
-
-
-
- -

◆ compute_component_centers_of_gravity()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Center_of_Gravity.compute_component_centers_of_gravity.compute_component_centers_of_gravity ( vehicle,
 compute_propulsor_origin = False 
)
-
-
computes the CG of all of the vehicle components based on correlations 
-from AA241
-
-Assumptions:
-None
-
-Source:
-AA 241 Notes
-
-Inputs:
-vehicle
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
-
- -

◆ compute_mission_center_of_gravity()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Center_of_Gravity.compute_mission_center_of_gravity.compute_mission_center_of_gravity ( vehicle,
 mission_fuel_weight 
)
-
- -

compute_mission_center_of_gravity.py

-

Created: Nov 2015, M. Vegh Modified: Jan 2016, E. Botero

computes the CG for the vehicle based on the mzfw cg of the
-vehicle, and an assigned fuel
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-vehicle 
-mission_fuel_weight           [Newtons]
-
-Outputs:
-cg                            [meters]
-
-Properties Used:
-N/A
-
-
-
-
-
- - - - diff --git a/_site/doxygen/group__Methods-Center__of__Gravity.js b/_site/doxygen/group__Methods-Center__of__Gravity.js deleted file mode 100644 index 71ecfaba..00000000 --- a/_site/doxygen/group__Methods-Center__of__Gravity.js +++ /dev/null @@ -1,6 +0,0 @@ -var group__Methods_Center__of__Gravity = -[ - [ "compute_aircraft_center_of_gravity", "group__Methods-Center__of__Gravity.html#gab07340ed39f8011a722913b0359beec9", null ], - [ "compute_component_centers_of_gravity", "group__Methods-Center__of__Gravity.html#gaa3b24268349627cb2f3db8131229b94f", null ], - [ "compute_mission_center_of_gravity", "group__Methods-Center__of__Gravity.html#gad04a471f2c790cce693dab0107e3f82b", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Methods-Costs-Industrial__Costs.html b/_site/doxygen/group__Methods-Costs-Industrial__Costs.html deleted file mode 100644 index 9999b32b..00000000 --- a/_site/doxygen/group__Methods-Costs-Industrial__Costs.html +++ /dev/null @@ -1,377 +0,0 @@ - - - - - - - -SUAVE: Industrial Costs - - - - - - - - - - - - - - - -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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Industrial Costs
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These functions provide cost estimates for an aircraft program. -More...

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-Functions

def SUAVE.Methods.Costs.Correlations.Industrial_Costs.compute_industrial_costs.compute_industrial_costs (vehicle)
 
def SUAVE.Methods.Costs.Correlations.Industrial_Costs.compute_industrial_costs.call_print (config)
 
def SUAVE.Methods.Costs.Correlations.Industrial_Costs.distribute_non_recurring_cost.distribute_non_recurring_cost (costs)
 
def SUAVE.Methods.Costs.Correlations.Industrial_Costs.estimate_escalation_factor.estimate_escalation_factor (reference_year)
 
def SUAVE.Methods.Costs.Correlations.Industrial_Costs.estimate_hourly_rates.estimate_hourly_rates (year)
 
-

Detailed Description

-

These functions provide cost estimates for an aircraft program.

-

Function Documentation

- -

◆ call_print()

- -
-
- - - - - - - - -
def SUAVE.Methods.Costs.Correlations.Industrial_Costs.compute_industrial_costs.call_print ( config)
-
-
Prints precalculated costs for an airplane program.
-
-Assumptions:
-N/A
-
-Source:
-N/A
-
-Inputs:
-config.tag                <string>
-config.costs.industrial.
-  non_recurring.total     [$]
-  unit_cost               [$]
-  recurring.total         [$]
-  production_total_units  [$]
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
-
- -

◆ compute_industrial_costs()

- -
-
- - - - - - - - -
def SUAVE.Methods.Costs.Correlations.Industrial_Costs.compute_industrial_costs.compute_industrial_costs ( vehicle)
-
-
Computes costs for design, development, test, and manufacturing of an airplane program
-
-Assumptions:
-Production tooling is considered a non-recurring cost
-
-Source:
-"Airplane Design, Part VIII - Airplane Cost Estimation", Roskam
-
-Inputs:
-vehicle.costs.industrial.        data dictionary with inputs for costs estimations:
-  reference_year                 [-]        reference date for calculations
-  production_total_units         [-]        total units to be produced
-  units_to_amortize              [-]        number of units to amortize development costs
-  prototypes_units               [-]        number of prototypes used in flight test campaign
-  avionics_cost                  [$]        user-informed avionics costs
-  test_facilities_cost           [$]        user-informed test facilities costs
-  manufacturing_facilities_cost  [$]        user-informed manufact. facilities costs
-  development_total_years        [-]        total years of development, for cash flow
-  aircraft_type                  <string>   for interior costs: 'military' or 'general aviation' or 'regional' or 'commercial' or 'business'.
-  difficulty_factor              [-]        1.0 for conventional tech., 1.5 for moderately advanc. tech., 2 for agressive use of adv. tech.
-  cad_factor                     [-]        1.2 for learning CAD, 1.0 for manual, 0.8 for experienced
-  stealth                        [-]        0 for non-stealth, 1 for stealth
-  material_factor                [-]        1.0 for conventional Al, 1.5 for stainless steel, 2~2.5 for composites, 3 for carbon fiber
-vehicle.mass_properties.empty    [kg]
-vehicle.propulsors.turbofan.
-  number_of_engines              [-]
-  sealevel_static_thrust         [N]
-vehicle.passengers               [-]
-
-Outputs:
-vehicle.costs.industrial.
-  unit_cost                      [$] total cost of each airplane produced
-  non_recurring.total            [$]
-  non_recurring.breakdown.       
-    airframe_engineering         [$]
-    development_support          [$]
-    flight_test                  [$]
-    engines                      [$]
-    avionics                     [$]
-    tooling_development          [$]
-    tooling_production           [$]
-    manufacturing_labor          [$]
-    manufacturing_material       [$]
-    quality_control              [$]
-    test_facilities              [$]
-    manufacturing_facilities     [$]
-    total                        [$]
-  recurring.total                [$]
-  recurring.breakdown.           
-    airframe_engineering         [$]
-    interior                     [$]
-    manufacturing_labor          [$]
-    manufacturing_material       [$]
-    quality_control              [$]
-    engines                      [$]
-    avionics                     [$]
-    total                        [$]
-
-Properties Used:
-N/A
-
-
-
- -

◆ distribute_non_recurring_cost()

- -
-
- - - - - - - - -
def SUAVE.Methods.Costs.Correlations.Industrial_Costs.distribute_non_recurring_cost.distribute_non_recurring_cost ( costs)
-
-
Distributes the non-recurring costs over the appropriate time period
-
-Assumptions:
-None
-
-Source:
-Markish, J., 'Valuation Techniques for Commercial Aircraft Program Design'
-
-Inputs:
-cost.industrial.
-  development_total_years        [-]        
-  non_recurring.breakdown.
-    airframe_engineering         [$]
-    development_support          [$]
-    flight_test                  [$]
-    engines                      [$]
-    avionics                     [$]
-    tooling_development          [$]
-    tooling_production           [$]
-    manufacturing_labor          [$]
-    manufacturing_material       [$]
-    quality_control              [$]
-    test_facilities              [$]
-    manufacturing_facilities     [$]
-
-Outputs:
-costs.industrial.non_recurring.cash_flow.:
-  breakdown.engineering          [$]
-  breakdown.manufacturing        [$]
-  breakdown.tooling_design       [$]
-  breakdown.tooling_production   [$]
-  breakdown.support              [$]
-  breakdown.facilities           [$]
-  total                          [$]
-
-Properties Used:
-N/A
-
-
-
- -

◆ estimate_escalation_factor()

- -
-
- - - - - - - - -
def SUAVE.Methods.Costs.Correlations.Industrial_Costs.estimate_escalation_factor.estimate_escalation_factor ( reference_year)
-
-
Estimates the escalation factor for a given year. Escalation is similar 
-to inflation but for a specific good.
-
-Assumptions:
-None
-
-Source:
-Historical data from United States Consumer Price Index
-
-Inputs:
-reference_year    [-]
-
-Outputs:
-escalation_factor [-]
-
-Properties Used:
-N/A
-
-
-
- -

◆ estimate_hourly_rates()

- -
-
- - - - - - - - -
def SUAVE.Methods.Costs.Correlations.Industrial_Costs.estimate_hourly_rates.estimate_hourly_rates ( year)
-
-
Estimates the hourly rate according to a trend line.
-
-Assumptions:
-None
-
-Source:
-Trends in hourly rates according to "Fundamentals of Aircraft Design", 
-  vol 1, Nicolai Figure 24.4.
-
-Inputs:
-year              [-]
-
-Outputs:
-hourly_rates.
-  engineering     [$/hr]
-  tooling         [$/hr]
-  manufacturing   [$/hr]
-  quality_control [$/hr]
-
-Properties Used:
-N/A
-
-
-
-
-
- - - - diff --git a/_site/doxygen/group__Methods-Costs-Industrial__Costs.js b/_site/doxygen/group__Methods-Costs-Industrial__Costs.js deleted file mode 100644 index 78cd4420..00000000 --- a/_site/doxygen/group__Methods-Costs-Industrial__Costs.js +++ /dev/null @@ -1,8 +0,0 @@ -var group__Methods_Costs_Industrial__Costs = -[ - [ "call_print", "group__Methods-Costs-Industrial__Costs.html#ga3d2583d564f60ad9654df204cef7e11a", null ], - [ "compute_industrial_costs", "group__Methods-Costs-Industrial__Costs.html#ga35a25c347a4527853d123de555e5cd38", null ], - [ "distribute_non_recurring_cost", "group__Methods-Costs-Industrial__Costs.html#ga227d25bf208e5c3af05ea5a76e853278", null ], - [ "estimate_escalation_factor", "group__Methods-Costs-Industrial__Costs.html#ga1370c8ef946e4c1e45e81b7d2f5d4139", null ], - [ "estimate_hourly_rates", "group__Methods-Costs-Industrial__Costs.html#ga65197d1d30198c75c0676e6f507c11c1", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Methods-Costs-Operating__Costs.html b/_site/doxygen/group__Methods-Costs-Operating__Costs.html deleted file mode 100644 index 957f2719..00000000 --- a/_site/doxygen/group__Methods-Costs-Operating__Costs.html +++ /dev/null @@ -1,142 +0,0 @@ - - - - - - - -SUAVE: Operating Costs - - - - - - - - - - - - - - - -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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Operating Costs
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def SUAVE.Methods.Costs.Correlations.Operating_Costs.compute_operating_costs.compute_operating_costs (vehicle)
 
-

Detailed Description

-

This is a stub for computing operating costs.

-

The function currently does nothing.

-

Function Documentation

- -

◆ compute_operating_costs()

- -
-
- - - - - - - - -
def SUAVE.Methods.Costs.Correlations.Operating_Costs.compute_operating_costs.compute_operating_costs ( vehicle)
-
-
This is a stub. It is called by the default costs analysis, but does nothing.
-
-
-
-
- - - - diff --git a/_site/doxygen/group__Methods-Costs-Operating__Costs.js b/_site/doxygen/group__Methods-Costs-Operating__Costs.js deleted file mode 100644 index 18669d00..00000000 --- a/_site/doxygen/group__Methods-Costs-Operating__Costs.js +++ /dev/null @@ -1,4 +0,0 @@ -var group__Methods_Costs_Operating__Costs = -[ - [ "compute_operating_costs", "group__Methods-Costs-Operating__Costs.html#gaa32e5999542fc0de24c94c102841b368", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Methods-Costs.html b/_site/doxygen/group__Methods-Costs.html deleted file mode 100644 index 7109191e..00000000 --- a/_site/doxygen/group__Methods-Costs.html +++ /dev/null @@ -1,127 +0,0 @@ - - - - - - - -SUAVE: Costs - - - - - - - - - - - - - - - -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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Costs
-
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This contains functions that can compute costs associated with building and operating an aircraft. -More...

- - - - - - - - -

-Modules

 Industrial Costs
 These functions provide cost estimates for an aircraft program.
 
 Operating Costs
 This is a stub for computing operating costs.
 
-

Detailed Description

-

This contains functions that can compute costs associated with building and operating an aircraft.

-

Currently there are modules for industrial cost and operating cost.

-
-
- - - - diff --git a/_site/doxygen/group__Methods-Costs.js b/_site/doxygen/group__Methods-Costs.js deleted file mode 100644 index ff40e538..00000000 --- a/_site/doxygen/group__Methods-Costs.js +++ /dev/null @@ -1,5 +0,0 @@ -var group__Methods_Costs = -[ - [ "Industrial Costs", "group__Methods-Costs-Industrial__Costs.html", "group__Methods-Costs-Industrial__Costs" ], - [ "Operating Costs", "group__Methods-Costs-Operating__Costs.html", "group__Methods-Costs-Operating__Costs" ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Methods-Flight__Dynamics-Dynamic__Stability-Approximations.html b/_site/doxygen/group__Methods-Flight__Dynamics-Dynamic__Stability-Approximations.html deleted file mode 100644 index 21b93b55..00000000 --- a/_site/doxygen/group__Methods-Flight__Dynamics-Dynamic__Stability-Approximations.html +++ /dev/null @@ -1,601 +0,0 @@ - - - - - - - -SUAVE: Approximations - - - - - - - - - - - - - - - -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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def SUAVE.Methods.Flight_Dynamics.Dynamic_Stability.Approximations.dutch_roll.dutch_roll (velocity, Cn_Beta, S_gross_w, density, span, I_z, Cn_r)
 
def SUAVE.Methods.Flight_Dynamics.Dynamic_Stability.Approximations.phugoid.phugoid (g, velocity, CD, CL)
 
def SUAVE.Methods.Flight_Dynamics.Dynamic_Stability.Approximations.roll.roll (I_x, S_gross_w, density, velocity, span, Cl_p)
 
def SUAVE.Methods.Flight_Dynamics.Dynamic_Stability.Approximations.short_period.short_period (velocity, density, S_gross_w, mac, Cm_q, Cz_alpha, mass, Cm_alpha, Iy, Cm_alpha_dot)
 
def SUAVE.Methods.Flight_Dynamics.Dynamic_Stability.Approximations.spiral.spiral (mass, velocity, density, S_gross_w, Cl_p, Cn_Beta, Cy_phi, Cl_Beta, Cn_r, Cl_r)
 spiral.py More...
 
-

Detailed Description

-

Function Documentation

- -

◆ dutch_roll()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Flight_Dynamics.Dynamic_Stability.Approximations.dutch_roll.dutch_roll ( velocity,
 Cn_Beta,
 S_gross_w,
 density,
 span,
 I_z,
 Cn_r 
)
-
-
This calculates the natural frequency and damping ratio for the 
-approximate dutch roll characteristics       
-
-Assumptions:
-    Major effect of rudder deflection is the generation of the Dutch roll mode.
-    Dutch roll mode only consists of sideslip and yaw
-    Beta = -Psi
-    Phi and its derivatives are zero
-    consider only delta_r input and Theta = 0
-    Neglect Cy_r
-    X-Z axis is plane of symmetry
-    Constant mass of aircraft
-    Origin of axis system at c.g. of aircraft
-    Aircraft is a rigid body
-    Earth is inertial reference frame
-    Perturbations from equilibrium are small
-    Flow is Quasisteady
-  
-Source:
-  J.H. Blakelock, "Automatic Control of Aircraft and Missiles" Wiley & Sons, Inc. New York, 1991, p 132-134.      
-  
-Inputs:
-    velocity - flight velocity at the condition being considered          [meters/seconds]
-    Cn_Beta - coefficient for change in yawing moment due to sideslip     [dimensionless]
-    S_gross_w - area of the wing                                          [meters**2]
-    density - flight density at condition being considered                [kg/meters**3]
-    span - wing span of the aircraft                                      [meters]
-    I_z - moment of interia about the body z axis                         [kg * meters**2]
-    Cn_r - coefficient for change in yawing moment due to yawing velocity [dimensionless]
-
-Outputs:
-    output - a data dictionary with fields:
-    dutch_w_n - natural frequency of the dutch roll mode                  [radian/second]
-    dutch_zeta - damping ratio of the dutch roll mode                     [dimensionless]
- 
-Properties Used:
-    N/A                    
-
-
-
- -

◆ phugoid()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Flight_Dynamics.Dynamic_Stability.Approximations.phugoid.phugoid ( g,
 velocity,
 CD,
 CL 
)
-
-
This calculates the natural frequency and damping ratio for the approximate 
-phugoid characteristics       
-
-Assumptions:
-    constant angle of attack
-    theta changes very slowly
-    Inertial forces are neglected
-    Neglect Cz_q
-    Theta = 0
-    X-Z axis is plane of symmetry
-    Constant mass of aircraft
-    Origin of axis system at c.g. of aircraft
-    Aircraft is a rigid body
-    Earth is inertial reference frame
-    Perturbations from equilibrium are small
-    Flow is Quasisteady 
-    
-Source:
-    J.H. Blakelock, "Automatic Control of Aircraft and Missiles" Wiley & Sons, Inc. New York, 1991, p 50-53.
-    
-Inputs:
-    g - gravitational constant                                   [meters/second**2]
-    velocity - flight velocity at the condition being considered [meters/seconds]
-    CD - coefficient of drag                                     [dimensionless]
-    CL - coefficient of lift                                     [dimensionless]
-
-Outputs:
-    output - a data dictionary with fields:
-        phugoid_w_n - natural frequency of the phugoid mode      [radian/second]
-        phugoid_zeta - damping ratio of the phugoid mode         [dimensionless]
-               
-Properties Used:
-    N/A  
-
-
-
- -

◆ roll()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Flight_Dynamics.Dynamic_Stability.Approximations.roll.roll ( I_x,
 S_gross_w,
 density,
 velocity,
 span,
 Cl_p 
)
-
-
This calculates the approximate time constant for the roll mode       
-
-Assumptions:
-   Only the rolling moment equation is needed from the Lateral-Directional equations
-   Sideslip and yaw angle are being neglected and thus set to be zero.
-   delta_r = 0
-   X-Z axis is plane of symmetry
-   Constant mass of aircraft
-   Origin of axis system at c.g. of aircraft
-   Aircraft is a rigid body
-   Earth is inertial reference frame
-   Perturbations from equilibrium are small
-   Flow is Quasisteady
-   
-Source:
-   J.H. Blakelock, "Automatic Control of Aircraft and Missiles" Wiley & Sons, Inc. New York, 1991, p 134-135.
-   
-Inputs:
-   I_x -  moment of interia about the body x axis [kg * meters**2]
-   S_gross_w - area of the wing [meters**2]
-   density - flight density at condition being considered [kg/meters**3]
-   span - wing span of the aircraft [meters]
-   velocity - flight velocity at the condition being considered [meters/seconds]
-   Cl_p - change in rolling moment due to the rolling velocity [dimensionless]
-   
-Outputs:
-   roll_tau - approximation of the time constant of the roll mode of an aircraft [seconds] (positive values are bad)
-
-Properties Used:
-   N/A         
-
-
-
- -

◆ short_period()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Flight_Dynamics.Dynamic_Stability.Approximations.short_period.short_period ( velocity,
 density,
 S_gross_w,
 mac,
 Cm_q,
 Cz_alpha,
 mass,
 Cm_alpha,
 Iy,
 Cm_alpha_dot 
)
-
-
This calculates the natural frequency and damping ratio for the approximate short
-period characteristics        
-        
-Assumptions:
-    X-Z axis is plane of symmetry
-    Constant mass of aircraft
-    Origin of axis system at c.g. of aircraft
-    Aircraft is a rigid body
-    Earth is inertial reference frame
-    Perturbations from equilibrium are small
-    Flow is Quasisteady
-    Constant forward airspeed
-    Neglect Cz_alpha_dot and Cz_q
-    Theta = 0
-    
-Source:
-    J.H. Blakelock, "Automatic Control of Aircraft and Missiles" Wiley & Sons, Inc. New York, 1991, p 46-50.
-    
-Inputs:
-    velocity - flight velocity at the condition being considered                                          [meters/seconds]
-    density - flight density at condition being considered                                                [kg/meters**3]
-    S_gross_w - area of the wing                                                                          [meters**2]
-    mac - mean aerodynamic chord of the wing                                                              [meters]
-    Cm_q - coefficient for the change in pitching moment due to pitch rate                                [dimensionless]
-    Cz_alpha - coefficient for the change in Z force due to the angle of attack                           [dimensionless]
-    mass - mass of the aircraft                                                                           [kilograms]
-    Cm_alpha - coefficient for the change in pitching moment due to angle of attack                       [dimensionless]
-    Iy - moment of interia about the body y axis                                                          [kg * meters**2]
-    Cm_alpha_dot - coefficient for the change in pitching moment due to rate of change of angle of attack [dimensionless]
-
-Outputs:
-    output - a data dictionary with fields:
-    w_n - natural frequency of the short period mode                                                      [radian/second]
-    zeta - damping ratio of the short period mode                                                         [dimensionless]
-
-Properties Used:
-    N/A          
-
-
-
- -

◆ spiral()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Flight_Dynamics.Dynamic_Stability.Approximations.spiral.spiral ( mass,
 velocity,
 density,
 S_gross_w,
 Cl_p,
 Cn_Beta,
 Cy_phi,
 Cl_Beta,
 Cn_r,
 Cl_r 
)
-
- -

spiral.py

-

Created: Apr 2014, A. Wendorff Modified: Jan 2016, E. Botero

This calcualtes the approximate time constant for the spiral mode         
-  
-Assumptions:
-    Linearized equations of motion
-    X-Z axis is plane of symmetry
-    Constant mass of aircraft
-    Origin of axis system at c.g. of aircraft
-    Aircraft is a rigid body
-    Earth is inertial reference frame
-    Perturbations from equilibrium are small
-    Flow is Quasisteady      
-               
-Source:
-    J.H. Blakelock, "Automatic Control of Aircraft and Missiles" Wiley & Sons, Inc. New York, 1991, p 142.        
-    
-Inputs:
-    mass - mass of the aircraft                                            [kilograms]
-    velocity - flight velocity at the condition being considered           [meters/seconds]
-    density - flight density at condition being considered                 [kg/meters**3]
-    S_gross_w - area of the wing                                           [meters**2]
-    Cl_p - change in rolling moment due to the rolling velocity            [dimensionless]
-    Cn_Beta - coefficient for change in yawing moment due to sideslip      [dimensionless]
-    Cy_phi - coefficient for change in sideforce due to aircraft roll      [dimensionless] (Usually equals C_L)
-    Cl_Beta - coefficient for change in rolling moment due to sideslip     [dimensionless]
-    Cn_r - coefficient for change in yawing moment due to yawing velocity  [dimensionless]
-    Cl_r - coefficient for change in rolling moment due to yawing velocity [dimensionless] (Usually equals C_L/4)
-
-Outputs:
-    spiral_tau - time constant for the spiral mode                         [seconds] (positive values are bad)
- 
-Properties Used:
-    N/A           
-
-
-
-
-
- - - - diff --git a/_site/doxygen/group__Methods-Flight__Dynamics-Dynamic__Stability-Approximations.js b/_site/doxygen/group__Methods-Flight__Dynamics-Dynamic__Stability-Approximations.js deleted file mode 100644 index ba750d39..00000000 --- a/_site/doxygen/group__Methods-Flight__Dynamics-Dynamic__Stability-Approximations.js +++ /dev/null @@ -1,8 +0,0 @@ -var group__Methods_Flight__Dynamics_Dynamic__Stability_Approximations = -[ - [ "dutch_roll", "group__Methods-Flight__Dynamics-Dynamic__Stability-Approximations.html#ga31ade80e6cc5c5bc4f5dffa28ca2e22d", null ], - [ "phugoid", "group__Methods-Flight__Dynamics-Dynamic__Stability-Approximations.html#ga4bdfc55722a023f2b375c4865787fe75", null ], - [ "roll", "group__Methods-Flight__Dynamics-Dynamic__Stability-Approximations.html#gab0ce29027729a1ed25a6594625a87ef9", null ], - [ "short_period", "group__Methods-Flight__Dynamics-Dynamic__Stability-Approximations.html#gac683f1cb317464cbed0d12b979774e55", null ], - [ "spiral", "group__Methods-Flight__Dynamics-Dynamic__Stability-Approximations.html#gaf046624c9794e72f3a8924c0da70768b", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Methods-Flight__Dynamics-Dynamic__Stability-Full__Linearized__Equations-Supporting__Functions.html b/_site/doxygen/group__Methods-Flight__Dynamics-Dynamic__Stability-Full__Linearized__Equations-Supporting__Functions.html deleted file mode 100644 index 56b59e38..00000000 --- a/_site/doxygen/group__Methods-Flight__Dynamics-Dynamic__Stability-Full__Linearized__Equations-Supporting__Functions.html +++ /dev/null @@ -1,865 +0,0 @@ - - - - - - - -SUAVE: Supporting_Functions - - - - - - - - - - - - - - - -
-
- - - - - - - - -
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SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
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-Functions

def SUAVE.Methods.Flight_Dynamics.Dynamic_Stability.Full_Linearized_Equations.Supporting_Functions.cl_beta.cl_beta (geometry, cl_p)
 cl_beta.py More...
 
def SUAVE.Methods.Flight_Dynamics.Dynamic_Stability.Full_Linearized_Equations.Supporting_Functions.cl_p.cl_p (cl_alpha, geometry)
 cl_p.py More...
 
def SUAVE.Methods.Flight_Dynamics.Dynamic_Stability.Full_Linearized_Equations.Supporting_Functions.cl_r.cl_r (cLw)
 cl_r.py More...
 
def SUAVE.Methods.Flight_Dynamics.Dynamic_Stability.Full_Linearized_Equations.Supporting_Functions.cm_alphadot.cm_alphadot (cm_i, ep_alpha, l_t, mac)
 cm_alphadot.py More...
 
def SUAVE.Methods.Flight_Dynamics.Dynamic_Stability.Full_Linearized_Equations.Supporting_Functions.cm_q.cm_q (cm_i, l_t, mac)
 cm_q.py More...
 
def SUAVE.Methods.Flight_Dynamics.Dynamic_Stability.Full_Linearized_Equations.Supporting_Functions.cn_p.cn_p (cLw, depdalpha)
 cn_p.py More...
 
def SUAVE.Methods.Flight_Dynamics.Dynamic_Stability.Full_Linearized_Equations.Supporting_Functions.cn_r.cn_r (cDw, Sv, Sref, l_v, span, eta_v, cLv_alpha)
 cn_r.py More...
 
def SUAVE.Methods.Flight_Dynamics.Dynamic_Stability.Full_Linearized_Equations.Supporting_Functions.cx_alpha.cx_alpha (cL, cL_alpha)
 cx_alpha.py More...
 
def SUAVE.Methods.Flight_Dynamics.Dynamic_Stability.Full_Linearized_Equations.Supporting_Functions.cx_u.cx_u (cD)
 cx_u.py More...
 
def SUAVE.Methods.Flight_Dynamics.Dynamic_Stability.Full_Linearized_Equations.Supporting_Functions.cy_phi.cy_phi (CL)
 cy_phi.py More...
 
def SUAVE.Methods.Flight_Dynamics.Dynamic_Stability.Full_Linearized_Equations.Supporting_Functions.cz_alphadot.cz_alphadot (cm_i, ep_alpha)
 cz_alphadot.py More...
 
def SUAVE.Methods.Flight_Dynamics.Dynamic_Stability.Full_Linearized_Equations.Supporting_Functions.cz_q.cz_q (cm_i)
 cz_q.py More...
 
def SUAVE.Methods.Flight_Dynamics.Dynamic_Stability.Full_Linearized_Equations.Supporting_Functions.cz_u.cz_u (cL, U, cL_u=0)
 cz_u.py More...
 
def SUAVE.Methods.Flight_Dynamics.Dynamic_Stability.Full_Linearized_Equations.Supporting_Functions.ep_alpha.ep_alpha (cL_w_alpha, Sref, span)
 
-

Detailed Description

-

Function Documentation

- -

◆ cl_beta()

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- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Flight_Dynamics.Dynamic_Stability.Full_Linearized_Equations.Supporting_Functions.cl_beta.cl_beta ( geometry,
 cl_p 
)
-
- -

cl_beta.py

-

Created: Aug 2016, A. van Korlaar Modified: Aug 2016, L. Kulik

THis calculates the derivative of roll rate with respect 
-to sideslip (dihedral effect)
-Assumptions: 
-None: 
-
-Source:
-STABILITY, USAF. "Control Datcom." Air Force Flight Dynamics Laboratory, 
-Wright-Patterson Air Force Base, Ohio (1972) 
-
-Inputs:
-dihedral    [radians]
-taper       [dimensionless]
-
-Outputs:
-cl_beta     [dimensionless]
-
-Properties Used:
-N/A
-
-
-
- -

◆ cl_p()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Flight_Dynamics.Dynamic_Stability.Full_Linearized_Equations.Supporting_Functions.cl_p.cl_p ( cl_alpha,
 geometry 
)
-
- -

cl_p.py

-

Created: Aug 2016, A. van Korlaar Modified: Aug 2016, L. Kulik

This calculates the derivative of rolling moment with respect 
-to roll rate
-
-Assumptions:
-None
-
-Source:
-STABILITY, USAF. "Control Datcom." Air Force Flight Dynamics 
-Laboratory, Wright-Patterson Air Force Base, Ohio (1972)
-
-Inputs:
-taper        [dimensionless]
-cl_alpha     [dimensionless]   
-
-Outputs:
-cl_p         [dimensionless]
-
-Properties Used:
-N/A
-
-
-
- -

◆ cl_r()

- -
-
- - - - - - - - -
def SUAVE.Methods.Flight_Dynamics.Dynamic_Stability.Full_Linearized_Equations.Supporting_Functions.cl_r.cl_r ( cLw)
-
- -

cl_r.py

-

Created: Jun 2014, A. Wendorff Modified: Jan 2016, E. Botero

This calculates the rolling moment coefficient with respect to
-perturbational angular rate around the z-body-axis        
-
-Assumptions:
-None
-
-Source:
-J.H. Blakelock, "Automatic Control of Aircraft and Missiles" 
-Wiley & Sons, Inc. New York, 1991, (pg 23
-
-Inputs:
-clw          [dimensionless]
-         
-Outputs:
-cl_r         [dimensionless]
-        
-Properties Used:
-N/A                
-
-
-
- -

◆ cm_alphadot()

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def SUAVE.Methods.Flight_Dynamics.Dynamic_Stability.Full_Linearized_Equations.Supporting_Functions.cm_alphadot.cm_alphadot ( cm_i,
 ep_alpha,
 l_t,
 mac 
)
-
- -

cm_alphadot.py

-

Created: Jun 2014, A. Wendorff Modified: Jan 2016, E. Botero

This calculates the pitching moment coefficient with respect to the 
-rate of change of the alpha of attack of the aircraft        
-
-Assumptions:
-None
-
-Source:
-J.H. Blakelock, "Automatic Control of Aircraft and Missiles" 
-Wiley & Sons, Inc. New York, 1991, (pg 23)
-
-Inputs:
-cm_i                [dimensionless]
-ep_alpha            [dimensionless]
-l_t                 [meters]
-mac                 [meters]
-         
-Outputs:
-cm_alphadot         [dimensionless]
-        
-Properties Used:
-N/A           
-
-
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- -

◆ cm_q()

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def SUAVE.Methods.Flight_Dynamics.Dynamic_Stability.Full_Linearized_Equations.Supporting_Functions.cm_q.cm_q ( cm_i,
 l_t,
 mac 
)
-
- -

cm_q.py

-

Created: Jun 2014, A. Wendorff Modified: Jan 2016, E. Botero

This calculates the damping in pitch coefficient        
-
-Assumptions:
-None
-
-Source:
-J.H. Blakelock, "Automatic Control of Aircraft and Missiles" 
-Wiley & Sons, Inc. New York, 1991, (pg 23)
-
-Inputs:
-cm_i                [dimensionless]
-l_t                 [meters]
-mac                 [meters]
-
-Outputs:
-cm_q                [dimensionless]
-
-Properties Used:
-N/A           
-
-
-
- -

◆ cn_p()

- -
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- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Flight_Dynamics.Dynamic_Stability.Full_Linearized_Equations.Supporting_Functions.cn_p.cn_p ( cLw,
 depdalpha 
)
-
- -

cn_p.py

-

Created: Jun 2014, A. Wendorff Modified: Jan 2016, E. Botero

This calculats the yawing moment coefficient with respect
-to perturbational angular rate around the x-body-axis            
-
-Assumptions:
-None
-
-Source:
-J.H. Blakelock, "Automatic Control of Aircraft and Missiles" 
-Wiley & Sons, Inc. New York, 1991, (pg 23)
-
-Inputs:
-clw          [dimensionless]
-dep_alpha    [dimensionless]
-         
-Outputs:
-cn_p         [dimensionless]
-        
-Properties Used:
-N/A           
-
-
-
- -

◆ cn_r()

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def SUAVE.Methods.Flight_Dynamics.Dynamic_Stability.Full_Linearized_Equations.Supporting_Functions.cn_r.cn_r ( cDw,
 Sv,
 Sref,
 l_v,
 span,
 eta_v,
 cLv_alpha 
)
-
- -

cn_r.py

-

Created: Jun 2014, A. Wendorff Modified: Jan 2016, E. Botero

This calculats the yawing moment coefficient with respect to 
-perturbational angular rate around the z-body-axis           
-
-Assumptions:
-None
-
-Source:
-J.H. Blakelock, "Automatic Control of Aircraft and Missiles" 
-Wiley & Sons, Inc. New York, 1991, (pg 23)
-
-Inputs:
-eta_v              [dimensionless]
-cDw                [dimensionless]
-l_v                [meters]
-span               [meters]
-Sref               [meters**2]
-Sv                 [meters**2]
-         
-Outputs:
-cn_r               [dimensionless]
-        
-Properties Used:
-N/A           
-
-
-
- -

◆ cx_alpha()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Flight_Dynamics.Dynamic_Stability.Full_Linearized_Equations.Supporting_Functions.cx_alpha.cx_alpha ( cL,
 cL_alpha 
)
-
- -

cx_alpha.py

-

Created: Jun 2014, A. Wendorff Modified: Jan 2016, E. Botero

This calculates the coefficient of force in the x direction
-with respect to the change in angle of attack of the aircraft        
-
-Assumptions:
-None
-
-Source:
-J.H. Blakelock, "Automatic Control of Aircraft and Missiles" 
-Wiley & Sons, Inc. New York, 1991, (pg 23)
-
-Inputs:
-cL              [dimensionless]
-cL_alpha        [dimensionless]
-         
-Outputs:
-cx_alpha        [dimensionless]
-        
-Properties Used:
-N/A                
-
-
-
- -

◆ cx_u()

- -
-
- - - - - - - - -
def SUAVE.Methods.Flight_Dynamics.Dynamic_Stability.Full_Linearized_Equations.Supporting_Functions.cx_u.cx_u ( cD)
-
- -

cx_u.py

-

Created: Jun 2014, A. Wendorff Modified: Jan 2016, E. Botero

This calculates the coefficient of force in the x direction
-with respect to the change in forward velocity of the aircraft        
-
-Assumptions:
-None
-
-Source:
-J.H. Blakelock, "Automatic Control of Aircraft and Missiles" 
-Wiley & Sons, Inc. New York, 1991, (pg 23)
-
-Inputs:
-cD                  [dimensionless]
-
-Outputs:
-cx_u                [dimensionless]
-
-Properties Used:
-N/A           
-
-
-
- -

◆ cy_phi()

- -
-
- - - - - - - - -
def SUAVE.Methods.Flight_Dynamics.Dynamic_Stability.Full_Linearized_Equations.Supporting_Functions.cy_phi.cy_phi ( CL)
-
- -

cy_phi.py

-

Created: Jun 2014, A. Wendorff Modified: Jan 2016, E. Botero

This calculates the force coefficient in the y direction 
-with respect to the roll angle of the aircraft        
-
-Assumptions:
-None
-
-Source:
-J.H. Blakelock, "Automatic Control of Aircraft and Missiles" 
-Wiley & Sons, Inc. New York, 1991, (pg 23)
-
-Inputs:
-CL                [dimensionless]
-
-Outputs:
-cy_phi            [dimensionless]
-
-Properties Used:
-N/A           
-
-
-
- -

◆ cz_alphadot()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Flight_Dynamics.Dynamic_Stability.Full_Linearized_Equations.Supporting_Functions.cz_alphadot.cz_alphadot ( cm_i,
 ep_alpha 
)
-
- -

cz_alphadot.py

-

Created: Jun 2014, A. Wendorff Modified: Jan 2016, E. Botero

This calculates the coefficient of force in the z direction with 
-respect to the rate of change of the alpha of attack of the aircraft        
-
-Assumptions:
-None
-
-Source:
-J.H. Blakelock, "Automatic Control of Aircraft and Missiles" 
-Wiley & Sons, Inc. New York, 1991, (pg 23)
-
-Inputs:
-cm_i                       [dimensionless]
-ep_alpha                   [dimensionless]
-
-Outputs:
-cz_alphadot                [dimensionless]
-
-Properties Used:
-N/A           
-
-
-
- -

◆ cz_q()

- -
-
- - - - - - - - -
def SUAVE.Methods.Flight_Dynamics.Dynamic_Stability.Full_Linearized_Equations.Supporting_Functions.cz_q.cz_q ( cm_i)
-
- -

cz_q.py

-

Created: Jun 2014, A. Wendorff Modified: Jan 2016, E. Botero

This calculates the coefficient of force in the z direction 
-with respect to the rate of change of the alpha of attack of the aircraft        
-
-Assumptions:
-None
-
-Source:
-J.H. Blakelock, "Automatic Control of Aircraft and Missiles" 
-Wiley & Sons, Inc. New York, 1991, (pg 23)
-
-Inputs:
-cm_i                [dimensionless]
-
-Outputs:
-cz_q                [dimensionless]
-
-Properties Used:
-N/A           
-
-
-
- -

◆ cz_u()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Flight_Dynamics.Dynamic_Stability.Full_Linearized_Equations.Supporting_Functions.cz_u.cz_u ( cL,
 U,
 cL_u = 0 
)
-
- -

cz_u.py

-

Created: Jun 2014, A. Wendorff Modified: Jan 2016, E. Botero

This calculates the coefficient of force in the z direction
-with respect to the change in the forward velocity        
-
-Assumptions:
-None
-
-Source:
-J.H. Blakelock, "Automatic Control of Aircraft and Missiles" 
-Wiley & Sons, Inc. New York, 1991, (pg 23)
-
-Inputs:
-cL                 [dimensionless]
-U                  [meters/second]
-cL_u               
-
-Outputs:
-cz_u               [dimensionless]
-
-Properties Used:
-N/A           
-
-
-
- -

◆ ep_alpha()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Flight_Dynamics.Dynamic_Stability.Full_Linearized_Equations.Supporting_Functions.ep_alpha.ep_alpha ( cL_w_alpha,
 Sref,
 span 
)
-
-
Calculates the change in the downwash with change in 
-angle of attack         
-
-Assumptions:
-None
-
-Source:
-J.H. Blakelock, "Automatic Control of Aircraft and Missiles" 
-Wiley & Sons, Inc. New York, 1991, (pg 34)
-
-Inputs:
-span            [meters]
-Sref            [square meters]
-cL_w_alpha      [unitless]
-         
-Outputs:
-ep_alpha        [Unitless]
-        
-Properties Used:
-N/A                
-
-
-
-
-
- - - - diff --git a/_site/doxygen/group__Methods-Flight__Dynamics-Dynamic__Stability-Full__Linearized__Equations-Supporting__Functions.js b/_site/doxygen/group__Methods-Flight__Dynamics-Dynamic__Stability-Full__Linearized__Equations-Supporting__Functions.js deleted file mode 100644 index a5b70410..00000000 --- a/_site/doxygen/group__Methods-Flight__Dynamics-Dynamic__Stability-Full__Linearized__Equations-Supporting__Functions.js +++ /dev/null @@ -1,17 +0,0 @@ -var group__Methods_Flight__Dynamics_Dynamic__Stability_Full__Linearized__Equations_Supporting__Functions = -[ - [ "cl_beta", "group__Methods-Flight__Dynamics-Dynamic__Stability-Full__Linearized__Equations-Supporting__Functions.html#ga1bd50ffd8cd55aa0b71da7920c20329a", null ], - [ "cl_p", "group__Methods-Flight__Dynamics-Dynamic__Stability-Full__Linearized__Equations-Supporting__Functions.html#ga1a5ce3b547d39548f2518b7d0b6264c2", null ], - [ "cl_r", "group__Methods-Flight__Dynamics-Dynamic__Stability-Full__Linearized__Equations-Supporting__Functions.html#ga9c12c972a3c678bb9ab31081250c91cb", null ], - [ "cm_alphadot", "group__Methods-Flight__Dynamics-Dynamic__Stability-Full__Linearized__Equations-Supporting__Functions.html#gaf234fa19d8249426a03409ebc94fec24", null ], - [ "cm_q", "group__Methods-Flight__Dynamics-Dynamic__Stability-Full__Linearized__Equations-Supporting__Functions.html#ga64e8a40e0f7216e8fe500c7f730cb47a", null ], - [ "cn_p", "group__Methods-Flight__Dynamics-Dynamic__Stability-Full__Linearized__Equations-Supporting__Functions.html#ga9d56d78b211b08c5d0196e7d42d0a9fd", null ], - [ "cn_r", "group__Methods-Flight__Dynamics-Dynamic__Stability-Full__Linearized__Equations-Supporting__Functions.html#ga6092c143a38e833443e0a5589fe34230", null ], - [ "cx_alpha", "group__Methods-Flight__Dynamics-Dynamic__Stability-Full__Linearized__Equations-Supporting__Functions.html#gaf3a9163453e2581e06c163184574728a", null ], - [ "cx_u", "group__Methods-Flight__Dynamics-Dynamic__Stability-Full__Linearized__Equations-Supporting__Functions.html#ga0de14d339971da15d92050659247c276", null ], - [ "cy_phi", "group__Methods-Flight__Dynamics-Dynamic__Stability-Full__Linearized__Equations-Supporting__Functions.html#ga625055093f395be46c79aba09de8631e", null ], - [ "cz_alphadot", "group__Methods-Flight__Dynamics-Dynamic__Stability-Full__Linearized__Equations-Supporting__Functions.html#ga334e69f989781d88897470a54367a4d9", null ], - [ "cz_q", "group__Methods-Flight__Dynamics-Dynamic__Stability-Full__Linearized__Equations-Supporting__Functions.html#ga66926a44954158558688a2f96f1715a4", null ], - [ "cz_u", "group__Methods-Flight__Dynamics-Dynamic__Stability-Full__Linearized__Equations-Supporting__Functions.html#ga37f2ef9db3aee489aeffce9a8fec734b", null ], - [ "ep_alpha", "group__Methods-Flight__Dynamics-Dynamic__Stability-Full__Linearized__Equations-Supporting__Functions.html#ga991dffe8cd78ff98b7bd20f8c2ebbe64", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Methods-Flight__Dynamics-Dynamic__Stability-Full__Linearized__Equations.html b/_site/doxygen/group__Methods-Flight__Dynamics-Dynamic__Stability-Full__Linearized__Equations.html deleted file mode 100644 index 240882f9..00000000 --- a/_site/doxygen/group__Methods-Flight__Dynamics-Dynamic__Stability-Full__Linearized__Equations.html +++ /dev/null @@ -1,454 +0,0 @@ - - - - - - - -SUAVE: Full_Linearized_Equations - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
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Full_Linearized_Equations
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- - - - -

-Modules

 Supporting_Functions
 
- - - - - -

-Functions

def SUAVE.Methods.Flight_Dynamics.Dynamic_Stability.Full_Linearized_Equations.lateral_directional.lateral_directional (velocity, Cn_Beta, S_gross_w, density, span, I_z, Cn_r, I_x, Cl_p, J_xz, Cl_r, Cl_Beta, Cn_p, Cy_phi, Cy_psi, Cy_Beta, mass)
 
def SUAVE.Methods.Flight_Dynamics.Dynamic_Stability.Full_Linearized_Equations.longitudinal.longitudinal (velocity, density, S_gross_w, mac, Cm_q, Cz_alpha, mass, Cm_alpha, Iy, Cm_alpha_dot, Cz_u, Cz_alpha_dot, Cz_q, Cw, Theta, Cx_u, Cx_alpha)
 
-

Detailed Description

-

Function Documentation

- -

◆ lateral_directional()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Flight_Dynamics.Dynamic_Stability.Full_Linearized_Equations.lateral_directional.lateral_directional ( velocity,
 Cn_Beta,
 S_gross_w,
 density,
 span,
 I_z,
 Cn_r,
 I_x,
 Cl_p,
 J_xz,
 Cl_r,
 Cl_Beta,
 Cn_p,
 Cy_phi,
 Cy_psi,
 Cy_Beta,
 mass 
)
-
-
This calculates the natural frequency and damping ratio for the full linearized dutch 
-roll mode along with the time constants for the roll and spiral modes   
-
-Assumptions:
-    X-Z axis is plane of symmetry
-    Constant mass of aircraft
-    Origin of axis system at c.g. of aircraft
-    Aircraft is a rigid body
-    Earth is inertial reference frame
-    Perturbations from equilibrium are small
-    Flow is Quasisteady
-    Zero initial conditions
-    Neglect Cy_p and Cy_r
-    
-Source:
-    J.H. Blakelock, "Automatic Control of Aircraft and Missiles" Wiley & Sons, Inc. New York, 1991, p 118-124.
-    
-Inputs:
-    velocity - flight velocity at the condition being considered                          [meters/seconds]
-    Cn_Beta - coefficient for change in yawing moment due to sideslip                     [dimensionless] (no simple relation)
-    S_gross_w - area of the wing                                                          [meters**2]
-    density - flight density at condition being considered                                [kg/meters**3]
-    span - wing span of the aircraft                                                      [meters]
-    I_z - moment of interia about the body z axis                                         [kg * meters**2]
-    Cn_r - coefficient for change in yawing moment due to yawing velocity                 [dimensionless] ( - C_D(wing)/4 - 2 * Sv/S * (l_v/b)**2 * (dC_L/dalpha)(vert) * eta(vert))
-    I_x - moment of interia about the body x axis                                         [kg * meters**2]
-    Cl_p - change in rolling moment due to the rolling velocity                           [dimensionless] (no simple relation for calculation)
-    J_xz - products of inertia in the x-z direction                                       [kg * meters**2] (if X and Z lie in a plane of symmetry then equal to zero)
-    Cl_r - coefficient for change in rolling moment due to yawing velocity                [dimensionless] (Usually equals C_L(wing)/4)
-    Cl_Beta - coefficient for change in rolling moment due to sideslip                    [dimensionless] 
-    Cn_p - coefficient for the change in yawing moment due to rolling velocity            [dimensionless] (-C_L(wing)/8*(1 - depsilon/dalpha)) (depsilon/dalpha = 2/pi/e/AspectRatio dC_L(wing)/dalpha)
-    Cy_phi  - coefficient for change in sideforce due to aircraft roll                    [dimensionless] (Usually equals C_L)
-    Cy_psi - coefficient to account for gravity                                           [dimensionless] (C_L * tan(Theta))
-    Cy_Beta - coefficient for change in Y force due to sideslip                           [dimensionless] (no simple relation)
-    mass - mass of the aircraft                                                           [kilograms]
-
-Outputs:
-    output - a data dictionary with fields:
-    dutch_w_n - natural frequency of the dutch roll mode                                  [radian/second]
-    dutch_zeta - damping ratio of the dutch roll mode                                     [dimensionless]
-    roll_tau - approximation of the time constant of the roll mode of an aircraft         [seconds] (positive values are bad)
-    spiral_tau - time constant for the spiral mode                                        [seconds] (positive values are bad)
-
-Properties Used:
-    N/A         
-
-
-
- -

◆ longitudinal()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Flight_Dynamics.Dynamic_Stability.Full_Linearized_Equations.longitudinal.longitudinal ( velocity,
 density,
 S_gross_w,
 mac,
 Cm_q,
 Cz_alpha,
 mass,
 Cm_alpha,
 Iy,
 Cm_alpha_dot,
 Cz_u,
 Cz_alpha_dot,
 Cz_q,
 Cw,
 Theta,
 Cx_u,
 Cx_alpha 
)
-
-
This calculates the natural frequency and damping ratio for the full 
-linearized short period and phugoid modes        
-
-Assumptions:
-    X-Z axis is plane of symmetry
-    Constant mass of aircraft
-    Origin of axis system at c.g. of aircraft
-    Aircraft is a rigid body
-    Earth is inertial reference frame
-    Perturbations from equilibrium are small
-    Flow is Quasisteady
-    Zero initial conditions
-    Cm_a = CF_z_a = CF_x_a = 0
-    Neglect Cx_alpha_dot, Cx_q and Cm_u
-    
-Source:
-    J.H. Blakelock, "Automatic Control of Aircraft and Missiles" Wiley & Sons, Inc. New York, 1991, p 26-41.
-    
-Inputs:
-    velocity - flight velocity at the condition being considered                                          [meters/seconds]
-    density - flight density at condition being considered                                                [kg/meters**3]
-    S_gross_w - area of the wing                                                                          [meters**2]
-    mac - mean aerodynamic chord of the wing                                                              [meters]
-    Cm_q - coefficient for the change in pitching moment due to pitch rate                                [dimensionless] (2 * K * dC_m/di * lt/c where K is approximately 1.1)
-    Cz_alpha - coefficient for the change in Z force due to the angle of attack                           [dimensionless] (-C_D - dC_L/dalpha)
-    mass - mass of the aircraft                                                                           [kilograms]
-    Cm_alpha - coefficient for the change in pitching moment due to angle of attack                       [dimensionless] (dC_m/dC_L * dCL/dalpha)
-    Iy - moment of interia about the body y axis                                                          [kg * meters**2]
-    Cm_alpha_dot - coefficient for the change in pitching moment due to rate of change of angle of attack [dimensionless] (2 * dC_m/di * depsilon/dalpha * lt/mac)
-    Cz_u - coefficient for the change in force in the Z direction due to change in forward velocity       [dimensionless] (usually -2 C_L or -2C_L - U dC_L/du)
-    Cz_alpha_dot - coefficient for the change of angle of attack caused by w_dot on the Z force           [dimensionless] (2 * dC_m/di * depsilon/dalpha)
-    Cz_q - coefficient for the change in Z force due to pitching velocity                                 [dimensionless] (2 * K * dC_m/di where K is approximately 1.1)
-    Cw - coefficient to account for gravity                                                               [dimensionless] (-C_L)
-    Theta - angle between the horizontal axis and the body axis measured in the vertical plane            [radians]
-    Cx_u - coefficient for the change in force in the X direction due to change in the forward velocity   [dimensionless] (-2C_D)
-    Cx_alpha - coefficient for the change in force in the X direction due to the change in angle of attack caused by w [dimensionless] (C_L-dC_L/dalpha)
-
-Outputs:
-    output - a data dictionary with fields:
-        short_w_n - natural frequency of the short period mode                                            [radian/second]
-        short_zeta - damping ratio of the short period mode                                               [dimensionless]
-        phugoid_w_n - natural frequency of the short period mode                                          [radian/second]
-        phugoid_zeta - damping ratio of the short period mode                                             [dimensionless]
-    
-Properties Used:
-N/A  
-
-
-
-
-
- - - - diff --git a/_site/doxygen/group__Methods-Flight__Dynamics-Dynamic__Stability-Full__Linearized__Equations.js b/_site/doxygen/group__Methods-Flight__Dynamics-Dynamic__Stability-Full__Linearized__Equations.js deleted file mode 100644 index ddcc5ee7..00000000 --- a/_site/doxygen/group__Methods-Flight__Dynamics-Dynamic__Stability-Full__Linearized__Equations.js +++ /dev/null @@ -1,6 +0,0 @@ -var group__Methods_Flight__Dynamics_Dynamic__Stability_Full__Linearized__Equations = -[ - [ "Supporting_Functions", "group__Methods-Flight__Dynamics-Dynamic__Stability-Full__Linearized__Equations-Supporting__Functions.html", "group__Methods-Flight__Dynamics-Dynamic__Stability-Full__Linearized__Equations-Supporting__Functions" ], - [ "lateral_directional", "group__Methods-Flight__Dynamics-Dynamic__Stability-Full__Linearized__Equations.html#ga509c906325361dbec974fd9560837381", null ], - [ "longitudinal", "group__Methods-Flight__Dynamics-Dynamic__Stability-Full__Linearized__Equations.html#gafc900a18ec3e2b9d7463474288c3dc91", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Methods-Flight__Dynamics-Dynamic__Stability.html b/_site/doxygen/group__Methods-Flight__Dynamics-Dynamic__Stability.html deleted file mode 100644 index 91732b00..00000000 --- a/_site/doxygen/group__Methods-Flight__Dynamics-Dynamic__Stability.html +++ /dev/null @@ -1,120 +0,0 @@ - - - - - - - -SUAVE: Dynamic_Stability - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
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- -
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- - -
- -
- -
- -
-
Dynamic_Stability
-
-
- - - - - - -

-Modules

 Approximations
 
 Full_Linearized_Equations
 
-

Detailed Description

-
-
- - - - diff --git a/_site/doxygen/group__Methods-Flight__Dynamics-Dynamic__Stability.js b/_site/doxygen/group__Methods-Flight__Dynamics-Dynamic__Stability.js deleted file mode 100644 index 92cc3c57..00000000 --- a/_site/doxygen/group__Methods-Flight__Dynamics-Dynamic__Stability.js +++ /dev/null @@ -1,5 +0,0 @@ -var group__Methods_Flight__Dynamics_Dynamic__Stability = -[ - [ "Approximations", "group__Methods-Flight__Dynamics-Dynamic__Stability-Approximations.html", "group__Methods-Flight__Dynamics-Dynamic__Stability-Approximations" ], - [ "Full_Linearized_Equations", "group__Methods-Flight__Dynamics-Dynamic__Stability-Full__Linearized__Equations.html", "group__Methods-Flight__Dynamics-Dynamic__Stability-Full__Linearized__Equations" ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Methods-Flight__Dynamics-Static__Stability-Approximations-Supporting__Functions.html b/_site/doxygen/group__Methods-Flight__Dynamics-Static__Stability-Approximations-Supporting__Functions.html deleted file mode 100644 index ce82208f..00000000 --- a/_site/doxygen/group__Methods-Flight__Dynamics-Static__Stability-Approximations-Supporting__Functions.html +++ /dev/null @@ -1,342 +0,0 @@ - - - - - - - -SUAVE: Supporting_Functions - - - - - - - - - - - - - - - -
-
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An Aerospace Vehicle Environment for Designing Future Aircraft
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-Functions

def SUAVE.Methods.Flight_Dynamics.Static_Stability.Approximations.Supporting_Functions.convert_sweep.convert_sweep (wing, old_ref_chord_fraction=0.0, new_ref_chord_fraction=0.25)
 
def SUAVE.Methods.Flight_Dynamics.Static_Stability.Approximations.Supporting_Functions.extend_to_ref_area.extend_to_ref_area (surface)
 
def SUAVE.Methods.Flight_Dynamics.Static_Stability.Approximations.Supporting_Functions.trapezoid_ac_x.trapezoid_ac_x (wing)
 
def SUAVE.Methods.Flight_Dynamics.Static_Stability.Approximations.Supporting_Functions.trapezoid_mac.trapezoid_mac (wing)
 trapezoid_mac.py More...
 
-

Detailed Description

-

Function Documentation

- -

◆ convert_sweep()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Flight_Dynamics.Static_Stability.Approximations.Supporting_Functions.convert_sweep.convert_sweep ( wing,
 old_ref_chord_fraction = 0.0,
 new_ref_chord_fraction = 0.25 
)
-
-
This method converts the sweep of a wing planform to refer to a new
-chord fraction. Defaults to converting from leading-edge sweep to 
-quarter-chord sweep.
-
-Assumptions:
-    Assumes a simple trapezoidal wing shape. If the input wing object does
-    not have a simple trapezoidal shape, this function will convert sweeps
-    for an equivalent trapezoid having the same reference sweep, aspect 
-    ratio, and taper ratio.
-
-Source:
-    Unknown
-
-Inputs:
-    wing - a data dictionary with the fields:
-        apsect_ratio - wing aspect ratio                            [dimensionless]
-        sweep        - wing sweep                                   [radians]
-        taper        - wing taper ratio                             [dimensionless]
- 
-    old_ref_chord_fraction - a float value between 0 and 1.0 that 
-                             tells what fraction of the local chord
-                             the sweep line follows. (For example, 
-                             a value of 0.25 refers to quarter-chord
-                             sweep
-    new_ref_chord_fraction - a float value between 0 and 1.0 that
-                             tells what fraction of the local chord
-                             is the new reference for sweep.
-
-Outputs:
-    output - a single float value, new_sweep, which is the sweep
-             angle referenced to the new_ref_chord_fraction.
-
-Defaults:
-    Defaults to converting from leading edge sweep to quater-chord sweep.
-    
- Properties Used:
-    N/A       
-
-
-
- -

◆ extend_to_ref_area()

- -
-
- - - - - - - - -
def SUAVE.Methods.Flight_Dynamics.Static_Stability.Approximations.Supporting_Functions.extend_to_ref_area.extend_to_ref_area ( surface)
-
-
This method takes inputs describing the exposed portion of a trapezoidal
-aerodynamic surface and calculates the dimensions of a corresponding
-aerodynamic surface that extends all the way to the fuselage centerline.
-Particularly used to get the vertical tail reference area for lateral
-stability calculations when the dimensions of the exposed tail are known.
-
-
-Assumptions:
-    Assumes a simple trapezoidal half-wing shape.
-
-Source:
-    Unknown
-
-Inputs:
-    surface - a SUAVE Wing object with the fields:
-        spans.projected - projected span (height for a vertical tail) of
-         the exposed surface                                                     [meters]
-        sweep - leading edge sweep of the aerodynamic surface                    [radians]
-        chords.root - chord length at the junction between the tail and
-         the fuselage                                                            [meters]
-        chords.tip - chord length at the tip of the aerodynamic surface          [meters]                                                                                   
-        symmetric - Is the wing symmetric across the fuselage centerline?
-        exposed_root_chord_offset - the displacement from the fuselage
-         centerline to the exposed area's physical root chordline                [meters]
-
-Outputs:
-    ref_surface - a data dictionary with the fields:
-        spans.projected - The span/height measured from the fuselage centerline  [meters]                                                                                                
-        area.reference - The area of the extended trapezoidal surface            [meters**2]                                                                                                
-        aspect_ratio - The aspect ratio of the extended surface                  [meters]                                                                                               
-        chords.root - The chord of the extended trapezoidal surface
-        where it meets the fuselage centerline                                   [meters]
-        root_LE_change - The change in the leading edge position of the
-        surface compared to the smaller surface that only extended to the
-        fuselage surface. This value is negative for sweptback surfaces          [meters]
-        
-Properties Used:
-     N/A        
-
-
-
- -

◆ trapezoid_ac_x()

- -
-
- - - - - - - - -
def SUAVE.Methods.Flight_Dynamics.Static_Stability.Approximations.Supporting_Functions.trapezoid_ac_x.trapezoid_ac_x ( wing)
-
-
This method computes the aerodynamic center x-position of a linearly
-tapered trapezoidal aerodynamic surface
-
-Assumptions:
-    Assumes a simple trapezoidal wing shape.
-    Does not account for twist or LE/TE extensions
-    Assumes the aerodynamic center of the wing is located at the quarter-
-    chord of the MAC.
-
-Source:
-     Unknown 
-
-Inputs:
-    wing - a data dictionary with the fields:
-        areas.reference - planform area of the trapezoidal wing              [meters**2]
-        spans.projected - wing span                                          [meters]
-        chords.root - wing root chord                                        [meters]
-        taper - wing taper ratio                                             [dimensionless]
-        sweep - wing leading edge sweep                                      [radians]
-        symmetric - wing symmetry                                            [Boolean]
-
-Outputs:
-    dx_ac - the x-direction distance of the aerodynamic center of the wing
-    (or equivalent trapezoid) measured from the leading edge of the wing
-    root                                                                     [meters]
-
-Properties Used:
-N/A
-
-
-
- -

◆ trapezoid_mac()

- -
-
- - - - - - - - -
def SUAVE.Methods.Flight_Dynamics.Static_Stability.Approximations.Supporting_Functions.trapezoid_mac.trapezoid_mac ( wing)
-
- -

trapezoid_mac.py

-

Created: Mar 2014, T. Momose Modified: Jan 2016, E. Botero

This method computes the mean aerodynamic chord of a linearly tapered
-trapezoidal aerodynamic surface
-
-Assumptions:
-    Assumes a simple trapezoidal wing shape.
-    
-Source:
-    Unknown
-
-Inputs:
-    wing - a data dictionary with the fields:
-        areas.reference - the planform area of the trapezoidal wing               [meters**2]
-        spans.projected - wing span                                               [meters]
-        chords.root - the wing root chord                                         [meters]
-        {One of the following}
-        chords.tip - the wing tip chord                                           [meters]
-        taper - taper ratio of the wing                                           [dimensionless]
-
-Outputs:
-    mac - the mean aerodynamic chord of the wing (or equivalent trapezoid)        [meters]
-
-Properties Used:
-    N/A
-
-
-
-
-
- - - - diff --git a/_site/doxygen/group__Methods-Flight__Dynamics-Static__Stability-Approximations-Supporting__Functions.js b/_site/doxygen/group__Methods-Flight__Dynamics-Static__Stability-Approximations-Supporting__Functions.js deleted file mode 100644 index 58170885..00000000 --- a/_site/doxygen/group__Methods-Flight__Dynamics-Static__Stability-Approximations-Supporting__Functions.js +++ /dev/null @@ -1,7 +0,0 @@ -var group__Methods_Flight__Dynamics_Static__Stability_Approximations_Supporting__Functions = -[ - [ "convert_sweep", "group__Methods-Flight__Dynamics-Static__Stability-Approximations-Supporting__Functions.html#ga73fbf404355311e90e887d2b16718526", null ], - [ "extend_to_ref_area", "group__Methods-Flight__Dynamics-Static__Stability-Approximations-Supporting__Functions.html#ga1466483a340b19cb9952443921532dcc", null ], - [ "trapezoid_ac_x", "group__Methods-Flight__Dynamics-Static__Stability-Approximations-Supporting__Functions.html#gac364b994a3b8fddd8e32535b7b47956b", null ], - [ "trapezoid_mac", "group__Methods-Flight__Dynamics-Static__Stability-Approximations-Supporting__Functions.html#gaa93cc36245fbf7b5abd89bbfe4af0120", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Methods-Flight__Dynamics-Static__Stability-Approximations-Tube__Wing.html b/_site/doxygen/group__Methods-Flight__Dynamics-Static__Stability-Approximations-Tube__Wing.html deleted file mode 100644 index aa956d2d..00000000 --- a/_site/doxygen/group__Methods-Flight__Dynamics-Static__Stability-Approximations-Tube__Wing.html +++ /dev/null @@ -1,246 +0,0 @@ - - - - - - - -SUAVE: Tube_Wing - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
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-
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-Functions

def SUAVE.Methods.Flight_Dynamics.Static_Stability.Approximations.Tube_Wing.taw_cnbeta.taw_cnbeta (geometry, conditions, configuration)
 
-

Detailed Description

-

Function Documentation

- -

◆ taw_cnbeta()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Flight_Dynamics.Static_Stability.Approximations.Tube_Wing.taw_cnbeta.taw_cnbeta ( geometry,
 conditions,
 configuration 
)
-
-
This method computes the static directional stability derivative for a
-standard Tube-and-Wing aircraft configuration.        
-
-CAUTION: The correlations used in this method do not account for the
-destabilizing moments due to propellers. This can lead to higher-than-
-expected values of CnBeta, particularly for smaller prop-driven aircraft
-
-Assumptions:
-    -Assumes a tube-and-wing configuration with a single centered 
-    vertical tail
-    -Uses vertical tail effective aspect ratio, currently calculated by
-    hand, using methods from USAF Stability and Control DATCOM
-    -The validity of correlations for KN is questionable for sqrt(h1/h2)
-    greater than about 4 or h_max/w_max outside [0.3,2].
-    -This method assumes a small angle of attack, so the vertical tail AC
-    z-position does not affect the sideslip derivative.
-
-Source:
-    Correlations are taken from Roskam's Airplane Design, Part VI.
-
-Inputs:
-    geometry - aircraft geometrical features: a data dictionary with the fields:
-        wings                                                                         ['Main Wing'] - the aircraft's main wing
-            areas.reference - wing reference area                                     [meters**2]
-            spans.projected - span of the wing                                        [meters]
-            sweep - sweep of the wing leading edge                                    [radians]
-            aspect_ratio - wing aspect ratio                                          [dimensionless]
-            origin - the position of the wing root in the aircraft body frame         [meters]
-        wings                                                                         ['Vertical Stabilizer']
-            spans.projected - projected span (height for a vertical tail) of
-             the exposed surface                                                      [meters]
-            areas.reference - area of the reference vertical tail                     [meters**2]
-            sweep - leading edge sweep of the aerodynamic surface                     [radians]
-            chords.root - chord length at the junction between the tail and 
-             the fuselage                                                             [meters]
-            chords.tip - chord length at the tip of the aerodynamic surface           [meters]
-            symmetric - Is the wing symmetric across the fuselage centerline?
-            origin - the position of the vertical tail root in the aircraft body frame[meters]
-            exposed_root_chord_offset - the displacement from the fuselage
-             centerline to the exposed area's physical root chordline                 [meters]
-
-        fuselages.Fuselage - a data dictionary with the fields:
-            areas.side_projected - fuselage body side area                            [meters**2]
-            lengths.total - length of the fuselage                                    [meters]
-            heights.maximum - maximum height of the fuselage                          [meters]
-            width - maximum width of the fuselage                                     [meters]
-            heights.at_quarter_length - fuselage height at 1/4 of the fuselage length [meters]
-            heights.at_three_quarters_length - fuselage height at 3/4 of fuselage 
-             length                                                                   [meters]
-            heights.at_vertical_root_quarter_chord - fuselage height at the quarter 
-             chord of the vertical tail root                                          [meters]
-        vertical - a data dictionary with the fields below:
-        NOTE: This vertical tail geometry will be used to define a reference
-         vertical tail that extends to the fuselage centerline.
-
-            x_ac_LE - the x-coordinate of the vertical tail aerodynamic 
-            center measured relative to the tail root leading edge (root
-            of reference tail area - at fuselage centerline)
-            leading edge, relative to the nose                                        [meters]
-            sweep_le - leading edge sweep of the vertical tail                        [radians]
-            span - height of the vertical tail                                        [meters]
-            taper - vertical tail taper ratio                                         [dimensionless]
-            aspect_ratio - vertical tail AR: bv/(Sv)^2                                [dimensionless]
-            effective_aspect_ratio - effective aspect ratio considering
-            the effects of fuselage and horizontal tail                               [dimensionless]
-            symmetric - indicates whether the vertical panel is symmetric
-            about the fuselage centerline                                             [Boolean]
-        other_bodies - an list of data dictionaries containing bodies 
-        such as nacelles if these are large enough to strongly influence
-        stability. Each body data dictionary contains the same fields as
-        the fuselage data dictionary (described above), except no value 
-        is needed for 'height_at_vroot_quarter_chord'. CAN BE EMPTY LIST
-            x_front - This is the only new field needed: the x-coordinate 
-            of the nose of the body relative to the fuselage nose
-
-    conditions - a data dictionary with the fields:
-        v_inf - true airspeed                                                         [meters/second]
-        M - flight Mach number
-        rho - air density                                                             [kg/meters**3]
-        mew - air dynamic dynamic_viscosity                                           [kg/meter/second]
-
-    configuration - a data dictionary with the fields:
-        mass_properties - a data dictionary with the field:
-            center_of_gravity - A vector in 3-space indicating CG position            [meters]
-        other - a dictionary of aerodynamic bodies, other than the fuselage,
-        whose effect on directional stability is to be included in the analysis
-
-Outputs:
-    CnBeta - a single float value: The static directional stability 
-    derivative
-
-Properties Used:
-    N/A  
-
-
-
-
-
- - - - diff --git a/_site/doxygen/group__Methods-Flight__Dynamics-Static__Stability-Approximations-Tube__Wing.js b/_site/doxygen/group__Methods-Flight__Dynamics-Static__Stability-Approximations-Tube__Wing.js deleted file mode 100644 index b56be38a..00000000 --- a/_site/doxygen/group__Methods-Flight__Dynamics-Static__Stability-Approximations-Tube__Wing.js +++ /dev/null @@ -1,4 +0,0 @@ -var group__Methods_Flight__Dynamics_Static__Stability_Approximations_Tube__Wing = -[ - [ "taw_cnbeta", "group__Methods-Flight__Dynamics-Static__Stability-Approximations-Tube__Wing.html#ga29a3aa2f9d4e36caacbf651748d1526b", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Methods-Flight__Dynamics-Static__Stability-Approximations.html b/_site/doxygen/group__Methods-Flight__Dynamics-Static__Stability-Approximations.html deleted file mode 100644 index 23254fe4..00000000 --- a/_site/doxygen/group__Methods-Flight__Dynamics-Static__Stability-Approximations.html +++ /dev/null @@ -1,184 +0,0 @@ - - - - - - - -SUAVE: Approximations - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
-
- - - -
-
- -
-
-
- -
- -
-
- - -
- -
- -
- - -
-
- - - - - - -

-Modules

 Supporting_Functions
 
 Tube_Wing
 
- - - -

-Functions

def SUAVE.Methods.Flight_Dynamics.Static_Stability.Approximations.datcom.datcom (wing, mach)
 
-

Detailed Description

-

Function Documentation

- -

◆ datcom()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Flight_Dynamics.Static_Stability.Approximations.datcom.datcom ( wing,
 mach 
)
-
-
This method uses the DATCOM formula to compute dCL/dalpha without 
-correlations for downwash of lifting surfaces further ahead on the 
-aircraft or upwash resulting from the position of the wing on the body.
-
-CAUTION: The method presented here is applicable for subsonic speeds.
-May be inaccurate for transonic or supersonic flight. A correction factor
-for supersonic flight is included, but may not be completely accurate.
-
-Assumptions:
-Mach number should not be transonic
-
-Source:
-    None
-     
-Inputs:
-    wing - a data dictionary with the fields:
-        effective_apsect_ratio - wing aspect ratio [dimensionless]. If 
-        this variable is not inlcuded in the input, the method will look
-        for a variable named 'aspect_ratio'.
-        sweep_le - wing leading-edge sweep angle [radians]
-        taper - wing taper ratio [dimensionless]
-    mach - flight Mach number [dimensionless]. Should be a numpy array
-        with one or more elements.
-
-Outputs:
-    cL_alpha - The derivative of 3D lift coefficient with respect to AoA
-
-Properties Used:
-N/A
-
-
-
-
-
- - - - diff --git a/_site/doxygen/group__Methods-Flight__Dynamics-Static__Stability-Approximations.js b/_site/doxygen/group__Methods-Flight__Dynamics-Static__Stability-Approximations.js deleted file mode 100644 index 2b8c0d58..00000000 --- a/_site/doxygen/group__Methods-Flight__Dynamics-Static__Stability-Approximations.js +++ /dev/null @@ -1,6 +0,0 @@ -var group__Methods_Flight__Dynamics_Static__Stability_Approximations = -[ - [ "Supporting_Functions", "group__Methods-Flight__Dynamics-Static__Stability-Approximations-Supporting__Functions.html", "group__Methods-Flight__Dynamics-Static__Stability-Approximations-Supporting__Functions" ], - [ "Tube_Wing", "group__Methods-Flight__Dynamics-Static__Stability-Approximations-Tube__Wing.html", "group__Methods-Flight__Dynamics-Static__Stability-Approximations-Tube__Wing" ], - [ "datcom", "group__Methods-Flight__Dynamics-Static__Stability-Approximations.html#ga38877c856f6e41a0969d9d7f12023907", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Methods-Flight__Dynamics-Static__Stability.html b/_site/doxygen/group__Methods-Flight__Dynamics-Static__Stability.html deleted file mode 100644 index 51c7a585..00000000 --- a/_site/doxygen/group__Methods-Flight__Dynamics-Static__Stability.html +++ /dev/null @@ -1,118 +0,0 @@ - - - - - - - -SUAVE: Static_Stability - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
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-
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- - -
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- -
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Static_Stability
-
-
- - - - -

-Modules

 Approximations
 
-

Detailed Description

-
-
- - - - diff --git a/_site/doxygen/group__Methods-Flight__Dynamics-Static__Stability.js b/_site/doxygen/group__Methods-Flight__Dynamics-Static__Stability.js deleted file mode 100644 index 9a171e3a..00000000 --- a/_site/doxygen/group__Methods-Flight__Dynamics-Static__Stability.js +++ /dev/null @@ -1,4 +0,0 @@ -var group__Methods_Flight__Dynamics_Static__Stability = -[ - [ "Approximations", "group__Methods-Flight__Dynamics-Static__Stability-Approximations.html", "group__Methods-Flight__Dynamics-Static__Stability-Approximations" ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Methods-Flight__Dynamics.html b/_site/doxygen/group__Methods-Flight__Dynamics.html deleted file mode 100644 index 09293550..00000000 --- a/_site/doxygen/group__Methods-Flight__Dynamics.html +++ /dev/null @@ -1,124 +0,0 @@ - - - - - - - -SUAVE: Flight_Dynamics - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
-
- - - -
-
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-
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Flight_Dynamics
-
-
- -

Description. -More...

- - - - - - -

-Modules

 Dynamic_Stability
 
 Static_Stability
 
-

Detailed Description

-

Description.

-
-
- - - - diff --git a/_site/doxygen/group__Methods-Flight__Dynamics.js b/_site/doxygen/group__Methods-Flight__Dynamics.js deleted file mode 100644 index 49bb7b3f..00000000 --- a/_site/doxygen/group__Methods-Flight__Dynamics.js +++ /dev/null @@ -1,5 +0,0 @@ -var group__Methods_Flight__Dynamics = -[ - [ "Dynamic_Stability", "group__Methods-Flight__Dynamics-Dynamic__Stability.html", "group__Methods-Flight__Dynamics-Dynamic__Stability" ], - [ "Static_Stability", "group__Methods-Flight__Dynamics-Static__Stability.html", "group__Methods-Flight__Dynamics-Static__Stability" ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Methods-Geometry-Three__Dimensional.html b/_site/doxygen/group__Methods-Geometry-Three__Dimensional.html deleted file mode 100644 index 40a8e4ca..00000000 --- a/_site/doxygen/group__Methods-Geometry-Three__Dimensional.html +++ /dev/null @@ -1,567 +0,0 @@ - - - - - - - -SUAVE: Three Dimensional - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
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- - - -
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-
Three Dimensional
-
-
- -

Geometry functions for three dimensions. -More...

- - - - - - - - - - - - - - - - - - - - - - - - -

-Functions

def SUAVE.Methods.Geometry.Three_Dimensional.angles_to_dcms.angles_to_dcms (rotations, sequence=(2, 1, 0))
 
def SUAVE.Methods.Geometry.Three_Dimensional.angles_to_dcms.T0 (a)
 
def SUAVE.Methods.Geometry.Three_Dimensional.angles_to_dcms.T1 (a)
 
def SUAVE.Methods.Geometry.Three_Dimensional.angles_to_dcms.T2 (a)
 
def SUAVE.Methods.Geometry.Three_Dimensional.angles_to_dcms.new_tensor (a)
 
def SUAVE.Methods.Geometry.Three_Dimensional.compute_chord_length_from_span_location.compute_chord_length_from_span_location (wing, span_location)
 compute_chord_length_from_span_location.py More...
 
def SUAVE.Methods.Geometry.Three_Dimensional.compute_span_location_from_chord_length.compute_span_location_from_chord_length (wing, chord_length)
 compute_span_location_from_chord_length.py More...
 
def SUAVE.Methods.Geometry.Three_Dimensional.estimate_naca_4_series_internal_volume.estimate_naca_4_series_internal_volume (wing, m, p)
 
def SUAVE.Methods.Geometry.Three_Dimensional.orientation_product.orientation_product (T, Bb)
 
def SUAVE.Methods.Geometry.Three_Dimensional.orientation_transpose.orientation_transpose (T)
 
-

Detailed Description

-

Geometry functions for three dimensions.

-

Function Documentation

- -

◆ angles_to_dcms()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Geometry.Three_Dimensional.angles_to_dcms.angles_to_dcms ( rotations,
 sequence = (2,1,0) 
)
-
-
Builds an euler angle rotation matrix
-
-Assumptions:
-N/A
-
-Source:
-N/A
-
-Inputs:
-rotations     [radians]  [r1s r2s r3s], column array of rotations
-sequence      [-]        (2,1,0) (default), (2,1,2), etc.. a combination of three column indices
-
-Outputs:
-transform     [-]        3-dimensional array with direction cosine matrices
-                         patterned along dimension zero
-
-Properties Used:
-N/A
-
-
-
- -

◆ compute_chord_length_from_span_location()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Geometry.Three_Dimensional.compute_chord_length_from_span_location.compute_chord_length_from_span_location ( wing,
 span_location 
)
-
- -

compute_chord_length_from_span_location.py

-

Created: Oct 2015, M. Vegh, Modified: Jan 2016, E. Botero

Computes the chord length given a location along the half-span.
-
-Assumptions:
-Linear variation of chord with span.
-
-Source:
-None
-
-Inputs:
-wing.chords.
-  root                [m]
-  tip                 [m]
-wing.spans.projected  [m]
-span_location         [m]
-
-Outputs:
-chord_length          [m]
-
-Properties Used:
-N/A
-
-
-
- -

◆ compute_span_location_from_chord_length()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Geometry.Three_Dimensional.compute_span_location_from_chord_length.compute_span_location_from_chord_length ( wing,
 chord_length 
)
-
- -

compute_span_location_from_chord_length.py

-

Created: Oct 2015, M. Vegh, Modified: Jan 2016, E. Botero

Computes the location along the half-span given a chord length.
-
-Assumptions:
-Linear variation of chord with span. Returns 0 if constant chord wing.
-
-Source:
-None
-
-Inputs:
-wing.chords.
-  root                [m]
-  tip                 [m]
-wing.spans.projected  [m]
-chord_length          [m]
-
-Outputs:
-span_location         [m] 
-
-Properties Used:
-N/A
-
-
-
- -

◆ estimate_naca_4_series_internal_volume()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Geometry.Three_Dimensional.estimate_naca_4_series_internal_volume.estimate_naca_4_series_internal_volume ( wing,
 m,
 p 
)
-
-
Computes the volume of a wing with NACA 4-series airfoils.
-
-Assumptions:
-Wing has constant thickness to chord along the span
-Front spar is at 10%chord and rear spar is at 60% chord
-
-Source:
-Wikipedia, based on Moran, Jack (2003). An introduction to theoretical and 
-  computational aerodynamics. Dover.
-
-Inputs:
-m                       [-]  percent camber (.1 is 10%)
-p                       [-]  location of max camber (.1 is 10% along chord)
-wing.chords.
-  root                  [m]
-  tip                   [m]
-wing.taper              [-]
-wing.thickness_to_chord [-]
-wing.spans.projected    [m]
-chord_length            [m]
-
-Outputs:
-volume                  [m^3] 
-
-Properties Used:
-N/A
-
-
-
- -

◆ new_tensor()

- -
-
- - - - - - - - -
def SUAVE.Methods.Geometry.Three_Dimensional.angles_to_dcms.new_tensor ( a)
-
-
Initializes the required tensor. Able to handle imaginary values.
-
-Assumptions:
-N/A
-
-Source:
-N/A
-
-Inputs:
-a        [radians] angle of rotation
-
-Outputs:
-T        [-]       3-dimensional array with identity matrix
-                   patterned along dimension zero
-
-Properties Used:
-N/A
-
-
-
- -

◆ orientation_product()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Geometry.Three_Dimensional.orientation_product.orientation_product ( T,
 Bb 
)
-
-
Computes the product of a tensor and a vector.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-T         [-] 3-dimensional array with rotation matrix
-              patterned along dimension zero
-Bb        [-] 3-dimensional vector
-
-Outputs:
-C         [-] transformed vector
-
-Properties Used:
-N/A
-
-
-
- -

◆ orientation_transpose()

- -
-
- - - - - - - - -
def SUAVE.Methods.Geometry.Three_Dimensional.orientation_transpose.orientation_transpose ( T)
-
-
Computes the transpose of a tensor.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-T         [-] 3-dimensional array with rotation matrix
-              patterned along dimension zero
-
-Outputs:
-Tt        [-] transformed tensor
-
-Properties Used:
-N/A
-
-
-
- -

◆ T0()

- -
-
- - - - - - - - -
def SUAVE.Methods.Geometry.Three_Dimensional.angles_to_dcms.T0 ( a)
-
-
Rotation matrix about first axis
-
-Assumptions:
-N/A
-
-Source:
-N/A
-
-Inputs:
-a        [radians] angle of rotation
-
-Outputs:
-T        [-]       rotation matrix
-
-Properties Used:
-N/A
-
-
-
- -

◆ T1()

- -
-
- - - - - - - - -
def SUAVE.Methods.Geometry.Three_Dimensional.angles_to_dcms.T1 ( a)
-
-
Rotation matrix about second axis
-
-Assumptions:
-N/A
-
-Source:
-N/A
-
-Inputs:
-a        [radians] angle of rotation
-
-Outputs:
-T        [-]       rotation matrix
-
-Properties Used:
-N/A
-
-
-
- -

◆ T2()

- -
-
- - - - - - - - -
def SUAVE.Methods.Geometry.Three_Dimensional.angles_to_dcms.T2 ( a)
-
-
Rotation matrix about third axis
-
-Assumptions:
-N/A
-
-Source:
-N/A
-
-Inputs:
-a        [radians] angle of rotation
-
-Outputs:
-T        [-]       rotation matrix
-
-Properties Used:
-N/A
-
-
-
-
-
- - - - diff --git a/_site/doxygen/group__Methods-Geometry-Three__Dimensional.js b/_site/doxygen/group__Methods-Geometry-Three__Dimensional.js deleted file mode 100644 index 38df1e56..00000000 --- a/_site/doxygen/group__Methods-Geometry-Three__Dimensional.js +++ /dev/null @@ -1,13 +0,0 @@ -var group__Methods_Geometry_Three__Dimensional = -[ - [ "angles_to_dcms", "group__Methods-Geometry-Three__Dimensional.html#gaa13090aedf386216826d3d7da871521a", null ], - [ "compute_chord_length_from_span_location", "group__Methods-Geometry-Three__Dimensional.html#gaeaa9c43e096c3954b83d9acdd6c065c0", null ], - [ "compute_span_location_from_chord_length", "group__Methods-Geometry-Three__Dimensional.html#gafae12beb45b896882a3c5b6ae0e22d64", null ], - [ "estimate_naca_4_series_internal_volume", "group__Methods-Geometry-Three__Dimensional.html#ga8828e15eacd057b8beaa6a477575b472", null ], - [ "new_tensor", "group__Methods-Geometry-Three__Dimensional.html#ga16788464c8acdf43da2e3f00c0e3b00c", null ], - [ "orientation_product", "group__Methods-Geometry-Three__Dimensional.html#ga7a88f551f81b035a4d09bfcccbe4c71c", null ], - [ "orientation_transpose", "group__Methods-Geometry-Three__Dimensional.html#ga5b7b94ba73128099aa30725f46b4084d", null ], - [ "T0", "group__Methods-Geometry-Three__Dimensional.html#ga00ac4c1fd8825e5356e49833c969ebd0", null ], - [ "T1", "group__Methods-Geometry-Three__Dimensional.html#gabd6752acfd492dad145e2c497a9252cc", null ], - [ "T2", "group__Methods-Geometry-Three__Dimensional.html#ga20e4c3e3cf2f37b9cab9bac7587b0731", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Methods-Geometry-Two__Dimensional-Cross__Section-Airfoil.html b/_site/doxygen/group__Methods-Geometry-Two__Dimensional-Cross__Section-Airfoil.html deleted file mode 100644 index 3afdc758..00000000 --- a/_site/doxygen/group__Methods-Geometry-Two__Dimensional-Cross__Section-Airfoil.html +++ /dev/null @@ -1,282 +0,0 @@ - - - - - - - -SUAVE: Airfoil - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
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- -
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Geometry functions for two dimensional airfoils. -More...

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-Functions

def SUAVE.Methods.Geometry.Two_Dimensional.Cross_Section.Airfoil.compute_naca_4series.compute_naca_4series (camber, camber_loc, thickness, npoints=200)
 
def SUAVE.Methods.Geometry.Two_Dimensional.Cross_Section.Airfoil.compute_naca_4series.compute_naca_4series_lines (x, camber, camber_loc, thickness)
 
def SUAVE.Methods.Geometry.Two_Dimensional.Cross_Section.Airfoil.import_airfoil_dat.import_airfoil_dat (filename)
 
-

Detailed Description

-

Geometry functions for two dimensional airfoils.

-

Function Documentation

- -

◆ compute_naca_4series()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Geometry.Two_Dimensional.Cross_Section.Airfoil.compute_naca_4series.compute_naca_4series ( camber,
 camber_loc,
 thickness,
 npoints = 200 
)
-
-
Computes the points of NACA 4-series airfoil
-
-Assumptions:
-None
-
-Source:
-None
-
-Inputs:
-camber      [-] Maximum camber as a fraction of chord
-camber_loc  [-] Maximum camber location as a fraction of chord
-thickness   [-] Maximum thickness as a fraction of chord
-npoints     [-] Total number of points
-
-Outputs:
-upper       [-] numpy array of x-y coordinates on the upper surface
-lower       [-] numpy array of x-y coordinates on the lower surface
-
-Properties Used:
-N/A
-
-
-
- -

◆ compute_naca_4series_lines()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Geometry.Two_Dimensional.Cross_Section.Airfoil.compute_naca_4series.compute_naca_4series_lines ( x,
 camber,
 camber_loc,
 thickness 
)
-
-
Computes the camber, thickness, and the angle of the camber line
-at a given point along the airfoil.
-
-Assumptions:
-None
-
-Source:
-Similar to http://airfoiltools.com/airfoil/naca4digit
-
-Inputs:
-camber      [-]       Maximum camber as a fraction of chord
-camber_loc  [-]       Maximum camber location as a fraction of chord
-thickness   [-]       Maximum thickness as a fraction of chord
-
-Outputs:
-zt          [-]       Thickness
-zc          [-]       Camber
-th          [radians] Angle of the camber line
-
-Properties Used:
-N/A
-
-
-
- -

◆ import_airfoil_dat()

- -
-
- - - - - - - - -
def SUAVE.Methods.Geometry.Two_Dimensional.Cross_Section.Airfoil.import_airfoil_dat.import_airfoil_dat ( filename)
-
-
Import an airfoil data file and stores it in a numpy array.
-
-Assumptions:
-Airfoil file in Lednicer format
-
-Source:
-None
-
-Inputs:
-filename   <string>
-
-Outputs:
-data       numpy array with airfoil data
-
-Properties Used:
-N/A
-
-
-
-
-
- - - - diff --git a/_site/doxygen/group__Methods-Geometry-Two__Dimensional-Cross__Section-Airfoil.js b/_site/doxygen/group__Methods-Geometry-Two__Dimensional-Cross__Section-Airfoil.js deleted file mode 100644 index 746bfe8d..00000000 --- a/_site/doxygen/group__Methods-Geometry-Two__Dimensional-Cross__Section-Airfoil.js +++ /dev/null @@ -1,6 +0,0 @@ -var group__Methods_Geometry_Two__Dimensional_Cross__Section_Airfoil = -[ - [ "compute_naca_4series", "group__Methods-Geometry-Two__Dimensional-Cross__Section-Airfoil.html#gad9b707f99354749a179f1c932d25f8b1", null ], - [ "compute_naca_4series_lines", "group__Methods-Geometry-Two__Dimensional-Cross__Section-Airfoil.html#gae1ae9095df65c2c151b5ad746a74c8a9", null ], - [ "import_airfoil_dat", "group__Methods-Geometry-Two__Dimensional-Cross__Section-Airfoil.html#ga68ca3b8f890d1f6714e88b276cbce559", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Methods-Geometry-Two__Dimensional-Cross__Section-Propulsion.html b/_site/doxygen/group__Methods-Geometry-Two__Dimensional-Cross__Section-Propulsion.html deleted file mode 100644 index f77d0baf..00000000 --- a/_site/doxygen/group__Methods-Geometry-Two__Dimensional-Cross__Section-Propulsion.html +++ /dev/null @@ -1,228 +0,0 @@ - - - - - - - -SUAVE: Propulsion - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
-
- - - -
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- -
-
-
- -
- -
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- - -
- -
- - -
- -

Geometry functions for two dimensional propulsion measurements. -More...

- - - - - - -

-Functions

def SUAVE.Methods.Geometry.Two_Dimensional.Cross_Section.Propulsion.compute_ducted_fan_geometry.compute_ducted_fan_geometry (ducted_fan, conditions)
 
def SUAVE.Methods.Geometry.Two_Dimensional.Cross_Section.Propulsion.compute_turbofan_geometry.compute_turbofan_geometry (turbofan, conditions)
 
-

Detailed Description

-

Geometry functions for two dimensional propulsion measurements.

-

Function Documentation

- -

◆ compute_ducted_fan_geometry()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Geometry.Two_Dimensional.Cross_Section.Propulsion.compute_ducted_fan_geometry.compute_ducted_fan_geometry ( ducted_fan,
 conditions 
)
-
-
Estimates geometry for a ducted fan.
-
-Assumptions:
-None
-
-Source:
-None
-
-Inputs:
-ducted_fan.thrust.
-  mass_flow_rate_design [kg/s]
-ducted_fan.fan_nozzle.
-  outputs.velocity      [m/s]
-  outputs.density       [kg/m^3]
-  outputs.area_ratio    [-]
-conditions.freestream.
-  velocity              [m/s]
-  density               [kg/m^3]
-
-Outputs:
-ducted_fan.
-  areas.maximum         [m^2]
-  areas.wetted          [m^2]
-  nacelle_diameter      [m]
-  engine_length         [m]
-
-Properties Used:
-N/A
-
-
-
- -

◆ compute_turbofan_geometry()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Geometry.Two_Dimensional.Cross_Section.Propulsion.compute_turbofan_geometry.compute_turbofan_geometry ( turbofan,
 conditions 
)
-
-
Estimates geometry for a ducted fan.
-
-Assumptions:
-None
-
-Source:
-http://adg.stanford.edu/aa241/AircraftDesign.html
-
-Inputs:
-turbofan.sealevel_static_thrust [N]
-
-Outputs:
-turbofan.
-  engine_length                 [m]
-  nacelle_diameter              [m]
-  areas.wetted                  [m^2]
-
-Properties Used:
-N/A
-
-
-
-
-
- - - - diff --git a/_site/doxygen/group__Methods-Geometry-Two__Dimensional-Cross__Section-Propulsion.js b/_site/doxygen/group__Methods-Geometry-Two__Dimensional-Cross__Section-Propulsion.js deleted file mode 100644 index 9e0899e3..00000000 --- a/_site/doxygen/group__Methods-Geometry-Two__Dimensional-Cross__Section-Propulsion.js +++ /dev/null @@ -1,5 +0,0 @@ -var group__Methods_Geometry_Two__Dimensional_Cross__Section_Propulsion = -[ - [ "compute_ducted_fan_geometry", "group__Methods-Geometry-Two__Dimensional-Cross__Section-Propulsion.html#gabbca63e71ae9b78043c985ea40db0bab", null ], - [ "compute_turbofan_geometry", "group__Methods-Geometry-Two__Dimensional-Cross__Section-Propulsion.html#ga3ac328d4ae5282b2e4ce66d519777c73", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Methods-Geometry-Two__Dimensional-Cross__Section.html b/_site/doxygen/group__Methods-Geometry-Two__Dimensional-Cross__Section.html deleted file mode 100644 index 9d600a01..00000000 --- a/_site/doxygen/group__Methods-Geometry-Two__Dimensional-Cross__Section.html +++ /dev/null @@ -1,126 +0,0 @@ - - - - - - - -SUAVE: Cross Section - - - - - - - - - - - - - - - -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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Geometry functions for two dimensional cross sections. -More...

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-Modules

 Airfoil
 Geometry functions for two dimensional airfoils.
 
 Propulsion
 Geometry functions for two dimensional propulsion measurements.
 
-

Detailed Description

-

Geometry functions for two dimensional cross sections.

-
-
- - - - diff --git a/_site/doxygen/group__Methods-Geometry-Two__Dimensional-Cross__Section.js b/_site/doxygen/group__Methods-Geometry-Two__Dimensional-Cross__Section.js deleted file mode 100644 index b9de485c..00000000 --- a/_site/doxygen/group__Methods-Geometry-Two__Dimensional-Cross__Section.js +++ /dev/null @@ -1,5 +0,0 @@ -var group__Methods_Geometry_Two__Dimensional_Cross__Section = -[ - [ "Airfoil", "group__Methods-Geometry-Two__Dimensional-Cross__Section-Airfoil.html", "group__Methods-Geometry-Two__Dimensional-Cross__Section-Airfoil" ], - [ "Propulsion", "group__Methods-Geometry-Two__Dimensional-Cross__Section-Propulsion.html", "group__Methods-Geometry-Two__Dimensional-Cross__Section-Propulsion" ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Methods-Geometry-Two__Dimensional-Planform.html b/_site/doxygen/group__Methods-Geometry-Two__Dimensional-Planform.html deleted file mode 100644 index fea0e1df..00000000 --- a/_site/doxygen/group__Methods-Geometry-Two__Dimensional-Planform.html +++ /dev/null @@ -1,113 +0,0 @@ - - - - - - - -SUAVE: Planform - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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Geometry functions for two dimensional planforms. -More...

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Geometry functions for two dimensional planforms.

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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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Two Dimensional
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Geometry functions for two dimensions. -More...

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-Modules

 Cross Section
 Geometry functions for two dimensional cross sections.
 
 Planform
 Geometry functions for two dimensional planforms.
 
-

Detailed Description

-

Geometry functions for two dimensions.

-
-
- - - - diff --git a/_site/doxygen/group__Methods-Geometry-Two__Dimensional.js b/_site/doxygen/group__Methods-Geometry-Two__Dimensional.js deleted file mode 100644 index 7fbdc31c..00000000 --- a/_site/doxygen/group__Methods-Geometry-Two__Dimensional.js +++ /dev/null @@ -1,5 +0,0 @@ -var group__Methods_Geometry_Two__Dimensional = -[ - [ "Cross Section", "group__Methods-Geometry-Two__Dimensional-Cross__Section.html", "group__Methods-Geometry-Two__Dimensional-Cross__Section" ], - [ "Planform", "group__Methods-Geometry-Two__Dimensional-Planform.html", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Methods-Geometry.html b/_site/doxygen/group__Methods-Geometry.html deleted file mode 100644 index 916ec17d..00000000 --- a/_site/doxygen/group__Methods-Geometry.html +++ /dev/null @@ -1,127 +0,0 @@ - - - - - - - -SUAVE: Geometry - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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Geometry
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These methods are primarily used for sizing. -More...

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 Three Dimensional
 Geometry functions for three dimensions.
 
 Two Dimensional
 Geometry functions for two dimensions.
 
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Detailed Description

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These methods are primarily used for sizing.

-

Anything that modifies geometry belong here.

-
-
- - - - diff --git a/_site/doxygen/group__Methods-Geometry.js b/_site/doxygen/group__Methods-Geometry.js deleted file mode 100644 index 5acdc1f7..00000000 --- a/_site/doxygen/group__Methods-Geometry.js +++ /dev/null @@ -1,5 +0,0 @@ -var group__Methods_Geometry = -[ - [ "Three Dimensional", "group__Methods-Geometry-Three__Dimensional.html", "group__Methods-Geometry-Three__Dimensional" ], - [ "Two Dimensional", "group__Methods-Geometry-Two__Dimensional.html", "group__Methods-Geometry-Two__Dimensional" ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Methods-Missions-Segments-Climb.html b/_site/doxygen/group__Methods-Missions-Segments-Climb.html deleted file mode 100644 index 8cbee64e..00000000 --- a/_site/doxygen/group__Methods-Missions-Segments-Climb.html +++ /dev/null @@ -1,1351 +0,0 @@ - - - - - - - -SUAVE: Climb - - - - - - - - - - - - - - - -
-
- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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Climb mission methods containing the functions for setting up and solving a mission. -More...

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-Functions

def SUAVE.Methods.Missions.Segments.Climb.Common.unpack_unknowns (segment, state)
 
def SUAVE.Methods.Missions.Segments.Climb.Common.residual_total_forces (segment, state)
 
def SUAVE.Methods.Missions.Segments.Climb.Common.update_differentials_altitude (segment, state)
 
def SUAVE.Methods.Missions.Segments.Climb.Constant_Dynamic_Pressure_Constant_Angle.initialize_conditions_unpack_unknowns (segment, state)
 
def SUAVE.Methods.Missions.Segments.Climb.Constant_Dynamic_Pressure_Constant_Angle.residual_total_forces (segment, state)
 
def SUAVE.Methods.Missions.Segments.Climb.Constant_Dynamic_Pressure_Constant_Rate.initialize_conditions (segment, state)
 
def SUAVE.Methods.Missions.Segments.Climb.Constant_EAS_Constant_Rate.initialize_conditions (segment, state)
 
def SUAVE.Methods.Missions.Segments.Climb.Constant_Mach_Constant_Angle.initialize_conditions (segment, state)
 
def SUAVE.Methods.Missions.Segments.Climb.Constant_Mach_Constant_Rate.initialize_conditions (segment, state)
 
def SUAVE.Methods.Missions.Segments.Climb.Constant_Mach_Linear_Altitude.initialize_conditions (segment, state)
 
def SUAVE.Methods.Missions.Segments.Climb.Constant_Speed_Constant_Angle.initialize_conditions (segment, state)
 
def SUAVE.Methods.Missions.Segments.Climb.Constant_Speed_Constant_Angle_Noise.expand_state (segment, state)
 
def SUAVE.Methods.Missions.Segments.Climb.Constant_Speed_Constant_Rate.initialize_conditions (segment, state)
 
def SUAVE.Methods.Missions.Segments.Climb.Constant_Speed_Linear_Altitude.initialize_conditions (segment, state)
 Constant_Speed_Linear_Altitude.py Created: Jul 2014, SUAVE Team Modified: Jun 2017, E. More...
 
def SUAVE.Methods.Missions.Segments.Climb.Constant_Throttle_Constant_Speed.unpack_body_angle (segment, state)
 
def SUAVE.Methods.Missions.Segments.Climb.Constant_Throttle_Constant_Speed.initialize_conditions (segment, state)
 
def SUAVE.Methods.Missions.Segments.Climb.Constant_Throttle_Constant_Speed.update_differentials_altitude (segment, state)
 
-def SUAVE.Methods.Missions.Segments.Climb.Constant_Throttle_Constant_Speed.update_velocity_vector_from_wind_angle (segment, state)
 
def SUAVE.Methods.Missions.Segments.Climb.Linear_Mach_Constant_Rate.initialize_conditions (segment, state)
 
def SUAVE.Methods.Missions.Segments.Climb.Linear_Speed_Constant_Rate.initialize_conditions (segment, state)
 
def SUAVE.Methods.Missions.Segments.Climb.Optimized.unpack_unknowns (segment, state)
 
def SUAVE.Methods.Missions.Segments.Climb.Optimized.update_differentials (segment, state)
 
def SUAVE.Methods.Missions.Segments.Climb.Optimized.objective (segment, state)
 
def SUAVE.Methods.Missions.Segments.Climb.Optimized.constraints (segment, state)
 
def SUAVE.Methods.Missions.Segments.Climb.Optimized.cache_inputs (segment, state)
 
def SUAVE.Methods.Missions.Segments.Climb.Optimized.solve_linear_speed_constant_rate (segment, state)
 
-

Detailed Description

-

Climb mission methods containing the functions for setting up and solving a mission.

-

Function Documentation

- -

◆ cache_inputs()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Missions.Segments.Climb.Optimized.cache_inputs ( segment,
 state 
)
-
-
This function caches the prior inputs to make sure the same inputs are not run twice in a row
-
-
- -

◆ constraints()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Missions.Segments.Climb.Optimized.constraints ( segment,
 state 
)
-
-
This function pulls the equality constraints from the results of flying the segment and returns it to the optimizer
-
-    Inputs:
-    state
-    
-    Outputs:
-    state.constraint_values [vector]
-
-
- -

◆ expand_state()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Missions.Segments.Climb.Constant_Speed_Constant_Angle_Noise.expand_state ( segment,
 state 
)
-
-
Makes all vectors in the state the same size. Determines the minimum amount of points needed to get data for noise certification.
-
-Assumptions:
-Half second intervals for certification requirements. Fixed microphone position
-
-Source:
-N/A
-
-Inputs:
-state.numerics.number_control_points  [Unitless]
-
-Outputs:
-N/A
-
-Properties Used:
-Position of the flyover microphone is 6500 meters
-
-
-
- -

◆ initialize_conditions() [1/11]

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Missions.Segments.Climb.Constant_Speed_Linear_Altitude.initialize_conditions ( segment,
 state 
)
-
- -

Constant_Speed_Linear_Altitude.py Created: Jul 2014, SUAVE Team Modified: Jun 2017, E.

-

Botero

Sets the specified conditions which are given for the segment type.
-
-Assumptions:
-Constrant dynamic pressure and constant rate of climb
-
-Source:
-N/A
-
-Inputs:
-segment.air_speed                           [meters/second]
-segment.altitude_start                      [meters]
-segment.altitude_end                        [meters]
-segment.distance                            [meters]
-
-Outputs:
-conditions.frames.inertial.velocity_vector  [meters/second]
-conditions.frames.inertial.position_vector  [meters]
-conditions.freestream.altitude              [meters]
-conditions.frames.inertial.time             [seconds]
-
-Properties Used:
-N/A
-
-
-
- -

◆ initialize_conditions() [2/11]

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Missions.Segments.Climb.Constant_Speed_Constant_Rate.initialize_conditions ( segment,
 state 
)
-
-
Sets the specified conditions which are given for the segment type.
-
-Assumptions:
-Constant true airspeed, with a constant rate of climb
-
-Source:
-N/A
-
-Inputs:
-segment.climb_rate                          [meters/second]
-segment.air_speed                           [meters/second]
-segment.altitude_start                      [meters]
-segment.altitude_end                        [meters]
-state.numerics.dimensionless.control_points [Unitless]
-conditions.freestream.density               [kilograms/meter^3]
-
-Outputs:
-conditions.frames.inertial.velocity_vector  [meters/second]
-conditions.frames.inertial.position_vector  [meters]
-conditions.freestream.altitude              [meters]
-
-Properties Used:
-N/A
-
-
-
- -

◆ initialize_conditions() [3/11]

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Missions.Segments.Climb.Constant_Speed_Constant_Angle.initialize_conditions ( segment,
 state 
)
-
-
Sets the specified conditions which are given for the segment type.
-
-Assumptions:
-Constant true airspeed, with a constant climb angle
-
-Source:
-N/A
-
-Inputs:
-segment.climb_angle                         [radians]
-segment.air_speed                           [meter/second]
-segment.altitude_start                      [meters]
-segment.altitude_end                        [meters]
-state.numerics.dimensionless.control_points [Unitless]
-conditions.freestream.density               [kilograms/meter^3]
-
-Outputs:
-conditions.frames.inertial.velocity_vector  [meters/second]
-conditions.frames.inertial.position_vector  [meters]
-conditions.freestream.altitude              [meters]
-
-Properties Used:
-N/A
-
-
-
- -

◆ initialize_conditions() [4/11]

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Missions.Segments.Climb.Constant_Dynamic_Pressure_Constant_Rate.initialize_conditions ( segment,
 state 
)
-
-
Sets the specified conditions which are given for the segment type.
-
-Assumptions:
-Constant dynamic pressure and constant rate of climb
-
-Source:
-N/A
-
-Inputs:
-segment.climb_rate                          [meters/second]
-segment.dynamic_pressure                    [pascals]
-segment.altitude_start                      [meters]
-segment.altitude_end                        [meters]
-state.numerics.dimensionless.control_points [Unitless]
-conditions.freestream.density               [kilograms/meter^3]
-
-Outputs:
-conditions.frames.inertial.velocity_vector  [meters/second]
-conditions.frames.inertial.position_vector  [meters]
-conditions.freestream.altitude              [meters]
-
-Properties Used:
-N/A
-
-
-
- -

◆ initialize_conditions() [5/11]

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Missions.Segments.Climb.Constant_Mach_Constant_Rate.initialize_conditions ( segment,
 state 
)
-
-
Sets the specified conditions which are given for the segment type.
-
-Assumptions:
-Constant Mach number, with a constant rate of climb
-
-Source:
-N/A
-
-Inputs:
-segment.climb_rate                          [meters/second]
-segment.mach                                [Unitless]
-segment.altitude_start                      [meters]
-segment.altitude_end                        [meters]
-state.numerics.dimensionless.control_points [Unitless]
-conditions.freestream.density               [kilograms/meter^3]
-
-Outputs:
-conditions.frames.inertial.velocity_vector  [meters/second]
-conditions.frames.inertial.position_vector  [meters]
-conditions.freestream.altitude              [meters]
-
-Properties Used:
-N/A
-
-
-
- -

◆ initialize_conditions() [6/11]

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Missions.Segments.Climb.Constant_Mach_Linear_Altitude.initialize_conditions ( segment,
 state 
)
-
-
Sets the specified conditions which are given for the segment type.
-
-Assumptions:
-Constrant dynamic pressure and constant rate of climb
-
-Source:
-N/A
-
-Inputs:
-segment.mach                                [unitless]
-segment.dynamic_pressure                    [pascals]
-segment.altitude_start                      [meters]
-segment.altitude_end                        [meters]
-segment.distance                            [meters]
-
-Outputs:
-conditions.frames.inertial.velocity_vector  [meters/second]
-conditions.frames.inertial.position_vector  [meters]
-conditions.freestream.altitude              [meters]
-conditions.frames.inertial.time             [seconds]
-
-Properties Used:
-N/A
-
-
-
- -

◆ initialize_conditions() [7/11]

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Missions.Segments.Climb.Constant_Mach_Constant_Angle.initialize_conditions ( segment,
 state 
)
-
-
Sets the specified conditions which are given for the segment type.
-
-Assumptions:
-Constant Mach number, with a constant angle of climb
-
-Source:
-N/A
-
-Inputs:
-segment.climb_angle                         [radians]
-segment.mach                                [Unitless]
-segment.altitude_start                      [meters]
-segment.altitude_end                        [meters]
-state.numerics.dimensionless.control_points [Unitless]
-conditions.freestream.density               [kilograms/meter^3]
-
-Outputs:
-conditions.frames.inertial.velocity_vector  [meters/second]
-conditions.frames.inertial.position_vector  [meters]
-conditions.freestream.altitude              [meters]
-
-Properties Used:
-N/A
-
-
-
- -

◆ initialize_conditions() [8/11]

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Missions.Segments.Climb.Linear_Speed_Constant_Rate.initialize_conditions ( segment,
 state 
)
-
-
Sets the specified conditions which are given for the segment type.
-
-Assumptions:
-Linearly changing airspeed, with a constant rate of climb
-
-Source:
-N/A
-
-Inputs:
-segment.climb_rate                          [meters/second]
-segment.air_speed_start                     [meters/second]
-segment.air_speed_end                       [meters/second]
-segment.altitude_end                        [meters]
-state.numerics.dimensionless.control_points [Unitless]
-conditions.freestream.density               [kilograms/meter^3]
-
-Outputs:
-conditions.frames.inertial.velocity_vector  [meters/second]
-conditions.frames.inertial.position_vector  [meters]
-conditions.freestream.altitude              [meters]
-
-Properties Used:
-N/A
-
-
-
- -

◆ initialize_conditions() [9/11]

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Missions.Segments.Climb.Linear_Mach_Constant_Rate.initialize_conditions ( segment,
 state 
)
-
-
Sets the specified conditions which are given for the segment type.
-
-Assumptions:
-Linearly changing mach number, with a constant rate of climb
-
-Source:
-N/A
-
-Inputs:
-segment.climb_rate                          [meters/second]
-segment.mach_start                          [Unitless]
-segment.mach_end                            [Unitless]
-segment.altitude_end                        [meters]
-state.numerics.dimensionless.control_points [Unitless]
-conditions.freestream.density               [kilograms/meter^3]
-
-Outputs:
-conditions.frames.inertial.velocity_vector  [meters/second]
-conditions.frames.inertial.position_vector  [meters]
-conditions.freestream.altitude              [meters]
-
-Properties Used:
-N/A
-
-
-
- -

◆ initialize_conditions() [10/11]

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Missions.Segments.Climb.Constant_EAS_Constant_Rate.initialize_conditions ( segment,
 state 
)
-
-
Sets the specified conditions which are given for the segment type.
-
-Assumptions:
-Constant true airspeed with a constant rate of climb
-
-Source:
-N/A
-
-Inputs:
-segment.climb_rate                          [meters/second]
-segment.equivalent_air_speed                [meters/second]
-segment.altitude_start                      [meters]
-segment.altitude_end                        [meters]
-state.numerics.dimensionless.control_points [Unitless]
-conditions.freestream.density               [kilograms/meter^3]
-
-Outputs:
-conditions.frames.inertial.velocity_vector  [meters/second]
-conditions.frames.inertial.position_vector  [meters]
-conditions.freestream.altitude              [meters]
-
-Properties Used:
-N/A
-
-
-
- -

◆ initialize_conditions() [11/11]

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Missions.Segments.Climb.Constant_Throttle_Constant_Speed.initialize_conditions ( segment,
 state 
)
-
-
Sets the specified conditions which are given for the segment type.
-
-Assumptions:
-Constant throttle estting, with a constant true airspeed
-
-Source:
-N/A
-
-Inputs:
-segment.air_speed                           [meters/second]
-segment.throttle                            [Unitless]
-segment.altitude_start                      [meters]
-segment.altitude_end                        [meters]
-state.numerics.dimensionless.control_points [Unitless]
-conditions.freestream.density               [kilograms/meter^3]
-
-Outputs:
-conditions.frames.inertial.velocity_vector  [meters/second]
-conditions.propulsion.throttle              [Unitless]
-
-Properties Used:
-N/A
-
-
-
- -

◆ initialize_conditions_unpack_unknowns()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Missions.Segments.Climb.Constant_Dynamic_Pressure_Constant_Angle.initialize_conditions_unpack_unknowns ( segment,
 state 
)
-
-
Sets the specified conditions which are given for the segment type.
-
-Assumptions:
-Constrant dynamic pressure and constant rate of climb
-
-Source:
-N/A
-
-Inputs:
-segment.climb_angle                         [radians]
-segment.dynamic_pressure                    [pascals]
-segment.altitude_start                      [meters]
-segment.altitude_end                        [meters]
-state.numerics.dimensionless.control_points [unitless]
-conditions.freestream.density               [kilograms/meter^3]
-state.unknowns.throttle                     [unitless]
-state.unknowns.body_angle                   [radians]
-state.unknowns.altitudes                    [meter]
-
-Outputs:
-conditions.frames.inertial.velocity_vector  [meters/second]
-conditions.frames.inertial.position_vector  [meters]
-conditions.propulsion.throttle              [unitless]
-conditions.frames.body.inertial_rotations   [radians]
-
-Properties Used:
-N/A
-
-
-
- -

◆ objective()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Missions.Segments.Climb.Optimized.objective ( segment,
 state 
)
-
-
This function pulls the objective from the results of flying the segment and returns it to the optimizer
-
-    Inputs:
-    state
-    
-    Outputs:
-    state.objective_value [float]
-
-
- -

◆ residual_total_forces() [1/2]

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def SUAVE.Methods.Missions.Segments.Climb.Common.residual_total_forces ( segment,
 state 
)
-
-
Takes the summation of forces and makes a residual from the accelerations.
-
-Assumptions:
-No higher order terms.
-
-Source:
-N/A
-
-Inputs:
-state.conditions.frames.inertial.total_force_vector   [Newtons]
-sstate.conditions.frames.inertial.acceleration_vector [meter/second^2]
-state.conditions.weights.total_mass                   [kilogram]
-
-Outputs:
-state.residuals.forces                                [Unitless]
-
-Properties Used:
-N/A
-
-
-
- -

◆ residual_total_forces() [2/2]

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def SUAVE.Methods.Missions.Segments.Climb.Constant_Dynamic_Pressure_Constant_Angle.residual_total_forces ( segment,
 state 
)
-
-
Takes the summation of forces and makes a residual from the accelerations and altitude.
-
-Assumptions:
-No higher order terms.
-
-Source:
-N/A
-
-Inputs:
-state.conditions.frames.inertial.total_force_vector   [Newtons]
-sstate.conditions.frames.inertial.acceleration_vector [meter/second^2]
-state.conditions.weights.total_mass                   [kilogram]
-state.conditions.freestream.altitude                  [meter]
-
-Outputs:
-state.residuals.forces                                [Unitless]
-
-Properties Used:
-N/A
-
-
-
- -

◆ solve_linear_speed_constant_rate()

- -
-
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def SUAVE.Methods.Missions.Segments.Climb.Optimized.solve_linear_speed_constant_rate ( segment,
 state 
)
-
-
The sets up an solves a mini segment that is a linear speed constant rate segment. The results become the initial conditions for an optimized climb segment later
-
-Assumptions:
-N/A
-
-Source:
-N/A
-
-Inputs:
-segment.altitude_start             [meters]
-segment.altitude_end               [meters]
-segment.air_speed_start            [meters/second]
-segment.air_speed_end              [meters/second]
-segment.analyses                   [Data]
-state.numerics                     [Data]
-
-Outputs:
-state.unknowns.throttle            [Unitless]
-state.unknowns.body_angle          [Radians]
-state.unknowns.flight_path_angle   [Radians]
-state.unknowns.velocity            [meters/second]
-
-Properties Used:
-N/A    
-
-
- -

◆ unpack_body_angle()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Missions.Segments.Climb.Constant_Throttle_Constant_Speed.unpack_body_angle ( segment,
 state 
)
-
-
Unpacks and sets the proper value for body angle
-
-Assumptions:
-N/A
-
-Source:
-N/A
-
-Inputs:
-state.unknowns.body_angle                      [Radians]
-
-Outputs:
-state.conditions.frames.body.inertial_rotation [Radians]
-
-Properties Used:
-N/A
-
-
-
- -

◆ unpack_unknowns() [1/2]

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def SUAVE.Methods.Missions.Segments.Climb.Common.unpack_unknowns ( segment,
 state 
)
-
-
Unpacks the unknowns set in the mission to be available for the mission.
-
-Assumptions:
-N/A
-
-Source:
-N/A
-
-Inputs:
-state.unknowns.throttle            [Unitless]
-state.unknowns.body_angle          [Radians]
-
-Outputs:
-state.conditions.propulsion.throttle            [Unitless]
-state.conditions.frames.body.inertial_rotations [Radians]
-
-Properties Used:
-N/A
-
-
-
- -

◆ unpack_unknowns() [2/2]

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def SUAVE.Methods.Missions.Segments.Climb.Optimized.unpack_unknowns ( segment,
 state 
)
-
-
Unpacks the unknowns set in the mission to be available for the mission.
-
-Assumptions:
-N/A
-
-Source:
-N/A
-
-Inputs:
-state.unknowns.throttle            [Unitless]
-state.unknowns.body_angle          [Radians]
-state.unknowns.flight_path_angle   [Radians]
-state.unknowns.velocity            [meters/second]
-segment.altitude_start             [meters]
-segment.altitude_end               [meters]
-segment.air_speed_start            [meters/second]
-segment.air_speed_end              [meters/second]
-
-Outputs:
-state.conditions.propulsion.throttle            [Unitless]
-state.conditions.frames.body.inertial_rotations [Radians]
-conditions.frames.inertial.velocity_vector      [meters/second]
-
-Properties Used:
-N/A
-
-
-
- -

◆ update_differentials()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Missions.Segments.Climb.Optimized.update_differentials ( segment,
 state 
)
-
-
On each iteration creates the differentials and integration funcitons from knowns about the problem. Sets the time at each point. Must return in dimensional time, with t[0] = 0. This is different from the common method as it also includes the scaling of operators.
-
-    Assumptions:
-    Works with a segment discretized in vertical position, altitude
-
-    Inputs:
-    state.numerics.dimensionless.control_points      [Unitless]
-    state.numerics.dimensionless.differentiate       [Unitless]
-    state.numerics.dimensionless.integrate           [Unitless]
-    state.conditions.frames.inertial.position_vector [meter]
-    state.conditions.frames.inertial.velocity_vector [meter/second]
-    
-
-    Outputs:
-    state.conditions.frames.inertial.time            [second]
-
-
- -

◆ update_differentials_altitude() [1/2]

- -
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def SUAVE.Methods.Missions.Segments.Climb.Common.update_differentials_altitude ( segment,
 state 
)
-
-
On each iteration creates the differentials and integration funcitons from knowns about the problem. Sets the time at each point. Must return in dimensional time, with t[0] = 0
-
-    Assumptions:
-    Works with a segment discretized in vertical position, altitude
-
-    Inputs:
-    state.numerics.dimensionless.control_points      [Unitless]
-    state.numerics.dimensionless.differentiate       [Unitless]
-    state.numerics.dimensionless.integrate           [Unitless]
-    state.conditions.frames.inertial.position_vector [meter]
-    state.conditions.frames.inertial.velocity_vector [meter/second]
-    
-
-    Outputs:
-    state.conditions.frames.inertial.time            [second]
-
-
- -

◆ update_differentials_altitude() [2/2]

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-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Missions.Segments.Climb.Constant_Throttle_Constant_Speed.update_differentials_altitude ( segment,
 state 
)
-
-
On each iteration creates the differentials and integration funcitons from knowns about the problem. Sets the time at each point. Must return in dimensional time, with t[0] = 0
-
-Assumptions:
-Constant throttle setting, with a constant true airspeed.
-
-Source:
-N/A
-
-Inputs:
-segment.climb_angle                         [radians]
-state.conditions.frames.inertial.velocity_vector [meter/second]
-segment.altitude_start                      [meters]
-segment.altitude_end                        [meters]
-
-Outputs:
-state.conditions.frames.inertial.time       [seconds]
-conditions.frames.inertial.position_vector  [meters]
-conditions.freestream.altitude              [meters]
-
-Properties Used:
-N/A
-
-
-
-
-
- - - - diff --git a/_site/doxygen/group__Methods-Missions-Segments-Climb.js b/_site/doxygen/group__Methods-Missions-Segments-Climb.js deleted file mode 100644 index 179153ed..00000000 --- a/_site/doxygen/group__Methods-Missions-Segments-Climb.js +++ /dev/null @@ -1,28 +0,0 @@ -var group__Methods_Missions_Segments_Climb = -[ - [ "cache_inputs", "group__Methods-Missions-Segments-Climb.html#ga5ec6e7e89ae5204a6bbc4518b9ceca73", null ], - [ "constraints", "group__Methods-Missions-Segments-Climb.html#ga9d57e92ca2c358a479e9bfdc49dc4ac1", null ], - [ "expand_state", "group__Methods-Missions-Segments-Climb.html#gabdde25a995acf46c265e0e6fab34e8b2", null ], - [ "initialize_conditions", "group__Methods-Missions-Segments-Climb.html#gaf50de17ff1541146247a44d338b28768", null ], - [ "initialize_conditions", "group__Methods-Missions-Segments-Climb.html#ga6e68cb34033fbe00aac9627de12986fc", null ], - [ "initialize_conditions", "group__Methods-Missions-Segments-Climb.html#gafec7759517a07b28bee9be68267d6f91", null ], - [ "initialize_conditions", "group__Methods-Missions-Segments-Climb.html#gae30d8b553e31793b12ea7b5b769adf67", null ], - [ "initialize_conditions", "group__Methods-Missions-Segments-Climb.html#ga7ea38cf00e0e00585da25a0888f94a45", null ], - [ "initialize_conditions", "group__Methods-Missions-Segments-Climb.html#ga0227df0558df5ba16ade99872b6d3ebb", null ], - [ "initialize_conditions", "group__Methods-Missions-Segments-Climb.html#ga82b7151ae7fcfb604dbbddb3754008ff", null ], - [ "initialize_conditions", "group__Methods-Missions-Segments-Climb.html#ga00600dbf3ab12a10572a5f4980279c82", null ], - [ "initialize_conditions", "group__Methods-Missions-Segments-Climb.html#ga39a8d04132b0d01e604ca2761da5033f", null ], - [ "initialize_conditions", "group__Methods-Missions-Segments-Climb.html#gab2b400ae79a4a2f0d8694c20512f3afe", null ], - [ "initialize_conditions", "group__Methods-Missions-Segments-Climb.html#ga7cf88701a5d299ccd5d99cee94fd570e", null ], - [ "initialize_conditions_unpack_unknowns", "group__Methods-Missions-Segments-Climb.html#gaa128a9c20b00aac7104d6f24119b9447", null ], - [ "objective", "group__Methods-Missions-Segments-Climb.html#gafbdcd0f752087b5ec8b144fd917ec3e5", null ], - [ "residual_total_forces", "group__Methods-Missions-Segments-Climb.html#ga8817bf89f7c17d350fc861cb83a476c3", null ], - [ "residual_total_forces", "group__Methods-Missions-Segments-Climb.html#gafc8a7871277f15c01aa0c951f4f1eef1", null ], - [ "solve_linear_speed_constant_rate", "group__Methods-Missions-Segments-Climb.html#gabecf74a86a38e945e7855fbf6ed09800", null ], - [ "unpack_body_angle", "group__Methods-Missions-Segments-Climb.html#gaec4a6e3dad562d56f0cff0cd839a5800", null ], - [ "unpack_unknowns", "group__Methods-Missions-Segments-Climb.html#ga560db4e14a7bc0aed412880b7370893f", null ], - [ "unpack_unknowns", "group__Methods-Missions-Segments-Climb.html#gaeb0685a1f445cbaba03c97c00106669b", null ], - [ "update_differentials", "group__Methods-Missions-Segments-Climb.html#ga8014ac487703c19bfbb00d70a6d9971a", null ], - [ "update_differentials_altitude", "group__Methods-Missions-Segments-Climb.html#ga554da51f265e8299ebef51b7a832f48b", null ], - [ "update_differentials_altitude", "group__Methods-Missions-Segments-Climb.html#ga052a29792178588704d70ef919ed2072", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Methods-Missions-Segments-Common.html b/_site/doxygen/group__Methods-Missions-Segments-Common.html deleted file mode 100644 index 8668b7a6..00000000 --- a/_site/doxygen/group__Methods-Missions-Segments-Common.html +++ /dev/null @@ -1,1237 +0,0 @@ - - - - - - - -SUAVE: Common - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
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- - - - - - -
-
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Climb mission methods containing the functions for setting up and solving a mission. -More...

- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Functions

def SUAVE.Methods.Missions.Segments.Common.Aerodynamics.update_altitude (segment, state)
 
def SUAVE.Methods.Missions.Segments.Common.Aerodynamics.update_atmosphere (segment, state)
 
def SUAVE.Methods.Missions.Segments.Common.Aerodynamics.update_freestream (segment, state)
 
def SUAVE.Methods.Missions.Segments.Common.Aerodynamics.update_aerodynamics (segment, state)
 
def SUAVE.Methods.Missions.Segments.Common.Aerodynamics.update_stability (segment, state)
 
def SUAVE.Methods.Missions.Segments.Common.Energy.initialize_battery (segment, state)
 
def SUAVE.Methods.Missions.Segments.Common.Energy.update_thrust (segment, state)
 
def SUAVE.Methods.Missions.Segments.Common.Frames.initialize_inertial_position (segment, state)
 
def SUAVE.Methods.Missions.Segments.Common.Frames.initialize_time (segment, state)
 
def SUAVE.Methods.Missions.Segments.Common.Frames.initialize_planet_position (segment, state)
 
def SUAVE.Methods.Missions.Segments.Common.Frames.update_planet_position (segment, state)
 
def SUAVE.Methods.Missions.Segments.Common.Frames.update_orientations (segment, state)
 
def SUAVE.Methods.Missions.Segments.Common.Frames.update_forces (segment, state)
 
def SUAVE.Methods.Missions.Segments.Common.Frames.integrate_inertial_horizontal_position (segment, state)
 
def SUAVE.Methods.Missions.Segments.Common.Frames.update_acceleration (segment, state)
 
def SUAVE.Methods.Missions.Segments.Common.Numerics.initialize_differentials_dimensionless (segment, state)
 
def SUAVE.Methods.Missions.Segments.Common.Numerics.update_differentials_time (segment, state)
 
def SUAVE.Methods.Missions.Segments.Common.Sub_Segments.expand_sub_segments (segment, state)
 
def SUAVE.Methods.Missions.Segments.Common.Sub_Segments.update_sub_segments (segment, state)
 
def SUAVE.Methods.Missions.Segments.Common.Sub_Segments.finalize_sub_segments (segment, state)
 
def SUAVE.Methods.Missions.Segments.Common.Sub_Segments.sequential_sub_segments (segment, state)
 
def SUAVE.Methods.Missions.Segments.Common.Weights.initialize_weights (segment, state)
 
def SUAVE.Methods.Missions.Segments.Common.Weights.update_gravity (segment, state)
 
def SUAVE.Methods.Missions.Segments.Common.Weights.update_weights (segment, state)
 
-

Detailed Description

-

Climb mission methods containing the functions for setting up and solving a mission.

-

Function Documentation

- -

◆ expand_sub_segments()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Missions.Segments.Common.Sub_Segments.expand_sub_segments ( segment,
 state 
)
-
-
Fills in the segments to a mission with data, sets initials data if necessary
-
-    Assumptions:
-    N/A
-    
-    Inputs:
-    N/A
-        
-    Outputs:
-    N/A
-
-    Properties Used:
-    N/A
-
-
- -

◆ finalize_sub_segments()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Missions.Segments.Common.Sub_Segments.finalize_sub_segments ( segment,
 state 
)
-
-
Sets the conditions in each sub segment for a mission
-
-    Assumptions:
-    N/A
-    
-    Inputs:
-    N/A
-        
-    Outputs:
-    N/A
-
-    Properties Used:
-    N/A
-
-
- -

◆ initialize_battery()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Missions.Segments.Common.Energy.initialize_battery ( segment,
 state 
)
-
-
Sets the initial battery energy at the start of the mission
-
-    Assumptions:
-    N/A
-    
-    Inputs:
-        state.initials.conditions:
-            propulsion.battery_energy    [Joules]
-        segment.battery_energy           [Joules]
-        
-    Outputs:
-        state.conditions:
-            propulsion.battery_energy    [Joules]
-
-    Properties Used:
-    N/A
-
-
- -

◆ initialize_differentials_dimensionless()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Missions.Segments.Common.Numerics.initialize_differentials_dimensionless ( segment,
 state 
)
-
-
Discretizes the differential operators
-
-    Assumptions:
-    N/A
-    
-    Inputs:
-        state.numerics:
-            number_control_points [int]
-            discretization_method [function]
-        
-    Outputs:
-        numerics.dimensionless:           
-            control_points        [array]
-            differentiate         [array]
-            integrate             [array]
-
-    Properties Used:
-    N/A
-
-
- -

◆ initialize_inertial_position()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Missions.Segments.Common.Frames.initialize_inertial_position ( segment,
 state 
)
-
-
Sets the initial location of the vehicle at the start of the segment
-
-    Assumptions:
-    Only used if there is an initial condition
-    
-    Inputs:
-        state.initials.conditions:
-            frames.inertial.position_vector   [meters]
-        state.conditions:           
-            frames.inertial.position_vector   [meters]
-        
-    Outputs:
-        state.conditions:           
-            frames.inertial.position_vector   [meters]
-
-    Properties Used:
-    N/A
-
-
- -

◆ initialize_planet_position()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Missions.Segments.Common.Frames.initialize_planet_position ( segment,
 state 
)
-
-
Sets the initial location of the vehicle relative to the planet at the start of the segment
-
-    Assumptions:
-    Only used if there is an initial condition
-    
-    Inputs:
-        state.initials.conditions:
-            frames.planet.longitude [Radians]
-            frames.planet.latitude  [Radians]
-        segment.longitude           [Radians]
-        segment.latitude            [Radians]
-
-    Outputs:
-        state.conditions:           
-            frames.planet.latitude  [Radians]
-            frames.planet.longitude [Radians]
-
-    Properties Used:
-    N/A
-
-
- -

◆ initialize_time()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Missions.Segments.Common.Frames.initialize_time ( segment,
 state 
)
-
-
Sets the initial time of the vehicle at the start of the segment
-
-    Assumptions:
-    Only used if there is an initial condition
-    
-    Inputs:
-        state.initials.conditions:
-            frames.inertial.time     [seconds]
-            frames.planet.start_time [seconds]
-        state.conditions:           
-            frames.inertial.time     [seconds]
-        segment.start_time           [seconds]
-        
-    Outputs:
-        state.conditions:           
-            frames.inertial.time     [seconds]
-            frames.planet.start_time [seconds]
-
-    Properties Used:
-    N/A
-
-
- -

◆ initialize_weights()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Missions.Segments.Common.Weights.initialize_weights ( segment,
 state 
)
-
-
Sets the initial weight of the vehicle at the start of the segment
-
-    Assumptions:
-    Only used if there is an initial condition
-    
-    Inputs:
-        state.initials.conditions:
-            weights.total_mass     [newtons]
-        state.conditions:           
-            weights.total_mass     [newtons]
-        
-    Outputs:
-        state.conditions:           
-            weights.total_mass     [newtons]
-
-    Properties Used:
-    N/A
-
-
- -

◆ integrate_inertial_horizontal_position()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Missions.Segments.Common.Frames.integrate_inertial_horizontal_position ( segment,
 state 
)
-
-
Determines how far the airplane has traveled. 
-
-    Assumptions:
-    Assumes a flat earth, this is planar motion.
-    
-    Inputs:
-        state.conditions:
-            frames.inertial.position_vector [meters]
-            frames.inertial.velocity_vector [meters/second]
-        state.numerics.time.integrate       [float]
-        
-    Outputs:
-        state.conditions:           
-            frames.inertial.position_vector [meters]
-
-    Properties Used:
-    N/A
-
-
- -

◆ sequential_sub_segments()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Missions.Segments.Common.Sub_Segments.sequential_sub_segments ( segment,
 state 
)
-
-
Evaluates all the segments in a mission one by one
-
-    Assumptions:
-    N/A
-    
-    Inputs:
-    N/A
-        
-    Outputs:
-    N/A
-
-    Properties Used:
-    N/A
-
-
- -

◆ update_acceleration()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Missions.Segments.Common.Frames.update_acceleration ( segment,
 state 
)
-
-
Differentiates the velocity vector to get accelerations
-
-    Assumptions:
-    Assumes a flat earth, this is planar motion.
-    
-    Inputs:
-        state.conditions:
-            frames.inertial.velocity_vector     [meters/second]
-        state.numerics.time.differentiate       [float]
-        
-    Outputs:
-        state.conditions:           
-            frames.inertial.acceleration_vector [meters]
-
-    Properties Used:
-    N/A
-
-
- -

◆ update_aerodynamics()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Missions.Segments.Common.Aerodynamics.update_aerodynamics ( segment,
 state 
)
-
-
Gets aerodynamics conditions
-
-    Assumptions:
-    +X out nose
-    +Y out starboard wing
-    +Z down
-
-    Inputs:
-        segment.analyses.aerodynamics_model                  [Function]
-        aerodynamics_model.settings.maximum_lift_coefficient [unitless]
-        aerodynamics_model.geometry.reference_area           [meter^2]
-        state.conditions.freestream.dynamic_pressure         [pascals]
-
-    Outputs:
-        conditions.aerodynamics.lift_coefficient [unitless]
-        conditions.aerodynamics.drag_coefficient [unitless]
-        conditions.frames.wind.lift_force_vector [newtons]
-        conditions.frames.wind.drag_force_vector [newtons]
-
-    Properties Used:
-    N/A
-
-
-
- -

◆ update_altitude()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Missions.Segments.Common.Aerodynamics.update_altitude ( segment,
 state 
)
-
-
Updates freestream altitude from inertial position
-    
-    Assumptions:
-    N/A
-    
-    Inputs:
-        state.conditions:
-            frames.inertial.position_vector [meters]
-    Outputs:
-        state.conditions:
-            freestream.altitude             [meters]
-  
-    Properties Used:
-    N/A
-
-
- -

◆ update_atmosphere()

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def SUAVE.Methods.Missions.Segments.Common.Aerodynamics.update_atmosphere ( segment,
 state 
)
-
-
Computes conditions of the atmosphere at given altitudes
-
-    Assumptions:
-    N/A
-    
-    Inputs:
-        state.conditions:
-            freestream.altitude    [meters]
-        segment.analyses.atmoshere [Function]
-        
-    Outputs:
-        state.conditions:
-            freestream.pressure          [pascals]
-            freestream.temperature       [kelvin]
-            freestream.density           [kilogram/meter^3]
-            freestream.speed_of_sound    [meter/second]
-            freestream.dynamic_viscosity [pascals-seconds]
-            
-    Properties Used:
-    N/A
-
-
- -

◆ update_differentials_time()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Missions.Segments.Common.Numerics.update_differentials_time ( segment,
 state 
)
-
-
Scales the differential operators (integrate and differentiate) based on mission time
-
-    Assumptions:
-    N/A
-    
-    Inputs:
-        numerics.dimensionless:           
-            control_points                    [array]
-            differentiate                     [array]
-            integrate                         [array]
-        state.conditions.frames.inertial.time [seconds]
-        
-    Outputs:
-        numerics.time:           
-            control_points        [array]
-            differentiate         [array]
-            integrate             [array]
-
-    Properties Used:
-    N/A
-
-
- -

◆ update_forces()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Missions.Segments.Common.Frames.update_forces ( segment,
 state 
)
-
-
Summation of forces: lift, drag, thrust, weight. Future versions will include new definitions of dreams, FAA, money, and reality.
-
-    Assumptions:
-    You only have these 4 forces applied to the vehicle
-    
-    Inputs:
-    state.conditions:
-        frames.wind.lift_force_vector          [newtons]
-        frames.wind.drag_force_vector          [newtons]
-        frames.inertial.gravity_force_vector   [newtons]
-        frames.body.thrust_force_vector        [newtons]
-        frames.body.transform_to_inertial      [newtons]
-        frames.wind.transform_to_inertial      [newtons]
-
-        
-    Outputs:
-        state.conditions:           
-            frames.inertial.total_force_vector [newtons]
-
-
-
-    Properties Used:
-    N/A
-
-
-
- -

◆ update_freestream()

- -
-
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def SUAVE.Methods.Missions.Segments.Common.Aerodynamics.update_freestream ( segment,
 state 
)
-
-
Computes freestream values
-    
-    Assumptions:
-    N/A
-
-    Inputs:
-        state.conditions:
-            frames.inertial.velocity_vector [meter/second]
-            freestream.density              [kilogram/meter^3]
-            freestream.speed_of_sound       [meter/second]
-            freestream.dynamic_viscosity    [pascals-seconds]
-
-    Outputs:
-        state.conditions:
-            freestream.dynamic pressure     [pascals]
-            freestream.mach number          [Unitless]
-            freestream.reynolds number      [1/meter]
-                           
-    Properties Used:
-    N/A
-
-
-
- -

◆ update_gravity()

- -
-
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def SUAVE.Methods.Missions.Segments.Common.Weights.update_gravity ( segment,
 state 
)
-
-
Sets the gravity for each part of the mission
-
-    Assumptions:
-    Fixed sea level gravity, doesn't use a gravity model yet
-    
-    Inputs:
-    segment.analyses.planet.features.sea_level_gravity [Data] 
-        
-    Outputs:
-    state.conditions.freestream.gravity [meters/second^2]
-
-    Properties Used:
-    N/A
-
-
- -

◆ update_orientations()

- -
-
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def SUAVE.Methods.Missions.Segments.Common.Frames.update_orientations ( segment,
 state 
)
-
-
Updates the orientation of the vehicle throughout the mission for each relevant axis
-
-    Assumptions:
-    This assumes the vehicle has 3 frames: inertial, body, and wind. There also contains bits for stability axis which are not used. Creates tensors and solves for alpha and beta.
-    
-    Inputs:
-    state.conditions:
-        frames.inertial.velocity_vector          [meters/second]
-        frames.body.inertial_rotations           [Radians]
-    segment.analyses.planet.features.mean_radius [meters]
-    state.numerics.time.integrate                [float]
-        
-    Outputs:
-        state.conditions:           
-            aerodynamics.angle_of_attack      [Radians]
-            aerodynamics.side_slip_angle      [Radians]
-            aerodynamics.roll_angle           [Radians]
-            frames.body.transform_to_inertial [Radians]
-            frames.wind.body_rotations        [Radians]
-            frames.wind.transform_to_inertial [Radians]
-
-
-    Properties Used:
-    N/A
-
-
-
- -

◆ update_planet_position()

- -
-
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def SUAVE.Methods.Missions.Segments.Common.Frames.update_planet_position ( segment,
 state 
)
-
-
Updates the location of the vehicle relative to the Planet throughout the mission
-
-    Assumptions:
-    This is valid for small movements and times as it does not account for the rotation of the Planet beneath the vehicle
-    
-    Inputs:
-    state.conditions:
-        freestream.velocity                      [meters/second]
-        freestream.altitude                      [meters]
-        frames.body.inertial_rotations           [Radians]
-    segment.analyses.planet.features.mean_radius [meters]
-    state.numerics.time.integrate                [float]
-        
-    Outputs:
-        state.conditions:           
-            frames.planet.latitude  [Radians]
-            frames.planet.longitude [Radians]
-
-    Properties Used:
-    N/A
-
-
- -

◆ update_stability()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Missions.Segments.Common.Aerodynamics.update_stability ( segment,
 state 
)
-
-
Initiates the stability model
-
-    Assumptions:
-    N/A
-
-    Inputs:
-        state.conditions           [Data]
-        segment.analyses.stability [function]
-
-    Outputs:
-    N/A
-
-    Properties Used:
-    N/A
-
-
-
- -

◆ update_sub_segments()

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def SUAVE.Methods.Missions.Segments.Common.Sub_Segments.update_sub_segments ( segment,
 state 
)
-
-
Loops through the segments and fills them in
-
-    Assumptions:
-    N/A
-    
-    Inputs:
-    N/A
-        
-    Outputs:
-    N/A
-
-    Properties Used:
-    N/A
-
-
- -

◆ update_thrust()

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-
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def SUAVE.Methods.Missions.Segments.Common.Energy.update_thrust ( segment,
 state 
)
-
-
Evaluates the energy network to find the thrust force and mass rate
-
-    Inputs -
-        segment.analyses.energy_network    [Function]
-        state                              [Data]
-
-    Outputs -
-        state.conditions:
-           frames.body.thrust_force_vector [Newtons]
-           weights.vehicle_mass_rate       [kg/s]
-
-
-    Assumptions -
-
-
- -

◆ update_weights()

- -
-
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def SUAVE.Methods.Missions.Segments.Common.Weights.update_weights ( segment,
 state 
)
-
-
Integrate tbe mass rate to update the weights throughout a segment
-
-    Assumptions:
-    Only the energy network/propulsion system can change the mass
-    
-    Inputs:
-    state.conditions:
-        weights.total_mass              [kilograms]
-        weights.vehicle_mass_rate       [kilograms/second]
-        freestream.gravity              [meters/second^2]
-    segment.analyses.weights:
-        mass_properties.operating_empty [kilograms]
-    state.numerics.time.integrate       [array]
-        
-    Outputs:
-    state.conditions:
-        weights.total_mass                   [kilograms]
-        frames.inertial.gravity_force_vector [kilograms]
-
-    Properties Used:
-    N/A
-
-
-
-
- - - - diff --git a/_site/doxygen/group__Methods-Missions-Segments-Common.js b/_site/doxygen/group__Methods-Missions-Segments-Common.js deleted file mode 100644 index 9d1e50aa..00000000 --- a/_site/doxygen/group__Methods-Missions-Segments-Common.js +++ /dev/null @@ -1,27 +0,0 @@ -var group__Methods_Missions_Segments_Common = -[ - [ "expand_sub_segments", "group__Methods-Missions-Segments-Common.html#ga079e5a37c661722e1c901040dd78d544", null ], - [ "finalize_sub_segments", "group__Methods-Missions-Segments-Common.html#ga03f607d22f766fd78769caf7dc27556e", null ], - [ "initialize_battery", "group__Methods-Missions-Segments-Common.html#ga94506d993490deb6e2902784b79bb02d", null ], - [ "initialize_differentials_dimensionless", "group__Methods-Missions-Segments-Common.html#ga7277f70a1093a4c10146e45c48b88ed4", null ], - [ "initialize_inertial_position", "group__Methods-Missions-Segments-Common.html#gaf417ce9f9fc6785a6a312274f6316990", null ], - [ "initialize_planet_position", "group__Methods-Missions-Segments-Common.html#gae3fbb540567a4e08e5b0f44548328db1", null ], - [ "initialize_time", "group__Methods-Missions-Segments-Common.html#ga888fab97485f10a9335a020a6a2e818f", null ], - [ "initialize_weights", "group__Methods-Missions-Segments-Common.html#ga28afe6dccd37e6dd3e9bb5d9defc09a5", null ], - [ "integrate_inertial_horizontal_position", "group__Methods-Missions-Segments-Common.html#ga3a5b6e449d878f0c462f9b3aae5fb21e", null ], - [ "sequential_sub_segments", "group__Methods-Missions-Segments-Common.html#gac5eadfe8d73ea29bf45f9c715043f00f", null ], - [ "update_acceleration", "group__Methods-Missions-Segments-Common.html#ga1fc39f83024cb8c207f5b82baeaccf43", null ], - [ "update_aerodynamics", "group__Methods-Missions-Segments-Common.html#ga5b618bac1bc4073916460a4f76f0e4df", null ], - [ "update_altitude", "group__Methods-Missions-Segments-Common.html#gab2637dce007776f926ee1af68ba0bca6", null ], - [ "update_atmosphere", "group__Methods-Missions-Segments-Common.html#ga251ef83f6b960654414d87bc3182e181", null ], - [ "update_differentials_time", "group__Methods-Missions-Segments-Common.html#gac4217dbf63f9649cac48522146405a2b", null ], - [ "update_forces", "group__Methods-Missions-Segments-Common.html#gaf9366945be87f7cbc146b2af89ddb2dc", null ], - [ "update_freestream", "group__Methods-Missions-Segments-Common.html#ga81df0274f076e00098e713c81b3a1dd7", null ], - [ "update_gravity", "group__Methods-Missions-Segments-Common.html#ga6acbb3f963502e3d4cb49e2b0126b67e", null ], - [ "update_orientations", "group__Methods-Missions-Segments-Common.html#gab28256a8e226536e94abafb5c962101f", null ], - [ "update_planet_position", "group__Methods-Missions-Segments-Common.html#ga3f20c80c750dab6059ec090536c0b313", null ], - [ "update_stability", "group__Methods-Missions-Segments-Common.html#ga9924ff4f90b841fb8915dbd71786ed2f", null ], - [ "update_sub_segments", "group__Methods-Missions-Segments-Common.html#gab45c41851f057901a21d150205c8279a", null ], - [ "update_thrust", "group__Methods-Missions-Segments-Common.html#ga561d5582a141f6b2d2868bf3e01c0797", null ], - [ "update_weights", "group__Methods-Missions-Segments-Common.html#gab48e9a5d35173af364ff2ffc2e5be796", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Methods-Missions-Segments-Cruise.html b/_site/doxygen/group__Methods-Missions-Segments-Cruise.html deleted file mode 100644 index 68f21ece..00000000 --- a/_site/doxygen/group__Methods-Missions-Segments-Cruise.html +++ /dev/null @@ -1,1019 +0,0 @@ - - - - - - - -SUAVE: Cruise - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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Cruise mission methods containing the functions for setting up and solving a mission. -More...

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-Functions

def SUAVE.Methods.Missions.Segments.Cruise.Common.unpack_unknowns (segment, state)
 
def SUAVE.Methods.Missions.Segments.Cruise.Common.residual_total_forces (segment, state)
 
def SUAVE.Methods.Missions.Segments.Cruise.Constant_Acceleration_Constant_Altitude.initialize_conditions (segment, state)
 Constant_Accleration_Constant_Altitude.py. More...
 
def SUAVE.Methods.Missions.Segments.Cruise.Constant_Acceleration_Constant_Altitude.residual_total_forces (segment, state)
 
def SUAVE.Methods.Missions.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude.initialize_conditions (segment, state)
 
def SUAVE.Methods.Missions.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude_Loiter.initialize_conditions (segment, state)
 
def SUAVE.Methods.Missions.Segments.Cruise.Constant_Mach_Constant_Altitude.initialize_conditions (segment, state)
 
def SUAVE.Methods.Missions.Segments.Cruise.Constant_Mach_Constant_Altitude_Loiter.initialize_conditions (segment, state)
 
def SUAVE.Methods.Missions.Segments.Cruise.Constant_Pitch_Rate_Constant_Altitude.initialize_conditions (segment, state)
 
def SUAVE.Methods.Missions.Segments.Cruise.Constant_Pitch_Rate_Constant_Altitude.residual_total_forces (segment, state)
 
def SUAVE.Methods.Missions.Segments.Cruise.Constant_Pitch_Rate_Constant_Altitude.unpack_unknowns (segment, state)
 
def SUAVE.Methods.Missions.Segments.Cruise.Constant_Speed_Constant_Altitude.initialize_conditions (segment, state)
 Constant_Speed_Constant_Altitude.py. More...
 
def SUAVE.Methods.Missions.Segments.Cruise.Constant_Speed_Constant_Altitude_Loiter.initialize_conditions (segment, state)
 
-def SUAVE.Methods.Missions.Segments.Cruise.Constant_Throttle_Constant_Altitude.unpack_unknowns (segment, state)
 
def SUAVE.Methods.Missions.Segments.Cruise.Constant_Throttle_Constant_Altitude.initialize_conditions (segment, state)
 
def SUAVE.Methods.Missions.Segments.Cruise.Constant_Throttle_Constant_Altitude.solve_residuals (segment, state)
 
def SUAVE.Methods.Missions.Segments.Cruise.Variable_Cruise_Distance.initialize_cruise_distance (segment, state)
 Variable_Cruise_Distance.py. More...
 
def SUAVE.Methods.Missions.Segments.Cruise.Variable_Cruise_Distance.unknown_cruise_distance (segment, state)
 
def SUAVE.Methods.Missions.Segments.Cruise.Variable_Cruise_Distance.residual_landing_weight (segment, state)
 
-

Detailed Description

-

Cruise mission methods containing the functions for setting up and solving a mission.

-

Function Documentation

- -

◆ initialize_conditions() [1/9]

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def SUAVE.Methods.Missions.Segments.Cruise.Constant_Acceleration_Constant_Altitude.initialize_conditions ( segment,
 state 
)
-
- -

Constant_Accleration_Constant_Altitude.py.

-

Created: Jul 2014, SUAVE Team Modified: Jan 2016, E. Botero

Sets the specified conditions which are given for the segment type.
-
-Assumptions:
-Constant acceleration and constant altitude
-
-Source:
-N/A
-
-Inputs:
-segment.altitude                [meters]
-segment.air_speed_start         [meters/second]
-segment.air_speed_end           [meters/second]
-segment.acceleration            [meters/second^2]
-conditions.frames.inertial.time [seconds]
-
-Outputs:
-conditions.frames.inertial.velocity_vector  [meters/second]
-conditions.frames.inertial.position_vector  [meters]
-conditions.freestream.altitude              [meters]
-conditions.frames.inertial.time             [seconds]
-
-Properties Used:
-N/A
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- -

◆ initialize_conditions() [2/9]

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def SUAVE.Methods.Missions.Segments.Cruise.Constant_Speed_Constant_Altitude.initialize_conditions ( segment,
 state 
)
-
- -

Constant_Speed_Constant_Altitude.py.

-

Created: Jul 2014, SUAVE Team Modified: Jan 2016, E. Botero

Sets the specified conditions which are given for the segment type.
-
-Assumptions:
-Constant speed and constant altitude
-
-Source:
-N/A
-
-Inputs:
-segment.altitude                [meters]
-segment.distance                [meters]
-segment.speed                   [meters/second]
-
-Outputs:
-conditions.frames.inertial.velocity_vector  [meters/second]
-conditions.frames.inertial.position_vector  [meters]
-conditions.freestream.altitude              [meters]
-conditions.frames.inertial.time             [seconds]
-
-Properties Used:
-N/A
-
-
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- -

◆ initialize_conditions() [3/9]

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def SUAVE.Methods.Missions.Segments.Cruise.Constant_Mach_Constant_Altitude_Loiter.initialize_conditions ( segment,
 state 
)
-
-
Sets the specified conditions which are given for the segment type.
-
-Assumptions:
-Constant mach and constant altitude with set loiter time
-
-Source:
-N/A
-
-Inputs:
-segment.altitude                [meters]
-segment.time                    [seconds]
-segment.mach                    [unitless]
-
-Outputs:
-conditions.frames.inertial.velocity_vector  [meters/second]
-conditions.frames.inertial.position_vector  [meters]
-conditions.freestream.altitude              [meters]
-conditions.frames.inertial.time             [seconds]
-
-Properties Used:
-N/A
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◆ initialize_conditions() [4/9]

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def SUAVE.Methods.Missions.Segments.Cruise.Constant_Pitch_Rate_Constant_Altitude.initialize_conditions ( segment,
 state 
)
-
-
Sets the specified conditions which are given for the segment type.
-
-Assumptions:
-Constant acceleration and constant altitude
-
-Source:
-N/A
-
-Inputs:
-segment.altitude                [meters]
-segment.pitch_initial           [radians]
-segment.pitch_final             [radians]
-segment.pitch_rate              [radians/second]
-
-Outputs:
-conditions.frames.body.inertial_rotations   [radians/second]
-conditions.frames.inertial.position_vector  [meters]
-conditions.freestream.altitude              [meters]
-conditions.frames.inertial.time             [seconds]
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-Properties Used:
-N/A
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◆ initialize_conditions() [5/9]

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def SUAVE.Methods.Missions.Segments.Cruise.Constant_Mach_Constant_Altitude.initialize_conditions ( segment,
 state 
)
-
-
Sets the specified conditions which are given for the segment type.
-
-Assumptions:
-Constant mach and constant altitude
-
-Source:
-N/A
-
-Inputs:
-segment.altitude                [meters]
-segment.distance                [meters]
-segment.mach                    [unitless]
-
-Outputs:
-conditions.frames.inertial.velocity_vector  [meters/second]
-conditions.frames.inertial.position_vector  [meters]
-conditions.freestream.altitude              [meters]
-conditions.frames.inertial.time             [seconds]
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◆ initialize_conditions() [6/9]

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def SUAVE.Methods.Missions.Segments.Cruise.Constant_Speed_Constant_Altitude_Loiter.initialize_conditions ( segment,
 state 
)
-
-
Sets the specified conditions which are given for the segment type.
-
-Assumptions:
-Constant speed and constant altitude with set loiter time
-
-Source:
-N/A
-
-Inputs:
-segment.altitude                [meters]
-segment.time                    [seconds]
-segment.speed                   [meters/second]
-
-Outputs:
-conditions.frames.inertial.velocity_vector  [meters/second]
-conditions.frames.inertial.position_vector  [meters]
-conditions.freestream.altitude              [meters]
-conditions.frames.inertial.time             [seconds]
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-N/A
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◆ initialize_conditions() [7/9]

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def SUAVE.Methods.Missions.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude.initialize_conditions ( segment,
 state 
)
-
-
Sets the specified conditions which are given for the segment type.
-
-Assumptions:
-Constant dynamic pressure and constant altitude
-
-Source:
-N/A
-
-Inputs:
-segment.altitude                [meters]
-segment.distance                [meters]
-segment.dynamic_pressure        [pascals]
-
-Outputs:
-conditions.frames.inertial.velocity_vector  [meters/second]
-conditions.frames.inertial.position_vector  [meters]
-conditions.freestream.altitude              [meters]
-conditions.frames.inertial.time             [seconds]
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-N/A
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◆ initialize_conditions() [8/9]

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def SUAVE.Methods.Missions.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude_Loiter.initialize_conditions ( segment,
 state 
)
-
-
Sets the specified conditions which are given for the segment type.
-
-Assumptions:
-Constant dynamic pressure and constant altitude with set loiter time
-
-Source:
-N/A
-
-Inputs:
-segment.altitude                [meters]
-segment.time                    [seconds]
-segment.dynamic_pressure        [pascals]
-
-Outputs:
-conditions.frames.inertial.velocity_vector  [meters/second]
-conditions.frames.inertial.position_vector  [meters]
-conditions.freestream.altitude              [meters]
-conditions.frames.inertial.time             [seconds]
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-Properties Used:
-N/A
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◆ initialize_conditions() [9/9]

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def SUAVE.Methods.Missions.Segments.Cruise.Constant_Throttle_Constant_Altitude.initialize_conditions ( segment,
 state 
)
-
-
Sets the specified conditions which are given for the segment type.
-
-Assumptions:
-Constant throttle and constant altitude, allows for acceleration
-
-Source:
-N/A
-
-Inputs:
-segment.altitude                             [meters]
-segment.air_speed_start                      [meters/second]
-segment.air_speed_end                        [meters/second]
-segment.throttle                             [unitless]
-segment.state.numerics.number_control_points [int]
-
-Outputs:
-state.conditions.propulsion.throttle        [unitless]
-conditions.frames.inertial.position_vector  [meters]
-conditions.freestream.altitude              [meters]
-
-Properties Used:
-N/A
-
-
-
- -

◆ initialize_cruise_distance()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Missions.Segments.Cruise.Variable_Cruise_Distance.initialize_cruise_distance ( segment,
 state 
)
-
- -

Variable_Cruise_Distance.py.

-

Created: Jul 2014, SUAVE Team Modified: Jan 2016, E. Botero

This is a method that allows your vehicle to land at prescribed landing weight
-
-Assumptions:
-N/A
-
-Source:
-N/A
-
-Inputs:
-segment.cruise_tag              [string]
-segment.distance                [meters]
-
-Outputs:
-state.unknowns.cruise_distance  [meters]
-
-Properties Used:
-N/A
-
-
-
- -

◆ residual_landing_weight()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Missions.Segments.Cruise.Variable_Cruise_Distance.residual_landing_weight ( segment,
 state 
)
-
-
This is a method that allows your vehicle to land at prescribed landing weight.
-This takes the final weight and compares it against the prescribed landing weight.
-
-Assumptions:
-N/A
-
-Source:
-N/A
-
-Inputs:
-state.segments[-1].conditions.weights.total_mass [kilogram]
-segment.target_landing_weight                    [kilogram]
-
-Outputs:
-state.residuals.landing_weight                   [kilogram]
-
-Properties Used:
-N/A
-
-
-
- -

◆ residual_total_forces() [1/3]

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Missions.Segments.Cruise.Common.residual_total_forces ( segment,
 state 
)
-
-
Calculates a residual based on forces
-
-    Assumptions:
-    The vehicle is not accelerating, doesn't use gravity
-    
-    Inputs:
-        state.conditions:
-            frames.inertial.total_force_vector [Newtons]
-            weights.total_mass                 [kg]
-        
-    Outputs:
-        state.residuals.forces [meters/second^2]
-
-    Properties Used:
-    N/A
-
-
- -

◆ residual_total_forces() [2/3]

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Missions.Segments.Cruise.Constant_Acceleration_Constant_Altitude.residual_total_forces ( segment,
 state 
)
-
-
Calculates a residual based on forces
-
-    Assumptions:
-    The vehicle is not accelerating, doesn't use gravity
-    
-    Inputs:
-        segment.acceleration                   [meters/second^2]
-        segment.state.ones_row                 [vector]
-        state.conditions:
-            frames.inertial.total_force_vector [Newtons]
-            weights.total_mass                 [kg]
-        
-    Outputs:
-        state.conditions:
-            state.residuals.forces [meters/second^2]
-
-    Properties Used:
-    N/A
-
-
- -

◆ residual_total_forces() [3/3]

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Missions.Segments.Cruise.Constant_Pitch_Rate_Constant_Altitude.residual_total_forces ( segment,
 state 
)
-
-
Calculates a residual based on forces
-
-    Assumptions:
-    The vehicle is accelerating, doesn't use gravity
-    
-    Inputs:
-    state.conditions:
-        frames.inertial.total_force_vector [Newtons]
-        weights.total_mass                 [kg]
-        frames.inertial.velocity_vector    [meters/second]
-        
-    Outputs:
-    state:
-        residuals.forces [meters/second^2]
-        conditions.frames.inertial.acceleration_vector [meters/second^2]
-
-    Properties Used:
-    N/A
-
-
- -

◆ solve_residuals()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Missions.Segments.Cruise.Constant_Throttle_Constant_Altitude.solve_residuals ( segment,
 state 
)
-
-
Calculates a residual based on forces
-
-    Assumptions:
-    The vehicle accelerates, residual on forces and to get it to the final speed
-    
-    Inputs:
-    segment.air_speed_end                  [meters/second]
-    state.conditions:
-        frames.inertial.total_force_vector [Newtons]
-        frames.inertial.velocity_vector    [meters/second]
-        weights.total_mass                 [kg]
-    state.numerics.time.differentiate
-        
-    Outputs:
-    state.residuals:
-        forces               [meters/second^2]
-        final_velocity_error [meters/second]
-    state.conditions:
-        conditions.frames.inertial.acceleration_vector [meters/second^2]
-
-    Properties Used:
-    N/A
-
-
- -

◆ unknown_cruise_distance()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Missions.Segments.Cruise.Variable_Cruise_Distance.unknown_cruise_distance ( segment,
 state 
)
-
-
This is a method that allows your vehicle to land at prescribed landing weight
-
-Assumptions:
-N/A
-
-Source:
-N/A
-
-Inputs:
-segment.cruise_tag              [string]
-state.unknowns.cruise_distance  [meters]
-
-Outputs:
-segment.distance                [meters]
-
-Properties Used:
-N/A
-
-
-
- -

◆ unpack_unknowns() [1/2]

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Missions.Segments.Cruise.Common.unpack_unknowns ( segment,
 state 
)
-
-
Unpacks the throttle setting and body angle from the solver to the mission
-
-    Assumptions:
-    N/A
-    
-    Inputs:
-        state.unknowns:
-            throttle    [Unitless]
-            body_angle  [Radians]
-        
-    Outputs:
-        state.conditions:
-            propulsion.throttle            [Unitless]
-            frames.body.inertial_rotations [Radians]
-
-    Properties Used:
-    N/A
-
-
- -

◆ unpack_unknowns() [2/2]

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Missions.Segments.Cruise.Constant_Pitch_Rate_Constant_Altitude.unpack_unknowns ( segment,
 state 
)
-
-
Unpacks the throttle setting and velocity from the solver to the mission
-
-    Assumptions:
-    N/A
-    
-    Inputs:
-        state.unknowns:
-            throttle    [Unitless]
-            velocity    [meters/second]
-        
-    Outputs:
-        state.conditions:
-            propulsion.throttle             [Unitless]
-            frames.inertial.velocity_vector [meters/second]
-
-    Properties Used:
-    N/A
-
-
-
-
- - - - diff --git a/_site/doxygen/group__Methods-Missions-Segments-Cruise.js b/_site/doxygen/group__Methods-Missions-Segments-Cruise.js deleted file mode 100644 index 41dc0574..00000000 --- a/_site/doxygen/group__Methods-Missions-Segments-Cruise.js +++ /dev/null @@ -1,21 +0,0 @@ -var group__Methods_Missions_Segments_Cruise = -[ - [ "initialize_conditions", "group__Methods-Missions-Segments-Cruise.html#gaeceef878340ee4ca38c91d9b9d4b1825", null ], - [ "initialize_conditions", "group__Methods-Missions-Segments-Cruise.html#gae83d32238010a7766ce5f6f59c665171", null ], - [ "initialize_conditions", "group__Methods-Missions-Segments-Cruise.html#gaa1662df44e801b11b5cee1cec98ddddb", null ], - [ "initialize_conditions", "group__Methods-Missions-Segments-Cruise.html#ga1225173de6209af379d294d66aae3765", null ], - [ "initialize_conditions", "group__Methods-Missions-Segments-Cruise.html#ga2392289bf9075cc49a7e82593eff969b", null ], - [ "initialize_conditions", "group__Methods-Missions-Segments-Cruise.html#ga5629f4cd6d3db707b418a90e3b83c4cf", null ], - [ "initialize_conditions", "group__Methods-Missions-Segments-Cruise.html#ga8fe5b4a602fc2842046270b062c0725f", null ], - [ "initialize_conditions", "group__Methods-Missions-Segments-Cruise.html#ga31753e9e792ee9b624a0b0c52a339839", null ], - [ "initialize_conditions", "group__Methods-Missions-Segments-Cruise.html#gafb9a53c01768546934f739572cba457e", null ], - [ "initialize_cruise_distance", "group__Methods-Missions-Segments-Cruise.html#ga5c2953ac08ccf0627c021f6ed58b2bf5", null ], - [ "residual_landing_weight", "group__Methods-Missions-Segments-Cruise.html#gab9d38bfe2130ae943109fd2b9daaf8bd", null ], - [ "residual_total_forces", "group__Methods-Missions-Segments-Cruise.html#gad0c58596842a06b26ce45ae82de1f553", null ], - [ "residual_total_forces", "group__Methods-Missions-Segments-Cruise.html#ga94d5d0eeaad27145f52e2281d66b518d", null ], - [ "residual_total_forces", "group__Methods-Missions-Segments-Cruise.html#gadb8015617e942644480f81b10df76f6d", null ], - [ "solve_residuals", "group__Methods-Missions-Segments-Cruise.html#gac7b8afbde2853ba75656032eb9f71e40", null ], - [ "unknown_cruise_distance", "group__Methods-Missions-Segments-Cruise.html#gaf312be28fd54ce6ef3252aa138066d97", null ], - [ "unpack_unknowns", "group__Methods-Missions-Segments-Cruise.html#gac16b02c25a09a594b81e8a5846c5ec12", null ], - [ "unpack_unknowns", "group__Methods-Missions-Segments-Cruise.html#ga1a0168bbee3e90402744d6b35a6b1e74", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Methods-Missions-Segments-Descent.html b/_site/doxygen/group__Methods-Missions-Segments-Descent.html deleted file mode 100644 index cbe16eb5..00000000 --- a/_site/doxygen/group__Methods-Missions-Segments-Descent.html +++ /dev/null @@ -1,381 +0,0 @@ - - - - - - - -SUAVE: Descent - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
-
- - - -
-
- -
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-
- -
- -
-
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- -
- -
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-
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-
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Descent mission methods containing the functions for setting up and solving a mission. -More...

- - - - - - - - - - - - -

-Functions

def SUAVE.Methods.Missions.Segments.Descent.Constant_EAS_Constant_Rate.initialize_conditions (segment, state)
 
def SUAVE.Methods.Missions.Segments.Descent.Constant_Speed_Constant_Angle.initialize_conditions (segment, state)
 
def SUAVE.Methods.Missions.Segments.Descent.Constant_Speed_Constant_Angle_Noise.expand_state (segment, state)
 
def SUAVE.Methods.Missions.Segments.Descent.Constant_Speed_Constant_Angle_Noise.initialize_conditions (segment, state)
 
def SUAVE.Methods.Missions.Segments.Descent.Constant_Speed_Constant_Rate.initialize_conditions (segment, state)
 
-

Detailed Description

-

Descent mission methods containing the functions for setting up and solving a mission.

-

Function Documentation

- -

◆ expand_state()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Missions.Segments.Descent.Constant_Speed_Constant_Angle_Noise.expand_state ( segment,
 state 
)
-
-
Makes all vectors in the state the same size.
-
-Assumptions:
-A 4 km threshold, this discretizes the mission to take measurements at the right place for certification maneuvers.
-
-Source:
-N/A
-
-Inputs:
-state.numerics.number_control_points  [Unitless]
-segment.descent_angle                 [Radians]
-segment.air_speed                     [meters/second]
- 
-Outputs:
-state.numerics.number_control_points
-
-Properties Used:
-N/A
-
-
-
- -

◆ initialize_conditions() [1/4]

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Missions.Segments.Descent.Constant_Speed_Constant_Rate.initialize_conditions ( segment,
 state 
)
-
-
Sets the specified conditions which are given for the segment type.
-
-Assumptions:
-Constant speed and constant descent rate
-
-Source:
-N/A
-
-Inputs:
-segment.descent_rate                        [meters/second]
-segment.altitude_start                      [meters]
-segment.altitude_end                        [meters]
-segment.air_speed                           [meters/second]
-state.numerics.dimensionless.control_points [array]
-
-Outputs:
-conditions.frames.inertial.velocity_vector  [meters/second]
-conditions.frames.inertial.position_vector  [meters]
-conditions.freestream.altitude              [meters]
-conditions.frames.inertial.time             [seconds]
-
-Properties Used:
-N/A
-
-
-
- -

◆ initialize_conditions() [2/4]

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Missions.Segments.Descent.Constant_Speed_Constant_Angle.initialize_conditions ( segment,
 state 
)
-
-
Sets the specified conditions which are given for the segment type.
-
-Assumptions:
-Constant speed and constant descent angle
-
-Source:
-N/A
-
-Inputs:
-segment.descent_angle                       [radians]
-segment.altitude_start                      [meters]
-segment.altitude_end                        [meters]
-segment.air_speed                           [meters/second]
-state.numerics.dimensionless.control_points [array]
-
-Outputs:
-conditions.frames.inertial.velocity_vector  [meters/second]
-conditions.frames.inertial.position_vector  [meters]
-conditions.freestream.altitude              [meters]
-conditions.frames.inertial.time             [seconds]
-
-Properties Used:
-N/A
-
-
-
- -

◆ initialize_conditions() [3/4]

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Missions.Segments.Descent.Constant_EAS_Constant_Rate.initialize_conditions ( segment,
 state 
)
-
-
Sets the specified conditions which are given for the segment type.
-
-Assumptions:
-Constant EAS speed and constant descent rate
-
-Source:
-N/A
-
-Inputs:
-segment.equivalent_air_speed                [meters/second]
-segment.altitude_start                      [meters]
-segment.altitude_end                        [meters]
-segment.descent_rate                        [meters/second]
-state.numerics.dimensionless.control_points [array]
-
-Outputs:
-conditions.frames.inertial.velocity_vector  [meters/second]
-conditions.frames.inertial.position_vector  [meters]
-conditions.freestream.altitude              [meters]
-conditions.frames.inertial.time             [seconds]
-
-Properties Used:
-N/A
-
-
-
- -

◆ initialize_conditions() [4/4]

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Missions.Segments.Descent.Constant_Speed_Constant_Angle_Noise.initialize_conditions ( segment,
 state 
)
-
-
Sets the specified conditions which are given for the segment type.
-
-Assumptions:
-Constant speed, constant descent angle. However, this follows a 2000 meter segment. This is a certification maneuver standard. The last point for the noise measurement is 50 feet.
-
-Source:
-N/A
-
-Inputs:
-segment.descent_angle                       [radians]
-segment.altitude_start                      [meters]
-segment.altitude_end                        [meters]
-segment.air_speed                           [meters/second]
-state.numerics.dimensionless.control_points [array]
-
-Outputs:
-conditions.frames.inertial.velocity_vector  [meters/second]
-conditions.frames.inertial.position_vector  [meters]
-conditions.freestream.altitude              [meters]
-conditions.frames.inertial.time             [seconds]
-
-Properties Used:
-N/A
-
-
-
-
-
- - - - diff --git a/_site/doxygen/group__Methods-Missions-Segments-Descent.js b/_site/doxygen/group__Methods-Missions-Segments-Descent.js deleted file mode 100644 index a0881df9..00000000 --- a/_site/doxygen/group__Methods-Missions-Segments-Descent.js +++ /dev/null @@ -1,8 +0,0 @@ -var group__Methods_Missions_Segments_Descent = -[ - [ "expand_state", "group__Methods-Missions-Segments-Descent.html#gaf42a40b22cba7bb56609d82dd1b675d9", null ], - [ "initialize_conditions", "group__Methods-Missions-Segments-Descent.html#gabbd9496321d7bc45c1796b734d2f4b38", null ], - [ "initialize_conditions", "group__Methods-Missions-Segments-Descent.html#gac8fb34b9581a8fa70713a2ad9d5fa03b", null ], - [ "initialize_conditions", "group__Methods-Missions-Segments-Descent.html#gad7dddc4ee25bf0b1e76687a266ad0025", null ], - [ "initialize_conditions", "group__Methods-Missions-Segments-Descent.html#ga217350b7498475f50bd2893122404dfa", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Methods-Missions-Segments-Ground.html b/_site/doxygen/group__Methods-Missions-Segments-Ground.html deleted file mode 100644 index 04e5b0ae..00000000 --- a/_site/doxygen/group__Methods-Missions-Segments-Ground.html +++ /dev/null @@ -1,465 +0,0 @@ - - - - - - - -SUAVE: Ground - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
-
- - - -
-
- -
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-
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- -
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-
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Descent mission methods containing the functions for setting up and solving a mission. -More...

- - - - - - - - - - - - - - - - -

-Functions

def SUAVE.Methods.Missions.Segments.Ground.Common.unpack_unknowns (segment, state)
 
def SUAVE.Methods.Missions.Segments.Ground.Common.initialize_conditions (segment, state)
 
def SUAVE.Methods.Missions.Segments.Ground.Common.compute_ground_forces (segment, state)
 
def SUAVE.Methods.Missions.Segments.Ground.Common.compute_forces (segment, state)
 
def SUAVE.Methods.Missions.Segments.Ground.Common.solve_residuals (segment, state)
 
def SUAVE.Methods.Missions.Segments.Ground.Landing.initialize_conditions (segment, state)
 
def SUAVE.Methods.Missions.Segments.Ground.Takeoff.initialize_conditions (segment, state)
 
-

Detailed Description

-

Descent mission methods containing the functions for setting up and solving a mission.

-

Function Documentation

- -

◆ compute_forces()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Missions.Segments.Ground.Common.compute_forces ( segment,
 state 
)
-
-
Adds the rolling friction to the traditional 4 forces of flight
-
-Assumptions:
-
-
-Source:
-N/A
-
-Inputs:
-conditions:
-    frames.inertial.total_force_vector  [newtons]
-    frames.inertial.ground_force_vector [newtons]
-
-Outputs:
-frames.inertial.ground_force_vector     [newtons]
-
-Properties Used:
-N/A
-
-
-
- -

◆ compute_ground_forces()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Missions.Segments.Ground.Common.compute_ground_forces ( segment,
 state 
)
-
-
Compute the rolling friction on the aircraft 
-
-Assumptions:
-Does a force balance to calculate the load on the wheels using only lift. Uses only a single friction coefficient.
-
-Source:
-N/A
-
-Inputs:
-conditions:
-    frames.inertial.gravity_force_vector       [meters/second^2]
-    ground.friction_coefficient                [unitless]
-    frames.wind.lift_force_vector              [newtons]
-
-Outputs:
-conditions.frames.inertial.ground_force_vector [newtons]
-
-Properties Used:
-N/A
-
-
-
- -

◆ initialize_conditions() [1/3]

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Missions.Segments.Ground.Takeoff.initialize_conditions ( segment,
 state 
)
-
-
Sets the specified conditions which are given for the segment type.
-
-Assumptions:
-Builds on the initialize conditions for common
-
-Source:
-N/A
-
-Inputs:
-segment.throttle                           [unitless]
-conditions.frames.inertial.position_vector [meters]
-conditions.weights.total_mass              [kilogram]
-
-Outputs:
-conditions.weights.total_mass              [kilogram]
-conditions.frames.inertial.position_vector [unitless]
-conditions.propulsion.throttle             [meters]
-
-Properties Used:
-N/A
-
-
-
- -

◆ initialize_conditions() [2/3]

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Missions.Segments.Ground.Landing.initialize_conditions ( segment,
 state 
)
-
-
Sets the specified conditions which are given for the segment type.
-
-Assumptions:
-Builds on the initialize conditions for common
-
-Source:
-N/A
-
-Inputs:
-segment.throttle                                         [unitless]
-segment.analyses.weights.vehicle.mass_properties.landing [kilogram]
-
-Outputs:
-conditions.weights.total_mass   [kilogram]
-conditions.propulsion.throttle  [unitless]
-
-Properties Used:
-N/A
-
-
-
- -

◆ initialize_conditions() [3/3]

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Missions.Segments.Ground.Common.initialize_conditions ( segment,
 state 
)
-
-
Sets the specified conditions which are given for the segment type.
-
-Assumptions:
-Checks to make sure non of the velocities are exactly zero
-
-Source:
-N/A
-
-Inputs:
-segment.velocity_start             [meters]
-segment.velocity_end               [meters]
-segment.speed                      [meters/second]
-segment.friction_coefficient       [unitless]
-segment.ground_incline             [radians]
-
-Outputs:
-conditions.frames.inertial.velocity_vector  [meters/second]
-conditions.ground.incline                   [radians]
-conditions.ground.friction_coefficient      [unitless]
-state.unknowns.velocity_x                   [meters/second]
-
-Properties Used:
-N/A
-
-
-
- -

◆ solve_residuals()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Missions.Segments.Ground.Common.solve_residuals ( segment,
 state 
)
-
-
Calculates a residual based on forces
-
-    Assumptions:
-    
-    Inputs:
-        state.conditions:
-            frames.inertial.total_force_vector [Newtons]
-            frames.inertial.velocity_vector    [meters/second]
-            weights.total_mass                 [kg]
-        state.numerics.time.differentiate      [vector]
-        segment.velocity_end                   [meters/second]
-        
-    Outputs:
-        state:
-            residuals.acceleration_x           [meters/second^2]
-            residuals.final_velocity_error     [meters/second]
-
-    Properties Used:
-    N/A
-
-
- -

◆ unpack_unknowns()

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def SUAVE.Methods.Missions.Segments.Ground.Common.unpack_unknowns ( segment,
 state 
)
-
-
Unpacks the times and velocities from the solver to the mission
-
-    Assumptions:
-    Overrides the velocities if they go to zero
-    
-    Inputs:
-        state.unknowns:
-            velocity_x         [meters/second]
-            time               [second]
-        segment.velocity_start [meters/second]
-        segment.velocity_start [meters/second]
-        
-    Outputs:
-        state.conditions:
-            frames.inertial.velocity_vector [meters/second]
-            frames.inertial.time            [second]
-
-    Properties Used:
-    N/A
-
-
-
-
- - - - diff --git a/_site/doxygen/group__Methods-Missions-Segments-Ground.js b/_site/doxygen/group__Methods-Missions-Segments-Ground.js deleted file mode 100644 index ab822c8e..00000000 --- a/_site/doxygen/group__Methods-Missions-Segments-Ground.js +++ /dev/null @@ -1,10 +0,0 @@ -var group__Methods_Missions_Segments_Ground = -[ - [ "compute_forces", "group__Methods-Missions-Segments-Ground.html#ga85d169294fd62de7c701bc919ee98edc", null ], - [ "compute_ground_forces", "group__Methods-Missions-Segments-Ground.html#gaa3bd9d26957028bad0bedf8c65003279", null ], - [ "initialize_conditions", "group__Methods-Missions-Segments-Ground.html#ga5197a82000f2be0f17faa141c7b5e710", null ], - [ "initialize_conditions", "group__Methods-Missions-Segments-Ground.html#ga5a0f970144080b1a249a75ca5f39fbfc", null ], - [ "initialize_conditions", "group__Methods-Missions-Segments-Ground.html#ga5fa0a3728e6f7a2ff4ca2d264bf618b4", null ], - [ "solve_residuals", "group__Methods-Missions-Segments-Ground.html#gaafc05476619f88953ab2020d62f7c39f", null ], - [ "unpack_unknowns", "group__Methods-Missions-Segments-Ground.html#ga07708893d61d25bb85382fef856dbfe7", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Methods-Missions-Segments-Hover.html b/_site/doxygen/group__Methods-Missions-Segments-Hover.html deleted file mode 100644 index 4dc6eb3c..00000000 --- a/_site/doxygen/group__Methods-Missions-Segments-Hover.html +++ /dev/null @@ -1,378 +0,0 @@ - - - - - - - -SUAVE: Hover - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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Hover mission methods containing the functions for setting up and solving a mission. -More...

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def SUAVE.Methods.Missions.Segments.Hover.Climb.initialize_conditions (segment, state)
 Climb.py. More...
 
def SUAVE.Methods.Missions.Segments.Hover.Common.unpack_unknowns (segment, state)
 Common.py. More...
 
def SUAVE.Methods.Missions.Segments.Hover.Common.residual_total_forces (segment, state)
 
def SUAVE.Methods.Missions.Segments.Hover.Descent.initialize_conditions (segment, state)
 Descent.py. More...
 
def SUAVE.Methods.Missions.Segments.Hover.Hover.initialize_conditions (segment, state)
 Hover.py. More...
 
-

Detailed Description

-

Hover mission methods containing the functions for setting up and solving a mission.

-

Function Documentation

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◆ initialize_conditions() [1/3]

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def SUAVE.Methods.Missions.Segments.Hover.Climb.initialize_conditions ( segment,
 state 
)
-
- -

Climb.py.

-

Created: Jan 2016, E. Botero Modified:

Sets the specified conditions which are given for the segment type.
-
-Assumptions:
-Climb segment with a constant rate of climb.
-
-Source:
-N/A
-
-Inputs:
-segment.altitude_start                      [meters]
-segment.altitude_end                        [meters]
-segment.climb_rate                          [meters/second]
-state.numerics.dimensionless.control_points [Unitless]
-state.conditions.frames.inertial.time       [seconds]
-
-Outputs:
-conditions.frames.inertial.velocity_vector  [meters/second]
-conditions.frames.inertial.position_vector  [meters]
-conditions.freestream.altitude              [meters]
-conditions.frames.inertial.time             [seconds]
-
-Properties Used:
-N/A
-
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- -

◆ initialize_conditions() [2/3]

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def SUAVE.Methods.Missions.Segments.Hover.Hover.initialize_conditions ( segment,
 state 
)
-
- -

Hover.py.

-

Created: Jan 2016, E. Botero Modified:

Sets the specified conditions which are given for the segment type.
-
-Assumptions:
-Descent segment with a constant rate.
-
-Source:
-N/A
-
-Inputs:
-segment.altitude                            [meters]
-segment.tim                                 [second]
-state.numerics.dimensionless.control_points [Unitless]
-state.conditions.frames.inertial.time       [seconds]
-
-Outputs:
-conditions.frames.inertial.velocity_vector  [meters/second]
-conditions.frames.inertial.position_vector  [meters]
-conditions.freestream.altitude              [meters]
-conditions.frames.inertial.time             [seconds]
-
-Properties Used:
-N/A
-
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- -

◆ initialize_conditions() [3/3]

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def SUAVE.Methods.Missions.Segments.Hover.Descent.initialize_conditions ( segment,
 state 
)
-
- -

Descent.py.

-

Created: Jan 2016, E. Botero Modified:

Sets the specified conditions which are given for the segment type.
-
-Assumptions:
-Descent segment with a constant rate.
-
-Source:
-N/A
-
-Inputs:
-segment.altitude_start                      [meters]
-segment.altitude_end                        [meters]
-segment.descent_rate                        [meters/second]
-state.numerics.dimensionless.control_points [Unitless]
-state.conditions.frames.inertial.time       [seconds]
-
-Outputs:
-conditions.frames.inertial.velocity_vector  [meters/second]
-conditions.frames.inertial.position_vector  [meters]
-conditions.freestream.altitude              [meters]
-conditions.frames.inertial.time             [seconds]
-
-Properties Used:
-N/A
-
-
-
- -

◆ residual_total_forces()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Missions.Segments.Hover.Common.residual_total_forces ( segment,
 state 
)
-
-
Calculates a residual based on forces
-
-    Assumptions:
-    The vehicle is not accelerating, doesn't use gravity. Only vertical forces
-    
-    Inputs:
-        state.conditions:
-            frames.inertial.total_force_vector [Newtons]
-        
-    Outputs:
-        state.residuals.forces [meters/second^2]
-
-    Properties Used:
-    N/A
-
-
- -

◆ unpack_unknowns()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Missions.Segments.Hover.Common.unpack_unknowns ( segment,
 state 
)
-
- -

Common.py.

-

Created: Jan 2016, E. Botero Modified:

Unpacks the throttle setting from the solver to the mission
-
-    Assumptions:
-    N/A
-    
-    Inputs:
-        state.unknowns:
-            throttle    [Unitless]
-        
-    Outputs:
-        state.conditions:
-            propulsion.throttle            [Unitless]
-
-    Properties Used:
-    N/A
-
-
-
-
- - - - diff --git a/_site/doxygen/group__Methods-Missions-Segments-Hover.js b/_site/doxygen/group__Methods-Missions-Segments-Hover.js deleted file mode 100644 index 78d98f5d..00000000 --- a/_site/doxygen/group__Methods-Missions-Segments-Hover.js +++ /dev/null @@ -1,8 +0,0 @@ -var group__Methods_Missions_Segments_Hover = -[ - [ "initialize_conditions", "group__Methods-Missions-Segments-Hover.html#ga9328ce0d2ebc56f4ab7bc415c77ad377", null ], - [ "initialize_conditions", "group__Methods-Missions-Segments-Hover.html#gacb4620638688fa39b69e8ca3c24622e9", null ], - [ "initialize_conditions", "group__Methods-Missions-Segments-Hover.html#ga302afed2dba4fc73d087f885c604f74a", null ], - [ "residual_total_forces", "group__Methods-Missions-Segments-Hover.html#ga4573e7a193846ce40e8e86d6286a77f9", null ], - [ "unpack_unknowns", "group__Methods-Missions-Segments-Hover.html#ga1cf7c2ad01008b2535a9356aab7ee480", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Methods-Missions-Segments-Single__Point.html b/_site/doxygen/group__Methods-Missions-Segments-Single__Point.html deleted file mode 100644 index e23ea021..00000000 --- a/_site/doxygen/group__Methods-Missions-Segments-Single__Point.html +++ /dev/null @@ -1,372 +0,0 @@ - - - - - - - -SUAVE: Single_Point - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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Single_Point
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Single Point mission methods containing the functions for setting up and solving a mission. -More...

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-Functions

def SUAVE.Methods.Missions.Segments.Single_Point.Set_Speed_Set_Altitude.initialize_conditions (segment, state)
 
def SUAVE.Methods.Missions.Segments.Single_Point.Set_Speed_Set_Altitude.update_weights (segment, state)
 
def SUAVE.Methods.Missions.Segments.Single_Point.Set_Speed_Set_Throttle.initialize_conditions (segment, state)
 
def SUAVE.Methods.Missions.Segments.Single_Point.Set_Speed_Set_Throttle.update_weights (segment, state)
 
def SUAVE.Methods.Missions.Segments.Single_Point.Set_Speed_Set_Throttle.unpack_unknowns (segment, state)
 
-

Detailed Description

-

Single Point mission methods containing the functions for setting up and solving a mission.

-

Function Documentation

- -

◆ initialize_conditions() [1/2]

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def SUAVE.Methods.Missions.Segments.Single_Point.Set_Speed_Set_Altitude.initialize_conditions ( segment,
 state 
)
-
-
Sets the specified conditions which are given for the segment type.
-
-Assumptions:
-A fixed speed and altitude
-
-Source:
-N/A
-
-Inputs:
-segment.altitude                            [meters]
-segment.air_speed                           [meters/second]
-segment.x_accel                             [meters/second^2]
-segment.z_accel                             [meters/second^2]
-
-Outputs:
-conditions.frames.inertial.acceleration_vector [meters/second^2]
-conditions.frames.inertial.velocity_vector     [meters/second]
-conditions.frames.inertial.position_vector     [meters]
-conditions.freestream.altitude                 [meters]
-conditions.frames.inertial.time                [seconds]
-
-Properties Used:
-N/A
-
-
-
- -

◆ initialize_conditions() [2/2]

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def SUAVE.Methods.Missions.Segments.Single_Point.Set_Speed_Set_Throttle.initialize_conditions ( segment,
 state 
)
-
-
Sets the specified conditions which are given for the segment type.
-
-Assumptions:
-A fixed speed and throttle
-
-Source:
-N/A
-
-Inputs:
-segment.altitude                               [meters]
-segment.air_speed                              [meters/second]
-segment.throttle                               [unitless]
-segment.z_accel                                [meters/second^2]
-state.unknowns.x_accel                         [meters/second^2]
-
-Outputs:
-conditions.frames.inertial.acceleration_vector [meters/second^2]
-conditions.frames.inertial.velocity_vector     [meters/second]
-conditions.frames.inertial.position_vector     [meters]
-conditions.freestream.altitude                 [meters]
-conditions.frames.inertial.time                [seconds]
-
-Properties Used:
-N/A
-
-
-
- -

◆ unpack_unknowns()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Missions.Segments.Single_Point.Set_Speed_Set_Throttle.unpack_unknowns ( segment,
 state 
)
-
-
Unpacks the x accleration and body angle from the solver to the mission
-
-    Assumptions:
-    N/A
-    
-    Inputs:
-        state.unknowns:
-            x_accel                             [meters/second^2]
-            body_angle                          [radians]
-        
-    Outputs:
-        state.conditions:
-            frames.inertial.acceleration_vector [meters/second^2]
-            frames.body.inertial_rotations      [radians]
-
-    Properties Used:
-    N/A
-
-
- -

◆ update_weights() [1/2]

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- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Missions.Segments.Single_Point.Set_Speed_Set_Altitude.update_weights ( segment,
 state 
)
-
-
Sets the gravity force vector during the segment
-
-Assumptions:
-A fixed speed and altitde
-
-Source:
-N/A
-
-Inputs:
-conditions:
-    weights.total_mass                          [kilogram]
-    freestream.gravity                          [meters/second^2]
-
-Outputs:
-conditions.frames.inertial.gravity_force_vector [newtons]
-
-
-Properties Used:
-N/A
-
-
-
- -

◆ update_weights() [2/2]

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-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Missions.Segments.Single_Point.Set_Speed_Set_Throttle.update_weights ( segment,
 state 
)
-
-
Sets the gravity force vector during the segment
-
-Assumptions:
-A fixed speed and altitde
-
-Source:
-N/A
-
-Inputs:
-conditions:
-    weights.total_mass                          [kilogram]
-    freestream.gravity                          [meters/second^2]
-
-Outputs:
-conditions.frames.inertial.gravity_force_vector [newtons]
-
-
-Properties Used:
-N/A
-
-
-
-
-
- - - - diff --git a/_site/doxygen/group__Methods-Missions-Segments-Single__Point.js b/_site/doxygen/group__Methods-Missions-Segments-Single__Point.js deleted file mode 100644 index d3401a1c..00000000 --- a/_site/doxygen/group__Methods-Missions-Segments-Single__Point.js +++ /dev/null @@ -1,8 +0,0 @@ -var group__Methods_Missions_Segments_Single__Point = -[ - [ "initialize_conditions", "group__Methods-Missions-Segments-Single__Point.html#gaab3442c514383fad1367ab5bdefdc1f8", null ], - [ "initialize_conditions", "group__Methods-Missions-Segments-Single__Point.html#ga090e629e786b91635afbecc678c9cd9e", null ], - [ "unpack_unknowns", "group__Methods-Missions-Segments-Single__Point.html#gaa50cc92ee0391088fb1e5adb35a35ddd", null ], - [ "update_weights", "group__Methods-Missions-Segments-Single__Point.html#ga0e4950f3684d067bab0a32c92b74b07e", null ], - [ "update_weights", "group__Methods-Missions-Segments-Single__Point.html#gabc3632cdc444579b2fb132baafbe76de", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Methods-Missions-Segments.html b/_site/doxygen/group__Methods-Missions-Segments.html deleted file mode 100644 index 4480b4f3..00000000 --- a/_site/doxygen/group__Methods-Missions-Segments.html +++ /dev/null @@ -1,547 +0,0 @@ - - - - - - - -SUAVE: Segments - - - - - - - - - - - - - - - -
-
- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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Segments
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Mission Segment folders containing the functions for setting up and solving a mission. -More...

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-Modules

 Climb
 Climb mission methods containing the functions for setting up and solving a mission.
 
 Common
 Climb mission methods containing the functions for setting up and solving a mission.
 
 Cruise
 Cruise mission methods containing the functions for setting up and solving a mission.
 
 Descent
 Descent mission methods containing the functions for setting up and solving a mission.
 
 Ground
 Descent mission methods containing the functions for setting up and solving a mission.
 
 Hover
 Hover mission methods containing the functions for setting up and solving a mission.
 
 Single_Point
 Single Point mission methods containing the functions for setting up and solving a mission.
 
- - - - - - - - - - - - - - - - - -

-Functions

def SUAVE.Methods.Missions.Segments.converge_root.converge_root (segment, state)
 
def SUAVE.Methods.Missions.Segments.converge_root.iterate (unknowns, segment, state)
 
def SUAVE.Methods.Missions.Segments.optimize.converge_opt (segment, state)
 
def SUAVE.Methods.Missions.Segments.optimize.get_objective (unknowns, segment, state)
 
def SUAVE.Methods.Missions.Segments.optimize.get_econstraints (unknowns, segment, state)
 
def SUAVE.Methods.Missions.Segments.optimize.make_bnds (unknowns, segment, state)
 
def SUAVE.Methods.Missions.Segments.optimize.get_ieconstraints (unknowns, segment, state)
 
def SUAVE.Methods.Missions.Segments.optimize.get_problem_pyopt (unknowns, segment, state)
 
-

Detailed Description

-

Mission Segment folders containing the functions for setting up and solving a mission.

-

Function Documentation

- -

◆ converge_opt()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Missions.Segments.optimize.converge_opt ( segment,
 state 
)
-
-
Interfaces the mission to an optimization algorithm
-
-Assumptions:
-N/A
-
-Source:
-N/A
-
-Inputs:
-state.unknowns                     [Data]
-segment                            [Data]
-state                              [Data]
-segment.algorithm                  [string]
-
-Outputs:
-state.unknowns                     [Any]
-
-Properties Used:
-N/A
-
-
-
- -

◆ converge_root()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Missions.Segments.converge_root.converge_root ( segment,
 state 
)
-
-
Interfaces the mission to a numerical solver. The solver may be changed by using root_finder.
-
-Assumptions:
-N/A
-
-Source:
-N/A
-
-Inputs:
-state.unknowns                     [Data]
-segment                            [Data]
-state                              [Data]
-segment.settings.root_finder       [Data]
-state.numerics.tolerance_solution  [Unitless]
-
-Outputs:
-state.unknowns                     [Any]
-segment.state.numerics.converged   [Unitless]
-
-Properties Used:
-N/A
-
-
-
- -

◆ get_econstraints()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Missions.Segments.optimize.get_econstraints ( unknowns,
 segment,
 state 
)
-
-
Runs the mission if the equality constraint values are needed
-
-    Assumptions:
-    N/A
-    
-    Inputs:
-    state.unknowns      [Data]
-        
-    Outputs:
-    constraints          [array]
-
-    Properties Used:
-    N/A
-
-
- -

◆ get_ieconstraints()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Missions.Segments.optimize.get_ieconstraints ( unknowns,
 segment,
 state 
)
-
-
Runs the mission if the inequality constraint values are needed
-
-    Assumptions:
-    Time only goes forward
-    CL is less than a specified limit
-    All altitudes are greater than zero
-    
-    Inputs:
-    state.unknowns      [Data]
-        
-    Outputs:
-    constraints          [array]
-
-    Properties Used:
-    N/A
-
-
- -

◆ get_objective()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Missions.Segments.optimize.get_objective ( unknowns,
 segment,
 state 
)
-
-
Runs the mission if the objective value is needed
-
-    Assumptions:
-    N/A
-    
-    Inputs:
-    state.unknowns      [Data]
-
-    Outputs:
-    objective           [float]
-
-    Properties Used:
-    N/A
-
-
- -

◆ get_problem_pyopt()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Missions.Segments.optimize.get_problem_pyopt ( unknowns,
 segment,
 state 
)
-
-
Runs the mission and obtains the objective and all constraints. This is formatted for pyopt
-
-    Assumptions:
-    Time only goes forward
-    CL is less than a specified limit
-    All altitudes are greater than zero
-    
-    Inputs:
-    state.unknowns      [Data]
-
-    Outputs:
-    obj                 [float]
-    con                 [array]
-    fail                [boolean]
-
-    Properties Used:
-    N/A
-
-
- -

◆ iterate()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Missions.Segments.converge_root.iterate ( unknowns,
 segment,
 state 
)
-
-
Runs one iteration of of all analyses for the mission.
-
-Assumptions:
-N/A
-
-Source:
-N/A
-
-Inputs:
-state.unknowns                [Data]
-segment.process.iterate       [Data]
-
-Outputs:
-residuals                     [Unitless]
-
-Properties Used:
-N/A
-
-
-
- -

◆ make_bnds()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Missions.Segments.optimize.make_bnds ( unknowns,
 segment,
 state 
)
-
-
Automatically sets the bounds of the optimization.
-
-    Assumptions:
-    Restricts throttle to between 0 and 100%
-    Restricts body angle from 0 to pi/2 radians
-    Restricts flight path angle from 0 to pi/2 radians
-    
-    Inputs:
-    none
-        
-    Outputs:
-    bnds
-
-    Properties Used:
-    N/A
-
-
-
-
- - - - diff --git a/_site/doxygen/group__Methods-Missions-Segments.js b/_site/doxygen/group__Methods-Missions-Segments.js deleted file mode 100644 index de95bafd..00000000 --- a/_site/doxygen/group__Methods-Missions-Segments.js +++ /dev/null @@ -1,18 +0,0 @@ -var group__Methods_Missions_Segments = -[ - [ "Climb", "group__Methods-Missions-Segments-Climb.html", "group__Methods-Missions-Segments-Climb" ], - [ "Common", "group__Methods-Missions-Segments-Common.html", "group__Methods-Missions-Segments-Common" ], - [ "Cruise", "group__Methods-Missions-Segments-Cruise.html", "group__Methods-Missions-Segments-Cruise" ], - [ "Descent", "group__Methods-Missions-Segments-Descent.html", "group__Methods-Missions-Segments-Descent" ], - [ "Ground", "group__Methods-Missions-Segments-Ground.html", "group__Methods-Missions-Segments-Ground" ], - [ "Hover", "group__Methods-Missions-Segments-Hover.html", "group__Methods-Missions-Segments-Hover" ], - [ "Single_Point", "group__Methods-Missions-Segments-Single__Point.html", "group__Methods-Missions-Segments-Single__Point" ], - [ "converge_opt", "group__Methods-Missions-Segments.html#ga6a15ecfced108358c27c0f4a8ed532cb", null ], - [ "converge_root", "group__Methods-Missions-Segments.html#ga13921466d6f6f405b48229bd2a2e9fa5", null ], - [ "get_econstraints", "group__Methods-Missions-Segments.html#ga17833fb35560ed7c1616cbd7039091ad", null ], - [ "get_ieconstraints", "group__Methods-Missions-Segments.html#gaf5f56473e84fbfa6ae39a3cf22fb8419", null ], - [ "get_objective", "group__Methods-Missions-Segments.html#gade8f58fd70859197f15ad050a9be4e70", null ], - [ "get_problem_pyopt", "group__Methods-Missions-Segments.html#ga1c03859f235b7957e3ff47ef8be0c0e6", null ], - [ "iterate", "group__Methods-Missions-Segments.html#gad082382d971ef537dfe9b8dbeed7a776", null ], - [ "make_bnds", "group__Methods-Missions-Segments.html#ga0c332a9e67af11deb7921508a7a09c72", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Methods-Missions.html b/_site/doxygen/group__Methods-Missions.html deleted file mode 100644 index c99b317a..00000000 --- a/_site/doxygen/group__Methods-Missions.html +++ /dev/null @@ -1,123 +0,0 @@ - - - - - - - -SUAVE: Missions - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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Missions
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Mission methods contain the functions for setting up and solving a mission. -More...

- - - - - -

-Modules

 Segments
 Mission Segment folders containing the functions for setting up and solving a mission.
 
-

Detailed Description

-

Mission methods contain the functions for setting up and solving a mission.

-
-
- - - - diff --git a/_site/doxygen/group__Methods-Missions.js b/_site/doxygen/group__Methods-Missions.js deleted file mode 100644 index 788834ea..00000000 --- a/_site/doxygen/group__Methods-Missions.js +++ /dev/null @@ -1,4 +0,0 @@ -var group__Methods_Missions = -[ - [ "Segments", "group__Methods-Missions-Segments.html", "group__Methods-Missions-Segments" ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Methods-Noise-Correlations.html b/_site/doxygen/group__Methods-Noise-Correlations.html deleted file mode 100644 index 3386f366..00000000 --- a/_site/doxygen/group__Methods-Noise-Correlations.html +++ /dev/null @@ -1,113 +0,0 @@ - - - - - - - -SUAVE: Correlations - - - - - - - - - - - - - - - -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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Correlations
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Correlation type methods for calculating noise. -More...

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Correlation type methods for calculating noise.

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An Aerospace Vehicle Environment for Designing Future Aircraft
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Airframe
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Fidelity One level noise calculations for the airframe components. -More...

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Fidelity One level noise calculations for the airframe components.

-
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An Aerospace Vehicle Environment for Designing Future Aircraft
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Fidelity One level noise calculations for the engine. -More...

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Fidelity One level noise calculations for the engine.

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An Aerospace Vehicle Environment for Designing Future Aircraft
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Noise Tools
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Various functions that are used to calculate noise using the fidelity one level. -More...

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Various functions that are used to calculate noise using the fidelity one level.

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An Aerospace Vehicle Environment for Designing Future Aircraft
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Fidelity_One
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Description. -More...

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-Modules

 Airframe
 Fidelity One level noise calculations for the airframe components.
 
 Engine
 Fidelity One level noise calculations for the engine.
 
 Noise Tools
 Various functions that are used to calculate noise using the fidelity one level.
 
-

Detailed Description

-

Description.

-
-
- - - - diff --git a/_site/doxygen/group__Methods-Noise-Fidelity__One.js b/_site/doxygen/group__Methods-Noise-Fidelity__One.js deleted file mode 100644 index 53c72142..00000000 --- a/_site/doxygen/group__Methods-Noise-Fidelity__One.js +++ /dev/null @@ -1,6 +0,0 @@ -var group__Methods_Noise_Fidelity__One = -[ - [ "Airframe", "group__Methods-Noise-Fidelity__One-Airframe.html", null ], - [ "Engine", "group__Methods-Noise-Fidelity__One-Engine.html", null ], - [ "Noise Tools", "group__Methods-Noise-Fidelity__One-Noise__Tools.html", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Methods-Noise.html b/_site/doxygen/group__Methods-Noise.html deleted file mode 100644 index 94996311..00000000 --- a/_site/doxygen/group__Methods-Noise.html +++ /dev/null @@ -1,126 +0,0 @@ - - - - - - - -SUAVE: Noise - - - - - - - - - - - - - - - -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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Noise
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Description. -More...

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 Correlations
 Correlation type methods for calculating noise.
 
 Fidelity_One
 Description.
 
-

Detailed Description

-

Description.

-
-
- - - - diff --git a/_site/doxygen/group__Methods-Noise.js b/_site/doxygen/group__Methods-Noise.js deleted file mode 100644 index bf6727da..00000000 --- a/_site/doxygen/group__Methods-Noise.js +++ /dev/null @@ -1,5 +0,0 @@ -var group__Methods_Noise = -[ - [ "Correlations", "group__Methods-Noise-Correlations.html", null ], - [ "Fidelity_One", "group__Methods-Noise-Fidelity__One.html", "group__Methods-Noise-Fidelity__One" ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Methods-Performance.html b/_site/doxygen/group__Methods-Performance.html deleted file mode 100644 index 768857b2..00000000 --- a/_site/doxygen/group__Methods-Performance.html +++ /dev/null @@ -1,548 +0,0 @@ - - - - - - - -SUAVE: Performance - - - - - - - - - - - - - - - -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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Performance
-
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This is a set of basic aircraft performance estimation functions. -More...

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-Functions

def SUAVE.Methods.Performance.estimate_landing_field_length.estimate_landing_field_length (vehicle, analyses, airport)
 
def SUAVE.Methods.Performance.estimate_take_off_field_length.estimate_take_off_field_length (vehicle, analyses, airport, compute_2nd_seg_climb=0)
 
def SUAVE.Methods.Performance.find_takeoff_weight_given_tofl.find_takeoff_weight_given_tofl (vehicle, analyses, airport, target_tofl)
 
def SUAVE.Methods.Performance.payload_range.payload_range (vehicle, mission, cruise_segment_tag, reserves=0.)
 
def SUAVE.Methods.Performance.size_mission_range_given_weights.size_mission_range_given_weights (vehicle, mission, cruise_segment_tag, mission_payload, takeoff_weight=0., reserve_fuel=0.)
 
def SUAVE.Methods.Performance.size_weights_given_mission_range.size_weights_given_mission_range (vehicle, mission, cruise_segment_tag, mission_payload, target_range, reserve_fuel=0.)
 
-

Detailed Description

-

This is a set of basic aircraft performance estimation functions.

-

It includes field length and range calculations.

-

Function Documentation

- -

◆ estimate_landing_field_length()

- -
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- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Performance.estimate_landing_field_length.estimate_landing_field_length ( vehicle,
 analyses,
 airport 
)
-
-
Computes the landing field length for a given vehicle configuration in a given airport.
-
-Assumptions:
-See source
-Two wheel trucks (code needed for four wheel trucks also included)
-
-Source:
-Torenbeek, E., "Advanced Aircraft Design", 2013 (equation 9.25)
-
-Inputs:
-airport.
-  atmosphere                           [SUAVE data type]
-  altitude                             [m]
-  delta_isa                            [K]
-vehicle.
-  mass_properties.landing              [kg]
-  reference_area                       [m^2]
-  maximum_lift_coefficient (optional)  [Unitless]
-
-Outputs:
-landing_field_length                   [m]
-
-Properties Used:
-N/A
-
-
-
- -

◆ estimate_take_off_field_length()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Performance.estimate_take_off_field_length.estimate_take_off_field_length ( vehicle,
 analyses,
 airport,
 compute_2nd_seg_climb = 0 
)
-
-
Computes the takeoff field length for a given vehicle configuration in a given airport.
-Also optionally computes the second segment climb gradient.
-
-Assumptions:
-For second segment climb gradient:
-One engine inoperative
-Only validated for two engine aircraft
-
-Source:
-http://adg.stanford.edu/aa241/AircraftDesign.html
-
-Inputs:
-analyses.base.atmosphere               [SUAVE data type]
-airport.
-  altitude                             [m]
-  delta_isa                            [K]
-vehicle.
-  mass_properties.takeoff              [kg]
-  reference_area                       [m^2]
-  V2_VS_ratio (optional)               [Unitless]
-  maximum_lift_coefficient (optional)  [Unitless]
-  propulsors.*.number_of_engines       [Unitless]
-
-Outputs:
-takeoff_field_length                   [m]
-
-Properties Used:
-N/A
-
-
-
- -

◆ find_takeoff_weight_given_tofl()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Performance.find_takeoff_weight_given_tofl.find_takeoff_weight_given_tofl ( vehicle,
 analyses,
 airport,
 target_tofl 
)
-
-
Estimates the takeoff weight given a certain takeoff field length.
-
-Assumptions:
-assumptions per estimate_take_off_field_length()
-
-Source:
-N/A
-
-Inputs:
-vehicle.mass_properties.
-  operating_empty         [kg]
-  max_takeoff             [kg]
-  analyses                [SUAVE data structure]
-  airport                 [SUAVE data structure]
-  target_tofl             [m]
-  
-Outputs:
-max_tow                   [kg]
-
-Properties Used:
-N/A
-
-
-
- -

◆ payload_range()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Performance.payload_range.payload_range ( vehicle,
 mission,
 cruise_segment_tag,
 reserves = 0. 
)
-
-
Calculates a vehicle's payload range diagram. Includes plotting.
-
-Assumptions:
-Constant altitude cruise
-
-Source:
-N/A
-
-Inputs:
-vehicle.mass_properties.
-  operating_empty                     [kg]
-  max_zero_fuel                       [kg]
-  max_takeoff                         [kg]
-  max_payload                         [kg]
-  max_fuel                            [kg]
-  takeoff                             [kg]
-mission.segments[0].analyses.weights.
-  vehicle.mass_properties.takeoff     [kg]
-cruise_segment_tag                    <string>
-
-Outputs:
-payload_range.
-  range                             [m]
-  payload                           [kg]
-  fuel                              [kg]
-  takeoff_weight                    [kg]
-PayloadRangeDiagram.dat (text file)
-
-Properties Used:
-N/A
-
-
-
- -

◆ size_mission_range_given_weights()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Performance.size_mission_range_given_weights.size_mission_range_given_weights ( vehicle,
 mission,
 cruise_segment_tag,
 mission_payload,
 takeoff_weight = 0.,
 reserve_fuel = 0. 
)
-
-
Calculates a vehicle's range and fuel for a given takeoff weight and payload
-
-Assumptions:
-Constant altitude cruise
-
-Source:
-N/A
-
-Inputs:
-vehicle.mass_properties.
-  operating_empty                     [kg]
-  takeoff                             [kg]
-mission.segments[0].analyses.weights.
-  mass_properties.takeoff             [kg]
-cruise_segment_tag                    <string>
-mission_payload                       [kg]
-takeoff_weight (optional)             [kg]
-reserve_fuel                          [kg]
-
-Outputs:
-distance                              [m]
-fuel                                  [kg]
-
-Properties Used:
-N/A
-
-
-
- -

◆ size_weights_given_mission_range()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Performance.size_weights_given_mission_range.size_weights_given_mission_range ( vehicle,
 mission,
 cruise_segment_tag,
 mission_payload,
 target_range,
 reserve_fuel = 0. 
)
-
-
Calculates a vehicle's fuel and takeoff weight for a given range. Also returns the range.
-
-Assumptions:
-Constant altitude cruise
-
-Source:
-N/A
-
-Inputs:
-vehicle.mass_properties.
-  operating_empty                     [kg]
-  max_zero_fuel                       [kg]
-  max_takeoff                         [kg]
-  max_payload                         [kg]
-  max_fuel                            [kg]
-mission                               [SUAVE data structure]
-cruise_segment_tag                    <string>
-mission_payload                       [kg]
-target_range                          [m]
-reserve_fuel (optional)               [kg]
-
-Outputs:
-distance                              [m]
-fuel                                  [kg]
-tow                                   [kg]
-
-Properties Used:
-N/A
-
-
-
-
-
- - - - diff --git a/_site/doxygen/group__Methods-Performance.js b/_site/doxygen/group__Methods-Performance.js deleted file mode 100644 index e94d5a91..00000000 --- a/_site/doxygen/group__Methods-Performance.js +++ /dev/null @@ -1,9 +0,0 @@ -var group__Methods_Performance = -[ - [ "estimate_landing_field_length", "group__Methods-Performance.html#ga938d16e3a48381c15d259c87588d5fc5", null ], - [ "estimate_take_off_field_length", "group__Methods-Performance.html#ga02d56e7967cb530e3f0e4fea121599bd", null ], - [ "find_takeoff_weight_given_tofl", "group__Methods-Performance.html#ga42e523c866aa6dcc695a6c587eaf0123", null ], - [ "payload_range", "group__Methods-Performance.html#gab6d53e36ef47e7ccd43b25ea7bab6c40", null ], - [ "size_mission_range_given_weights", "group__Methods-Performance.html#ga183d28f783ad524339c6deb9cf3cf46c", null ], - [ "size_weights_given_mission_range", "group__Methods-Performance.html#ga71b994da90770582a5f3d3bff7e2fc3a", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Methods-Power-Battery-Discharge.html b/_site/doxygen/group__Methods-Power-Battery-Discharge.html deleted file mode 100644 index e969ce0a..00000000 --- a/_site/doxygen/group__Methods-Power-Battery-Discharge.html +++ /dev/null @@ -1,177 +0,0 @@ - - - - - - - -SUAVE: Discharge - - - - - - - - - - - - - - - -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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Discharge
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Functions to evaluate battery discharge losses and voltage requirements. -More...

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-Functions

def SUAVE.Methods.Power.Battery.Discharge.datta_discharge.datta_discharge (battery, numerics)
 
-

Detailed Description

-

Functions to evaluate battery discharge losses and voltage requirements.

-

Function Documentation

- -

◆ datta_discharge()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Power.Battery.Discharge.datta_discharge.datta_discharge ( battery,
 numerics 
)
-
-
models discharge losses based on an empirical correlation
-   Based on method taken from Datta and Johnson: 
-   
-   Assumptions: 
-   Constant Peukart coefficient
-   
-   Source:
-   "Requirements for a Hydrogen Powered All-Electric Manned Helicopter" by Datta and Johnson
-  
-   voltage model from from Chen, M. and Rincon-Mora, G. A., "Accurate Electrical Battery Model Capable of Predicting
-   # Runtime and I - V Performance" IEEE Transactions on Energy Conversion, Vol. 21, No. 2, June 2006, pp. 504-511
-   
-   Inputs:
-   battery.
-    resistance                      [Ohms]
-    max_energy                      [Joules]
-    current_energy (to be modified) [Joules]
-    inputs.
-        current                     [amps]
-        power_in                    [Watts]
-   
-   Outputs:
-   battery.
-    current energy                  [Joules]
-    resistive_losses                [Watts]
-    voltage_open_circuit            [Volts]
-    voltage_under_load              [Volts]
-
-
-
-
- - - - diff --git a/_site/doxygen/group__Methods-Power-Battery-Discharge.js b/_site/doxygen/group__Methods-Power-Battery-Discharge.js deleted file mode 100644 index 1b123a37..00000000 --- a/_site/doxygen/group__Methods-Power-Battery-Discharge.js +++ /dev/null @@ -1,4 +0,0 @@ -var group__Methods_Power_Battery_Discharge = -[ - [ "datta_discharge", "group__Methods-Power-Battery-Discharge.html#ga2bac69c7b319cbf510379a320ab83922", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Methods-Power-Battery-Ragone.html b/_site/doxygen/group__Methods-Power-Battery-Ragone.html deleted file mode 100644 index 3e0d0f28..00000000 --- a/_site/doxygen/group__Methods-Power-Battery-Ragone.html +++ /dev/null @@ -1,301 +0,0 @@ - - - - - - - -SUAVE: Ragone - - - - - - - - - - - - - - - -
-
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An Aerospace Vehicle Environment for Designing Future Aircraft
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Ragone
-
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- -

Functions to evaluate a Ragone of the battery. -More...

- - - - - - - - - -

-Functions

def SUAVE.Methods.Power.Battery.Ragone.find_ragone_optimum.find_ragone_optimum (battery, energy, power)
 
def SUAVE.Methods.Power.Battery.Ragone.find_ragone_properties.find_ragone_properties (specific_energy, battery, energy, power)
 
def SUAVE.Methods.Power.Battery.Ragone.find_specific_power.find_specific_power (battery, specific_energy)
 find_specific_power.py More...
 
-

Detailed Description

-

Functions to evaluate a Ragone of the battery.

-

Function Documentation

- -

◆ find_ragone_optimum()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Power.Battery.Ragone.find_ragone_optimum.find_ragone_optimum ( battery,
 energy,
 power 
)
-
-
Uses Brent's Bracketing Method to find an optimum-mass battery based on the 
-specific energy and specific power of the battery determined from the battery's ragone plot.
-
-Assumptions:
-Specific power can be modeled as a curve vs. specific energy of the form c1*10**(c2*specific_energy)
-
-Inputs:
-energy            [J]
-power             [W]
-battery.
-  specific_energy [J/kg]               
-  specific_power  [W/kg]
-  ragone.
-    constant_1    [W/kg]
-    constant_2    [J/kg]
-    upper_bound   [J/kg]
-    lower_bound   [J/kg]
-            
-Outputs:
-battery.
-  specific_energy [J/kg]
-  specific_power  [W/kg]
-  mass_properties.
-    mass           [kg]    
-            
-       
-
-Properties Used:
-N/A  
-
-
-
- -

◆ find_ragone_properties()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Power.Battery.Ragone.find_ragone_properties.find_ragone_properties ( specific_energy,
 battery,
 energy,
 power 
)
-
-
determines mass of a battery based on the specific energy, energy required, and power required,
-works by calling find_specific_power and initialize_from_energy_and_power
-Assumptions:
-None
-
-Inputs:
-energy            [J]
-power             [W]
-battery.
-
-battery.
-  type
-  specific_energy [J/kg]               
-  specific_power  [W/kg]
-  ragone.
-    constant_1    [W/kg]
-    constant_2    [J/kg]
-    upper_bound   [J/kg]
-    lower_bound   [J/kg]
-            
-Outputs:
-battery.
-  max_energy      [J]
-  max_power       [W]
-  specific_energy [J/kg]
-  specific_power  [W/kg]
-  mass_properties.
-    mass           [kg]    
-
-
- -

◆ find_specific_power()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Power.Battery.Ragone.find_specific_power.find_specific_power ( battery,
 specific_energy 
)
-
- -

find_specific_power.py

-

Created: ### 2104, M. Vegh Modified: Sep 2105, M. Vegh Feb 2016, E. Botero

determines specific specific power from a ragone curve correlation
-Assumptions:
-None
-
-Inputs:
-battery.
-  specific_energy [J/kg]               
-  ragone.
-    constant_1    [W/kg]
-    constant_2    [J/kg]
-            
-Outputs:
-battery.
-  specific_power  [W/kg]   
-
-
-
-
- - - - diff --git a/_site/doxygen/group__Methods-Power-Battery-Ragone.js b/_site/doxygen/group__Methods-Power-Battery-Ragone.js deleted file mode 100644 index 53bdf3c0..00000000 --- a/_site/doxygen/group__Methods-Power-Battery-Ragone.js +++ /dev/null @@ -1,6 +0,0 @@ -var group__Methods_Power_Battery_Ragone = -[ - [ "find_ragone_optimum", "group__Methods-Power-Battery-Ragone.html#gaed8efbd2faf894c5ca24a3fe8efbbd2c", null ], - [ "find_ragone_properties", "group__Methods-Power-Battery-Ragone.html#gae1c67014479895681cf7a69b6efeab37", null ], - [ "find_specific_power", "group__Methods-Power-Battery-Ragone.html#ga8bc3b8dcb9730e81fa33814cdd8bfc79", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Methods-Power-Battery-Sizing.html b/_site/doxygen/group__Methods-Power-Battery-Sizing.html deleted file mode 100644 index 07688feb..00000000 --- a/_site/doxygen/group__Methods-Power-Battery-Sizing.html +++ /dev/null @@ -1,226 +0,0 @@ - - - - - - - -SUAVE: Sizing - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
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-
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- - - -
-
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- -
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Sizing
-
-
- -

Functions to size battery from mass, specific energy, and specific power. -More...

- - - - - - -

-Functions

def SUAVE.Methods.Power.Battery.Sizing.initialize_from_energy_and_power.initialize_from_energy_and_power (battery, energy, power, max='hard')
 
def SUAVE.Methods.Power.Battery.Sizing.initialize_from_mass.initialize_from_mass (battery, mass)
 
-

Detailed Description

-

Functions to size battery from mass, specific energy, and specific power.

-

Function Documentation

- -

◆ initialize_from_energy_and_power()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Power.Battery.Sizing.initialize_from_energy_and_power.initialize_from_energy_and_power ( battery,
 energy,
 power,
 max = 'hard' 
)
-
-
Uses a soft_max function to calculate the batter mass, maximum energy, and maximum power
-from the energy and power requirements, as well as the specific energy and specific power
-
-Assumptions:
-None
-
-Inputs:
-energy            [J]
-power             [W]
-battery.
-  specific_energy [J/kg]               
-  specific_power  [W/kg]
-
-Outputs:
- battery.
-   max_energy
-   max_power
-   mass_properties.
-    mass
-
-
- -

◆ initialize_from_mass()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Power.Battery.Sizing.initialize_from_mass.initialize_from_mass ( battery,
 mass 
)
-
-
Calculate the max energy and power based of the mass
-Assumptions:
-A constant value of specific energy and power
-
-Inputs:
-mass              [kilograms]
-battery.
-  specific_energy [J/kg]               
-  specific_power  [W/kg]
-
-Outputs:
- battery.
-   max_energy
-   max_power
-   mass_properties.
-    mass
-
-
-
-
- - - - diff --git a/_site/doxygen/group__Methods-Power-Battery-Sizing.js b/_site/doxygen/group__Methods-Power-Battery-Sizing.js deleted file mode 100644 index 6cabc561..00000000 --- a/_site/doxygen/group__Methods-Power-Battery-Sizing.js +++ /dev/null @@ -1,5 +0,0 @@ -var group__Methods_Power_Battery_Sizing = -[ - [ "initialize_from_energy_and_power", "group__Methods-Power-Battery-Sizing.html#ga87ecd44d90a6e2da93c783e7da06eaf0", null ], - [ "initialize_from_mass", "group__Methods-Power-Battery-Sizing.html#ga47f170235ace9f4f3bf06f1857155164", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Methods-Power-Battery-Variable__Mass.html b/_site/doxygen/group__Methods-Power-Battery-Variable__Mass.html deleted file mode 100644 index ae755b60..00000000 --- a/_site/doxygen/group__Methods-Power-Battery-Variable__Mass.html +++ /dev/null @@ -1,201 +0,0 @@ - - - - - - - -SUAVE: Variable_Mass - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
-
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Variable_Mass
-
-
- -

Functions pertaining to variable mass batteries (such as metal air) -More...

- - - - - - - - -

-Functions

def SUAVE.Methods.Power.Battery.Variable_Mass.find_mass_gain_rate.find_mass_gain_rate (battery, power)
 find_mass_gain_rate.py More...
 
def SUAVE.Methods.Power.Battery.Variable_Mass.find_total_mass_gain.find_total_mass_gain (battery)
 find_total_mass_gain.py More...
 
-

Detailed Description

-

Functions pertaining to variable mass batteries (such as metal air)

-

Function Documentation

- -

◆ find_mass_gain_rate()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Power.Battery.Variable_Mass.find_mass_gain_rate.find_mass_gain_rate ( battery,
 power 
)
-
- -

find_mass_gain_rate.py

-

Created: ### 2104, M. Vegh Modified: Feb 2016, E. Botero

finds the mass gain rate of the battery from the ambient air
-Assumptions:
-Earth Atmospheric composition
-
-Inputs:
-power              [W]
-battery.
-  mass_gain_factor [kg/W]
-  
-Outputs:
-  mdot             [kg/s]
-
-
-
- -

◆ find_total_mass_gain()

- -
-
- - - - - - - - -
def SUAVE.Methods.Power.Battery.Variable_Mass.find_total_mass_gain.find_total_mass_gain ( battery)
-
- -

find_total_mass_gain.py

-

Created: ### 2104, M. Vegh Modified: Feb 2016, E. Botero

finds the total mass of air that the battery 
-accumulates when discharged fully
-
-Assumptions:
-Earth Atmospheric composition
-
-Inputs:
-battery.max_energy [J]
-battery.
-  mass_gain_factor [kg/W]
-  
-Outputs:
-  mdot             [kg]
-
-
-
-
-
- - - - diff --git a/_site/doxygen/group__Methods-Power-Battery-Variable__Mass.js b/_site/doxygen/group__Methods-Power-Battery-Variable__Mass.js deleted file mode 100644 index 812e5b5d..00000000 --- a/_site/doxygen/group__Methods-Power-Battery-Variable__Mass.js +++ /dev/null @@ -1,5 +0,0 @@ -var group__Methods_Power_Battery_Variable__Mass = -[ - [ "find_mass_gain_rate", "group__Methods-Power-Battery-Variable__Mass.html#ga7e00c9d8f8150f884dac20ff29e5bf03", null ], - [ "find_total_mass_gain", "group__Methods-Power-Battery-Variable__Mass.html#gaf64d2a748bdf09e9612241b60c5d2722", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Methods-Power-Battery.html b/_site/doxygen/group__Methods-Power-Battery.html deleted file mode 100644 index b268a926..00000000 --- a/_site/doxygen/group__Methods-Power-Battery.html +++ /dev/null @@ -1,132 +0,0 @@ - - - - - - - -SUAVE: Battery - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
-
- - - -
-
- -
-
-
- -
- -
-
- - -
- -
- -
- -
-
Battery
-
-
- -

Functions pertaining to battery discharge and sizing. -More...

- - - - - - - - - - - - - - -

-Modules

 Discharge
 Functions to evaluate battery discharge losses and voltage requirements.
 
 Ragone
 Functions to evaluate a Ragone of the battery.
 
 Sizing
 Functions to size battery from mass, specific energy, and specific power.
 
 Variable_Mass
 Functions pertaining to variable mass batteries (such as metal air)
 
-

Detailed Description

-

Functions pertaining to battery discharge and sizing.

-
-
- - - - diff --git a/_site/doxygen/group__Methods-Power-Battery.js b/_site/doxygen/group__Methods-Power-Battery.js deleted file mode 100644 index 3b80e502..00000000 --- a/_site/doxygen/group__Methods-Power-Battery.js +++ /dev/null @@ -1,7 +0,0 @@ -var group__Methods_Power_Battery = -[ - [ "Discharge", "group__Methods-Power-Battery-Discharge.html", "group__Methods-Power-Battery-Discharge" ], - [ "Ragone", "group__Methods-Power-Battery-Ragone.html", "group__Methods-Power-Battery-Ragone" ], - [ "Sizing", "group__Methods-Power-Battery-Sizing.html", "group__Methods-Power-Battery-Sizing" ], - [ "Variable_Mass", "group__Methods-Power-Battery-Variable__Mass.html", "group__Methods-Power-Battery-Variable__Mass" ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Methods-Power-Fuel__Cell-Chemistry.html b/_site/doxygen/group__Methods-Power-Fuel__Cell-Chemistry.html deleted file mode 100644 index 8883646e..00000000 --- a/_site/doxygen/group__Methods-Power-Fuel__Cell-Chemistry.html +++ /dev/null @@ -1,182 +0,0 @@ - - - - - - - -SUAVE: Chemistry - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
-
- - - -
-
- -
-
-
- -
- -
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- - -
- -
- -
- -
-
Chemistry
-
-
- -

Fuel_Cell methods contain the functions for the fuel cell analyses. -More...

- - - - -

-Functions

def SUAVE.Methods.Power.Fuel_Cell.Chemistry.hydrogen.hydrogen (fuel_cell, conditions, numerics)
 
-

Detailed Description

-

Fuel_Cell methods contain the functions for the fuel cell analyses.

-

Function Documentation

- -

◆ hydrogen()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Power.Fuel_Cell.Chemistry.hydrogen.hydrogen ( fuel_cell,
 conditions,
 numerics 
)
-
-
Calculates chemical properties of fuel cell exhaust
- 
-   Assumptions: 
-   Stoichiometric reaction
-   
-   
-   Inputs:
-   fuel_cell.
-     efficiency                     [dimensionless]
-     inputs.
-       power_in                     [Watts]
-     propellant.
-       tag
-       specific_energy              [J/kg]
-     oxidizer.
-       Composition.
-         O2
-   thermo.
-     gamma                          [dimensionless]
-     cp                             [J/kg-K]
-     Tt(to be modified)             [K]
-     Pt(to be modified)             [Pa]
-   
-   Outputs:
-     mdot                           [kg/s]
-     mdot+mdot_air                  [kg/s]
-
-
-
-
- - - - diff --git a/_site/doxygen/group__Methods-Power-Fuel__Cell-Chemistry.js b/_site/doxygen/group__Methods-Power-Fuel__Cell-Chemistry.js deleted file mode 100644 index 427a9574..00000000 --- a/_site/doxygen/group__Methods-Power-Fuel__Cell-Chemistry.js +++ /dev/null @@ -1,4 +0,0 @@ -var group__Methods_Power_Fuel__Cell_Chemistry = -[ - [ "hydrogen", "group__Methods-Power-Fuel__Cell-Chemistry.html#gae19781cb3391103fa518fbb0bee0b7dd", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Methods-Power-Fuel__Cell-Discharge.html b/_site/doxygen/group__Methods-Power-Fuel__Cell-Discharge.html deleted file mode 100644 index b0149844..00000000 --- a/_site/doxygen/group__Methods-Power-Fuel__Cell-Discharge.html +++ /dev/null @@ -1,406 +0,0 @@ - - - - - - - -SUAVE: Discharge - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
-
- - - -
-
- -
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Discharge
-
-
- -

Functions to evaluate fuel cell discharge losses and voltage requirements. -More...

- - - - - - - - - - - - - - - - -

-Functions

def SUAVE.Methods.Power.Fuel_Cell.Discharge.find_power_diff_larminie.find_power_diff_larminie (current_density, fuel_cell, power_desired)
 
def SUAVE.Methods.Power.Fuel_Cell.Discharge.find_power_larminie.find_power_larminie (current_density, fuel_cell, sign=1.0)
 
def SUAVE.Methods.Power.Fuel_Cell.Discharge.find_voltage_larminie.find_voltage_larminie (fuel_cell, current_density)
 
def SUAVE.Methods.Power.Fuel_Cell.Discharge.larminie.larminie (fuel_cell, conditions, numerics)
 
def SUAVE.Methods.Power.Fuel_Cell.Discharge.setup_larminie.setup_larminie (fuel_cell)
 default values representative of a hydrogen fuel cell More...
 
def SUAVE.Methods.Power.Fuel_Cell.Discharge.zero_fidelity.zero_fidelity (fuel_cell, conditions, numerics)
 zero_fidelity.py More...
 
-

Detailed Description

-

Functions to evaluate fuel cell discharge losses and voltage requirements.

-

Function Documentation

- -

◆ find_power_diff_larminie()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Power.Fuel_Cell.Discharge.find_power_diff_larminie.find_power_diff_larminie ( current_density,
 fuel_cell,
 power_desired 
)
-
-
function that determines the power difference between the actual power
-and a desired input power, based on an input current density
-
-Assumptions:
-None
-
-Inputs:
-current_density                [Amps/m**2]
-power_desired                  [Watts]
-fuel_cell
-  
-
-Outputs
-(power_desired-power_out)**2   [Watts**2]
-
-
-
- -

◆ find_power_larminie()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Power.Fuel_Cell.Discharge.find_power_larminie.find_power_larminie ( current_density,
 fuel_cell,
 sign = 1.0 
)
-
-
Function that determines the power output per cell, based on in 
-input current density
-
-Assumptions:
-None(calls other functions)
-
-Inputs:
-current_density      [Amps/m**2]
-fuel cell.
-    interface area   [m**2]
-    
-Outputs:
-power_out            [W]
-
-
- -

◆ find_voltage_larminie()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Power.Fuel_Cell.Discharge.find_voltage_larminie.find_voltage_larminie ( fuel_cell,
 current_density 
)
-
-
function that determines the fuel cell voltage based on an input
-current density and some semi-empirical values to describe the voltage
-drop off with current
-
-Assumptions:
-voltage curve is a function of current density of the form
-v = Eoc-r*i1-A1*np.log(i1)-m*np.exp(n*i1)
-
-Inputs:
-current_density           [A/m**2]
-fuel_cell.
-    r                     [Ohms*m**2]
-    A1                    [V]
-    m                     [V]
-    n                     [m**2/A]
-    Eoc                   [V]
-   
-Outputs:
-    V                     [V]
-
-
- -

◆ larminie()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Power.Fuel_Cell.Discharge.larminie.larminie ( fuel_cell,
 conditions,
 numerics 
)
-
-
function that determines the mass flow rate based on a required power input
-
-Assumptions:
-None (calls other functions)
-
-Inputs:
-fuel_cell.
-    inputs.
-        power_in       [W]
-    ideal_voltage      [V] 
-
-Outputs:
-    mdot               [kg/s]
-
-
- -

◆ setup_larminie()

- -
-
- - - - - - - - -
def SUAVE.Methods.Power.Fuel_Cell.Discharge.setup_larminie.setup_larminie ( fuel_cell)
-
- -

default values representative of a hydrogen fuel cell

-
sets up additional values of fuel cell to run method from Larminie and 
-Dicks (Fuel Cell Systems Explained)
-
-Inputs:
-    fuel cell
- 
-Outputs:
-    fuel_cell.
-        number_of_cells
-        interface_area       [m**2]
-        r                    [ohms*m**2]
-        Eoc                  [V]
-        A1                   [V]
-        m                    [V]
-        n                    [m**2/A]
-        ideal_voltage        [V]
-        cell_density         [kg/m^3]
-        porousity_coeffient  
-
-
- -

◆ zero_fidelity()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Power.Fuel_Cell.Discharge.zero_fidelity.zero_fidelity ( fuel_cell,
 conditions,
 numerics 
)
-
- -

zero_fidelity.py

-

Created : Apr 2015, M. Vegh Modified: Sep 2015, M. Vegh Feb 2016, E. Botero

Assumptions:
-constant efficiency
-
-Inputs:
-    fuel_cell.
-        inputs.
-            power_in              [W]
-        propellant.
-            specific_energy       [J/kg]
-        efficiency    
-
-Outputs:
-    mdot                          [kg/s]
-
-
-
-
- - - - diff --git a/_site/doxygen/group__Methods-Power-Fuel__Cell-Discharge.js b/_site/doxygen/group__Methods-Power-Fuel__Cell-Discharge.js deleted file mode 100644 index 13e54a8b..00000000 --- a/_site/doxygen/group__Methods-Power-Fuel__Cell-Discharge.js +++ /dev/null @@ -1,9 +0,0 @@ -var group__Methods_Power_Fuel__Cell_Discharge = -[ - [ "find_power_diff_larminie", "group__Methods-Power-Fuel__Cell-Discharge.html#ga0d32d07fe34da8f7cd9505514496892c", null ], - [ "find_power_larminie", "group__Methods-Power-Fuel__Cell-Discharge.html#gaaffcb85d0aaa18b15f4d3a512159822d", null ], - [ "find_voltage_larminie", "group__Methods-Power-Fuel__Cell-Discharge.html#ga14d6182cd0cf3bb0726e4d0b12d448d2", null ], - [ "larminie", "group__Methods-Power-Fuel__Cell-Discharge.html#gab8870acc8ac36d11ca9a7a8c9e67da1a", null ], - [ "setup_larminie", "group__Methods-Power-Fuel__Cell-Discharge.html#ga403a82357d1b4c28d50450d77bee0bb6", null ], - [ "zero_fidelity", "group__Methods-Power-Fuel__Cell-Discharge.html#gabefb624517227f36a90278455638b89d", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Methods-Power-Fuel__Cell-Sizing.html b/_site/doxygen/group__Methods-Power-Fuel__Cell-Sizing.html deleted file mode 100644 index 9fa141a0..00000000 --- a/_site/doxygen/group__Methods-Power-Fuel__Cell-Sizing.html +++ /dev/null @@ -1,211 +0,0 @@ - - - - - - - -SUAVE: Sizing - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
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Sizing
-
-
- -

Fuel_Cell methods contain the functions for the fuel cell analyses. -More...

- - - - - - -

-Functions

def SUAVE.Methods.Power.Fuel_Cell.Sizing.initialize_from_power.initialize_from_power (fuel_cell, power)
 
def SUAVE.Methods.Power.Fuel_Cell.Sizing.initialize_larminie_from_power.initialize_larminie_from_power (fuel_cell, power)
 
-

Detailed Description

-

Fuel_Cell methods contain the functions for the fuel cell analyses.

-

Function Documentation

- -

◆ initialize_from_power()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Power.Fuel_Cell.Sizing.initialize_from_power.initialize_from_power ( fuel_cell,
 power 
)
-
-
assigns the mass of the fuel cell based on the power and specific power
-Assumptions:
-None
-
-Inputs:
-power            [J]
-fuel_cell.
-  specific_power [W/kg]
-
-
-Outputs:
-fuel_cell.
-  mass_properties.
-    mass         [kg]
-
-
-
- -

◆ initialize_larminie_from_power()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Power.Fuel_Cell.Sizing.initialize_larminie_from_power.initialize_larminie_from_power ( fuel_cell,
 power 
)
-
-
Initializes extra paramters for the fuel cell when using the larminie method
-Determines the number of stacks
-
-Inputs:
-power                 [W]
-fuel_cell
-
-Outputs:
-
-fuel_cell.
-    power_per_cell    [W]
-    number_of_cells
-    max_power         [W]
-    volume            [m**3]
-    specific_power    [W/kg]
-    mass_properties.
-        mass          [kg]
-
-
-
-
- - - - diff --git a/_site/doxygen/group__Methods-Power-Fuel__Cell-Sizing.js b/_site/doxygen/group__Methods-Power-Fuel__Cell-Sizing.js deleted file mode 100644 index 04084356..00000000 --- a/_site/doxygen/group__Methods-Power-Fuel__Cell-Sizing.js +++ /dev/null @@ -1,5 +0,0 @@ -var group__Methods_Power_Fuel__Cell_Sizing = -[ - [ "initialize_from_power", "group__Methods-Power-Fuel__Cell-Sizing.html#gadb322e6400aa307123b210eee15d77d8", null ], - [ "initialize_larminie_from_power", "group__Methods-Power-Fuel__Cell-Sizing.html#ga25edd0c7cf35cb3c61180d57e8124698", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Methods-Power-Fuel__Cell.html b/_site/doxygen/group__Methods-Power-Fuel__Cell.html deleted file mode 100644 index 11718556..00000000 --- a/_site/doxygen/group__Methods-Power-Fuel__Cell.html +++ /dev/null @@ -1,129 +0,0 @@ - - - - - - - -SUAVE: Fuel_Cell - - - - - - - - - - - - - - - -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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Fuel_Cell
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Fuel_Cell methods contain the functions for the fuel cell analyses. -More...

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-Modules

 Chemistry
 Fuel_Cell methods contain the functions for the fuel cell analyses.
 
 Discharge
 Functions to evaluate fuel cell discharge losses and voltage requirements.
 
 Sizing
 Fuel_Cell methods contain the functions for the fuel cell analyses.
 
-

Detailed Description

-

Fuel_Cell methods contain the functions for the fuel cell analyses.

-
-
- - - - diff --git a/_site/doxygen/group__Methods-Power-Fuel__Cell.js b/_site/doxygen/group__Methods-Power-Fuel__Cell.js deleted file mode 100644 index 431561f5..00000000 --- a/_site/doxygen/group__Methods-Power-Fuel__Cell.js +++ /dev/null @@ -1,6 +0,0 @@ -var group__Methods_Power_Fuel__Cell = -[ - [ "Chemistry", "group__Methods-Power-Fuel__Cell-Chemistry.html", "group__Methods-Power-Fuel__Cell-Chemistry" ], - [ "Discharge", "group__Methods-Power-Fuel__Cell-Discharge.html", "group__Methods-Power-Fuel__Cell-Discharge" ], - [ "Sizing", "group__Methods-Power-Fuel__Cell-Sizing.html", "group__Methods-Power-Fuel__Cell-Sizing" ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Methods-Power.html b/_site/doxygen/group__Methods-Power.html deleted file mode 100644 index b14093fb..00000000 --- a/_site/doxygen/group__Methods-Power.html +++ /dev/null @@ -1,126 +0,0 @@ - - - - - - - -SUAVE: Power - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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Power
-
-
- -

Power methods contain the functions for electric systems such as batteries and fuel cells. -More...

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-Modules

 Battery
 Functions pertaining to battery discharge and sizing.
 
 Fuel_Cell
 Fuel_Cell methods contain the functions for the fuel cell analyses.
 
-

Detailed Description

-

Power methods contain the functions for electric systems such as batteries and fuel cells.

-
-
- - - - diff --git a/_site/doxygen/group__Methods-Power.js b/_site/doxygen/group__Methods-Power.js deleted file mode 100644 index 54443297..00000000 --- a/_site/doxygen/group__Methods-Power.js +++ /dev/null @@ -1,5 +0,0 @@ -var group__Methods_Power = -[ - [ "Battery", "group__Methods-Power-Battery.html", "group__Methods-Power-Battery" ], - [ "Fuel_Cell", "group__Methods-Power-Fuel__Cell.html", "group__Methods-Power-Fuel__Cell" ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Methods-Propulsion.html b/_site/doxygen/group__Methods-Propulsion.html deleted file mode 100644 index a70c84d5..00000000 --- a/_site/doxygen/group__Methods-Propulsion.html +++ /dev/null @@ -1,295 +0,0 @@ - - - - - - - -SUAVE: Propulsion - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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Propulsion
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Description. -More...

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-Functions

def SUAVE.Methods.Propulsion.ducted_fan_sizing.ducted_fan_sizing (ducted_fan, mach_number=None, altitude=None, delta_isa=0, conditions=None)
 
def SUAVE.Methods.Propulsion.electric_motor_sizing.size_from_kv (motor, kv)
 
def SUAVE.Methods.Propulsion.fm_id.fm_id (M)
 fm_id.py More...
 
def SUAVE.Methods.Propulsion.turbofan_nox_emission_index.turbofan_nox_emission_index (turbofan, state)
 
-

Detailed Description

-

Description.

-

Function Documentation

- -

◆ ducted_fan_sizing()

- -
-
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def SUAVE.Methods.Propulsion.ducted_fan_sizing.ducted_fan_sizing ( ducted_fan,
 mach_number = None,
 altitude = None,
 delta_isa = 0,
 conditions = None 
)
-
-
creates and evaluates a ducted_fan network based on an atmospheric sizing condition
-
-Inputs:
-ducted_fan       ducted fan network object (to be modified)
-mach_number
-altitude         [meters]
-delta_isa        temperature difference [K]
-conditions       ordered dict object
-
-
-
- -

◆ fm_id()

- -
-
- - - - - - - - -
def SUAVE.Methods.Propulsion.fm_id.fm_id ( M)
-
- -

fm_id.py

-

Created: ### ####, SUAVE Team Modified: Feb 2016, E. Botero

Function that takes in the Mach number, and outputs a function fm
-that's commonly used in compressible flow calculations
-
-Inputs:
-M       [dimensionless]
-
-Outputs:
-fm
-
-
- -

◆ size_from_kv()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Propulsion.electric_motor_sizing.size_from_kv ( motor,
 kv 
)
-
-
Determines a motors mass based on the speed constant KV
-
-Source:
-Gur, O., Rosen, A, AIAA 2008-5916.
-
-Inputs:
-motor    (to be modified)
-kv       motor speed constant
-
-Outputs:
-motor.
-  resistance         [ohms]
-  no_load_current    [amps]
-  mass               [kg]
-
-
- -

◆ turbofan_nox_emission_index()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Propulsion.turbofan_nox_emission_index.turbofan_nox_emission_index ( turbofan,
 state 
)
-
-
Outputs a turbofan's nox_emission_index takens from a regression calculated
-from NASA's Engine Performance Program (NEPP)
-
-Inputs:
-turbofan.
-  combustor.
-    inputs.
-      stagnation_pressure     [Pa]
-      stagnation_temperature  [K]
-    outputs.
-      stagnation_temperature  [K]
-      
-Outputs:      
-nox_emission_index            [kg/kg]
-
-Source: Antione, Nicholas, Aircraft Optimization for Minimal Environmental Impact, pp. 31 (PhD Thesis)
-
-
-
-
- - - - diff --git a/_site/doxygen/group__Methods-Propulsion.js b/_site/doxygen/group__Methods-Propulsion.js deleted file mode 100644 index 0ff7fa1f..00000000 --- a/_site/doxygen/group__Methods-Propulsion.js +++ /dev/null @@ -1,7 +0,0 @@ -var group__Methods_Propulsion = -[ - [ "ducted_fan_sizing", "group__Methods-Propulsion.html#ga3e6153003ae73397bf8d06367e10e9ba", null ], - [ "fm_id", "group__Methods-Propulsion.html#ga5eee2c77f3e47c316ee77b8960b86866", null ], - [ "size_from_kv", "group__Methods-Propulsion.html#ga7448a7c9da5a37c6912b33fd90c98306", null ], - [ "turbofan_nox_emission_index", "group__Methods-Propulsion.html#gabc52d81a51c667a4bad13558e252ba07", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Methods-Utilities-Chebyshev.html b/_site/doxygen/group__Methods-Utilities-Chebyshev.html deleted file mode 100644 index 9cea058d..00000000 --- a/_site/doxygen/group__Methods-Utilities-Chebyshev.html +++ /dev/null @@ -1,250 +0,0 @@ - - - - - - - -SUAVE: Chebyshev - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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Chebyshev
-
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These functions provide methods for discrete derivative and integral calculations. -More...

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-Functions

def SUAVE.Methods.Utilities.Chebyshev.chebyshev_data.chebyshev_data (N=16, integration=True, options)
 
def SUAVE.Methods.Utilities.Chebyshev.linear_data.linear_data (N=16, integration=True, options)
 
-

Detailed Description

-

These functions provide methods for discrete derivative and integral calculations.

-

Function Documentation

- -

◆ chebyshev_data()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Utilities.Chebyshev.chebyshev_data.chebyshev_data ( N = 16,
 integration = True,
 options 
)
-
-
Calculates the differentiation and integration matricies
-using chebyshev's pseudospectral algorithm, based on cosine
-spaced samples in x.
-
-D and I are not symmetric
-get derivatives with df_dy = np.dot(D,f)
-get integral with    int_f = np.dot(I,f)
-    where f is either a 1-d vector or 2-d column array
-    
-A full example is available in the function code.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-N                      [-]        Number of points
-integration (optional) <boolean>  Determines if the integration operator is calculated
-
-Outputs:
-x                      [-]        N-number of cosine spaced control points, in range [0,1]
-D                      [-]        Differentiation operation matrix
-I                      [-]        Integration operation matrix, or None if integration = False
-
-Properties Used:
-N/A
-
-
-
- -

◆ linear_data()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Utilities.Chebyshev.linear_data.linear_data ( N = 16,
 integration = True,
 options 
)
-
-
Calculates the differentiation and integration matricies
-using chebyshev's pseudospectral algorithm, based on linearly
-spaced samples in x.
-
-D and I are not symmetric
-get derivatives with df_dy = np.dot(D,f)
-get integral with    int_f = np.dot(I,f)
-    where f is either a 1-d vector or 2-d column array
-    
-A full example of how these operators are used is available in 
-the chebyshev_data.py (same folder)
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-N                      [-]        Number of points
-integration (optional) <boolean>  Determines if the integration operator is calculated
-
-Outputs:
-x                      [-]        N-number of cosine spaced control points, in range [0,1]
-D                      [-]        Differentiation operation matrix
-I                      [-]        Integration operation matrix, or None if integration = False
-
-Properties Used:
-N/A
-
-
-
-
-
- - - - diff --git a/_site/doxygen/group__Methods-Utilities-Chebyshev.js b/_site/doxygen/group__Methods-Utilities-Chebyshev.js deleted file mode 100644 index 733e8249..00000000 --- a/_site/doxygen/group__Methods-Utilities-Chebyshev.js +++ /dev/null @@ -1,5 +0,0 @@ -var group__Methods_Utilities_Chebyshev = -[ - [ "chebyshev_data", "group__Methods-Utilities-Chebyshev.html#ga52d35a64916a9bce3b636e296f4ef53b", null ], - [ "linear_data", "group__Methods-Utilities-Chebyshev.html#ga63215eedc2e365dd6273325e8a142b48", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Methods-Utilities.html b/_site/doxygen/group__Methods-Utilities.html deleted file mode 100644 index dc9e72b8..00000000 --- a/_site/doxygen/group__Methods-Utilities.html +++ /dev/null @@ -1,243 +0,0 @@ - - - - - - - -SUAVE: Utilities - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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Utilities
-
-
- -

These provide functionality that is not easily grouped into another set. -More...

- - - - - -

-Modules

 Chebyshev
 These functions provide methods for discrete derivative and integral calculations.
 
- - - - - - -

-Functions

def SUAVE.Methods.Utilities.latin_hypercube_sampling.latin_hypercube_sampling (num_dimensions, num_samples, bounds=None, criterion='random')
 If needed for mapping to normal distribution: from scipy.stats.distributions import norm. More...
 
def SUAVE.Methods.Utilities.soft_max.soft_max (x1, x2)
 
-

Detailed Description

-

These provide functionality that is not easily grouped into another set.

-

Most of these provide some type of mathematical functionality.

-

Function Documentation

- -

◆ latin_hypercube_sampling()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Utilities.latin_hypercube_sampling.latin_hypercube_sampling ( num_dimensions,
 num_samples,
 bounds = None,
 criterion = 'random' 
)
-
- -

If needed for mapping to normal distribution: from scipy.stats.distributions import norm.

-
Provides an array of chosen dimensionality and number of samples taken according
-to latin hypercube sampling. Bounds can be optionally specified.
-
-Assumptions:
-None
-
-Source:
-None
-
-Inputs:
-num_dimensions       [-]
-num_samples          [-]
-bounds (optional)    [-]      Default is 0 to 1. Input value should be in the form (with numpy arrays)
-                              (array([low_bnd_1,low_bnd_2,..]), array([up_bnd_1,up_bnd_2,..]))
-criterion            <string> Possible values: random and center. Determines if samples are 
-                              taken at the center of a bucket or randomly from within it.
-                     
-Outputs:             
-lhd                  [-]      Array of samples
-
-Properties Used:
-N/A
-
-
-
- -

◆ soft_max()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Utilities.soft_max.soft_max ( x1,
 x2 
)
-
-
Computes the soft maximum of two inputs.
-
-Assumptions:
-None
-
-Source:
-http://www.johndcook.com/blog/2010/01/20/how-to-compute-the-soft-maximum/
-
-Inputs:
-x1   [-]
-x2   [-]
-
-Outputs:             
-f    [-] The soft max
-
-Properties Used:
-N/A
-
-
-
-
-
- - - - diff --git a/_site/doxygen/group__Methods-Utilities.js b/_site/doxygen/group__Methods-Utilities.js deleted file mode 100644 index d1da47b9..00000000 --- a/_site/doxygen/group__Methods-Utilities.js +++ /dev/null @@ -1,6 +0,0 @@ -var group__Methods_Utilities = -[ - [ "Chebyshev", "group__Methods-Utilities-Chebyshev.html", "group__Methods-Utilities-Chebyshev" ], - [ "latin_hypercube_sampling", "group__Methods-Utilities.html#gad7f4326f99edc2e3d142e7d2a0fffcf0", null ], - [ "soft_max", "group__Methods-Utilities.html#ga839620ce7852f1839a0d851f4a21475d", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Methods-Weights-Correlations-BWB.html b/_site/doxygen/group__Methods-Weights-Correlations-BWB.html deleted file mode 100644 index fa439f21..00000000 --- a/_site/doxygen/group__Methods-Weights-Correlations-BWB.html +++ /dev/null @@ -1,385 +0,0 @@ - - - - - - - -SUAVE: BWB - - - - - - - - - - - - - - - -
-
- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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Provides structural weight correlations for a BWB concept. -More...

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-Functions

def SUAVE.Methods.Weights.Correlations.BWB.aft_centerbody.aft_centerbody (no_of_engines, aft_centerbody_area, aft_centerbody_taper, TOGW)
 
def SUAVE.Methods.Weights.Correlations.BWB.cabin.cabin (cabin_area, TOGW)
 
def SUAVE.Methods.Weights.Correlations.BWB.empty.empty (vehicle)
 
def SUAVE.Methods.Weights.Correlations.BWB.systems.systems (num_seats, ctrl_type, S_h, S_gross_w, ac_type)
 
-

Detailed Description

-

Provides structural weight correlations for a BWB concept.

-

Function Documentation

- -

◆ aft_centerbody()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Weights.Correlations.BWB.aft_centerbody.aft_centerbody ( no_of_engines,
 aft_centerbody_area,
 aft_centerbody_taper,
 TOGW 
)
-
-
Weight estimate for the aft section of a BWB centerbody.
-Regression from FEA by K. Bradley (George Washington University).
-
-Assumptions:
-    -The engines are mounted on the aft centerbody
-    -The aft centerbody is unpressurized
-
-Sources:
-    Bradley, K. R., "A Sizing Methodology for the Conceptual Design of 
-    Blended-Wing-Body Transports," NASA/CR-2004-213016, 2004.
-    
-Inputs:
-    no_of_engines - the number of engines mounted on the aft centerbody 
-    [dimensionless]
-    aft_centerbody_area - the planform area of the aft centerbody. 
-    Typcially the area behind 70% chord [meters**2]
-    aft_centerbody_taper - the taper ratio of the aft centerbody (exclude
-    the chord taken up by the pressurized passenger cabin) [dimensionless]
-    TOGW - Takeoff gross weight of the aircraft [kilograms]
-Outputs:
-    aft_wt - the estimated structural weight of the BWB aft centerbody
-        
-Properties Used:
-N/A
-
-
-
- -

◆ cabin()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Weights.Correlations.BWB.cabin.cabin ( cabin_area,
 TOGW 
)
-
-
Weight estimate for the cabin (forward section of centerbody) of a BWB.
-Regression from FEA by K. Bradley (George Washington University).
-
-Assumptions:
-    -The centerbody uses a pressurized sandwich composite structure
-    -Ultimate cabin pressure differential of 18.6psi
-    -Critical flight condition: +2.5g maneuver at maximum TOGW
-
-Sources:
-    Bradley, K. R., "A Sizing Methodology for the Conceptual Design of 
-    Blended-Wing-Body Transports," NASA/CR-2004-213016, 2004.
-
-Inputs:
-    cabin_area - the planform area representing the passenger cabin  [meters**2]
-    TOGW - Takeoff gross weight of the aircraft                      [kilograms]
-Outputs:
-    cabin_wt - the estimated structural weight of the BWB cabin      [kilograms]
-        
-Properties Used:
-N/A
-
-
-
- -

◆ empty()

- -
-
- - - - - - - - -
def SUAVE.Methods.Weights.Correlations.BWB.empty.empty ( vehicle)
-
-
This is for a BWB aircraft configuration. 
-
-Assumptions:
-     calculated aircraft weight from correlations created per component of historical aircraft
-  
-Source: 
-    N/A
-     
-Inputs:
-    engine - a data dictionary with the fields:                    
-        thrust_sls - sea level static thrust of a single engine                                        [Newtons]
-
-    wing - a data dictionary with the fields:
-        gross_area - wing gross area                                                                   [meters**2]
-        span - span of the wing                                                                        [meters]
-        taper - taper ratio of the wing                                                                [dimensionless]
-        t_c - thickness-to-chord ratio of the wing                                                     [dimensionless]
-        sweep - sweep angle of the wing                                                                [radians]
-        mac - mean aerodynamic chord of the wing                                                       [meters]
-        r_c - wing root chord                                                                          [meters]
-
-    aircraft - a data dictionary with the fields:                    
-        Nult - ultimate load of the aircraft                                                           [dimensionless]
-        Nlim - limit load factor at zero fuel weight of the aircraft                                   [dimensionless]
-        TOW - maximum takeoff weight of the aircraft                                                   [kilograms]
-        zfw - maximum zero fuel weight of the aircraft                                                 [kilograms]
-        num_eng - number of engines on the aircraft                                                    [dimensionless]
-        num_pax - number of passengers on the aircraft                                                 [dimensionless]
-        wt_cargo - weight of the bulk cargo being carried on the aircraft                              [kilograms]
-        num_seats - number of seats installed on the aircraft                                          [dimensionless]
-        ctrl - specifies if the control system is "fully powered", "partially powered", or not powered [dimensionless]
-        ac - determines type of instruments, electronics, and operating items based on types: 
-            "short-range", "medium-range", "long-range", "business", "cargo", "commuter", "sst"        [dimensionless]
-
-     fuselage - a data dictionary with the fields:
-        area - fuselage wetted area                                                                    [meters**2]
-        diff_p - Maximum fuselage pressure differential                                                [Pascal]
-        width - width of the fuselage                                                                  [meters]
-        height - height of the fuselage                                                                [meters]
-        length - length of the fuselage                                                                [meters]   
-    
-Outputs:
-    output - a data dictionary with fields:
-        wt_payload - weight of the passengers plus baggage and paid cargo                              [kilograms]
-        wt_pax - weight of all the passengers                                                          [kilogram]
-        wt_bag - weight of all the baggage                                                             [kilogram]
-        wt_fuel - weight of the fuel carried                                                           [kilogram]
-        wt_empty - operating empty weight of the aircraft                                              [kilograms]
-
-Properties Used:
-N/A
-
-
-
- -

◆ systems()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Weights.Correlations.BWB.systems.systems ( num_seats,
 ctrl_type,
 S_h,
 S_gross_w,
 ac_type 
)
-
-
Calculate the weight of the different engine systems on the aircraft
-
-Assumptions:
-    numbers based on FAA regulations and correlations from previous aircraft
-            
-Source:
-    N/A  
-
-Inputs:
-    num_seats - total number of seats on the aircraft                                                   [dimensionless]
-    ctrl_type - specifies if the control system is fully power, partially powered, or not powered       [dimensionless]
-    S_h - area of the BWB outer aileron                                                                 [meters**2]
-    S_gross_w - area of the wing                                                                        [meters**2]
-    ac_type - determines type of instruments, electronics, and operating items based on type of vehicle [dimensionless]
-
-Outputs:
-    output - a data dictionary with fields:
-        wt_flt_ctrl - weight of the flight control system                                               [kilograms]
-        wt_apu - weight of the apu                                                                      [kilograms]
-        wt_hyd_pnu - weight of the hydraulics and pneumatics                                            [kilograms]
-        wt_instruments - weight of the instruments and navigational equipment                           [kilograms]
-        wt_avionics - weight of the avionics                                                            [kilograms]
-        wt_opitems - weight of the optional items based on the type of aircraft                         [kilograms]
-        wt_elec - weight of the electrical items                                                        [kilograms]
-        wt_ac - weight of the air conditioning and anti-ice system                                      [kilograms]
-        wt_furnish - weight of the furnishings in the fuselage                                          [kilograms]
-    
-Properties Used:
-N/A
-
-
-
-
-
- - - - diff --git a/_site/doxygen/group__Methods-Weights-Correlations-BWB.js b/_site/doxygen/group__Methods-Weights-Correlations-BWB.js deleted file mode 100644 index 8c23c589..00000000 --- a/_site/doxygen/group__Methods-Weights-Correlations-BWB.js +++ /dev/null @@ -1,7 +0,0 @@ -var group__Methods_Weights_Correlations_BWB = -[ - [ "aft_centerbody", "group__Methods-Weights-Correlations-BWB.html#ga6fbf6d817a459d781b07fa73faeee5ad", null ], - [ "cabin", "group__Methods-Weights-Correlations-BWB.html#gaf79b9d073d3341d628c056ca69469809", null ], - [ "empty", "group__Methods-Weights-Correlations-BWB.html#ga94172601f2f840265bd87601800de860", null ], - [ "systems", "group__Methods-Weights-Correlations-BWB.html#ga49462fb84af76259349c80f42402decf", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Methods-Weights-Correlations-Common.html b/_site/doxygen/group__Methods-Weights-Correlations-Common.html deleted file mode 100644 index a278856e..00000000 --- a/_site/doxygen/group__Methods-Weights-Correlations-Common.html +++ /dev/null @@ -1,343 +0,0 @@ - - - - - - - -SUAVE: Common - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
-
- - - -
-
- -
-
-
- -
- -
-
- - -
- -
- -
- - -
-
- -

Provides structural weight correlations for aircraft components applicable to all aircraft configurations. -More...

- - - - - - - - - -

-Functions

def SUAVE.Methods.Weights.Correlations.Common.landing_gear.landing_gear (TOW, landing_gear_wt_factor=0.04)
 landing_gear.py More...
 
def SUAVE.Methods.Weights.Correlations.Common.payload.payload (TOW, empty, num_pax, wt_cargo, wt_passenger=195 *Units.lbs, wt_baggage=30 *Units.lbs)
 
def SUAVE.Methods.Weights.Correlations.Common.wing_main.wing_main (S_gross_w, b, lambda_w, t_c_w, sweep_w, Nult, TOW, wt_zf)
 
-

Detailed Description

-

Provides structural weight correlations for aircraft components applicable to all aircraft configurations.

-

Function Documentation

- -

◆ landing_gear()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Weights.Correlations.Common.landing_gear.landing_gear ( TOW,
 landing_gear_wt_factor = 0.04 
)
-
- -

landing_gear.py

-

Created: Jan 2014, A. Wendorff Modified: Feb 2016, E. Botero Jul 2017, M. Clarke

Calculate the weight of the landing gear assuming that the gear 
-weight is 4 percent of the takeoff weight        
-
-Assumptions:
-    calculating the landing gear weight based on the takeoff weight
-
-Source: 
-    N/A
-    
-Inputs:
-    TOW - takeoff weight of the aircraft                              [kilograms]
-    landing_gear_wt_factor - landing gear weight as percentage of TOW [dimensionless]
-
-Outputs:
-    weight - weight of the landing gear                               [kilograms]
-        
-Properties Used:
-    N/A
-
-
-
- -

◆ payload()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Weights.Correlations.Common.payload.payload ( TOW,
 empty,
 num_pax,
 wt_cargo,
 wt_passenger = 195*Units.lbs,
 wt_baggage = 30*Units.lbs 
)
-
-
Calculate the weight of the payload and the resulting fuel mass
-
-Assumptions:
-    based on FAA guidelines for weight of passengers
-    
-Source: 
-    N/A
-    
-Inputs:
-    TOW -                                                              [kilograms]
-    wt_empty - Operating empty weight of the aircraft                  [kilograms]
-    num_pax - number of passengers on the aircraft                     [dimensionless]
-    wt_cargo - weight of cargo being carried on the aircraft           [kilogram]
-    wt_passenger - weight of each passenger on the aircraft            [kilogram]
-    wt_baggage - weight of the baggage for each passenger              [kilogram]
-
-Outputs:
-    output - a data dictionary with fields:
-        payload - weight of the passengers plus baggage and paid cargo [kilograms]
-        pax - weight of all the passengers                             [kilogram]
-        bag - weight of all the baggage                                [kilogram]
-        fuel - weight of the fuel carried                              [kilogram]
-        empty - operating empty weight of the aircraft                 [kilograms]
-           
-Properties Used:
-    N/A
-
-
-
- -

◆ wing_main()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Weights.Correlations.Common.wing_main.wing_main ( S_gross_w,
 b,
 lambda_w,
 t_c_w,
 sweep_w,
 Nult,
 TOW,
 wt_zf 
)
-
-
Calculate the wing weight of the aircraft based on the fully-stressed 
-bending weight of the wing box
-
-Assumptions:
-    calculated total wing weight based on a bending index and actual data 
-    from 15 transport aircraft 
-
-Source: 
-    N/A
-    
-Inputs:
-    S_gross_w - area of the wing                 [meters**2]
-    b - span of the wing                         [meters**2]
-    lambda_w - taper ratio of the wing           [dimensionless]
-    t_c_w - thickness-to-chord ratio of the wing [dimensionless]
-    sweep_w - sweep of the wing                  [radians]
-    Nult - ultimate load factor of the aircraft  [dimensionless]
-    TOW - maximum takeoff weight of the aircraft [kilograms]
-    wt_zf - zero fuel weight of the aircraft     [kilograms]
-
-Outputs:
-    weight - weight of the wing                  [kilograms]          
-    
-Properties Used:
-    N/A
-
-
-
-
-
- - - - diff --git a/_site/doxygen/group__Methods-Weights-Correlations-Common.js b/_site/doxygen/group__Methods-Weights-Correlations-Common.js deleted file mode 100644 index ff27346f..00000000 --- a/_site/doxygen/group__Methods-Weights-Correlations-Common.js +++ /dev/null @@ -1,6 +0,0 @@ -var group__Methods_Weights_Correlations_Common = -[ - [ "landing_gear", "group__Methods-Weights-Correlations-Common.html#ga8a44f526125ceed65e6d2f27fe5aa82c", null ], - [ "payload", "group__Methods-Weights-Correlations-Common.html#gacf280c435b3294c568c1b374d0ff7c3b", null ], - [ "wing_main", "group__Methods-Weights-Correlations-Common.html#gaeaee339d59dc928ac31ef8a65ddbde33", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Methods-Weights-Correlations-Human__Powered.html b/_site/doxygen/group__Methods-Weights-Correlations-Human__Powered.html deleted file mode 100644 index 847b90e4..00000000 --- a/_site/doxygen/group__Methods-Weights-Correlations-Human__Powered.html +++ /dev/null @@ -1,445 +0,0 @@ - - - - - - - -SUAVE: Human_Powered - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
-
- - - -
-
- -
-
-
- -
- -
-
- - -
- -
- -
- -
-
Human_Powered
-
-
- -

Provides structural weight correlations for a human-powered aircraft; applicable to solar-UAVs. -More...

- - - - - - - - - - - - - -

-Functions

def SUAVE.Methods.Weights.Correlations.Human_Powered.empty.empty (vehicle)
 
def SUAVE.Methods.Weights.Correlations.Human_Powered.fuselage.fuselage (Sts, qm, Ltb)
 fuselage.py More...
 
def SUAVE.Methods.Weights.Correlations.Human_Powered.tail.tail (Sts, bts, cts, Ntsr, t_cts, qm)
 tail.py More...
 
def SUAVE.Methods.Weights.Correlations.Human_Powered.wing.wing (Sw, bw, cw, Nwr, t_cw, Nwer, nult, GW)
 wing.py More...
 
-

Detailed Description

-

Provides structural weight correlations for a human-powered aircraft; applicable to solar-UAVs.

-

Function Documentation

- -

◆ empty()

- -
-
- - - - - - - - -
def SUAVE.Methods.Weights.Correlations.Human_Powered.empty.empty ( vehicle)
-
-
Computes weights estimates for human powered aircraft
-
-Assumptions:
-   All of this is from AIAA 89-2048, units are in kg. These weight estimates
-   are from the MIT Daedalus and are valid for very lightweight
-   carbon fiber composite structures. This may need to be solved iteratively since
-   gross weight is an input.
-   
-Source: 
-    MIT Daedalus
-                   
-Inputs:
-    wing - a data dictionary with the fields:
-        Sw -       wing area                                                       [meters**2]
-        bw -       wing span                                                       [meters]
-        cw -       average wing chord                                              [meters]
-        deltaw -   average rib spacing to average chord ratio                      [dimensionless]
-        Nwr -      number of wing surface ribs (bw**2)/(deltaw*Sw)                 [dimensionless]
-        t_cw -     wing airfoil thickness to chord ratio                           [dimensionless]
-        Nwer -     number of wing end ribs (2*number of individual wing panels -2) [dimensionless]
-        
-    horizontal - a data dictionary with the fields:
-        Sts -      tail surface area                                               [meters]
-        bts -      tail surface span                                               [meters]
-        cts -      average tail surface chord                                      [meters]
-        deltawts - average rib spacing to average chord ratio                      [dimensionless]
-        Ntsr -     number of tail surface ribs (bts^2)/(deltats*Sts)               [dimensionless]
-        t_cts -    tail airfoil thickness to chord ratio                           [dimensionless]
-        
-    vertical - a data dictionary with the fields:
-        Sts -      tail surface area                                               [meters]
-        bts -      tail surface span                                               [meters]
-        cts -      average tail surface chord                                      [meters]
-        deltawts - average rib spacing to average chord ratio                      [dimensionless]
-        Ntsr -     number of tail surface ribs (bts**2)/(deltats*Sts)              [dimensionless]
-        t_cts -    tail airfoil thickness to chord ratio                           [dimensionless]
-        
-    aircraft - a data dictionary with the fields:    
-        nult -     ultimate load factor                                            [dimensionless]
-        GW -       aircraft gross weight                                           [kilogram]
-        qm -       dynamic pressure at maneuvering speed                           [Pascals]
-        Ltb -      tailboom length                                                 [meters]
-
-Outputs:
-    Wws -      weight of wing spar                                                 [kilogram]
-    Wtss -     weight of tail surface spar                                         [kilogram]
-    Wwr -      weight of wing ribs                                                 [kilogram]
-    Wtsr -     weight of tail surface ribs                                         [kilogram]
-    Wwer -     weight of wing end ribs                                             [kilogram]
-    WwLE -     weight of wing leading edge                                         [kilogram]
-    WtsLE -    weight of tail surface leading edge                                 [kilogram]
-    WwTE -     weight of wing trailing edge                                        [kilogram]
-    Wwc -      weight of wing covering                                             [kilogram]
-    Wtsc -     weight of tail surface covering                                     [kilogram]
-    Wtb -      tailboom weight                                                     [kilogram]
-            
-Properties Used:
-    N/A
-
-
-
- -

◆ fuselage()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Weights.Correlations.Human_Powered.fuselage.fuselage ( Sts,
 qm,
 Ltb 
)
-
- -

fuselage.py

-

Created: Jun 2014, E. Botero Modified: Feb 2016, E. Botero

Compute weifht estimate of human-powered aircraft fuselage 
-
-Assumptions:
-   All of this is from AIAA 89-2048, units are in kg. These weight estimates
-   are from the MIT Daedalus and are valid for very lightweight
-   carbon fiber composite structures. This may need to be solved iteratively since
-   gross weight is an input.
-   
-Source: 
-    MIT Daedalus
-    
-Inputs:
-    Sts -      tail surface area                     [meters]
-    qm -       dynamic pressure at maneuvering speed [Pascals]
-    Ltb -      tailboom length                       [meters]
-
-Outputs:
-    Wtb -      tailboom weight                       [kilogram]
-    
-Properties Used:
-    N/A
-
-
-
- -

◆ tail()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Weights.Correlations.Human_Powered.tail.tail ( Sts,
 bts,
 cts,
 Ntsr,
 t_cts,
 qm 
)
-
- -

tail.py

-

Created: Jun 2014, E. Botero Modified: Feb 2016, E. Botero

Compute weight of human-powered aircraft tail     
-
-Assumptions:
-   All of this is from AIAA 89-2048, units are in kg. These weight estimates
-   are from the MIT Daedalus and are valid for very lightweight
-   carbon fiber composite structures. This may need to be solved iteratively since
-   gross weight is an input.
-   
-Source: 
-    MIT Daedalus
-            
-Inputs:
-    Sts -      tail surface area                                [meters]
-    bts -      tail surface span                                [meters]
-    cts -      average tail surface chord                       [meters]
-    deltats -  average rib spacing to average chord ratio       [dimensionless]
-    Ntsr -     number of tail surface ribs (bts^2)/(deltats*Sts)[dimensionless]
-    t_cts -    tail airfoil thickness to chord ratio            [dimensionless]
-    qm -       dynamic pressure at maneuvering speed            [Pascals]
-
-Outputs:
-    Wtss -     weight of tail surface spar                      [kilogram]
-    Wtsr -     weight of tail surface ribs                      [kilogram]
-    WtsLE -    weight of tail surface leading edge              [kilogram]
-    Wtsc -     weight of tail surface covering                  [kilogram]
-        
-Properties Used:
-    N/A
-
-
-
- -

◆ wing()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Weights.Correlations.Human_Powered.wing.wing ( Sw,
 bw,
 cw,
 Nwr,
 t_cw,
 Nwer,
 nult,
 GW 
)
-
- -

wing.py

-

Created: Jun 2014, E. Botero Modified: Feb 2016, E. Botero

Compute weight of human-powered aircraft wing 
-
-Assumptions:
-   All of this is from AIAA 89-2048, units are in kg. These weight estimates
-   are from the MIT Daedalus and are valid for very lightweight
-   carbon fiber composite structures. This may need to be solved iteratively since
-   gross weight is an input.
-   
-Source: 
-    MIT Daedalus
-    
-Inputs:
-    Sw -       wing area                                                       [meters**2]
-    bw -       wing span                                                       [meters]
-    cw -       average wing chord                                              [meters]
-    eltaw -   average rib spacing to average chord ratio                       [dimensionless]
-    Nwr -      number of wing or tail surface ribs (bw^2)/(deltaw*Sw)          [dimensionless]
-    t_cw -     wing airfoil thickness to chord ratio                           [dimensionless]
-    Nwer -     number of wing end ribs (2*number of individual wing panels -2) [dimensionless]
-    nult -     ultimate load factor                                            [dimensionless]
-    GW -       aircraft gross weight                                           [kilogram]
-
-Outputs:
-    Wws -      weight of wing spar                                             [kilogram]
-    Wwr -      weight of wing ribs                                             [kilogram]
-    Wwer -     weight of wing end ribs                                         [kilogram]
-    WwLE -     weight of wing leading edge                                     [kilogram]
-    WwTE -     weight of wing trailing edge                                    [kilogram]
-    Wwc -      weight of wing covering                                         [kilogram]
-
-Properties Used:
-    N/A
-
-
-
-
-
- - - - diff --git a/_site/doxygen/group__Methods-Weights-Correlations-Human__Powered.js b/_site/doxygen/group__Methods-Weights-Correlations-Human__Powered.js deleted file mode 100644 index 5ec660ac..00000000 --- a/_site/doxygen/group__Methods-Weights-Correlations-Human__Powered.js +++ /dev/null @@ -1,7 +0,0 @@ -var group__Methods_Weights_Correlations_Human__Powered = -[ - [ "empty", "group__Methods-Weights-Correlations-Human__Powered.html#gaaecbf938c83082c10701c8c5b358d9f3", null ], - [ "fuselage", "group__Methods-Weights-Correlations-Human__Powered.html#gaeec5ba9b1b81becbceda022ba62a5439", null ], - [ "tail", "group__Methods-Weights-Correlations-Human__Powered.html#gac77c04f3e7f673c8dcb0414cdf63a415", null ], - [ "wing", "group__Methods-Weights-Correlations-Human__Powered.html#ga44dc2d0fd1cde113b20de336869fd6c7", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Methods-Weights-Correlations-Propulsion.html b/_site/doxygen/group__Methods-Weights-Correlations-Propulsion.html deleted file mode 100644 index d90ec2b1..00000000 --- a/_site/doxygen/group__Methods-Weights-Correlations-Propulsion.html +++ /dev/null @@ -1,314 +0,0 @@ - - - - - - - -SUAVE: Propulsion - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
-
- - - -
-
- -
-
-
- -
- -
-
- - -
- -
- -
- -
-
Propulsion
-
-
- -

Contains some methods for calculating different propulsion system weights. -More...

- - - - - - - - - - - - -

-Functions

def SUAVE.Methods.Weights.Correlations.Propulsion.air_cooled_motor.air_cooled_motor (max_power, kwt2=1.96, xwt=.8897)
 
def SUAVE.Methods.Weights.Correlations.Propulsion.engine_jet.engine_jet (thrust_sls)
 
def SUAVE.Methods.Weights.Correlations.Propulsion.hts_motor.hts_motor (max_power)
 hts_motor.py More...
 
def SUAVE.Methods.Weights.Correlations.Propulsion.integrated_propulsion.integrated_propulsion (engine_jet, num_eng, engine_wt_factor=1.6)
 integrated_propulsion.py More...
 
-

Detailed Description

-

Contains some methods for calculating different propulsion system weights.

-

Function Documentation

- -

◆ air_cooled_motor()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Weights.Correlations.Propulsion.air_cooled_motor.air_cooled_motor ( max_power,
 kwt2 = 1.96,
 xwt = .8897 
)
-
-
Calculate the weight of an air-cooled motor    
-weight correlation; weight=kwt2*(max_power**xwt)
-    
-Assumptions:
-        calculated from fit of commercial available motors
-        
-Source: Sinsay, J.D., Tracey, B., Alonso, J.J., Kontinos, D.K., Melton, J.E., Grabbe, S.,
-        "Air Vehicle Design and Technology Considerations for an Electric VTOL Metro-Regional Public Transportation System,"
-        12th AIAA Aviation Technology, Integration, and Operations (ATIO) Conference and 14th AIAA/ISSMO Multidisciplinary
-        Analysis and Optimization Conference, Indianapolis, IN, Sept.2012  
-
-Inputs:
-        max_power- maximum power the motor can deliver safely      [Watts]
-        kwt2
-        xwt
-        
-Outputs:
-        weight- weight of the motor                                [kilograms]
-    
-Properties Used:
-        N/A
-
-
-
- -

◆ engine_jet()

- -
-
- - - - - - - - -
def SUAVE.Methods.Weights.Correlations.Propulsion.engine_jet.engine_jet ( thrust_sls)
-
-
Calculate the weight of the dry engine  
-
-Assumptions:
-        calculated engine weight from a correlation of engines
-
-Source: 
-        N/A
-        
-Inputs:
-        thrust_sls - sea level static thrust of a single engine [Newtons]
-
-Outputs:
-        weight - weight of the dry engine                       [kilograms]
-    
-Properties Used:
-        N/A
-
-
-
- -

◆ hts_motor()

- -
-
- - - - - - - - -
def SUAVE.Methods.Weights.Correlations.Propulsion.hts_motor.hts_motor ( max_power)
-
- -

hts_motor.py

-

Created: Jan 2014, M. Vegh, Modified: Feb 2014, A. Wendorff Feb 2016, E. Botero

Calculate the weight of a high temperature superconducting motor
-
-   Assumptions:
-       calculated from fit of commercial available motors
-       
-   Source: [10] Snyder, C., Berton, J., Brown, G. et all
-       'Propulsion Investigation for Zero and Near-Zero Emissions Aircraft,' NASA STI Program,
-       NASA Glenn,  2009.012
-       
-   Inputs:
-       max_power- maximum power the motor can deliver safely   [Watts]
-   
-   Outputs:
-       weight- weight of the motor                             [kilograms]
-   
-Properties Used:
-       N/A
-
-
-
- -

◆ integrated_propulsion()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Weights.Correlations.Propulsion.integrated_propulsion.integrated_propulsion ( engine_jet,
 num_eng,
 engine_wt_factor = 1.6 
)
-
- -

integrated_propulsion.py

-

Created: Jan 2014, M. A. Wendorff Modified: Feb 2014, A. Wendorff Feb 2016, E. Botero

Calculate the weight of the entire propulsion system 
-
-Assumptions:
-        The propulsion system is a fixed 60% greater than the dry engine alone. 
-        The propulsion system includes the engines, engine exhaust, reverser, starting,
-        controls, lubricating, and fuel systems. The nacelle and pylon weight are also
-        part of this calculation.           
-        
-Source: 
-        N/A
-        
-Inputs:
-        engine_jet - dry weight of the engine                                             [kilograms]
-        num_eng - total number of engines on the aircraft                                 [dimensionless]
-        engine_wt_factor - weight increase factor for entire integrated propulsion system [dimensionless]
-
-Outputs:
-        weight - weight of the full propulsion system                                     [kilograms]
-    
-Properties Used:
-        N/A
-
-
-
-
-
- - - - diff --git a/_site/doxygen/group__Methods-Weights-Correlations-Propulsion.js b/_site/doxygen/group__Methods-Weights-Correlations-Propulsion.js deleted file mode 100644 index 69ad1cb5..00000000 --- a/_site/doxygen/group__Methods-Weights-Correlations-Propulsion.js +++ /dev/null @@ -1,7 +0,0 @@ -var group__Methods_Weights_Correlations_Propulsion = -[ - [ "air_cooled_motor", "group__Methods-Weights-Correlations-Propulsion.html#gacfd59c496391c06249de12a45252f28e", null ], - [ "engine_jet", "group__Methods-Weights-Correlations-Propulsion.html#ga5292d6ea3b25c2acecd08c2b033f69eb", null ], - [ "hts_motor", "group__Methods-Weights-Correlations-Propulsion.html#ga4910a296a5c344da2cae7b81c05895c1", null ], - [ "integrated_propulsion", "group__Methods-Weights-Correlations-Propulsion.html#gaa6dd0b5a3adb2b4948101434f55a197a", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Methods-Weights-Correlations-Tube__Wing.html b/_site/doxygen/group__Methods-Weights-Correlations-Tube__Wing.html deleted file mode 100644 index 3bf03c61..00000000 --- a/_site/doxygen/group__Methods-Weights-Correlations-Tube__Wing.html +++ /dev/null @@ -1,599 +0,0 @@ - - - - - - - -SUAVE: Tube_Wing - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
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-
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Provides structural weight correlations for a tube and wing aircraft. -More...

- - - - - - - - - - - - -

-Functions

def SUAVE.Methods.Weights.Correlations.Tube_Wing.empty.empty (vehicle)
 
def SUAVE.Methods.Weights.Correlations.Tube_Wing.systems.systems (num_seats, ctrl_type, S_h, S_v, S_gross_w, ac_type)
 
def SUAVE.Methods.Weights.Correlations.Tube_Wing.tail_horizontal.tail_horizontal (b_h, sweep_h, Nult, S_h, TOW, mac_w, mac_h, l_w2h, t_c_h, exposed)
 
def SUAVE.Methods.Weights.Correlations.Tube_Wing.tail_vertical.tail_vertical (S_v, Nult, b_v, TOW, t_c_v, sweep_v, S_gross_w, t_tail, rudder_fraction=0.25)
 
def SUAVE.Methods.Weights.Correlations.Tube_Wing.tube.tube (S_fus, diff_p_fus, w_fus, h_fus, l_fus, Nlim, wt_zf, wt_wing, wt_propulsion, wing_c_r)
 
-

Detailed Description

-

Provides structural weight correlations for a tube and wing aircraft.

-

Function Documentation

- -

◆ empty()

- -
-
- - - - - - - - -
def SUAVE.Methods.Weights.Correlations.Tube_Wing.empty.empty ( vehicle)
-
-
This is for a standard Tube and Wing aircraft configuration.        
-
-Assumptions:
-    calculated aircraft weight from correlations created per component of historical aircraft
-
-Source:
-    N/A
-    
-Inputs:
-  engine - a data dictionary with the fields:                    
-      thrust_sls - sea level static thrust of a single engine                [Newtons]
-
-  wing - a data dictionary with the fields:
-      gross_area - wing gross area                                           [meters**2]
-      span - span of the wing                                                [meters]
-      taper - taper ratio of the wing                                        [dimensionless]
-      t_c - thickness-to-chord ratio of the wing                             [dimensionless]
-      sweep - sweep angle of the wing                                        [radians]
-      mac - mean aerodynamic chord of the wing                               [meters]
-      r_c - wing root chord                                                  [meters]
-
-  aircraft - a data dictionary with the fields:                    
-      Nult - ultimate load of the aircraft                                   [dimensionless]
-      Nlim - limit load factor at zero fuel weight of the aircraft           [dimensionless]
-      TOW - maximum takeoff weight of the aircraft                           [kilograms]
-      zfw - maximum zero fuel weight of the aircraft                         [kilograms]
-      num_eng - number of engines on the aircraft                            [dimensionless]
-      num_pax - number of passengers on the aircraft                         [dimensionless]
-      wt_cargo - weight of the bulk cargo being carried on the aircraft      [kilograms]
-      num_seats - number of seats installed on the aircraft                  [dimensionless]
-      ctrl - specifies if the control system is "fully powered", "partially powered", or not powered [dimensionless]
-      ac - determines type of instruments, electronics, and operating items based on types: 
-          "short-range", "medium-range", "long-range", "business", "cargo", "commuter", "sst"        [dimensionless]
-      w2h - tail length (distance from the airplane c.g. to the horizontal tail aerodynamic center)  [meters]
-
-  fuselage - a data dictionary with the fields:
-      area - fuselage wetted area                                            [meters**2]
-      diff_p - Maximum fuselage pressure differential                        [Pascal]
-      width - width of the fuselage                                          [meters]
-      height - height of the fuselage                                        [meters]
-      length - length of the fuselage                                        [meters]                     
-
-  horizontal
-      area - area of the horizontal tail                                     [meters**2]
-      span - span of the horizontal tail                                     [meters]
-      sweep - sweep of the horizontal tail                                   [radians]
-      mac - mean aerodynamic chord of the horizontal tail                    [meters]
-      t_c - thickness-to-chord ratio of the horizontal tail                  [dimensionless]
-      exposed - exposed area ratio for the horizontal tail                   [dimensionless]
-
-  vertical
-      area - area of the vertical tail                                       [meters**2]
-      span - sweight = weight * Units.lbpan of the vertical                  [meters]
-      t_c - thickness-to-chord ratio of the vertical tail                    [dimensionless]
-      sweep - sweep angle of the vertical tail                               [radians]
-      t_tail - factor to determine if aircraft has a t-tail, "yes"           [dimensionless]
-
-Outputs:
-    output - a data dictionary with fields:
-        wt_payload - weight of the passengers plus baggage and paid cargo    [kilograms]
-        wt_pax - weight of all the passengers                                [kilogram]
-        wt_bag - weight of all the baggage                                   [kilogram]
-        wt_fuel - weight of the fuel carried                                 [kilogram]
-        wt_empty - operating empty weight of the aircraft                    [kilograms]
- 
-Properties Used:
-    N/A
-
-
-
- -

◆ systems()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Weights.Correlations.Tube_Wing.systems.systems ( num_seats,
 ctrl_type,
 S_h,
 S_v,
 S_gross_w,
 ac_type 
)
-
-
Calculate the weight of the different engine systems on the aircraft
-
-Assumptions:
-    numbers based on FAA regulations and correlations from previous aircraft 
-
-Source: 
-    N/A
-            
-   Inputs:
-   num_seats - total number of seats on the aircraft                                                   [dimensionless]
-   ctrl_type - specifies if the control system is fully power, partially powered, or not powered       [dimensionless]
-   S_h - area of the horizontal tail                                                                   [meters**2]
-   S_v - area of the vertical tail                                                                     [meters**2]
-   S_gross_w - area of the wing                                                                        [meters**2]
-   ac_type - determines type of instruments, electronics, and operating items based on type of vehicle [dimensionless]
-   
-   Outputs:
-   output - a data dictionary with fields:
-       wt_flt_ctrl - weight of the flight control system                                               [kilograms]
-       wt_apu - weight of the apu                                                                      [kilograms]
-       wt_hyd_pnu - weight of the hydraulics and pneumatics                                            [kilograms]
-       wt_instruments - weight of the instruments and navigational equipment                           [kilograms]
-       wt_avionics - weight of the avionics                                                            [kilograms]
-       wt_opitems - weight of the optional items based on the type of aircraft                         [kilograms]
-       wt_elec - weight of the electrical items                                                        [kilograms]
-       wt_ac - weight of the air conditioning and anti-ice system                                      [kilograms]
-       wt_furnish - weight of the furnishings in the fuselage                                          [kilograms]
-   
-Properties Used:
-    N/A
-
-
-
- -

◆ tail_horizontal()

- -
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def SUAVE.Methods.Weights.Correlations.Tube_Wing.tail_horizontal.tail_horizontal ( b_h,
 sweep_h,
 Nult,
 S_h,
 TOW,
 mac_w,
 mac_h,
 l_w2h,
 t_c_h,
 exposed 
)
-
-
Calculate the weight of the horizontal tail in a standard configuration
-
-Assumptions:
-    calculated weight of the horizontal tail including the elevator
-    Assume that the elevator is 25% of the horizontal tail 
-
-Source: 
-    N/A
-    
-Inputs:
-    b_h - span of the horizontal tail                                                               [meters]
-    sweep_h - sweep of the horizontal tail                                                          [radians]
-    Nult - ultimate design load of the aircraft                                                     [dimensionless]
-    S_h - area of the horizontal tail                                                               [meters**2]
-    TOW - maximum takeoff weight of the aircraft                                                    [kilograms]
-    mac_w - mean aerodynamic chord of the wing                                                      [meters]
-    mac_h - mean aerodynamic chord of the horizontal tail                                           [meters]
-    l_w2h - tail length (distance from the airplane c.g. to the horizontal tail aerodynamic center) [meters]
-    t_c_h - thickness-to-chord ratio of the horizontal tail                                         [dimensionless]
-    exposed - exposed area ratio for the horizontal tail                                            [dimensionless]
-
-Outputs:
-    weight - weight of the horizontal tail                                                          [kilograms]
-   
-Properties Used:
-    N/A
-
-
-
- -

◆ tail_vertical()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Weights.Correlations.Tube_Wing.tail_vertical.tail_vertical ( S_v,
 Nult,
 b_v,
 TOW,
 t_c_v,
 sweep_v,
 S_gross_w,
 t_tail,
 rudder_fraction = 0.25 
)
-
-
Calculate the weight of the vertical fin of an aircraft without the weight of 
-the rudder and then calculate the weight of the rudder 
-
-Assumptions:
-    Vertical tail weight is the weight of the vertical fin without the rudder weight.
-    Rudder occupies 25% of the S_v and weighs 60% more per unit area.     
-    
-Source: 
-    N/A 
-    
-Inputs:
-    S_v - area of the vertical tail (combined fin and rudder)                      [meters**2]
-    Nult - ultimate load of the aircraft                                           [dimensionless]
-    b_v - span of the vertical                                                     [meters]
-    TOW - maximum takeoff weight of the aircraft                                   [kilograms]
-    t_c_v - thickness-to-chord ratio of the vertical tail                          [dimensionless]
-    sweep_v - sweep angle of the vertical tail                                     [radians]
-    S_gross_w - wing gross area                                                    [meters**2]
-    t_tail - factor to determine if aircraft has a t-tail                          [dimensionless]
-    rudder_fraction - fraction of the vertical tail that is the rudder             [dimensionless]
-
-Outputs:
-    output - a dictionary with outputs:
-        wt_tail_vertical - weight of the vertical fin portion of the vertical tail [kilograms]
-        wt_rudder - weight of the rudder on the aircraft                           [kilograms]
-  
-Properties Used:
-    N/A
-
-
-
- -

◆ tube()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Weights.Correlations.Tube_Wing.tube.tube ( S_fus,
 diff_p_fus,
 w_fus,
 h_fus,
 l_fus,
 Nlim,
 wt_zf,
 wt_wing,
 wt_propulsion,
 wing_c_r 
)
-
-
Calculate the weight of a fuselage in the state tube and wing configuration
-
-Assumptions:
-    fuselage in a standard wing and tube configuration         
-
-Source: 
-    N/A 
-    
-Inputs:
-    S_fus - fuselage wetted area                                           [meters**2]
-    diff_p_fus - Maximum fuselage pressure differential                    [Pascal]
-    w_fus - width of the fuselage                                          [meters]
-    h_fus - height of the fuselage                                         [meters]
-    l_fus - length of the fuselage                                         [meters]
-    Nlim - limit load factor at zero fuel weight of the aircraft           [dimensionless]
-    wt_zf - zero fuel weight of the aircraft                               [kilograms]
-    wt_wing - weight of the wing of the aircraft                           [kilograms]
-    wt_propulsion - weight of the entire propulsion system of the aircraft [kilograms]
-    wing_c_r - wing root chord                                             [meters]
-    
-Outputs:
-    weight - weight of the fuselage                                        [kilograms]
-        
-Properties Used:
-    N/A
-
-
-
-
-
- - - - diff --git a/_site/doxygen/group__Methods-Weights-Correlations-Tube__Wing.js b/_site/doxygen/group__Methods-Weights-Correlations-Tube__Wing.js deleted file mode 100644 index 4f17b1db..00000000 --- a/_site/doxygen/group__Methods-Weights-Correlations-Tube__Wing.js +++ /dev/null @@ -1,8 +0,0 @@ -var group__Methods_Weights_Correlations_Tube__Wing = -[ - [ "empty", "group__Methods-Weights-Correlations-Tube__Wing.html#ga88d820445757e8a0b404bd4a927987af", null ], - [ "systems", "group__Methods-Weights-Correlations-Tube__Wing.html#ga30ab082cdcf65e2353337185bf791f18", null ], - [ "tail_horizontal", "group__Methods-Weights-Correlations-Tube__Wing.html#ga01911fdc8a489264f6085fc867f64a85", null ], - [ "tail_vertical", "group__Methods-Weights-Correlations-Tube__Wing.html#ga76320919117c9debed0edc4395fe7e9b", null ], - [ "tube", "group__Methods-Weights-Correlations-Tube__Wing.html#gafd8256895c20e1a5343c362d922aa8c1", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Methods-Weights-Correlations-UAV.html b/_site/doxygen/group__Methods-Weights-Correlations-UAV.html deleted file mode 100644 index 56aa2e7a..00000000 --- a/_site/doxygen/group__Methods-Weights-Correlations-UAV.html +++ /dev/null @@ -1,160 +0,0 @@ - - - - - - - -SUAVE: UAV - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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Provides structural weight correlations for UAVs. -More...

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-Functions

def SUAVE.Methods.Weights.Correlations.UAV.empty.empty (vehicle)
 
-

Detailed Description

-

Provides structural weight correlations for UAVs.

-

Function Documentation

- -

◆ empty()

- -
-
- - - - - - - - -
def SUAVE.Methods.Weights.Correlations.UAV.empty.empty ( vehicle)
-
-
This comoutes the weigt of a UAV   
-
-Assumptions:
-    Assumes a 'main wing' is attached
-
-Source:
-    Structural Weight correlation from all 415 samples of fixed-wing UAVs and sailplanes
-    Equation 3.16 from 'Design of Solar Powered Airplanes for Continuous Flight' by Andre Noth
-    Relatively valid for a wide variety of vehicles, may be optimistic 
-
-Inputs:
-    S                [meters**2]
-    AR               [dimensionless]
-    
-Outputs:
-    weight           [kilograms]
-
-Properties Used:
-    N/A
-
-
-
-
-
- - - - diff --git a/_site/doxygen/group__Methods-Weights-Correlations-UAV.js b/_site/doxygen/group__Methods-Weights-Correlations-UAV.js deleted file mode 100644 index 3cd6894a..00000000 --- a/_site/doxygen/group__Methods-Weights-Correlations-UAV.js +++ /dev/null @@ -1,4 +0,0 @@ -var group__Methods_Weights_Correlations_UAV = -[ - [ "empty", "group__Methods-Weights-Correlations-UAV.html#gacdd594163b3b6ae3e879aa060413000e", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Methods-Weights-Correlations.html b/_site/doxygen/group__Methods-Weights-Correlations.html deleted file mode 100644 index 877fcbb1..00000000 --- a/_site/doxygen/group__Methods-Weights-Correlations.html +++ /dev/null @@ -1,138 +0,0 @@ - - - - - - - -SUAVE: Correlations - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
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- -
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- -
-
Correlations
-
-
- -

Correlation methods provide component weight breakdowns for different vehicle configurations based on regressed data. -More...

- - - - - - - - - - - - - - - - - - - - -

-Modules

 BWB
 Provides structural weight correlations for a BWB concept.
 
 Common
 Provides structural weight correlations for aircraft components applicable to all aircraft configurations.
 
 Human_Powered
 Provides structural weight correlations for a human-powered aircraft; applicable to solar-UAVs.
 
 Propulsion
 Contains some methods for calculating different propulsion system weights.
 
 Tube_Wing
 Provides structural weight correlations for a tube and wing aircraft.
 
 UAV
 Provides structural weight correlations for UAVs.
 
-

Detailed Description

-

Correlation methods provide component weight breakdowns for different vehicle configurations based on regressed data.

-
-
- - - - diff --git a/_site/doxygen/group__Methods-Weights-Correlations.js b/_site/doxygen/group__Methods-Weights-Correlations.js deleted file mode 100644 index 8a260723..00000000 --- a/_site/doxygen/group__Methods-Weights-Correlations.js +++ /dev/null @@ -1,9 +0,0 @@ -var group__Methods_Weights_Correlations = -[ - [ "BWB", "group__Methods-Weights-Correlations-BWB.html", "group__Methods-Weights-Correlations-BWB" ], - [ "Common", "group__Methods-Weights-Correlations-Common.html", "group__Methods-Weights-Correlations-Common" ], - [ "Human_Powered", "group__Methods-Weights-Correlations-Human__Powered.html", "group__Methods-Weights-Correlations-Human__Powered" ], - [ "Propulsion", "group__Methods-Weights-Correlations-Propulsion.html", "group__Methods-Weights-Correlations-Propulsion" ], - [ "Tube_Wing", "group__Methods-Weights-Correlations-Tube__Wing.html", "group__Methods-Weights-Correlations-Tube__Wing" ], - [ "UAV", "group__Methods-Weights-Correlations-UAV.html", "group__Methods-Weights-Correlations-UAV" ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Methods-Weights.html b/_site/doxygen/group__Methods-Weights.html deleted file mode 100644 index dac04104..00000000 --- a/_site/doxygen/group__Methods-Weights.html +++ /dev/null @@ -1,123 +0,0 @@ - - - - - - - -SUAVE: Weights - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
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- -
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Weights
-
-
- -

Weights methods provide different means of estimating vehicle weight breakdowns. -More...

- - - - - -

-Modules

 Correlations
 Correlation methods provide component weight breakdowns for different vehicle configurations based on regressed data.
 
-

Detailed Description

-

Weights methods provide different means of estimating vehicle weight breakdowns.

-
-
- - - - diff --git a/_site/doxygen/group__Methods-Weights.js b/_site/doxygen/group__Methods-Weights.js deleted file mode 100644 index 37ef2471..00000000 --- a/_site/doxygen/group__Methods-Weights.js +++ /dev/null @@ -1,4 +0,0 @@ -var group__Methods_Weights = -[ - [ "Correlations", "group__Methods-Weights-Correlations.html", "group__Methods-Weights-Correlations" ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Methods.html b/_site/doxygen/group__Methods.html deleted file mode 100644 index 322b228e..00000000 --- a/_site/doxygen/group__Methods.html +++ /dev/null @@ -1,209 +0,0 @@ - - - - - - - -SUAVE: Methods - - - - - - - - - - - - - - - -
-
- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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Methods
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Methods provide the functions needed to perform analyses. -More...

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-Modules

 Aerodynamics
 Aerodynamic methods contain the functions for the aerodynamic analyses.
 
 Center_of_Gravity
 Description.
 
 Costs
 This contains functions that can compute costs associated with building and operating an aircraft.
 
 Flight_Dynamics
 Description.
 
 Geometry
 These methods are primarily used for sizing.
 
 Missions
 Mission methods contain the functions for setting up and solving a mission.
 
 Noise
 Description.
 
 Performance
 This is a set of basic aircraft performance estimation functions.
 
 Power
 Power methods contain the functions for electric systems such as batteries and fuel cells.
 
 Propulsion
 Description.
 
 Utilities
 These provide functionality that is not easily grouped into another set.
 
 Weights
 Weights methods provide different means of estimating vehicle weight breakdowns.
 
- - - -

-Functions

def SUAVE.Methods.skip.skip (args, kwarg)
 
-

Detailed Description

-

Methods provide the functions needed to perform analyses.

-

These are generally not classes.

-

Function Documentation

- -

◆ skip()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.skip.skip ( args,
 kwarg 
)
-
-
This method can be used to replace default functions when
-no action is desired instead.
-
-Assumptions:
-N/A
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
-
-
-
- - - - diff --git a/_site/doxygen/group__Methods.js b/_site/doxygen/group__Methods.js deleted file mode 100644 index 9dbde42f..00000000 --- a/_site/doxygen/group__Methods.js +++ /dev/null @@ -1,16 +0,0 @@ -var group__Methods = -[ - [ "Aerodynamics", "group__Methods-Aerodynamics.html", "group__Methods-Aerodynamics" ], - [ "Center_of_Gravity", "group__Methods-Center__of__Gravity.html", "group__Methods-Center__of__Gravity" ], - [ "Costs", "group__Methods-Costs.html", "group__Methods-Costs" ], - [ "Flight_Dynamics", "group__Methods-Flight__Dynamics.html", "group__Methods-Flight__Dynamics" ], - [ "Geometry", "group__Methods-Geometry.html", "group__Methods-Geometry" ], - [ "Missions", "group__Methods-Missions.html", "group__Methods-Missions" ], - [ "Noise", "group__Methods-Noise.html", "group__Methods-Noise" ], - [ "Performance", "group__Methods-Performance.html", "group__Methods-Performance" ], - [ "Power", "group__Methods-Power.html", "group__Methods-Power" ], - [ "Propulsion", "group__Methods-Propulsion.html", "group__Methods-Propulsion" ], - [ "Utilities", "group__Methods-Utilities.html", "group__Methods-Utilities" ], - [ "Weights", "group__Methods-Weights.html", "group__Methods-Weights" ], - [ "skip", "group__Methods.html#gaf0740dc1eaaae86e6127b7eebc718d8f", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Optimization-Package__Setups-TRMM.html b/_site/doxygen/group__Optimization-Package__Setups-TRMM.html deleted file mode 100644 index c70d33e7..00000000 --- a/_site/doxygen/group__Optimization-Package__Setups-TRMM.html +++ /dev/null @@ -1,189 +0,0 @@ - - - - - - - -SUAVE: TRMM - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
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-
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-
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-
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- -
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- -

Trust Region Model Management Scripts live here. -More...

- - - - - - -

-Classes

class  SUAVE.Optimization.Package_Setups.TRMM.Trust_Region.Trust_Region
 
class  SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization
 
- - - -

-Functions

def SUAVE.Optimization.Package_Setups.TRMM.TRMM_setup.TRMM_Solve (problem, tr=None, tr_opt=None, print_output=False)
 
-

Detailed Description

-

Trust Region Model Management Scripts live here.

-

Function Documentation

- -

◆ TRMM_Solve()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Optimization.Package_Setups.TRMM.TRMM_setup.TRMM_Solve ( problem,
 tr = None,
 tr_opt = None,
 print_output = False 
)
-
-
This solves your TRMM
-
-    Assumptions:
-    None
-
-    Source:
-    N/A
-
-    Inputs:
-    problem       [nexus()]
-    tr            [Trust_Region()]
-    tr_opt        [Trust_Region_Optimization()]
-    print_output  [bool]
-
-    Outputs:
-    None
-
-    Properties Used:
-    None
-
-
-
-
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- - - - - - -SUAVE: Package_Setups - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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Package_Setups
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Individual package setups that help you interface with other codes. -More...

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-Modules

 TRMM
 Trust Region Model Management Scripts live here.
 
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-Functions

def SUAVE.Optimization.Package_Setups.additive_setup.Additive_Solve (problem, num_fidelity_levels=2, num_samples=10, max_iterations=10, tolerance=1e-6, opt_type='basic', num_starts=3, print_output=True)
 
def SUAVE.Optimization.Package_Setups.additive_setup.evaluate_model (problem, x, cons)
 
def SUAVE.Optimization.Package_Setups.additive_setup.evaluate_corrected_model (x, problem=None, obj_surrogate=None, cons_surrogate=None)
 
def SUAVE.Optimization.Package_Setups.additive_setup.evaluate_expected_improvement (x, problem=None, obj_surrogate=None, cons_surrogate=None, fstar=np.inf, cons=None)
 
def SUAVE.Optimization.Package_Setups.additive_setup.expected_improvement_carpet (lbs, ubs, problem, obj_surrogate, cons_surrogate, fstar, show_log_improvement=False)
 
def SUAVE.Optimization.Package_Setups.additive_setup.scale_vals (inp, con, ini, bnd, scl)
 
def SUAVE.Optimization.Package_Setups.additive_setup.initialize_opt_vals (opt_prob, obj, inp, x_low_bound, x_up_bound, con_low_edge, con_up_edge, nam, con, x_eval)
 
def SUAVE.Optimization.Package_Setups.additive_setup.run_objective_optimization (opt_prob, problem, f_additive_surrogate, g_additive_surrogate)
 
def SUAVE.Optimization.Package_Setups.ipopt_setup.Ipopt_Solve (problem)
 
def SUAVE.Optimization.Package_Setups.ipopt_setup.eval_grad_f (x, problem)
 
def SUAVE.Optimization.Package_Setups.ipopt_setup.eval_jac_g (x, flag, problem)
 
def SUAVE.Optimization.Package_Setups.ipopt_setup.eval_f (x, problem)
 
def SUAVE.Optimization.Package_Setups.ipopt_setup.eval_g (x, problem)
 
def SUAVE.Optimization.Package_Setups.ipopt_setup.make_structure (problem)
 
def SUAVE.Optimization.Package_Setups.pyopt_setup.Pyopt_Solve (problem, solver='SNOPT', FD='single', sense_step=1.0E-6, nonderivative_line_search=False)
 
def SUAVE.Optimization.Package_Setups.pyopt_setup.PyOpt_Problem (problem, x)
 
def SUAVE.Optimization.Package_Setups.pyopt_surrogate_setup.pyopt_surrogate_setup (surrogate_function, inputs, constraints)
 
def SUAVE.Optimization.Package_Setups.scipy_setup.SciPy_Solve (problem, solver='SLSQP', sense_step=1.4901161193847656e-08)
 
def SUAVE.Optimization.Package_Setups.scipy_setup.SciPy_Problem (problem, x)
 
-

Detailed Description

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Individual package setups that help you interface with other codes.

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Function Documentation

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◆ Additive_Solve()

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def SUAVE.Optimization.Package_Setups.additive_setup.Additive_Solve ( problem,
 num_fidelity_levels = 2,
 num_samples = 10,
 max_iterations = 10,
 tolerance = 1e-6,
 opt_type = 'basic',
 num_starts = 3,
 print_output = True 
)
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-
Solves a multifidelity problem using an additive corrections
-
-Assumptions:
-N/A
-
-Source:
-N/A
-
-Inputs:
-problem             [nexus()]
-num_fidelity_levels [int]
-num_samples         [int]
-max_iterations      [int]
-tolerance           [float]
-opt_type            [str]
-num_starts          [int]
-print_output        [bool]
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-Outputs:
-(fOpt,xOpt)  [tuple]
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-Properties Used:
-N/A
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◆ eval_f()

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def SUAVE.Optimization.Package_Setups.ipopt_setup.eval_f ( x,
 problem 
)
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Find the objective
-
-    Assumptions:
-    You can actually install ipopt on your machine
-
-    Source:
-    N/A
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-    Inputs:
-    x          [array]
-    problem    [nexus()]
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-    Outputs:
-    obj        [float]
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-    Properties Used:
-    None
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◆ eval_g()

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def SUAVE.Optimization.Package_Setups.ipopt_setup.eval_g ( x,
 problem 
)
-
-
Find the constraints
-
-    Assumptions:
-    You can actually install ipopt on your machine
-
-    Source:
-    N/A
-
-    Inputs:
-    x          [array]
-    problem    [nexus()]
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-    Outputs:
-    con        [array]
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-    Properties Used:
-    None
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◆ eval_grad_f()

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def SUAVE.Optimization.Package_Setups.ipopt_setup.eval_grad_f ( x,
 problem 
)
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Calculate the gradient of the objective function
-
-    Assumptions:
-    You can actually install ipopt on your machine
-
-    Source:
-    N/A
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-    Inputs:
-    x          [array]
-    problem    [nexus()]
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-    Outputs:
-    grad     [array]
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-    Properties Used:
-    None
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◆ eval_jac_g()

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def SUAVE.Optimization.Package_Setups.ipopt_setup.eval_jac_g ( x,
 flag,
 problem 
)
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Calculate the jacobian of the constraint function
-    If flag is used a structure shape is provided to allow ipopt to size the constraints
-
-    Assumptions:
-    You can actually install ipopt on your machine
-
-    Source:
-    N/A
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-    Inputs:
-    x          [array]
-    flag       [bool]
-    problem    [nexus()]
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-    Outputs:
-    jac_g      [array]
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-    Properties Used:
-    None
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◆ evaluate_corrected_model()

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def SUAVE.Optimization.Package_Setups.additive_setup.evaluate_corrected_model ( x,
 problem = None,
 obj_surrogate = None,
 cons_surrogate = None 
)
-
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Evaluates the corrected model with the low fidelity plus the corrections
-
-Assumptions:
-N/A
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-Source:
-N/A
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-Inputs:
-x              [array]
-problem        [nexus()]
-obj_surrogate  [fun()]
-cons_surrogate [fun()]
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-Outputs:
-obj            [float]
-const          [array]
-fail           [bool]
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-Properties Used:
-N/A    
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◆ evaluate_expected_improvement()

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def SUAVE.Optimization.Package_Setups.additive_setup.evaluate_expected_improvement ( x,
 problem = None,
 obj_surrogate = None,
 cons_surrogate = None,
 fstar = np.inf,
 cons = None 
)
-
-
Evaluates the expected improvement of the point x
-
-Assumptions:
-N/A
-
-Source:
-N/A
-
-Inputs:
-x              [array]
-problem        [nexus()]
-obj_surrogate  [fun()]
-cons_surrogate [fun()]
-fstar          [float]
-cons           [vector]
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-Outputs:
--EI            [float]
-const          [array]
-fail           [bool]
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-Properties Used:
-N/A    
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◆ evaluate_model()

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def SUAVE.Optimization.Package_Setups.additive_setup.evaluate_model ( problem,
 x,
 cons 
)
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Solves the optimization problem to get the objective and constraints
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-Assumptions:
-N/A
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-Source:
-N/A
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-Inputs:
-problem   [nexus()]
-x         [array]
-cons      [array]
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-Outputs:
-f         [float]
-g         [array]
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-Properties Used:
-N/A    
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◆ expected_improvement_carpet()

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def SUAVE.Optimization.Package_Setups.additive_setup.expected_improvement_carpet ( lbs,
 ubs,
 problem,
 obj_surrogate,
 cons_surrogate,
 fstar,
 show_log_improvement = False 
)
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-
Makes a carpet plot of the expected improvement
-
-Assumptions:
-N/A
-
-Source:
-N/A
-
-Inputs:
-lbs                  [array]
-lbs                  [array]
-problem              [nexus()]
-obj_surrogate        [fun()]
-cons_surrogate       [fun()]
-fstar                [float]
-show_log_improvement [bool]
-
-Outputs:
-Alluring plots that you could only dream of
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-Properties Used:
-N/A    
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◆ initialize_opt_vals()

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def SUAVE.Optimization.Package_Setups.additive_setup.initialize_opt_vals ( opt_prob,
 obj,
 inp,
 x_low_bound,
 x_up_bound,
 con_low_edge,
 con_up_edge,
 nam,
 con,
 x_eval 
)
-
-
Sets up the optimization values 
-
-Assumptions:
-N/A
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-Source:
-N/A
-
-Inputs:
-opt_prob         [pyopt_problem()]
-obj              [float]
-inp              [array]
-x_low_bound      [array]
-x_up_bound       [array]
-con_low_edge     [array]
-con_up_edge      [array]
-nam              [list of str]
-con              [array]
-x_eval           [array]
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-Outputs:
-N/A
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-Properties Used:
-N/A    
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◆ Ipopt_Solve()

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def SUAVE.Optimization.Package_Setups.ipopt_setup.Ipopt_Solve ( problem)
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Solves a Nexus optimization problem using ipopt
-
-    Assumptions:
-    You can actually install ipopt on your machine
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-    Source:
-    N/A
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-    Inputs:
-    problem    [nexus()]
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-    Outputs:
-    result     [array]
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-    Properties Used:
-    None
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◆ make_structure()

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def SUAVE.Optimization.Package_Setups.ipopt_setup.make_structure ( problem)
-
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Create an array structure to let ipopt know the size of the problem
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-    Assumptions:
-    You can actually install ipopt on your machine
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-    Source:
-    N/A
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-    Inputs:
-    problem    [nexus()]
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-    Outputs:
-    array      [array]
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-    Properties Used:
-    None
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◆ PyOpt_Problem()

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def SUAVE.Optimization.Package_Setups.pyopt_setup.PyOpt_Problem ( problem,
 x 
)
-
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This wrapper runs the SUAVE problem and is called by the PyOpt solver.
-    Prints the inputs (x) as well as the objective values and constraints.
-    If any values produce NaN then a fail flag is thrown.
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-    Assumptions:
-    None
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-    Source:
-    N/A
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-    Inputs:
-    problem   [nexus()]
-    x         [array]
-
-    Outputs:
-    obj       [float]
-    cons      [array]
-    fail      [bool]
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-    Properties Used:
-    None
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◆ Pyopt_Solve()

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def SUAVE.Optimization.Package_Setups.pyopt_setup.Pyopt_Solve ( problem,
 solver = 'SNOPT',
 FD = 'single',
 sense_step = 1.0E-6,
 nonderivative_line_search = False 
)
-
-
This converts your SUAVE Nexus problem into a PyOpt optimization problem and solves it
-    PyOpt has many algorithms, they can be switched out by using the solver input. 
-
-    Assumptions:
-    None
-
-    Source:
-    N/A
-
-    Inputs:
-    problem                   [nexus()]
-    solver                    [str]
-    FD (parallel or single)   [str]
-    sense_step                [float]
-    nonderivative_line_search [bool]
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-    Outputs:
-    outputs                   [list]
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-    Properties Used:
-    None
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◆ pyopt_surrogate_setup()

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def SUAVE.Optimization.Package_Setups.pyopt_surrogate_setup.pyopt_surrogate_setup ( surrogate_function,
 inputs,
 constraints 
)
-
-
sets up a surrogate problem so it can be run by pyOpt. Makes the problem to be run
-
-    Assumptions:
-    None
-
-    Source:
-    N/A
-
-    Inputs:
-    surrogate_function [nexus()]
-    inputs             [array]
-    constraints        [array]
-
-    Outputs:
-    opt_problem        [pyOpt problem]
-
-    Properties Used:
-    None
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◆ run_objective_optimization()

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def SUAVE.Optimization.Package_Setups.additive_setup.run_objective_optimization ( opt_prob,
 problem,
 f_additive_surrogate,
 g_additive_surrogate 
)
-
-
Runs SNOPT to optimize
-
-Assumptions:
-N/A
-
-Source:
-N/A
-
-Inputs:
-opt_prob             [pyopt_problem()]
-problem              [nexus()]
-f_additive_surrogate [fun()]  
-g_additive_surrogate [fun()]
-
-Outputs:
-fOpt                 [float]
-xOpt                 [array]
-
-Properties Used:
-N/A    
-
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◆ scale_vals()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Optimization.Package_Setups.additive_setup.scale_vals ( inp,
 con,
 ini,
 bnd,
 scl 
)
-
-
Scales values to help setup the problem
-
-Assumptions:
-N/A
-
-Source:
-N/A
-
-Inputs:
-inp                         [array]
-con                         [array]
-ini                         [array]
-bnd                         [array]
-scl                         [array]
-
-Outputs:
-    tuple:
-        x                   [array]
-        scaled_constraints  [array]
-        x_low_bounds        [array]
-        x_up_bounds         [array]
-        con_up_edge         [array]
-        con_low_edge        [array]
-
-Properties Used:
-N/A    
-
-
- -

◆ SciPy_Problem()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Optimization.Package_Setups.scipy_setup.SciPy_Problem ( problem,
 x 
)
-
-
This wrapper runs the SUAVE problem and is called by the Scipy solver.
-    Prints the inputs (x) as well as the objective value
-
-    Assumptions:
-    None
-
-    Source:
-    N/A
-
-    Inputs:
-    problem   [nexus()]
-    x         [array]
-
-    Outputs:
-    obj       [float]
-
-    Properties Used:
-    None
-
-
-
- -

◆ SciPy_Solve()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Optimization.Package_Setups.scipy_setup.SciPy_Solve ( problem,
 solver = 'SLSQP',
 sense_step = 1.4901161193847656e-08 
)
-
-
This converts your SUAVE Nexus problem into a SciPy optimization problem and solves it
-    SciPy has many algorithms, they can be switched out by using the solver input. 
-
-    Assumptions:
-    1.4901161193847656e-08 is SLSQP default FD step in scipy
-
-    Source:
-    N/A
-
-    Inputs:
-    problem                   [nexus()]
-    solver                    [str]
-    sense_step                [float]
-
-    Outputs:
-    outputs                   [list]
-
-    Properties Used:
-    None
-
-
-
-
-
- - - - diff --git a/_site/doxygen/group__Optimization-Package__Setups.js b/_site/doxygen/group__Optimization-Package__Setups.js deleted file mode 100644 index eb403f78..00000000 --- a/_site/doxygen/group__Optimization-Package__Setups.js +++ /dev/null @@ -1,23 +0,0 @@ -var group__Optimization_Package__Setups = -[ - [ "TRMM", "group__Optimization-Package__Setups-TRMM.html", "group__Optimization-Package__Setups-TRMM" ], - [ "Additive_Solve", "group__Optimization-Package__Setups.html#gabb534dc553c269c0b883908092d6f2ed", null ], - [ "eval_f", "group__Optimization-Package__Setups.html#ga98973b9e47004f10152a0cf6ecec5594", null ], - [ "eval_g", "group__Optimization-Package__Setups.html#ga7199ae6dab817398c93252096797a1c4", null ], - [ "eval_grad_f", "group__Optimization-Package__Setups.html#gaec2e3de7f3b64d10edfe40b91cd6b5ab", null ], - [ "eval_jac_g", "group__Optimization-Package__Setups.html#ga2b96466343bf8317ec428d7b851f8d41", null ], - [ "evaluate_corrected_model", "group__Optimization-Package__Setups.html#ga9b73c8d202a3e4c4bad264c7137b7e02", null ], - [ "evaluate_expected_improvement", "group__Optimization-Package__Setups.html#gaa37f71305979147550b800385506b273", null ], - [ "evaluate_model", "group__Optimization-Package__Setups.html#ga391d6c55cf2297cfc0c2582db19676e6", null ], - [ "expected_improvement_carpet", "group__Optimization-Package__Setups.html#ga595a0239c702615e76556141cbdc235a", null ], - [ "initialize_opt_vals", "group__Optimization-Package__Setups.html#ga55bbd6058098de65ac5e59c10c7f90bb", null ], - [ "Ipopt_Solve", "group__Optimization-Package__Setups.html#ga9b30cb43a55ff698b8f6d2e6b0d01272", null ], - [ "make_structure", "group__Optimization-Package__Setups.html#gaea0f7002ef7f26f7ace5bc50bf7b869b", null ], - [ "PyOpt_Problem", "group__Optimization-Package__Setups.html#ga5c240bcf69db9bdb19e34bf3b8934518", null ], - [ "Pyopt_Solve", "group__Optimization-Package__Setups.html#ga15bf2d97e59321d406a21617f5140576", null ], - [ "pyopt_surrogate_setup", "group__Optimization-Package__Setups.html#ga9a79b2d8360c0ccdffaa4ee2a0a5c785", null ], - [ "run_objective_optimization", "group__Optimization-Package__Setups.html#ga00b222e15be6c8f9bf756a669dda63c2", null ], - [ "scale_vals", "group__Optimization-Package__Setups.html#ga3404bfd5a112bd1528b155f0886a7eb5", null ], - [ "SciPy_Problem", "group__Optimization-Package__Setups.html#gaf64bbbdea4a28ea4184ce286e99fc22d", null ], - [ "SciPy_Solve", "group__Optimization-Package__Setups.html#ga455ed3db18d3969bc8541ad9ef033897", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Optimization.html b/_site/doxygen/group__Optimization.html deleted file mode 100644 index b040cb85..00000000 --- a/_site/doxygen/group__Optimization.html +++ /dev/null @@ -1,785 +0,0 @@ - - - - - - - -SUAVE: Optimization - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
-
- - - -
-
- -
-
-
- -
- -
-
- - -
- -
- -
- -
-
Optimization
-
-
- -

The files that help you setup an optimization problem. -More...

- - - - - -

-Modules

 Package_Setups
 Individual package setups that help you interface with other codes.
 
- - - - - -

-Classes

class  SUAVE.Optimization.Nexus.Nexus
 
class  SUAVE.Optimization.Surrogate_Optimization.Surrogate_Optimization
 
- - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Functions

def SUAVE.Optimization.carpet_plot.carpet_plot (problem, number_of_points, plot_obj=1, plot_const=0, sweep_index_0=0, sweep_index_1=1)
 
def SUAVE.Optimization.helper_functions.set_values (dictionary, input_dictionary, converted_values, aliases)
 
def SUAVE.Optimization.helper_functions.find_a_star (dictionary, string)
 
def SUAVE.Optimization.helper_functions.scale_input_values (inputs, x)
 
def SUAVE.Optimization.helper_functions.convert_values (inputs)
 
def SUAVE.Optimization.helper_functions.get_values (dictionary, outputs, aliases)
 
def SUAVE.Optimization.helper_functions.scale_obj_values (inputs, x)
 
def SUAVE.Optimization.helper_functions.scale_const_values (inputs, x)
 
def SUAVE.Optimization.helper_functions.scale_const_bnds (inputs)
 
def SUAVE.Optimization.helper_functions.unscale_const_values (inputs, x)
 
def SUAVE.Optimization.read_optimization_outputs.format_input_data (data)
 
def SUAVE.Optimization.read_optimization_outputs.read_optimization_outputs (filename, base_inputs, constraint_inputs)
 
def SUAVE.Optimization.write_optimization_outputs.write_optimization_outputs (nexus, filename)
 
-

Detailed Description

-

The files that help you setup an optimization problem.

-

Function Documentation

- -

◆ carpet_plot()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Optimization.carpet_plot.carpet_plot ( problem,
 number_of_points,
 plot_obj = 1,
 plot_const = 0,
 sweep_index_0 = 0,
 sweep_index_1 = 1 
)
-
-
Takes in an optimization problem and runs a carpet plot of the first 2 variables
-    sweep_index_0, sweep_index_1 is index of variables you want to run carpet plot (i.e. sweep_index_0=0 means you want to sweep first variable, sweep_index_0 = 4 is the 5th variable)
-
-    Assumptions:
-    N/A
-
-    Source:
-    N/A
-
-    Inputs:
-    problem            [Nexus Class]
-    number_of_points   [int]
-    plot_obj           [int]
-    plot_const         [int]
-    sweep_index_0      [int]
-    sweep_index_1      [int]
-    
-    Outputs:
-    Beautiful Beautiful Plots!
-        Outputs:
-            inputs     [array]
-            objective  [array]
-            constraint [array]
-
-    Properties Used:
-    N/A
-
-
-
- -

◆ convert_values()

- -
-
- - - - - - - - -
def SUAVE.Optimization.helper_functions.convert_values ( inputs)
-
-
Converts an inputs from an optimization into the right units
-
-Assumptions:
-Always multiply the units by 1!
-
-Source:
-N/A
-
-Inputs:
-inputs           [list]
-
-Outputs:
-converted_values [list of str]
-
-Properties Used:
-N/A
-
-
-
- -

◆ find_a_star()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Optimization.helper_functions.find_a_star ( dictionary,
 string 
)
-
-
Searches through a dictionary looking for an *
-
-Assumptions:
-There may or may not be an asterisk
-
-Source:
-N/A
-
-Inputs:
-dictionary       [Data()]
-input_dictionary [Data()]
-converted_values [Data()]
-aliases          [list of str]
-
-Outputs:
-newstrings       [list of str]
-
-Properties Used:
-N/A
-
-
-
- -

◆ format_input_data()

- -
-
- - - - - - - - -
def SUAVE.Optimization.read_optimization_outputs.format_input_data ( data)
-
-
Takes in a result from an optimization problem and 
-
-    Assumptions:
-    None
-
-    Source:
-    N/A
-
-    Inputs:
-    data
-
-    Outputs:
-    data_out
-
-    Properties Used:
-    None
-
-
-
- -

◆ get_values()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Optimization.helper_functions.get_values ( dictionary,
 outputs,
 aliases 
)
-
-
Retrieves values saved in a dictionary 
-
-Assumptions:
-N/A
-
-Source:
-N/A
-
-Inputs:
-dictionary       [Data()]
-outputs          [Data()]
-aliases          [list of str]
-
-Outputs:
-values           [float]
-
-Properties Used:
-N/A
-
-
-
- -

◆ read_optimization_outputs()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Optimization.read_optimization_outputs.read_optimization_outputs ( filename,
 base_inputs,
 constraint_inputs 
)
-
-
Reads in the outputs of an optimization problem
-
-    Assumptions:
-    None
-
-    Source:
-    N/A
-
-    Inputs:
-    filename          [str]
-    base_inputs       [data]
-    constraint_inputs [data]
-
-    Outputs:
-    iterations        [int]
-    obj_values        [list]
-    inputs            [array]
-    constraints       [array]
-    
-
-    Properties Used:
-    None
-
-
-
- -

◆ scale_const_bnds()

- -
-
- - - - - - - - -
def SUAVE.Optimization.helper_functions.scale_const_bnds ( inputs)
-
-
Rescales constraint bounds based on Nexus inputs scale
-
-Assumptions:
-N/A
-
-Source:
-N/A
-
-Inputs:
-inputs           [Data()]
-
-Outputs:
-converted_values [array]
-
-Properties Used:
-N/A
-
-
-
- -

◆ scale_const_values()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Optimization.helper_functions.scale_const_values ( inputs,
 x 
)
-
-
Rescales constraint values based on Nexus inputs scale
-
-Assumptions:
-N/A
-
-Source:
-N/A
-
-Inputs:
-inputs          [Data()]
-x               [array]
-
-Outputs:
-scaled          [array]
-
-Properties Used:
-N/A
-
-
-
- -

◆ scale_input_values()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Optimization.helper_functions.scale_input_values ( inputs,
 x 
)
-
-
Scales the values according to the a provided scale
-
-Assumptions:
-
-
-Source:
-N/A
-
-Inputs:
-x                [array]         
-inputs           [list]
-
-Outputs:
-inputs           [list]
-
-Properties Used:
-N/A
-
-
-
- -

◆ scale_obj_values()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Optimization.helper_functions.scale_obj_values ( inputs,
 x 
)
-
-
Rescales an objective based on Nexus inputs scale
-
-Assumptions:
-N/A
-
-Source:
-N/A
-
-Inputs:
-inputs          [Data()]
-x               [float]
-
-Outputs:
-scaled          [float]
-
-Properties Used:
-N/A
-
-
-
- -

◆ set_values()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Optimization.helper_functions.set_values ( dictionary,
 input_dictionary,
 converted_values,
 aliases 
)
-
-
This method regresses through a dictionary to set the required values.
-    dictionary is the base class that will be modified, input_dictionary is
-    the set of inputs to be used, converted_values are values to be set in the
-    base dictionary, and finally the aliases which are where in the dictionary
-    the names link to
-
-Assumptions:
-N/A
-
-Source:
-N/A
-
-Inputs:
-dictionary       [Data()]
-input_dictionary [Data()]
-converted_values [Data()]
-aliases          [list of str]
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
-
- -

◆ unscale_const_values()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Optimization.helper_functions.unscale_const_values ( inputs,
 x 
)
-
-
Rescales constraint bounds based on Nexus inputs scale
-
-Assumptions:
-N/A
-
-Source:
-N/A
-
-Inputs:
-inputs           [Data()]
-x                [array]
-
-Outputs:
-scaled           [array]
-
-Properties Used:
-N/A
-
-
-
- -

◆ write_optimization_outputs()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Optimization.write_optimization_outputs.write_optimization_outputs ( nexus,
 filename 
)
-
-
Writes the optimization outputs to a file
-
-Assumptions:
-N/A
-
-Source:
-N/A
-
-Inputs:
-nexus            [nexus()]
-filename         [str]
-
-Outputs:
-N/A
-
-Properties Used:
-N/A
-
-
-
-
-
- - - - diff --git a/_site/doxygen/group__Optimization.js b/_site/doxygen/group__Optimization.js deleted file mode 100644 index 40cd8832..00000000 --- a/_site/doxygen/group__Optimization.js +++ /dev/null @@ -1,52 +0,0 @@ -var group__Optimization = -[ - [ "Package_Setups", "group__Optimization-Package__Setups.html", "group__Optimization-Package__Setups" ], - [ "Nexus", "classSUAVE_1_1Optimization_1_1Nexus_1_1Nexus.html", [ - [ "__defaults__", "classSUAVE_1_1Optimization_1_1Nexus_1_1Nexus.html#aa322d3e87229966ab24c85f885ab3570", null ], - [ "all_constraints", "classSUAVE_1_1Optimization_1_1Nexus_1_1Nexus.html#a283bba67ee91bdc858cca6a317a578f5", null ], - [ "constraints_individual", "classSUAVE_1_1Optimization_1_1Nexus_1_1Nexus.html#a47f18af949a54d34571cf342d9bc07f3", null ], - [ "equality_constraint", "classSUAVE_1_1Optimization_1_1Nexus_1_1Nexus.html#ab53543f4eaa1f6c9e9fa34dc568b4192", null ], - [ "evaluate", "classSUAVE_1_1Optimization_1_1Nexus_1_1Nexus.html#a2ccf05f1c95dd06c8e3e03fc444a73fa", null ], - 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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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Plugins
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These are external packages that have been incorporated into SUAVE. -More...

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-Functions

def SUAVE.Plugins.load_plugin.load_plugin (package_name)
 
-

Detailed Description

-

These are external packages that have been incorporated into SUAVE.

-

SUAVE specific documentation is not used for these packages. Currently the only package used is pint.

-

Function Documentation

- -

◆ load_plugin()

- -
-
- - - - - - - - -
def SUAVE.Plugins.load_plugin.load_plugin ( package_name)
-
-
This function loads a package that uses absolute package imports
-by temporarily modifying the python sys.path.
-
-Assumptions:
-Packages are in the same folder as load_plugin.py
-
-Source:
-N/A
-
-Inputs:
-package_name   <string> name of the package to import
-
-Outputs:
-package        imported package
-
-Properties Used:
-N/A
-
-
-
-
-
- - - - diff --git a/_site/doxygen/group__Plugins.js b/_site/doxygen/group__Plugins.js deleted file mode 100644 index 473e6400..00000000 --- a/_site/doxygen/group__Plugins.js +++ /dev/null @@ -1,4 +0,0 @@ -var group__Plugins = -[ - [ "load_plugin", "group__Plugins.html#ga776b8deb0fef4e607d74eef012884fef", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Sizing.html b/_site/doxygen/group__Sizing.html deleted file mode 100644 index a5f0000c..00000000 --- a/_site/doxygen/group__Sizing.html +++ /dev/null @@ -1,265 +0,0 @@ - - - - - - - -SUAVE: Sizing - - - - - - - - - - - - - - - -
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- - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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Sizing
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Sizing provides methods to size a vehicle's mass, battery energy(s), and power based on its geometric properties and mission. -More...

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-Classes

class  SUAVE.Sizing.Sizing_Loop.Sizing_Loop
 
- - - - - - - -

-Functions

def SUAVE.Sizing.read_sizing_inputs.read_sizing_inputs (sizing_loop, opt_inputs)
 
def SUAVE.Sizing.read_sizing_inputs.format_input_data (data)
 
def SUAVE.Sizing.Sizing_Loop.Finite_Difference_Gradient (x, f, my_function, inputs, scaling, iter, h)
 
-

Detailed Description

-

Sizing provides methods to size a vehicle's mass, battery energy(s), and power based on its geometric properties and mission.

-

Function Documentation

- -

◆ Finite_Difference_Gradient()

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def SUAVE.Sizing.Sizing_Loop.Finite_Difference_Gradient ( x,
 f,
 my_function,
 inputs,
 scaling,
 iter,
 h 
)
-
-
Uses a first-order finite difference step to calculate the Jacobian
-
-Inputs:
-x               [array]
-f               [array]
-my_function     function that returns the residual f and sizing variable y-y_save
-inputs          ordered dict that is unpacked within my_function
-scaling         [array]
-iter            [int]
-h               [float]
-
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- -

◆ format_input_data()

- -
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- - - - - - - - -
def SUAVE.Sizing.read_sizing_inputs.format_input_data ( data)
-
-
Properly formats an input data structure so it can be read as an array
-of floats
-
-Inputs:
-data
-
-Outputs:
-data_out
-
-
- -

◆ read_sizing_inputs()

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- - - - - - - - - - - - - - - - - - -
def SUAVE.Sizing.read_sizing_inputs.read_sizing_inputs ( sizing_loop,
 opt_inputs 
)
-
-
This function reads a sizing loop outputs file and returns an array 
-of design variables, an array of sizing variables, and an output 
-flag to indicate whether the file was successfully read.
-
-Inputs:
-sizing_loop.
-    output_filename
-opt_inputs
-
-Outputs:
-data_inputs
-data_outputs
-read_success
-
-
-
-
- - - - diff --git a/_site/doxygen/group__Sizing.js b/_site/doxygen/group__Sizing.js deleted file mode 100644 index 8134bcd4..00000000 --- a/_site/doxygen/group__Sizing.js +++ /dev/null @@ -1,24 +0,0 @@ -var group__Sizing = -[ - [ "Sizing_Loop", "classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.html", [ - [ "__defaults__", "classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.html#a178ec5c05131960d4fa8d5ad6e3c3e11", null ], - [ "broyden_update", "classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.html#a52d275bd606778420dde57df5c710ced", null ], - [ "damped_newton_update", "classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.html#a5942e4cd16b9a18ed372e79d4e8dbd70", null ], - [ "evaluate", "classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.html#a153a6ac6de2d18f130320b5e871756de", null ], - [ "newton_raphson_update", "classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.html#afee06f0c84b5023393a68b8163024939", null ], - [ "successive_substitution_update", "classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.html#a4222e0b4efa8045836ef6fb1ba94a6f3", null ], - [ "default_scaling", "classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.html#addd0442dc00517c1db5c0de356e75e68", null ], - [ "default_y", "classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.html#ac3d271509f69df8f90e10e2bf709413e", null ], - [ "initial_step", "classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.html#a5afe4453cdff685473f8f94cb6f054df", null ], - [ "iteration_options", "classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.html#af4d73d77d7b7748b08cd8e5f6cedf4fd", null ], - [ "maximum_iterations", "classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.html#a880e2af1ba6856fd9ba640aaa2b78136", null ], - [ "output_filename", "classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.html#a8bd8cbf5a638d448371e44a2f59fb4bd", null ], - [ "sizing_evaluation", "classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.html#aa9f5e946792b134387052287be34a531", null ], - [ "tolerance", "classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.html#ab945e6e09e3783f41580e291da29559f", null ], - [ "update_method", "classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.html#a82aceccafa7e1f519154a06057f02fe9", null ], - [ "write_threshhold", "classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.html#afb271146361bd7c3157ded88876df9e9", null ] - ] ], - [ "Finite_Difference_Gradient", "group__Sizing.html#gacb282e3da193d9ca04443b8303bd76d2", null ], - [ "format_input_data", "group__Sizing.html#ga473313e047f6db43c1fc004366311cae", null ], - [ "read_sizing_inputs", "group__Sizing.html#ga5080520bcc9bf040df348fb54023e7fa", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Surrogate.html b/_site/doxygen/group__Surrogate.html deleted file mode 100644 index b413de75..00000000 --- a/_site/doxygen/group__Surrogate.html +++ /dev/null @@ -1,345 +0,0 @@ - - - - - - - -SUAVE: Surrogate - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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Surrogate
-
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Surrogate provides methods for different surrogate formulations of the original problem. -More...

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class  SUAVE.Surrogate.Surrogate_Problem.Surrogate_Problem
 
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-Functions

def SUAVE.Surrogate.kriging_surrogate_functions.build_kriging_models (obj_values, inputs, constraints)
 
def SUAVE.Surrogate.scikit_surrogate_functions.build_scikit_models (surrogate_optimization, obj_values, inputs, constraints)
 
def SUAVE.Surrogate.svr_surrogate_functions.build_svr_models (obj_values, inputs, constraints, kernel='rbf', C=1E5, epsilon=.01)
 
def SUAVE.Surrogate.svr_surrogate_functions.check_svr_accuracy (x, data_inputs, data_outputs, imin=-1)
 
-

Detailed Description

-

Surrogate provides methods for different surrogate formulations of the original problem.

-

Function Documentation

- -

◆ build_kriging_models()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Surrogate.kriging_surrogate_functions.build_kriging_models ( obj_values,
 inputs,
 constraints 
)
-
-
Uses the pyKriging package to build a surrogate formulation of an optimization problem
-
-Inputs:
-obj_values          [array]
-inputs              [array]
-constraints         [array]
-
-Outputs:
-obj_surrogate            callable function(inputs)
-constraints_surrogates   [array(callable function(inputs))]
-surrogate_function       callable function(inputs): returns the objective, constraints, and whether it succeeded as an int 
-
-
- -

◆ build_scikit_models()

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- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Surrogate.scikit_surrogate_functions.build_scikit_models ( surrogate_optimization,
 obj_values,
 inputs,
 constraints 
)
-
-
Uses the scikit-learn package to build a surrogate formulation of an optimization problem
-
-Inputs:
-obj_values          [array]
-inputs              [array]
-constraints         [array]
-
-Outputs:
-obj_surrogate            callable function(inputs)
-constraints_surrogates   [array(callable function(inputs))]
-surrogate_function       callable function(inputs): returns the objective, constraints, and whether it succeeded as an int 
-
-
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◆ build_svr_models()

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def SUAVE.Surrogate.svr_surrogate_functions.build_svr_models ( obj_values,
 inputs,
 constraints,
 kernel = 'rbf',
 C = 1E5,
 epsilon = .01 
)
-
-
Uses the scikit-learn package to build a surrogate formulation of an optimization problem,
-using support vector regression. Includes additional options specific to support vector regression
-
-Inputs:
-obj_values          [array]
-inputs              [array]
-constraints         [array]
-kernel              [string]
-C                   [float]
-epsilon             [float]
-
-Outputs:
-obj_surrogate            callable function(inputs)
-constraints_surrogates   [array(callable function(inputs))]
-surrogate_function       callable function(inputs): returns the objective, constraints, and whether it succeeded as an int 
-
-
- -

◆ check_svr_accuracy()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Surrogate.svr_surrogate_functions.check_svr_accuracy ( x,
 data_inputs,
 data_outputs,
 imin = -1 
)
-
-
Determines how accurate the SVR function is at a given point
-
-Inputs:
-x            [array]
-data_inputs  [array]
-data_outputs [array]
-imin         [int]
-
-Outputs:
-output       [float]
-
-
-
-
-
- - - - diff --git a/_site/doxygen/group__Surrogate.js b/_site/doxygen/group__Surrogate.js deleted file mode 100644 index 923bfd7f..00000000 --- a/_site/doxygen/group__Surrogate.js +++ /dev/null @@ -1,13 +0,0 @@ -var group__Surrogate = -[ - [ "Surrogate_Problem", "classSUAVE_1_1Surrogate_1_1Surrogate__Problem_1_1Surrogate__Problem.html", [ - [ "__defaults__", "classSUAVE_1_1Surrogate_1_1Surrogate__Problem_1_1Surrogate__Problem.html#a01369a3a73449c9e32b85f7ced1a24d6", null ], - [ "compute", "classSUAVE_1_1Surrogate_1_1Surrogate__Problem_1_1Surrogate__Problem.html#ae2f195b54e2c25ed08009ba54272ecfa", null ], - [ "constraints_surrogates", "classSUAVE_1_1Surrogate_1_1Surrogate__Problem_1_1Surrogate__Problem.html#aa9100b4649696cd28f63c3875c6c2ef3", null ], - [ "obj_surrogate", "classSUAVE_1_1Surrogate_1_1Surrogate__Problem_1_1Surrogate__Problem.html#ac78ab6ca32dd1abe9c4a105f6ca738b9", null ] - ] ], - [ "build_kriging_models", "group__Surrogate.html#ga230db69d9477e1281bed3a0b06967aa9", null ], - [ "build_scikit_models", "group__Surrogate.html#ga07eea3b8f0a33d2d9e761e77fc0bb686", null ], - [ "build_svr_models", "group__Surrogate.html#gabf255222a4df99bcf6ed14d5d998c175", null ], - [ "check_svr_accuracy", "group__Surrogate.html#gae2a8d70ae77e437e467102f7432199ed", null ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__Vehicle.html b/_site/doxygen/group__Vehicle.html deleted file mode 100644 index bdfc96dd..00000000 --- a/_site/doxygen/group__Vehicle.html +++ /dev/null @@ -1,127 +0,0 @@ - - - - - - - -SUAVE: Vehicle - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.0.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
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Vehicle
-
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- -

Vehicle.py. -More...

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-Classes

class  SUAVE.Vehicle.Vehicle
 
class  SUAVE.Vehicle.Vehicle_Mass_Properties
 
class  SUAVE.Vehicle.Costs
 
-

Detailed Description

-

Vehicle.py.

-

Created: ### 2013, SUAVE Team Modified: ### ####, M. Vegh Feb 2016, E. Botero Apr 2017, M. Clarke

-
-
- - - - diff --git a/_site/doxygen/group__Vehicle.js b/_site/doxygen/group__Vehicle.js deleted file mode 100644 index 792d0705..00000000 --- a/_site/doxygen/group__Vehicle.js +++ /dev/null @@ -1,46 +0,0 @@ -var group__Vehicle = -[ - [ "Vehicle", "classSUAVE_1_1Vehicle_1_1Vehicle.html", [ - [ "__init__", "classSUAVE_1_1Vehicle_1_1Vehicle.html#ae6908bd99e7d8f4708f4fbcf64ec821d", null ], - [ "__defaults__", "classSUAVE_1_1Vehicle_1_1Vehicle.html#ab279ed6a6b71a4a34fd5e07595b5d640", null ], - [ "append_component", "classSUAVE_1_1Vehicle_1_1Vehicle.html#a33e2631545860ec0f2d89affae0569e7", null ], - [ "find_component_root", "classSUAVE_1_1Vehicle_1_1Vehicle.html#aa5f8c6794e64be4f87f2fc5848d1c5bf", null ], - [ "costs", "classSUAVE_1_1Vehicle_1_1Vehicle.html#a5a86ec750966687ee01ecd04f18f9b61", null ], - [ "energy", "classSUAVE_1_1Vehicle_1_1Vehicle.html#a8dd71874edebf03de72c240406ef6fed", null ], - [ "envelope", "classSUAVE_1_1Vehicle_1_1Vehicle.html#af627044c07d1d292a963abafad9ad4f8", null ], - [ "fuselages", "classSUAVE_1_1Vehicle_1_1Vehicle.html#aa5a1c52d2f0be67663a3a84b5f918182", null ], - [ "mass_properties", "classSUAVE_1_1Vehicle_1_1Vehicle.html#aa8694bc77300ae2ff815e9d59f3775e3", null ], - [ "max_lift_coefficient_factor", "classSUAVE_1_1Vehicle_1_1Vehicle.html#a763d9473ea2c6f89f8da5f07a8521adc", null ], - [ "passengers", "classSUAVE_1_1Vehicle_1_1Vehicle.html#afc67cdf2695b8ecc92f5f067639c3ada", null ], - [ "propulsors", "classSUAVE_1_1Vehicle_1_1Vehicle.html#a50c78d84e282ec3b88d50d5596cdba2c", null ], - [ "reference_area", "classSUAVE_1_1Vehicle_1_1Vehicle.html#a60668c7b9710b4df0a667ec8e9c0d7dd", null ], - [ "systems", "classSUAVE_1_1Vehicle_1_1Vehicle.html#ab8b0b39ab3b930928b161151cacfdc59", null ], - [ "tag", "classSUAVE_1_1Vehicle_1_1Vehicle.html#a91d0af7fac13cf22c95a7d085ec96dbf", null ], - [ "wings", "classSUAVE_1_1Vehicle_1_1Vehicle.html#aecfdeb1df5bdcea1e38d1b9e1a5dce70", null ] - ] ], - [ "Vehicle_Mass_Properties", "classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties.html", [ - [ "__defaults__", "classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties.html#af568a38393c43082549c3e7f0bc84776", null ], - [ "cargo", "classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties.html#adbde9a453b4d3ca1e2741e2e300d6e1d", null ], - [ "center_of_gravity", "classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties.html#ad36a0a734f8ae4b41f05e283661c586f", null ], - [ "crew", "classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties.html#a39046a61d2b3ed8b384979511664d599", null ], - [ "fuel", "classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties.html#affb84ea67f2a0b653e28e89508600ecb", null ], - [ "landing", "classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties.html#a07f79f8b79143a05e0b7ca66682064cf", null ], - [ "max_cargo", "classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties.html#af57c262dd32191437d3ee529406e17e9", null ], - [ "max_fuel", "classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties.html#ad32f98f3ed16911912400e1b7e24140e", null ], - [ "max_landing", "classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties.html#affdccf217779e61ad989a198c1e6c39c", null ], - [ "max_payload", "classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties.html#a6224c6e029582499676789ef957a047a", null ], - [ "max_takeoff", "classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties.html#a655e0f48b48b4ea63a76ba45ac3e5437", null ], - [ "max_zero_fuel", "classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties.html#a30db860638dbf91625a7bb6d6a20e13e", null ], - [ "operating_empty", "classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties.html#ac40e731a21e2e1bb5184af4cdd318b94", null ], - [ "passenger", "classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties.html#a68699c58cb0d984fd6d59abb422c659e", null ], - [ "payload", "classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties.html#a7626274633166b37c23dd5236ec70925", null ], - [ "takeoff", "classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties.html#a5c8f0a58b0892e19cae442c9630423d9", null ], - [ "zero_fuel_center_of_gravity", "classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties.html#afb63d59caed1c5937f3596caa7feec43", null ] - ] ], - [ "Costs", "classSUAVE_1_1Vehicle_1_1Costs.html", [ - [ "__defaults__", "classSUAVE_1_1Vehicle_1_1Costs.html#a9a95eda69e637d6463d6ca1fe3e421bb", null ], - [ "industrial", "classSUAVE_1_1Vehicle_1_1Costs.html#ae740e9233b089a130cb78c1d75defc6f", null ], - [ "operating", "classSUAVE_1_1Vehicle_1_1Costs.html#aef6f2597ec88cc8a923d1203d1121fc5", null ], - [ "tag", "classSUAVE_1_1Vehicle_1_1Costs.html#a23079e49e279971f9508ef8fb6d18168", null ] - ] ] -]; \ No newline at end of file diff --git a/_site/doxygen/group__components-fuselages.html b/_site/doxygen/group__components-fuselages.html deleted file mode 100644 index 9763b6d9..00000000 --- a/_site/doxygen/group__components-fuselages.html +++ /dev/null @@ -1,123 +0,0 @@ - - - - - - - -SUAVE: Fuselages - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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Fuselages
-
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Components traditionally considered to be the fuselage of a vehicle. -More...

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-Classes

class  SUAVE.Components.Fuselages.Fuselage.Fuselage
 
-

Detailed Description

-

Components traditionally considered to be the fuselage of a vehicle.

-

These typically contain the primary payload of the vehicle.

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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE Documentation
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http://jquery.org/license - * - * http://docs.jquery.com/UI/Mouse - * - * Depends: - * jquery.ui.widget.js - */ -(function(b,c){var a=false;b(document).mouseup(function(d){a=false});b.widget("ui.mouse",{options:{cancel:":input,option",distance:1,delay:0},_mouseInit:function(){var d=this;this.element.bind("mousedown."+this.widgetName,function(e){return d._mouseDown(e)}).bind("click."+this.widgetName,function(e){if(true===b.data(e.target,d.widgetName+".preventClickEvent")){b.removeData(e.target,d.widgetName+".preventClickEvent");e.stopImmediatePropagation();return false}});this.started=false},_mouseDestroy:function(){this.element.unbind("."+this.widgetName)},_mouseDown:function(f){if(a){return}(this._mouseStarted&&this._mouseUp(f));this._mouseDownEvent=f;var e=this,g=(f.which==1),d=(typeof this.options.cancel=="string"&&f.target.nodeName?b(f.target).closest(this.options.cancel).length:false);if(!g||d||!this._mouseCapture(f)){return true}this.mouseDelayMet=!this.options.delay;if(!this.mouseDelayMet){this._mouseDelayTimer=setTimeout(function(){e.mouseDelayMet=true},this.options.delay)}if(this._mouseDistanceMet(f)&&this._mouseDelayMet(f)){this._mouseStarted=(this._mouseStart(f)!==false);if(!this._mouseStarted){f.preventDefault();return true}}if(true===b.data(f.target,this.widgetName+".preventClickEvent")){b.removeData(f.target,this.widgetName+".preventClickEvent")}this._mouseMoveDelegate=function(h){return e._mouseMove(h)};this._mouseUpDelegate=function(h){return e._mouseUp(h)};b(document).bind("mousemove."+this.widgetName,this._mouseMoveDelegate).bind("mouseup."+this.widgetName,this._mouseUpDelegate);f.preventDefault();a=true;return true},_mouseMove:function(d){if(b.browser.msie&&!(document.documentMode>=9)&&!d.button){return this._mouseUp(d)}if(this._mouseStarted){this._mouseDrag(d);return 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i=this.className.match(/ui-resizable-(se|sw|ne|nw|n|e|s|w)/i)}f.axis=i&&i[1]?i[1]:"se"}});if(k.autoHide){this._handles.hide();c(this.element).addClass("ui-resizable-autohide").hover(function(){if(k.disabled){return}c(this).removeClass("ui-resizable-autohide");f._handles.show()},function(){if(k.disabled){return}if(!f.resizing){c(this).addClass("ui-resizable-autohide");f._handles.hide()}})}this._mouseInit()},destroy:function(){this._mouseDestroy();var e=function(g){c(g).removeClass("ui-resizable ui-resizable-disabled ui-resizable-resizing").removeData("resizable").unbind(".resizable").find(".ui-resizable-handle").remove()};if(this.elementIsWrapper){e(this.element);var f=this.element;f.after(this.originalElement.css({position:f.css("position"),width:f.outerWidth(),height:f.outerHeight(),top:f.css("top"),left:f.css("left")})).remove()}this.originalElement.css("resize",this.originalResizeStyle);e(this.originalElement);return this},_mouseCapture:function(f){var g=false;for(var e in this.handles){if(c(this.handles[e])[0]==f.target){g=true}}return !this.options.disabled&&g},_mouseStart:function(g){var j=this.options,f=this.element.position(),e=this.element;this.resizing=true;this.documentScroll={top:c(document).scrollTop(),left:c(document).scrollLeft()};if(e.is(".ui-draggable")||(/absolute/).test(e.css("position"))){e.css({position:"absolute",top:f.top,left:f.left})}this._renderProxy();var k=b(this.helper.css("left")),h=b(this.helper.css("top"));if(j.containment){k+=c(j.containment).scrollLeft()||0;h+=c(j.containment).scrollTop()||0}this.offset=this.helper.offset();this.position={left:k,top:h};this.size=this._helper?{width:e.outerWidth(),height:e.outerHeight()}:{width:e.width(),height:e.height()};this.originalSize=this._helper?{width:e.outerWidth(),height:e.outerHeight()}:{width:e.width(),height:e.height()};this.originalPosition={left:k,top:h};this.sizeDiff={width:e.outerWidth()-e.width(),height:e.outerHeight()-e.height()};this.originalMousePosition={left:g.pageX,top:g.pageY};this.aspectRatio=(typeof j.aspectRatio=="number")?j.aspectRatio:((this.originalSize.width/this.originalSize.height)||1);var i=c(".ui-resizable-"+this.axis).css("cursor");c("body").css("cursor",i=="auto"?this.axis+"-resize":i);e.addClass("ui-resizable-resizing");this._propagate("start",g);return true},_mouseDrag:function(e){var h=this.helper,g=this.options,m={},q=this,j=this.originalMousePosition,n=this.axis;var r=(e.pageX-j.left)||0,p=(e.pageY-j.top)||0;var i=this._change[n];if(!i){return false}var l=i.apply(this,[e,r,p]),k=c.browser.msie&&c.browser.version<7,f=this.sizeDiff;this._updateVirtualBoundaries(e.shiftKey);if(this._aspectRatio||e.shiftKey){l=this._updateRatio(l,e)}l=this._respectSize(l,e);this._propagate("resize",e);h.css({top:this.position.top+"px",left:this.position.left+"px",width:this.size.width+"px",height:this.size.height+"px"});if(!this._helper&&this._proportionallyResizeElements.length){this._proportionallyResize()}this._updateCache(l);this._trigger("resize",e,this.ui());return false},_mouseStop:function(h){this.resizing=false;var i=this.options,m=this;if(this._helper){var g=this._proportionallyResizeElements,e=g.length&&(/textarea/i).test(g[0].nodeName),f=e&&c.ui.hasScroll(g[0],"left")?0:m.sizeDiff.height,k=e?0:m.sizeDiff.width;var n={width:(m.helper.width()-k),height:(m.helper.height()-f)},j=(parseInt(m.element.css("left"),10)+(m.position.left-m.originalPosition.left))||null,l=(parseInt(m.element.css("top"),10)+(m.position.top-m.originalPosition.top))||null;if(!i.animate){this.element.css(c.extend(n,{top:l,left:j}))}m.helper.height(m.size.height);m.helper.width(m.size.width);if(this._helper&&!i.animate){this._proportionallyResize()}}c("body").css("cursor","auto");this.element.removeClass("ui-resizable-resizing");this._propagate("stop",h);if(this._helper){this.helper.remove()}return false},_updateVirtualBoundaries:function(g){var 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SUAVE: An Aerospace Vehicle Environment for Designing Future Aircraft
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This is the documentation page for SUAVE. For more information on general capabilities, current development efforts, and code/documentation style, please check the main website.

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- - - - - diff --git a/_site/doxygen/md_2_overview.html b/_site/doxygen/md_2_overview.html deleted file mode 100644 index 1b4f5f0c..00000000 --- a/_site/doxygen/md_2_overview.html +++ /dev/null @@ -1,112 +0,0 @@ - - - - - - - -SUAVE: Code Overview - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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Code Overview
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SUAVE is a conceptual level aircraft design environment built with the ability to analyze and optimize both conventional and unconventional designs. This capability is achieved in part by allowing analysis information for aircraft to be drawn from multiple sources. Many other software tools for aircraft conceptual design rely on fixed empirical correlations and other handbook approximation. SUAVE instead provides a framework that can be used to design aircraft featuring advanced technologies by augmenting relevant correlations with physics-based methods.

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SUAVE is an open source suite constructed as a modular set of analysis tools written in Python. Additional capabilities can be incorporated using extensible interfaces and prototyped with a top-level script. The flexibility of the environment allows the creation of arbitrary mission profiles, unconventional propulsion networks, and right-fidelity at right-time discipline analyses. Development is currently lead by the Aerospace Design Lab at Stanford University.

-

We recognize that learning to use a large code base can be daunting, so we have provided several tutorials in the guides section of our website. In addition, we have created high level documentation with the intention of showing the structure used for various types of funcionality, along with some advice on how to add modifications. These can be found in the sidebar under this document. If these two resources are not enough to answer questions you have about the code, please ask on our forum.

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- - - - diff --git a/_site/doxygen/md_3_doc_instructions.html b/_site/doxygen/md_3_doc_instructions.html deleted file mode 100644 index aafa54b3..00000000 --- a/_site/doxygen/md_3_doc_instructions.html +++ /dev/null @@ -1,189 +0,0 @@ - - - - - - - -SUAVE: How to Read (and Write) the Documentation - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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How to Read (and Write) the Documentation
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This is an explanation of how documentation is built in SUAVE so that the user can know what to look for and how to write it if they wish to add their own code.

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Docstrings

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All classes and functions in SUAVE have docstrings have docstrings. These give the user an understanding of what the function does and information on the input and output variables.

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Classes

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For a class, the docstring has three parts:

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  • General description
  • -
  • Assumptions
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  • Source
  • -
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The general description provides a brief summary of what the class is used for. Assumptions list any significant assumptions are important in how it is used. This may be listed as None or N/A if there are no important assumptions. The source section should provide the general source of methods in the class. If there is no overall source, a message like 'see sources in functions' may be appropriate. There are also cases where a source is not relevant, such as simple geometric functions, and may also be listed as None or N/A.

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Class Docstring Template

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This is the general template that can be used when creating a new class. It should be placed directly under the class declaration.

"""<Description>
-
-Assumptions:
-<any assumptions>
-
-Source:
-<source>
-"""
-

Functions

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For functions there are six categories:

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    -
  • Description
  • -
-

This is a general description of what the function does. It should also include any key information that does not fit into one of the other categories.

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    -
  • Assumptions
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This should contain any assumptions made by the function. None or N/A can be used if none are used.

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  • Source
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The source of any methods that have been implemented. Simple methods like basic geometric relations do not need a source.

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  • Inputs
  • -
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This should contain any variables or functions passed to the function. If the passed variable is a data structure, the components that are used should be listed. Each item should include a description if it is not obvious from the name, and any relevant units. It may

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Example Case

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This is the docstring from [Supersonic_Nozzle]()

    """ This computes the output values from the input values according to
-    equations from the source.
-
-    Assumptions:
-    Constant polytropic efficiency and pressure ratio
-
-    Source:
-    https://web.stanford.edu/~cantwell/AA283_Course_Material/AA283_Course_Notes/
-
-    Inputs:
-      conditions data class with conditions.freestream.
-        isentropic_expansion_factor         [Unitless]
-        specific_heat_at_constant_pressure  [J/(kg K)]
-        pressure                            [Pa]
-        stagnation_pressure                 [Pa]
-        stagnation_temperature              [K]
-        universal_gas_constant              [J/(kg K)] (this is a bad name)
-        mach_number                         [Unitless]
-
-      self.inputs.
-        stagnation_temperature              [K]
-        stagnation_pressure                 [Pa]
-
-    Outputs:
-      self.outputs.
-        stagnation_temperature              [K]  
-        stagnation_pressure                 [Pa]
-        stagnation_enthalpy                 [J/kg]
-        mach_number                         [Unitless]
-        static_temperature                  [K]
-        static_enthalpy                     [J/kg]
-        velocity                            [m/s]
-        static_pressure                     [Pa]
-        area_ratio                          [Unitless]
-
-    Properties Used:
-      self.
-        pressure_ratio                      [Unitless]
-        polytropic_efficiency               [Unitless]
-        """       
-

The docstring is broken into

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- - - - diff --git a/_site/doxygen/md_4_mission_solver.html b/_site/doxygen/md_4_mission_solver.html deleted file mode 100644 index 010541e6..00000000 --- a/_site/doxygen/md_4_mission_solver.html +++ /dev/null @@ -1,293 +0,0 @@ - - - - - - - -SUAVE: Mission Solver Structure - - - - - - - - - - - - - - - -
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SUAVE -  1.0.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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Mission Solver Structure
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This is a high level overview of how the mission solver functions. The purpose is to show the structure that is used for an existing mission, and show where changes should be made if different functionality is desired.

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File Structure

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Mission scripts are split into two folders in the SUAVE repository. The first is in trunk/SUAVE/**Analyses/Mission**/Segments, and the second is in trunk/SUAVE/**Methods/Missions**/Segments. As with other types of analyses and methods, the distinction between these is that the Analyses folder contains classes that are built to use functions stored in the Methods folder. This division is done to make it easier to build new analysis classes using a mix of available methods.

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A typical mission segment analysis file contains four keys parts. The first specifies default user inputs, unknowns, and residuals. The inputs are used to provide the analysis with conditions that need to be met, while the unknowns and residuals are used as part of the solution process. The second sets the initialization functions for the analysis, which are run at the beginning. The third picks the convergence method and specifies the functions that will be used during iteration. The fourth finalizes the data and processes it for results output.

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Initialization

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For this tutorial, we will be considering the constant speed constant altitude cruise segment. The files are available here (Analysis) and here (Method). This class also inherits information from more general segment classes, which include many of the processing functions. As with other segments, the user will specify key conditions. For this case, altitude, air speed, and distance are the necessary inputs. If the user does not specify an altitude, it will be taken automatically from the last value in the previous segment. These inputs must be specified in some way for the mission segment to be evaluated. They are shown below as well:

self.altitude  = None
-self.air_speed = 10. * Units['km/hr']
-self.distance  = 10. * Units.km
-

The other set of segment specific initial values are the values used for solving the segment (typically this means satisfying a force balance at every evaluation point). These can be changed by the user if needed, but the default values should perform fine for most cases.

self.state.unknowns.throttle   = ones_row(1) * 0.5
-self.state.unknowns.body_angle = ones_row(1) * 0.0
-self.state.residuals.forces    = ones_row(2) * 0.0
-

Here throttle and body angle are the unknowns, and the values shown here are the values they will start at. The residuals will be computed based on these unknowns, so their initial value is not important. Instead they are initialized just to create the necessary data structure. The ones_row line will create a numpy array with the number of elements needed for evaluation.

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Evaluation Details

-

Most of the missions in SUAVE, including this one, are broken into several points in time based on a Chebyshev polynomial. This causes the points to be closer together at either end of the segment. The choice of a Chebyshev polynomial (which creates cosine spacing) provides better convergence and smoothness properties versus other methods such as linear spacing.

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At each of these points the aerodynamic analysis is queried to find CL and CD, which are then converted to lift and drag. These values will be dependent on the body angle unknown and other aerodynamic parameters. Thrust is found from the vehicle's energy network, which is dependent on the throttle unknown. A weight is determined by looking at the initial weight and subsequent mass rate (typically corresponding with fuel burn). In this cruise segment, these forces are summed in 2D and the results are put in the residuals. The functions needed to arrive these forces are found in the Update Conditions section of the [Analysis file](dox_link). This section is also shown below in one of the steps to create a new mission.

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Once the evaluation process has been performed at all points, the unknowns and residuals are fed back to the solve routine, which in this case is scipy's fsolve. The file that performs this process is here. This routine continues evaluating the points until convergence is reached. Once this happens, post processing is done to put the data in the results output.

-

Using Multiple Segments

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Multiple segments can be run sequentially by appending them in the desired order. Examples of this are in all the tutorial files that have an aircraft fly a full mission. In addition, the full mission can be run simultaneously will all segment constraints used together. If you are interested in doing something like this, please ask us about it on our forum.

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Process Summary

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Mission Setup

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  • Initializes default values for unknowns
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  • Initializes set of functions used to determine residuals
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Evaluate

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  • -
  • Repeats process for each segment until full mission is complete
  • -
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Adding New Mission Segments

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The segment described above uses two unknowns to solve force residuals in two dimensions. This general setup works well for many problems of interest, but SUAVE is designed to accommodate other mission analysis types as well. A user may want to add control surface deflection and solve for moments as well, or look at forces in all three dimensions.

-

In addition, a user may want to modify how the mission is flown, as is done with the many other segments currently available. They may want to modify how the mission is solved, such as is done in our single point evaluation segments where finite differencing is not relevant.

-

Here we will explain the process of modifying our constant speed constant rate climb segment to be constant throttle constant speed. This still uses 2D force balance but changes the profile. There are four functions that are modified here. The first is shown below. The functions can be found in [here]() and [here]()

def initialize_conditions(segment,state):
-
-    # unpack
-    climb_rate = segment.climb_rate
-    air_speed  = segment.air_speed   
-    alt0       = segment.altitude_start 
-    altf       = segment.altitude_end
-    t_nondim   = state.numerics.dimensionless.control_points
-    conditions = state.conditions  
-
-    # check for initial altitude
-    if alt0 is None:
-        if not state.initials: raise AttributeError('initial altitude not set')
-        alt0 = -1.0 * state.initials.conditions.frames.inertial.position_vector[-1,2]
-
-    # discretize on altitude
-    alt = t_nondim * (altf-alt0) + alt0
-
-    # process velocity vector
-    v_mag = air_speed
-    v_z   = -climb_rate # z points down
-    v_x   = np.sqrt( v_mag**2 - v_z**2 )
-
-    # pack conditions    
-    conditions.frames.inertial.velocity_vector[:,0] = v_x
-    conditions.frames.inertial.velocity_vector[:,2] = v_z
-    conditions.frames.inertial.position_vector[:,2] = -alt[:,0] # z points down
-    conditions.freestream.altitude[:,0]             =  alt[:,0] # positive altitude in this context
-

This function initializes speed and altitude based on the given climb rate, airspeed, and altitude end points. t_nondim gives nondimensional time in cosine spacing from 0 to 1 in order to pick the values at the points to be evaluated. Unfortunately, when we use constant throttle we cannot know beforehand exactly how altitude (or climb rate in this case) will vary with time, so altitude cannot be spaced with this method. Instead a different function is used to initialize conditions:

def initialize_conditions(segment,state):
-
-    # unpack
-    throttle   = segment.throttle
-    air_speed  = segment.air_speed   
-    alt0       = segment.altitude_start 
-    altf       = segment.altitude_end
-    t_nondim   = state.numerics.dimensionless.control_points
-    conditions = state.conditions  
-
-    # check for initial altitude
-    if alt0 is None:
-        if not state.initials: raise AttributeError('initial altitude not set')
-        alt0 = -1.0 * state.initials.conditions.frames.inertial.position_vector[-1,2]
-
-    # pack conditions  
-    conditions.propulsion.throttle[:,0] = throttle
-    conditions.frames.inertial.velocity_vector[:,0] = air_speed # start up value
-

Here only the throttle and air speed are loaded in, and discretization of other values will need to occur later so that it is part of the iteration loop. This requires a new function that updates the altitude differentials.

def update_differentials_altitude(segment,state):
-
-    # unpack
-    t = state.numerics.dimensionless.control_points
-    D = state.numerics.dimensionless.differentiate
-    I = state.numerics.dimensionless.integrate
-
-
-    # Unpack segment initials
-    alt0       = segment.altitude_start 
-    altf       = segment.altitude_end    
-    conditions = state.conditions  
-
-    r = state.conditions.frames.inertial.position_vector
-    v = state.conditions.frames.inertial.velocity_vector
-
-    # check for initial altitude
-    if alt0 is None:
-        if not state.initials: raise AttributeError('initial altitude not set')
-        alt0 = -1.0 * state.initials.conditions.frames.inertial.position_vector[-1,2]    
-
-    # get overall time step
-    vz = -v[:,2,None] # Inertial velocity is z down
-    dz = altf- alt0    
-    dt = dz / np.dot(I[-1,:],vz)[-1] # maintain column array
-
-    # Integrate vz to get altitudes
-    alt = alt0 + np.dot(I*dt,vz)
-
-    # rescale operators
-    t = t * dt
-
-    # pack
-    t_initial = state.conditions.frames.inertial.time[0,0]
-    state.conditions.frames.inertial.time[:,0] = t_initial + t[:,0]
-    conditions.frames.inertial.position_vector[:,2] = -alt[:,0] # z points down
-    conditions.freestream.altitude[:,0]             =  alt[:,0] # positive altitude in this context    
-
-    return
-

In this function, t, D, and I are numpy arrays that allow approximate differentiation and integration. Since the total time is not known without determining the climb rate, we must first determine the time required to reach the final altitude. The line dt = dz / np.dot(I[-1,:],vz)[-1] does this with the integrator providing the amount of altitude gained if the velocities were spread across just one second instead of the full segment time. This gives the scaling quantity dt that is then used to get the altitude at every point in alt = alt0 + np.dot(I*dt,vz). The values for altitude are then are then packed for use in other functions.

-

The above allows us to deal with discretization without a known profile, but we also must calculate the velocity in order to use this. This is done with another added function.

def update_velocity_vector_from_wind_angle(segment,state):
-
-    # unpack
-    conditions = state.conditions 
-    v_mag  = segment.air_speed 
-    alpha  = state.unknowns.wind_angle[:,0][:,None]
-    theta  = state.unknowns.body_angle[:,0][:,None]
-
-    # Flight path angle
-    gamma = theta-alpha
-
-    # process
-    v_x =  v_mag * np.cos(gamma)
-    v_z = -v_mag * np.sin(gamma) # z points down
-
-    # pack
-    conditions.frames.inertial.velocity_vector[:,0] = v_x[:,0]
-    conditions.frames.inertial.velocity_vector[:,2] = v_z[:,0]
-
-    return conditions
-

This uses our new set of unknowns to determine the velocities.

-

Additionally, since the unknowns are different we must change the function that unpacks them. Wind angle does not need to be stored so it is not included here.

def unpack_body_angle(segment,state):
-
-    # unpack unknowns
-    theta  = state.unknowns.body_angle
-
-    # apply unknowns
-    state.conditions.frames.body.inertial_rotations[:,1] = theta[:,0]
-

We now add these functions to the segment process list.

    # --------------------------------------------------------------
-    #   Initialize - before iteration
-    # --------------------------------------------------------------
-    initialize = self.process.initialize
-
-    initialize.expand_state            = Methods.expand_state
-    initialize.differentials           = Methods.Common.Numerics.initialize_differentials_dimensionless
-    initialize.conditions              = Methods.Climb.Constant_Throttle_Constant_Speed.initialize_conditions
-    initialize.velocities              = Methods.Climb.Constant_Throttle_Constant_Speed.update_velocity_vector_from_wind_angle
-    initialize.differentials_altitude  = Methods.Climb.Constant_Throttle_Constant_Speed.update_differentials_altitude      
-

and

    # Unpack Unknowns
-    iterate.unknowns = Process()
-    iterate.unknowns.mission           = Methods.Climb.Constant_Throttle_Constant_Speed.unpack_body_angle 
-
-    # Update Conditions
-    iterate.conditions = Process()
-    iterate.conditions.velocities      = Methods.Climb.Constant_Throttle_Constant_Speed.update_velocity_vector_from_wind_angle
-    iterate.conditions.differentials_a = Methods.Climb.Constant_Throttle_Constant_Speed.update_differentials_altitude
-    iterate.conditions.differentials_b = Methods.Common.Numerics.update_differentials_time
-    iterate.conditions.acceleration    = Methods.Common.Frames.update_acceleration
-    iterate.conditions.altitude        = Methods.Common.Aerodynamics.update_altitude
-    iterate.conditions.atmosphere      = Methods.Common.Aerodynamics.update_atmosphere
-    iterate.conditions.gravity         = Methods.Common.Weights.update_gravity
-    iterate.conditions.freestream      = Methods.Common.Aerodynamics.update_freestream
-    iterate.conditions.orientations    = Methods.Common.Frames.update_orientations
-    iterate.conditions.aerodynamics    = Methods.Common.Aerodynamics.update_aerodynamics
-    iterate.conditions.stability       = Methods.Common.Aerodynamics.update_stability
-    iterate.conditions.propulsion      = Methods.Common.Energy.update_thrust
-    iterate.conditions.weights         = Methods.Common.Weights.update_weights
-    iterate.conditions.forces          = Methods.Common.Frames.update_forces
-    iterate.conditions.planet_position = Methods.Common.Frames.update_planet_position
-

If you have any questions that are not answered in other tutorials or the FAQ please ask on our forum page. This is also the place to go if you want help building a more elaborate evaluation, such as one that includes moments.

-
-
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Optimization Structure
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This is an overview of how optimization is done in SUAVE. A specific tutorial case is also available here.

-

Nexus Class

-

The Nexus class is the underlying data structure that is used for optimization. It is created to hold all data and functionality needed to link together optimizers and the various analysis modules in SUAVE. Detailed information on each of the functions can be found in our [doxygen site]().

-

Standard Optimization File Structure

-

These are the standard files that are used in the optimization process. They are typically stored as Optimize.py, Vehicle.py, Analysis.py, Mission.py, Procedure.py, and Plot_Mission.py. These names can be changed if desired.

-

Optimize

-

This is the top level file that is run to perform the optimization. Inputs, objective, constraints, and aliases are specified here. The inputs have an initial value, bounds, a scaling factor, and the units used. This provides later functions with the information needed to vary the parameters. Units.less indicates a unitless quantity. SI units are the default in SUAVE's internal calculations, so Units.meter will not modify the internal value, while something like Units.foot will.

problem.inputs = np.array([
-    [ 'wing_area'     ,  125.  , (   120.   ,   180.   )  ,   100.  , Units.meter**2],
-    [ 'aspect_ratio'  ,  3.3   , (   2.0    ,   6.0    )  ,   10.   , Units.less],
-])
-

Constraints and the objective are similar. Both have scaling quantities and constraints also have bounds.

problem.constraints = np.array([
-    [ 'design_range_fuel_margin', '>', 0., 1E-1, Units.less]
-])
-
-problem.objective = np.array([
-    ['fuel_burn_rate', 1., Units.kg/Units.s]
-])
-

Finally we have aliases. This provides the optimization process with the position of the various parameters in the data structure. Aliases are used so that short names can be used for variables and a single variable can control multiple items in the data structure. Controlling multiple items can be important if different vehicle configurations are used at different points in the mission, and one of the vehicle parameters should change in the same way for all of the configurations. We can use * as a wildcard. This is used below to change the aspect ratio of the main wing in every vehicle configuration.

problem.aliases = [
-    [ 'wing_area'       ,   ['vehicle_configurations.base.wings.main_wing.areas.reference',
-                                              'vehicle_configurations.base.reference_area']],
-    [ 'aspect_ratio'    ,    'vehicle_configurations.*.wings.main_wing.aspect_ratio'       ],
-    [ 'fuel_burn_rate'  ,    'summary.fuel_burn_rate'                                      ],
-]    
-

This file then specifies the configurations, analyses, missions, and procedure that will be used. This are typically contained in separate files and more details on each are below. Once all of this is specified, the desired optimizer is called with the nexus class created by this setup.

-

Vehicle Setup

-

This contains the vehicle information such as geometric data and configurations. It is the same as the vehicle setup used for basic analysis purposes.

-

Analysis Setup

-

This contains information on what analyses should be run for the vehicle. For example if correlation-based aerodynamics or AVL should be used for computations. It requires vehicle information from the previous step.

-

Mission Setup

-

This is also the same as the standard mission setup. It determines how the mission will be flown. It requires analysis information from the previous step.

-

Procedure

-

This is an optimization specific file that determines how the vehicle, analysis, or mission is modified with the input values in the optimization and also runs the mission. For example, changing the wing area will usually require changes to other wing parameters, such as root chord length. This module reads the new inputs and changes other values accordingly based on user specified processes.

-

Plotting

-

This function is not necessary to the optimization, but is often included in the files used and is added to the optimize main call as a way to visualize the results.

-

Optimizer Interface

-

The other step that must be taken to perform an optimization is to convert the standardized input above into values that can be used by the selected optimizer. This is done through a separate script for each optimizer, all of which are found in the [optimization folder](doxygen_link_here).

-

For example, if we are using PyOpt to optimize, we might use `output = pyopt_setup.Pyopt_Solve(problem,solver='SNOPT')` in the main function of the top level optimizer. This function reads the inputs, constraints, and objective and converts them to a format that the selected optimizer (SNOPT here) can understand.

-

Evaluation Process

-

This shows the typical evaluation process, including where items like inputs and aliases are used. This chart assumes a single objective call, but some optimizers will include calls such as all_constraints which require another evaluation. If the evaluation is a duplicate, data from the previous evaluation will be used instead of stepping through the procedure again.

-

 

-
- -
-

 

-

Incorporating Multi-fidelity

-

Multiple levels of fidelity are designed to be relatively easy to incorporate in SUAVE, but there are still a few things to keep in mind. First, the chosen optimizer must support multi-fidelity and be able to change the nexus.fidelity_level value. Once this is done, it is also important to remember that the mission is set up based on the analyses. This means that if a change is made to the analyses then the mission must be rebuilt with the new settings. As an example, code below for changing the analysis level is shown. This is a function that has been added to the procedure file.

def set_fidelity_level(nexus):
-
-    if nexus.has_key('fidelity_level') == False:
-        print 'Fidelity level not set, defaulting to 1'
-        nexus.fidelity_level = 1
-
-    if nexus.fidelity_level == 2:
-        aerodynamics = SUAVE.Analyses.Aerodynamics.Supersonic_OpenVSP_Wave_Drag()
-        aerodynamics.settings.number_slices    = 20
-        aerodynamics.settings.number_rotations = 10        
-    elif nexus.fidelity_level == 1:
-        aerodynamics = SUAVE.Analyses.Aerodynamics.Supersonic_Zero()
-    else:
-        raise ValueError('Selected fidelity level not supported')
-    aerodynamics.geometry = copy.deepcopy(nexus.vehicle_configurations.base)
-    nexus.analyses.base.append(aerodynamics)
-
-    nexus.missions = mission_as2.setup(nexus.analyses)
-
-    return nexus
-

Here we see that nexus.missions has been updated in addition to nexus.analyses, since failing to do this would have the mission run with the previous analysis settings.

-

Key Functions in the Optimizer Setup

-

We briefly mentioned how optimization parameters would need to be converted so that they could run with a particular optimizer. Here we show how this is managed and show which functions are likely to be useful in building a new optimizer setup.

-

The key items that will be needed for most optimizers are shown below, taken from the PyOpt setup:

inp = problem.optimization_problem.inputs
-obj = problem.optimization_problem.objective
-con = problem.optimization_problem.constraints  
-
-# Set inputs
-nam = inp[:,0] # Names
-ini = inp[:,1] # Initials
-bnd = inp[:,2] # Bounds
-scl = inp[:,3] # Scale
-typ = inp[:,4] # Type
-

These can be scaled with two helper functions that are part of the SUAVE distribution:

from SUAVE.Optimization import helper_functions as help_fun
-
-bnd_constraints    = help_fun.scale_const_bnds(con)
-scaled_constraints = help_fun.scale_const_values(con,bnd_constraints)
-x                  = ini/scl
-

What happens next is entirely dependent on what optimizer you want to use. Some may require that constraint bounds happen at 0 or are either > or <. However this setup is done, you will likely need to create a function that can accept the problem and inputs and give required outputs such as the objective value and constraints. In the PyOpt case, this is done with a simple wrapper and an added function:

mywrap = lambda x:PyOpt_Problem(problem,x)
-

...

def PyOpt_Problem(problem,x):
-
-    obj   = problem.objective(x)
-    const = problem.all_constraints(x).tolist()
-    fail  = np.array(np.isnan(obj.tolist()) or np.isnan(np.array(const).any())).astype(int)
-
-
-    print 'Inputs'
-    print x
-    print 'Obj'
-    print obj
-    print 'Con'
-    print const
-
-    return obj,const,fail
-

Please visit our forum if you have any other questions on how the optimizer interface works or how to convert the values to what you need.

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Energy Networks
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Energy networks are really a fancy name for your propulsion system. The reason we call them a network rather than "engine" or the like is that it encompasses far more than that. These "energy networks" are the complex systems that future aircraft will incorporate that can reduce or eliminate fuel burn. For example if you have a hybrid gas-electric aircraft you don't have just an engine. You have an engine, a motor, batteries, a generator, a gearbox, a propeller or ducted fan, wiring, electronics... and that doesn't include the parts inside the internal combustion engine. Modeling these systems completely is essential in designing such a vehicle.

-

To do this we depart from the typical SUAVE structure of analyses and methods. This was done because we want to look at each component of the network individually. All components behave in their own ways. The purpose of the network is to link together every component in the system to work together.

-

File Structure

-

One of the biggest sources of confusion for energy networks is the file structure. The files for every part of a network are located at trunk/SUAVE/**Components/Energy**. Within that we have several subfolders.

-

/Converters

-

Converters are defined as component that takes energy or power from one form to another. It could be electrical to mechanical, or even chemical to mechanical, etc.. Examples in this folder include a motor, a solar panel, and the compressor section of a jet engine.

/Distributors

-

Distributors move power from one part of the network to another. The common use of this is an electronic speed controller for a small UAV.

/Networks

-

This is where all the "Network" scripts that tie together all of the pieces are kept. Examples in here are a turbofan network.

/Peripherals

-

Peripherals are items that rely on the network but do not produce thrust or power for the vehicle. For example, avionics require electricity which must be accounted for.

/Processes

-

Processes are non tangible parts of a network that are necessary. For example the process is thrust. This function is useful for jet engines to combine and dimensionalize the final thrust once all the components are combined in the network.

/Storages

-

Storages, for now, include batteries. However, in the future we could have fuel tanks here. Currently fuel is only handled as a mass variation.

-

Component Example

-

Below is a simple example of the most basic energy component in SUAVE. All energy components are classes. The A solar panel is a converter since it converts a photonic flux calculated by a solar radiation model and converts it to a power.

# Solar_Panel.py
-#
-# Created:  Jun 2014, E. Botero
-# Modified: Jan 2016, T. MacDonald
-
-# ----------------------------------------------------------------------
-#  Imports
-# ----------------------------------------------------------------------
-
-# suave imports
-import SUAVE
-
-from SUAVE.Components.Energy.Energy_Component import Energy_Component
-
-# ----------------------------------------------------------------------
-#  Solar_Panel Class
-# ----------------------------------------------------------------------
-class Solar_Panel(Energy_Component):
-
-    def __defaults__(self):
-        self.area       = 0.0
-        self.efficiency = 0.0
-
-    def power(self):
-
-        # Unpack
-        flux       = self.inputs.flux
-        efficiency = self.efficiency
-        area       = self.area
-
-        p = flux*area*efficiency
-
-        # Store to outputs
-        self.outputs.power = p
-
-        return p
-

These classes contain functions that simulate a process. Multiple functions can exist within a component. This component has defaults, inputs, and outputs. Defaults are provided that give the user an idea of what the fixed parameters of the component are. These values are set when initializing a vehicle. This is the recipe that all energy components are built off.

-

Network Scripts

-

Network scripts are the link between these components. The network script allows you to reconfigure the connection between components to create your dream propulsion system. These must be logically created as components have set inputs and outputs. For example, you can't magically go from a battery to a propeller without anything in between. Some knowledge of the inputs and outputs are necessary, however they're generally quite intuitive. One interesting avenue for SUAVE is that you can create networks of networks.

-

The linking process works like this:

    # step 1
-    solar_flux.solar_radiation(conditions)
-    # link
-    solar_panel.inputs.flux = solar_flux.outputs.flux
-    # step 2
-    solar_panel.power()
-    # link
-    solar_logic.inputs.powerin = solar_panel.outputs.power
-

Notice the first step above is to calculate the solar radiation. Once the solar radiation is calculated the components are linked and step 2 can continue with the the power being calculated. From there a solar logic component will use that power.

-

The other main hallmark of a network is that they are called at every point in the mission to calculate the state of the system. Given some conditions data that defines the state of the vehicle the components must provide back to the mission being solved a thrust force and a mass rate. Other outputs can be stored back to conditions, however a thrust and a mass rate must be returned.

-

Vehicle Script Setup of a Network

-

Here we will provide a snippet of the turbofan setup for a B737.

# ------------------------------------------------------------------
-#  Component 3 - Low Pressure Compressor
-
-# instantiate 
-compressor = SUAVE.Components.Energy.Converters.Compressor()    
-compressor.tag = 'low_pressure_compressor'
-
-# setup
-compressor.polytropic_efficiency = 0.91
-compressor.pressure_ratio        = 1.14    
-
-# add to network
-turbofan.append(compressor)
-

In the above example, a compressor is added to the network. The compressor is tagged as the low_pressure_compressor to distinguish it from the high pressure compressor. The polytropic efficiency and pressure ratio are set. Finall it is appended to the network.

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- - - - diff --git a/_site/doxygen/modules.html b/_site/doxygen/modules.html deleted file mode 100644 index a01091bd..00000000 --- a/_site/doxygen/modules.html +++ /dev/null @@ -1,251 +0,0 @@ - - - - - - - -SUAVE: Modules - - - - - - - - - - - - - - - -
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Modules
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Here is a list of all modules:
-
[detail level 12345]
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
 AnalysesAnalyses are classes that are comprised of several methods
 AerodynamicsThese are the analyses that control aerodynamic evaluations
 AtmosphericClasses that represent the different types of atmospheres that may be used for analysis
 CostsCost Analysis
 EnergyThis is the analysis that controls energy network evaluations
 GeometryThis is the analysis that controls vehicle geometry evaluations
 LoadsThis is the analysis that controls vehicle load evaluations
 MissionMission Analyses to setup each part of a mission to fly
 SegmentSegment analyses to setup each part of a mission to fly
 Vary_CruiseVariable cruise mission setups
 NoiseThese are the analyses that control noise evaluations
 SizingThis is the analysis that controls vehicle sizing evaluations
 Stability
 StructuresThis is the analysis that controls vehicle structure evaluations
 WeightsClasses that represent the types of aircraft configuration weight computations
 AttributesAttributes provide objects that can be attached to various analyses
 AirportsThese are airport related classes
 AtmospheresContains basic data for atmospheres
 EarthContains basic data for specific Earth atmosphere types
 ConstantsContains basic data for atmospheres
 GasesCommon gasesclasses
 LiquidsCommon liquidsclasses
 PlanetsAvailable planetsclasses
 PropellantsCommon propellantsclasses
 ComponentsComponents are classes that represent objects that are put together to form a vehicle
 ConfigsThis is the component that defines the template for vehicle configurations
 CostsCost component
 EnergyComponents used in energy networks
 ConvertersEnergy components meant to be used within an energy network
 DistributorsComponents that move energy/control energy/power in a network
 NetworksComponents used in energy networks
 PeripheralsThese are components that use energy but are otherwise not part of a network
 ProcessesThese are components that use energy to perform a process
 StoragesEnergy components that store energy (such as batteries)
 FuselagesComponents traditionally considered to be the fuselage of a vehicle
 Landing GearComponents considered are the Main and Nose Landing Gear
 PayloadsAvailable payload componentsinit.py
 PropulsorsThese are the components used to provide thrust to a vehicle
 SystemsThese are the components which define a vehicle's onboard systems
 Wingsinit.py
 Airfoilsinit.py
 CoreCore is all the under the hood magic that makes SUAVE work
 Input_OutputThese functions provide SUAVE data storage capabilities and capabilities to work with files for other programs
 D3JSFiles to handle D3JS output
 FreeMindFunction to save FreeMind output
 GMSHFunctions needed to work with GMSH
 OpenVSPFunctions needed to work with OpenVSP
 ResultsMiscellaneous functions to print results
 SU2Functions needed to interface with SU2
 SUAVEFunctions needed to save SUAVE data structures in JSON form
 XMLFiles to handle XML input and output
 MethodsMethods provide the functions needed to perform analyses
 AerodynamicsAerodynamic methods contain the functions for the aerodynamic analyses
 AERODASFunctions to perform calculations according to AERODAS models
 AVLFunctions to AVL calculations
 Fidelity_ZeroFunctions to perform low-fidelity calculations
 OpenVSP_Wave_DragFunctions to perform wave drag calculations using OpenVSP
 SU2_EulerSU2_Euler contains the function needed to run the SU2 Euler Analysis
 Supersonic_ZeroFunctions to perform low-fidelity calculations including supersonics
 Center_of_GravityDescription
 CostsThis contains functions that can compute costs associated with building and operating an aircraft
 Industrial CostsThese functions provide cost estimates for an aircraft program
 Operating CostsThis is a stub for computing operating costs
 Flight_DynamicsDescription
 Dynamic_Stability
 Static_Stability
 GeometryThese methods are primarily used for sizing
 Three DimensionalGeometry functions for three dimensions
 Two DimensionalGeometry functions for two dimensions
 MissionsMission methods contain the functions for setting up and solving a mission
 SegmentsMission Segment folders containing the functions for setting up and solving a mission
 NoiseDescription
 CorrelationsCorrelation type methods for calculating noise
 Fidelity_OneDescription
 PerformanceThis is a set of basic aircraft performance estimation functions
 PowerPower methods contain the functions for electric systems such as batteries and fuel cells
 BatteryFunctions pertaining to battery discharge and sizing
 Fuel_CellFuel_Cell methods contain the functions for the fuel cell analyses
 PropulsionDescription
 UtilitiesThese provide functionality that is not easily grouped into another set
 ChebyshevThese functions provide methods for discrete derivative and integral calculations
 WeightsWeights methods provide different means of estimating vehicle weight breakdowns
 CorrelationsCorrelation methods provide component weight breakdowns for different vehicle configurations based on regressed data
 OptimizationThe files that help you setup an optimization problem
 Package_SetupsIndividual package setups that help you interface with other codes
 TRMMTrust Region Model Management Scripts live here
 PluginsThese are external packages that have been incorporated into SUAVE
 SizingSizing provides methods to size a vehicle's mass, battery energy(s), and power based on its geometric properties and mission
 SurrogateSurrogate provides methods for different surrogate formulations of the original problem
 VehicleVehicle.py
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a.highlighted{background:#fff}.sm-dox.sm-vertical a.disabled{background-image:url("tab_b.png")}.sm-dox.sm-vertical a span.sub-arrow{right:8px;top:50%;margin-top:-5px;border-width:5px;border-style:dashed dashed dashed solid;border-color:transparent transparent transparent #555}.sm-dox.sm-vertical>li>ul:before,.sm-dox.sm-vertical>li>ul:after{display:none}.sm-dox.sm-vertical ul a{padding:10px 20px}.sm-dox.sm-vertical ul a:hover,.sm-dox.sm-vertical ul a:focus,.sm-dox.sm-vertical ul a:active,.sm-dox.sm-vertical ul a.highlighted{background:#eee}.sm-dox.sm-vertical ul a.disabled{background:#fff}} \ No newline at end of file diff --git a/_site/email/email_v03.html b/_site/email/email_v03.html deleted file mode 100644 index 388721c7..00000000 --- a/_site/email/email_v03.html +++ /dev/null @@ -1,293 +0,0 @@ - - - - - -SUAVE v0.3 Release - - - - - - - - - - - - -
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To all of our SUAVE friends,

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Our core team and affiliates have the pleasure of announcing the release of SUAVE version 0.3.

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SUAVE v0.3 is large step forward towards developing a fresh and modern approach to conceptual aircraft design. - Our recent publication highlights some of the new capabilities.

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The big improvements for version 0.3 are:

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We have had recent publications using SUAVE for:

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- Download the latest release here -
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Sincerely,

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The SUAVE Team

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- - - - - - - - - - - - - - diff --git a/_site/email/email_v09.html b/_site/email/email_v09.html deleted file mode 100644 index c1e91ff0..00000000 --- a/_site/email/email_v09.html +++ /dev/null @@ -1,285 +0,0 @@ - - - - - -SUAVE v0.9 Release - - - - - - - - - - - - -
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To all of our SUAVE friends,

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Our core team and affiliates have the pleasure of announcing the release of SUAVE version 0.9. - At SciTech 2017 we presented our work towards integrating CFD simulations in SU2 from SUAVE in an automated way. - With this release, we want to provide to you the ability to perform the same types of analyses. - We've jumped several versions ahead from the last release, this is an indication of how much the code has matured. - We suggest all users update their SUAVE packages to take advantage of these changes.

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The big improvements for version 0.9 are:

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  • OpenVSP API connectivity to create vehicles from SUAVE -
  • Automatic mesh generation using GMSH interface -
  • Aerodynamic model regression using scikit-learn -
  • Methods to compute industrial costs -
  • SUAVE Core rewrite to boost speed by over 30% -
  • New open source license, LGPL-2.1, the same as SU2 -
  • Results files are now saved as JSON files rather than PKL for portability -
  • Many bug fixes and code cleanups -
  • And much, much more! -
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Sincerely,

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The SUAVE Team

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- - - - - - - - - - - - - - diff --git a/_site/email/email_v100.html b/_site/email/email_v100.html deleted file mode 100644 index 5e5f2c8b..00000000 --- a/_site/email/email_v100.html +++ /dev/null @@ -1,285 +0,0 @@ - - - - - -SUAVE v1.0.0 Release - - - - - - - - - - - - -
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To the SUAVE aerospace designers,

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Our core team and affiliates have the pleasure of announcing the release of SUAVE version 1.0.0. This is a big step forward in SUAVE's progress towards the goal of being a fully encompassing aerospace design tool. In the future SUAVE will continue to increment in this versioning scheme. Many things have changed since 0.9.0 under the hood so we suggest all users update their SUAVE packages to take advantage of these changes.

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The big new features for version 1.0.0 are:

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  • Optimized climb segments -
  • Propulsion surrogates -
  • New regression testing scheme -
  • Updated tutorials -
  • Far less confusing code structure -
  • Many bug fixes and code cleanups -
  • And much, much more! -
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- Download SUAVE 1.0.0 -
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Sincerely,

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The SUAVE Team

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- - - - - - - - - - - - - - diff --git a/_site/faq.html b/_site/faq.html deleted file mode 100644 index 3ff2f884..00000000 --- a/_site/faq.html +++ /dev/null @@ -1,212 +0,0 @@ - - - - - - - - Frequently Asked Questions - SUAVE - - - - - - - - - - - - - - -
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Frequently Asked Questions

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Alright, you dove in and now you’re stuck. You’ve come to a good starting point. If this FAQ fails you then we suggest you go through tutorials, maybe our paper, send us a question in the forum, or if all else fails start reading code. Don’t worry the code is more readable than most engineering textbooks.

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How do I get started?

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  • Download SUAVE’s current release on our download page. Specific steps and further instructions for additional software requirements are also listed there.
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  • Get familiar with the code using our guides. Be sure to start the Boeing 737 Tutorial for a basic introduction and the Regional Jet Optimization for the optimization tools.
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  • Ask any remaining questions on the forum
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What version of Python should I use?

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SUAVE is developed in Python 2.7.

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Can I use SUAVE for my own research?

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Yes, you may! Please cite our papers:

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How can I contribute?

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We encourage SUAVE users to expand the environment according to their personal interests. The main areas to be developed are listed here.

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How can I best get in touch with you or ask for help?

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The forum is our main point of contact for SUAVE discussions.

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Where can I see the recent additions to the SUAVE environment?

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Go and check the develop branch on our GitHub site. This branch contains new features that are functional but not necessarily ready for release. Everything in this branch is added to the master branch at the next release. Several other feature branches can also be seen here. These are typically under active development. For any more information on what is available please ask on the forum

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Are there plans to make a Graphical User Interface?

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The core development team is currently not planning on developing a GUI, but you can help! Contact us via the forum.

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How is a mission solved?

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A mission is divided into segments, for example climb, cruise, etc… Then the segment is divided into discrete points that are cosine spaced in time. These make up Chebyshev collocation points. One of the beauties of this method is the integration and differentiation operator. So if you know the velocity at every point, then you can get accelerations and vice-versa.

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The default value is 16 points in each segment for SUAVE. However, our internal numerical experiments have shown highly accurate results with ~0.1% error with only 4 control points and ~.0001% error with 8 as measured from a very highly refined answered.

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For each control point there are various unknowns and residuals. An example of an unknown would be pitch angle, and a residual would be the forces in the Z direction. After performing an analysis using the unknowns the residuals are calculated. These unknowns and residuals are iterated through a hybrid solver (much like a Newton method) in SciPy to converge the residual to zero. Voila, with a little magic you have results!

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- - - - - - - - - - diff --git a/_site/feed.xml b/_site/feed.xml deleted file mode 100644 index 32738099..00000000 --- a/_site/feed.xml +++ /dev/null @@ -1,2128 +0,0 @@ - - - - SUAVE - A multi-fidelity conceptual design environment. Its purpose is to credibly produce conceptual-level design conclusions for future aircraft incorporating advanced technologies. - - http://localhost:4000/ - - Tue, 20 Mar 2018 19:22:42 -0700 - Tue, 20 Mar 2018 19:22:42 -0700 - Jekyll v3.7.3 - - - Code Style - <link rel="stylesheet" href="//cdn.jsdelivr.net/highlight.js/8.6/styles/default.min.css" /> - -<script src="//cdn.jsdelivr.net/highlight.js/8.6/highlight.min.js"></script> - -<script>hljs.initHighlightingOnLoad();</script> - -<h2 id="suave-code-style-guide">SUAVE Code Style Guide</h2> - -<p>SUAVE is built on a slightly modified PEP8 style guide, with changes made to implement a data-oriented view of the code. To help support discovering code, the SUAVE folder structure explicitly mirrors the package structure. Flexibility of the package structure is important, so in general all objects live in their own file, with the same file name as the object name. In order to maintain a separation between Analysis and Data structures, there are often parallel package trees inside the main branches of the package, like SUAVE.Methods.Aerodynamics and SUAVE.Analysis.Aerodynamics. Where possible the names of fields that live in the SUAVE package are written out verbosely, avoiding jargon built on mathematical variable names or acronyms.</p> - -<p>Templates for new methods and objects can be found in the SUAVE repo’s <a href="https://github.com/suavecode/SUAVE/tree/develop/templates">templates</a> folder.</p> - -<h3 id="naming-convention">Naming Convention</h3> - -<p>In terms of typography –</p> - -<ul> - <li><code class="highlighter-rouge">any_variable_name</code> - lower case with underscore <br /> - This includes working variables and instantiated objects.</li> - <li><code class="highlighter-rouge">field_name</code> - lower case with underscore - Any field of an object should be lower case.</li> - <li><code class="highlighter-rouge">function_name</code> - lower case with underscore</li> - <li><code class="highlighter-rouge">Class_Type</code> - upper case with underscore <br /> - The underscores are chosen here to permit the inclusion of acronyms if needed and to maintain symmetry with field name styling.</li> - <li><code class="highlighter-rouge">Package_Name</code> - upper case with underscore <br /> - For example folders within the SUAVE package.</li> -</ul> - -<p>In terms of naming –</p> - -<ul> - <li>Chunk similar field types under a containing field</li> - <li>Bias names towards being specific</li> - <li>Write out field name verbosely, but try to keep short</li> -</ul> - -<h3 id="development-life-cycle">Development Life Cycle</h3> - -<p>As you develop new features for SUAVE, this is generally how you can expect your feature to evolve, in terms of its level of abstraction, and where it lives.</p> - -<ol> - <li> - <p>Prototype <br /> -Either a new function or class. You may want to test these within a separate folder. If you are developing a new analysis approach, for example for aerodynamics or weights, you can usually start with a function. If you are working off of an object like a wing, you can abstract the objects as needed. Generally the lowest level object you’ll use is the SUAVE.Core.Data class. <br /> -A lot of development can be accomplished in a local environment.</p> - </li> - <li>Initial Integration <br /> -Once you’re comfortable that your new feature works robustly, and that it has been tested, it’s time to integrate it into SUAVE. Here are some tips for identifying where it could live. - <ul> - <li>SUAVE.Methods - if it’s a python function. Ping the <a href="http:suavecode.github.io/forum">forum</a> if you want to double check your decision!</li> - <li>SUAVE.Analyses - if it’s an object that manages an analysis like aerodynamics</li> - <li>SUAVE.Components - if it’s a data storage container for a vehicle component like a wing or landing gear</li> - <li>SUAVE.Attributes - if it’s a data storage container for any other type of object, like atmospheres or water<br /></li> - </ul> - - <p>At this point you might want to initiate a pull request to contribute the code back to the main repository.<br /></p> - </li> - <li>Full-Blown Subpackage <br /> -As you write more code, and follow the SUAVE style of keeping one file per object, you will need to create a folder to contain a subpackage. This step may come later in the life of your code, so don’t rush to it if you don’t need the extra overhead.</li> -</ol> - - Tue, 10 Jan 2017 05:25:00 -0800 - http://localhost:4000/guides/style.html - http://localhost:4000/guides/style.html - - - documentation - - blog - - - - - Using the Documentation - <h3 id="how-to-read-and-write-the-documentation">How to Read (and Write) the Documentation</h3> - -<p>This is an explanation of how documentation is built in SUAVE so that the user can know what to look for and how to write it if they wish to add their own code. The doxygen page is available <a href="/doxygen">here</a>.</p> - -<h3 id="docstrings">Docstrings</h3> - -<p>All classes and functions in SUAVE have docstrings have docstrings. These give the user an understanding of what the function does and information on the input and output variables.</p> - -<h4 id="classes">Classes</h4> - -<p>For a class, the docstring has three parts:</p> - -<ul> - <li>General description</li> - <li>Assumptions</li> - <li>Source</li> -</ul> - -<p>The general description provides a brief summary of what the class is used for. Assumptions list any significant assumptions are important in how it is used. This may be listed as None or N/A if there are no important assumptions. The source section should provide the general source of methods in the class. If there is no overall source, a message like ‘see sources in functions’ may be appropriate. There are also cases where a source is not relevant, such as simple geometric functions, and may also be listed as None or N/A.</p> - -<h4 id="class-docstring-template">Class Docstring Template</h4> - -<p>This is the general template that can be used when creating a new class. It should be placed directly under the class declaration.</p> - -<div class="highlighter-rouge"><div class="highlight"><pre class="highlight"><code>"""&lt;Description&gt; - -Assumptions: -&lt;any assumptions&gt; - -Source: -&lt;source&gt; -""" -</code></pre></div></div> - -<h4 id="functions">Functions</h4> - -<p>For functions there are six categories:</p> - -<ul> - <li>Description</li> -</ul> - -<p>This is a general description of what the function does. It should also include any key information that does not fit into one of the other categories.</p> - -<ul> - <li>Assumptions</li> -</ul> - -<p>This should contain any assumptions made by the function. None or N/A can be used if none are used.</p> - -<ul> - <li>Source</li> -</ul> - -<p>The source of any methods that have been implemented. Simple methods like basic geometric relations do not need a source.</p> - -<ul> - <li>Inputs</li> -</ul> - -<p>This should contain any variables or functions passed to the function. If the passed variable is a data structure, the components that are used should be listed. Each item should include a description if it is not obvious from the name. It should also include any relevant units. In addition, information about the variable type or any other information that might be important can be added here.</p> - -<ul> - <li>Outputs</li> -</ul> - -<p>This should contain the same information as in the inputs. It may also contain information on variables that are modified but not explicitly returned.</p> - -<ul> - <li>Properties Used</li> -</ul> - -<p>This carries the same information as input and outputs. It typically contains variables that are properties of the parent class but are not modified. There is some overlap with inputs and outputs, but either category is acceptable as long as the variable is documented.</p> - -<h4 id="function-docstring-template">Function Docstring Template</h4> - -<p>This is a template docstring:</p> - -<div class="highlighter-rouge"><div class="highlight"><pre class="highlight"><code> """&lt;Description&gt; - - Assumptions: - &lt;any assumptions&gt; - - Source: - &lt;source&gt; - - Inputs: - &lt;input1&gt; &lt;units&gt; - &lt;input2&gt; &lt;units&gt; - .. - - Outputs: - &lt;output1&gt; &lt;units&gt; - &lt;output2&gt; &lt;units&gt; - .. - - Properties Used: - &lt;property1&gt; &lt;units&gt; - &lt;property2&gt; &lt;units&gt; - .. - """ -</code></pre></div></div> - -<h3 id="doxygen-grouping-tags">Doxygen Grouping Tags</h3> - -<p>Tags are used to put files into groups that match the SUAVE file structure. <code class="highlighter-rouge">@defgroup</code> tags define a group and should be placed in the init file. An example is shown here:</p> - -<div class="highlighter-rouge"><div class="highlight"><pre class="highlight"><code>## @defgroup Analyses-Aerodynamics Aerodynamics -# These are the analyses that control aerodynamic evaluations. -# @ingroup Analyses -</code></pre></div></div> - -<p>In this example, <code class="highlighter-rouge">Analyses-Aerodynamics</code> is the doxygen tag for the group, while the group appears in the documentation as <code class="highlighter-rouge">Aerodynamics</code>, the next part of the string. The tag is based on the file structure (Analyses/Aerodynamics here). Since this is a subgroup of Analyses, <code class="highlighter-rouge">@ingroup Analyses</code> is used here, with <code class="highlighter-rouge">Analyses</code> as the doxygen tag for the next level up.</p> - -<p>In files, the <code class="highlighter-rouge">@ingroup</code> tag should be inserted before all classes and stand-alone functions. The tag should match the tag in the folder init file’s <code class="highlighter-rouge">@defgroup</code> string.</p> - - Mon, 09 Jan 2017 05:25:00 -0800 - http://localhost:4000/guides/docs.html - http://localhost:4000/guides/docs.html - - - documentation - - blog - - - - - Mission Solver Structure - <h2 id="mission-solver-code-structure">Mission Solver Code Structure</h2> - -<p>This is a high level overview of how the mission solver functions. The purpose is to show the structure that is used for an existing mission, and show where changes should be made if different functionality is desired.</p> - -<h3 id="file-structure">File Structure</h3> - -<p>Mission scripts are split into two folders in the SUAVE repository. The first is in trunk/SUAVE/<strong>Analyses/Mission</strong>/Segments, and the second is in trunk/SUAVE/<strong>Methods/Missions</strong>/Segments. As with other types of analyses and methods, the distinction between these is that the Analyses folder contains classes that are built to use functions stored in the Methods folder. This division is done to make it easier to build new analysis classes using a mix of available methods.</p> - -<p>A typical mission segment analysis file contains four keys parts. The first specifies default user inputs, unknowns, and residuals. The inputs are used to provide the analysis with conditions that need to be met, while the unknowns and residuals are used as part of the solution process. The second sets the initialization functions for the analysis, which are run at the beginning. The third picks the convergence method and specifies the functions that will be used during iteration. The fourth finalizes the data and processes it for results output.</p> - -<h3 id="initialization">Initialization</h3> - -<p>For this tutorial, we will be considering the constant speed constant altitude cruise segment. The files are available <a href="https://github.com/suavecode/SUAVE/blob/develop/trunk/SUAVE/Analyses/Mission/Segments/Cruise/Constant_Speed_Constant_Altitude.py">here (Analysis)</a> and <a href="https://github.com/suavecode/SUAVE/blob/develop/trunk/SUAVE/Methods/Missions/Segments/Cruise/Constant_Speed_Constant_Altitude.py">here (Method)</a>. This class also inherits information from more general segment classes, which include many of the processing functions. As with other segments, the user will specify key conditions. For this case, altitude, air speed, and distance are the necessary inputs. If the user does not specify an altitude, it will be taken automatically from the last value in the previous segment. These inputs must be specified in some way for the mission segment to be evaluated. They are shown below as well:</p> - -<div class="highlighter-rouge"><div class="highlight"><pre class="highlight"><code>self.altitude = None -self.air_speed = 10. * Units['km/hr'] -self.distance = 10. * Units.km -</code></pre></div></div> - -<p>The other set of segment specific initial values are the values used for solving the segment (typically this means satisfying a force balance at every evaluation point). These can be changed by the user if needed, but the default values should perform fine for most cases.</p> - -<div class="highlighter-rouge"><div class="highlight"><pre class="highlight"><code>self.state.unknowns.throttle = ones_row(1) * 0.5 -self.state.unknowns.body_angle = ones_row(1) * 0.0 -self.state.residuals.forces = ones_row(2) * 0.0 -</code></pre></div></div> - -<p>Here throttle and body angle are the unknowns, and the values shown here are the values they will start at. The residuals will be computed based on these unknowns, so their initial value is not important. Instead they are initialized just to create the necessary data structure. The ones_row line will create a numpy array with the number of elements needed for evaluation.</p> - -<h3 id="evaluation-details">Evaluation Details</h3> - -<p>Most of the missions in SUAVE, including this one, are broken into several points in time based on a Chebyshev polynomial. This causes the points to be closer together at either end of the segment. The choice of a Chebyshev polynomial (which creates cosine spacing) provides better convergence and smoothness properties versus other methods such as linear spacing.</p> - -<p><img src="http://suave.stanford.edu/images/drag_components_2.png" width="800" height="234" /></p> - -<p>At each of these points the aerodynamic analysis is queried to find CL and CD, which are then converted to lift and drag. These values will be dependent on the body angle unknown and other aerodynamic parameters. Thrust is found from the vehicle’s energy network, which is dependent on the throttle unknown. A weight is determined by looking at the initial weight and subsequent mass rate (typically corresponding with fuel burn). In this cruise segment, these forces are summed in 2D and the results are put in the residuals. The functions needed to arrive these forces are found in the Update Conditions section of the Analysis file. This section is also shown below in one of the steps to create a new mission.</p> - -<p>Once the evaluation process has been performed at all points, the unknowns and residuals are fed back to the solve routine, which in this case is scipy’s fsolve. The file that performs this process is <a href="https://github.com/suavecode/SUAVE/blob/develop/trunk/SUAVE/Methods/Missions/Segments/converge_root.py">here</a>. This routine continues evaluating the points until convergence is reached. Once this happens, post processing is done to put the data in the results output.</p> - -<h3 id="using-multiple-segments">Using Multiple Segments</h3> - -<p>Multiple segments can be run sequentially by appending them in the desired order. Examples of this are in all the tutorial files that have an aircraft fly a full mission. In addition, the full mission can be run simultaneously will all segment constraints used together. If you are interested in doing something like this, please ask us about it on our <a href="/forum">forum</a>.</p> - -<h4 id="process-summary">Process Summary</h4> - -<p>Mission Setup</p> - -<ul> - <li>Initializes default values for unknowns</li> - <li>Initializes set of functions used to determine residuals</li> - <li>Reads user input for segment parameters</li> - <li>Adds the analysis group to be used (including the vehicle and items like atmosphere)</li> - <li>Appends segments in order</li> -</ul> - -<p>Evaluate</p> - -<ul> - <li>Varies unknowns until residual convergence is reached using scipy’s fsolve</li> - <li>Repeats process for each segment until full mission is complete</li> -</ul> - -<h3 id="adding-new-mission-segments">Adding New Mission Segments</h3> - -<p>The segment described above uses two unknowns to solve force residuals in two dimensions. This general setup works well for many problems of interest, but SUAVE is designed to accommodate other mission analysis types as well. A user may want to add control surface deflection and solve for moments as well, or look at forces in all three dimensions.</p> - -<p>In addition, a user may want to modify how the mission is flown, as is done with the many other segments currently available. They may want to modify how the mission is solved, such as is done in our single point evaluation segments where finite differencing is not relevant.</p> - -<p>Here we will explain the process of modifying our constant speed constant rate climb segment to be constant throttle constant speed. This still uses 2D force balance but changes the profile. There are four functions that are modified here. The first is shown below. The functions can be found in <a href="">here</a> and <a href="">here</a></p> - -<div class="highlighter-rouge"><div class="highlight"><pre class="highlight"><code>def initialize_conditions(segment,state): - - # unpack - climb_rate = segment.climb_rate - air_speed = segment.air_speed - alt0 = segment.altitude_start - altf = segment.altitude_end - t_nondim = state.numerics.dimensionless.control_points - conditions = state.conditions - - # check for initial altitude - if alt0 is None: - if not state.initials: raise AttributeError('initial altitude not set') - alt0 = -1.0 * state.initials.conditions.frames.inertial.position_vector[-1,2] - - # discretize on altitude - alt = t_nondim * (altf-alt0) + alt0 - - # process velocity vector - v_mag = air_speed - v_z = -climb_rate # z points down - v_x = np.sqrt( v_mag**2 - v_z**2 ) - - # pack conditions - conditions.frames.inertial.velocity_vector[:,0] = v_x - conditions.frames.inertial.velocity_vector[:,2] = v_z - conditions.frames.inertial.position_vector[:,2] = -alt[:,0] # z points down - conditions.freestream.altitude[:,0] = alt[:,0] # positive altitude in this context -</code></pre></div></div> - -<p>This function initializes speed and altitude based on the given climb rate, airspeed, and altitude end points. t_nondim gives nondimensional time in cosine spacing from 0 to 1 in order to pick the values at the points to be evaluated. Unfortunately, when we use constant throttle we cannot know beforehand exactly how altitude (or climb rate in this case) will vary with time, so altitude cannot be spaced with this method. Instead a different function is used to initialize conditions:</p> - -<div class="highlighter-rouge"><div class="highlight"><pre class="highlight"><code>def initialize_conditions(segment,state): - - # unpack - throttle = segment.throttle - air_speed = segment.air_speed - alt0 = segment.altitude_start - altf = segment.altitude_end - t_nondim = state.numerics.dimensionless.control_points - conditions = state.conditions - - # check for initial altitude - if alt0 is None: - if not state.initials: raise AttributeError('initial altitude not set') - alt0 = -1.0 * state.initials.conditions.frames.inertial.position_vector[-1,2] - - # pack conditions - conditions.propulsion.throttle[:,0] = throttle - conditions.frames.inertial.velocity_vector[:,0] = air_speed # start up value -</code></pre></div></div> - -<p>Here only the throttle and air speed are loaded in, and discretization of other values will need to occur later so that it is part of the iteration loop. This requires a new function that updates the altitude differentials.</p> - -<div class="highlighter-rouge"><div class="highlight"><pre class="highlight"><code>def update_differentials_altitude(segment,state): - - # unpack - t = state.numerics.dimensionless.control_points - D = state.numerics.dimensionless.differentiate - I = state.numerics.dimensionless.integrate - - - # Unpack segment initials - alt0 = segment.altitude_start - altf = segment.altitude_end - conditions = state.conditions - - r = state.conditions.frames.inertial.position_vector - v = state.conditions.frames.inertial.velocity_vector - - # check for initial altitude - if alt0 is None: - if not state.initials: raise AttributeError('initial altitude not set') - alt0 = -1.0 * state.initials.conditions.frames.inertial.position_vector[-1,2] - - # get overall time step - vz = -v[:,2,None] # Inertial velocity is z down - dz = altf- alt0 - dt = dz / np.dot(I[-1,:],vz)[-1] # maintain column array - - # Integrate vz to get altitudes - alt = alt0 + np.dot(I*dt,vz) - - # rescale operators - t = t * dt - - # pack - t_initial = state.conditions.frames.inertial.time[0,0] - state.conditions.frames.inertial.time[:,0] = t_initial + t[:,0] - conditions.frames.inertial.position_vector[:,2] = -alt[:,0] # z points down - conditions.freestream.altitude[:,0] = alt[:,0] # positive altitude in this context - - return -</code></pre></div></div> - -<p>In this function, t, D, and I are numpy arrays that allow approximate differentiation and integration. Since the total time is not known without determining the climb rate, we must first determine the time required to reach the final altitude. The line <code class="highlighter-rouge">dt = dz / np.dot(I[-1,:],vz)[-1]</code> does this with the integrator providing the amount of altitude gained if the velocities were spread across just one second instead of the full segment time. This gives the scaling quantity <code class="highlighter-rouge">dt</code> that is then used to get the altitude at every point in <code class="highlighter-rouge">alt = alt0 + np.dot(I*dt,vz)</code>. The values for altitude are then are then packed for use in other functions.</p> - -<p>The above allows us to deal with discretization without a known profile, but we also must calculate the velocity in order to use this. This is done with another added function.</p> - -<div class="highlighter-rouge"><div class="highlight"><pre class="highlight"><code>def update_velocity_vector_from_wind_angle(segment,state): - - # unpack - conditions = state.conditions - v_mag = segment.air_speed - alpha = state.unknowns.wind_angle[:,0][:,None] - theta = state.unknowns.body_angle[:,0][:,None] - - # Flight path angle - gamma = theta-alpha - - # process - v_x = v_mag * np.cos(gamma) - v_z = -v_mag * np.sin(gamma) # z points down - - # pack - conditions.frames.inertial.velocity_vector[:,0] = v_x[:,0] - conditions.frames.inertial.velocity_vector[:,2] = v_z[:,0] - - return conditions -</code></pre></div></div> - -<p>This uses our new set of unknowns to determine the velocities.</p> - -<p>Additionally, since the unknowns are different we must change the function that unpacks them. Wind angle does not need to be stored so it is not included here.</p> - -<div class="highlighter-rouge"><div class="highlight"><pre class="highlight"><code>def unpack_body_angle(segment,state): - - # unpack unknowns - theta = state.unknowns.body_angle - - # apply unknowns - state.conditions.frames.body.inertial_rotations[:,1] = theta[:,0] -</code></pre></div></div> - -<p>We now add these functions to the segment process list.</p> - -<div class="highlighter-rouge"><div class="highlight"><pre class="highlight"><code> # -------------------------------------------------------------- - # Initialize - before iteration - # -------------------------------------------------------------- - initialize = self.process.initialize - - initialize.expand_state = Methods.expand_state - initialize.differentials = Methods.Common.Numerics.initialize_differentials_dimensionless - initialize.conditions = Methods.Climb.Constant_Throttle_Constant_Speed.initialize_conditions - initialize.velocities = Methods.Climb.Constant_Throttle_Constant_Speed.update_velocity_vector_from_wind_angle - initialize.differentials_altitude = Methods.Climb.Constant_Throttle_Constant_Speed.update_differentials_altitude -</code></pre></div></div> - -<p>and</p> - -<div class="highlighter-rouge"><div class="highlight"><pre class="highlight"><code> # Unpack Unknowns - iterate.unknowns = Process() - iterate.unknowns.mission = Methods.Climb.Constant_Throttle_Constant_Speed.unpack_body_angle - - # Update Conditions - iterate.conditions = Process() - iterate.conditions.velocities = Methods.Climb.Constant_Throttle_Constant_Speed.update_velocity_vector_from_wind_angle - iterate.conditions.differentials_a = Methods.Climb.Constant_Throttle_Constant_Speed.update_differentials_altitude - iterate.conditions.differentials_b = Methods.Common.Numerics.update_differentials_time - iterate.conditions.acceleration = Methods.Common.Frames.update_acceleration - iterate.conditions.altitude = Methods.Common.Aerodynamics.update_altitude - iterate.conditions.atmosphere = Methods.Common.Aerodynamics.update_atmosphere - iterate.conditions.gravity = Methods.Common.Weights.update_gravity - iterate.conditions.freestream = Methods.Common.Aerodynamics.update_freestream - iterate.conditions.orientations = Methods.Common.Frames.update_orientations - iterate.conditions.aerodynamics = Methods.Common.Aerodynamics.update_aerodynamics - iterate.conditions.stability = Methods.Common.Aerodynamics.update_stability - iterate.conditions.propulsion = Methods.Common.Energy.update_thrust - iterate.conditions.weights = Methods.Common.Weights.update_weights - iterate.conditions.forces = Methods.Common.Frames.update_forces - iterate.conditions.planet_position = Methods.Common.Frames.update_planet_position -</code></pre></div></div> - -<p>If you have any questions that are not answered in other tutorials or the FAQ please ask on our <a href="/forum">forum</a> page. This is also the place to go if you want help building a more elaborate evaluation, such as one that includes moments.</p> - - Sat, 07 Jan 2017 05:25:00 -0800 - http://localhost:4000/guides/mission.html - http://localhost:4000/guides/mission.html - - - documentation - - blog - - - - - Energy Networks - <p>##Energy Networks -Energy networks are really a fancy name for your propulsion system. The reason we call them a network rather than “engine” or the like is that it encompasses far more than that. These “energy networks” are the complex systems that future aircraft will incorporate that can reduce or eliminate fuel burn. For example if you have a hybrid gas-electric aircraft you don’t have just an engine. You have an engine, a motor, batteries, a generator, a gearbox, a propeller or ducted fan, wiring, electronics… and that doesn’t include the parts inside the internal combustion engine. Modeling these systems completely is essential in designing such a vehicle.</p> - -<p>To do this we depart from the typical SUAVE structure of analyses and methods. This was done because we want to look at each component of the network individually. All components behave in their own ways. The purpose of the network is to link together every component in the system to work together.</p> - -<h3 id="file-structure">File Structure</h3> -<p>One of the biggest sources of confusion for energy networks is the file structure. The files for every part of a network are located at trunk/SUAVE/<strong>Components/Energy</strong>. Within that we have several subfolders.</p> - -<h4 id="converters">/Converters</h4> -<p>Converters are defined as component that takes energy or power from one form to another. It could be electrical to mechanical, or even chemical to mechanical, etc.. Examples in this folder include a motor, a solar panel, and the compressor section of a jet engine.</p> -<h4 id="distributors">/Distributors</h4> -<p>Distributors move power from one part of the network to another. The common use of this is an electronic speed controller for a small UAV.</p> -<h4 id="networks">/Networks</h4> -<p>This is where all the “Network” scripts that tie together all of the pieces are kept. Examples in here are a turbofan network.</p> -<h4 id="peripherals">/Peripherals</h4> -<p>Peripherals are items that rely on the network but do not produce thrust or power for the vehicle. For example, avionics require electricity which must be accounted for.</p> -<h4 id="processes">/Processes</h4> -<p>Processes are non tangible parts of a network that are necessary. For example the process is thrust. This function is useful for jet engines to combine and dimensionalize the final thrust once all the components are combined in the network.</p> -<h4 id="storages">/Storages</h4> -<p>Storages, for now, include batteries. However, in the future we could have fuel tanks here. Currently fuel is only handled as a mass variation.</p> - -<h3 id="component-example">Component Example</h3> -<p>Below is a simple example of the most basic energy component in SUAVE. All energy components are classes. The A solar panel is a converter since it converts a photonic flux calculated by a solar radiation model and converts it to a power.</p> - -<div class="highlighter-rouge"><div class="highlight"><pre class="highlight"><code># Solar_Panel.py -# -# Created: Jun 2014, E. Botero -# Modified: Jan 2016, T. MacDonald - -# ---------------------------------------------------------------------- -# Imports -# ---------------------------------------------------------------------- - -# suave imports -import SUAVE - -from SUAVE.Components.Energy.Energy_Component import Energy_Component - -# ---------------------------------------------------------------------- -# Solar_Panel Class -# ---------------------------------------------------------------------- -class Solar_Panel(Energy_Component): - - def __defaults__(self): - self.area = 0.0 - self.efficiency = 0.0 - - def power(self): - - # Unpack - flux = self.inputs.flux - efficiency = self.efficiency - area = self.area - - p = flux*area*efficiency - - # Store to outputs - self.outputs.power = p - - return p -</code></pre></div></div> - -<p>These classes contain functions that simulate a process. Multiple functions can exist within a component. This component has defaults, inputs, and outputs. Defaults are provided that give the user an idea of what the fixed parameters of the component are. These values are set when initializing a vehicle. This is the recipe that all energy components are built off.</p> - -<h3 id="network-scripts">Network Scripts</h3> -<p>Network scripts are the link between these components. The network script allows you to reconfigure the connection between components to create your dream propulsion system. These must be logically created as components have set inputs and outputs. For example, you can’t magically go from a battery to a propeller without anything in between. Some knowledge of the inputs and outputs are necessary, however they’re generally quite intuitive. One interesting avenue for SUAVE is that you can create networks of networks.</p> - -<p>The linking process works like this:</p> - -<div class="highlighter-rouge"><div class="highlight"><pre class="highlight"><code> # step 1 - solar_flux.solar_radiation(conditions) - # link - solar_panel.inputs.flux = solar_flux.outputs.flux - # step 2 - solar_panel.power() - # link - solar_logic.inputs.powerin = solar_panel.outputs.power -</code></pre></div></div> - -<p>Notice the first step above is to calculate the solar radiation. Once the solar radiation is calculated the components are linked and step 2 can continue with the the power being calculated. From there a solar logic component will use that power.</p> - -<p>The other main hallmark of a network is that they are called at every point in the mission to calculate the state of the system. Given some <em>conditions</em> data that defines the state of the vehicle the components must provide back to the mission being solved a thrust force and a mass rate. Other outputs can be stored back to conditions, however a thrust and a mass rate must be returned.</p> - -<h3 id="vehicle-script-setup-of-a-network">Vehicle Script Setup of a Network</h3> - -<p>Here we will provide a snippet of the turbofan setup for a B737.</p> - -<div class="highlighter-rouge"><div class="highlight"><pre class="highlight"><code># ------------------------------------------------------------------ -# Component 3 - Low Pressure Compressor - -# instantiate -compressor = SUAVE.Components.Energy.Converters.Compressor() -compressor.tag = 'low_pressure_compressor' - -# setup -compressor.polytropic_efficiency = 0.91 -compressor.pressure_ratio = 1.14 - -# add to network -turbofan.append(compressor) -</code></pre></div></div> - -<p>In the above example, a compressor is added to the network. The compressor is tagged as the low_pressure_compressor to distinguish it from the high pressure compressor. The polytropic efficiency and pressure ratio are set. Finall it is appended to the network.</p> - - Fri, 06 Jan 2017 05:25:00 -0800 - http://localhost:4000/guides/energy_structure.html - http://localhost:4000/guides/energy_structure.html - - - documentation - - blog - - - - - Optimization Structure - <h2 id="optimization-code-structure">Optimization Code Structure</h2> - -<p>This is an overview of how optimization is done in SUAVE. A specific tutorial case is also available <a href="/guides/regional_jet_optimization.html">here</a>.</p> - -<h3 id="nexus-class">Nexus Class</h3> - -<p>The Nexus class is the underlying data structure that is used for optimization. It is created to hold all data and functionality needed to link together optimizers and the various analysis modules in SUAVE. Detailed information on each of the functions can be found on our <a href="/doxygen">doxygen page</a>.</p> - -<h3 id="standard-optimization-file-structure">Standard Optimization File Structure</h3> - -<p>These are the standard files that are used in the optimization process. They are typically stored as Optimize.py, Vehicle.py, Analysis.py, Mission.py, Procedure.py, and Plot_Mission.py. These names can be changed if desired.</p> - -<h4 id="optimize">Optimize</h4> - -<p>This is the top level file that is run to perform the optimization. Inputs, objective, constraints, and aliases are specified here. The inputs have an initial value, bounds, a scaling factor, and the units used. This provides later functions with the information needed to vary the parameters. Units.less indicates a unitless quantity. SI units are the default in SUAVE’s internal calculations, so Units.meter will not modify the internal value, while something like Units.foot will.</p> - -<div class="highlighter-rouge"><div class="highlight"><pre class="highlight"><code>problem.inputs = np.array([ - [ 'wing_area' , 125. , ( 120. , 180. ) , 100. , Units.meter**2], - [ 'aspect_ratio' , 3.3 , ( 2.0 , 6.0 ) , 10. , Units.less], -]) -</code></pre></div></div> - -<p>Constraints and the objective are similar. Both have scaling quantities and constraints also have bounds.</p> - -<div class="highlighter-rouge"><div class="highlight"><pre class="highlight"><code>problem.constraints = np.array([ - [ 'design_range_fuel_margin', '&gt;', 0., 1E-1, Units.less] -]) - -problem.objective = np.array([ - ['fuel_burn_rate', 1., Units.kg/Units.s] -]) -</code></pre></div></div> - -<p>Finally we have aliases. This provides the optimization process with the position of the various parameters in the data structure. Aliases are used so that short names can be used for variables and a single variable can control multiple items in the data structure. Controlling multiple items can be important if different vehicle configurations are used at different points in the mission, and one of the vehicle parameters should change in the same way for all of the configurations. We can use * as a wildcard. This is used below to change the aspect ratio of the main wing in every vehicle configuration.</p> - -<div class="highlighter-rouge"><div class="highlight"><pre class="highlight"><code>problem.aliases = [ - [ 'wing_area' , ['vehicle_configurations.base.wings.main_wing.areas.reference', - 'vehicle_configurations.base.reference_area']], - [ 'aspect_ratio' , 'vehicle_configurations.*.wings.main_wing.aspect_ratio' ], - [ 'fuel_burn_rate' , 'summary.fuel_burn_rate' ], -] -</code></pre></div></div> - -<p>This file then specifies the configurations, analyses, missions, and procedure that will be used. This are typically contained in separate files and more details on each are below. Once all of this is specified, the desired optimizer is called with the nexus class created by this setup.</p> - -<h4 id="vehicle-setup">Vehicle Setup</h4> - -<p>This contains the vehicle information such as geometric data and configurations. It is the same as the vehicle setup used for basic analysis purposes.</p> - -<h4 id="analysis-setup">Analysis Setup</h4> - -<p>This contains information on what analyses should be run for the vehicle. For example if correlation-based aerodynamics or AVL should be used for computations. It requires vehicle information from the previous step.</p> - -<h4 id="mission-setup">Mission Setup</h4> - -<p>This is also the same as the standard mission setup. It determines how the mission will be flown. It requires analysis information from the previous step.</p> - -<h4 id="procedure">Procedure</h4> - -<p>This is an optimization specific file that determines how the vehicle, analysis, or mission is modified with the input values in the optimization and also runs the mission. For example, changing the wing area will usually require changes to other wing parameters, such as root chord length. This module reads the new inputs and changes other values accordingly based on user specified processes.</p> - -<h4 id="plotting">Plotting</h4> - -<p>This function is not necessary to the optimization, but is often included in the files used and is added to the optimize main call as a way to visualize the results.</p> - -<h3 id="optimizer-interface">Optimizer Interface</h3> - -<p>The other step that must be taken to perform an optimization is to convert the standardized input above into values that can be used by the selected optimizer. This is done through a separate script for each optimizer, all of which are found in the <a href="doxygen_link_here">optimization folder</a>.</p> - -<p>For example, if we are using PyOpt to optimize, we might use <code class="highlighter-rouge">output = pyopt_setup.Pyopt_Solve(problem,solver='SNOPT')</code> in the main function of the top level optimizer. This function reads the inputs, constraints, and objective and converts them to a format that the selected optimizer (SNOPT here) can understand.</p> - -<h3 id="evaluation-process">Evaluation Process</h3> - -<p>This shows the typical evaluation process, including where items like inputs and aliases are used. This chart assumes a single objective call, but some optimizers will include calls such as <code class="highlighter-rouge">all_constraints</code> which require another evaluation. If the evaluation is a duplicate, data from the previous evaluation will be used instead of stepping through the procedure again.</p> - -<p> </p> - -<p><img src="http://suave.stanford.edu/images/opt_flow.png" width="600" height="338" /></p> - -<p> </p> - -<h3 id="incorporating-multi-fidelity">Incorporating Multi-fidelity</h3> - -<p>Multiple levels of fidelity are designed to be relatively easy to incorporate in SUAVE, but there are still a few things to keep in mind. First, the chosen optimizer must support multi-fidelity and be able to change the <code class="highlighter-rouge">nexus.fidelity_level</code> value. Once this is done, it is also important to remember that the mission is set up based on the analyses. This means that if a change is made to the analyses then the mission must be rebuilt with the new settings. As an example, code below for changing the analysis level is shown. This is a function that has been added to the procedure file.</p> - -<div class="highlighter-rouge"><div class="highlight"><pre class="highlight"><code>def set_fidelity_level(nexus): - - if nexus.has_key('fidelity_level') == False: - print 'Fidelity level not set, defaulting to 1' - nexus.fidelity_level = 1 - - if nexus.fidelity_level == 2: - aerodynamics = SUAVE.Analyses.Aerodynamics.Supersonic_OpenVSP_Wave_Drag() - aerodynamics.settings.number_slices = 20 - aerodynamics.settings.number_rotations = 10 - elif nexus.fidelity_level == 1: - aerodynamics = SUAVE.Analyses.Aerodynamics.Supersonic_Zero() - else: - raise ValueError('Selected fidelity level not supported') - aerodynamics.geometry = copy.deepcopy(nexus.vehicle_configurations.base) - nexus.analyses.base.append(aerodynamics) - - nexus.missions = mission_as2.setup(nexus.analyses) - - return nexus -</code></pre></div></div> - -<p>Here we see that <code class="highlighter-rouge">nexus.missions</code> has been updated in addition to <code class="highlighter-rouge">nexus.analyses</code>, since failing to do this would have the mission run with the previous analysis settings.</p> - -<h3 id="key-functions-in-the-optimizer-setup">Key Functions in the Optimizer Setup</h3> - -<p>We briefly mentioned how optimization parameters would need to be converted so that they could run with a particular optimizer. Here we show how this is managed and show which functions are likely to be useful in building a new optimizer setup.</p> - -<p>The key items that will be needed for most optimizers are shown below, taken from the PyOpt setup:</p> - -<div class="highlighter-rouge"><div class="highlight"><pre class="highlight"><code>inp = problem.optimization_problem.inputs -obj = problem.optimization_problem.objective -con = problem.optimization_problem.constraints - -# Set inputs -nam = inp[:,0] # Names -ini = inp[:,1] # Initials -bnd = inp[:,2] # Bounds -scl = inp[:,3] # Scale -typ = inp[:,4] # Type -</code></pre></div></div> - -<p>These can be scaled with two helper functions that are part of the SUAVE distribution:</p> - -<div class="highlighter-rouge"><div class="highlight"><pre class="highlight"><code>from SUAVE.Optimization import helper_functions as help_fun - -bnd_constraints = help_fun.scale_const_bnds(con) -scaled_constraints = help_fun.scale_const_values(con,bnd_constraints) -x = ini/scl -</code></pre></div></div> - -<p>What happens next is entirely dependent on what optimizer you want to use. Some may require that constraint bounds happen at 0 or are either &gt; or &lt;. However this setup is done, you will likely need to create a function that can accept the problem and inputs and give required outputs such as the objective value and constraints. In the PyOpt case, this is done with a simple wrapper and an added function:</p> - -<div class="highlighter-rouge"><div class="highlight"><pre class="highlight"><code>mywrap = lambda x:PyOpt_Problem(problem,x) -</code></pre></div></div> - -<p>…</p> - -<div class="highlighter-rouge"><div class="highlight"><pre class="highlight"><code>def PyOpt_Problem(problem,x): - - obj = problem.objective(x) - const = problem.all_constraints(x).tolist() - fail = np.array(np.isnan(obj.tolist()) or np.isnan(np.array(const).any())).astype(int) - - - print 'Inputs' - print x - print 'Obj' - print obj - print 'Con' - print const - - return obj,const,fail -</code></pre></div></div> - -<p>Please visit our <a href="/forum">forum</a> if you have any other questions on how the optimizer interface works or how to convert the values to what you need.</p> - - Thu, 05 Jan 2017 05:25:00 -0800 - http://localhost:4000/guides/optimization.html - http://localhost:4000/guides/optimization.html - - - documentation - - blog - - - - - Boeing 737-800 - <link rel="stylesheet" href="//cdn.jsdelivr.net/highlight.js/8.6/styles/default.min.css" /> - -<script src="//cdn.jsdelivr.net/highlight.js/8.6/highlight.min.js"></script> - -<script>hljs.initHighlightingOnLoad();</script> - -<h2 id="boeing-737-800-analysis-tutorial">Boeing 737-800 Analysis Tutorial</h2> - -<p>This tutorial shows how the user can setup a conventional configuration aircraft, a mission the aircraft is to fly, and then simulate the aircraft’s performance over the defined mission. The code is divided into a number of functions that are called from the main function.</p> - -<h3 id="steps-to-simulate-the-aircrafts-performance-over-a-mission-">Steps to simulate the aircraft’s performance over a mission :</h3> - -<p>1) Locate the folder where you have the tutorial repository. If using the command line, cd to this directory.</p> - -<p>2) Open the tut_mission_B737.py script in your favorite editor or IDE. The script is setup to run the B737 on its design mission. Run it in your IDE. If using the command line use the command</p> - -<pre><code class="python"> python tut_mission_B737_800.py </code></pre> - -<p>3) A few plots depicting the variation of the different aircraft performance parameters over the course of the mission are shown.</p> - -<h3 id="important-functions-">Important Functions :</h3> - -<p>The script is divided into a set of functions that setup different aspects of the modeling process. The important functions are:</p> - -<h4 id="vehicle_setup">vehicle_setup()</h4> -<p>function is where the aircraft’s geometry is specified.</p> - -<h5 id="setting-up-a-wing">Setting up a wing</h5> -<p>The code below shows how the main wing of the aircraft is set up. The basic geometric inputs that define the wing are specified. Then the wing is then appended to the vehicle, which is an instance of the aircraft class.</p> - -<p>In SUAVE units are identified through the use of a units package called Pint. Notice, that for the wing sweep that the units are specified in degrees through *Units.deg. To get results into a desired unit use /Units.deg.</p> - -<p>The wing sweep is defined as the sweep of the quarter chord. Additionally, a symmetric wing means that it is symmetric about the root, i.e. there is right and left side.</p> - -<pre><code class="python"> - wing = SUAVE.Components.Wings.Main_Wing() - wing.tag = 'main_wing' - - wing.aspect_ratio = 10.18 - wing.sweeps.quarter_chord = 25 * Units.deg - wing.thickness_to_chord = 0.1 - wing.taper = 0.1 - wing.span_efficiency = 0.9 - wing.spans.projected = 34.32 * Units.meter - wing.chords.root = 7.760 * Units.meter - wing.chords.tip = 0.782 * Units.meter - wing.chords.mean_aerodynamic = 4.235 * Units.meter - wing.areas.reference = 124.862 * Units['meters**2'] - wing.twists.root = 4.0 * Units.degrees - wing.twists.tip = 0.0 * Units.degrees - wing.origin = [13.61,0,-1.27] # meters - wing.vertical = False - wing.symmetric = True - wing.high_lift = True - wing.dynamic_pressure_ratio = 1.0 - -</code></pre> - -<h5 id="setting-up-the-fuselage">Setting up the fuselage</h5> -<p>Similar to the wing above, the code below illustrates how a fuselage can be added to the vehicle. Again the user is required to specify the basic fuselage geometric parameters and then add the fuselage object to the vehicle.</p> - -<pre><code class="python"> - fuselage = SUAVE.Components.Fuselages.Fuselage() - fuselage.tag = 'fuselage' - - fuselage.number_coach_seats = vehicle.passengers - fuselage.seats_abreast = 6 - fuselage.seat_pitch = 1 * Units.meter - fuselage.fineness.nose = 1.6 - fuselage.fineness.tail = 2. - fuselage.lengths.nose = 6.4 * Units.meter - fuselage.lengths.tail = 8.0 * Units.meter - fuselage.lengths.cabin = 28.85 * Units.meter - fuselage.lengths.total = 38.02 * Units.meter - fuselage.lengths.fore_space = 6. * Units.meter - fuselage.lengths.aft_space = 5. * Units.meter - fuselage.width = 3.74 * Units.meter - fuselage.heights.maximum = 3.74 * Units.meter - fuselage.effective_diameter = 3.74 * Units.meter - fuselage.areas.side_projected = 142.1948 * Units['meters**2'] - fuselage.areas.wetted = 446.718 * Units['meters**2'] - fuselage.areas.front_projected = 12.57 * Units['meters**2'] - fuselage.differential_pressure = 5.0e4 * Units.pascal # Maximum differential pressure - - fuselage.heights.at_quarter_length = 3.74 * Units.meter - fuselage.heights.at_three_quarters_length = 3.65 * Units.meter - fuselage.heights.at_wing_root_quarter_chord = 3.74 * Units.meter - - # add to vehicle - vehicle.append_component(fuselage) -</code></pre> - -<h5 id="setting-up-the-propulsion-system">Setting up the propulsion system</h5> - -<p>The aircraft uses a turbofan engine. This engine can be constructed piece by piece using the energy network framework. We instantiate the network as shown below.</p> - -<pre><code class="python"> - # ------------------------------------------------------------------ - # Turbofan Network - # ------------------------------------------------------------------ - - #instantiate the gas turbine network - turbofan = SUAVE.Components.Energy.Networks.Turbofan() - turbofan.tag = 'turbofan' - - # setup - turbofan.number_of_engines = 2 - turbofan.bypass_ratio = 5.4 - turbofan.engine_length = 2.71 * Units.meter - turbofan.nacelle_diameter = 2.05 * Units.meter - turbofan.origin = [[13.72, 4.86,-1.9],[13.72, -4.86,-1.9]] # meters - - #compute engine areas - turbofan.areas.wetted = 1.1*np.pi*turbofan.nacelle_diameter*turbofan.engine_length - - # working fluid - turbofan.working_fluid = SUAVE.Attributes.Gases.Air() - -</code></pre> - -<p>Next the components of the turbofan are initialized and added to the engine as shown in the energy networks section. The turbofan is composed of an inlet diffuser (nozzle), low and high pressure compressors, a combustor, a fan, a high and low pressure turbine, and exit nozzles for the core and the fan.</p> - -<p>Finally the network is added to the aircraft as shown below.</p> - -<pre><code class="python"> -#size the turbofan -turbofan_sizing(turbofan,mach_number,altitude) - -# add gas turbine network turbofan to the vehicle -vehicle.append_component(turbofan) - -# add gas turbine network gt_engine to the vehicle -vehicle.append_component(turbofan) -</code></pre> - -<h4 id="data-structure-visualization">Data Structure Visualization</h4> -<p>The data structure associated with the Boeing 737-800 can be visualized <a href="/guides/data_structures/B737.html">here</a>.</p> - -<p><a href="/guides/data_structures/B737.html"><img src="../images/b737_datastructure_preview.png" alt="Boeing 737 Data Structure" /></a></p> - -<p>This visualization shows the hierarchy of data in a SUAVE vehicle. Some of the values are defaulted, for example costs. This is because we are not performing cost analysis on the Boeing 737-800. Additionally, this snapshot of the data structure was taken prior to analysis. Therefore weights have not been calculated and are not part of the data. During the mission analysis component weights will be determined and weights will be populated.</p> - -<h4 id="configs_setup">configs_setup()</h4> -<p>The aircraft geometry created is converted into configurations that can be used to make simple modifications to the geometric parameters while not modifying the aircraft geometry completely. An example of the use of this feature is when high-lift devices need to be deployed during landing and takeoff. Thus a landing and takeoff configuration can be added as shown below and then during say the flaps and slats settings can be set differently for each of the configurations.</p> - -<pre><code class="python"> - # ------------------------------------------------------------------ - # Cruise Configuration - # ------------------------------------------------------------------ - config = SUAVE.Components.Configs.Config(base_config) - config.tag = 'cruise' - configs.append(config) - - # ------------------------------------------------------------------ - # Takeoff Configuration - # ------------------------------------------------------------------ - config = SUAVE.Components.Configs.Config(base_config) - config.tag = 'takeoff' - config.wings['main_wing'].flaps.angle = 20. * Units.deg - config.wings['main_wing'].slats.angle = 25. * Units.deg - config.max_lift_coefficient_factor = 1. - - configs.append(config) -</code></pre> - -<h4 id="mission_setup">mission_setup()</h4> -<p>To modify the baseline mission that the aircraft flies, go to the mission_setup() function and add or delete segments of the mission</p> - -<pre><code class="python"> - segment = Segments.Cruise.Constant_Speed_Constant_Altitude(base_segment) - segment.tag = "cruise" - - segment.analyses.extend( analyses.cruise ) - - segment.air_speed = 230.412 * Units['m/s'] - segment.distance = 2490. * Units.nautical_miles - - # add to mission - mission.append_segment(segment) -</code></pre> - -<h4 id="base_analysis">base_analysis()</h4> -<p>Also to leverage SUAVE’s multifidelity capability and use a different fidelity analysis for any of the disciplines (aerodynamics,propulsion, stability, etc), the base_analysis function can be modified by switching out an analysis module for a different one.</p> - -<h3 id="other-functions-">Other Functions :</h3> - -<h4 id="main">main()</h4> - -<p>The main function is the driver function for the mission simulation. It calls the various routines in the appropriate order in order to set up the geometry and the mission, evaluate the performance of the aircraft over the mission and return the results.</p> - -<h4 id="full_setup">full_setup()</h4> - -<p>This function (called from the main() function) sets up the aircraft geometry, configs and the missions the aircraft is to be analysed for by calling the vehicle_setup, configs_setup, analyses_setup, mission_setup and missions_setup functions.</p> - -<h4 id="simple_sizing">simple_sizing()</h4> - -<p>The simple sizing function sizes the aircraft’s geometric components based on the geometric inputs specified by the user in the vehicle_setup() function.</p> - -<h4 id="base_analysis-1">base_analysis()</h4> - -<p>The method takes in the vehicle and assigns different analysis methods (for aero, propulsion, weights, stability) to the analyses object.</p> - -<h4 id="analyses_setup">analyses_setup()</h4> - -<p>This functions takes in the base analysis and sets up different analysis methods for different configurations.</p> - -<h4 id="missions_setup">missions_setup()</h4> - -<p>This method allows the user to set up a variety of missions that need to be evaluated for an aircraft.</p> - -<h4 id="plot_mission">plot_mission()</h4> - -<p>This is a post processing function that takes in the results data structure and generates the necessary plots.</p> - -<h3 id="results">RESULTS</h3> - -<p>The plots shown below should be generated if the mission analysis executes correctly. The results show the aerodynamic, propulsion and mission properties of the B737-800 for the defined mission.</p> - -<p><img src="/images/B737_mission.png" alt="B737 mission" /></p> - -<p><img src="/images/B737_aero.png" alt="B737 Aerodynamics" /></p> - -<p><img src="/images/B737_engine.png" alt="B737 Propulsion" /></p> - -<p><img src="/images/B737_drag.png" alt="B737 Drag" /></p> - -<h3 id="modifying-the-aircrafts-geometry-or-mission-">Modifying the Aircraft’s Geometry or Mission :</h3> - -<p>Suppose we want to simulate a high span variant of the B737-800. The span is increased to 40.0 m. We assume the wing chords, sweep, taper ratio, thickness to chord ratio remain the same. Thus changing the span only changes the aspect ratio and the wing area.</p> - -<p>Now we try to fly the aircraft at a lower cruise speed of 200m/s at a cruise altitude of 25000 ft</p> - -<p>1) To update the geometry, scroll to the vehicle_setup() function</p> - -<p>2) Modify the parameters of the main wing</p> - -<pre><code class="python"> -wing.aspect_ratio = 10.12 -wing.spans.projected = 40.0 * Units.meter -wing.areas.reference = 158.0 * Units['meters**2'] -</code></pre> - -<p>You may also need to update the reference area for the aircraft.</p> - -<pre><code class="python">vehicle.reference_area = 158.0 -</code></pre> - -<p>3) Update the mission parameters by moving to the mission_setup() function</p> - -<p>4) First update the end altitude of the final climb segment. Although the original script has the altitude stated in m, courtesy of the Units package it is easy to modify the altitude to 25,000ft without worrying about the units conversion as shown below.</p> - -<pre><code class="python">segment = Segments.Climb.Constant_Speed_Constant_Rate(base_segment) -segment.tag = "climb_3" - -segment.analyses.extend( analyses.cruise ) - -segment.altitude_end = 25000 * Units.ft -segment.air_speed = 226.0 * Units['m/s'] -segment.climb_rate = 3.0 * Units['m/s'] - -mission.append_segment(segment) -</code></pre> - -<p>5) Next update the cruise segment velocity to the new speed value</p> - -<pre><code class="python">segment = Segments.Cruise.Constant_Speed_Constant_Altitude(base_segment) -segment.tag = "cruise" - -segment.analyses.extend( analyses.cruise ) - -segment.air_speed = 200.0 * Units['m/s'] -segment.distance = 2490. * Units.nautical_miles - -# add to mission -mission.append_segment(segment) -</code></pre> - -<p>6) Now go back and run the mission for the updated geometry and mission using the steps specified in ‘Steps to run the aircraft on a mission’</p> - - - Sun, 14 Feb 2016 05:25:00 -0800 - http://localhost:4000/guides/boeing_737-800.html - http://localhost:4000/guides/boeing_737-800.html - - - guides - - blog - - - - - Concorde - <link rel="stylesheet" href="//cdn.jsdelivr.net/highlight.js/8.6/styles/default.min.css" /> - -<script src="//cdn.jsdelivr.net/highlight.js/8.6/highlight.min.js"></script> - -<script>hljs.initHighlightingOnLoad();</script> - -<h2 id="concorde-tutorial">Concorde Tutorial</h2> - -<p>This tutorial gives an overview of changes made to the setup to evaluate a supersonic mission.</p> - -<h3 id="aerodynamics-module">Aerodynamics Module:</h3> - -<p>To allow aerodynamic calculations in supersonic flight, we use the zero fidelity supersonic module. This is quite easy to swap with the subsonic zero fidelity model. This model and the zero fidelity subsonic module are in the same directory, so they can be switched by changing a single line in the analysis section:</p> - -<div class="highlighter-rouge"><div class="highlight"><pre class="highlight"><code>aerodynamics = SUAVE.Analyses.Aerodynamics.Fidelity_Zero() -</code></pre></div></div> - -<p>to</p> - -<div class="highlighter-rouge"><div class="highlight"><pre class="highlight"><code>aerodynamics = SUAVE.Analyses.Aerodynamics.Supersonic_Zero() -</code></pre></div></div> -<p>The supersonic aerodynamics module can still handle the subsonic portions of the flight.</p> - -<h3 id="wing-additions">Wing Additions:</h3> - -<p>Some of the calculations are changed to account for different properties that are not automatically captured in the model.</p> - -<ul> - <li>Vortex lift is set to true. This causes the vortex lift module to add a CL increment to the aircraft.</li> - <li>High Mach is set to true. This changes the way that high subsonic compressibility drag is calculated and brings it more in line with Concorde behavior.</li> -</ul> - -<div class="highlighter-rouge"><div class="highlight"><pre class="highlight"><code> wing.vortex_lift = True -</code></pre></div></div> - -<div class="highlighter-rouge"><div class="highlight"><pre class="highlight"><code> wing.high_mach = True -</code></pre></div></div> - -<p>Note also that Concorde does not have a horizontal tail, so this is not included in the vehicle setup.</p> - -<h3 id="turbojet-module">Turbojet Module:</h3> - -<p>Since Concorde has a diverging nozzle that allows for supersonic outflow, a modified turbojet is used that can account for this. This turbojet component is again switched out with a single line.</p> - -<div class="highlighter-rouge"><div class="highlight"><pre class="highlight"><code>nozzle = SUAVE.Components.Energy.Converters.Supersonic_Nozzle() -</code></pre></div></div> - -<p>instead of</p> - -<div class="highlighter-rouge"><div class="highlight"><pre class="highlight"><code>nozzle = SUAVE.Components.Energy.Converters.Expansion_Nozzle() -</code></pre></div></div> - -<h3 id="mission-segments">Mission Segments:</h3> - -<p>The mission typically flown by Concorde calls for mission segments that are not utilized in the Boeing 737 case. These are Mach number dependent, and require different inputs from the segments previously given. The new mission segments are linear Mach constant rate (climb and descent). Both require a starting and ending Mach number, which will vary linearly in time over the descent. For an example, check the third climb segment:</p> - -<div class="highlighter-rouge"><div class="highlight"><pre class="highlight"><code>segment = Segments.Climb.Linear_Mach_Constant_Rate(base_segment) -segment.tag = "climb_3" - -segment.analyses.extend( analyses.cruise ) - -segment.altitude_end = 7.60 * Units.km -segment.mach_start = 0.64 -segment.mach_end = 1.0 -segment.climb_rate = 5.05 * Units['m/s'] -</code></pre></div></div> - -<h3 id="takeoff-and-landing-configuration">Takeoff and Landing Configuration</h3> - -<p>Since Concorde does not have flaps or slats, specific takeoff and landing configurations are not used.</p> - - Wed, 15 Jul 2015 07:25:00 -0700 - http://localhost:4000/guides/concorde.html - http://localhost:4000/guides/concorde.html - - - guides - - blog - - - - - Solar UAV - <link rel="stylesheet" href="//cdn.jsdelivr.net/highlight.js/8.6/styles/default.min.css" /> - -<script src="//cdn.jsdelivr.net/highlight.js/8.6/highlight.min.js"></script> - -<script>hljs.initHighlightingOnLoad();</script> - -<h2 id="introduction">Introduction</h2> - -<p>The purpose of this tutorial is to educate users on how to setup a preconfigured solar energy network to work with a high altitude solar UAV. In this tutorial it is assumed that the user has some familiarity with SUAVE having completed the fundamental tutorial for the Boeing 737-800. You will learn about setting up the following:</p> - -<ul> - <li>Solar missions,</li> - <li>Human powered/solar weight estimation,</li> - <li>Boundary layer transition</li> - <li>Solar panels,</li> - <li>Batteries,</li> - <li>Electric motors,</li> - <li>Propellers,</li> - <li>Electric network integration in a solar UAV</li> -</ul> - -<p>Because of the flexible nature of SUAVE, the approach shown is just one way to setup the UAV for analysis. By experimenting and eventually developing your own code you will be able to do far more than what is shown in this tutorial. The original script can be found in the tutorial repository as tut_solar_uav.py.</p> - -<h2 id="vehicle-and-mission">Vehicle and Mission</h2> - -<p>The vehicle is similar to the Qinetiq Zephyr but far larger at 40 meters in wing span and a weight of 200 kg. However, it does carry double the payload of the Zephyr at 5 kg and accounts for constant payload power usage. The battery energy density is set to an optimistic estimate of 450 Watt-hours per kg. Additionally, 90 percent of the wings are covered with solar panels that have a 25 percent efficiency.</p> - -<p>This mission exercises the methods developed for solar radiation estimation, propeller and motor integration, as well as the human powered aircraft weight estimation. The mission setup is a constant altitude cruise at 15 km at Mach 0.12 for about 24 hours. The location is over the California Bay Area during the summer solstice.</p> - -<h2 id="setup">Setup</h2> - -<p>This tutorial highlights the differences between setting up a typical aircraft like a Boeing 737 and a solar UAV.</p> - -<h3 id="mission-setup">Mission Setup</h3> - -<p>For a solar UAV, the starting location as well as the day and time are critical. So the first segment must be modified to include this information. It is important to note that the start times provided are in “Zulu” time or Greenwich Mean Time. This is typical for aircraft navigation to prevent time zone errors and ambiguity.</p> - -<pre><code class="python">segment.state.numerics.number_control_points = 64 -segment.start_time = time.strptime("Tue, Jun 21 11:30:00 2015", "%a, %b %d %H:%M:%S %Y",) -segment.altitude = 15.0 * Units.km -segment.mach = 0.12 -segment.distance = 3050.0 * Units.km -segment.battery_energy = vehicle.propulsors.network.battery.max_energy*0.2 #Set the battery charge to start -segment.latitude = 37.4300 -segment.longitude = -122.1700 -</code></pre> - -<p>Additionally, this mission is highly simplified. It consists of only one mission segment. To provide ample resolution the number of control points have been increased to 64.</p> - -<h3 id="structural-weight-sizing">Structural Weight Sizing</h3> - -<p>The vehicle sizing of the human powered aircraft or solar UAV requires the dimensions of the vehicle like in other weight estimation methods. However, it also requires information about the number of wing ribs and the number of end ribs. The end ribs are relevant for wing designs where the sections can come apart for transportation.</p> - -<pre><code class="python">wing.number_ribs = 26. -wing.number_end_ribs = 2. -</code></pre> - -<h3 id="wing-boundary-layer-transition">Wing Boundary Layer Transition</h3> - -<p>The transition location of the boundary layer can have a great impact on the drag of the wing. This is especially important in properly designed low Reynolds number flows when laminar flow can be extended for larger percentages of the surface. The code snippet below is how surfaces have transition points set. These are estimates provided from the designer based on experience.</p> - -<pre><code class="python">wing.transition_x_upper = 0.6 -wing.transition_x_lower = 1.0 -</code></pre> - -<h3 id="solar-panels">Solar Panels</h3> - -<p>The solar panel model is quite simple and only requires a capture area, an efficiency, and mass. In this case we assume that 90% of the wing area is covered in solar panels.</p> - -<pre><code class="python">panel.area = vehicle.reference_area * 0.9 -panel.efficiency = 0.25 -panel.mass_properties.mass = panel.area*(0.60 * Units.kg) -</code></pre> - -<h3 id="batteries">Batteries</h3> - -<p>The batteries are set up with knowledge of the mass of the battery and the specific energy. In this case a futuristic specific energy of 450 Watt-hr/kg is set for lithium ion type batteries. The resistance of the batteries is another important input to determine charging and discharging losses.</p> - -<pre><code class="python">bat = SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion() -bat.mass_properties.mass = 55.0 * Units.kg -bat.specific_energy = 450.*Units.Wh/Units.kg -bat.resistance = 0.05 -initialize_from_mass(bat,bat.mass_properties.mass) -net.battery = bat -</code></pre> - -<h3 id="propeller">Propeller</h3> - -<p>To setup the propeller we will actually design an optimized propeller. This is done through the methods provided by Adkins and Liebeck. The attributes of the propeller design are then seeded to the motor and network to accelerate convergence of the propeller and motor models.</p> - -<pre><code class="python">prop_attributes = Data() -prop_attributes.number_blades = 2.0 -prop_attributes.freestream_velocity = 40.0 # freestream m/s -prop_attributes.angular_velocity = 150. * Units['rpm'] -prop_attributes.tip_radius = 4.25 -prop_attributes.hub_radius = 0.05 -prop_attributes.design_Cl = 0.7 -prop_attributes.design_altitude = 14.0 * Units.km -prop_attributes.design_thrust = 0.0 -prop_attributes.design_power = 3500.0 -prop_attributes = propeller_design(prop_attributes) - -prop = SUAVE.Components.Energy.Converters.Propeller() -prop.prop_attributes = prop_attributes -net.propeller = prop -</code></pre> - -<h3 id="motor">Motor</h3> - -<p>This motor model relies on data that is generally available from motor manufacturers. This includes the resistance, no load current, and the speed constant. Additionally, any gearbox is specified here and basic information about the propeller is entered here to help inform the solver when converging the motor and propeller analyses.</p> - -<pre><code class="python">motor = SUAVE.Components.Energy.Converters.Motor() -motor.resistance = 0.008 -motor.no_load_current = 4.5 -motor.speed_constant = 120. * Units['rpm'] # RPM/volt converted to (rad/s)/volt -motor.propeller_radius = prop.prop_attributes.tip_radius -motor.propeller_Cp = prop.prop_attributes.Cp -motor.gear_ratio = 12. # Gear ratio -motor.gearbox_efficiency = .98 # Gear box efficiency -motor.expected_current = 160. # Expected current -motor.mass_properties.mass = 2.0 -net.motor = motor -</code></pre> - -<h2 id="running">Running</h2> - -<p>As you should be familiar with by now, running this script is just like any other.</p> -<pre><code class="bash">python tut_solar_uav.py -</code></pre> - -<h2 id="results">Results</h2> - -<p>If all went well the script ran and it provided you with more plots than you ever wanted. Here are some of the plots that were generated when we ran it:</p> - -<p><img src="/images/solar_flux.png" alt="solar_flux" /></p> - -<p><img src="/images/battery_charging.png" alt="battery charging" /></p> - -<p><img src="/images/battery_energy.png" alt="battery energy" /></p> - - - Thu, 18 Jun 2015 16:22:20 -0700 - http://localhost:4000/guides/solar_uav.html - http://localhost:4000/guides/solar_uav.html - - - guides - - blog - - - - - Payload Range Diagram - <h3 id="embraer-e-190-payload-range-diagram-tutorial">Embraer E-190 Payload Range Diagram Tutorial</h3> -<p>1) Locate the tutorial script folder.</p> - -<p>2) Open the test_payload_range.py script in your favorite editor or IDE.</p> - -<p>3) Similar to the B737-800 Tutorial, the setup is divided into steps.</p> - -<p>4) For the Payload Range Diagram, besides the vehicle and mission, the user must provide the following inputs:</p> - -<ul> - <li><strong>cruise_segment_tag</strong>: You must enter the tag of the segment which will have its length modified in order to comply with required fuel burn for each one of the payload range diagram points.</li> - <li><strong>reserves</strong>: This will be considered as a fixed fuel reserve for all the diagram points.</li> -</ul> - -<p>5) The tutorial presents the following definition:</p> - -<div class="highlighter-rouge"><div class="highlight"><pre class="highlight"><code># run payload diagram -cruise_segment_tag = "Cruise" -reserves = 1750. -payload_range_results = payload_range(vehicle,mission,cruise_segment_tag,reserves) -</code></pre></div></div> - -<p>6) First, let’s just run it as it is for now. Run the script in either the IDE or in a terminal as <code class="highlighter-rouge">python tut_payload_range.py</code></p> - -<p>7) After the calculations are completed, the payload diagram will be plotted and the data will be stored in a file named ‘PayloadRangeDiagram.dat’. This is in the folder where you run the script.</p> - -<p>8) You can try to modify vehicle and/or mission parameters and see how the payload range diagram is affected. For now, let’s add some drag counts to the airplane:</p> - -<ul> - <li>Locate and open the script test_mission_Embraer_E190_constThr.py, in the tutorial folder (this is the script that contains the vehicle and mission setups)</li> - <li>Locate <code class="highlighter-rouge">base_analysis()</code> and then the Aerodynamics Analysis text block (line 113)</li> - <li>Add 50 drag counts to the vehicle (line 115): <code class="highlighter-rouge">aerodynamics.settings.drag_coefficient_increment = 0.0050 </code></li> - <li>Rerun the script as before and notice the changes in the results.</li> -</ul> - -<p>9) Similarly the mission parameters can be changed. Again, this lets the user decide what changes they want to explore.</p> - - - Wed, 17 Jun 2015 16:22:21 -0700 - http://localhost:4000/guides/payload_range_diagram.html - http://localhost:4000/guides/payload_range_diagram.html - - - guides - - blog - - - - - Turbofan Network - <link rel="stylesheet" href="//cdn.jsdelivr.net/highlight.js/8.6/styles/default.min.css" /> - -<script src="//cdn.jsdelivr.net/highlight.js/8.6/highlight.min.js"></script> - -<script>hljs.initHighlightingOnLoad();</script> - -<h2 id="turbofan-modeling-tutorial">Turbofan Modeling Tutorial</h2> - -<p>This tutorial describes how the energy network framework in SUAVE can be used to build a model of a turbofan engine. Once this is clear to the user, understanding the setup of the other gasturbine models, the ducted fan and the turbojet will be much easier. The turbofan model is built with several turbofan components as its building blocks. These are then linked together through their inputs and outputs. The script to follow is the tut_mission_B737.py script that was used in the <a href="/guides/boeing_737-800.html">Boeing 737-800 Analysis Tutorial</a></p> - -<h3 id="setting-up-the-turbofan-model">Setting up the Turbofan model</h3> - -<p>First the turbofan energy network is instantiated. The parameters associated with the network as a whole are assigned.</p> - -<pre><code class="python"># ------------------------------------------------------------------ -# Turbofan Network -# ------------------------------------------------------------------ - -#instantiate the gas turbine network -turbofan = SUAVE.Components.Energy.Networks.Turbofan() -turbofan.tag = 'turbofan' - -# setup -turbofan.bypass_ratio = 5.4 -turbofan.number_of_engines = 2.0 -turbofan.engine_length = 2.5 -turbofan.nacelle_diameter = 1.580 - -# working fluid -turbofan.working_fluid = SUAVE.Attributes.Gases.Air() -</code></pre> - -<p>Then the different components are added</p> - -<h3 id="components">Components</h3> - -<p>The basic components used to model the turbofan are described below.</p> - -<h4 id="ram">Ram</h4> - -<p>The ‘Ram’ component is used to convert the freestream quantities that are passed into the turbofan network into stagnation quantities. As the turbofan network is based on a 1D gasdynamic analysis, most of the energy transfer across the different components are modelled as changes in the stagnation quantities. Thus the Ram component acts as a preprocessor converting the input conditions into quantities required by the network.</p> - -<pre><code class="python"># ------------------------------------------------------------------ -# Component 1 - Ram - -# to convert freestream static to stagnation quantities - -# instantiate -ram = SUAVE.Components.Energy.Converters.Ram() -ram.tag = 'ram' - -# add to the network -turbofan.append(ram) -</code></pre> - -<h4 id="nozzle">Nozzle</h4> - -<p>The ‘Nozzle’ component is used to model the inlet diffuser, the outlet fan, and the compressor nozzles as shown below.</p> - -<pre><code class="python"># ------------------------------------------------------------------ -# Component 2 - Inlet Nozzle - -# instantiate -inlet_nozzle = SUAVE.Components.Energy.Converters.Compression_Nozzle() -inlet_nozzle.tag = 'inlet_nozzle' - -# setup -inlet_nozzle.polytropic_efficiency = 0.98 -inlet_nozzle.pressure_ratio = 0.98 - -# add to network -turbofan.append(inlet_nozzle) - -# ------------------------------------------------------------------ -# Component 8 - Core Nozzle - -# instantiate -nozzle = SUAVE.Components.Energy.Converters.Expansion_Nozzle() -nozzle.tag = 'core_nozzle' - -# setup -nozzle.polytropic_efficiency = 0.95 -nozzle.pressure_ratio = 0.99 - -# add to network -turbofan.append(nozzle) - -# ------------------------------------------------------------------ -# Component 9 - Fan Nozzle - -# instantiate -nozzle = SUAVE.Components.Energy.Converters.Expansion_Nozzle() -nozzle.tag = 'fan_nozzle' - -# setup -nozzle.polytropic_efficiency = 0.95 -nozzle.pressure_ratio = 0.99 - -# add to network -turbofan.append(nozzle) -</code></pre> - -<h4 id="compressor">Compressor</h4> - -<p>Two compressors are used in the turbofan model, a low and a high pressure compressor.</p> - -<pre><code class="python"># ------------------------------------------------------------------ -# Component 3 - Low Pressure Compressor - -# instantiate -compressor = SUAVE.Components.Energy.Converters.Compressor() -compressor.tag = 'low_pressure_compressor' - -# setup -compressor.polytropic_efficiency = 0.91 -compressor.pressure_ratio = 1.14 - -# add to network -turbofan.append(compressor) - -# ------------------------------------------------------------------ -# Component 4 - High Pressure Compressor - -# instantiate -compressor = SUAVE.Components.Energy.Converters.Compressor() -compressor.tag = 'high_pressure_compressor' - -# setup -compressor.polytropic_efficiency = 0.91 -compressor.pressure_ratio = 13.415 - -# add to network -turbofan.append(compressor) -</code></pre> - -<h4 id="fan">Fan</h4> - -<p>A fan component is also added to the network. If you were to model a turbojet, the fan component and the fan nozzle would not be added but all the other components would remain the same.</p> - -<pre><code class="python"># ------------------------------------------------------------------ -# Component 10 - Fan - -# instantiate -fan = SUAVE.Components.Energy.Converters.Fan() -fan.tag = 'fan' - -# setup -fan.polytropic_efficiency = 0.93 -fan.pressure_ratio = 1.7 - -# add to network -turbofan.append(fan) -</code></pre> - -<h4 id="combustor">Combustor</h4> - -<p>The combustor component is where the the fuel to air ratio is computed. It is also used to compute the sfc and the thrust later in the network.</p> - -<pre><code class="python"># ------------------------------------------------------------------ -# Component 7 - Combustor - -# instantiate -combustor = SUAVE.Components.Energy.Converters.Combustor() -combustor.tag = 'combustor' - -# setup -combustor.efficiency = 0.99 -combustor.turbine_inlet_temperature = 1450 -combustor.pressure_ratio = 0.95 -combustor.fuel_data = SUAVE.Attributes.Propellants.Jet_A() - -# add to network -turbofan.append(combustor) -</code></pre> - -<h4 id="turbine">Turbine</h4> - -<p>The work done by the fan and the compressors is used to compute the turbine work required. This is used to compute the change in the stagnation quantities across the turbine.</p> - -<pre><code class="python"># ------------------------------------------------------------------ -# Component 5 - Low Pressure Turbine - -# instantiate -turbine = SUAVE.Components.Energy.Converters.Turbine() -turbine.tag='low_pressure_turbine' - -# setup -turbine.mechanical_efficiency = 0.99 -turbine.polytropic_efficiency = 0.93 - -# add to network -turbofan.append(turbine) - -# ------------------------------------------------------------------ -# Component 6 - High Pressure Turbine - -# instantiate -turbine = SUAVE.Components.Energy.Converters.Turbine() -turbine.tag='high_pressure_turbine' - -# setup -turbine.mechanical_efficiency = 0.99 -turbine.polytropic_efficiency = 0.93 - -# add to network -turbofan.append(turbine) -</code></pre> - -<h4 id="thrust">Thrust</h4> - -<p>The thrust component takes in the initial (inputs of the inlet nozzle) and final (exit of the fan and core exirt nozzles) stagnation quantities of the network and the fuel to air ratio and computes the specific fuel conspumption (sfc) and thrust generated by the network (turbofan engine).</p> - -<pre><code class="python"># ------------------------------------------------------------------ -# Component 10 - Thrust - -# to compute thrust - -# instantiate -thrust = SUAVE.Components.Energy.Processes.Thrust() -thrust.tag ='thrust' - -# setup -thrust.total_design =42383.01 - -# add to network -turbofan.thrust = thrust -</code></pre> - -<h3 id="sizing-the-turbofan">Sizing the Turbofan</h3> - -<p>Once the network is built, it is essential to size the engine with a set of sizing conditions. The sizing function ‘turbofan_sizing’ takes in the model of the turbofan and the mach number and the altitude for which the turbofan is sized. The sizing thrust is an engine/network property (defined in the ‘Setting up the Turbofan model’ section above). The function takes these quantities and computes the design mass flow rate through the components. Once sized, the network/engine can be added to the vehicle as shown in the B737 tutorial.</p> - -<pre><code class="python">#bypass ratio closer to fan - -#design sizing conditions -altitude = 35000.0*Units.ft -mach_number = 0.78 -isa_deviation = 0. - -# add to network -turbofan.thrust = thrust - -#size the turbofan (for thrust) -turbofan_sizing(turbofan,mach_number,altitude) - -#compute the turbofan diameter and engine length -#note that the second input is to maintain a common interface with other sizing methods -compute_turbofan_geometry(turbofan,None) -</code></pre> - - - Mon, 15 Jun 2015 07:20:03 -0700 - http://localhost:4000/guides/turbofan_network.html - http://localhost:4000/guides/turbofan_network.html - - - guides - - blog - - - - - Regional Jet Optimization - <link rel="stylesheet" href="//cdn.jsdelivr.net/highlight.js/8.6/styles/default.min.css" /> - -<script src="//cdn.jsdelivr.net/highlight.js/8.6/highlight.min.js"></script> - -<script>hljs.initHighlightingOnLoad();</script> - -<h3 id="regional-jet-optimization-tutorial">Regional Jet Optimization Tutorial</h3> -<p>This tutorial assumes familiarity with SUAVE and knowledge of the information in the Boeing 737-800 analysis tutorial. It provides a specific case of the more general information provided in the optimization structure tutorial, and some more information on how to modify the code for different uses.</p> - -<p>Some important files for the optimization problem can be seen below</p> - -<h3 id="important-files-">Important Files :</h3> - -<h4 id="optimizepy">Optimize.py:</h4> -<p>Defines the optimization framework of the problem, wherein one minimizes an assigned objective, subject to certain constraints, by altering some design variables.</p> - -<p>In order to ensure that the subfunctions can communicate with eachother, and that SUAVE can communicate with the external optimizer, a special data object called the “Nexus” is used. The nexus object contains all of the vehicles, missions, results, and other important information. It alters these values at each optimizer iteration, depending on the input parameters defined in Optimize.py.</p> - -<p>In this particular setup, there are two design variables: wing area and cruise altitude. The objective is fuel burn, and there is only one constraint: fuel margin. The default inputs are defined in the following lines.</p> - -<div class="highlighter-rouge"><div class="highlight"><pre class="highlight"><code># [ tag, initial, (lb,ub), scaling, units] -problem.inputs = np.array([ - [ 'wing_area' , 95., ( 90., 130.), 100., Units.meter**2], - [ 'cruise_altitude', 11., ( 9., 14.), 10., Units.km ], -]) -</code></pre></div></div> - -<p>Each input parameter takes in 5 values; a tag (an identification to communicate between the optimizer and SUAVE), an initial value, set of bounds, a scale factor (many optimizers tend to be more effective when the input values are of order 1), as well as the units used.</p> - -<p>The objective and constraints are defined in the lines below.</p> - -<div class="highlighter-rouge"><div class="highlight"><pre class="highlight"><code># [ tag, scaling, units ] -problem.objective = np.array([ - [ 'fuel_burn', 10000, Units.kg ] -]) - -# [ tag, sense, edge, scaling, units ] -problem.constraints = np.array([ - [ 'design_range_fuel_margin' , '&gt;', 0., 1E-1, Units.less], -]) -</code></pre></div></div> - -<p>Note that in this case, only a single constraint is used; Multiple constraints may be used using a list format, similar to the input variables.</p> - -<p>This file also defines the “aliasing,” i.e. how the design variables, constraints, and objective map to the variables used in Procedure.py (which is where the problem is evaluated). The aliases for this problem are defined in the lines below. Note that the first entry refers to the tag defined in either problem.inputs, problem.objective, or problem.constraints.</p> - -<div class="highlighter-rouge"><div class="highlight"><pre class="highlight"><code>problem.aliases = [ - [ 'wing_area' , ['vehicle_configurations.*.wings.main_wing.areas.reference', - 'vehicle_configurations.*.reference_area' ]], - [ 'cruise_altitude' , 'missions.base.segments.climb_5.altitude_end' ], - [ 'fuel_burn' , 'summary.base_mission_fuelburn' ], - [ 'design_range_fuel_margin' , 'summary.max_zero_fuel_margin' ], -] -</code></pre></div></div> - -<p>Note that, sometimes, a single input can map to multiple outputs, such as the “wing_area” design variable; in this case, use a list for the outputs, as seen above. The use of a wild card “*”, can also allow values to map to multiple outputs. Values to be outputted cannot contain wild cards as that would be ambiguous to an optimizer.</p> - -<h4 id="procedurepy">Procedure.py:</h4> -<p>This links everything together by defining the steps you would use to size and analyze the aircraft at each optimizer iteration.</p> - -<p>This file contains a number of subfunctions to alter the vehicle and mission. The function setup() instantiates the procedure, defining the functions that are called at each step of the optimizer in their order of execution.</p> - -<ol> - <li> - <p>simple_sizing() defines the geometry of the aircraft based on the input parameters (in this case, wing area and cruise altitude).</p> - </li> - <li> - <p>weights() determines the weight breakdown of the aircraft</p> - </li> - <li> - <p>mission() decides which missions are run at each step, as well as the design mission of the aircraft</p> - </li> - <li> - <p>post_process() handles the results from the missions, saving the constraints and objective value</p> - </li> -</ol> - -<p>Each step of the procedure takes the nexus object as an input, and returns the object as an output, ensuring that the data is available for handling.</p> - -<h4 id="vehiclespy">Vehicles.py:</h4> -<p>Initializes the vehicle (or vehicles if desired) used in the optimization problem. This includes two subfunctions: base_setup(), where the vehicle structure is itself defined, including the fuselage, wing, vertical and horizontal tails, and the propulsion system.</p> - -<p>configs_setup() takes in the vehicle that was defined in base_setup() and defines other configurations (such as takeoff and landing, which include different flap settings). This may be used to define other parameters, such as changing the sweep angle of a variable-sweep-wing at higher Mach Numbers, or changing a propulsion component.</p> - -<h4 id="missionspy">Missions.py:</h4> -<p>Initializes the missions that are run at each iteration. In this case, only a single mission is run.</p> - -<h4 id="analysespy">Analyses.py:</h4> -<p>Defines the set of features that are used in this particular problem (e.g. weights correlations, aerodynamics correlations, etc.).</p> - -<h4 id="plot_missionpy">Plot_Mission.py:</h4> -<p>Plots the mission outputs.</p> - -<h3 id="running-the-problem">Running the Problem:</h3> -<ol> - <li> - <p>Locate the tutorial script folder “Regional_Jet_Optimization.”</p> - </li> - <li> - <p>Open the Optimize.py script in a text editor or IDE. You will see this line near the top of main():</p> - - <p><code class="highlighter-rouge">output = problem.objective()</code></p> - </li> - <li> - <p>This runs the problem with the default inputs. Run the file using an IDE or type <code class="highlighter-rouge">python Optimize.py</code> in the command line. You should see a set of output plots.</p> - </li> -</ol> - -<h3 id="running-a-sweep-of-the-inputs">Running a Sweep of the Inputs</h3> -<p>Now try running a 2D sweep of the problem to observe the shape of the design space: comment <code class="highlighter-rouge">output = problem.objective</code> then uncomment the following (the next line down in the code).</p> - -<div class="highlighter-rouge"><div class="highlight"><pre class="highlight"><code>variable_sweep(problem) -</code></pre></div></div> - -<p>Then run the program again. This could take a few minutes. The results should look like the plot below.</p> - -<p><img src="/images/wing_area_v_cruise_altitude_v_fuel_burn_5_steps.png" alt="2D Sweep" /></p> - -<p>The labeled lines depict the fuel margin (i.e. fraction of the aircraft remaining weight that can be loaded with fuel). Positive values indicate a feasible design. Fuel burn is shown in the colored contours. Note that a smoother plot may be created by changing the number of points in the sweep function, but this will take more time. A carpet plot run using 400 points on can be seen below. A local minimum is now visible.</p> - -<p><img src="/images/wing_area_v_cruise_altitude_v_fuel_burn.png" alt="2D Sweep_20" /></p> - -<p>Note: If you run this 400 point case yourself you may see messages indicating that a segment did not converge. This is normal and can happen when a mission is run far from a feasible point. In this case, it does not have a negative impact on the results.</p> - -<h3 id="optimizing">Optimizing:</h3> - -<p>Now try running an Optimization. Recomment <code class="highlighter-rouge">variable_sweep(problem)</code> then uncomment the lines below:</p> - -<div class="highlighter-rouge"><div class="highlight"><pre class="highlight"><code>output = scipy_setup.SciPy_Solve(problem,solver='SLSQP') -print output -</code></pre></div></div> - -<p>and run the file again.</p> - -<p>From the default inputs, the terminal (or IDE output) should display an optimum of [ 1.08980937 1.02089232], which corresponds to a wing area of 109 m^2, and 10.2 km. It appears to have found the local minimum.</p> - -<p>Now try starting the optimization from a different initial guess. You can either modify the input parameters in the initial formulation (the relevant lines are repeated below with the modification)</p> - -<div class="highlighter-rouge"><div class="highlight"><pre class="highlight"><code># [ tag , initial, (lb,ub) , scaling , units ] -problem.inputs = np.array([ - [ 'wing_area' , 128 , ( 90. , 130. ) , 100. , Units.meter**2], - [ 'cruise_altitude' , 13.8 , ( 9 , 14. ) , 10. , Units.km], -]) -</code></pre></div></div> - -<p>or set up the optimization problem and change the inputs manually by uncommenting the following lines.</p> - -<div class="highlighter-rouge"><div class="highlight"><pre class="highlight"><code>inputs = [1.28, 1.38] -scaling = problem.optimization_problem.inputs[:,3] # have to - rescale inputs to start problem from here -scaled_inputs = np.multiply(inputs,scaling) -problem.optimization_problem.inputs[:,1] = scaled_inputs -output = scipy_setup.SciPy_Solve(problem,solver='SLSQP') -print output -</code></pre></div></div> - -<p>This starts the optimization problem above the feasible region (wing area = 128 m^2, altitude = 13.8 km), and results in a fuel burn that is 30 kg lower than the result using the initial guess. This illustrates the important of choosing a starting point when running optimization problem. Additionally, this demonstrates SUAVE’s ability to handle infeasible cases, showing that it can converge to a feasible case even when starting from an infeasible set of initial inputs.</p> - -<p>At this point, you can explore other starting points, or alter the vehicle or mission properties in Vehicles.py or Missions.py. Additionally, feel free to start using this as the basis for creating custom optimization scripts.</p> - - Sun, 14 Jun 2015 16:22:25 -0700 - http://localhost:4000/guides/regional_jet_optimization.html - http://localhost:4000/guides/regional_jet_optimization.html - - - guides - - blog - - - - - Solar UAV Optimization - <h2 id="solar-uav-optimization-tutorial">Solar UAV Optimization Tutorial</h2> - -<p>The purpose of this tutorial is to illustrate a different type of problem. We assume you have gone through the first optimization tutorial: Regional Jet Optimization. This tutorial will illustrate a little more complex setup that modifies a mission parameter.</p> - -<p>Your objective is simple: get a small UAV to fly from San Francisco to San Diego. In fact you can pose that as an optimization problem, with some constraints that govern how it works. There is no requirement to minimize this or maximize that. Of course you could try to minimize something, but you just want something that works for now. Later iterations can do fancier things.</p> - -<p>Next we will go into detail about some of the required files. <em>Analyses.py</em> and <em>Plot_mission.py</em> are straightforward from prior tutorials. So we will not go into those in detail, except to say that we are using a UAV weight model in <em>Analyses.py</em>.</p> - -<h3 id="optimizepy">Optimize.py:</h3> - -<p>Let’s pose the optimization problem first and then setup the rest. We start with the <em>Nexus</em> first as usual. With this design problem there are things you are uncertain of and want to solve for.</p> - -<p>You’re not sure if you really need any solar panels on the airplane, so to start there will be none. The solar ratio is the ratio of wing area to solar area. A value of 1 would the whole top of the wing covered with solar panels.</p> - -<pre><code class="python"> - # [ tag , initial, [lb,ub], scaling, units ] - problem.inputs = np.array([ - [ 'wing_area' , 0.5, ( 0.1, 1.5 ), 0.5, Units.meter ], - [ 'aspect_ratio' , 10.0, ( 5.0, 20.0 ), 10.0, Units.less ], - [ 'dynamic_pressure', 125.0, ( 1.0, 2000.0 ), 125.0, Units.pascals ], - [ 'solar_ratio' , 0.0, ( 0.0, 0.97), 1.0, Units.less ], - [ 'kv' , 800.0, ( 10.0, 1500.0 ), 800.0, Units['rpm/volt']], - ]) -</code></pre> - -<p>Next come the constraints. The first constraint is that the battery energy can never go negative, the math behind this will be elaborated on later. The next constraint is that the plane must have a battery. Finally there are limits to coefficients of lift and throttle settings.</p> - -<pre><code class="python"> - # [ tag, sense, edge, scaling, units ] - problem.constraints = np.array([ - [ 'energy_constraint', '=', 0.0, 1.0, Units.less], - [ 'battery_mass' , '&gt;', 0.0, 1.0, Units.kg ], - [ 'CL' , '&gt;', 0.0, 1.0, Units.less], - [ 'Throttle_min' , '&gt;', 0.0, 1.0, Units.less], - [ 'Throttle_max' , '&gt;', 0.0, 1.0, Units.less], - ]) -</code></pre> - -<p>Notice here that all constraints are greater than zero. This is because SciPy’s SLSQP optimization algorithm assumes this form. To correct for these, the values are adjusted in Procedure.py. Other optimization packages such as PyOpt don’t require this strict form.</p> - -<p>Finally, the objective. It’s nothing of course! As long as the constraints are met, the goal of the design is satisfied.</p> - -<pre><code class="python"> - # [ tag, scaling, units ] - problem.objective = np.array([ - [ 'Nothing', 1. , Units.kg], - ]) -</code></pre> - -<h3 id="vehiclespy">Vehicles.py:</h3> - -<p>Next, you will setup the vehicle. This is very similar to the prior Solar UAV tutorial. So we will gloss over this, the one noticeable difference is that a lower fidelity energy network is used. This means that most components operate with prescribed efficiencies. For example:</p> - -<pre><code class="python"> - # Component 4 the Motor - motor = SUAVE.Components.Energy.Converters.Motor_Lo_Fid() - kv = 800. * Units['rpm/volt'] # RPM/volt is standard - motor = size_from_kv(motor, kv) - motor.gear_ratio = 1. # Gear ratio, no gearbox - motor.gearbox_efficiency = 1. # Gear box efficiency, no gearbox - motor.motor_efficiency = 0.825; - net.motor = motor - ]) -</code></pre> - -<h3 id="missionspy">Missions.py:</h3> - -<p>Now for the mission setup. Here we assume it will take 1000 km and the plane will cruise off the coast at 1000 feet in altitude. The distance is a bit longer than the straight line distance, but we’re not going to fly through populated areas. The heading, or body rotation, must be set to account for the changes in latitude and longitude to accurately calculate the solar radiation. We will cruise at a constant altitude and assume it takes no time to climb and descend compared to the cruise time.</p> - -<pre><code class="python"> - segment.state.numerics.number_control_points = 50 - segment.dynamic_pressure = 115.0 * Units.pascals - segment.start_time = time.strptime("Tue, Jun 21 11:00:00 2016", "%a, %b %d %H:%M:%S %Y",) - segment.altitude = 1000.0 * Units.feet - segment.distance = 1000.0 * Units.km - segment.charge_ratio = 1.0 - segment.latitude = 37.4 - segment.longitude = -122.15 - segment.state.conditions.frames.wind.body_rotations[:,2] = 125.* Units.degrees -</code></pre> - -<h3 id="procedurepy">Procedure.py:</h3> - -<p>Finally we have the procedure setup. In the procedure, we resize the vehicle, calculate weights, finalize the analyses, solve the mission, and post process.</p> - -<p>Some notes about sizing. Each wing component (main wing, horizontal tail, and vertical tail) needs the surfaces sized based on its area and aspect ratio. Next the solar panels are sized based on the wing area and solar_ratio. Finally the motor is resized based on correlations for the speed constant of the motor.</p> - -<pre><code class="python"> -def simple_sizing(nexus): - - # Pull out the vehicle - vec = nexus.vehicle_configurations.base - - # Change the dynamic pressure based on the, add a factor of safety - vec.envelope.maximum_dynamic_pressure = nexus.missions.mission.segments.cruise.dynamic_pressure*1.2 - - # Scale the horizontal and vertical tails based on the main wing area - vec.wings.horizontal_stabilizer.areas.reference = 0.15 * vec.reference_area - vec.wings.vertical_stabilizer.areas.reference = 0.08 * vec.reference_area - - # wing spans,areas, and chords - for wing in vec.wings: - - # Unpack - AR = wing.aspect_ratio - S = wing.areas.reference - - # Set the spans - wing.spans.projected = np.sqrt(AR*S) - - # Set all of the areas for the surfaces - wing.areas.wetted = 2.0 * S - wing.areas.exposed = 1.0 * wing.areas.wetted - wing.areas.affected = 1.0 * wing.areas.wetted - - # Set all of the chord lengths - chord = wing.areas.reference/wing.spans.projected - wing.chords.mean_aerodynamic = chord - wing.chords.mean_geometric = chord - wing.chords.root = chord - wing.chords.tip = chord - - # Size solar panel area - wing_area = vec.reference_area - spanel = vec.propulsors.network.solar_panel - sratio = spanel.ratio - solar_area = wing_area*sratio - spanel.area = solar_area - spanel.mass_properties.mass = solar_area*(0.60 * Units.kg) - - # Resize the motor - motor = vec.propulsors.network.motor - kv = motor.speed_constant - motor = size_from_kv(motor, kv) - - # diff the new data - vec.store_diff() - - return nexus -</code></pre> - -<p>Here the battery is sized and charged. The battery weight consists of everything that is left over from sizing.</p> - -<pre><code class="python"> -def weights_battery(nexus): - - # Evaluate weights for all of the configurations - config = nexus.analyses.base - config.weights.evaluate() - - vec = nexus.vehicle_configurations.base - payload = vec.propulsors.network.payload.mass_properties.mass - msolar = vec.propulsors.network.solar_panel.mass_properties.mass - MTOW = vec.mass_properties.max_takeoff - empty = vec.weight_breakdown.empty - mmotor = vec.propulsors.network.motor.mass_properties.mass - - # Calculate battery mass - batmass = MTOW - empty - payload - msolar -mmotor - bat = vec.propulsors.network.battery - initialize_from_mass(bat,batmass) - vec.propulsors.network.battery.mass_properties.mass = batmass - - # Set Battery Charge - maxcharge = nexus.vehicle_configurations.base.propulsors.network.battery.max_energy - charge = maxcharge - - nexus.missions.mission.segments.cruise.battery_energy = charge - - return nexus -</code></pre> - -<p>The next we run the mission and post process the results. The post_process function will setup the information of importance for the user. The energy constraint is a way of ensuring that nowhere in the mission the battery energy goes negative. The coefficient of lift is limited to 1.2. The throttle is limited to 0.9, to make sure there is excess throttle to climb. Throttle is also limited from going negative. Finally, the objective, nothing is specified to be zero.</p> - -<pre><code class="python"> -def post_process(nexus): - - # Unpack - mis = nexus.missions.mission.segments.cruise - vec = nexus.vehicle_configurations.base - res = nexus.results.mission.segments.cruise.conditions - - # Final Energy - maxcharge = vec.propulsors.network.battery.max_energy - - # Energy constraints, the battery doesn't go to zero anywhere, using a P norm - p = 8. - energies = res.propulsion.battery_energy[:,0]/np.abs(maxcharge) - energies[energies&gt;0] = 0.0 # Exclude the values greater than zero - energy_constraint = np.sum((np.abs(energies)**p))**(1/p) - - # CL max constraint, it is the same throughout the mission - CL = res.aerodynamics.lift_coefficient[0] - - # Pack up - summary = nexus.summary - summary.CL = 1.2 - CL - summary.energy_constraint = energy_constraint - summary.throttle_min = res.propulsion.throttle[0] - summary.throttle_max = 0.9 - res.propulsion.throttle[0] - summary.nothing = 0.0 - - return nexus -</code></pre> - -<h3 id="results">Results</h3> -<p>Let’s look at the results:</p> - -<pre><code class="python"> -Optimization terminated successfully. (Exit mode 0) - Current function value: [0.0] - Iterations: 4 - Function evaluations: 29 - Gradient evaluations: 4 -[ 1.12963146 1.43880081 1.39329626 0.65589785 0.97171879] -Design Variable Table: - -[['wing_area' 0.5648157324099996 (0.1, 1.5) 0.5 1.0] - ['aspect_ratio' 14.388008119672202 (5.0, 20.0) 10.0 1.0] - ['dynamic_pressure' 174.16203234031317 (1.0, 2000.0) 125.0 1.0] - ['solar_ratio' 0.6558978486767236 (0.0, 0.97) 1.0 1.0] - ['kv' 777.3750338508712 (10.0, 1500.0) 800.0 0.10471975511965977]] - -Constraint Table: - -[['energy_constraint' 0.0 '=' 0.0 1.0 &lt;Quantity(1.0, 'less')&gt;] - ['battery_mass' 4.939962596982861 '&gt;' 0.0 1.0 &lt;Quantity(1.0, 'kilogram')&gt;] - ['CL' 0.5309682332699428 '&gt;' 0.0 1.0 &lt;Quantity(1.0, 'less')&gt;] - ['Throttle_min' 0.7319219623084848 '&gt;' 0.0 1.0 &lt;Quantity(1.0, 'less')&gt;] - ['Throttle_max' 0.1680780376915152 '&gt;' 0.0 1.0 &lt;Quantity(1.0, 'less')&gt;]] -</code></pre> - -<p>Okay looks like SciPy found a feasible solution without too much time. Now let’s review the plots.</p> - -<p><img src="/images/opt_battery_energy.png" alt="battery_energy" /></p> - -<p>So we can tell now that the battery energy doesn’t go all the way to zero. Let’s look at how the solar flux varies throughout the day and how that affects the draw from the battery.</p> - -<p><img src="/images/opt_solar_flux.png" alt="solar flux" /></p> - -<p><img src="/images/opt_battery_draw.png" alt="battery draw" /></p> - -<p>So maybe those solar panels actually are worth it. They seem to decrease the load on the battery considerably during the daytime.</p> - - - Sun, 14 Jun 2015 16:22:21 -0700 - http://localhost:4000/guides/solar_uav_optimization.html - http://localhost:4000/guides/solar_uav_optimization.html - - - guides - - blog - - - - - Frequently Asked Questions - <link rel="stylesheet" href="//cdn.jsdelivr.net/highlight.js/8.6/styles/default.min.css" /> - -<script src="//cdn.jsdelivr.net/highlight.js/8.6/highlight.min.js"></script> - -<script>hljs.initHighlightingOnLoad();</script> - -<p>Alright, you dove in and now you’re stuck. You’ve come to a good starting point. If this FAQ fails you then we suggest you go through tutorials, maybe our <a href="http://adl.stanford.edu/papers/suave-open-source.pdf">paper</a>, send us a question in the forum, or if all else fails start reading code. Don’t worry the code is more readable than most engineering textbooks.</p> - -<ul> - <li><a href="#how-do-i-get-started">How do I get started?</a></li> - <li><a href="#what-version-of-python-should-i-use">What version of Python should I use?</a></li> - <li><a href="#can-i-use-suave-for-my-own-research">Can I use SUAVE for my own research?</a></li> - <li><a href="#how-can-i-contribute">How can I contribute?</a></li> - <li><a href="#how-can-i-best-get-in-touch-with-you-or-ask-for-help">How can I best get in touch with you or ask for help?</a></li> - <li><a href="#where-can-i-see-the-recent-additions-to-the-suave-environment">Where can I see the recent additions to the SUAVE environment?</a></li> - <li><a href="#are-there-plans-to-make-a-graphical-user-interface">Are there plans to make a Graphical User Interface?</a></li> - <li><a href="#how-is-a-mission-solved">How is a mission solved?</a></li> -</ul> - -<p><br /></p> - -<h3 id="how-do-i-get-started">How do I get started?</h3> - -<ul> - <li>Download SUAVE’s current release on our <a href="/download/">download</a> page. Specific steps and further instructions for additional software requirements are also listed there.</li> - <li>Get familiar with the code using our <a href="guides/">guides</a>. Be sure to start the <a href="/guides/boeing_737-800.html">Boeing 737 Tutorial</a> for a basic introduction and the Regional Jet Optimization for the optimization tools.</li> - <li>Ask any remaining questions on the <a href="/forum">forum</a></li> -</ul> - -<h3 id="what-version-of-python-should-i-use">What version of Python should I use?</h3> -<p>SUAVE is developed in Python 2.7.</p> - -<h3 id="can-i-use-suave-for-my-own-research">Can I use SUAVE for my own research?</h3> -<p>Yes, you may! Please cite our papers:</p> - -<ul> - <li> - <p><a href="http://adl.stanford.edu/papers/suave-open-source.pdf">T. Lukaczyk, A. Wendorff, E. Botero, T. MacDonald, T. Momose, A. Variyar, J. M. Vegh, M. Colonno, T. Economon, J. J. Alonso, T. Orra, C. Ilario, “SUAVE: An Open-Source Environment for Multi-Fidelity Conceptual Vehicle Design”, 16th AIAA Multidisciplinary Analysis and Optimization Conference, Dallas, TX, June 2015.</a></p> - </li> - <li> - <p><a href="http://adl.stanford.edu/papers/suave-optimization.pdf">E. Botero, A. Wendorff, T. MacDonald, A. Variyar, J. M. Vegh, T. Lukaczyk, J. J. Alonso, T. Orra, C. Ilario da Silva. “SUAVE: An Open-Source Environment for Conceptual Vehicle Design and Optimization”, 54th AIAA Aerospace Sciences Meeting, San Diego, CA, January 2016.</a></p> - </li> - <li> - <p><a href="http://adl.stanford.edu/papers/suave-hi-fi.pdf">T. MacDonald, E. Botero, J. M. Vegh, A. Variyar, J. J. Alonso, T. Orra, C. Ilario da Silva. “SUAVE: An Open-Source Environment Enabling Unconventional Designs through Higher Fidelity”, 55th AIAA Aerospace Sciences Meeting, Grapevine, TX, January 2017.</a></p> - </li> - <li> - <p><a href="http://adl.stanford.edu/papers/suave-mf-opt.pdf">T. MacDonald, M. Clarke, E. Botero, J. M. Vegh, J. J. Alonso. “SUAVE: An Open-Source Environment Enabling Multi-fidelity Vehicle Optimization”, 16th AIAA Multidisciplinary Analysis and Optimization Conference, Denver, CO, June 2017.</a></p> - </li> -</ul> - -<h3 id="how-can-i-contribute">How can I contribute?</h3> -<p>We encourage SUAVE users to expand the environment according to their personal interests. The main areas to be developed are listed <a href="/develop/#areas-of-development">here</a>.</p> - -<h3 id="how-can-i-best-get-in-touch-with-you-or-ask-for-help">How can I best get in touch with you or ask for help?</h3> -<p>The <a href="/forum">forum</a> is our main point of contact for SUAVE discussions.</p> - -<h3 id="where-can-i-see-the-recent-additions-to-the-suave-environment">Where can I see the recent additions to the SUAVE environment?</h3> -<p>Go and check the develop branch on our <a href="https://github.com/suavecode/SUAVE">GitHub site</a>. This branch contains new features that are functional but not necessarily ready for release. Everything in this branch is added to the master branch at the next release. Several other feature branches can also be seen here. These are typically under active development. For any more information on what is available please ask on the <a href="/forum">forum</a></p> - -<h3 id="are-there-plans-to-make-a-graphical-user-interface">Are there plans to make a Graphical User Interface?</h3> -<p>The core development team is currently not planning on developing a GUI, but you can help! Contact us via the <a href="/forum">forum</a>.</p> - -<h3 id="how-is-a-mission-solved">How is a mission solved?</h3> - -<p>A mission is divided into segments, for example climb, cruise, etc… Then the segment is divided into discrete points that are cosine spaced in time. These make up Chebyshev collocation points. One of the beauties of this method is the integration and differentiation operator. So if you know the velocity at every point, then you can get accelerations and vice-versa.</p> - -<p>The default value is 16 points in each segment for SUAVE. However, our internal numerical experiments have shown highly accurate results with ~0.1% error with only 4 control points and ~.0001% error with 8 as measured from a very highly refined answered.</p> - -<p>For each control point there are various unknowns and residuals. An example of an unknown would be pitch angle, and a residual would be the forces in the Z direction. After performing an analysis using the unknowns the residuals are calculated. These unknowns and residuals are iterated through a hybrid solver (much like a Newton method) in SciPy to converge the residual to zero. Voila, with a little magic you have results!</p> - -<!--- For more information see this [guide](). --> - - Tue, 15 Jun 2010 07:20:00 -0700 - http://localhost:4000/faq.html - http://localhost:4000/faq.html - - - documentation - - blog - - - - - diff --git a/_site/forum/index.html b/_site/forum/index.html deleted file mode 100644 index e7f1bb62..00000000 --- a/_site/forum/index.html +++ /dev/null @@ -1,139 +0,0 @@ - - - - - - - - Forum - SUAVE - - - - - - - - - - - - - - -
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Together we design exotic aerospace configurations

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Boeing 737-800

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Boeing 737-800 Analysis Tutorial

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This tutorial shows how the user can setup a conventional configuration aircraft, a mission the aircraft is to fly, and then simulate the aircraft’s performance over the defined mission. The code is divided into a number of functions that are called from the main function.

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Steps to simulate the aircraft’s performance over a mission :

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1) Locate the folder where you have the tutorial repository. If using the command line, cd to this directory.

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2) Open the tut_mission_B737.py script in your favorite editor or IDE. The script is setup to run the B737 on its design mission. Run it in your IDE. If using the command line use the command

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3) A few plots depicting the variation of the different aircraft performance parameters over the course of the mission are shown.

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Important Functions :

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The script is divided into a set of functions that setup different aspects of the modeling process. The important functions are:

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vehicle_setup()

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function is where the aircraft’s geometry is specified.

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Setting up a wing
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The code below shows how the main wing of the aircraft is set up. The basic geometric inputs that define the wing are specified. Then the wing is then appended to the vehicle, which is an instance of the aircraft class.

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In SUAVE units are identified through the use of a units package called Pint. Notice, that for the wing sweep that the units are specified in degrees through *Units.deg. To get results into a desired unit use /Units.deg.

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The wing sweep is defined as the sweep of the quarter chord. Additionally, a symmetric wing means that it is symmetric about the root, i.e. there is right and left side.

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-    wing = SUAVE.Components.Wings.Main_Wing()
-    wing.tag = 'main_wing'
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-    wing.aspect_ratio            = 10.18
-    wing.sweeps.quarter_chord    = 25 * Units.deg
-    wing.thickness_to_chord      = 0.1
-    wing.taper                   = 0.1
-    wing.span_efficiency         = 0.9
-    wing.spans.projected         = 34.32 * Units.meter
-    wing.chords.root             = 7.760 * Units.meter
-    wing.chords.tip              = 0.782 * Units.meter
-    wing.chords.mean_aerodynamic = 4.235 * Units.meter
-    wing.areas.reference         = 124.862 * Units['meters**2']  
-    wing.twists.root             = 4.0 * Units.degrees
-    wing.twists.tip              = 0.0 * Units.degrees
-    wing.origin                  = [13.61,0,-1.27] # meters
-    wing.vertical                = False
-    wing.symmetric               = True
-    wing.high_lift               = True
-    wing.dynamic_pressure_ratio  = 1.0
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Setting up the fuselage
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Similar to the wing above, the code below illustrates how a fuselage can be added to the vehicle. Again the user is required to specify the basic fuselage geometric parameters and then add the fuselage object to the vehicle.

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-    fuselage = SUAVE.Components.Fuselages.Fuselage()
-    fuselage.tag = 'fuselage'
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-    fuselage.number_coach_seats    = vehicle.passengers
-    fuselage.seats_abreast         = 6
-    fuselage.seat_pitch            = 1     * Units.meter
-    fuselage.fineness.nose         = 1.6
-    fuselage.fineness.tail         = 2.
-    fuselage.lengths.nose          = 6.4   * Units.meter
-    fuselage.lengths.tail          = 8.0   * Units.meter
-    fuselage.lengths.cabin         = 28.85 * Units.meter
-    fuselage.lengths.total         = 38.02 * Units.meter
-    fuselage.lengths.fore_space    = 6.    * Units.meter
-    fuselage.lengths.aft_space     = 5.    * Units.meter
-    fuselage.width                 = 3.74  * Units.meter
-    fuselage.heights.maximum       = 3.74  * Units.meter
-    fuselage.effective_diameter    = 3.74     * Units.meter
-    fuselage.areas.side_projected  = 142.1948 * Units['meters**2'] 
-    fuselage.areas.wetted          = 446.718  * Units['meters**2'] 
-    fuselage.areas.front_projected = 12.57    * Units['meters**2'] 
-    fuselage.differential_pressure = 5.0e4 * Units.pascal # Maximum differential pressure
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-    fuselage.heights.at_quarter_length          = 3.74 * Units.meter
-    fuselage.heights.at_three_quarters_length   = 3.65 * Units.meter
-    fuselage.heights.at_wing_root_quarter_chord = 3.74 * Units.meter
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-    # add to vehicle
-    vehicle.append_component(fuselage)
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Setting up the propulsion system
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The aircraft uses a turbofan engine. This engine can be constructed piece by piece using the energy network framework. We instantiate the network as shown below.

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-    #   Turbofan Network
-    # ------------------------------------------------------------------    
-    
-    #instantiate the gas turbine network
-    turbofan = SUAVE.Components.Energy.Networks.Turbofan()
-    turbofan.tag = 'turbofan'
-    
-    # setup
-    turbofan.number_of_engines = 2
-    turbofan.bypass_ratio      = 5.4
-    turbofan.engine_length     = 2.71 * Units.meter
-    turbofan.nacelle_diameter  = 2.05 * Units.meter
-    turbofan.origin            = [[13.72, 4.86,-1.9],[13.72, -4.86,-1.9]] # meters
-    
-    #compute engine areas
-    turbofan.areas.wetted      = 1.1*np.pi*turbofan.nacelle_diameter*turbofan.engine_length
-    
-    # working fluid
-    turbofan.working_fluid = SUAVE.Attributes.Gases.Air()
-
-
- -

Next the components of the turbofan are initialized and added to the engine as shown in the energy networks section. The turbofan is composed of an inlet diffuser (nozzle), low and high pressure compressors, a combustor, a fan, a high and low pressure turbine, and exit nozzles for the core and the fan.

- -

Finally the network is added to the aircraft as shown below.

- -

-#size the turbofan
-turbofan_sizing(turbofan,mach_number,altitude)   
-    
-# add  gas turbine network turbofan to the vehicle 
-vehicle.append_component(turbofan)  
-
-# add  gas turbine network gt_engine to the vehicle
-vehicle.append_component(turbofan)  
-
- -

Data Structure Visualization

-

The data structure associated with the Boeing 737-800 can be visualized here.

- -

Boeing 737 Data Structure

- -

This visualization shows the hierarchy of data in a SUAVE vehicle. Some of the values are defaulted, for example costs. This is because we are not performing cost analysis on the Boeing 737-800. Additionally, this snapshot of the data structure was taken prior to analysis. Therefore weights have not been calculated and are not part of the data. During the mission analysis component weights will be determined and weights will be populated.

- -

configs_setup()

-

The aircraft geometry created is converted into configurations that can be used to make simple modifications to the geometric parameters while not modifying the aircraft geometry completely. An example of the use of this feature is when high-lift devices need to be deployed during landing and takeoff. Thus a landing and takeoff configuration can be added as shown below and then during say the flaps and slats settings can be set differently for each of the configurations.

- -

-    # ------------------------------------------------------------------
-    #   Cruise Configuration
-    # ------------------------------------------------------------------
-    config = SUAVE.Components.Configs.Config(base_config)
-    config.tag = 'cruise'
-    configs.append(config)
-
-    # ------------------------------------------------------------------
-    #   Takeoff Configuration
-    # ------------------------------------------------------------------
-    config = SUAVE.Components.Configs.Config(base_config)
-    config.tag = 'takeoff'
-    config.wings['main_wing'].flaps.angle = 20. * Units.deg
-    config.wings['main_wing'].slats.angle = 25. * Units.deg
-    config.max_lift_coefficient_factor    = 1.
-
-    configs.append(config)
-
- -

mission_setup()

-

To modify the baseline mission that the aircraft flies, go to the mission_setup() function and add or delete segments of the mission

- -

-    segment = Segments.Cruise.Constant_Speed_Constant_Altitude(base_segment)
-    segment.tag = "cruise"
-
-    segment.analyses.extend( analyses.cruise )
-
-    segment.air_speed  = 230.412 * Units['m/s']
-    segment.distance   = 2490. * Units.nautical_miles
-
-    # add to mission
-    mission.append_segment(segment)
-
- -

base_analysis()

-

Also to leverage SUAVE’s multifidelity capability and use a different fidelity analysis for any of the disciplines (aerodynamics,propulsion, stability, etc), the base_analysis function can be modified by switching out an analysis module for a different one.

- -

Other Functions :

- -

main()

- -

The main function is the driver function for the mission simulation. It calls the various routines in the appropriate order in order to set up the geometry and the mission, evaluate the performance of the aircraft over the mission and return the results.

- -

full_setup()

- -

This function (called from the main() function) sets up the aircraft geometry, configs and the missions the aircraft is to be analysed for by calling the vehicle_setup, configs_setup, analyses_setup, mission_setup and missions_setup functions.

- -

simple_sizing()

- -

The simple sizing function sizes the aircraft’s geometric components based on the geometric inputs specified by the user in the vehicle_setup() function.

- -

base_analysis()

- -

The method takes in the vehicle and assigns different analysis methods (for aero, propulsion, weights, stability) to the analyses object.

- -

analyses_setup()

- -

This functions takes in the base analysis and sets up different analysis methods for different configurations.

- -

missions_setup()

- -

This method allows the user to set up a variety of missions that need to be evaluated for an aircraft.

- -

plot_mission()

- -

This is a post processing function that takes in the results data structure and generates the necessary plots.

- -

RESULTS

- -

The plots shown below should be generated if the mission analysis executes correctly. The results show the aerodynamic, propulsion and mission properties of the B737-800 for the defined mission.

- -

B737 mission

- -

B737 Aerodynamics

- -

B737 Propulsion

- -

B737 Drag

- -

Modifying the Aircraft’s Geometry or Mission :

- -

Suppose we want to simulate a high span variant of the B737-800. The span is increased to 40.0 m. We assume the wing chords, sweep, taper ratio, thickness to chord ratio remain the same. Thus changing the span only changes the aspect ratio and the wing area.

- -

Now we try to fly the aircraft at a lower cruise speed of 200m/s at a cruise altitude of 25000 ft

- -

1) To update the geometry, scroll to the vehicle_setup() function

- -

2) Modify the parameters of the main wing

- -

-wing.aspect_ratio            = 10.12      
-wing.spans.projected         = 40.0  * Units.meter
-wing.areas.reference         = 158.0 * Units['meters**2'] 
-
- -

You may also need to update the reference area for the aircraft.

- -
vehicle.reference_area         =     158.0
-
- -

3) Update the mission parameters by moving to the mission_setup() function

- -

4) First update the end altitude of the final climb segment. Although the original script has the altitude stated in m, courtesy of the Units package it is easy to modify the altitude to 25,000ft without worrying about the units conversion as shown below.

- -
segment = Segments.Climb.Constant_Speed_Constant_Rate(base_segment)
-segment.tag = "climb_3"
-
-segment.analyses.extend( analyses.cruise )
-
-segment.altitude_end = 25000 * Units.ft  
-segment.air_speed    = 226.0  * Units['m/s']
-segment.climb_rate   = 3.0    * Units['m/s']
-
-mission.append_segment(segment)
-
- -

5) Next update the cruise segment velocity to the new speed value

- -
segment = Segments.Cruise.Constant_Speed_Constant_Altitude(base_segment)
-segment.tag = "cruise"
-
-segment.analyses.extend( analyses.cruise )
-
-segment.air_speed  = 200.0 * Units['m/s']
-segment.distance   = 2490. * Units.nautical_miles
-
-# add to mission
-mission.append_segment(segment)
-
- -

6) Now go back and run the mission for the updated geometry and mission using the steps specified in ‘Steps to run the aircraft on a mission’

- - -
- -
-
- - -
- -
- - -
- -
-
- - - - - - - - - - diff --git a/_site/guides/concorde.html b/_site/guides/concorde.html deleted file mode 100644 index e9856b76..00000000 --- a/_site/guides/concorde.html +++ /dev/null @@ -1,211 +0,0 @@ - - - - - - - - Concorde - SUAVE - - - - - - - - - - - - - - -
-
- -
-
- -
- -
-
-

Concorde

-
-
- -
- - - - - - -

Concorde Tutorial

- -

This tutorial gives an overview of changes made to the setup to evaluate a supersonic mission.

- -

Aerodynamics Module:

- -

To allow aerodynamic calculations in supersonic flight, we use the zero fidelity supersonic module. This is quite easy to swap with the subsonic zero fidelity model. This model and the zero fidelity subsonic module are in the same directory, so they can be switched by changing a single line in the analysis section:

- -
aerodynamics = SUAVE.Analyses.Aerodynamics.Fidelity_Zero()
-
- -

to

- -
aerodynamics = SUAVE.Analyses.Aerodynamics.Supersonic_Zero()
-
-

The supersonic aerodynamics module can still handle the subsonic portions of the flight.

- -

Wing Additions:

- -

Some of the calculations are changed to account for different properties that are not automatically captured in the model.

- -
    -
  • Vortex lift is set to true. This causes the vortex lift module to add a CL increment to the aircraft.
  • -
  • High Mach is set to true. This changes the way that high subsonic compressibility drag is calculated and brings it more in line with Concorde behavior.
  • -
- -
    wing.vortex_lift             = True
-
- -
    wing.high_mach               = True
-
- -

Note also that Concorde does not have a horizontal tail, so this is not included in the vehicle setup.

- -

Turbojet Module:

- -

Since Concorde has a diverging nozzle that allows for supersonic outflow, a modified turbojet is used that can account for this. This turbojet component is again switched out with a single line.

- -
nozzle = SUAVE.Components.Energy.Converters.Supersonic_Nozzle()
-
- -

instead of

- -
nozzle = SUAVE.Components.Energy.Converters.Expansion_Nozzle()  
-
- -

Mission Segments:

- -

The mission typically flown by Concorde calls for mission segments that are not utilized in the Boeing 737 case. These are Mach number dependent, and require different inputs from the segments previously given. The new mission segments are linear Mach constant rate (climb and descent). Both require a starting and ending Mach number, which will vary linearly in time over the descent. For an example, check the third climb segment:

- -
segment = Segments.Climb.Linear_Mach_Constant_Rate(base_segment)
-segment.tag = "climb_3"
-
-segment.analyses.extend( analyses.cruise )
-
-segment.altitude_end = 7.60   * Units.km
-segment.mach_start   = 0.64
-segment.mach_end     = 1.0
-segment.climb_rate   = 5.05  * Units['m/s']
-
- -

Takeoff and Landing Configuration

- -

Since Concorde does not have flaps or slats, specific takeoff and landing configurations are not used.

- -
- -
-
- - -
- -
- - -
- -
-
- - - - - - - - - - diff --git a/_site/guides/data_structures/B737.html b/_site/guides/data_structures/B737.html deleted file mode 100644 index 32d03a46..00000000 --- a/_site/guides/data_structures/B737.html +++ /dev/null @@ -1,58 +0,0 @@ - - - - - - - -
- - \ No newline at end of file diff --git a/_site/guides/data_structures/B737.js b/_site/guides/data_structures/B737.js deleted file mode 100644 index 7400b601..00000000 --- a/_site/guides/data_structures/B737.js +++ /dev/null @@ -1,511 +0,0 @@ -// Get JSON data -treeJSON = d3.json("B737.json", function(error, treeData) { - - // Calculate total nodes, max label length - var totalNodes = 0; - var maxLabelLength = 0; - // variables for drag/drop - var selectedNode = null; - var draggingNode = null; - // panning variables - var panSpeed = 200; - var panBoundary = 20; // Within 20px from edges will pan when dragging. - // Misc. variables - var i = 0; - var duration = 750; - var root; - - // size of the diagram - var viewerWidth = $(document).width(); - var viewerHeight = $(document).height(); - - var tree = d3.layout.tree() - .size([viewerHeight, viewerWidth]); - - // define a d3 diagonal projection for use by the node paths later on. - var diagonal = d3.svg.diagonal() - .projection(function(d) { - return [d.y, d.x]; - }); - - // A recursive helper function for performing some setup by walking through all nodes - - function visit(parent, visitFn, childrenFn) { - if (!parent) return; - - visitFn(parent); - - var children = childrenFn(parent); - if (children) { - var count = children.length; - for (var i = 0; i < count; i++) { - visit(children[i], visitFn, childrenFn); - } - } - } - - // Call visit function to establish maxLabelLength - visit(treeData, function(d) { - totalNodes++; - maxLabelLength = Math.max(d.name.length, maxLabelLength); - - }, function(d) { - return d.children && d.children.length > 0 ? d.children : null; - }); - - - // sort the tree according to the node names - - function sortTree() { - tree.sort(function(a, b) { - return b.name.toLowerCase() < a.name.toLowerCase() ? 1 : -1; - }); - } - - // Sort the tree initially incase the JSON isn't in a sorted order. - //sortTree(); - - // TODO: Pan function, can be better implemented. - - function pan(domNode, direction) { - var speed = panSpeed; - if (panTimer) { - clearTimeout(panTimer); - translateCoords = d3.transform(svgGroup.attr("transform")); - if (direction == 'left' || direction == 'right') { - translateX = direction == 'left' ? translateCoords.translate[0] + speed : translateCoords.translate[0] - speed; - translateY = translateCoords.translate[1]; - } else if (direction == 'up' || direction == 'down') { - translateX = translateCoords.translate[0]; - translateY = direction == 'up' ? translateCoords.translate[1] + speed : translateCoords.translate[1] - speed; - } - scaleX = translateCoords.scale[0]; - scaleY = translateCoords.scale[1]; - scale = zoomListener.scale(); - svgGroup.transition().attr("transform", "translate(" + translateX + "," + translateY + ")scale(" + scale + ")"); - d3.select(domNode).select('g.node').attr("transform", "translate(" + translateX + "," + translateY + ")"); - zoomListener.scale(zoomListener.scale()); - zoomListener.translate([translateX, translateY]); - panTimer = setTimeout(function() { - pan(domNode, speed, direction); - }, 50); - } - } - - // Define the zoom function for the zoomable tree - - function zoom() { - svgGroup.attr("transform", "translate(" + d3.event.translate + ")scale(" + d3.event.scale + ")"); - } - - // define the zoomListener which calls the zoom function on the "zoom" event constrained within the scaleExtents - var zoomListener = d3.behavior.zoom().scaleExtent([0.1, 3]).on("zoom", zoom); - - // define the baseSvg, attaching a class for styling and the zoomListener - var baseSvg = d3.select("#tree-container").append("svg") - .attr("width", viewerWidth) - .attr("height", viewerHeight) - .attr("class", "overlay") - .call(zoomListener); - - - // Define the drag listeners for drag/drop behaviour of nodes. - dragListener = d3.behavior.drag() - .on("dragstart", function(d) { - if (d == root) { - return; - } - dragStarted = true; - nodes = tree.nodes(d); - d3.event.sourceEvent.stopPropagation(); - // it's important that we suppress the mouseover event on the node being dragged. Otherwise it will absorb the mouseover event and the underlying node will not detect it d3.select(this).attr('pointer-events', 'none'); - }) - .on("drag", function(d) { - if (d == root) { - return; - } - if (dragStarted) { - domNode = this; - initiateDrag(d, domNode); - } - - // get coords of mouseEvent relative to svg container to allow for panning - relCoords = d3.mouse($('svg').get(0)); - if (relCoords[0] < panBoundary) { - panTimer = true; - pan(this, 'left'); - } else if (relCoords[0] > ($('svg').width() - panBoundary)) { - - panTimer = true; - pan(this, 'right'); - } else if (relCoords[1] < panBoundary) { - panTimer = true; - pan(this, 'up'); - } else if (relCoords[1] > ($('svg').height() - panBoundary)) { - panTimer = true; - pan(this, 'down'); - } else { - try { - clearTimeout(panTimer); - } catch (e) { - - } - } - - d.x0 += d3.event.dy; - d.y0 += d3.event.dx; - var node = d3.select(this); - node.attr("transform", "translate(" + d.y0 + "," + d.x0 + ")"); - updateTempConnector(); - }).on("dragend", function(d) { - if (d == root) { - return; - } - domNode = this; - if (selectedNode) { - // now remove the element from the parent, and insert it into the new elements children - var index = draggingNode.parent.children.indexOf(draggingNode); - if (index > -1) { - draggingNode.parent.children.splice(index, 1); - } - if (typeof selectedNode.children !== 'undefined' || typeof selectedNode._children !== 'undefined') { - if (typeof selectedNode.children !== 'undefined') { - selectedNode.children.push(draggingNode); - } else { - selectedNode._children.push(draggingNode); - } - } else { - selectedNode.children = []; - selectedNode.children.push(draggingNode); - } - // Make sure that the node being added to is expanded so user can see added node is correctly moved - expand(selectedNode); - sortTree(); - endDrag(); - } else { - endDrag(); - } - }); - - function endDrag() { - selectedNode = null; - d3.selectAll('.ghostCircle').attr('class', 'ghostCircle'); - d3.select(domNode).attr('class', 'node'); - // now restore the mouseover event or we won't be able to drag a 2nd time - d3.select(domNode).select('.ghostCircle').attr('pointer-events', ''); - updateTempConnector(); - if (draggingNode !== null) { - update(root); - centerNode(draggingNode); - draggingNode = null; - } - } - - // Helper functions for collapsing and expanding nodes. - - function collapse(d) { - if (d.children) { - d._children = d.children; - d._children.forEach(collapse); - d.children = null; - } - } - - function expand(d) { - if (d._children) { - d.children = d._children; - d.children.forEach(expand); - d._children = null; - } - } - - var overCircle = function(d) { - selectedNode = d; - updateTempConnector(); - }; - var outCircle = function(d) { - selectedNode = null; - updateTempConnector(); - }; - - // Function to update the temporary connector indicating dragging affiliation - var updateTempConnector = function() { - var data = []; - if (draggingNode !== null && selectedNode !== null) { - // have to flip the source coordinates since we did this for the existing connectors on the original tree - data = [{ - source: { - x: selectedNode.y0, - y: selectedNode.x0 - }, - target: { - x: draggingNode.y0, - y: draggingNode.x0 - } - }]; - } - var link = svgGroup.selectAll(".templink").data(data); - - link.enter().append("path") - .attr("class", "templink") - .attr("d", d3.svg.diagonal()) - .attr('pointer-events', 'none'); - - link.attr("d", d3.svg.diagonal()); - - link.exit().remove(); - }; - - // Function to center node when clicked/dropped so node doesn't get lost when collapsing/moving with large amount of children. - - function centerNode(source) { - scale = zoomListener.scale(); - x = -source.y0; - y = -source.x0; - x = x * scale + viewerWidth / 2; - y = y * scale + viewerHeight / 2; - d3.select('g').transition() - .duration(duration) - .attr("transform", "translate(" + x + "," + y + ")scale(" + scale + ")"); - zoomListener.scale(scale); - zoomListener.translate([x, y]); - } - - // Toggle children function - - function toggleChildren(d) { - if (d.children) { - //d._children = d.children; - //d.children = null; - collapse(d) - } else if (d._children) { - d.children = d._children; - d._children = null; - d.children.forEach( function(d) { - if (d._children && d._children.length == 1) { - if (!d._children[0]._children) { - toggleChildren(d); - } - } - }); - } - return d; - } - - // Toggle children on click. - - function click(d) { - if (d3.event.defaultPrevented) return; // click suppressed - d = toggleChildren(d); - update(d); - centerNode(d); - } - - function update(source) { - // Compute the new height, function counts total children of root node and sets tree height accordingly. - // This prevents the layout looking squashed when new nodes are made visible or looking sparse when nodes are removed - // This makes the layout more consistent. - var levelWidth = [1]; - var childCount = function(level, n) { - - if (n.children && n.children.length > 0) { - if (levelWidth.length <= level + 1) levelWidth.push(0); - - levelWidth[level + 1] += n.children.length; - n.children.forEach(function(d) { - childCount(level + 1, d); - }); - } - }; - childCount(0, root); - var newHeight = d3.max(levelWidth) * 25; // 25 pixels per line - tree = tree.size([newHeight, viewerWidth]); - - // Compute the new tree layout. - var nodes = tree.nodes(root).reverse(), - links = tree.links(nodes); 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"end" : "start"; - }) - .text(function(d) { - return d.name; - }) - .style("fill-opacity", 0); - - // phantom node to give us mouseover in a radius around it - nodeEnter.append("circle") - .attr('class', 'ghostCircle') - .attr("r", 30) - .attr("opacity", 0.2) // change this to zero to hide the target area - .style("fill", "red") - .attr('pointer-events', 'mouseover') - .on("mouseover", function(node) { - overCircle(node); - }) - .on("mouseout", function(node) { - outCircle(node); - }); - - // Update the text to reflect whether node has children or not. - node.select('text') - .attr("x", function(d) { - return d.children || d._children ? -12 : 12; - }) - .attr("text-anchor", function(d) { - return d.children || d._children ? 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"children": [ - { - "name": "moments_of_inertia", - "children": [ - { - "name": "center", - "children": [ - { - "name": "[ 0. 0. 0.]" - } - ] - }, - { - "name": "tensor", - "children": [ - { - "name": "[[ 0. 0. 0.]\n [ 0. 0. 0.]\n [ 0. 0. 0.]]" - } - ] - } - ] - }, - { - "name": "cargo", - "children": [ - { - "name": "10000.0" - } - ] - }, - { - "name": "max_fuel", - "children": [ - { - "name": "0.0" - } - ] - }, - { - "name": "max_zero_fuel", - "children": [ - { - "name": "71114.22" - } - ] - }, - { - "name": "passenger", - "children": [ - { - "name": "0.0" - } - ] - }, - { - "name": "max_takeoff", - "children": [ - { - "name": "79015.8" - } - ] - }, - { - "name": "max_payload", - "children": [ - { - "name": "0.0" - } - ] - }, - { - "name": "takeoff", - "children": [ - { - "name": "79015.8" - } - ] - }, - { - "name": "landing", - "children": [ - { - "name": "0.0" - } - ] - }, - { - "name": "payload", - "children": [ - { - "name": "0.0" - } - ] - }, - { - "name": "volume", - "children": [ - { - "name": "0.0" - } - ] - }, - { - "name": "zero_fuel_center_of_gravity", - "children": [ - { - "name": "[ 0. 0. 0.]" - } - ] - }, - { - "name": "mass", - "children": [ - { - "name": "0.0" - } - ] - }, - { - "name": "center_of_gravity", - "children": [ - { - "name": "[0.0, 0.0, 0.0]" - } - ] - }, - { - "name": "fuel", - "children": [ - { - "name": "0.0" - } - ] - }, - { - "name": "max_cargo", - "children": [ - { - "name": "0.0" - } - ] - }, - { - "name": "crew", - "children": [ - { - "name": "0.0" - } - ] - }, - { - "name": "operating_empty", - "children": [ - { - "name": "39128.8287516" - } - ] - }, - { - "name": "max_landing", - "children": [ - { - "name": "0.0" - } - ] - } - ] - }, - { - "name": "furnishings", - "children": [ - { - "name": "origin", - "children": [ - { - "name": "[[0.0, 0.0, 0.0]]" - } - ] - }, - { - "name": "symmetric", - "children": [ - { - "name": "False" - } - ] - }, - { - "name": "tag", - "children": [ - { - "name": "Component" - } - ] - }, - { - "name": "mass_properties", - "children": [ - { - "name": "volume", - "children": [ - { - "name": "0.0" - } - ] - }, - { - "name": "moments_of_inertia", - "children": [ - { - "name": "center", - "children": [ - { - "name": "[ 0. 0. 0.]" - } - ] - }, - { - "name": "tensor", - "children": [ - { - "name": "[[ 0. 0. 0.]\n [ 0. 0. 0.]\n [ 0. 0. 0.]]" - } - ] - } - ] - }, - { - "name": "mass", - "children": [ - { - "name": "6431.80372889" - } - ] - }, - { - "name": "center_of_gravity", - "children": [ - { - "name": "[ 0. 0. 0.]" - } - ] - } - ] - } - ] - }, - { - "name": "air_conditioner", - "children": [ - { - "name": "origin", - "children": [ - { - "name": "[[0.0, 0.0, 0.0]]" - } - ] - }, - { - "name": "symmetric", - "children": [ - { - "name": "False" - } - ] - }, - { - "name": "tag", - "children": [ - { - "name": "Component" - } - ] - }, - { - "name": "mass_properties", - "children": [ - { - "name": "volume", - "children": [ - { - "name": "0.0" - } - ] - }, - { - "name": "moments_of_inertia", - "children": [ - { - "name": "center", - "children": [ - { - "name": "[ 0. 0. 0.]" - } - ] - }, - { - "name": "tensor", - "children": [ - { - "name": "[[ 0. 0. 0.]\n [ 0. 0. 0.]\n [ 0. 0. 0.]]" - } - ] - } - ] - }, - { - "name": "mass", - "children": [ - { - "name": "1156.6605435" - } - ] - }, - { - "name": "center_of_gravity", - "children": [ - { - "name": "[ 0. 0. 0.]" - } - ] - } - ] - } - ] - }, - { - "name": "passenger_weights", - "children": [ - { - "name": "origin", - "children": [ - { - "name": "[[0.0, 0.0, 0.0]]" - } - ] - }, - { - "name": "symmetric", - "children": [ - { - "name": "False" - } - ] - }, - { - "name": "tag", - "children": [ - { - "name": "Component" - } - ] - }, - { - "name": "mass_properties", - "children": [ - { - "name": "volume", - "children": [ - { - "name": "0.0" - } - ] - }, - { - "name": "moments_of_inertia", - "children": [ - { - "name": "center", - "children": [ - { - "name": "[ 0. 0. 0.]" - } - ] - }, - { - "name": "tensor", - "children": [ - { - "name": "[[ 0. 0. 0.]\n [ 0. 0. 0.]\n [ 0. 0. 0.]]" - } - ] - } - ] - }, - { - "name": "mass", - "children": [ - { - "name": "17349.9081525" - } - ] - }, - { - "name": "center_of_gravity", - "children": [ - { - "name": "[ 0. 0. 0.]" - } - ] - } - ] - } - ] - }, - { - "name": "costs", - "children": [ - { - "name": "industrial", - "children": [ - { - "name": "hourly_rates", - "children": [ - { - "name": "engineering", - "children": [ - { - "name": "0.0" - } - ] - }, - { - "name": "manufacturing", - "children": [ - { - "name": "0.0" - } - ] - }, - { - "name": "quality_control", - "children": [ - { - "name": "0.0" - } - ] - }, - { - "name": "tooling", - "children": [ - { - "name": "0.0" - } - ] - } - ] - }, - { - "name": "development_total_years", - "children": [ - { - "name": "0.0" - } - ] - }, - { - "name": "cad_factor", - "children": [ - { - "name": "1.0" - } - ] - }, - { - "name": "test_facilities_cost", - "children": [ - { - "name": "0.0" - } - ] - }, - { - "name": "escalation_factor", - "children": [ - { - "name": "0.0" - } - ] - }, - { - "name": "production_total_units", - "children": [ - { - "name": "0.0" - } - ] - }, - { - "name": "material_factor", - "children": [ - { - "name": "1.0" - } - ] - }, - { - "name": "manufacturing_facilities_cost", - "children": [ - { - "name": "0.0" - } - ] - }, - { - "name": "avionics_cost", - "children": [ - { - "name": "0.0" - } - ] - }, - { - "name": "stealth", - "children": [ - { - "name": "0.0" - } - ] - }, - { - "name": "tag", - "children": [ - { - "name": "industrial_costs" - } - ] - }, - { - "name": "units_to_amortize", - "children": [ - { - "name": "None" - } - ] - }, - { - "name": "reference_year", - "children": [ - { - "name": "0.0" - } - ] - }, - { - "name": "aircraft_type", - "children": [ - { - "name": "None" - } - ] - }, - { - "name": "prototypes_units", - "children": [ - { - "name": "0.0" - } - ] - }, - { - "name": "difficulty_factor", - "children": [ - { - "name": "1.0" - } - ] - } - ] - }, - { - "name": "tag", - "children": [ - { - "name": "costs" - } - ] - }, - { - "name": "operating", - "children": [ - { - "name": "insure_rate", - "children": [ - { - "name": "0.0" - } - ] - }, - { - "name": "reference_dollars", - "children": [ - { - "name": "0.0" - } - ] - }, - { - "name": "maintenance_rate", - "children": [ - { - "name": "0.0" - } - ] - }, - { - "name": "oil_price", - "children": [ - { - "name": "0.0" - } - ] - }, - { - "name": "crew_rate", - "children": [ - { - "name": "0.0" - } - ] - }, - { - "name": "tag", - "children": [ - { - "name": "operating_costs" - } - ] - }, - { - "name": "fuel_price", - "children": [ - { - "name": "0.0" - } - ] - }, - { - "name": "pilot_rate", - "children": [ - { - "name": "0.0" - } - ] - }, - { - "name": "depreciate_years", - "children": [ - { - "name": "0.0" - } - ] - }, - { - "name": "inflator", - "children": [ - { - "name": "0.0" - } - ] - } - ] - } - ] - } - ] -} \ No newline at end of file diff --git a/_site/guides/docs.html b/_site/guides/docs.html deleted file mode 100644 index 260b3a37..00000000 --- a/_site/guides/docs.html +++ /dev/null @@ -1,256 +0,0 @@ - - - - - - - - Using the Documentation - SUAVE - - - - - - - - - - - - - - -
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Using the Documentation

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How to Read (and Write) the Documentation

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This is an explanation of how documentation is built in SUAVE so that the user can know what to look for and how to write it if they wish to add their own code. The doxygen page is available here.

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Docstrings

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All classes and functions in SUAVE have docstrings have docstrings. These give the user an understanding of what the function does and information on the input and output variables.

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Classes

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For a class, the docstring has three parts:

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  • General description
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The general description provides a brief summary of what the class is used for. Assumptions list any significant assumptions are important in how it is used. This may be listed as None or N/A if there are no important assumptions. The source section should provide the general source of methods in the class. If there is no overall source, a message like ‘see sources in functions’ may be appropriate. There are also cases where a source is not relevant, such as simple geometric functions, and may also be listed as None or N/A.

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Class Docstring Template

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This is the general template that can be used when creating a new class. It should be placed directly under the class declaration.

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"""<Description>
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-<source>
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Functions

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For functions there are six categories:

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This is a general description of what the function does. It should also include any key information that does not fit into one of the other categories.

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This should contain any assumptions made by the function. None or N/A can be used if none are used.

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The source of any methods that have been implemented. Simple methods like basic geometric relations do not need a source.

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This should contain any variables or functions passed to the function. If the passed variable is a data structure, the components that are used should be listed. Each item should include a description if it is not obvious from the name. It should also include any relevant units. In addition, information about the variable type or any other information that might be important can be added here.

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This should contain the same information as in the inputs. It may also contain information on variables that are modified but not explicitly returned.

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This carries the same information as input and outputs. It typically contains variables that are properties of the parent class but are not modified. There is some overlap with inputs and outputs, but either category is acceptable as long as the variable is documented.

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Function Docstring Template

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This is a template docstring:

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-    <input1> <units>
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-    <output1> <units>
-    <output2> <units>
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-    Properties Used:
-    <property1> <units>
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Doxygen Grouping Tags

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Tags are used to put files into groups that match the SUAVE file structure. @defgroup tags define a group and should be placed in the init file. An example is shown here:

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## @defgroup Analyses-Aerodynamics Aerodynamics
-# These are the analyses that control aerodynamic evaluations.
-# @ingroup Analyses
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In this example, Analyses-Aerodynamics is the doxygen tag for the group, while the group appears in the documentation as Aerodynamics, the next part of the string. The tag is based on the file structure (Analyses/Aerodynamics here). Since this is a subgroup of Analyses, @ingroup Analyses is used here, with Analyses as the doxygen tag for the next level up.

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In files, the @ingroup tag should be inserted before all classes and stand-alone functions. The tag should match the tag in the folder init file’s @defgroup string.

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- - - - - - - - - - diff --git a/_site/guides/energy_structure.html b/_site/guides/energy_structure.html deleted file mode 100644 index 47d50b5d..00000000 --- a/_site/guides/energy_structure.html +++ /dev/null @@ -1,244 +0,0 @@ - - - - - - - - Energy Networks - SUAVE - - - - - - - - - - - - - - -
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Energy Networks

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##Energy Networks -Energy networks are really a fancy name for your propulsion system. The reason we call them a network rather than “engine” or the like is that it encompasses far more than that. These “energy networks” are the complex systems that future aircraft will incorporate that can reduce or eliminate fuel burn. For example if you have a hybrid gas-electric aircraft you don’t have just an engine. You have an engine, a motor, batteries, a generator, a gearbox, a propeller or ducted fan, wiring, electronics… and that doesn’t include the parts inside the internal combustion engine. Modeling these systems completely is essential in designing such a vehicle.

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To do this we depart from the typical SUAVE structure of analyses and methods. This was done because we want to look at each component of the network individually. All components behave in their own ways. The purpose of the network is to link together every component in the system to work together.

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File Structure

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One of the biggest sources of confusion for energy networks is the file structure. The files for every part of a network are located at trunk/SUAVE/Components/Energy. Within that we have several subfolders.

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/Converters

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Converters are defined as component that takes energy or power from one form to another. It could be electrical to mechanical, or even chemical to mechanical, etc.. Examples in this folder include a motor, a solar panel, and the compressor section of a jet engine.

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/Distributors

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Distributors move power from one part of the network to another. The common use of this is an electronic speed controller for a small UAV.

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/Networks

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This is where all the “Network” scripts that tie together all of the pieces are kept. Examples in here are a turbofan network.

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/Peripherals

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Peripherals are items that rely on the network but do not produce thrust or power for the vehicle. For example, avionics require electricity which must be accounted for.

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/Processes

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Processes are non tangible parts of a network that are necessary. For example the process is thrust. This function is useful for jet engines to combine and dimensionalize the final thrust once all the components are combined in the network.

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Storages, for now, include batteries. However, in the future we could have fuel tanks here. Currently fuel is only handled as a mass variation.

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Component Example

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Below is a simple example of the most basic energy component in SUAVE. All energy components are classes. The A solar panel is a converter since it converts a photonic flux calculated by a solar radiation model and converts it to a power.

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# Solar_Panel.py
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-# Created:  Jun 2014, E. Botero
-# Modified: Jan 2016, T. MacDonald
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-# ----------------------------------------------------------------------
-#  Imports
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-# suave imports
-import SUAVE
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-from SUAVE.Components.Energy.Energy_Component import Energy_Component
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-# ----------------------------------------------------------------------
-#  Solar_Panel Class
-# ----------------------------------------------------------------------
-class Solar_Panel(Energy_Component):
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-    def __defaults__(self):
-        self.area       = 0.0
-        self.efficiency = 0.0
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-    def power(self):
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-        # Unpack
-        flux       = self.inputs.flux
-        efficiency = self.efficiency
-        area       = self.area
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-        p = flux*area*efficiency
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-        # Store to outputs
-        self.outputs.power = p
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-        return p
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These classes contain functions that simulate a process. Multiple functions can exist within a component. This component has defaults, inputs, and outputs. Defaults are provided that give the user an idea of what the fixed parameters of the component are. These values are set when initializing a vehicle. This is the recipe that all energy components are built off.

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Network Scripts

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Network scripts are the link between these components. The network script allows you to reconfigure the connection between components to create your dream propulsion system. These must be logically created as components have set inputs and outputs. For example, you can’t magically go from a battery to a propeller without anything in between. Some knowledge of the inputs and outputs are necessary, however they’re generally quite intuitive. One interesting avenue for SUAVE is that you can create networks of networks.

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The linking process works like this:

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    # step 1
-    solar_flux.solar_radiation(conditions)
-    # link
-    solar_panel.inputs.flux = solar_flux.outputs.flux
-    # step 2
-    solar_panel.power()
-    # link
-    solar_logic.inputs.powerin = solar_panel.outputs.power
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Notice the first step above is to calculate the solar radiation. Once the solar radiation is calculated the components are linked and step 2 can continue with the the power being calculated. From there a solar logic component will use that power.

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The other main hallmark of a network is that they are called at every point in the mission to calculate the state of the system. Given some conditions data that defines the state of the vehicle the components must provide back to the mission being solved a thrust force and a mass rate. Other outputs can be stored back to conditions, however a thrust and a mass rate must be returned.

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Vehicle Script Setup of a Network

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Here we will provide a snippet of the turbofan setup for a B737.

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-#  Component 3 - Low Pressure Compressor
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-# instantiate 
-compressor = SUAVE.Components.Energy.Converters.Compressor()    
-compressor.tag = 'low_pressure_compressor'
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-# setup
-compressor.polytropic_efficiency = 0.91
-compressor.pressure_ratio        = 1.14    
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-# add to network
-turbofan.append(compressor)
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In the above example, a compressor is added to the network. The compressor is tagged as the low_pressure_compressor to distinguish it from the high pressure compressor. The polytropic efficiency and pressure ratio are set. Finall it is appended to the network.

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Tutorials

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Examples for Getting Started

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These are tutorials for SUAVE. The tutorials will then help you get started with SUAVE. We recommend starting with the Boeing 737-800 tutorial and then moving to the Transport Optimization or the Turbofan Network tutorial. These will allow you to explore the capabilities of SUAVE. If you haven't already downloaded the latest accompanying tutorial scripts you can find them here.

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Mission Solver Structure

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Mission Solver Code Structure

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This is a high level overview of how the mission solver functions. The purpose is to show the structure that is used for an existing mission, and show where changes should be made if different functionality is desired.

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File Structure

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Mission scripts are split into two folders in the SUAVE repository. The first is in trunk/SUAVE/Analyses/Mission/Segments, and the second is in trunk/SUAVE/Methods/Missions/Segments. As with other types of analyses and methods, the distinction between these is that the Analyses folder contains classes that are built to use functions stored in the Methods folder. This division is done to make it easier to build new analysis classes using a mix of available methods.

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A typical mission segment analysis file contains four keys parts. The first specifies default user inputs, unknowns, and residuals. The inputs are used to provide the analysis with conditions that need to be met, while the unknowns and residuals are used as part of the solution process. The second sets the initialization functions for the analysis, which are run at the beginning. The third picks the convergence method and specifies the functions that will be used during iteration. The fourth finalizes the data and processes it for results output.

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Initialization

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For this tutorial, we will be considering the constant speed constant altitude cruise segment. The files are available here (Analysis) and here (Method). This class also inherits information from more general segment classes, which include many of the processing functions. As with other segments, the user will specify key conditions. For this case, altitude, air speed, and distance are the necessary inputs. If the user does not specify an altitude, it will be taken automatically from the last value in the previous segment. These inputs must be specified in some way for the mission segment to be evaluated. They are shown below as well:

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self.altitude  = None
-self.air_speed = 10. * Units['km/hr']
-self.distance  = 10. * Units.km
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The other set of segment specific initial values are the values used for solving the segment (typically this means satisfying a force balance at every evaluation point). These can be changed by the user if needed, but the default values should perform fine for most cases.

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self.state.unknowns.throttle   = ones_row(1) * 0.5
-self.state.unknowns.body_angle = ones_row(1) * 0.0
-self.state.residuals.forces    = ones_row(2) * 0.0
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Here throttle and body angle are the unknowns, and the values shown here are the values they will start at. The residuals will be computed based on these unknowns, so their initial value is not important. Instead they are initialized just to create the necessary data structure. The ones_row line will create a numpy array with the number of elements needed for evaluation.

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Evaluation Details

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Most of the missions in SUAVE, including this one, are broken into several points in time based on a Chebyshev polynomial. This causes the points to be closer together at either end of the segment. The choice of a Chebyshev polynomial (which creates cosine spacing) provides better convergence and smoothness properties versus other methods such as linear spacing.

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At each of these points the aerodynamic analysis is queried to find CL and CD, which are then converted to lift and drag. These values will be dependent on the body angle unknown and other aerodynamic parameters. Thrust is found from the vehicle’s energy network, which is dependent on the throttle unknown. A weight is determined by looking at the initial weight and subsequent mass rate (typically corresponding with fuel burn). In this cruise segment, these forces are summed in 2D and the results are put in the residuals. The functions needed to arrive these forces are found in the Update Conditions section of the Analysis file. This section is also shown below in one of the steps to create a new mission.

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Once the evaluation process has been performed at all points, the unknowns and residuals are fed back to the solve routine, which in this case is scipy’s fsolve. The file that performs this process is here. This routine continues evaluating the points until convergence is reached. Once this happens, post processing is done to put the data in the results output.

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Using Multiple Segments

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Multiple segments can be run sequentially by appending them in the desired order. Examples of this are in all the tutorial files that have an aircraft fly a full mission. In addition, the full mission can be run simultaneously will all segment constraints used together. If you are interested in doing something like this, please ask us about it on our forum.

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Process Summary

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Mission Setup

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  • Initializes default values for unknowns
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  • Initializes set of functions used to determine residuals
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  • Reads user input for segment parameters
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  • Adds the analysis group to be used (including the vehicle and items like atmosphere)
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  • Appends segments in order
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Evaluate

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  • Varies unknowns until residual convergence is reached using scipy’s fsolve
  • -
  • Repeats process for each segment until full mission is complete
  • -
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Adding New Mission Segments

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The segment described above uses two unknowns to solve force residuals in two dimensions. This general setup works well for many problems of interest, but SUAVE is designed to accommodate other mission analysis types as well. A user may want to add control surface deflection and solve for moments as well, or look at forces in all three dimensions.

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In addition, a user may want to modify how the mission is flown, as is done with the many other segments currently available. They may want to modify how the mission is solved, such as is done in our single point evaluation segments where finite differencing is not relevant.

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Here we will explain the process of modifying our constant speed constant rate climb segment to be constant throttle constant speed. This still uses 2D force balance but changes the profile. There are four functions that are modified here. The first is shown below. The functions can be found in here and here

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def initialize_conditions(segment,state):
-
-    # unpack
-    climb_rate = segment.climb_rate
-    air_speed  = segment.air_speed   
-    alt0       = segment.altitude_start 
-    altf       = segment.altitude_end
-    t_nondim   = state.numerics.dimensionless.control_points
-    conditions = state.conditions  
-
-    # check for initial altitude
-    if alt0 is None:
-        if not state.initials: raise AttributeError('initial altitude not set')
-        alt0 = -1.0 * state.initials.conditions.frames.inertial.position_vector[-1,2]
-
-    # discretize on altitude
-    alt = t_nondim * (altf-alt0) + alt0
-    
-    # process velocity vector
-    v_mag = air_speed
-    v_z   = -climb_rate # z points down
-    v_x   = np.sqrt( v_mag**2 - v_z**2 )
-    
-    # pack conditions    
-    conditions.frames.inertial.velocity_vector[:,0] = v_x
-    conditions.frames.inertial.velocity_vector[:,2] = v_z
-    conditions.frames.inertial.position_vector[:,2] = -alt[:,0] # z points down
-    conditions.freestream.altitude[:,0]             =  alt[:,0] # positive altitude in this context
-
- -

This function initializes speed and altitude based on the given climb rate, airspeed, and altitude end points. t_nondim gives nondimensional time in cosine spacing from 0 to 1 in order to pick the values at the points to be evaluated. Unfortunately, when we use constant throttle we cannot know beforehand exactly how altitude (or climb rate in this case) will vary with time, so altitude cannot be spaced with this method. Instead a different function is used to initialize conditions:

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def initialize_conditions(segment,state):
-
-    # unpack
-    throttle   = segment.throttle
-    air_speed  = segment.air_speed   
-    alt0       = segment.altitude_start 
-    altf       = segment.altitude_end
-    t_nondim   = state.numerics.dimensionless.control_points
-    conditions = state.conditions  
-
-    # check for initial altitude
-    if alt0 is None:
-        if not state.initials: raise AttributeError('initial altitude not set')
-        alt0 = -1.0 * state.initials.conditions.frames.inertial.position_vector[-1,2]
-
-    # pack conditions  
-    conditions.propulsion.throttle[:,0] = throttle
-    conditions.frames.inertial.velocity_vector[:,0] = air_speed # start up value
-
- -

Here only the throttle and air speed are loaded in, and discretization of other values will need to occur later so that it is part of the iteration loop. This requires a new function that updates the altitude differentials.

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def update_differentials_altitude(segment,state):
-
-    # unpack
-    t = state.numerics.dimensionless.control_points
-    D = state.numerics.dimensionless.differentiate
-    I = state.numerics.dimensionless.integrate
-
-    
-    # Unpack segment initials
-    alt0       = segment.altitude_start 
-    altf       = segment.altitude_end    
-    conditions = state.conditions  
-
-    r = state.conditions.frames.inertial.position_vector
-    v = state.conditions.frames.inertial.velocity_vector
-    
-    # check for initial altitude
-    if alt0 is None:
-        if not state.initials: raise AttributeError('initial altitude not set')
-        alt0 = -1.0 * state.initials.conditions.frames.inertial.position_vector[-1,2]    
-    
-    # get overall time step
-    vz = -v[:,2,None] # Inertial velocity is z down
-    dz = altf- alt0    
-    dt = dz / np.dot(I[-1,:],vz)[-1] # maintain column array
-    
-    # Integrate vz to get altitudes
-    alt = alt0 + np.dot(I*dt,vz)
-
-    # rescale operators
-    t = t * dt
-
-    # pack
-    t_initial = state.conditions.frames.inertial.time[0,0]
-    state.conditions.frames.inertial.time[:,0] = t_initial + t[:,0]
-    conditions.frames.inertial.position_vector[:,2] = -alt[:,0] # z points down
-    conditions.freestream.altitude[:,0]             =  alt[:,0] # positive altitude in this context    
-
-    return
-
- -

In this function, t, D, and I are numpy arrays that allow approximate differentiation and integration. Since the total time is not known without determining the climb rate, we must first determine the time required to reach the final altitude. The line dt = dz / np.dot(I[-1,:],vz)[-1] does this with the integrator providing the amount of altitude gained if the velocities were spread across just one second instead of the full segment time. This gives the scaling quantity dt that is then used to get the altitude at every point in alt = alt0 + np.dot(I*dt,vz). The values for altitude are then are then packed for use in other functions.

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The above allows us to deal with discretization without a known profile, but we also must calculate the velocity in order to use this. This is done with another added function.

- -
def update_velocity_vector_from_wind_angle(segment,state):
-
-    # unpack
-    conditions = state.conditions 
-    v_mag  = segment.air_speed 
-    alpha  = state.unknowns.wind_angle[:,0][:,None]
-    theta  = state.unknowns.body_angle[:,0][:,None]
-    
-    # Flight path angle
-    gamma = theta-alpha
-    
-    # process
-    v_x =  v_mag * np.cos(gamma)
-    v_z = -v_mag * np.sin(gamma) # z points down
-    
-    # pack
-    conditions.frames.inertial.velocity_vector[:,0] = v_x[:,0]
-    conditions.frames.inertial.velocity_vector[:,2] = v_z[:,0]
-    
-    return conditions
-
- -

This uses our new set of unknowns to determine the velocities.

- -

Additionally, since the unknowns are different we must change the function that unpacks them. Wind angle does not need to be stored so it is not included here.

- -
def unpack_body_angle(segment,state):
-
-    # unpack unknowns
-    theta  = state.unknowns.body_angle
-    
-    # apply unknowns
-    state.conditions.frames.body.inertial_rotations[:,1] = theta[:,0]
-
- -

We now add these functions to the segment process list.

- -
    # --------------------------------------------------------------
-    #   Initialize - before iteration
-    # --------------------------------------------------------------
-    initialize = self.process.initialize
-    
-    initialize.expand_state            = Methods.expand_state
-    initialize.differentials           = Methods.Common.Numerics.initialize_differentials_dimensionless
-    initialize.conditions              = Methods.Climb.Constant_Throttle_Constant_Speed.initialize_conditions
-    initialize.velocities              = Methods.Climb.Constant_Throttle_Constant_Speed.update_velocity_vector_from_wind_angle
-    initialize.differentials_altitude  = Methods.Climb.Constant_Throttle_Constant_Speed.update_differentials_altitude      
-
- -

and

- -
    # Unpack Unknowns
-    iterate.unknowns = Process()
-    iterate.unknowns.mission           = Methods.Climb.Constant_Throttle_Constant_Speed.unpack_body_angle 
-    
-    # Update Conditions
-    iterate.conditions = Process()
-    iterate.conditions.velocities      = Methods.Climb.Constant_Throttle_Constant_Speed.update_velocity_vector_from_wind_angle
-    iterate.conditions.differentials_a = Methods.Climb.Constant_Throttle_Constant_Speed.update_differentials_altitude
-    iterate.conditions.differentials_b = Methods.Common.Numerics.update_differentials_time
-    iterate.conditions.acceleration    = Methods.Common.Frames.update_acceleration
-    iterate.conditions.altitude        = Methods.Common.Aerodynamics.update_altitude
-    iterate.conditions.atmosphere      = Methods.Common.Aerodynamics.update_atmosphere
-    iterate.conditions.gravity         = Methods.Common.Weights.update_gravity
-    iterate.conditions.freestream      = Methods.Common.Aerodynamics.update_freestream
-    iterate.conditions.orientations    = Methods.Common.Frames.update_orientations
-    iterate.conditions.aerodynamics    = Methods.Common.Aerodynamics.update_aerodynamics
-    iterate.conditions.stability       = Methods.Common.Aerodynamics.update_stability
-    iterate.conditions.propulsion      = Methods.Common.Energy.update_thrust
-    iterate.conditions.weights         = Methods.Common.Weights.update_weights
-    iterate.conditions.forces          = Methods.Common.Frames.update_forces
-    iterate.conditions.planet_position = Methods.Common.Frames.update_planet_position
-
- -

If you have any questions that are not answered in other tutorials or the FAQ please ask on our forum page. This is also the place to go if you want help building a more elaborate evaluation, such as one that includes moments.

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Optimization Structure

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Optimization Code Structure

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This is an overview of how optimization is done in SUAVE. A specific tutorial case is also available here.

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Nexus Class

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The Nexus class is the underlying data structure that is used for optimization. It is created to hold all data and functionality needed to link together optimizers and the various analysis modules in SUAVE. Detailed information on each of the functions can be found on our doxygen page.

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Standard Optimization File Structure

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These are the standard files that are used in the optimization process. They are typically stored as Optimize.py, Vehicle.py, Analysis.py, Mission.py, Procedure.py, and Plot_Mission.py. These names can be changed if desired.

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Optimize

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This is the top level file that is run to perform the optimization. Inputs, objective, constraints, and aliases are specified here. The inputs have an initial value, bounds, a scaling factor, and the units used. This provides later functions with the information needed to vary the parameters. Units.less indicates a unitless quantity. SI units are the default in SUAVE’s internal calculations, so Units.meter will not modify the internal value, while something like Units.foot will.

- -
problem.inputs = np.array([
-    [ 'wing_area'     ,  125.  , (   120.   ,   180.   )  ,   100.  , Units.meter**2],
-    [ 'aspect_ratio'  ,  3.3   , (   2.0    ,   6.0    )  ,   10.   , Units.less],
-])
-
- -

Constraints and the objective are similar. Both have scaling quantities and constraints also have bounds.

- -
problem.constraints = np.array([
-    [ 'design_range_fuel_margin', '>', 0., 1E-1, Units.less]
-])
-
-problem.objective = np.array([
-    ['fuel_burn_rate', 1., Units.kg/Units.s]
-])
-
- -

Finally we have aliases. This provides the optimization process with the position of the various parameters in the data structure. Aliases are used so that short names can be used for variables and a single variable can control multiple items in the data structure. Controlling multiple items can be important if different vehicle configurations are used at different points in the mission, and one of the vehicle parameters should change in the same way for all of the configurations. We can use * as a wildcard. This is used below to change the aspect ratio of the main wing in every vehicle configuration.

- -
problem.aliases = [
-    [ 'wing_area'       ,   ['vehicle_configurations.base.wings.main_wing.areas.reference',
-                                              'vehicle_configurations.base.reference_area']],
-    [ 'aspect_ratio'    ,    'vehicle_configurations.*.wings.main_wing.aspect_ratio'       ],
-    [ 'fuel_burn_rate'  ,    'summary.fuel_burn_rate'                                      ],
-]    
-
- -

This file then specifies the configurations, analyses, missions, and procedure that will be used. This are typically contained in separate files and more details on each are below. Once all of this is specified, the desired optimizer is called with the nexus class created by this setup.

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Vehicle Setup

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This contains the vehicle information such as geometric data and configurations. It is the same as the vehicle setup used for basic analysis purposes.

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Analysis Setup

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This contains information on what analyses should be run for the vehicle. For example if correlation-based aerodynamics or AVL should be used for computations. It requires vehicle information from the previous step.

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Mission Setup

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This is also the same as the standard mission setup. It determines how the mission will be flown. It requires analysis information from the previous step.

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Procedure

- -

This is an optimization specific file that determines how the vehicle, analysis, or mission is modified with the input values in the optimization and also runs the mission. For example, changing the wing area will usually require changes to other wing parameters, such as root chord length. This module reads the new inputs and changes other values accordingly based on user specified processes.

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Plotting

- -

This function is not necessary to the optimization, but is often included in the files used and is added to the optimize main call as a way to visualize the results.

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Optimizer Interface

- -

The other step that must be taken to perform an optimization is to convert the standardized input above into values that can be used by the selected optimizer. This is done through a separate script for each optimizer, all of which are found in the optimization folder.

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For example, if we are using PyOpt to optimize, we might use output = pyopt_setup.Pyopt_Solve(problem,solver='SNOPT') in the main function of the top level optimizer. This function reads the inputs, constraints, and objective and converts them to a format that the selected optimizer (SNOPT here) can understand.

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Evaluation Process

- -

This shows the typical evaluation process, including where items like inputs and aliases are used. This chart assumes a single objective call, but some optimizers will include calls such as all_constraints which require another evaluation. If the evaluation is a duplicate, data from the previous evaluation will be used instead of stepping through the procedure again.

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Incorporating Multi-fidelity

- -

Multiple levels of fidelity are designed to be relatively easy to incorporate in SUAVE, but there are still a few things to keep in mind. First, the chosen optimizer must support multi-fidelity and be able to change the nexus.fidelity_level value. Once this is done, it is also important to remember that the mission is set up based on the analyses. This means that if a change is made to the analyses then the mission must be rebuilt with the new settings. As an example, code below for changing the analysis level is shown. This is a function that has been added to the procedure file.

- -
def set_fidelity_level(nexus):
-    
-    if nexus.has_key('fidelity_level') == False:
-        print 'Fidelity level not set, defaulting to 1'
-        nexus.fidelity_level = 1
-
-    if nexus.fidelity_level == 2:
-        aerodynamics = SUAVE.Analyses.Aerodynamics.Supersonic_OpenVSP_Wave_Drag()
-        aerodynamics.settings.number_slices    = 20
-        aerodynamics.settings.number_rotations = 10        
-    elif nexus.fidelity_level == 1:
-        aerodynamics = SUAVE.Analyses.Aerodynamics.Supersonic_Zero()
-    else:
-        raise ValueError('Selected fidelity level not supported')
-    aerodynamics.geometry = copy.deepcopy(nexus.vehicle_configurations.base)
-    nexus.analyses.base.append(aerodynamics)
-    
-    nexus.missions = mission_as2.setup(nexus.analyses)
-    
-    return nexus
-
- -

Here we see that nexus.missions has been updated in addition to nexus.analyses, since failing to do this would have the mission run with the previous analysis settings.

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Key Functions in the Optimizer Setup

- -

We briefly mentioned how optimization parameters would need to be converted so that they could run with a particular optimizer. Here we show how this is managed and show which functions are likely to be useful in building a new optimizer setup.

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The key items that will be needed for most optimizers are shown below, taken from the PyOpt setup:

- -
inp = problem.optimization_problem.inputs
-obj = problem.optimization_problem.objective
-con = problem.optimization_problem.constraints  
-   
-# Set inputs
-nam = inp[:,0] # Names
-ini = inp[:,1] # Initials
-bnd = inp[:,2] # Bounds
-scl = inp[:,3] # Scale
-typ = inp[:,4] # Type
-
- -

These can be scaled with two helper functions that are part of the SUAVE distribution:

- -
from SUAVE.Optimization import helper_functions as help_fun
-
-bnd_constraints    = help_fun.scale_const_bnds(con)
-scaled_constraints = help_fun.scale_const_values(con,bnd_constraints)
-x                  = ini/scl
-
- -

What happens next is entirely dependent on what optimizer you want to use. Some may require that constraint bounds happen at 0 or are either > or <. However this setup is done, you will likely need to create a function that can accept the problem and inputs and give required outputs such as the objective value and constraints. In the PyOpt case, this is done with a simple wrapper and an added function:

- -
mywrap = lambda x:PyOpt_Problem(problem,x)
-
- -

- -
def PyOpt_Problem(problem,x):
-   
-	obj   = problem.objective(x)
-	const = problem.all_constraints(x).tolist()
-	fail  = np.array(np.isnan(obj.tolist()) or np.isnan(np.array(const).any())).astype(int)
-
-   
-	print 'Inputs'
-	print x
-	print 'Obj'
-	print obj
-	print 'Con'
-	print const
-   
-	return obj,const,fail
-
- -

Please visit our forum if you have any other questions on how the optimizer interface works or how to convert the values to what you need.

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Payload Range Diagram

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Embraer E-190 Payload Range Diagram Tutorial

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1) Locate the tutorial script folder.

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2) Open the test_payload_range.py script in your favorite editor or IDE.

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3) Similar to the B737-800 Tutorial, the setup is divided into steps.

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4) For the Payload Range Diagram, besides the vehicle and mission, the user must provide the following inputs:

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    -
  • cruise_segment_tag: You must enter the tag of the segment which will have its length modified in order to comply with required fuel burn for each one of the payload range diagram points.
  • -
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  • -
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5) The tutorial presents the following definition:

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# run payload diagram	
-cruise_segment_tag = "Cruise"
-reserves = 1750.
-payload_range_results = payload_range(vehicle,mission,cruise_segment_tag,reserves)
-
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6) First, let’s just run it as it is for now. Run the script in either the IDE or in a terminal as python tut_payload_range.py

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7) After the calculations are completed, the payload diagram will be plotted and the data will be stored in a file named ‘PayloadRangeDiagram.dat’. This is in the folder where you run the script.

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8) You can try to modify vehicle and/or mission parameters and see how the payload range diagram is affected. For now, let’s add some drag counts to the airplane:

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    -
  • Locate and open the script test_mission_Embraer_E190_constThr.py, in the tutorial folder (this is the script that contains the vehicle and mission setups)
  • -
  • Locate base_analysis() and then the Aerodynamics Analysis text block (line 113)
  • -
  • Add 50 drag counts to the vehicle (line 115): aerodynamics.settings.drag_coefficient_increment = 0.0050
  • -
  • Rerun the script as before and notice the changes in the results.
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9) Similarly the mission parameters can be changed. Again, this lets the user decide what changes they want to explore.

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Regional Jet Optimization

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Regional Jet Optimization Tutorial

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This tutorial assumes familiarity with SUAVE and knowledge of the information in the Boeing 737-800 analysis tutorial. It provides a specific case of the more general information provided in the optimization structure tutorial, and some more information on how to modify the code for different uses.

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Some important files for the optimization problem can be seen below

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Important Files :

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Optimize.py:

-

Defines the optimization framework of the problem, wherein one minimizes an assigned objective, subject to certain constraints, by altering some design variables.

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In order to ensure that the subfunctions can communicate with eachother, and that SUAVE can communicate with the external optimizer, a special data object called the “Nexus” is used. The nexus object contains all of the vehicles, missions, results, and other important information. It alters these values at each optimizer iteration, depending on the input parameters defined in Optimize.py.

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In this particular setup, there are two design variables: wing area and cruise altitude. The objective is fuel burn, and there is only one constraint: fuel margin. The default inputs are defined in the following lines.

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# [ tag, initial, (lb,ub), scaling, units]
-problem.inputs = np.array([
-	[ 'wing_area'      ,  95., ( 90., 130.), 100., Units.meter**2],
-	[ 'cruise_altitude',  11., (  9.,  14.),  10., Units.km      ],
-])
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Each input parameter takes in 5 values; a tag (an identification to communicate between the optimizer and SUAVE), an initial value, set of bounds, a scale factor (many optimizers tend to be more effective when the input values are of order 1), as well as the units used.

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The objective and constraints are defined in the lines below.

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# [ tag, scaling, units ]
-problem.objective = np.array([
-	[ 'fuel_burn', 10000, Units.kg ]
-])
-
-# [ tag, sense, edge, scaling, units ]
-problem.constraints = np.array([
-	[ 'design_range_fuel_margin' , '>', 0., 1E-1, Units.less],
-])
-
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Note that in this case, only a single constraint is used; Multiple constraints may be used using a list format, similar to the input variables.

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This file also defines the “aliasing,” i.e. how the design variables, constraints, and objective map to the variables used in Procedure.py (which is where the problem is evaluated). The aliases for this problem are defined in the lines below. Note that the first entry refers to the tag defined in either problem.inputs, problem.objective, or problem.constraints.

- -
problem.aliases = [
-	[ 'wing_area'                        ,   ['vehicle_configurations.*.wings.main_wing.areas.reference',
-	                                          'vehicle_configurations.*.reference_area'                    ]],  
-	[ 'cruise_altitude'                  ,    'missions.base.segments.climb_5.altitude_end'                 ],
-	[ 'fuel_burn'                        ,    'summary.base_mission_fuelburn'                               ],
-	[ 'design_range_fuel_margin'         ,    'summary.max_zero_fuel_margin'                                ],
-]    
-
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Note that, sometimes, a single input can map to multiple outputs, such as the “wing_area” design variable; in this case, use a list for the outputs, as seen above. The use of a wild card “*”, can also allow values to map to multiple outputs. Values to be outputted cannot contain wild cards as that would be ambiguous to an optimizer.

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Procedure.py:

-

This links everything together by defining the steps you would use to size and analyze the aircraft at each optimizer iteration.

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This file contains a number of subfunctions to alter the vehicle and mission. The function setup() instantiates the procedure, defining the functions that are called at each step of the optimizer in their order of execution.

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  1. -

    simple_sizing() defines the geometry of the aircraft based on the input parameters (in this case, wing area and cruise altitude).

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    weights() determines the weight breakdown of the aircraft

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    mission() decides which missions are run at each step, as well as the design mission of the aircraft

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Each step of the procedure takes the nexus object as an input, and returns the object as an output, ensuring that the data is available for handling.

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Vehicles.py:

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Initializes the vehicle (or vehicles if desired) used in the optimization problem. This includes two subfunctions: base_setup(), where the vehicle structure is itself defined, including the fuselage, wing, vertical and horizontal tails, and the propulsion system.

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configs_setup() takes in the vehicle that was defined in base_setup() and defines other configurations (such as takeoff and landing, which include different flap settings). This may be used to define other parameters, such as changing the sweep angle of a variable-sweep-wing at higher Mach Numbers, or changing a propulsion component.

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Missions.py:

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Initializes the missions that are run at each iteration. In this case, only a single mission is run.

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Analyses.py:

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Defines the set of features that are used in this particular problem (e.g. weights correlations, aerodynamics correlations, etc.).

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Plot_Mission.py:

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Plots the mission outputs.

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Running the Problem:

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  1. -

    Locate the tutorial script folder “Regional_Jet_Optimization.”

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  2. -
  3. -

    Open the Optimize.py script in a text editor or IDE. You will see this line near the top of main():

    - -

    output = problem.objective()

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  4. -
  5. -

    This runs the problem with the default inputs. Run the file using an IDE or type python Optimize.py in the command line. You should see a set of output plots.

    -
  6. -
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Running a Sweep of the Inputs

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Now try running a 2D sweep of the problem to observe the shape of the design space: comment output = problem.objective then uncomment the following (the next line down in the code).

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variable_sweep(problem)
-
- -

Then run the program again. This could take a few minutes. The results should look like the plot below.

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2D Sweep

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The labeled lines depict the fuel margin (i.e. fraction of the aircraft remaining weight that can be loaded with fuel). Positive values indicate a feasible design. Fuel burn is shown in the colored contours. Note that a smoother plot may be created by changing the number of points in the sweep function, but this will take more time. A carpet plot run using 400 points on can be seen below. A local minimum is now visible.

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2D Sweep_20

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Note: If you run this 400 point case yourself you may see messages indicating that a segment did not converge. This is normal and can happen when a mission is run far from a feasible point. In this case, it does not have a negative impact on the results.

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Optimizing:

- -

Now try running an Optimization. Recomment variable_sweep(problem) then uncomment the lines below:

- -
output = scipy_setup.SciPy_Solve(problem,solver='SLSQP')
-print output
-
- -

and run the file again.

- -

From the default inputs, the terminal (or IDE output) should display an optimum of [ 1.08980937 1.02089232], which corresponds to a wing area of 109 m^2, and 10.2 km. It appears to have found the local minimum.

- -

Now try starting the optimization from a different initial guess. You can either modify the input parameters in the initial formulation (the relevant lines are repeated below with the modification)

- -
#   [ tag                            , initial, (lb,ub)             , scaling , units ]
-problem.inputs = np.array([
-    [ 'wing_area'                    ,  128   , (   90. ,   130.   ) ,   100. , Units.meter**2],
-    [ 'cruise_altitude'              ,  13.8  , (   9   ,    14.   ) ,   10.  , Units.km],
-])
-
- -

or set up the optimization problem and change the inputs manually by uncommenting the following lines.

- -
inputs                                   = [1.28, 1.38]
-scaling                                  = problem.optimization_problem.inputs[:,3] # have to 
-										   rescale inputs to start problem from here
-scaled_inputs                            = np.multiply(inputs,scaling)
-problem.optimization_problem.inputs[:,1] = scaled_inputs
-output = scipy_setup.SciPy_Solve(problem,solver='SLSQP')
-print output        
-
- -

This starts the optimization problem above the feasible region (wing area = 128 m^2, altitude = 13.8 km), and results in a fuel burn that is 30 kg lower than the result using the initial guess. This illustrates the important of choosing a starting point when running optimization problem. Additionally, this demonstrates SUAVE’s ability to handle infeasible cases, showing that it can converge to a feasible case even when starting from an infeasible set of initial inputs.

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At this point, you can explore other starting points, or alter the vehicle or mission properties in Vehicles.py or Missions.py. Additionally, feel free to start using this as the basis for creating custom optimization scripts.

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Solar UAV

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The purpose of this tutorial is to educate users on how to setup a preconfigured solar energy network to work with a high altitude solar UAV. In this tutorial it is assumed that the user has some familiarity with SUAVE having completed the fundamental tutorial for the Boeing 737-800. You will learn about setting up the following:

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  • Solar missions,
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  • Solar panels,
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  • Batteries,
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Because of the flexible nature of SUAVE, the approach shown is just one way to setup the UAV for analysis. By experimenting and eventually developing your own code you will be able to do far more than what is shown in this tutorial. The original script can be found in the tutorial repository as tut_solar_uav.py.

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Vehicle and Mission

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The vehicle is similar to the Qinetiq Zephyr but far larger at 40 meters in wing span and a weight of 200 kg. However, it does carry double the payload of the Zephyr at 5 kg and accounts for constant payload power usage. The battery energy density is set to an optimistic estimate of 450 Watt-hours per kg. Additionally, 90 percent of the wings are covered with solar panels that have a 25 percent efficiency.

- -

This mission exercises the methods developed for solar radiation estimation, propeller and motor integration, as well as the human powered aircraft weight estimation. The mission setup is a constant altitude cruise at 15 km at Mach 0.12 for about 24 hours. The location is over the California Bay Area during the summer solstice.

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Setup

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This tutorial highlights the differences between setting up a typical aircraft like a Boeing 737 and a solar UAV.

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Mission Setup

- -

For a solar UAV, the starting location as well as the day and time are critical. So the first segment must be modified to include this information. It is important to note that the start times provided are in “Zulu” time or Greenwich Mean Time. This is typical for aircraft navigation to prevent time zone errors and ambiguity.

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segment.state.numerics.number_control_points = 64
-segment.start_time                           = time.strptime("Tue, Jun 21 11:30:00  2015", "%a, %b %d %H:%M:%S %Y",)
-segment.altitude                             = 15.0  * Units.km 
-segment.mach                                 = 0.12
-segment.distance                             = 3050.0 * Units.km
-segment.battery_energy                       = vehicle.propulsors.network.battery.max_energy*0.2 #Set the battery charge to start
-segment.latitude                             = 37.4300
-segment.longitude                            = -122.1700
-
- -

Additionally, this mission is highly simplified. It consists of only one mission segment. To provide ample resolution the number of control points have been increased to 64.

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Structural Weight Sizing

- -

The vehicle sizing of the human powered aircraft or solar UAV requires the dimensions of the vehicle like in other weight estimation methods. However, it also requires information about the number of wing ribs and the number of end ribs. The end ribs are relevant for wing designs where the sections can come apart for transportation.

- -
wing.number_ribs             = 26.
-wing.number_end_ribs         = 2.
-
- -

Wing Boundary Layer Transition

- -

The transition location of the boundary layer can have a great impact on the drag of the wing. This is especially important in properly designed low Reynolds number flows when laminar flow can be extended for larger percentages of the surface. The code snippet below is how surfaces have transition points set. These are estimates provided from the designer based on experience.

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wing.transition_x_upper      = 0.6
-wing.transition_x_lower      = 1.0
-
- -

Solar Panels

- -

The solar panel model is quite simple and only requires a capture area, an efficiency, and mass. In this case we assume that 90% of the wing area is covered in solar panels.

- -
panel.area                 = vehicle.reference_area * 0.9
-panel.efficiency           = 0.25
-panel.mass_properties.mass = panel.area*(0.60 * Units.kg)
-
- -

Batteries

- -

The batteries are set up with knowledge of the mass of the battery and the specific energy. In this case a futuristic specific energy of 450 Watt-hr/kg is set for lithium ion type batteries. The resistance of the batteries is another important input to determine charging and discharging losses.

- -
bat = SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion()
-bat.mass_properties.mass = 55.0 * Units.kg
-bat.specific_energy      = 450.*Units.Wh/Units.kg
-bat.resistance           = 0.05
-initialize_from_mass(bat,bat.mass_properties.mass)
-net.battery              = bat
-
- -

Propeller

- -

To setup the propeller we will actually design an optimized propeller. This is done through the methods provided by Adkins and Liebeck. The attributes of the propeller design are then seeded to the motor and network to accelerate convergence of the propeller and motor models.

- -
prop_attributes = Data()
-prop_attributes.number_blades       = 2.0
-prop_attributes.freestream_velocity = 40.0 # freestream m/s
-prop_attributes.angular_velocity    = 150. * Units['rpm']
-prop_attributes.tip_radius          = 4.25
-prop_attributes.hub_radius          = 0.05
-prop_attributes.design_Cl           = 0.7
-prop_attributes.design_altitude     = 14.0 * Units.km
-prop_attributes.design_thrust       = 0.0
-prop_attributes.design_power        = 3500.0
-prop_attributes                     = propeller_design(prop_attributes)
-
-prop = SUAVE.Components.Energy.Converters.Propeller()
-prop.prop_attributes = prop_attributes
-net.propeller        = prop
-
- -

Motor

- -

This motor model relies on data that is generally available from motor manufacturers. This includes the resistance, no load current, and the speed constant. Additionally, any gearbox is specified here and basic information about the propeller is entered here to help inform the solver when converging the motor and propeller analyses.

- -
motor = SUAVE.Components.Energy.Converters.Motor()
-motor.resistance           = 0.008
-motor.no_load_current      = 4.5
-motor.speed_constant       = 120. * Units['rpm'] # RPM/volt converted to (rad/s)/volt      
-motor.propeller_radius     = prop.prop_attributes.tip_radius
-motor.propeller_Cp         = prop.prop_attributes.Cp
-motor.gear_ratio           = 12. # Gear ratio
-motor.gearbox_efficiency   = .98 # Gear box efficiency
-motor.expected_current     = 160. # Expected current
-motor.mass_properties.mass = 2.0
-net.motor                  = motor   
-
- -

Running

- -

As you should be familiar with by now, running this script is just like any other.

-
python tut_solar_uav.py
-
- -

Results

- -

If all went well the script ran and it provided you with more plots than you ever wanted. Here are some of the plots that were generated when we ran it:

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solar_flux

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battery charging

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battery energy

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Solar UAV Optimization

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Solar UAV Optimization Tutorial

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The purpose of this tutorial is to illustrate a different type of problem. We assume you have gone through the first optimization tutorial: Regional Jet Optimization. This tutorial will illustrate a little more complex setup that modifies a mission parameter.

- -

Your objective is simple: get a small UAV to fly from San Francisco to San Diego. In fact you can pose that as an optimization problem, with some constraints that govern how it works. There is no requirement to minimize this or maximize that. Of course you could try to minimize something, but you just want something that works for now. Later iterations can do fancier things.

- -

Next we will go into detail about some of the required files. Analyses.py and Plot_mission.py are straightforward from prior tutorials. So we will not go into those in detail, except to say that we are using a UAV weight model in Analyses.py.

- -

Optimize.py:

- -

Let’s pose the optimization problem first and then setup the rest. We start with the Nexus first as usual. With this design problem there are things you are uncertain of and want to solve for.

- -

You’re not sure if you really need any solar panels on the airplane, so to start there will be none. The solar ratio is the ratio of wing area to solar area. A value of 1 would the whole top of the wing covered with solar panels.

- -

-	  # [ tag , initial, [lb,ub], scaling, units ]
-    problem.inputs = np.array([
-        [ 'wing_area'       ,   0.5, (  0.1,    1.5 ),    0.5, Units.meter      ],
-        [ 'aspect_ratio'    ,  10.0, (  5.0,   20.0 ),   10.0, Units.less       ], 
-        [ 'dynamic_pressure', 125.0, (  1.0, 2000.0 ),  125.0, Units.pascals    ], 
-        [ 'solar_ratio'     ,   0.0, (  0.0,    0.97),    1.0, Units.less       ], 
-        [ 'kv'              , 800.0, ( 10.0, 1500.0 ),  800.0, Units['rpm/volt']], 
-    ])
-
- -

Next come the constraints. The first constraint is that the battery energy can never go negative, the math behind this will be elaborated on later. The next constraint is that the plane must have a battery. Finally there are limits to coefficients of lift and throttle settings.

- -

-      # [ tag, sense, edge, scaling, units ]
-    problem.constraints = np.array([
-        [ 'energy_constraint', '=', 0.0, 1.0, Units.less],
-        [ 'battery_mass'     , '>', 0.0, 1.0, Units.kg  ],       
-        [ 'CL'               , '>', 0.0, 1.0, Units.less],
-        [ 'Throttle_min'     , '>', 0.0, 1.0, Units.less],
-        [ 'Throttle_max'     , '>', 0.0, 1.0, Units.less],
-    ])
-
- -

Notice here that all constraints are greater than zero. This is because SciPy’s SLSQP optimization algorithm assumes this form. To correct for these, the values are adjusted in Procedure.py. Other optimization packages such as PyOpt don’t require this strict form.

- -

Finally, the objective. It’s nothing of course! As long as the constraints are met, the goal of the design is satisfied.

- -

-    # [ tag, scaling, units ]
-    problem.objective = np.array([
-         [ 'Nothing', 1. , Units.kg],
-    ])
-
- -

Vehicles.py:

- -

Next, you will setup the vehicle. This is very similar to the prior Solar UAV tutorial. So we will gloss over this, the one noticeable difference is that a lower fidelity energy network is used. This means that most components operate with prescribed efficiencies. For example:

- -

-    # Component 4 the Motor
-    motor = SUAVE.Components.Energy.Converters.Motor_Lo_Fid()
-    kv                         = 800. * Units['rpm/volt'] # RPM/volt is standard
-    motor                      = size_from_kv(motor, kv)    
-    motor.gear_ratio           = 1. # Gear ratio, no gearbox
-    motor.gearbox_efficiency   = 1. # Gear box efficiency, no gearbox
-    motor.motor_efficiency     = 0.825;
-    net.motor                  = motor  
-    ])
-
- -

Missions.py:

- -

Now for the mission setup. Here we assume it will take 1000 km and the plane will cruise off the coast at 1000 feet in altitude. The distance is a bit longer than the straight line distance, but we’re not going to fly through populated areas. The heading, or body rotation, must be set to account for the changes in latitude and longitude to accurately calculate the solar radiation. We will cruise at a constant altitude and assume it takes no time to climb and descend compared to the cruise time.

- -

-    segment.state.numerics.number_control_points = 50
-    segment.dynamic_pressure = 115.0 * Units.pascals
-    segment.start_time       = time.strptime("Tue, Jun 21  11:00:00  2016", "%a, %b %d %H:%M:%S %Y",)
-    segment.altitude         = 1000.0 * Units.feet
-    segment.distance         = 1000.0 * Units.km
-    segment.charge_ratio     = 1.0
-    segment.latitude         = 37.4
-    segment.longitude        = -122.15
-    segment.state.conditions.frames.wind.body_rotations[:,2] = 125.* Units.degrees 
-
- -

Procedure.py:

- -

Finally we have the procedure setup. In the procedure, we resize the vehicle, calculate weights, finalize the analyses, solve the mission, and post process.

- -

Some notes about sizing. Each wing component (main wing, horizontal tail, and vertical tail) needs the surfaces sized based on its area and aspect ratio. Next the solar panels are sized based on the wing area and solar_ratio. Finally the motor is resized based on correlations for the speed constant of the motor.

- -

-def simple_sizing(nexus):
-    
-    # Pull out the vehicle
-    vec = nexus.vehicle_configurations.base
-    
-    # Change the dynamic pressure based on the, add a factor of safety   
-    vec.envelope.maximum_dynamic_pressure = nexus.missions.mission.segments.cruise.dynamic_pressure*1.2
-    
-    # Scale the horizontal and vertical tails based on the main wing area
-    vec.wings.horizontal_stabilizer.areas.reference = 0.15 * vec.reference_area
-    vec.wings.vertical_stabilizer.areas.reference   = 0.08 * vec.reference_area
-
-    # wing spans,areas, and chords
-    for wing in vec.wings:
-        
-        # Unpack
-        AR = wing.aspect_ratio
-        S  = wing.areas.reference
-        
-        # Set the spans
-        wing.spans.projected = np.sqrt(AR*S)
-        
-        # Set all of the areas for the surfaces
-        wing.areas.wetted   = 2.0 * S
-        wing.areas.exposed  = 1.0 * wing.areas.wetted
-        wing.areas.affected = 1.0 * wing.areas.wetted   
-        
-        # Set all of the chord lengths
-        chord = wing.areas.reference/wing.spans.projected
-        wing.chords.mean_aerodynamic = chord
-        wing.chords.mean_geometric   = chord
-        wing.chords.root             = chord
-        wing.chords.tip              = chord
-
-    # Size solar panel area
-    wing_area                   = vec.reference_area
-    spanel                      = vec.propulsors.network.solar_panel
-    sratio                      = spanel.ratio
-    solar_area                  = wing_area*sratio
-    spanel.area                 = solar_area
-    spanel.mass_properties.mass = solar_area*(0.60 * Units.kg)    
-    
-    # Resize the motor
-    motor = vec.propulsors.network.motor
-    kv    = motor.speed_constant
-    motor = size_from_kv(motor, kv)    
-    
-    # diff the new data
-    vec.store_diff()
-
-    return nexus
-
- -

Here the battery is sized and charged. The battery weight consists of everything that is left over from sizing.

- -

-def weights_battery(nexus):
-
-    # Evaluate weights for all of the configurations
-    config = nexus.analyses.base
-    config.weights.evaluate() 
-    
-    vec     = nexus.vehicle_configurations.base
-    payload = vec.propulsors.network.payload.mass_properties.mass  
-    msolar  = vec.propulsors.network.solar_panel.mass_properties.mass
-    MTOW    = vec.mass_properties.max_takeoff
-    empty   = vec.weight_breakdown.empty
-    mmotor  = vec.propulsors.network.motor.mass_properties.mass
-    
-    # Calculate battery mass
-    batmass = MTOW - empty - payload - msolar -mmotor
-    bat     = vec.propulsors.network.battery
-    initialize_from_mass(bat,batmass)
-    vec.propulsors.network.battery.mass_properties.mass = batmass
-        
-    # Set Battery Charge
-    maxcharge = nexus.vehicle_configurations.base.propulsors.network.battery.max_energy
-    charge    = maxcharge
-    
-    nexus.missions.mission.segments.cruise.battery_energy = charge 
-
-    return nexus
-
- -

The next we run the mission and post process the results. The post_process function will setup the information of importance for the user. The energy constraint is a way of ensuring that nowhere in the mission the battery energy goes negative. The coefficient of lift is limited to 1.2. The throttle is limited to 0.9, to make sure there is excess throttle to climb. Throttle is also limited from going negative. Finally, the objective, nothing is specified to be zero.

- -

-def post_process(nexus):
-    
-    # Unpack
-    mis = nexus.missions.mission.segments.cruise
-    vec = nexus.vehicle_configurations.base
-    res = nexus.results.mission.segments.cruise.conditions
-    
-    # Final Energy
-    maxcharge    = vec.propulsors.network.battery.max_energy
-    
-    # Energy constraints, the battery doesn't go to zero anywhere, using a P norm
-    p                    = 8.    
-    energies             = res.propulsion.battery_energy[:,0]/np.abs(maxcharge)
-    energies[energies>0] = 0.0 # Exclude the values greater than zero
-    energy_constraint    = np.sum((np.abs(energies)**p))**(1/p) 
-
-    # CL max constraint, it is the same throughout the mission
-    CL = res.aerodynamics.lift_coefficient[0]
-    
-    # Pack up
-    summary = nexus.summary
-    summary.CL                = 1.2 - CL
-    summary.energy_constraint = energy_constraint
-    summary.throttle_min      = res.propulsion.throttle[0]
-    summary.throttle_max      = 0.9 - res.propulsion.throttle[0]
-    summary.nothing           = 0.0
-    
-    return nexus    
-
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Results

-

Let’s look at the results:

- -

-Optimization terminated successfully.    (Exit mode 0)
-            Current function value: [0.0]
-            Iterations: 4
-            Function evaluations: 29
-            Gradient evaluations: 4
-[ 1.12963146  1.43880081  1.39329626  0.65589785  0.97171879]
-Design Variable Table:
-
-[['wing_area' 0.5648157324099996 (0.1, 1.5) 0.5 1.0]
- ['aspect_ratio' 14.388008119672202 (5.0, 20.0) 10.0 1.0]
- ['dynamic_pressure' 174.16203234031317 (1.0, 2000.0) 125.0 1.0]
- ['solar_ratio' 0.6558978486767236 (0.0, 0.97) 1.0 1.0]
- ['kv' 777.3750338508712 (10.0, 1500.0) 800.0 0.10471975511965977]]
-
-Constraint Table:
-
-[['energy_constraint' 0.0 '=' 0.0 1.0 <Quantity(1.0, 'less')>]
- ['battery_mass' 4.939962596982861 '>' 0.0 1.0 <Quantity(1.0, 'kilogram')>]
- ['CL' 0.5309682332699428 '>' 0.0 1.0 <Quantity(1.0, 'less')>]
- ['Throttle_min' 0.7319219623084848 '>' 0.0 1.0 <Quantity(1.0, 'less')>]
- ['Throttle_max' 0.1680780376915152 '>' 0.0 1.0 <Quantity(1.0, 'less')>]]
-
- -

Okay looks like SciPy found a feasible solution without too much time. Now let’s review the plots.

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battery_energy

- -

So we can tell now that the battery energy doesn’t go all the way to zero. Let’s look at how the solar flux varies throughout the day and how that affects the draw from the battery.

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solar flux

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battery draw

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So maybe those solar panels actually are worth it. They seem to decrease the load on the battery considerably during the daytime.

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SUAVE Code Style Guide

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SUAVE is built on a slightly modified PEP8 style guide, with changes made to implement a data-oriented view of the code. To help support discovering code, the SUAVE folder structure explicitly mirrors the package structure. Flexibility of the package structure is important, so in general all objects live in their own file, with the same file name as the object name. In order to maintain a separation between Analysis and Data structures, there are often parallel package trees inside the main branches of the package, like SUAVE.Methods.Aerodynamics and SUAVE.Analysis.Aerodynamics. Where possible the names of fields that live in the SUAVE package are written out verbosely, avoiding jargon built on mathematical variable names or acronyms.

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Templates for new methods and objects can be found in the SUAVE repo’s templates folder.

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Naming Convention

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In terms of typography –

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  • any_variable_name - lower case with underscore
    - This includes working variables and instantiated objects.
  • -
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    - The underscores are chosen here to permit the inclusion of acronyms if needed and to maintain symmetry with field name styling.
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    - For example folders within the SUAVE package.
  • -
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In terms of naming –

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    -
  • Chunk similar field types under a containing field
  • -
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  • -
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Development Life Cycle

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As you develop new features for SUAVE, this is generally how you can expect your feature to evolve, in terms of its level of abstraction, and where it lives.

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    Prototype
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    -A lot of development can be accomplished in a local environment.

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  3. Initial Integration
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    At this point you might want to initiate a pull request to contribute the code back to the main repository.

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  5. Full-Blown Subpackage
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Turbofan Network

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Turbofan Modeling Tutorial

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This tutorial describes how the energy network framework in SUAVE can be used to build a model of a turbofan engine. Once this is clear to the user, understanding the setup of the other gasturbine models, the ducted fan and the turbojet will be much easier. The turbofan model is built with several turbofan components as its building blocks. These are then linked together through their inputs and outputs. The script to follow is the tut_mission_B737.py script that was used in the Boeing 737-800 Analysis Tutorial

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Setting up the Turbofan model

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First the turbofan energy network is instantiated. The parameters associated with the network as a whole are assigned.

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# ------------------------------------------------------------------
-#   Turbofan Network
-# ------------------------------------------------------------------    
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-#instantiate the gas turbine network
-turbofan = SUAVE.Components.Energy.Networks.Turbofan()
-turbofan.tag = 'turbofan'
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-# setup
-turbofan.bypass_ratio      = 5.4
-turbofan.number_of_engines = 2.0
-turbofan.engine_length     = 2.5
-turbofan.nacelle_diameter  = 1.580
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-# working fluid
-turbofan.working_fluid = SUAVE.Attributes.Gases.Air()
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Then the different components are added

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Components

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The basic components used to model the turbofan are described below.

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Ram

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The ‘Ram’ component is used to convert the freestream quantities that are passed into the turbofan network into stagnation quantities. As the turbofan network is based on a 1D gasdynamic analysis, most of the energy transfer across the different components are modelled as changes in the stagnation quantities. Thus the Ram component acts as a preprocessor converting the input conditions into quantities required by the network.

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# ------------------------------------------------------------------
-#   Component 1 - Ram
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-# to convert freestream static to stagnation quantities
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-# instantiate
-ram = SUAVE.Components.Energy.Converters.Ram()
-ram.tag = 'ram'
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-# add to the network
-turbofan.append(ram)
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Nozzle

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The ‘Nozzle’ component is used to model the inlet diffuser, the outlet fan, and the compressor nozzles as shown below.

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# ------------------------------------------------------------------
-#  Component 2 - Inlet Nozzle
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-# instantiate
-inlet_nozzle = SUAVE.Components.Energy.Converters.Compression_Nozzle()
-inlet_nozzle.tag = 'inlet_nozzle'
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-# setup
-inlet_nozzle.polytropic_efficiency = 0.98
-inlet_nozzle.pressure_ratio        = 0.98
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-# add to network
-turbofan.append(inlet_nozzle)
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-# ------------------------------------------------------------------
-#  Component 8 - Core Nozzle
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-# instantiate
-nozzle = SUAVE.Components.Energy.Converters.Expansion_Nozzle()   
-nozzle.tag = 'core_nozzle'
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-# setup
-nozzle.polytropic_efficiency = 0.95
-nozzle.pressure_ratio        = 0.99    
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-# add to network
-turbofan.append(nozzle)
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-# ------------------------------------------------------------------
-#  Component 9 - Fan Nozzle
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-# instantiate
-nozzle = SUAVE.Components.Energy.Converters.Expansion_Nozzle()   
-nozzle.tag = 'fan_nozzle'
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-# setup
-nozzle.polytropic_efficiency = 0.95
-nozzle.pressure_ratio        = 0.99    
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-# add to network
-turbofan.append(nozzle)
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Compressor

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Two compressors are used in the turbofan model, a low and a high pressure compressor.

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# ------------------------------------------------------------------
-#  Component 3 - Low Pressure Compressor
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-# instantiate 
-compressor = SUAVE.Components.Energy.Converters.Compressor()    
-compressor.tag = 'low_pressure_compressor'
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-# setup
-compressor.polytropic_efficiency = 0.91
-compressor.pressure_ratio        = 1.14    
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-# add to network
-turbofan.append(compressor)
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-# ------------------------------------------------------------------
-#  Component 4 - High Pressure Compressor
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-# instantiate
-compressor = SUAVE.Components.Energy.Converters.Compressor()    
-compressor.tag = 'high_pressure_compressor'
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-compressor.polytropic_efficiency = 0.91
-compressor.pressure_ratio        = 13.415    
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-# add to network
-turbofan.append(compressor)
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Fan

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A fan component is also added to the network. If you were to model a turbojet, the fan component and the fan nozzle would not be added but all the other components would remain the same.

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# ------------------------------------------------------------------
-#  Component 10 - Fan
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-# instantiate
-fan = SUAVE.Components.Energy.Converters.Fan()   
-fan.tag = 'fan'
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-# setup
-fan.polytropic_efficiency = 0.93
-fan.pressure_ratio        = 1.7    
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-# add to network
-turbofan.append(fan)
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Combustor

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The combustor component is where the the fuel to air ratio is computed. It is also used to compute the sfc and the thrust later in the network.

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# ------------------------------------------------------------------
-#  Component 7 - Combustor
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-# instantiate    
-combustor = SUAVE.Components.Energy.Converters.Combustor()   
-combustor.tag = 'combustor'
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-# setup
-combustor.efficiency                = 0.99 
-combustor.turbine_inlet_temperature = 1450
-combustor.pressure_ratio            = 0.95
-combustor.fuel_data                 = SUAVE.Attributes.Propellants.Jet_A()    
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-# add to network
-turbofan.append(combustor)
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Turbine

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The work done by the fan and the compressors is used to compute the turbine work required. This is used to compute the change in the stagnation quantities across the turbine.

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# ------------------------------------------------------------------
-#  Component 5 - Low Pressure Turbine
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-# instantiate
-turbine = SUAVE.Components.Energy.Converters.Turbine()   
-turbine.tag='low_pressure_turbine'
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-# setup
-turbine.mechanical_efficiency = 0.99
-turbine.polytropic_efficiency = 0.93     
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-# add to network
-turbofan.append(turbine)
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-# ------------------------------------------------------------------
-#  Component 6 - High Pressure Turbine
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-# instantiate
-turbine = SUAVE.Components.Energy.Converters.Turbine()   
-turbine.tag='high_pressure_turbine'
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-# setup
-turbine.mechanical_efficiency = 0.99
-turbine.polytropic_efficiency = 0.93     
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-# add to network
-turbofan.append(turbine)
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Thrust

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The thrust component takes in the initial (inputs of the inlet nozzle) and final (exit of the fan and core exirt nozzles) stagnation quantities of the network and the fuel to air ratio and computes the specific fuel conspumption (sfc) and thrust generated by the network (turbofan engine).

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# ------------------------------------------------------------------
-#  Component 10 - Thrust
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-# to compute thrust
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-# instantiate
-thrust = SUAVE.Components.Energy.Processes.Thrust()       
-thrust.tag ='thrust'
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-# setup
-thrust.total_design =42383.01
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-# add to network
-turbofan.thrust = thrust   
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Sizing the Turbofan

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Once the network is built, it is essential to size the engine with a set of sizing conditions. The sizing function ‘turbofan_sizing’ takes in the model of the turbofan and the mach number and the altitude for which the turbofan is sized. The sizing thrust is an engine/network property (defined in the ‘Setting up the Turbofan model’ section above). The function takes these quantities and computes the design mass flow rate through the components. Once sized, the network/engine can be added to the vehicle as shown in the B737 tutorial.

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#bypass ratio  closer to fan
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-#design sizing conditions
-altitude      = 35000.0*Units.ft
-mach_number   = 0.78 
-isa_deviation = 0.
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-# add to network
-turbofan.thrust = thrust
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-#size the turbofan (for thrust)
-turbofan_sizing(turbofan,mach_number,altitude)   
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-#compute the turbofan diameter and engine length
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-compute_turbofan_geometry(turbofan,None)
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SUAVE

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An Aerospace Vehicle Environment for Designing Future Aircraft

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SUAVE is a conceptual level aircraft design environment built with the ability to analyze and optimize both conventional and unconventional designs. This capability is achieved in part by allowing analysis information for aircraft to be drawn from multiple sources. Many other software tools for aircraft conceptual design rely on fixed empirical correlations and other handbook approximation. SUAVE instead provides a framework that can be used to design aircraft featuring advanced technologies by augmenting relevant correlations with physics-based methods.

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Blended Wing Body

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While SUAVE is quite capable as built today, its most important strength is in the ease of creating and adding new vehicles, mission types, analyses, and optimizers. This flexibility is aided by SUAVE's status as an open-source Python code. Development is currently led by the Aerospace Design Lab at Stanford University. If you're interested in joining us, please visit our develop page for general instructions or reach out to us though our forum or email.

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Publications

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- We've recently presented papers on the technical background of SUAVE as applied to the analysis and optimization of aerospace vehicles. The first paper describes the initial models available and the motivations for the programming structures used in the package. The second paper details the schematics of setting up optimization problems and sample results. The third paper shows how higher fidelity models can be incorporated into the code. Finally, the fourth paper shows how optimization can be performed with multiple levels of fidelity. -

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-T. Lukaczyk, A. Wendorff, E. Botero, T. MacDonald, T. Momose, A. Variyar, J. M. Vegh, M. Colonno, T. Economon, J. J. Alonso, T. Orra, C. Ilario, "SUAVE: An Open-Source Environment for Multi-Fidelity Conceptual Vehicle Design", 16th AIAA Multidisciplinary Analysis and Optimization Conference, Dallas, TX, June 2015. -

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-E. Botero, A. Wendorff, T. MacDonald, A. Variyar, J. M. Vegh, T. Lukaczyk, J. J. Alonso, T. Orra, C. Ilario da Silva. "SUAVE: An Open-Source Environment for Conceptual Vehicle Design and Optimization", 54th AIAA Aerospace Sciences Meeting, San Diego, CA, January 2016. -

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-T. MacDonald, E. Botero, J. M. Vegh, A. Variyar, J. J. Alonso, T. Orra, C. Ilario da Silva. "SUAVE: An Open-Source Environment Enabling Unconventional Designs through Higher Fidelity", 55th AIAA Aerospace Sciences Meeting, Grapevine, TX, January 2017. -

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-T. MacDonald, M. Clarke, E. Botero, J. M. Vegh, J. J. Alonso. "SUAVE: An Open-Source Environment Enabling Multi-fidelity Vehicle Optimization", 16th AIAA Multidisciplinary Analysis and Optimization Conference, Denver, CO, June 2017. -

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Partners

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Together we design exotic aerospace configurations

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+ @media screen and (max-width: 1280px) { + + .container { + width: 960px; + } + + } + + @media screen and (max-width: 980px) { + + .container { + width: 95%; + } + + } + + @media screen and (max-width: 840px) { + + .container { + width: 95%; + } + + } + + @media screen and (max-width: 736px) { + + .container { + width: 90%; + } + + } + + @media screen and (max-width: 480px) { + + .container { + width: 100%; + } + + } + +/* Row */ + + .row { + display: flex; + flex-wrap: wrap; + box-sizing: border-box; + align-items: stretch; + } + + .row > * { + box-sizing: border-box; + } + + .row.gtr-uniform > * > :last-child { + margin-bottom: 0; + } + + .row.aln-left { + justify-content: flex-start; + } + + .row.aln-center { + justify-content: center; + } + + .row.aln-right { + justify-content: flex-end; + } + + .row.aln-top { + align-items: flex-start; + } + + .row.aln-middle { + align-items: center; + } + + .row.aln-bottom { + align-items: flex-end; + } + + .row > .imp { + order: -1; + } + + 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91.6666666667%; + } + + .row > .off-11 { + margin-left: 91.6666666667%; + } + + .row > .col-12 { + width: 100%; + } + + .row > .off-12 { + margin-left: 100%; + } + + .row.gtr-0 { + margin-top: 0px; + margin-left: 0px; + } + + .row.gtr-0 > * { + padding: 0px 0 0 0px; + } + + .row.gtr-0.gtr-uniform { + margin-top: 0px; + } + + .row.gtr-0.gtr-uniform > * { + padding-top: 0px; + } + + .row.gtr-25 { + margin-top: -12.5px; + margin-left: -12.5px; + } + + .row.gtr-25 > * { + padding: 12.5px 0 0 12.5px; + } + + .row.gtr-25.gtr-uniform { + margin-top: -12.5px; + } + + .row.gtr-25.gtr-uniform > * { + padding-top: 12.5px; + } + + .row.gtr-50 { + margin-top: -25px; + margin-left: -25px; + } + + .row.gtr-50 > * { + padding: 25px 0 0 25px; + } + + .row.gtr-50.gtr-uniform { + margin-top: -25px; + } + + .row.gtr-50.gtr-uniform > * { + padding-top: 25px; + } + + .row { + margin-top: -50px; + margin-left: -50px; + } + + .row > * { + padding: 50px 0 0 50px; + } + + .row.gtr-uniform { + margin-top: -50px; + } + + .row.gtr-uniform > * { + padding-top: 50px; + } + + .row.gtr-150 { + margin-top: -75px; + margin-left: -75px; + } + + .row.gtr-150 > * { + padding: 75px 0 0 75px; + } + + .row.gtr-150.gtr-uniform { + margin-top: -75px; + } + + .row.gtr-150.gtr-uniform > * { + padding-top: 75px; + } + + .row.gtr-200 { + margin-top: -100px; + margin-left: -100px; + } + + .row.gtr-200 > * { + padding: 100px 0 0 100px; + } + + .row.gtr-200.gtr-uniform { + margin-top: -100px; + } + + .row.gtr-200.gtr-uniform > * { + padding-top: 100px; + } + + @media screen and (max-width: 1680px) { + + .row { + display: flex; + flex-wrap: wrap; + box-sizing: border-box; + align-items: stretch; + } + + .row > * { + box-sizing: border-box; + } + + .row.gtr-uniform > * > :last-child { + margin-bottom: 0; + } + + .row.aln-left { + justify-content: flex-start; + } + + .row.aln-center { + justify-content: center; + } + + .row.aln-right { + justify-content: flex-end; + } + + .row.aln-top { + align-items: flex-start; + } + + .row.aln-middle { + align-items: center; + } + + .row.aln-bottom { + align-items: flex-end; + } + + .row > .imp-wide { + order: -1; + } + + .row > .col-1-wide { + width: 8.3333333333%; + } + + .row > .off-1-wide { + margin-left: 8.3333333333%; + } + + .row > .col-2-wide { + width: 16.6666666667%; + } + + .row > .off-2-wide { + margin-left: 16.6666666667%; + } + + .row > .col-3-wide { + width: 25%; + } + + .row > .off-3-wide { + margin-left: 25%; + } + + .row > .col-4-wide { + width: 33.3333333333%; + } + + .row > .off-4-wide { + margin-left: 33.3333333333%; + } + + .row > .col-5-wide { + width: 41.6666666667%; + } + + .row > .off-5-wide { + margin-left: 41.6666666667%; + } + + .row > .col-6-wide { + width: 50%; + } + + .row > .off-6-wide { + margin-left: 50%; + } + + .row > .col-7-wide { + width: 58.3333333333%; + } + + .row > .off-7-wide { + margin-left: 58.3333333333%; + } + + .row > .col-8-wide { + width: 66.6666666667%; + } + + .row > .off-8-wide { + margin-left: 66.6666666667%; + } + + .row > .col-9-wide { + width: 75%; + } + + .row > .off-9-wide { + margin-left: 75%; + } + + .row > .col-10-wide { + width: 83.3333333333%; + } + + .row > .off-10-wide { + margin-left: 83.3333333333%; + } + + .row > .col-11-wide { + width: 91.6666666667%; + } + + .row > .off-11-wide { + margin-left: 91.6666666667%; + } + + .row > .col-12-wide { + width: 100%; + } + + .row > .off-12-wide { + margin-left: 100%; + } + + .row.gtr-0 { + margin-top: 0px; + margin-left: 0px; + } + + .row.gtr-0 > * { + padding: 0px 0 0 0px; + } + + .row.gtr-0.gtr-uniform { + margin-top: 0px; + } + + .row.gtr-0.gtr-uniform > * { + padding-top: 0px; + } + + .row.gtr-25 { + margin-top: -10px; + margin-left: -10px; + } + + .row.gtr-25 > * { + padding: 10px 0 0 10px; + } + + .row.gtr-25.gtr-uniform { + margin-top: -10px; + } + + .row.gtr-25.gtr-uniform > * { + padding-top: 10px; + } + + .row.gtr-50 { + margin-top: -20px; + margin-left: -20px; + } + + .row.gtr-50 > * { + padding: 20px 0 0 20px; + } + + .row.gtr-50.gtr-uniform { + margin-top: -20px; + } + + .row.gtr-50.gtr-uniform > * { + padding-top: 20px; + } + + .row { + margin-top: -40px; + margin-left: -40px; + } + + .row > * { + padding: 40px 0 0 40px; + } + + .row.gtr-uniform { + margin-top: -40px; + } + + .row.gtr-uniform > * { + padding-top: 40px; + } + + .row.gtr-150 { + margin-top: -60px; + margin-left: -60px; + } + + .row.gtr-150 > * { + padding: 60px 0 0 60px; + } + + .row.gtr-150.gtr-uniform { + margin-top: -60px; + } + + .row.gtr-150.gtr-uniform > * { + padding-top: 60px; + } + + .row.gtr-200 { + margin-top: -80px; + margin-left: -80px; + } + + .row.gtr-200 > * { + padding: 80px 0 0 80px; + } + + .row.gtr-200.gtr-uniform { + margin-top: -80px; + } + + .row.gtr-200.gtr-uniform > * { + padding-top: 80px; + } + + } + + @media screen and (max-width: 1280px) { + + .row { + display: flex; + flex-wrap: wrap; + box-sizing: border-box; + align-items: stretch; + } + + .row > * { + box-sizing: border-box; + } + + .row.gtr-uniform > * > :last-child { + margin-bottom: 0; + } + + .row.aln-left { + justify-content: flex-start; + } + + .row.aln-center { + justify-content: center; + } + + .row.aln-right { + justify-content: flex-end; + } + + .row.aln-top { + align-items: flex-start; + } + + .row.aln-middle { + align-items: center; + } + + .row.aln-bottom { + align-items: flex-end; + } + + .row > .imp-normal { + order: -1; + } + + .row > .col-1-normal { + width: 8.3333333333%; + } + + .row > .off-1-normal { + margin-left: 8.3333333333%; + } + + .row > .col-2-normal { + width: 16.6666666667%; + } + + .row > .off-2-normal { + margin-left: 16.6666666667%; + } + + .row > .col-3-normal { + width: 25%; + } + + .row > .off-3-normal { + margin-left: 25%; + } + + .row > .col-4-normal { + width: 33.3333333333%; + } + + .row > .off-4-normal { + margin-left: 33.3333333333%; + } + + .row > .col-5-normal { + width: 41.6666666667%; + } + + .row > .off-5-normal { + margin-left: 41.6666666667%; + } + + .row > .col-6-normal { + width: 50%; + } + + .row > .off-6-normal { + margin-left: 50%; + } + + .row > .col-7-normal { + width: 58.3333333333%; + } + + .row > .off-7-normal { + margin-left: 58.3333333333%; + } + + .row > .col-8-normal { + width: 66.6666666667%; + } + + .row > .off-8-normal { + margin-left: 66.6666666667%; + } + + .row > .col-9-normal { + width: 75%; + } + + .row > .off-9-normal { + margin-left: 75%; + } + + .row > .col-10-normal { + width: 83.3333333333%; + } + + .row > .off-10-normal { + margin-left: 83.3333333333%; + } + + .row > .col-11-normal { + width: 91.6666666667%; + } + + .row > .off-11-normal { + margin-left: 91.6666666667%; + } + + .row > .col-12-normal { + width: 100%; + } + + .row > .off-12-normal { + margin-left: 100%; + } + + .row.gtr-0 { + margin-top: 0px; + margin-left: 0px; + } + + .row.gtr-0 > * { + padding: 0px 0 0 0px; + } + + .row.gtr-0.gtr-uniform { + margin-top: 0px; + } + + .row.gtr-0.gtr-uniform > * { + padding-top: 0px; + } + + .row.gtr-25 { + margin-top: -7.5px; + margin-left: -7.5px; + } + + .row.gtr-25 > * { + padding: 7.5px 0 0 7.5px; + } + + .row.gtr-25.gtr-uniform { + margin-top: -7.5px; + } + + .row.gtr-25.gtr-uniform > * { + padding-top: 7.5px; + } + + .row.gtr-50 { + margin-top: -15px; + margin-left: -15px; + } + + .row.gtr-50 > * { + padding: 15px 0 0 15px; + } + + .row.gtr-50.gtr-uniform { + margin-top: -15px; + } + + .row.gtr-50.gtr-uniform > * { + padding-top: 15px; + } + + .row { + margin-top: -30px; + margin-left: -30px; + } + + .row > * { + padding: 30px 0 0 30px; + } + + .row.gtr-uniform { + margin-top: -30px; + } + + .row.gtr-uniform > * { + padding-top: 30px; + } + + .row.gtr-150 { + margin-top: -45px; + margin-left: -45px; + } + + .row.gtr-150 > * { + padding: 45px 0 0 45px; + } + + .row.gtr-150.gtr-uniform { + margin-top: -45px; + } + + .row.gtr-150.gtr-uniform > * { + padding-top: 45px; + } + + .row.gtr-200 { + margin-top: -60px; + margin-left: -60px; + } + + .row.gtr-200 > * { + padding: 60px 0 0 60px; + } + + .row.gtr-200.gtr-uniform { + margin-top: -60px; + } + + .row.gtr-200.gtr-uniform > * { + padding-top: 60px; + } + + } + + @media screen and (max-width: 980px) { + + .row { + display: flex; + flex-wrap: wrap; + box-sizing: border-box; + align-items: stretch; + } + + .row > * { + box-sizing: border-box; + } + + .row.gtr-uniform > * > :last-child { + margin-bottom: 0; + } + + .row.aln-left { + justify-content: flex-start; + } + + .row.aln-center { + justify-content: center; + } + + .row.aln-right { + justify-content: flex-end; + } + + .row.aln-top { + align-items: flex-start; + } + + .row.aln-middle { + align-items: center; + } + + .row.aln-bottom { + align-items: flex-end; + } + + .row > .imp-narrow { + order: -1; + } + + .row > .col-1-narrow { + width: 8.3333333333%; + } + + .row > .off-1-narrow { + margin-left: 8.3333333333%; + } + + .row > .col-2-narrow { + width: 16.6666666667%; + } + + .row > .off-2-narrow { + margin-left: 16.6666666667%; + } + + .row > .col-3-narrow { + width: 25%; + } + + .row > .off-3-narrow { + margin-left: 25%; + } + + .row > .col-4-narrow { + width: 33.3333333333%; + } + + .row > .off-4-narrow { + margin-left: 33.3333333333%; + } + + .row > .col-5-narrow { + width: 41.6666666667%; + } + + .row > .off-5-narrow { + margin-left: 41.6666666667%; + } + + .row > .col-6-narrow { + width: 50%; + } + + .row > .off-6-narrow { + margin-left: 50%; + } + + .row > .col-7-narrow { + width: 58.3333333333%; + } + + .row > .off-7-narrow { + margin-left: 58.3333333333%; + } + + .row > .col-8-narrow { + width: 66.6666666667%; + } + + .row > .off-8-narrow { + margin-left: 66.6666666667%; + } + + .row > .col-9-narrow { + width: 75%; + } + + .row > .off-9-narrow { + margin-left: 75%; + } + + .row > .col-10-narrow { + width: 83.3333333333%; + } + + .row > .off-10-narrow { + margin-left: 83.3333333333%; + } + + .row > .col-11-narrow { + width: 91.6666666667%; + } + + .row > .off-11-narrow { + margin-left: 91.6666666667%; + } + + .row > .col-12-narrow { + width: 100%; + } + + .row > .off-12-narrow { + margin-left: 100%; + } + + .row.gtr-0 { + margin-top: 0px; + margin-left: 0px; + } + + .row.gtr-0 > * { + padding: 0px 0 0 0px; + } + + .row.gtr-0.gtr-uniform { + margin-top: 0px; + } + + .row.gtr-0.gtr-uniform > * { + padding-top: 0px; + } + + .row.gtr-25 { + margin-top: -7.5px; + margin-left: -7.5px; + } + + .row.gtr-25 > * { + padding: 7.5px 0 0 7.5px; + } + + .row.gtr-25.gtr-uniform { + margin-top: -7.5px; + } + + .row.gtr-25.gtr-uniform > * { + padding-top: 7.5px; + } + + .row.gtr-50 { + margin-top: -15px; + margin-left: -15px; + } + + .row.gtr-50 > * { + padding: 15px 0 0 15px; + } + + .row.gtr-50.gtr-uniform { + margin-top: -15px; + } + + .row.gtr-50.gtr-uniform > * { + padding-top: 15px; + } + + .row { + margin-top: -30px; + margin-left: -30px; + } + + .row > * { + padding: 30px 0 0 30px; + } + + .row.gtr-uniform { + margin-top: -30px; + } + + .row.gtr-uniform > * { + padding-top: 30px; + } + + .row.gtr-150 { + margin-top: -45px; + margin-left: -45px; + } + + .row.gtr-150 > * { + padding: 45px 0 0 45px; + } + + .row.gtr-150.gtr-uniform { + margin-top: -45px; + } + + .row.gtr-150.gtr-uniform > * { + padding-top: 45px; + } + + .row.gtr-200 { + margin-top: -60px; + margin-left: -60px; + } + + .row.gtr-200 > * { + padding: 60px 0 0 60px; + } + + .row.gtr-200.gtr-uniform { + margin-top: -60px; + } + + .row.gtr-200.gtr-uniform > * { + padding-top: 60px; + } + + } + + @media screen and (max-width: 840px) { + + .row { + display: flex; + flex-wrap: wrap; + box-sizing: border-box; + align-items: stretch; + } + + .row > * { + box-sizing: border-box; + } + + .row.gtr-uniform > * > :last-child { + margin-bottom: 0; + } + + .row.aln-left { + justify-content: flex-start; + } + + .row.aln-center { + justify-content: center; + } + + .row.aln-right { + justify-content: flex-end; + } + + .row.aln-top { + align-items: flex-start; + } + + .row.aln-middle { + align-items: center; + } + + .row.aln-bottom { + align-items: flex-end; + } + + .row > .imp-narrower { + order: -1; + } + + .row > .col-1-narrower { + width: 8.3333333333%; + } + + .row > .off-1-narrower { + margin-left: 8.3333333333%; + } + + .row > .col-2-narrower { + width: 16.6666666667%; + } + + .row > .off-2-narrower { + margin-left: 16.6666666667%; + } + + .row > .col-3-narrower { + width: 25%; + } + + .row > .off-3-narrower { + margin-left: 25%; + } + + .row > .col-4-narrower { + width: 33.3333333333%; + } + + .row > .off-4-narrower { + margin-left: 33.3333333333%; + } + + .row > .col-5-narrower { + width: 41.6666666667%; + } + + .row > .off-5-narrower { + margin-left: 41.6666666667%; + } + + .row > .col-6-narrower { + width: 50%; + } + + .row > .off-6-narrower { + margin-left: 50%; + } + + .row > .col-7-narrower { + width: 58.3333333333%; + } + + .row > .off-7-narrower { + margin-left: 58.3333333333%; + } + + .row > .col-8-narrower { + width: 66.6666666667%; + } + + .row > .off-8-narrower { + margin-left: 66.6666666667%; + } + + .row > .col-9-narrower { + width: 75%; + } + + .row > .off-9-narrower { + margin-left: 75%; + } + + .row > .col-10-narrower { + width: 83.3333333333%; + } + + .row > .off-10-narrower { + margin-left: 83.3333333333%; + } + + .row > .col-11-narrower { + width: 91.6666666667%; + } + + .row > .off-11-narrower { + margin-left: 91.6666666667%; + } + + .row > .col-12-narrower { + width: 100%; + } + + .row > .off-12-narrower { + margin-left: 100%; + } + + .row.gtr-0 { + margin-top: 0px; + margin-left: 0px; + } + + .row.gtr-0 > * { + padding: 0px 0 0 0px; + } + + .row.gtr-0.gtr-uniform { + margin-top: 0px; + } + + .row.gtr-0.gtr-uniform > * { + padding-top: 0px; + } + + .row.gtr-25 { + margin-top: -7.5px; + margin-left: -7.5px; + } + + .row.gtr-25 > * { + padding: 7.5px 0 0 7.5px; + } + + .row.gtr-25.gtr-uniform { + margin-top: -7.5px; + } + + .row.gtr-25.gtr-uniform > * { + padding-top: 7.5px; + } + + .row.gtr-50 { + margin-top: -15px; + margin-left: -15px; + } + + .row.gtr-50 > * { + padding: 15px 0 0 15px; + } + + .row.gtr-50.gtr-uniform { + margin-top: -15px; + } + + .row.gtr-50.gtr-uniform > * { + padding-top: 15px; + } + + .row { + margin-top: -30px; + margin-left: -30px; + } + + .row > * { + padding: 30px 0 0 30px; + } + + .row.gtr-uniform { + margin-top: -30px; + } + + .row.gtr-uniform > * { + padding-top: 30px; + } + + .row.gtr-150 { + margin-top: -45px; + margin-left: -45px; + } + + .row.gtr-150 > * { + padding: 45px 0 0 45px; + } + + .row.gtr-150.gtr-uniform { + margin-top: -45px; + } + + .row.gtr-150.gtr-uniform > * { + padding-top: 45px; + } + + .row.gtr-200 { + margin-top: -60px; + margin-left: -60px; + } + + .row.gtr-200 > * { + padding: 60px 0 0 60px; + } + + .row.gtr-200.gtr-uniform { + margin-top: -60px; + } + + .row.gtr-200.gtr-uniform > * { + padding-top: 60px; + } + + } + + @media screen and (max-width: 736px) { + + .row { + display: flex; + flex-wrap: wrap; + box-sizing: border-box; + align-items: stretch; + } + + .row > * { + box-sizing: border-box; + } + + .row.gtr-uniform > * > :last-child { + margin-bottom: 0; + } + + .row.aln-left { + justify-content: flex-start; + } + + .row.aln-center { + justify-content: center; + } + + .row.aln-right { + justify-content: flex-end; + } + + .row.aln-top { + align-items: flex-start; + } + + .row.aln-middle { + align-items: center; + } + + .row.aln-bottom { + align-items: flex-end; + } + + .row > .imp-mobile { + order: -1; + } + + .row > .col-1-mobile { + width: 8.3333333333%; + } + + .row > .off-1-mobile { + margin-left: 8.3333333333%; + } + + .row > .col-2-mobile { + width: 16.6666666667%; + } + + .row > .off-2-mobile { + margin-left: 16.6666666667%; + } + + .row > .col-3-mobile { + width: 25%; + } + + .row > .off-3-mobile { + margin-left: 25%; + } + + .row > .col-4-mobile { + width: 33.3333333333%; + } + + .row > .off-4-mobile { + margin-left: 33.3333333333%; + } + + .row > .col-5-mobile { + width: 41.6666666667%; + } + + .row > .off-5-mobile { + margin-left: 41.6666666667%; + } + + .row > .col-6-mobile { + width: 50%; + } + + .row > .off-6-mobile { + margin-left: 50%; + } + + .row > .col-7-mobile { + width: 58.3333333333%; + } + + .row > .off-7-mobile { + margin-left: 58.3333333333%; + } + + .row > .col-8-mobile { + width: 66.6666666667%; + } + + .row > .off-8-mobile { + margin-left: 66.6666666667%; + } + + .row > .col-9-mobile { + width: 75%; + } + + .row > .off-9-mobile { + margin-left: 75%; + } + + .row > .col-10-mobile { + width: 83.3333333333%; + } + + .row > .off-10-mobile { + margin-left: 83.3333333333%; + } + + .row > .col-11-mobile { + width: 91.6666666667%; + } + + .row > .off-11-mobile { + margin-left: 91.6666666667%; + } + + .row > .col-12-mobile { + width: 100%; + } + + .row > .off-12-mobile { + margin-left: 100%; + } + + .row.gtr-0 { + margin-top: 0px; + margin-left: 0px; + } + + .row.gtr-0 > * { + padding: 0px 0 0 0px; + } + + .row.gtr-0.gtr-uniform { + margin-top: 0px; + } + + .row.gtr-0.gtr-uniform > * { + padding-top: 0px; + } + + .row.gtr-25 { + margin-top: -5px; + margin-left: -5px; + } + + .row.gtr-25 > * { + padding: 5px 0 0 5px; + } + + .row.gtr-25.gtr-uniform { + margin-top: -5px; + } + + .row.gtr-25.gtr-uniform > * { + padding-top: 5px; + } + + .row.gtr-50 { + margin-top: -10px; + margin-left: -10px; + } + + .row.gtr-50 > * { + padding: 10px 0 0 10px; + } + + .row.gtr-50.gtr-uniform { + margin-top: -10px; + } + + .row.gtr-50.gtr-uniform > * { + padding-top: 10px; + } + + .row { + margin-top: -20px; + margin-left: -20px; + } + + .row > * { + padding: 20px 0 0 20px; + } + + .row.gtr-uniform { + margin-top: -20px; + } + + .row.gtr-uniform > * { + padding-top: 20px; + } + + .row.gtr-150 { + margin-top: -30px; + margin-left: -30px; + } + + .row.gtr-150 > * { + padding: 30px 0 0 30px; + } + + .row.gtr-150.gtr-uniform { + margin-top: -30px; + } + + .row.gtr-150.gtr-uniform > * { + padding-top: 30px; + } + + .row.gtr-200 { + margin-top: -40px; + margin-left: -40px; + } + + .row.gtr-200 > * { + padding: 40px 0 0 40px; + } + + .row.gtr-200.gtr-uniform { + margin-top: -40px; + } + + .row.gtr-200.gtr-uniform > * { + padding-top: 40px; + } + + } + + @media screen and (max-width: 480px) { + + .row { + display: flex; + flex-wrap: wrap; + box-sizing: border-box; + align-items: stretch; + } + + .row > * { + box-sizing: border-box; + } + + .row.gtr-uniform > * > :last-child { + margin-bottom: 0; + } + + .row.aln-left { + justify-content: flex-start; + } + + .row.aln-center { + justify-content: center; + } + + .row.aln-right { + justify-content: flex-end; + } + + .row.aln-top { + align-items: flex-start; + } + + .row.aln-middle { + align-items: center; + } + + .row.aln-bottom { + align-items: flex-end; + } + + .row > .imp-mobilep { + order: -1; + } + + .row > .col-1-mobilep { + width: 8.3333333333%; + } + + .row > .off-1-mobilep { + margin-left: 8.3333333333%; + } + + .row > .col-2-mobilep { + width: 16.6666666667%; + } + + .row > .off-2-mobilep { + margin-left: 16.6666666667%; + } + + .row > .col-3-mobilep { + width: 25%; + } + + .row > .off-3-mobilep { + margin-left: 25%; + } + + .row > .col-4-mobilep { + width: 33.3333333333%; + } + + .row > .off-4-mobilep { + margin-left: 33.3333333333%; + } + + .row > .col-5-mobilep { + width: 41.6666666667%; + } + + .row > .off-5-mobilep { + margin-left: 41.6666666667%; + } + + .row > .col-6-mobilep { + width: 50%; + } + + .row > .off-6-mobilep { + margin-left: 50%; + } + + .row > .col-7-mobilep { + width: 58.3333333333%; + } + + .row > .off-7-mobilep { + margin-left: 58.3333333333%; + } + + .row > .col-8-mobilep { + width: 66.6666666667%; + } + + .row > .off-8-mobilep { + margin-left: 66.6666666667%; + } + + .row > .col-9-mobilep { + width: 75%; + } + + .row > .off-9-mobilep { + margin-left: 75%; + } + + .row > .col-10-mobilep { + width: 83.3333333333%; + } + + .row > .off-10-mobilep { + margin-left: 83.3333333333%; + } + + .row > .col-11-mobilep { + width: 91.6666666667%; + } + + .row > .off-11-mobilep { + margin-left: 91.6666666667%; + } + + .row > .col-12-mobilep { + width: 100%; + } + + .row > .off-12-mobilep { + margin-left: 100%; + } + + .row.gtr-0 { + margin-top: 0px; + margin-left: 0px; + } + + .row.gtr-0 > * { + padding: 0px 0 0 0px; + } + + .row.gtr-0.gtr-uniform { + margin-top: 0px; + } + + .row.gtr-0.gtr-uniform > * { + padding-top: 0px; + } + + .row.gtr-25 { + margin-top: -5px; + margin-left: -5px; + } + + .row.gtr-25 > * { + padding: 5px 0 0 5px; + } + + .row.gtr-25.gtr-uniform { + margin-top: -5px; + } + + .row.gtr-25.gtr-uniform > * { + padding-top: 5px; + } + + .row.gtr-50 { + margin-top: -10px; + margin-left: -10px; + } + + .row.gtr-50 > * { + padding: 10px 0 0 10px; + } + + .row.gtr-50.gtr-uniform { + margin-top: -10px; + } + + .row.gtr-50.gtr-uniform > * { + padding-top: 10px; + } + + .row { + margin-top: -20px; + margin-left: -20px; + } + + .row > * { + padding: 20px 0 0 20px; + } + + .row.gtr-uniform { + margin-top: -20px; + } + + .row.gtr-uniform > * { + padding-top: 20px; + } + + .row.gtr-150 { + margin-top: -30px; + margin-left: -30px; + } + + .row.gtr-150 > * { + padding: 30px 0 0 30px; + } + + .row.gtr-150.gtr-uniform { + margin-top: -30px; + } + + .row.gtr-150.gtr-uniform > * { + padding-top: 30px; + } + + .row.gtr-200 { + margin-top: -40px; + margin-left: -40px; + } + + .row.gtr-200 > * { + padding: 40px 0 0 40px; + } + + .row.gtr-200.gtr-uniform { + margin-top: -40px; + } + + .row.gtr-200.gtr-uniform > * { + padding-top: 40px; + } + + } + +/* Section/Article */ + + section.special, article.special { + text-align: center; + } + + header p { + color: #999; + font-size: 1.25em; + position: relative; + margin-top: -1.25em; + margin-bottom: 2.25em; + } + + header.major { + text-align: center; + margin: 0 0 0 0; + } + + header.major h2 { + font-size: 2.25em; + } + + header.major p { + position: relative; + border-top: solid 1px #e0e0e0; + padding: 1em 0 0 0; + margin: 0; + top: -1em; + font-size: 1.5em; + letter-spacing: -0.025em; + } + + footer { + margin: 0 0 0 0; + } + + footer > :last-child { + margin-bottom: 0; + } + + footer.major { + padding-top: 3em; + } + +/* Form */ + + input[type="text"], + input[type="password"], + input[type="email"], + textarea { + -moz-appearance: none; + -webkit-appearance: none; + -ms-appearance: none; + appearance: none; + -moz-transition: border-color 0.2s ease-in-out; + -webkit-transition: border-color 0.2s ease-in-out; + -ms-transition: border-color 0.2s ease-in-out; + transition: border-color 0.2s ease-in-out; + background: #fff; + border: solid 1px #e0e0e0; + border-radius: 5px; + color: inherit; + display: block; + outline: 0; + padding: 0.75em; + text-decoration: none; + width: 100%; + } + + input[type="text"]:focus, + input[type="password"]:focus, + input[type="email"]:focus, + textarea:focus { + border-color: #37c0fb; + } + + input[type="text"], + input[type="password"], + input[type="email"] { + line-height: 1em; + } + + label { + display: block; + color: inherit; + font-weight: 600; + line-height: 1.75em; + margin-bottom: 0.5em; + } + + ::-webkit-input-placeholder { + color: #999; + position: relative; + top: 3px; + } + + :-moz-placeholder { + color: #999; + } + + ::-moz-placeholder { + color: #999; + } + + :-ms-input-placeholder { + color: #999; + } + +/* Image */ + + .image { + border: 0; + display: inline-block; + position: relative; + border-radius: 5px; + } + + .image img { + display: block; + border-radius: 5px; + } + + .image.left { + display: block; + float: left; + margin: 0 2em 2em 0; + position: relative; + top: 0.25em; + } + + .image.left img { + display: block; + width: 100%; + } + + .image.fit { + display: block; + } + + .image.fit img { + display: block; + width: 100%; + } + + .image.featured { + display: block; + margin: 0 0 2em 0; + } + + .image.featured img { + display: block; + width: 100%; + } + +/* Icon */ + + .icon { + text-decoration: none; + position: relative; + text-decoration: none; + } + .icon:before { + -moz-osx-font-smoothing: grayscale; + -webkit-font-smoothing: antialiased; + font-family: FontAwesome; + font-style: normal; + font-weight: normal; + text-transform: none !important; + font-size: 30px; + } + + .icon > .label { + display: none; + } + + .icon.major { + text-align: center; + cursor: default; + background-color: #8c1515; + background-image: -moz-linear-gradient(top, rgba(0,0,0,0), rgba(0,0,0,0.15)), url("images/bg01.png"); + background-image: -webkit-linear-gradient(top, rgba(0,0,0,0), rgba(0,0,0,0.15)), url("images/bg01.png"); + background-image: -ms-linear-gradient(top, rgba(0,0,0,0), rgba(0,0,0,0.15)), url("images/bg01.png"); + background-image: linear-gradient(top, rgba(0,0,0,0), rgba(0,0,0,0.15)), url("images/bg01.png"); + color: #fff; + border-radius: 100%; + display: inline-block; + width: 5em; + height: 5em; + line-height: 5em; + box-shadow: 0 0 0 7px white, 0 0 0 8px #e0e0e0; + margin: 0 0 2em 0; + } + + .icon.major:before { + font-size: 55px; + } + + + + .icon2 > img { + display: inline-block; + width: 32px; + height: 32px; + vertical-align: middle; } + + +/* Lists */ + + ol { + list-style: decimal; + padding-left: 1.25em; + } + + ol li { + padding-left: 0.25em; + } + + ul { + list-style: disc; + padding-left: 1em; + } + + ul li { + padding-left: 0.5em; + } + +/* Links */ + + ul.links { + list-style: none; + padding-left: 0; + } + + ul.links li { + line-height: 2.5em; + padding-left: 0; + } + +/* Icons */ + + ul.icons { + cursor: default; + list-style: none; + padding-left: 0; + } + + ul.icons li { + display: inline-block; + line-height: 1em; + padding-left: 1.5em; + } + + ul.icons li:first-child { + padding-left: 0; + } + + ul.icons li a, ul.icons li span { + font-size: 2em; + border: 0; + } + +/* Menu */ + + ul.menu { + list-style: none; + padding-left: 0; + } + + ul.menu li { + border-left: solid 1px #e0e0e0; + display: inline-block; + padding: 0 0 0 1em; + margin: 0 0 0 1em; + } + + ul.menu li:first-child { + border-left: 0; + margin-left: 0; + padding-left: 0; + } + +/* Actions */ + + ul.actions { + display: -moz-flex; + display: -webkit-flex; + display: -ms-flex; + display: flex; + cursor: default; + list-style: none; + margin-left: -1em; + padding-left: 0; + } + + ul.actions li { + padding: 0 0 0 1em; + vertical-align: middle; + } + + ul.actions.special { + -moz-justify-content: center; + -webkit-justify-content: center; + -ms-justify-content: center; + justify-content: center; + width: 100%; + margin-left: 0; + } + + ul.actions.special li:first-child { + padding-left: 0; + } + + ul.actions.stacked { + -moz-flex-direction: column; + -webkit-flex-direction: column; + -ms-flex-direction: column; + flex-direction: column; + margin-left: 0; + } + + ul.actions.stacked li { + padding: 1.25em 0 0 0; + } + + ul.actions.stacked li:first-child { + padding-top: 0; + } + + ul.actions.fit { + width: calc(100% + 1em); + } + + ul.actions.fit li { + -moz-flex-grow: 1; + -webkit-flex-grow: 1; + -ms-flex-grow: 1; + flex-grow: 1; + -moz-flex-shrink: 1; + -webkit-flex-shrink: 1; + -ms-flex-shrink: 1; + flex-shrink: 1; + width: 100%; + } + + ul.actions.fit li > * { + width: 100%; + } + + ul.actions.fit.stacked { + width: 100%; + } + + @media screen and (max-width: 736px) { + + ul.actions:not(.fixed) { + -moz-flex-direction: column; + -webkit-flex-direction: column; + -ms-flex-direction: column; + flex-direction: column; + margin-left: 0; + width: 100% !important; + } + + ul.actions:not(.fixed) li { + -moz-flex-grow: 1; + -webkit-flex-grow: 1; + -ms-flex-grow: 1; + flex-grow: 1; + -moz-flex-shrink: 1; + -webkit-flex-shrink: 1; + -ms-flex-shrink: 1; + flex-shrink: 1; + padding: 1em 0 0 0; + text-align: center; + width: 100%; + } + + ul.actions:not(.fixed) li > * { + width: 100%; + } + + ul.actions:not(.fixed) li:first-child { + padding-top: 0; + } + + ul.actions:not(.fixed) li input[type="submit"], + ul.actions:not(.fixed) li input[type="reset"], + ul.actions:not(.fixed) li input[type="button"], + ul.actions:not(.fixed) li button, + ul.actions:not(.fixed) li .button { + width: 100%; + } + + ul.actions:not(.fixed) li input[type="submit"].icon:before, + ul.actions:not(.fixed) li input[type="reset"].icon:before, + ul.actions:not(.fixed) li input[type="button"].icon:before, + ul.actions:not(.fixed) li button.icon:before, + ul.actions:not(.fixed) li .button.icon:before { + margin-left: -0.5em; + } + + } + +/* Tables */ + + table { + width: 100%; + } + + table.default { + width: 100%; + } + + table.default tbody tr { + border-bottom: solid 1px #e0e0e0; + } + + table.default td { + padding: 0.5em 1em 0.5em 1em; + } + + table.default th { + font-weight: 600; + padding: 0.5em 1em 0.5em 1em; + text-align: left; + } + + table.default thead { + background-color: #555555; + background-image: -moz-linear-gradient(top, rgba(0,0,0,0), rgba(0,0,0,0.15)), url("images/bg01.png"); + background-image: -webkit-linear-gradient(top, rgba(0,0,0,0), rgba(0,0,0,0.15)), url("images/bg01.png"); + background-image: -ms-linear-gradient(top, rgba(0,0,0,0), rgba(0,0,0,0.15)), url("images/bg01.png"); + background-image: linear-gradient(top, rgba(0,0,0,0), rgba(0,0,0,0.15)), url("images/bg01.png"); + color: #fff; + } + +/* Button */ + + input[type="submit"], + input[type="reset"], + input[type="button"], + button, + .button { + -moz-appearance: none; + -webkit-appearance: none; + -ms-appearance: none; + appearance: none; + -moz-transition: background-color 0.2s ease-in-out, color 0.2s ease-in-out, box-shadow 0.2s ease-in-out; + -webkit-transition: background-color 0.2s ease-in-out, color 0.2s ease-in-out, box-shadow 0.2s ease-in-out; + -ms-transition: background-color 0.2s ease-in-out, color 0.2s ease-in-out, box-shadow 0.2s ease-in-out; + transition: background-color 0.2s ease-in-out, color 0.2s ease-in-out, box-shadow 0.2s ease-in-out; + background-image: -moz-linear-gradient(top, rgba(0,0,0,0), rgba(0,0,0,0.15)), url("images/bg01.png"); + background-image: -webkit-linear-gradient(top, rgba(0,0,0,0), rgba(0,0,0,0.15)), url("images/bg01.png"); + background-image: -ms-linear-gradient(top, rgba(0,0,0,0), rgba(0,0,0,0.15)), url("images/bg01.png"); + background-image: linear-gradient(top, rgba(0,0,0,0), rgba(0,0,0,0.15)), url("images/bg01.png"); + background-color: #8C1515; + border-radius: 5px; + border: 0; + color: #fff; + cursor: pointer; + display: inline-block; + padding: 0 1.5em; + line-height: 2.75em; + min-width: 9em; + text-align: center; + text-decoration: none; + font-weight: 600; + letter-spacing: -0.025em; + } + + input[type="submit"]:hover, + input[type="reset"]:hover, + input[type="button"]:hover, + button:hover, + .button:hover { + background-color: #50c8fc; + color: #fff !important; + } + + input[type="submit"]:active, + input[type="reset"]:active, + input[type="button"]:active, + button:active, + .button:active { + background-color: #1eb8fb; + color: #fff; + } + + input[type="submit"].alt, + input[type="reset"].alt, + input[type="button"].alt, + button.alt, + .button.alt { + background-color: #555555; + color: #fff; + } + + input[type="submit"].alt:hover, + input[type="reset"].alt:hover, + input[type="button"].alt:hover, + button.alt:hover, + .button.alt:hover { + background-color: #626262; + } + + input[type="submit"].alt:active, + input[type="reset"].alt:active, + input[type="button"].alt:active, + button.alt:active, + .button.alt:active { + background-color: #484848; + } + + input[type="submit"].icon:before, + input[type="reset"].icon:before, + input[type="button"].icon:before, + button.icon:before, + .button.icon:before { + margin-right: 0.5em; + } + + input[type="submit"].fit, + input[type="reset"].fit, + input[type="button"].fit, + button.fit, + .button.fit { + width: 100%; + } + + input[type="submit"].small, + input[type="reset"].small, + input[type="button"].small, + button.small, + .button.small { + font-size: 0.8em; + } + +/* Box */ + + .box.highlight { + text-align: center; + } + + .box.post { + position: relative; + margin: 0 0 2em 0; + } + + .box.post:after { + content: ''; + display: block; + clear: both; + } + + .box.post .inner { + margin-left: calc(30% + 2em); + } + + .box.post .inner > :last-child { + margin-bottom: 0; + } + + .box.post .image { + width: 30%; + margin: 0; + } + +/* Header */ + + #header { + text-align: center; + padding: 0 0 0 0; + background-color: #333; + background-position: top left, top left, top left; + background-size: 100% 0em, 100% 6em, auto; + background-repeat: no-repeat, no-repeat, repeat; + } + + #header h1 { + padding: 0 0 0 0; + margin: 0; + } + + #header h1 a { + font-size: 0; + letter-spacing: -0.025em; + border: 0; + } + + #nav { + cursor: default; + background-color: #333; + background-image: -moz-linear-gradient(top, rgba(0,0,0,0), rgba(0,0,0,0.3)), url("images/bg01.png"); + background-image: -webkit-linear-gradient(top, rgba(0,0,0,0), rgba(0,0,0,0.3)), url("images/bg01.png"); + background-image: -ms-linear-gradient(top, rgba(0,0,0,0), rgba(0,0,0,0.3)), url("images/bg01.png"); + background-image: linear-gradient(top, rgba(0,0,0,0), rgba(0,0,0,0.3)), url("images/bg01.png"); + padding: 0; + + } + + #nav:after { + content: ''; + display: block; + width: 100%; + height: 0.75em; + background-color: #8c1515; + } + + #nav > ul { + margin: 0; + } + + #nav > ul > li { + position: relative; + display: inline-block; + margin-left: 1em; + } + + #nav > ul > li a { + color: #c0c0c0; + text-decoration: none; + border: 0; + display: block; + padding: 1.5em 0.5em 1.35em 0.5em; + } + + #nav > ul > li:first-child { + margin-left: 0; + } + + #nav > ul > li:hover a { + color: #fff; + } + + #nav > ul > li.current { + font-weight: 600; + } + + #nav > ul > li.current:before { + -moz-transform: rotateZ(45deg); + -webkit-transform: rotateZ(45deg); + -ms-transform: rotateZ(45deg); + transform: rotateZ(45deg); + width: 0.75em; + height: 0.75em; + content: ''; + display: block; + position: absolute; + bottom: -0.5em; + left: 50%; + margin-left: -0.375em; + background-color: #8c1515; + background-image: url("images/bg01.png"); + } + + #nav > ul > li.current a { + color: #fff; + } + + #nav > ul > li.active a { + color: #fff; + } + + #nav > ul > li.active.current:before { + opacity: 0; + } + + #nav > ul > li > ul { + display: none; + } + +/* Dropotron */ + + .dropotron { + background-image: -moz-linear-gradient(top, rgba(0,0,0,0.3), rgba(0,0,0,0)), url("images/bg01.png"); + background-image: -webkit-linear-gradient(top, rgba(0,0,0,0.3), rgba(0,0,0,0)), url("images/bg01.png"); + background-image: -ms-linear-gradient(top, rgba(0,0,0,0.3), rgba(0,0,0,0)), url("images/bg01.png"); + background-image: linear-gradient(top, rgba(0,0,0,0.3), rgba(0,0,0,0)), url("images/bg01.png"); + background-color: #333; + border-radius: 5px; + color: #fff; + min-width: 10em; + padding: 1em 0; + text-align: center; + box-shadow: 0 1em 1em 0 rgba(0, 0, 0, 0.5); + list-style: none; + } + + .dropotron > li { + line-height: 2em; + padding: 0 1.1em 0 1em; + } + + .dropotron > li > a { + color: #c0c0c0; + text-decoration: none; + border: 0; + } + + .dropotron > li.active > a, .dropotron > li:hover > a { + color: #fff; + } + + .dropotron.level-0 { + border-radius: 0 0 5px 5px; + font-size: 0.9em; + padding-top: 0; + margin-top: -1px; + } + +/* Banner */ + + #banner { + background-color: rgba(0,0,0,0); + background-image: url("https://suave.stanford.edu/../images/logo_no_text.svg"); + background-position: center top; + background-size: contain; + background-repeat: no-repeat; + height: 28em; + text-align: center; + position: relative; + } + + #banner header { + position: absolute; + bottom: 0; + left: 0; + width: 100%; + background: #212121; + background: rgba(77, 79, 83, 0.8); + color: #fff; + padding: 0.8em 0; + } + + #banner header h2 { + display: inline-block; + margin: 0; + font-size: 1.8em; + vertical-align: middle; + } + + #banner header h2 em { + opacity: 0.75; + } + + #banner header h2 a { + border-bottom-color: rgba(255, 255, 255, 0.5); + } + + #banner header h2 a:hover { + border-bottom-color: transparent; + } + + #banner header .button { + vertical-align: middle; + margin-left: 1em; + } + +/* Wrapper */ + + .wrapper { + padding: 3em 0 1em 0; + } + + .wrapper.style1 { + background: #fff; + } + + /*.wrapper.style2 {*/ + /*background-color: #fff;*/ + /*background-image: url("images/bg02.png"), url("images/bg03.png"), url("images/bg01.png");*/ + /*background-position: top left, bottom left, top left;*/ + /*background-size: 100% 6em, 100% 6em, auto;*/ + /*background-repeat: no-repeat, no-repeat, repeat;*/ + /*}*/ + + .wrapper.style3 { + background-color: #8C1515; + color: #fff; + } + + .wrapper.style3 .button { + background: #fff; + color: #474747; + vertical-align: middle; + } + + .wrapper.style3 .button:hover { + color: #37c0fb !important; + } + +/* CTA */ + + #cta { + text-align: center; + padding: 1.0em 0; + } + + #cta header h2 { + display: inline-block; + vertical-align: middle; + margin: 0; + } + + #cta header .button { + vertical-align: middle; + margin-left: 1em; + } + +/* Footer */ + + #footer { + padding: 4em 0 0 0; + text-align: left; + } + + #footer a { + color: inherit; + border-bottom-color: rgba(71, 71, 71, 0.25); + } + + #footer a:hover { + color: #37c0fb; + border-bottom-color: transparent; + } + + #footer .container { + margin-bottom: 4em; + } + + #footer .icons { + text-align: center; + margin: 0; + } + + #footer .icons a { + color: #999; + } + + #footer .icons a:hover { + color: #474747; + } + + #footer .copyright { + color: #999; + margin-top: 1.5em; + text-align: center; + font-size: 0.9em; + } + +/* Wide */ + + @media screen and (max-width: 1680px) { + + /* Basic */ + + body, input, select, textarea { + font-size: 14pt; + line-height: 1.5em; + } + + /* Banner */ + + #banner { + height: 24em; + } + + } + +/* Normal */ + + @media screen and (max-width: 1280px) { + + /* Basic */ + + body, input, select, textarea { + font-size: 13pt; + line-height: 1.5em; + } + + /* Lists */ + + ol { + padding-left: 1.25em; + } + + ol li { + padding-left: 0.25em; + } + + /* Icons */ + + ul.icons li a, ul.icons li span { + font-size: 1.5em; + } + + /* Header */ + + #header { + padding:0 0 0 0; + } + + #header h1 { + padding: 0 0 1.75em 0; + } + + /* Banner */ + + #banner { + height: 25em; + } + + /* Wrapper */ + + .wrapper { + padding: 2em 0 0 0; + } + + /* CTA */ + + #cta { + padding: 2em 0; + } + + /* Footer */ + + #footer { + padding: 3em 0 3em 0; + } + + #footer .container { + margin-bottom: 1em; + } + + } + +/* Narrow */ + + @media screen and (max-width: 980px) { + + /* Basic */ + + body, input, select, textarea { + font-size: 12pt; + line-height: 1.5em; + } + + } + +/* Narrower */ + + #navPanel, #titleBar { + display: none; + } + + @media screen and (max-width: 840px) { + + /* Basic */ + + html, body { + overflow-x: hidden; + } + + body, input, select, textarea { + font-size: 13pt; + } + + h1, h2, h3, h4, h5, h6 { + margin-bottom: 0.5em; + } + + header p { + margin-top: -0.75em; + } + + header.major { + text-align: center; + margin: 0 0 0 0; + } + + header.major h2 { + font-size: 1.75em; + } + + header.major p { + top: -0.25em; + font-size: 1.25em; + } + + /* Box */ + + .box.highlight { + text-align: left; + position: relative; + padding-left: 7em; + } + + .box.highlight i { + position: absolute; + margin: 0; + left: 0; + top: 0.25em; + } + + .box.post .inner { + margin-left: calc(20% + 2em); + } + + .box.post .image { + width: 20%; + } + + /* Header */ + + #header { + display: none; + } + + /* Banner */ + + #banner { + height: 20em; + } + + #banner header h2 { + display: block; + } + + #banner header .button { + margin: 1em 0 0 0; + } + + /* CTA */ + + #cta { + padding: 1.5em 0; + } + + #cta header h2 { + display: block; + } + + #cta header .button { + margin: 1em 0 0 0; + } + + /* Footer */ + + #footer { + text-align: center; + } + + #footer .container { + margin-bottom: 4em; + } + + #footer form .actions { + -moz-justify-content: center; + -webkit-justify-content: center; + -ms-justify-content: center; + justify-content: center; + width: 100%; + margin-left: 0; + } + + #footer form .actions li:first-child { + padding-left: 0; + } + + /* Nav */ + + #page-wrapper { + -moz-backface-visibility: hidden; + -webkit-backface-visibility: hidden; + -ms-backface-visibility: hidden; + backface-visibility: hidden; + -moz-transition: -moz-transform 0.5s ease; + -webkit-transition: -webkit-transform 0.5s ease; + -ms-transition: -ms-transform 0.5s ease; + transition: transform 0.5s ease; + padding-bottom: 1px; + padding-top: 44px; + } + + #titleBar { + -moz-backface-visibility: hidden; + -webkit-backface-visibility: hidden; + -ms-backface-visibility: hidden; + backface-visibility: hidden; + -moz-transition: -moz-transform 0.5s ease; + -webkit-transition: -webkit-transform 0.5s ease; + -ms-transition: -ms-transform 0.5s ease; + transition: transform 0.5s ease; + display: block; + height: 44px; + left: 0; + position: fixed; + top: 0; + width: 100%; + z-index: 10001; + background-color: #333; + background-image: -moz-linear-gradient(top, rgba(0,0,0,0), rgba(0,0,0,0.3)), url("images/bg01.png"); + background-image: -webkit-linear-gradient(top, rgba(0,0,0,0), rgba(0,0,0,0.3)), url("images/bg01.png"); + background-image: -ms-linear-gradient(top, rgba(0,0,0,0), rgba(0,0,0,0.3)), url("images/bg01.png"); + background-image: linear-gradient(top, rgba(0,0,0,0), rgba(0,0,0,0.3)), url("images/bg01.png"); + height: 44px; + line-height: 44px; + box-shadow: 0 4px 0 0 #8c1515; + } + + #titleBar .title { + display: block; + position: relative; + font-weight: 600; + text-align: center; + color: #fff; + z-index: 1; + } + + #titleBar .title em { + font-style: normal; + font-weight: 300; + } + + #titleBar .toggle { + text-decoration: none; + border: 0; + height: 60px; + left: 0; + position: absolute; + top: 0; + width: 80px; + z-index: 2; + } + + #titleBar .toggle:before { + -moz-osx-font-smoothing: grayscale; + -webkit-font-smoothing: antialiased; + font-family: FontAwesome; + font-style: normal; + font-weight: normal; + text-transform: none !important; + } + + #titleBar .toggle:before { + content: '\f0c9'; + display: block; + height: 44px; + text-align: center; + width: 44px; + color: #fff; + opacity: 0.5; + } + + #titleBar .toggle:active:before { + opacity: 0.75; + } + + #navPanel { + background-color: #1f1f1f; + box-shadow: inset -1px 0 3px 0 rgba(0, 0, 0, 0.5); + background-image: -moz-linear-gradient(left, rgba(0,0,0,0) 75%, rgba(0,0,0,0.15)), url("images/bg01.png"); + background-image: -webkit-linear-gradient(left, rgba(0,0,0,0) 75%, rgba(0,0,0,0.15)), url("images/bg01.png"); + background-image: -ms-linear-gradient(left, rgba(0,0,0,0) 75%, rgba(0,0,0,0.15)), url("images/bg01.png"); + background-image: linear-gradient(left, rgba(0,0,0,0) 75%, rgba(0,0,0,0.15)), url("images/bg01.png"); + -moz-backface-visibility: hidden; + -webkit-backface-visibility: hidden; + -ms-backface-visibility: hidden; + backface-visibility: hidden; + -moz-transform: translateX(-275px); + -webkit-transform: translateX(-275px); + -ms-transform: translateX(-275px); + transform: translateX(-275px); + -moz-transition: -moz-transform 0.5s ease; + -webkit-transition: -webkit-transform 0.5s ease; + -ms-transition: -ms-transform 0.5s ease; + transition: transform 0.5s ease; + display: block; + height: 100%; + left: 0; + overflow-y: auto; + position: fixed; + top: 0; + width: 275px; + z-index: 10002; + } + + #navPanel .link { + border-bottom: 0; + border-top: solid 1px rgba(255, 255, 255, 0.05); + color: #888; + display: block; + height: 48px; + line-height: 48px; + padding: 0 1em 0 1em; + text-decoration: none; + } + + #navPanel .link:first-child { + border-top: 0; + } + + #navPanel .link.depth-0 { + color: #fff; + } + + #navPanel .link .indent-1 { + display: inline-block; + width: 1em; + } + + #navPanel .link .indent-2 { + display: inline-block; + width: 2em; + } + + #navPanel .link .indent-3 { + display: inline-block; + width: 3em; + } + + #navPanel .link .indent-4 { + display: inline-block; + width: 4em; + } + + #navPanel .link .indent-5 { + display: inline-block; + width: 5em; + } + + body.navPanel-visible #page-wrapper { + -moz-transform: translateX(275px); + -webkit-transform: translateX(275px); + -ms-transform: translateX(275px); + transform: translateX(275px); + } + + body.navPanel-visible #titleBar { + -moz-transform: translateX(275px); + -webkit-transform: translateX(275px); + -ms-transform: translateX(275px); + transform: translateX(275px); + } + + body.navPanel-visible #navPanel { + -moz-transform: translateX(0); + -webkit-transform: translateX(0); + -ms-transform: translateX(0); + transform: translateX(0); + } + + } + +/* Mobile */ + + @media screen and (max-width: 736px) { + + /* Basic */ + + body, input, select, textarea { + font-size: 11pt; + line-height: 1.35em; + } + + h2 { + font-size: 1.25em; + letter-spacing: 0; + line-height: 1.35em; + } + + h3 { + font-size: 1em; + letter-spacing: 0; + line-height: 1.35em; + } + + header p { + margin-top: -0.5em; + font-size: 1em; + } + + header.major { + padding: 0 20px; + } + + header.major h2 { + font-size: 1.25em; + } + + header.major p { + top: 0; + margin-top: 1.25em; + font-size: 1em; + } + + /* Menu */ + + ul.menu li { + border: 0; + padding: 0; + margin: 0; + display: block; + line-height: 2em; + } + + /* Banner */ + + #banner { + height: 18em; + } + + /* Wrapper */ + + .wrapper { + padding: 2em 0 1px 0; + } + + } + +/* Mobile (Portrait) */ + + @media screen and (max-width: 480px) { + + /* Icon */ + + .icon.major { + width: 4em; + height: 4em; + line-height: 4em; + box-shadow: 0 0 0 7px white, 0 0 0 8px #8c1515; + } + + .icon.major:before { + font-size: 24px; + } + + /* Button */ + + input[type="submit"], + input[type="reset"], + input[type="button"], + button, + .button { + width: 100%; + display: block; + } + + /* Box */ + + .box.highlight { + padding-left: calc(4em + 30px); + } + + .box.post .inner { + margin-left: calc(30% + 20px); + } + + .box.post .image { + width: 30%; + } + + /* Banner */ + + #banner { + height: 20em; + } + + #banner header { + padding: 20px; + } + + /* Wrapper */ + + .wrapper { + padding: 2em 20px 1px 20px; + } + + /* CTA */ + + #cta { + padding: 20px; + } + + /* Footer */ + + #footer { + padding: 2em 0; + text-align: center; + } + + } \ No newline at end of file diff --git a/assets/css/prism.css b/assets/css/prism.css new file mode 100644 index 00000000..7fd4f98a --- /dev/null +++ b/assets/css/prism.css @@ -0,0 +1,143 @@ +/* PrismJS 1.21.0 +https://prismjs.com/download.html#themes=prism&languages=python */ +/** + * prism.js default theme for JavaScript, CSS and HTML + * Based on dabblet (http://dabblet.com) + * @author Lea Verou + */ + +code[class*="language-"], +pre[class*="language-"] { + color: black; + background: none; + text-shadow: 0 1px white; + font-family: Consolas, Monaco, 'Andale Mono', 'Ubuntu Mono', monospace; + font-size: 1em; + text-align: left; + white-space: pre; + word-spacing: normal; + word-break: normal; + word-wrap: normal; + line-height: 1.5; + + -moz-tab-size: 4; + -o-tab-size: 4; + tab-size: 4; + + -webkit-hyphens: none; + -moz-hyphens: none; + -ms-hyphens: none; + hyphens: none; +} + +pre[class*="language-"]::-moz-selection, pre[class*="language-"] ::-moz-selection, +code[class*="language-"]::-moz-selection, code[class*="language-"] ::-moz-selection { + text-shadow: none; + background: #b3d4fc; +} + +pre[class*="language-"]::selection, pre[class*="language-"] ::selection, +code[class*="language-"]::selection, code[class*="language-"] ::selection { + text-shadow: none; + background: #b3d4fc; +} + +@media print { + code[class*="language-"], + pre[class*="language-"] { + text-shadow: none; + } +} + +/* Code blocks */ +pre[class*="language-"] { + padding: 1em; + margin: .5em 0; + overflow: auto; +} + +:not(pre) > code[class*="language-"], +pre[class*="language-"] { + background: #f5f2f0; +} + +/* Inline code */ +:not(pre) > code[class*="language-"] { + padding: .1em; + border-radius: .3em; + white-space: normal; +} + +.token.comment, +.token.prolog, +.token.doctype, +.token.cdata { + color: slategray; +} + +.token.punctuation { + color: #999; +} + +.token.namespace { + opacity: .7; +} + +.token.property, +.token.tag, +.token.boolean, +.token.number, +.token.constant, +.token.symbol, +.token.deleted { + color: #905; +} + +.token.selector, +.token.attr-name, +.token.string, +.token.char, +.token.builtin, +.token.inserted { + color: #690; +} + +.token.operator, +.token.entity, +.token.url, +.language-css .token.string, +.style .token.string { + color: #9a6e3a; + /* This background color was intended by the author of this theme. */ + background: hsla(0, 0%, 100%, .5); +} + +.token.atrule, +.token.attr-value, +.token.keyword { + color: #07a; +} + +.token.function, +.token.class-name { + color: #DD4A68; +} + +.token.regex, +.token.important, +.token.variable { + color: #e90; +} + +.token.important, +.token.bold { + font-weight: bold; +} +.token.italic { + font-style: italic; +} + +.token.entity { + cursor: help; +} + diff --git a/assets/fonts/FontAwesome.otf b/assets/fonts/FontAwesome.otf new file mode 100644 index 00000000..401ec0f3 Binary files /dev/null and b/assets/fonts/FontAwesome.otf differ diff --git a/assets/fonts/fontawesome-webfont.eot b/assets/fonts/fontawesome-webfont.eot new file mode 100644 index 00000000..e9f60ca9 Binary files /dev/null and b/assets/fonts/fontawesome-webfont.eot differ diff --git a/assets/fonts/fontawesome-webfont.svg b/assets/fonts/fontawesome-webfont.svg new file mode 100644 index 00000000..855c845e --- /dev/null +++ b/assets/fonts/fontawesome-webfont.svg @@ -0,0 +1,2671 @@ + + + + +Created by FontForge 20120731 at Mon Oct 24 17:37:40 2016 + By ,,, +Copyright Dave Gandy 2016. 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+ + + + +
+
+
+ +
+
+ + + +
+
+

Documentation

+ +

SUAVE is fully documented through doxygen. However, some starter high level documentation is available on the left. We suggestion you read the high level information before jumping into the Doxygen based documentation.

+ + + +
+
+
+
+
+ + + + + + + + + + + + + + \ No newline at end of file diff --git a/documentation/.DS_Store b/documentation/.DS_Store new file mode 100644 index 00000000..1ff9569e Binary files /dev/null and b/documentation/.DS_Store differ diff --git a/documentation/_posts/2000-01-04-mission_solver.md b/documentation/_posts/2000-01-04-mission_solver.md deleted file mode 100644 index 39f5ca92..00000000 --- a/documentation/_posts/2000-01-04-mission_solver.md +++ /dev/null @@ -1,240 +0,0 @@ ---- -layout: post -title: Mission Solver Structure -date: 2017-01-07 13:25:00 -categories: blog -description: Understanding the mission solver - -permalink: /guides/mission.html ---- - -## Mission Solver Code Structure - -This is a high level overview of how the mission solver functions. The purpose is to show the structure that is used for an existing mission, and show where changes should be made if different functionality is desired. - -### File Structure - -Mission scripts are split into two folders in the SUAVE repository. The first is in trunk/SUAVE/**Analyses/Mission**/Segments, and the second is in trunk/SUAVE/**Methods/Missions**/Segments. As with other types of analyses and methods, the distinction between these is that the Analyses folder contains classes that are built to use functions stored in the Methods folder. This division is done to make it easier to build new analysis classes using a mix of available methods. - -A typical mission segment analysis file contains four keys parts. The first specifies default user inputs, unknowns, and residuals. The inputs are used to provide the analysis with conditions that need to be met, while the unknowns and residuals are used as part of the solution process. The second sets the initialization functions for the analysis, which are run at the beginning. The third picks the convergence method and specifies the functions that will be used during iteration. The fourth finalizes the data and processes it for results output. - -### Initialization - -For this tutorial, we will be considering the constant speed constant altitude cruise segment. The files are available [here (Analysis)](https://github.com/suavecode/SUAVE/blob/develop/trunk/SUAVE/Analyses/Mission/Segments/Cruise/Constant_Speed_Constant_Altitude.py) and [here (Method)](https://github.com/suavecode/SUAVE/blob/develop/trunk/SUAVE/Methods/Missions/Segments/Cruise/Constant_Speed_Constant_Altitude.py). This class also inherits information from more general segment classes, which include many of the processing functions. As with other segments, the user will specify key conditions. For this case, altitude, air speed, and distance are the necessary inputs. If the user does not specify an altitude, it will be taken automatically from the last value in the previous segment. These inputs must be specified in some way for the mission segment to be evaluated. They are shown below as well: - - self.altitude = None - self.air_speed = 10. * Units['km/hr'] - self.distance = 10. * Units.km - -The other set of segment specific initial values are the values used for solving the segment (typically this means satisfying a force balance at every evaluation point). These can be changed by the user if needed, but the default values should perform fine for most cases. - - self.state.unknowns.throttle = ones_row(1) * 0.5 - self.state.unknowns.body_angle = ones_row(1) * 0.0 - self.state.residuals.forces = ones_row(2) * 0.0 - -Here throttle and body angle are the unknowns, and the values shown here are the values they will start at. The residuals will be computed based on these unknowns, so their initial value is not important. Instead they are initialized just to create the necessary data structure. The ones_row line will create a numpy array with the number of elements needed for evaluation. - -### Evaluation Details - -Most of the missions in SUAVE, including this one, are broken into several points in time based on a Chebyshev polynomial. This causes the points to be closer together at either end of the segment. The choice of a Chebyshev polynomial (which creates cosine spacing) provides better convergence and smoothness properties versus other methods such as linear spacing. - - - -At each of these points the aerodynamic analysis is queried to find CL and CD, which are then converted to lift and drag. These values will be dependent on the body angle unknown and other aerodynamic parameters. Thrust is found from the vehicle's energy network, which is dependent on the throttle unknown. A weight is determined by looking at the initial weight and subsequent mass rate (typically corresponding with fuel burn). In this cruise segment, these forces are summed in 2D and the results are put in the residuals. The functions needed to arrive these forces are found in the Update Conditions section of the Analysis file. This section is also shown below in one of the steps to create a new mission. - -Once the evaluation process has been performed at all points, the unknowns and residuals are fed back to the solve routine, which in this case is scipy's fsolve. The file that performs this process is [here](https://github.com/suavecode/SUAVE/blob/develop/trunk/SUAVE/Methods/Missions/Segments/converge_root.py). This routine continues evaluating the points until convergence is reached. Once this happens, post processing is done to put the data in the results output. - -### Using Multiple Segments - -Multiple segments can be run sequentially by appending them in the desired order. Examples of this are in all the tutorial files that have an aircraft fly a full mission. In addition, the full mission can be run simultaneously will all segment constraints used together. If you are interested in doing something like this, please ask us about it on our [forum](/forum). - -#### Process Summary - -Mission Setup - -* Initializes default values for unknowns -* Initializes set of functions used to determine residuals -* Reads user input for segment parameters -* Adds the analysis group to be used (including the vehicle and items like atmosphere) -* Appends segments in order - -Evaluate - -* Varies unknowns until residual convergence is reached using scipy's fsolve -* Repeats process for each segment until full mission is complete - -### Adding New Mission Segments - -The segment described above uses two unknowns to solve force residuals in two dimensions. This general setup works well for many problems of interest, but SUAVE is designed to accommodate other mission analysis types as well. A user may want to add control surface deflection and solve for moments as well, or look at forces in all three dimensions. - -In addition, a user may want to modify how the mission is flown, as is done with the many other segments currently available. They may want to modify how the mission is solved, such as is done in our single point evaluation segments where finite differencing is not relevant. - -Here we will explain the process of modifying our constant speed constant rate climb segment to be constant throttle constant speed. This still uses 2D force balance but changes the profile. There are four functions that are modified here. The first is shown below. The functions can be found in [here]() and [here]() - - def initialize_conditions(segment,state): - - # unpack - climb_rate = segment.climb_rate - air_speed = segment.air_speed - alt0 = segment.altitude_start - altf = segment.altitude_end - t_nondim = state.numerics.dimensionless.control_points - conditions = state.conditions - - # check for initial altitude - if alt0 is None: - if not state.initials: raise AttributeError('initial altitude not set') - alt0 = -1.0 * state.initials.conditions.frames.inertial.position_vector[-1,2] - - # discretize on altitude - alt = t_nondim * (altf-alt0) + alt0 - - # process velocity vector - v_mag = air_speed - v_z = -climb_rate # z points down - v_x = np.sqrt( v_mag**2 - v_z**2 ) - - # pack conditions - conditions.frames.inertial.velocity_vector[:,0] = v_x - conditions.frames.inertial.velocity_vector[:,2] = v_z - conditions.frames.inertial.position_vector[:,2] = -alt[:,0] # z points down - conditions.freestream.altitude[:,0] = alt[:,0] # positive altitude in this context - -This function initializes speed and altitude based on the given climb rate, airspeed, and altitude end points. t_nondim gives nondimensional time in cosine spacing from 0 to 1 in order to pick the values at the points to be evaluated. Unfortunately, when we use constant throttle we cannot know beforehand exactly how altitude (or climb rate in this case) will vary with time, so altitude cannot be spaced with this method. Instead a different function is used to initialize conditions: - - def initialize_conditions(segment,state): - - # unpack - throttle = segment.throttle - air_speed = segment.air_speed - alt0 = segment.altitude_start - altf = segment.altitude_end - t_nondim = state.numerics.dimensionless.control_points - conditions = state.conditions - - # check for initial altitude - if alt0 is None: - if not state.initials: raise AttributeError('initial altitude not set') - alt0 = -1.0 * state.initials.conditions.frames.inertial.position_vector[-1,2] - - # pack conditions - conditions.propulsion.throttle[:,0] = throttle - conditions.frames.inertial.velocity_vector[:,0] = air_speed # start up value - -Here only the throttle and air speed are loaded in, and discretization of other values will need to occur later so that it is part of the iteration loop. This requires a new function that updates the altitude differentials. - - def update_differentials_altitude(segment,state): - - # unpack - t = state.numerics.dimensionless.control_points - D = state.numerics.dimensionless.differentiate - I = state.numerics.dimensionless.integrate - - - # Unpack segment initials - alt0 = segment.altitude_start - altf = segment.altitude_end - conditions = state.conditions - - r = state.conditions.frames.inertial.position_vector - v = state.conditions.frames.inertial.velocity_vector - - # check for initial altitude - if alt0 is None: - if not state.initials: raise AttributeError('initial altitude not set') - alt0 = -1.0 * state.initials.conditions.frames.inertial.position_vector[-1,2] - - # get overall time step - vz = -v[:,2,None] # Inertial velocity is z down - dz = altf- alt0 - dt = dz / np.dot(I[-1,:],vz)[-1] # maintain column array - - # Integrate vz to get altitudes - alt = alt0 + np.dot(I*dt,vz) - - # rescale operators - t = t * dt - - # pack - t_initial = state.conditions.frames.inertial.time[0,0] - state.conditions.frames.inertial.time[:,0] = t_initial + t[:,0] - conditions.frames.inertial.position_vector[:,2] = -alt[:,0] # z points down - conditions.freestream.altitude[:,0] = alt[:,0] # positive altitude in this context - - return - -In this function, t, D, and I are numpy arrays that allow approximate differentiation and integration. Since the total time is not known without determining the climb rate, we must first determine the time required to reach the final altitude. The line `dt = dz / np.dot(I[-1,:],vz)[-1]` does this with the integrator providing the amount of altitude gained if the velocities were spread across just one second instead of the full segment time. This gives the scaling quantity `dt` that is then used to get the altitude at every point in `alt = alt0 + np.dot(I*dt,vz)`. The values for altitude are then are then packed for use in other functions. - -The above allows us to deal with discretization without a known profile, but we also must calculate the velocity in order to use this. This is done with another added function. - - def update_velocity_vector_from_wind_angle(segment,state): - - # unpack - conditions = state.conditions - v_mag = segment.air_speed - alpha = state.unknowns.wind_angle[:,0][:,None] - theta = state.unknowns.body_angle[:,0][:,None] - - # Flight path angle - gamma = theta-alpha - - # process - v_x = v_mag * np.cos(gamma) - v_z = -v_mag * np.sin(gamma) # z points down - - # pack - conditions.frames.inertial.velocity_vector[:,0] = v_x[:,0] - conditions.frames.inertial.velocity_vector[:,2] = v_z[:,0] - - return conditions - -This uses our new set of unknowns to determine the velocities. - -Additionally, since the unknowns are different we must change the function that unpacks them. Wind angle does not need to be stored so it is not included here. - - def unpack_body_angle(segment,state): - - # unpack unknowns - theta = state.unknowns.body_angle - - # apply unknowns - state.conditions.frames.body.inertial_rotations[:,1] = theta[:,0] - -We now add these functions to the segment process list. - - # -------------------------------------------------------------- - # Initialize - before iteration - # -------------------------------------------------------------- - initialize = self.process.initialize - - initialize.expand_state = Methods.expand_state - initialize.differentials = Methods.Common.Numerics.initialize_differentials_dimensionless - initialize.conditions = Methods.Climb.Constant_Throttle_Constant_Speed.initialize_conditions - initialize.velocities = Methods.Climb.Constant_Throttle_Constant_Speed.update_velocity_vector_from_wind_angle - initialize.differentials_altitude = Methods.Climb.Constant_Throttle_Constant_Speed.update_differentials_altitude - -and - - # Unpack Unknowns - iterate.unknowns = Process() - iterate.unknowns.mission = Methods.Climb.Constant_Throttle_Constant_Speed.unpack_body_angle - - # Update Conditions - iterate.conditions = Process() - iterate.conditions.velocities = Methods.Climb.Constant_Throttle_Constant_Speed.update_velocity_vector_from_wind_angle - iterate.conditions.differentials_a = Methods.Climb.Constant_Throttle_Constant_Speed.update_differentials_altitude - iterate.conditions.differentials_b = Methods.Common.Numerics.update_differentials_time - iterate.conditions.acceleration = Methods.Common.Frames.update_acceleration - iterate.conditions.altitude = Methods.Common.Aerodynamics.update_altitude - iterate.conditions.atmosphere = Methods.Common.Aerodynamics.update_atmosphere - iterate.conditions.gravity = Methods.Common.Weights.update_gravity - iterate.conditions.freestream = Methods.Common.Aerodynamics.update_freestream - iterate.conditions.orientations = Methods.Common.Frames.update_orientations - iterate.conditions.aerodynamics = Methods.Common.Aerodynamics.update_aerodynamics - iterate.conditions.stability = Methods.Common.Aerodynamics.update_stability - iterate.conditions.propulsion = Methods.Common.Energy.update_thrust - iterate.conditions.weights = Methods.Common.Weights.update_weights - iterate.conditions.forces = Methods.Common.Frames.update_forces - iterate.conditions.planet_position = Methods.Common.Frames.update_planet_position - -If you have any questions that are not answered in other tutorials or the FAQ please ask on our [forum](/forum) page. This is also the place to go if you want help building a more elaborate evaluation, such as one that includes moments. \ No newline at end of file diff --git a/documentation/_posts/2000-01-05-energy_networks.md b/documentation/_posts/2000-01-05-energy_networks.md deleted file mode 100644 index 6b647d09..00000000 --- a/documentation/_posts/2000-01-05-energy_networks.md +++ /dev/null @@ -1,110 +0,0 @@ ---- -layout: post -title: Energy Networks -date: 2017-01-06 13:25:00 -categories: blog -description: Understanding energy network structure - -permalink: /guides/energy_structure.html ---- - -##Energy Networks -Energy networks are really a fancy name for your propulsion system. The reason we call them a network rather than "engine" or the like is that it encompasses far more than that. These "energy networks" are the complex systems that future aircraft will incorporate that can reduce or eliminate fuel burn. For example if you have a hybrid gas-electric aircraft you don't have just an engine. You have an engine, a motor, batteries, a generator, a gearbox, a propeller or ducted fan, wiring, electronics... and that doesn't include the parts inside the internal combustion engine. Modeling these systems completely is essential in designing such a vehicle. - -To do this we depart from the typical SUAVE structure of analyses and methods. This was done because we want to look at each component of the network individually. All components behave in their own ways. The purpose of the network is to link together every component in the system to work together. - -### File Structure -One of the biggest sources of confusion for energy networks is the file structure. The files for every part of a network are located at trunk/SUAVE/**Components/Energy**. Within that we have several subfolders. - -#### /Converters -Converters are defined as component that takes energy or power from one form to another. It could be electrical to mechanical, or even chemical to mechanical, etc.. Examples in this folder include a motor, a solar panel, and the compressor section of a jet engine. -#### /Distributors -Distributors move power from one part of the network to another. The common use of this is an electronic speed controller for a small UAV. -#### /Networks -This is where all the "Network" scripts that tie together all of the pieces are kept. Examples in here are a turbofan network. -#### /Peripherals -Peripherals are items that rely on the network but do not produce thrust or power for the vehicle. For example, avionics require electricity which must be accounted for. -#### /Processes -Processes are non tangible parts of a network that are necessary. For example the process is thrust. This function is useful for jet engines to combine and dimensionalize the final thrust once all the components are combined in the network. -#### /Storages -Storages, for now, include batteries. However, in the future we could have fuel tanks here. Currently fuel is only handled as a mass variation. - -### Component Example -Below is a simple example of the most basic energy component in SUAVE. All energy components are classes. The A solar panel is a converter since it converts a photonic flux calculated by a solar radiation model and converts it to a power. - - # Solar_Panel.py - # - # Created: Jun 2014, E. Botero - # Modified: Jan 2016, T. MacDonald - - # ---------------------------------------------------------------------- - # Imports - # ---------------------------------------------------------------------- - - # suave imports - import SUAVE - - from SUAVE.Components.Energy.Energy_Component import Energy_Component - - # ---------------------------------------------------------------------- - # Solar_Panel Class - # ---------------------------------------------------------------------- - class Solar_Panel(Energy_Component): - - def __defaults__(self): - self.area = 0.0 - self.efficiency = 0.0 - - def power(self): - - # Unpack - flux = self.inputs.flux - efficiency = self.efficiency - area = self.area - - p = flux*area*efficiency - - # Store to outputs - self.outputs.power = p - - return p - -These classes contain functions that simulate a process. Multiple functions can exist within a component. This component has defaults, inputs, and outputs. Defaults are provided that give the user an idea of what the fixed parameters of the component are. These values are set when initializing a vehicle. This is the recipe that all energy components are built off. - -### Network Scripts -Network scripts are the link between these components. The network script allows you to reconfigure the connection between components to create your dream propulsion system. These must be logically created as components have set inputs and outputs. For example, you can't magically go from a battery to a propeller without anything in between. Some knowledge of the inputs and outputs are necessary, however they're generally quite intuitive. One interesting avenue for SUAVE is that you can create networks of networks. - -The linking process works like this: - - # step 1 - solar_flux.solar_radiation(conditions) - # link - solar_panel.inputs.flux = solar_flux.outputs.flux - # step 2 - solar_panel.power() - # link - solar_logic.inputs.powerin = solar_panel.outputs.power - -Notice the first step above is to calculate the solar radiation. Once the solar radiation is calculated the components are linked and step 2 can continue with the the power being calculated. From there a solar logic component will use that power. - -The other main hallmark of a network is that they are called at every point in the mission to calculate the state of the system. Given some *conditions* data that defines the state of the vehicle the components must provide back to the mission being solved a thrust force and a mass rate. Other outputs can be stored back to conditions, however a thrust and a mass rate must be returned. - -### Vehicle Script Setup of a Network - -Here we will provide a snippet of the turbofan setup for a B737. - - # ------------------------------------------------------------------ - # Component 3 - Low Pressure Compressor - - # instantiate - compressor = SUAVE.Components.Energy.Converters.Compressor() - compressor.tag = 'low_pressure_compressor' - - # setup - compressor.polytropic_efficiency = 0.91 - compressor.pressure_ratio = 1.14 - - # add to network - turbofan.append(compressor) - -In the above example, a compressor is added to the network. The compressor is tagged as the low_pressure_compressor to distinguish it from the high pressure compressor. The polytropic efficiency and pressure ratio are set. Finall it is appended to the network. diff --git a/documentation/_posts/2000-01-06-optimization.md b/documentation/_posts/2000-01-06-optimization.md deleted file mode 100644 index 1d8ecf3a..00000000 --- a/documentation/_posts/2000-01-06-optimization.md +++ /dev/null @@ -1,163 +0,0 @@ ---- -layout: post -title: Optimization Structure -date: 2017-01-05 13:25:00 -categories: blog -description: Understanding the optimization framework - -permalink: /guides/optimization.html ---- - -## Optimization Code Structure - -This is an overview of how optimization is done in SUAVE. A specific tutorial case is also available [here](/guides/regional_jet_optimization.html). - -### Nexus Class - -The Nexus class is the underlying data structure that is used for optimization. It is created to hold all data and functionality needed to link together optimizers and the various analysis modules in SUAVE. Detailed information on each of the functions can be found on our [doxygen page](/doxygen). - -### Standard Optimization File Structure - -These are the standard files that are used in the optimization process. They are typically stored as Optimize.py, Vehicle.py, Analysis.py, Mission.py, Procedure.py, and Plot_Mission.py. These names can be changed if desired. - -#### Optimize - -This is the top level file that is run to perform the optimization. Inputs, objective, constraints, and aliases are specified here. The inputs have an initial value, bounds, a scaling factor, and the units used. This provides later functions with the information needed to vary the parameters. Units.less indicates a unitless quantity. SI units are the default in SUAVE's internal calculations, so Units.meter will not modify the internal value, while something like Units.foot will. - - problem.inputs = np.array([ - [ 'wing_area' , 125. , ( 120. , 180. ) , 100. , Units.meter**2], - [ 'aspect_ratio' , 3.3 , ( 2.0 , 6.0 ) , 10. , Units.less], - ]) - -Constraints and the objective are similar. Both have scaling quantities and constraints also have bounds. - - problem.constraints = np.array([ - [ 'design_range_fuel_margin', '>', 0., 1E-1, Units.less] - ]) - - problem.objective = np.array([ - ['fuel_burn_rate', 1., Units.kg/Units.s] - ]) - -Finally we have aliases. This provides the optimization process with the position of the various parameters in the data structure. Aliases are used so that short names can be used for variables and a single variable can control multiple items in the data structure. Controlling multiple items can be important if different vehicle configurations are used at different points in the mission, and one of the vehicle parameters should change in the same way for all of the configurations. We can use * as a wildcard. This is used below to change the aspect ratio of the main wing in every vehicle configuration. - - problem.aliases = [ - [ 'wing_area' , ['vehicle_configurations.base.wings.main_wing.areas.reference', - 'vehicle_configurations.base.reference_area']], - [ 'aspect_ratio' , 'vehicle_configurations.*.wings.main_wing.aspect_ratio' ], - [ 'fuel_burn_rate' , 'summary.fuel_burn_rate' ], - ] - -This file then specifies the configurations, analyses, missions, and procedure that will be used. This are typically contained in separate files and more details on each are below. Once all of this is specified, the desired optimizer is called with the nexus class created by this setup. - -#### Vehicle Setup - -This contains the vehicle information such as geometric data and configurations. It is the same as the vehicle setup used for basic analysis purposes. - -#### Analysis Setup - -This contains information on what analyses should be run for the vehicle. For example if correlation-based aerodynamics or AVL should be used for computations. It requires vehicle information from the previous step. - -#### Mission Setup - -This is also the same as the standard mission setup. It determines how the mission will be flown. It requires analysis information from the previous step. - -#### Procedure - -This is an optimization specific file that determines how the vehicle, analysis, or mission is modified with the input values in the optimization and also runs the mission. For example, changing the wing area will usually require changes to other wing parameters, such as root chord length. This module reads the new inputs and changes other values accordingly based on user specified processes. - -#### Plotting - -This function is not necessary to the optimization, but is often included in the files used and is added to the optimize main call as a way to visualize the results. - -### Optimizer Interface - -The other step that must be taken to perform an optimization is to convert the standardized input above into values that can be used by the selected optimizer. This is done through a separate script for each optimizer, all of which are found in the [optimization folder](doxygen_link_here). - -For example, if we are using PyOpt to optimize, we might use `output = pyopt_setup.Pyopt_Solve(problem,solver='SNOPT')` in the main function of the top level optimizer. This function reads the inputs, constraints, and objective and converts them to a format that the selected optimizer (SNOPT here) can understand. - -### Evaluation Process - -This shows the typical evaluation process, including where items like inputs and aliases are used. This chart assumes a single objective call, but some optimizers will include calls such as `all_constraints` which require another evaluation. If the evaluation is a duplicate, data from the previous evaluation will be used instead of stepping through the procedure again. - -  - - - -  - -### Incorporating Multi-fidelity - -Multiple levels of fidelity are designed to be relatively easy to incorporate in SUAVE, but there are still a few things to keep in mind. First, the chosen optimizer must support multi-fidelity and be able to change the `nexus.fidelity_level` value. Once this is done, it is also important to remember that the mission is set up based on the analyses. This means that if a change is made to the analyses then the mission must be rebuilt with the new settings. As an example, code below for changing the analysis level is shown. This is a function that has been added to the procedure file. - - def set_fidelity_level(nexus): - - if nexus.has_key('fidelity_level') == False: - print 'Fidelity level not set, defaulting to 1' - nexus.fidelity_level = 1 - - if nexus.fidelity_level == 2: - aerodynamics = SUAVE.Analyses.Aerodynamics.Supersonic_OpenVSP_Wave_Drag() - aerodynamics.settings.number_slices = 20 - aerodynamics.settings.number_rotations = 10 - elif nexus.fidelity_level == 1: - aerodynamics = SUAVE.Analyses.Aerodynamics.Supersonic_Zero() - else: - raise ValueError('Selected fidelity level not supported') - aerodynamics.geometry = copy.deepcopy(nexus.vehicle_configurations.base) - nexus.analyses.base.append(aerodynamics) - - nexus.missions = mission_as2.setup(nexus.analyses) - - return nexus - -Here we see that `nexus.missions` has been updated in addition to `nexus.analyses`, since failing to do this would have the mission run with the previous analysis settings. - -### Key Functions in the Optimizer Setup - -We briefly mentioned how optimization parameters would need to be converted so that they could run with a particular optimizer. Here we show how this is managed and show which functions are likely to be useful in building a new optimizer setup. - -The key items that will be needed for most optimizers are shown below, taken from the PyOpt setup: - - inp = problem.optimization_problem.inputs - obj = problem.optimization_problem.objective - con = problem.optimization_problem.constraints - - # Set inputs - nam = inp[:,0] # Names - ini = inp[:,1] # Initials - bnd = inp[:,2] # Bounds - scl = inp[:,3] # Scale - typ = inp[:,4] # Type - -These can be scaled with two helper functions that are part of the SUAVE distribution: - - from SUAVE.Optimization import helper_functions as help_fun - - bnd_constraints = help_fun.scale_const_bnds(con) - scaled_constraints = help_fun.scale_const_values(con,bnd_constraints) - x = ini/scl - -What happens next is entirely dependent on what optimizer you want to use. Some may require that constraint bounds happen at 0 or are either > or <. However this setup is done, you will likely need to create a function that can accept the problem and inputs and give required outputs such as the objective value and constraints. In the PyOpt case, this is done with a simple wrapper and an added function: - - mywrap = lambda x:PyOpt_Problem(problem,x) - -... - - def PyOpt_Problem(problem,x): - - obj = problem.objective(x) - const = problem.all_constraints(x).tolist() - fail = np.array(np.isnan(obj.tolist()) or np.isnan(np.array(const).any())).astype(int) - - - print 'Inputs' - print x - print 'Obj' - print obj - print 'Con' - print const - - return obj,const,fail - -Please visit our [forum](/forum) if you have any other questions on how the optimizer interface works or how to convert the values to what you need. \ No newline at end of file diff --git a/documentation/_posts/2015-06-14-Code_Style.md b/documentation/_posts/2015-06-14-Code_Style.md deleted file mode 100644 index 0b394f76..00000000 --- a/documentation/_posts/2015-06-14-Code_Style.md +++ /dev/null @@ -1,61 +0,0 @@ ---- -layout: post -title: Code Style -date: 2017-01-10 13:25:00 -categories: blog -description: Code style and basic development information - -permalink: /guides/style.html ---- - - - - - -## SUAVE Code Style Guide - -SUAVE is built on a slightly modified PEP8 style guide, with changes made to implement a data-oriented view of the code. To help support discovering code, the SUAVE folder structure explicitly mirrors the package structure. Flexibility of the package structure is important, so in general all objects live in their own file, with the same file name as the object name. In order to maintain a separation between Analysis and Data structures, there are often parallel package trees inside the main branches of the package, like SUAVE.Methods.Aerodynamics and SUAVE.Analysis.Aerodynamics. Where possible the names of fields that live in the SUAVE package are written out verbosely, avoiding jargon built on mathematical variable names or acronyms. - -Templates for new methods and objects can be found in the SUAVE repo's [templates](https://github.com/suavecode/SUAVE/tree/develop/templates) folder. - -### Naming Convention - -In terms of typography -- - -* ```any_variable_name``` - lower case with underscore
- This includes working variables and instantiated objects. -* ```field_name``` - lower case with underscore - Any field of an object should be lower case. -* ```function_name``` - lower case with underscore -* ```Class_Type``` - upper case with underscore
- The underscores are chosen here to permit the inclusion of acronyms if needed and to maintain symmetry with field name styling. -* ```Package_Name``` - upper case with underscore
- For example folders within the SUAVE package. - - -In terms of naming -- - -* Chunk similar field types under a containing field -* Bias names towards being specific -* Write out field name verbosely, but try to keep short - - -### Development Life Cycle - -As you develop new features for SUAVE, this is generally how you can expect your feature to evolve, in terms of its level of abstraction, and where it lives. - -1. Prototype
- Either a new function or class. You may want to test these within a separate folder. If you are developing a new analysis approach, for example for aerodynamics or weights, you can usually start with a function. If you are working off of an object like a wing, you can abstract the objects as needed. Generally the lowest level object you'll use is the SUAVE.Core.Data class.
- A lot of development can be accomplished in a local environment. - -2. Initial Integration
- Once you're comfortable that your new feature works robustly, and that it has been tested, it's time to integrate it into SUAVE. Here are some tips for identifying where it could live. - - SUAVE.Methods - if it's a python function. Ping the [forum](http:suavecode.github.io/forum) if you want to double check your decision! - - SUAVE.Analyses - if it's an object that manages an analysis like aerodynamics - - SUAVE.Components - if it's a data storage container for a vehicle component like a wing or landing gear - - SUAVE.Attributes - if it's a data storage container for any other type of object, like atmospheres or water
- - At this point you might want to initiate a pull request to contribute the code back to the main repository.
- -3. Full-Blown Subpackage
- As you write more code, and follow the SUAVE style of keeping one file per object, you will need to create a folder to contain a subpackage. This step may come later in the life of your code, so don't rush to it if you don't need the extra overhead. diff --git a/documentation/_posts/2015-06-14-doc_instructions.md b/documentation/_posts/2015-06-14-doc_instructions.md deleted file mode 100644 index ebabc15d..00000000 --- a/documentation/_posts/2015-06-14-doc_instructions.md +++ /dev/null @@ -1,108 +0,0 @@ ---- -layout: post -title: Using the Documentation -date: 2017-01-09 13:25:00 -categories: blog -description: Reading (and writing) the documentation - -permalink: /guides/docs.html ---- - -### How to Read (and Write) the Documentation - -This is an explanation of how documentation is built in SUAVE so that the user can know what to look for and how to write it if they wish to add their own code. The doxygen page is available [here](/doxygen). - -### Docstrings - -All classes and functions in SUAVE have docstrings have docstrings. These give the user an understanding of what the function does and information on the input and output variables. - -#### Classes - -For a class, the docstring has three parts: - -* General description -* Assumptions -* Source - -The general description provides a brief summary of what the class is used for. Assumptions list any significant assumptions are important in how it is used. This may be listed as None or N/A if there are no important assumptions. The source section should provide the general source of methods in the class. If there is no overall source, a message like 'see sources in functions' may be appropriate. There are also cases where a source is not relevant, such as simple geometric functions, and may also be listed as None or N/A. - -#### Class Docstring Template - -This is the general template that can be used when creating a new class. It should be placed directly under the class declaration. - - """ - - Assumptions: - - - Source: - - """ - -#### Functions - -For functions there are six categories: - -* Description - -This is a general description of what the function does. It should also include any key information that does not fit into one of the other categories. - -* Assumptions - -This should contain any assumptions made by the function. None or N/A can be used if none are used. - -* Source - -The source of any methods that have been implemented. Simple methods like basic geometric relations do not need a source. - -* Inputs - -This should contain any variables or functions passed to the function. If the passed variable is a data structure, the components that are used should be listed. Each item should include a description if it is not obvious from the name. It should also include any relevant units. In addition, information about the variable type or any other information that might be important can be added here. - -* Outputs - -This should contain the same information as in the inputs. It may also contain information on variables that are modified but not explicitly returned. - -* Properties Used - -This carries the same information as input and outputs. It typically contains variables that are properties of the parent class but are not modified. There is some overlap with inputs and outputs, but either category is acceptable as long as the variable is documented. - -#### Function Docstring Template - -This is a template docstring: - - """ - - Assumptions: - - - Source: - - - Inputs: - - - .. - - Outputs: - - - .. - - Properties Used: - - - .. - """ - -### Doxygen Grouping Tags - -Tags are used to put files into groups that match the SUAVE file structure. `@defgroup` tags define a group and should be placed in the init file. An example is shown here: - - ## @defgroup Analyses-Aerodynamics Aerodynamics - # These are the analyses that control aerodynamic evaluations. - # @ingroup Analyses - -In this example, `Analyses-Aerodynamics` is the doxygen tag for the group, while the group appears in the documentation as `Aerodynamics`, the next part of the string. The tag is based on the file structure (Analyses/Aerodynamics here). Since this is a subgroup of Analyses, `@ingroup Analyses` is used here, with `Analyses` as the doxygen tag for the next level up. - -In files, the `@ingroup` tag should be inserted before all classes and stand-alone functions. The tag should match the tag in the folder init file's `@defgroup` string. diff --git a/documentation/_posts/2018-06-15-FAQ.md b/documentation/_posts/2018-06-15-FAQ.md deleted file mode 100644 index 24217453..00000000 --- a/documentation/_posts/2018-06-15-FAQ.md +++ /dev/null @@ -1,68 +0,0 @@ ---- -layout: post -title: Frequently Asked Questions -date: 2010-06-15 14:20:00 -categories: blog -description: We know what you're thinking - -permalink: /faq.html ---- - - - -Alright, you dove in and now you're stuck. You've come to a good starting point. If this FAQ fails you then we suggest you go through tutorials, maybe our [paper](http://adl.stanford.edu/papers/suave-open-source.pdf), send us a question in the forum, or if all else fails start reading code. Don't worry the code is more readable than most engineering textbooks. - -[comment]: <> (lowercase, no question marks for tags, total freedom in text) - - - [How do I get started?](#how-do-i-get-started) - - [What version of Python should I use?](#what-version-of-python-should-i-use) - - [Can I use SUAVE for my own research?](#can-i-use-suave-for-my-own-research) - - [How can I contribute?](#how-can-i-contribute) - - [How can I best get in touch with you or ask for help?](#how-can-i-best-get-in-touch-with-you-or-ask-for-help) - - [Where can I see the recent additions to the SUAVE environment?](#where-can-i-see-the-recent-additions-to-the-suave-environment) - - [Are there plans to make a Graphical User Interface?](#are-there-plans-to-make-a-graphical-user-interface) - - [How is a mission solved?](#how-is-a-mission-solved) - -
- -### How do I get started? - -* Download SUAVE’s current release on our [download](/download/) page. Specific steps and further instructions for additional software requirements are also listed there. -* Get familiar with the code using our [guides](guides/). Be sure to start the [Boeing 737 Tutorial](/guides/boeing_737-800.html) for a basic introduction and the Regional Jet Optimization for the optimization tools. -* Ask any remaining questions on the [forum](/forum) - -### What version of Python should I use? -SUAVE is developed in Python 2.7. - -### Can I use SUAVE for my own research? -Yes, you may! Please cite our papers: - -- [T. Lukaczyk, A. Wendorff, E. Botero, T. MacDonald, T. Momose, A. Variyar, J. M. Vegh, M. Colonno, T. Economon, J. J. Alonso, T. Orra, C. Ilario, "SUAVE: An Open-Source Environment for Multi-Fidelity Conceptual Vehicle Design", 16th AIAA Multidisciplinary Analysis and Optimization Conference, Dallas, TX, June 2015.](http://adl.stanford.edu/papers/suave-open-source.pdf) - -- [E. Botero, A. Wendorff, T. MacDonald, A. Variyar, J. M. Vegh, T. Lukaczyk, J. J. Alonso, T. Orra, C. Ilario da Silva. "SUAVE: An Open-Source Environment for Conceptual Vehicle Design and Optimization", 54th AIAA Aerospace Sciences Meeting, San Diego, CA, January 2016.](http://adl.stanford.edu/papers/suave-optimization.pdf) - -- [T. MacDonald, E. Botero, J. M. Vegh, A. Variyar, J. J. Alonso, T. Orra, C. Ilario da Silva. "SUAVE: An Open-Source Environment Enabling Unconventional Designs through Higher Fidelity", 55th AIAA Aerospace Sciences Meeting, Grapevine, TX, January 2017.](http://adl.stanford.edu/papers/suave-hi-fi.pdf) - -- [T. MacDonald, M. Clarke, E. Botero, J. M. Vegh, J. J. Alonso. "SUAVE: An Open-Source Environment Enabling Multi-fidelity Vehicle Optimization", 16th AIAA Multidisciplinary Analysis and Optimization Conference, Denver, CO, June 2017.](http://adl.stanford.edu/papers/suave-mf-opt.pdf) - -### How can I contribute? -We encourage SUAVE users to expand the environment according to their personal interests. The main areas to be developed are listed [here](/develop/#areas-of-development). - -### How can I best get in touch with you or ask for help? -The [forum](/forum) is our main point of contact for SUAVE discussions. - -### Where can I see the recent additions to the SUAVE environment? -Go and check the develop branch on our [GitHub site](https://github.com/suavecode/SUAVE). This branch contains new features that are functional but not necessarily ready for release. Everything in this branch is added to the master branch at the next release. Several other feature branches can also be seen here. These are typically under active development. For any more information on what is available please ask on the [forum](/forum) - -### Are there plans to make a Graphical User Interface? -The core development team is currently not planning on developing a GUI, but you can help! Contact us via the [forum](/forum). - -### How is a mission solved? - -A mission is divided into segments, for example climb, cruise, etc… Then the segment is divided into discrete points that are cosine spaced in time. These make up Chebyshev collocation points. One of the beauties of this method is the integration and differentiation operator. So if you know the velocity at every point, then you can get accelerations and vice-versa. - -The default value is 16 points in each segment for SUAVE. However, our internal numerical experiments have shown highly accurate results with ~0.1% error with only 4 control points and ~.0001% error with 8 as measured from a very highly refined answered. - -For each control point there are various unknowns and residuals. An example of an unknown would be pitch angle, and a residual would be the forces in the Z direction. After performing an analysis using the unknowns the residuals are calculated. These unknowns and residuals are iterated through a hybrid solver (much like a Newton method) in SciPy to converge the residual to zero. Voila, with a little magic you have results! - - diff --git a/documentation/code_style.html b/documentation/code_style.html new file mode 100644 index 00000000..5a59e5e2 --- /dev/null +++ b/documentation/code_style.html @@ -0,0 +1,184 @@ + + + + + Code Style + + + + + + + + + +
+ + + + + +
+
+
+ + + + +

SUAVE Code Style Guide

+ +

SUAVE is built on a slightly modified PEP8 style guide, with changes made to implement a data-oriented view of the code. To help support discovering code, the SUAVE folder structure explicitly mirrors the package structure. Flexibility of the package structure is important, so in general all objects live in their own file, with the same file name as the object name. In order to maintain a separation between Analysis and Data structures, there are often parallel package trees inside the main branches of the package, like SUAVE.Methods.Aerodynamics and SUAVE.Analysis.Aerodynamics. Where possible the names of fields that live in the SUAVE package are written out verbosely, avoiding jargon built on mathematical variable names or acronyms.

+ +

Templates for new methods and objects can be found in the SUAVE repo’s templates folder.

+ +

Naming Convention

+ +

In terms of typography –

+ +
    +
  • any_variable_name - lower case with underscore
    + This includes working variables and instantiated objects.
  • +
  • field_name - lower case with underscore + Any field of an object should be lower case.
  • +
  • function_name - lower case with underscore
  • +
  • Class_Type - upper case with underscore
    + The underscores are chosen here to permit the inclusion of acronyms if needed and to maintain symmetry with field name styling.
  • +
  • Package_Name - upper case with underscore
    + For example folders within the SUAVE package.
  • +
+ +

In terms of naming –

+ +
    +
  • Chunk similar field types under a containing field
  • +
  • Bias names towards being specific
  • +
  • Write out field name verbosely, but try to keep short
  • +
+ +

Development Life Cycle

+ +

As you develop new features for SUAVE, this is generally how you can expect your feature to evolve, in terms of its level of abstraction, and where it lives.

+ +
    +
  1. +

    Prototype
    + Either a new function or class. You may want to test these within a separate folder. If you are developing a new analysis approach, for example for aerodynamics or weights, you can usually start with a function. If you are working off of an object like a wing, you can abstract the objects as needed. Generally the lowest level object you’ll use is the SUAVE.Core.Data class.
    + A lot of development can be accomplished in a local environment.

    +
  2. +
  3. Initial Integration
    + Once you’re comfortable that your new feature works robustly, and that it has been tested, it’s time to integrate it into SUAVE. Here are some tips for identifying where it could live. +
      +
    • SUAVE.Methods - if it’s a python function. Ping the forum if you want to double check your decision!
    • +
    • SUAVE.Analyses - if it’s an object that manages an analysis like aerodynamics
    • +
    • SUAVE.Components - if it’s a data storage container for a vehicle component like a wing or landing gear
    • +
    • SUAVE.Attributes - if it’s a data storage container for any other type of object, like atmospheres or water
    • +
    + +

    At this point you might want to initiate a pull request to contribute the code back to the main repository.

    +
  4. +
  5. Full-Blown Subpackage
    + As you write more code, and follow the SUAVE style of keeping one file per object, you will need to create a folder to contain a subpackage. This step may come later in the life of your code, so don’t rush to it if you don’t need the extra overhead.
  6. +
+ +
+ + +
+
+
+ + + + + + + + + + + + + + \ No newline at end of file diff --git a/documentation/energy_nets.html b/documentation/energy_nets.html new file mode 100644 index 00000000..01c18b45 --- /dev/null +++ b/documentation/energy_nets.html @@ -0,0 +1,234 @@ + + + + + Energy Networks + + + + + + + + + +
+ + + + + +
+
+
+ + +
+ +

Energy Networks

+

+Energy networks are really a fancy name for your propulsion system. The reason we call them a network rather than “engine” or the like is that it encompasses far more than that. These “energy networks” are the complex systems that future aircraft will incorporate that can reduce or eliminate fuel burn. For example if you have a hybrid gas-electric aircraft you don’t have just an engine. You have an engine, a motor, batteries, a generator, a gearbox, a propeller or ducted fan, wiring, electronics… and that doesn’t include the parts inside the internal combustion engine. Modeling these systems completely is essential in designing such a vehicle.

+ +

To do this we depart from the typical SUAVE structure of analyses and methods. This was done because we want to look at each component of the network individually. All components behave in their own ways. The purpose of the network is to link together every component in the system to work together.

+ +

File Structure

+

One of the biggest sources of confusion for energy networks is the file structure. The files for every part of a network are located at trunk/SUAVE/Components/Energy. Within that we have several subfolders.

+ +

/Converters

+

Converters are defined as component that takes energy or power from one form to another. It could be electrical to mechanical, or even chemical to mechanical, etc.. Examples in this folder include a motor, a solar panel, and the compressor section of a jet engine.

+

/Distributors

+

Distributors move power from one part of the network to another. The common use of this is an electronic speed controller for a small UAV.

+

/Networks

+

This is where all the “Network” scripts that tie together all of the pieces are kept. Examples in here are a turbofan network.

+

/Peripherals

+

Peripherals are items that rely on the network but do not produce thrust or power for the vehicle. For example, avionics require electricity which must be accounted for.

+

/Processes

+

Processes are non tangible parts of a network that are necessary. For example the process is thrust. This function is useful for jet engines to combine and dimensionalize the final thrust once all the components are combined in the network.

+

/Storages

+

Storages, for now, include batteries. However, in the future we could have fuel tanks here. Currently fuel is only handled as a mass variation.

+ +

Component Example

+

Below is a simple example of the most basic energy component in SUAVE. All energy components are classes. The A solar panel is a converter since it converts a photonic flux calculated by a solar radiation model and converts it to a power.

+ +
# Solar_Panel.py
+#
+# Created:  Jun 2014, E. Botero
+# Modified: Jan 2016, T. MacDonald
+
+# ----------------------------------------------------------------------
+#  Imports
+# ----------------------------------------------------------------------
+
+# suave imports
+import SUAVE
+
+from SUAVE.Components.Energy.Energy_Component import Energy_Component
+
+# ----------------------------------------------------------------------
+#  Solar_Panel Class
+# ----------------------------------------------------------------------
+class Solar_Panel(Energy_Component):
+
+def __defaults__(self):
+	self.area       = 0.0
+	self.efficiency = 0.0
+
+def power(self):
+	
+	# Unpack
+	flux       = self.inputs.flux
+	efficiency = self.efficiency
+	area       = self.area
+	
+	p = flux*area*efficiency
+	
+	# Store to outputs
+	self.outputs.power = p
+
+	return p
+
+ +

These classes contain functions that simulate a process. Multiple functions can exist within a component. This component has defaults, inputs, and outputs. Defaults are provided that give the user an idea of what the fixed parameters of the component are. These values are set when initializing a vehicle. This is the recipe that all energy components are built off.

+ +

Network Scripts

+

Network scripts are the link between these components. The network script allows you to reconfigure the connection between components to create your dream propulsion system. These must be logically created as components have set inputs and outputs. For example, you can’t magically go from a battery to a propeller without anything in between. Some knowledge of the inputs and outputs are necessary, however they’re generally quite intuitive. One interesting avenue for SUAVE is that you can create networks of networks.

+ +

The linking process works like this:

+ +
    # step 1
+solar_flux.solar_radiation(conditions)
+# link
+solar_panel.inputs.flux = solar_flux.outputs.flux
+# step 2
+solar_panel.power()
+# link
+solar_logic.inputs.powerin = solar_panel.outputs.power
+
+ +

Notice the first step above is to calculate the solar radiation. Once the solar radiation is calculated the components are linked and step 2 can continue with the the power being calculated. From there a solar logic component will use that power.

+ +

The other main hallmark of a network is that they are called at every point in the mission to calculate the state of the system. Given some conditions data that defines the state of the vehicle the components must provide back to the mission being solved a thrust force and a mass rate. Other outputs can be stored back to conditions, however a thrust and a mass rate must be returned.

+ +

Vehicle Script Setup of a Network

+ +

Here we will provide a snippet of the turbofan setup for a B737.

+ +
# ------------------------------------------------------------------
+#  Component 3 - Low Pressure Compressor
+
+# instantiate 
+compressor = SUAVE.Components.Energy.Converters.Compressor()    
+compressor.tag = 'low_pressure_compressor'
+
+# setup
+compressor.polytropic_efficiency = 0.91
+compressor.pressure_ratio        = 1.14    
+
+# add to network
+turbofan.append(compressor)
+
+ +

In the above example, a compressor is added to the network. The compressor is tagged as the low_pressure_compressor to distinguish it from the high pressure compressor. The polytropic efficiency and pressure ratio are set. Finall it is appended to the network.

+ +
+
+ +
+
+
+ + + + + + + + + + + + + + \ No newline at end of file diff --git a/documentation/faq.html b/documentation/faq.html new file mode 100644 index 00000000..0b9cd260 --- /dev/null +++ b/documentation/faq.html @@ -0,0 +1,194 @@ + + + + + Frequently Asked Questions + + + + + + + + + +
+ + + + + +
+
+
+ + + +

Frequently Asked Questions

+ +

Alright, you dove in and now you’re stuck. You’ve come to a good starting point. If this FAQ fails you then we suggest you go through tutorials, maybe our paper, send us a question in the forum, or if all else fails start reading code. Don’t worry the code is more readable than most engineering textbooks.

+ + + +


+ +

How do I get started?

+ +
    +
  • Download SUAVE’s current release on our download page. Specific steps and further instructions for additional software requirements are also listed there.
  • +
  • Get familiar with the code using our guides. Be sure to start the Boeing 737 Tutorial for a basic introduction and the Regional Jet Optimization for the optimization tools.
  • +
  • Ask any remaining questions on the forum
  • +
+ +

What version of Python should I use?

+

SUAVE is developed in Python 3.5+

+ +

Can I use SUAVE for my own research?

+

Yes, you may! Please cite our papers:

+ + + +

How can I contribute?

+

We encourage SUAVE users to expand the environment according to their personal interests. The main areas to be developed are listed here.

+ +

How can I best get in touch with you or ask for help?

+

The forum is our main point of contact for SUAVE discussions.

+ +

Where can I see the recent additions to the SUAVE environment?

+

Go and check the develop branch on our GitHub site. This branch contains new features that are functional but not necessarily ready for release. Everything in this branch is added to the master branch at the next release. Several other feature branches can also be seen here. These are typically under active development. For any more information on what is available please ask on the forum.

+ +

Are there plans to make a Graphical User Interface?

+

The core development team is currently not planning on developing a GUI, but you can help! Contact us via the forum.

+ +

How is a mission solved?

+ +

A mission is divided into segments, for example climb, cruise, etc… Then the segment is divided into discrete points that are cosine spaced in time. These make up Chebyshev collocation points. One of the beauties of this method is the integration and differentiation operator. So if you know the velocity at every point, then you can get accelerations and vice-versa.

+ +

The default value is 16 points in each segment for SUAVE. However, our internal numerical experiments have shown highly accurate results with ~0.1% error with only 4 control points and ~.0001% error with 8 as measured from a very highly refined answered.

+ +

For each control point there are various unknowns and residuals. An example of an unknown would be pitch angle, and a residual would be the forces in the Z direction. After performing an analysis using the unknowns the residuals are calculated. These unknowns and residuals are iterated through a hybrid solver (much like a Newton method) in SciPy to converge the residual to zero. Voila, with a little magic you have results!

+ +
+
+
+ + +
+ + + + + + + + + + + + + + diff --git a/documentation/index.html b/documentation/index.html deleted file mode 100644 index 6824145c..00000000 --- a/documentation/index.html +++ /dev/null @@ -1,49 +0,0 @@ ---- -layout: awesome ---- - -
- -
- -
-
-

Documentation

-

Everything you ever wanted to know to be SUAVE

-
-
- - -
-

SUAVE is fully documented through doxygen. However, some starter high level documentation is available below.

- - - -

           

-

           

-

           

-

           

-

           

-

           

-

           

-

           

-

           

-

           

- -
- -
- diff --git a/documentation/missions.html b/documentation/missions.html new file mode 100644 index 00000000..88c2ead3 --- /dev/null +++ b/documentation/missions.html @@ -0,0 +1,373 @@ + + + + + Mission Solver Structure + + + + + + + + + +
+ + + + + +
+
+
+ + + + +
+

Mission Solver Code Structure

+ +

This is a high level overview of how the mission solver functions. The purpose is to show the structure that is used for an existing mission, and show where changes should be made if different functionality is desired.

+ +

File Structure

+ +

Mission scripts are split into two folders in the SUAVE repository. The first is in trunk/SUAVE/Analyses/Mission/Segments, and the second is in trunk/SUAVE/Methods/Missions/Segments. As with other types of analyses and methods, the distinction between these is that the Analyses folder contains classes that are built to use functions stored in the Methods folder. This division is done to make it easier to build new analysis classes using a mix of available methods.

+ +

A typical mission segment analysis file contains four keys parts. The first specifies default user inputs, unknowns, and residuals. The inputs are used to provide the analysis with conditions that need to be met, while the unknowns and residuals are used as part of the solution process. The second sets the initialization functions for the analysis, which are run at the beginning. The third picks the convergence method and specifies the functions that will be used during iteration. The fourth finalizes the data and processes it for results output.

+ +

Initialization

+ +

For this tutorial, we will be considering the constant speed constant altitude cruise segment. The files are available here (Analysis) and here (Method). This class also inherits information from more general segment classes, which include many of the processing functions. As with other segments, the user will specify key conditions. For this case, altitude, air speed, and distance are the necessary inputs. If the user does not specify an altitude, it will be taken automatically from the last value in the previous segment. These inputs must be specified in some way for the mission segment to be evaluated. They are shown below as well:

+ +
self.altitude  = None
+		self.air_speed = 10. * Units['km/hr']
+		self.distance  = 10. * Units.km
+		
+ +

The other set of segment specific initial values are the values used for solving the segment (typically this means satisfying a force balance at every evaluation point). These can be changed by the user if needed, but the default values should perform fine for most cases.

+ +
self.state.unknowns.throttle   = ones_row(1) * 0.5
+		self.state.unknowns.body_angle = ones_row(1) * 0.0
+		self.state.residuals.forces    = ones_row(2) * 0.0
+		
+ +

Here throttle and body angle are the unknowns, and the values shown here are the values they will start at. The residuals will be computed based on these unknowns, so their initial value is not important. Instead they are initialized just to create the necessary data structure. The ones_row line will create a numpy array with the number of elements needed for evaluation.

+ +

Evaluation Details

+ +

Most of the missions in SUAVE, including this one, are broken into several points in time based on a Chebyshev polynomial. This causes the points to be closer together at either end of the segment. The choice of a Chebyshev polynomial (which creates cosine spacing) provides better convergence and smoothness properties versus other methods such as linear spacing.

+ +

+ +

At each of these points the aerodynamic analysis is queried to find CL and CD, which are then converted to lift and drag. These values will be dependent on the body angle unknown and other aerodynamic parameters. Thrust is found from the vehicle’s energy network, which is dependent on the throttle unknown. A weight is determined by looking at the initial weight and subsequent mass rate (typically corresponding with fuel burn). In this cruise segment, these forces are summed in 2D and the results are put in the residuals. The functions needed to arrive these forces are found in the Update Conditions section of the Analysis file. This section is also shown below in one of the steps to create a new mission.

+ +

Once the evaluation process has been performed at all points, the unknowns and residuals are fed back to the solve routine, which in this case is scipy’s fsolve. The file that performs this process is here. This routine continues evaluating the points until convergence is reached. Once this happens, post processing is done to put the data in the results output.

+ +

Using Multiple Segments

+ +

Multiple segments can be run sequentially by appending them in the desired order. Examples of this are in all the tutorial files that have an aircraft fly a full mission. In addition, the full mission can be run simultaneously will all segment constraints used together. If you are interested in doing something like this, please ask us about it on our forum.

+ +

Process Summary

+ +

Mission Setup

+ +
    +
  • Initializes default values for unknowns
  • +
  • Initializes set of functions used to determine residuals
  • +
  • Reads user input for segment parameters
  • +
  • Adds the analysis group to be used (including the vehicle and items like atmosphere)
  • +
  • Appends segments in order
  • +
+ +

Evaluate

+ +
    +
  • Varies unknowns until residual convergence is reached using scipy’s fsolve
  • +
  • Repeats process for each segment until full mission is complete
  • +
+ +

Adding New Mission Segments

+ +

The segment described above uses two unknowns to solve force residuals in two dimensions. This general setup works well for many problems of interest, but SUAVE is designed to accommodate other mission analysis types as well. A user may want to add control surface deflection and solve for moments as well, or look at forces in all three dimensions.

+ +

In addition, a user may want to modify how the mission is flown, as is done with the many other segments currently available. They may want to modify how the mission is solved, such as is done in our single point evaluation segments where finite differencing is not relevant.

+ +

Here we will explain the process of modifying our constant speed constant rate climb segment to be constant throttle constant speed. This still uses 2D force balance but changes the profile. There are four functions that are modified here. The first is shown below. The functions can be found in here and here

+ +
def initialize_conditions(segment,state):
+		
+		# unpack
+		climb_rate = segment.climb_rate
+		air_speed  = segment.air_speed   
+		alt0       = segment.altitude_start 
+		altf       = segment.altitude_end
+		t_nondim   = state.numerics.dimensionless.control_points
+		conditions = state.conditions  
+		
+		# check for initial altitude
+		if alt0 is None:
+			if not state.initials: raise AttributeError('initial altitude not set')
+			alt0 = -1.0 * state.initials.conditions.frames.inertial.position_vector[-1,2]
+		
+		# discretize on altitude
+		alt = t_nondim * (altf-alt0) + alt0
+		
+		# process velocity vector
+		v_mag = air_speed
+		v_z   = -climb_rate # z points down
+		v_x   = np.sqrt( v_mag**2 - v_z**2 )
+		
+		# pack conditions    
+		conditions.frames.inertial.velocity_vector[:,0] = v_x
+		conditions.frames.inertial.velocity_vector[:,2] = v_z
+		conditions.frames.inertial.position_vector[:,2] = -alt[:,0] # z points down
+		conditions.freestream.altitude[:,0]             =  alt[:,0] # positive altitude in this context
+		
+ +

This function initializes speed and altitude based on the given climb rate, airspeed, and altitude end points. t_nondim gives nondimensional time in cosine spacing from 0 to 1 in order to pick the values at the points to be evaluated. Unfortunately, when we use constant throttle we cannot know beforehand exactly how altitude (or climb rate in this case) will vary with time, so altitude cannot be spaced with this method. Instead a different function is used to initialize conditions:

+ +
def initialize_conditions(segment,state):
+		
+		# unpack
+		throttle   = segment.throttle
+		air_speed  = segment.air_speed   
+		alt0       = segment.altitude_start 
+		altf       = segment.altitude_end
+		t_nondim   = state.numerics.dimensionless.control_points
+		conditions = state.conditions  
+		
+		# check for initial altitude
+		if alt0 is None:
+			if not state.initials: raise AttributeError('initial altitude not set')
+			alt0 = -1.0 * state.initials.conditions.frames.inertial.position_vector[-1,2]
+		
+		# pack conditions  
+		conditions.propulsion.throttle[:,0] = throttle
+		conditions.frames.inertial.velocity_vector[:,0] = air_speed # start up value
+		
+ +

Here only the throttle and air speed are loaded in, and discretization of other values will need to occur later so that it is part of the iteration loop. This requires a new function that updates the altitude differentials.

+ +
def update_differentials_altitude(segment,state):
+		
+		# unpack
+		t = state.numerics.dimensionless.control_points
+		D = state.numerics.dimensionless.differentiate
+		I = state.numerics.dimensionless.integrate
+		
+		
+		# Unpack segment initials
+		alt0       = segment.altitude_start 
+		altf       = segment.altitude_end    
+		conditions = state.conditions  
+		
+		r = state.conditions.frames.inertial.position_vector
+		v = state.conditions.frames.inertial.velocity_vector
+		
+		# check for initial altitude
+		if alt0 is None:
+			if not state.initials: raise AttributeError('initial altitude not set')
+			alt0 = -1.0 * state.initials.conditions.frames.inertial.position_vector[-1,2]    
+		
+		# get overall time step
+		vz = -v[:,2,None] # Inertial velocity is z down
+		dz = altf- alt0    
+		dt = dz / np.dot(I[-1,:],vz)[-1] # maintain column array
+		
+		# Integrate vz to get altitudes
+		alt = alt0 + np.dot(I*dt,vz)
+		
+		# rescale operators
+		t = t * dt
+		
+		# pack
+		t_initial = state.conditions.frames.inertial.time[0,0]
+		state.conditions.frames.inertial.time[:,0] = t_initial + t[:,0]
+		conditions.frames.inertial.position_vector[:,2] = -alt[:,0] # z points down
+		conditions.freestream.altitude[:,0]             =  alt[:,0] # positive altitude in this context    
+		
+		return
+		
+ +

In this function, t, D, and I are numpy arrays that allow approximate differentiation and integration. Since the total time is not known without determining the climb rate, we must first determine the time required to reach the final altitude. The line dt = dz / np.dot(I[-1,:],vz)[-1] does this with the integrator providing the amount of altitude gained if the velocities were spread across just one second instead of the full segment time. This gives the scaling quantity dt that is then used to get the altitude at every point in alt = alt0 + np.dot(I*dt,vz). The values for altitude are then are then packed for use in other functions.

+ +

The above allows us to deal with discretization without a known profile, but we also must calculate the velocity in order to use this. This is done with another added function.

+ +
def update_velocity_vector_from_wind_angle(segment,state):
+		
+		# unpack
+		conditions = state.conditions 
+		v_mag  = segment.air_speed 
+		alpha  = state.unknowns.wind_angle[:,0][:,None]
+		theta  = state.unknowns.body_angle[:,0][:,None]
+		
+		# Flight path angle
+		gamma = theta-alpha
+		
+		# process
+		v_x =  v_mag * np.cos(gamma)
+		v_z = -v_mag * np.sin(gamma) # z points down
+		
+		# pack
+		conditions.frames.inertial.velocity_vector[:,0] = v_x[:,0]
+		conditions.frames.inertial.velocity_vector[:,2] = v_z[:,0]
+		
+		return conditions
+		
+ +

This uses our new set of unknowns to determine the velocities.

+ +

Additionally, since the unknowns are different we must change the function that unpacks them. Wind angle does not need to be stored so it is not included here.

+ +
def unpack_body_angle(segment,state):
+		
+		# unpack unknowns
+		theta  = state.unknowns.body_angle
+		
+		# apply unknowns
+		state.conditions.frames.body.inertial_rotations[:,1] = theta[:,0]
+		
+ +

We now add these functions to the segment process list.

+ +
    # --------------------------------------------------------------
+		#   Initialize - before iteration
+		# --------------------------------------------------------------
+		initialize = self.process.initialize
+		
+		initialize.expand_state            = Methods.expand_state
+		initialize.differentials           = Methods.Common.Numerics.initialize_differentials_dimensionless
+		initialize.conditions              = Methods.Climb.Constant_Throttle_Constant_Speed.initialize_conditions
+		initialize.velocities              = Methods.Climb.Constant_Throttle_Constant_Speed.update_velocity_vector_from_wind_angle
+		initialize.differentials_altitude  = Methods.Climb.Constant_Throttle_Constant_Speed.update_differentials_altitude      
+		
+ +

and

+ +
    # Unpack Unknowns
+		iterate.unknowns = Process()
+		iterate.unknowns.mission           = Methods.Climb.Constant_Throttle_Constant_Speed.unpack_body_angle 
+		
+		# Update Conditions
+		iterate.conditions = Process()
+		iterate.conditions.velocities      = Methods.Climb.Constant_Throttle_Constant_Speed.update_velocity_vector_from_wind_angle
+		iterate.conditions.differentials_a = Methods.Climb.Constant_Throttle_Constant_Speed.update_differentials_altitude
+		iterate.conditions.differentials_b = Methods.Common.Numerics.update_differentials_time
+		iterate.conditions.acceleration    = Methods.Common.Frames.update_acceleration
+		iterate.conditions.altitude        = Methods.Common.Aerodynamics.update_altitude
+		iterate.conditions.atmosphere      = Methods.Common.Aerodynamics.update_atmosphere
+		iterate.conditions.gravity         = Methods.Common.Weights.update_gravity
+		iterate.conditions.freestream      = Methods.Common.Aerodynamics.update_freestream
+		iterate.conditions.orientations    = Methods.Common.Frames.update_orientations
+		iterate.conditions.aerodynamics    = Methods.Common.Aerodynamics.update_aerodynamics
+		iterate.conditions.stability       = Methods.Common.Aerodynamics.update_stability
+		iterate.conditions.propulsion      = Methods.Common.Energy.update_thrust
+		iterate.conditions.weights         = Methods.Common.Weights.update_weights
+		iterate.conditions.forces          = Methods.Common.Frames.update_forces
+		iterate.conditions.planet_position = Methods.Common.Frames.update_planet_position
+		
+ +

If you have any questions that are not answered in other tutorials or the FAQ please ask on our forum page. This is also the place to go if you want help building a more elaborate evaluation, such as one that includes moments.

+ +
+
+
+
+
+ + + + + + + + + + + + + + \ No newline at end of file diff --git a/documentation/optimization.html b/documentation/optimization.html new file mode 100644 index 00000000..81e0c023 --- /dev/null +++ b/documentation/optimization.html @@ -0,0 +1,290 @@ + + + + + Optimization Code Structure + + + + + + + + + +
+ + + + + +
+
+
+ + + +
+

Optimization Code Structure

+ +

This is an overview of how optimization is done in SUAVE. A specific tutorial case is also available here.

+ +

Nexus Class

+ +

The Nexus class is the underlying data structure that is used for optimization. It is created to hold all data and functionality needed to link together optimizers and the various analysis modules in SUAVE. Detailed information on each of the functions can be found on our doxygen page.

+ +

Standard Optimization File Structure

+ +

These are the standard files that are used in the optimization process. They are typically stored as Optimize.py, Vehicle.py, Analysis.py, Mission.py, Procedure.py, and Plot_Mission.py. These names can be changed if desired.

+ +

Optimize

+ +

This is the top level file that is run to perform the optimization. Inputs, objective, constraints, and aliases are specified here. The inputs have an initial value, bounds, a scaling factor, and the units used. This provides later functions with the information needed to vary the parameters. Units.less indicates a unitless quantity. SI units are the default in SUAVE’s internal calculations, so Units.meter will not modify the internal value, while something like Units.foot will.

+ +
problem.inputs = np.array([
+[ 'wing_area'     ,  125.  , (   120.   ,   180.   )  ,   100.  , Units.meter**2],
+[ 'aspect_ratio'  ,  3.3   , (   2.0    ,   6.0    )  ,   10.   , Units.less],
+])
+
+ +

Constraints and the objective are similar. Both have scaling quantities and constraints also have bounds.

+ +
problem.constraints = np.array([
+[ 'design_range_fuel_margin', '>', 0., 1E-1, Units.less]
+])
+
+problem.objective = np.array([
+['fuel_burn_rate', 1., Units.kg/Units.s]
+])
+
+ +

Finally we have aliases. This provides the optimization process with the position of the various parameters in the data structure. Aliases are used so that short names can be used for variables and a single variable can control multiple items in the data structure. Controlling multiple items can be important if different vehicle configurations are used at different points in the mission, and one of the vehicle parameters should change in the same way for all of the configurations. We can use * as a wildcard. This is used below to change the aspect ratio of the main wing in every vehicle configuration.

+ +
problem.aliases = [
+[ 'wing_area'       ,   ['vehicle_configurations.base.wings.main_wing.areas.reference',
+					'vehicle_configurations.base.reference_area']],
+[ 'aspect_ratio'    ,    'vehicle_configurations.*.wings.main_wing.aspect_ratio'       ],
+[ 'fuel_burn_rate'  ,    'summary.fuel_burn_rate'                                      ],
+]    
+
+ +

This file then specifies the configurations, analyses, missions, and procedure that will be used. This are typically contained in separate files and more details on each are below. Once all of this is specified, the desired optimizer is called with the nexus class created by this setup.

+ +

Vehicle Setup

+ +

This contains the vehicle information such as geometric data and configurations. It is the same as the vehicle setup used for basic analysis purposes.

+ +

Analysis Setup

+ +

This contains information on what analyses should be run for the vehicle. For example if correlation-based aerodynamics or AVL should be used for computations. It requires vehicle information from the previous step.

+ +

Mission Setup

+ +

This is also the same as the standard mission setup. It determines how the mission will be flown. It requires analysis information from the previous step.

+ +

Procedure

+ +

This is an optimization specific file that determines how the vehicle, analysis, or mission is modified with the input values in the optimization and also runs the mission. For example, changing the wing area will usually require changes to other wing parameters, such as root chord length. This module reads the new inputs and changes other values accordingly based on user specified processes.

+ +

Plotting

+ +

This function is not necessary to the optimization, but is often included in the files used and is added to the optimize main call as a way to visualize the results.

+ +

Optimizer Interface

+ +

The other step that must be taken to perform an optimization is to convert the standardized input above into values that can be used by the selected optimizer. This is done through a separate script for each optimizer, all of which are found in the optimization folder.

+ +

For example, if we are using PyOpt to optimize, we might use output = pyopt_setup.Pyopt_Solve(problem,solver='SNOPT') in the main function of the top level optimizer. This function reads the inputs, constraints, and objective and converts them to a format that the selected optimizer (SNOPT here) can understand.

+ +

Evaluation Process

+ +

This shows the typical evaluation process, including where items like inputs and aliases are used. This chart assumes a single objective call, but some optimizers will include calls such as all_constraints which require another evaluation. If the evaluation is a duplicate, data from the previous evaluation will be used instead of stepping through the procedure again.

+ +

 

+ +

+ +

 

+ +

Incorporating Multi-fidelity

+ +

Multiple levels of fidelity are designed to be relatively easy to incorporate in SUAVE, but there are still a few things to keep in mind. First, the chosen optimizer must support multi-fidelity and be able to change the nexus.fidelity_level value. Once this is done, it is also important to remember that the mission is set up based on the analyses. This means that if a change is made to the analyses then the mission must be rebuilt with the new settings. As an example, code below for changing the analysis level is shown. This is a function that has been added to the procedure file.

+ +
def set_fidelity_level(nexus):
+
+if nexus.has_key('fidelity_level') == False:
+	print 'Fidelity level not set, defaulting to 1'
+	nexus.fidelity_level = 1
+
+if nexus.fidelity_level == 2:
+	aerodynamics = SUAVE.Analyses.Aerodynamics.Supersonic_OpenVSP_Wave_Drag()
+	aerodynamics.settings.number_slices    = 20
+	aerodynamics.settings.number_rotations = 10        
+elif nexus.fidelity_level == 1:
+	aerodynamics = SUAVE.Analyses.Aerodynamics.Supersonic_Zero()
+else:
+	raise ValueError('Selected fidelity level not supported')
+aerodynamics.geometry = copy.deepcopy(nexus.vehicle_configurations.base)
+nexus.analyses.base.append(aerodynamics)
+
+nexus.missions = mission_as2.setup(nexus.analyses)
+
+return nexus
+
+ +

Here we see that nexus.missions has been updated in addition to nexus.analyses, since failing to do this would have the mission run with the previous analysis settings.

+ +

Key Functions in the Optimizer Setup

+ +

We briefly mentioned how optimization parameters would need to be converted so that they could run with a particular optimizer. Here we show how this is managed and show which functions are likely to be useful in building a new optimizer setup.

+ +

The key items that will be needed for most optimizers are shown below, taken from the PyOpt setup:

+ +
inp = problem.optimization_problem.inputs
+obj = problem.optimization_problem.objective
+con = problem.optimization_problem.constraints  
+
+# Set inputs
+nam = inp[:,0] # Names
+ini = inp[:,1] # Initials
+bnd = inp[:,2] # Bounds
+scl = inp[:,3] # Scale
+typ = inp[:,4] # Type
+
+ +

These can be scaled with two helper functions that are part of the SUAVE distribution:

+ +
from SUAVE.Optimization import helper_functions as help_fun
+
+bnd_constraints    = help_fun.scale_const_bnds(con)
+scaled_constraints = help_fun.scale_const_values(con,bnd_constraints)
+x                  = ini/scl
+
+ +

What happens next is entirely dependent on what optimizer you want to use. Some may require that constraint bounds happen at 0 or are either > or <. However this setup is done, you will likely need to create a function that can accept the problem and inputs and give required outputs such as the objective value and constraints. In the PyOpt case, this is done with a simple wrapper and an added function:

+ +
mywrap = lambda x:PyOpt_Problem(problem,x)
+
+ +

+ +
def PyOpt_Problem(problem,x):
+
+	obj   = problem.objective(x)
+	const = problem.all_constraints(x).tolist()
+	fail  = np.array(np.isnan(obj.tolist()) or np.isnan(np.array(const).any())).astype(int)
+
+
+	print 'Inputs'
+	print x
+	print 'Obj'
+	print obj
+	print 'Con'
+	print const
+
+	return obj,const,fail
+
+ +

Please visit our forum if you have any other questions on how the optimizer interface works or how to convert the values to what you need.

+ +
+
+
+
+
+ + + + + + + + + + + + + + \ No newline at end of file diff --git a/documentation/using_docs.html b/documentation/using_docs.html new file mode 100644 index 00000000..453c4982 --- /dev/null +++ b/documentation/using_docs.html @@ -0,0 +1,243 @@ + + + + + Using the Documentation + + + + + + + + + +
+ + + + + +
+
+
+ + +
+

How to Read (and Write) the Documentation

+ +

This is an explanation of how documentation is built in SUAVE so that the user can know what to look for and how to write it if they wish to add their own code. The doxygen page is available here.

+ +

Docstrings

+ +

All classes and functions in SUAVE have docstrings have docstrings. These give the user an understanding of what the function does and information on the input and output variables.

+ +

Classes

+ +

For a class, the docstring has three parts:

+ +
    +
  • General description
  • +
  • Assumptions
  • +
  • Source
  • +
+ +

The general description provides a brief summary of what the class is used for. Assumptions list any significant assumptions are important in how it is used. This may be listed as None or N/A if there are no important assumptions. The source section should provide the general source of methods in the class. If there is no overall source, a message like ‘see sources in functions’ may be appropriate. There are also cases where a source is not relevant, such as simple geometric functions, and may also be listed as None or N/A.

+ +

Class Docstring Template

+ +

This is the general template that can be used when creating a new class. It should be placed directly under the class declaration.

+ +
"""<Description>
+			
+			Assumptions:
+			<any assumptions>
+			
+			Source:
+			<source>
+			"""
+			
+ +

Functions

+ +

For functions there are six categories:

+ +
    +
  • Description
  • +
+ +

This is a general description of what the function does. It should also include any key information that does not fit into one of the other categories.

+ +
    +
  • Assumptions
  • +
+ +

This should contain any assumptions made by the function. None or N/A can be used if none are used.

+ +
    +
  • Source
  • +
+ +

The source of any methods that have been implemented. Simple methods like basic geometric relations do not need a source.

+ +
    +
  • Inputs
  • +
+ +

This should contain any variables or functions passed to the function. If the passed variable is a data structure, the components that are used should be listed. Each item should include a description if it is not obvious from the name. It should also include any relevant units. In addition, information about the variable type or any other information that might be important can be added here.

+ +
    +
  • Outputs
  • +
+ +

This should contain the same information as in the inputs. It may also contain information on variables that are modified but not explicitly returned.

+ +
    +
  • Properties Used
  • +
+ +

This carries the same information as input and outputs. It typically contains variables that are properties of the parent class but are not modified. There is some overlap with inputs and outputs, but either category is acceptable as long as the variable is documented.

+ +

Function Docstring Template

+ +

This is a template docstring:

+ +
    """<Description>
+			
+			Assumptions:
+			<any assumptions>
+			
+			Source:
+			<source>
+			
+			Inputs:
+			<input1> <units>
+			<input2> <units>
+			..
+			
+			Outputs:
+			<output1> <units>
+			<output2> <units>
+			..
+			
+			Properties Used:
+			<property1> <units>
+			<property2> <units>
+			..
+			"""   
+			
+ +

Doxygen Grouping Tags

+ +

Tags are used to put files into groups that match the SUAVE file structure. @defgroup tags define a group and should be placed in the init file. An example is shown here:

+ +
## @defgroup Analyses-Aerodynamics Aerodynamics
+			# These are the analyses that control aerodynamic evaluations.
+			# @ingroup Analyses
+			
+ +

In this example, Analyses-Aerodynamics is the doxygen tag for the group, while the group appears in the documentation as Aerodynamics, the next part of the string. The tag is based on the file structure (Analyses/Aerodynamics here). Since this is a subgroup of Analyses, @ingroup Analyses is used here, with Analyses as the doxygen tag for the next level up.

+ +

In files, the @ingroup tag should be inserted before all classes and stand-alone functions. The tag should match the tag in the folder init file’s @defgroup string.

+ +
+
+
+
+
+ + + + + + + + + + + + + + \ No newline at end of file diff --git a/download.html b/download.html new file mode 100644 index 00000000..357cec92 --- /dev/null +++ b/download.html @@ -0,0 +1,157 @@ + + + + + Tutorials + + + + + + + + + + +
+ + + + +
+
+
+
+ +
+
+
+ + + +
+
+

Download

+

Jump in and design! Here are some helpful steps for downloading and installing the code. There are stable releases and beta releases. SUAVE is released with the permissive LGPL 2.1 license.

+
+ +

Which Install Option Should I Use?

+

If you're interesed in using existing SUAVE code to model vehicles, use the standard install.

+ +

If you're interesed in extending and customizing SUAVE code, use the develop install.

+ + +
+ +
+
+
+
+
+ + + + + + + + + + + + + + diff --git a/download.md b/download.md deleted file mode 100644 index 5626e75a..00000000 --- a/download.md +++ /dev/null @@ -1,154 +0,0 @@ ---- -layout: page -title: Download -subtitle: How to download and install this fantastic tool -permalink: /download/ ---- - - - -Jump in and design! Here are some helpful steps for downloading and installing the code. There are stable releases and beta releases. Also make sure to check out the license under which the code is available. - -
- -## Downloading - -SUAVE comes released as a set of project folders ready for learning and exploration. - -Please take a few seconds to register with us by filling out the form on the pages linked below. Upon registration, you'll be redirected to the appropriate distribution of the software. The information we collect is used _only_ for usage statistics by the development team. You'll only be contacted for notification of critical bug fixes and major releases. To get more involved in growing the community, definitely check out the [forum](/forum). Your support is greatly appreciated, it let's us build a better tool for everyone! - -### Stable Release -Download the latest stable release of SUAVE:
-[SUAVE Version 1.0.0](/register/) - -### License - -We want SUAVE to grow with the community, so it's available under a
[LGPL 2.1 License](https://www.gnu.org/licenses/old-licenses/lgpl-2.1.en.html). - -Please if you are interested in re-publishing SUAVE source code as part of a commercial software. - -### Tutorials - -We also update our tutorials repository with every release to show new users some of the capabilities and how to use the code. The tutorial files can be found [here](https://github.com/suavecode/Tutorials). If you would like to use these, you may either follow the Github download instructions on the [develop](/develop) page, but using `https://github.com/suavecode/Tutorials.git`, or you can download the files as a .zip using the "clone or download" button on the [Tutorials Github page](https://github.com/suavecode/Tutorials). - -
- -## Installation - -SUAVE is developed primarily on Python 2.7. It's known to work on versions 2.4 through 2.7. Let us know if you find that it works on additonal versions. - -We strongly recommend using a scientific python distribution like [Anaconda](http://continuum.io/downloads) or [Enthought-Canopy](https://store.enthought.com/downloads). All the package dependencies like scipy and numpy will come pre-packaged and stuff will just work. - -If you don't have access to a scientific python distribution, you can install the dependent packages separately. Check out the specific [dependencies](#dependencies) for more information - -### Simple Setup - -Once you've downloaded the code and prepared the software requrements, you're ready to install it into python! - -1. Download and extract the release archive -2. Open the directory SUAVE/trunk -3. Open a command prompt in that directory -4. Run this command: ```python setup.py install```
- If you are on a linux or mac, you may need to run
```sudo python setup.py install``` -5. Change to any other folder, open a python shell, and test the new module with the command `import SUAVE` - -If all goes well, you are now able to import SUAVE into your python projects. If you've downloaded the tutorials as well, check out the [guides](/guides) for examples on using thems! - -After trying out the guides you may find you want to make changes to the innards of the package to fit your problem, take a look at the [develop](/develop) notes for how to set this up. - -Have fun! - -If you had trouble installing or need to uninstall, there are some more tips ahead. - -
- -### Dependencies - -Below are the packages that SUAVE expects in order to run the tutorial cases. There are links to guides on using package managers for linux and mac, and python installers for windows. If these fail, check out the source forge links for additional installers or source code. - -|package | link | -|------------|-------| -| numpy | [linux](http://www.scipy.org/install.html#linux-packages), [mac](http://www.scipy.org/install.html#mac-packages), [windows](http://www.lfd.uci.edu/~gohlke/pythonlibs/#numpy), [source](http://sourceforge.net/projects/numpy/files/NumPy) | -| scipy | [linux](http://www.scipy.org/install.html#linux-packages), [mac](http://www.scipy.org/install.html#mac-packages), [windows](http://www.lfd.uci.edu/~gohlke/pythonlibs/#scipy), [source](http://sourceforge.net/projects/scipy/files/scipy) | -| matplotlib | [linux](http://www.scipy.org/install.html#linux-packages), [mac](http://www.scipy.org/install.html#mac-packages), [windows](http://www.lfd.uci.edu/~gohlke/pythonlibs/#matplotlib), [source](http://sourceforge.net/projects/matplotlib/files/matplotlib) | -| pip | [linux](https://pip.pypa.io/en/stable/installing.html#install-pip), [mac](https://pip.pypa.io/en/stable/installing.html#install-pip), [windows](https://pip.pypa.io/en/stable/installing.html#install-pip) | -| scikit-learn | [linux](http://scikit-learn.org/stable/install.html), [mac](http://scikit-learn.org/stable/install.html), [windows](http://scikit-learn.org/stable/install.html) | - -
-**Note**: For the windows installers, you can pick the latest version, for "cp2.7" (C-Python 2.7), for your architecture (32 or 64bit), and for numpy pick the MKL version (it's faster).
-**Note**: The pip installer above will also install setuptools, a sub-dependency. - - -### Dealing with Write Access - -You shouldn't need this part of the guide, unless you are unable to write-access the python site-packages directory. In that case, you can try these approaches to install SUAVE. - -#### A. Install to local site-packages - -This involves the user install option
-``` python setup.py install --user ``` - - -#### B. Start a local site-packages folder - -This involves creating a local directory, and setting up your PYTHONPATH environment variable. - -1. Create a local directory. - For example:
- ```~/python-site-packages``` or
- ```C:/Users/your-user-name/python-site-packages``` -2. Append this path to PYTHONPATH - - For Unix operating systems - - Append this line to your ~/.bashrc file
- ```export PYTHONPATH = $PYTHONPATH:~/python-site-packages``` - - And source the bashrc file
- ```$ source ~/.bashrc``` - - - For MacOS operating systems - - Append this line to your ~/.bash_profile file
- ```export PYTHONPATH = $PYTHONPATH:~/python-site-packages``` - - And source the bashrc file
- ```$ source ~/.bash_profile``` - - - For Windows operating systems - - Open the start menu and type "environ", this opens the environment variable editor - - Create or edit the PYTHONPATH "User" environment variable, appending the full path to your custom site-package directory, separating multiple paths with semicolons. For example:
- ```%PYTHONPATH%;C:/Users/your-user-name/python-site-packages``` - - After this you'll need to open a new command line window
-3. Now Install SUAVE
- Using the example of the custom directoy ~/python-site-packages:
- ``` python setup.py install --prefix=~/python-site-packages``` - -### Additional Install Options - -Additional setup options, such as overriding the default install location, can be found with the following commands:
-`python setup.py install --help`
-`python setup.py uninstall --help`
-`python setup.py develop --help`
-`python setup.py --help` - -
- -## Un-Installation - -SUAVE requires pip to uninstall. An alternate approach is provided further below if pip is not available. - -#### Un-Installation with pip: - -1. Navigate to the SUAVE/trunk directory by command line. -2. Run the uninstall command. (On unix platforms, these commands may require a sudo ('super-user-do') call.)
- ```python setup.py uninstall``` - -#### Alternate Approach: - Use this if you don't have the pip package. - -1. Find your site-packages folder. - Your site-packages folder is typically located in your python's install directory, unless you manually created it. You can find it by using the following commands.
- `$ python `
- `>>> import site`
- `>>> site.getsitepackages()` - -2. Manually delete any file including the name "SUAVE". - You may also check the file "easy_install.pth", if it exists, for references to the SUAVE package, and delete them. Never said this would be pretty... However it is a typical uninstall process for python packages. - - diff --git a/download/develop_install.html b/download/develop_install.html new file mode 100644 index 00000000..1bfd1859 --- /dev/null +++ b/download/develop_install.html @@ -0,0 +1,346 @@ + + + + + Develop Install + + + + + + + + + +
+ + + + +
+
+
+
+ +
+
+
+ + + +
+
+ +
+
+

Develop

+
+
+ +
+

If you want to make changes to SUAVE source, or contribute new functionalities back to the community, this is the page for you!

+ +

Background

+ +

SUAVE is developed via GitHub, and this page will describe how to get started. There is also a list of open topics available for contribution if you’re looking for ideas to get started.

+ +

As a developer, you’ll want to fork SUAVE to your personal account. This creates a copy of the whole SUAVE repository, including all past versions, inside your GitHub account. Generally you’ll want to start from the develop branch, but you can check with the developers if you think it would be more appropriate to work on a feature branch.

+ +

Development is done on separate branches. Our branching model is very similar to this one. Basically there are three types of branches.

+ +
    +
  • master – stable, latest release and fixes
  • +
  • develop – current development, generally the branch for you to start with
  • +
  • feature-* – feature specific branches, using names with underscores, check with the developer email list if you think this a better place to contribute
  • +
+ +

SUAVE merges new code contributions through pull requests. As you make changes to your copy of SUAVE, you’ll upload them to your GitHub fork, and then when they’re ready for review you’ll submit them for merge via pull request.

+ +

Style Guide

+ +

SUAVE is built on a slightly modified PEP8 style guide, with changes made to implement a data-oriented view of the code. To help support discovering code, the SUAVE folder structure explicitly mirrors the package structure. Flexibility of the package structure is important, so in general all objects live in their own file, with the same file name as the object name. In order to maintain a separation between Analysis and Data structures, there are often parallel package trees inside the main branches of the package, like SUAVE.Methods.Aerodynamics and SUAVE.Analysis.Aerodynamics. Where possible the names of fields that live in the SUAVE package are written out verbosely, avoiding jargon built on mathematical variable names or acronyms.

+ +

A full description of the style of SUAVE can be found on the Guides page.

+ +

Templates for new methods and objects can be found in the SUAVE repo’s templates folder.

+ +

Prerequisites

+ +

In addition to the package dependencies listed on the download page, you will need to install git.

+ +

Git-Client

+ +

Git is an advanced distributed version control system. It is the core of the majority of current open source projects. Here are some instructions for installing git on your machine.
+ linux , mac , windows , more info

+ +

There are several GUI’s available to help manage the repository. On Windows TortoiseGit is a useful one.

+ +

If you’re going to install TortoiseGit on windows, when installing the git client (MsysGit), uncheck “Windows Explorer Integration”. And when installing TortoiseGit, select “Checkout as-is, Unix-style line endings”

+ +

Once you’ve installed git, there a few post-install commands to run, documented here.

+ +

GitHub Account

+ +

GitHub is a hosting service for git projects. SUAVE’s repository is located here.

+ +

If you don’t have a github account already, go ahead and sign up!

+ +

Then, go to the SUAVE github repo at github.com/suavecode/SUAVE and check out the code! If you wouldn’t mind, tick the “Watch” and “Star” buttons at the top-right of the page, if you think this is a useful repo.

+ +


+ +

Developer Installation

+ +

Time to pull code. If you had previously installed a release distribution according to the download page, you’ll want to uninstall the existing package first.

+ +
    +
  1. Go to the SUAVE github repo.
  2. +
  3. To get your own copy of the source, with links into real-time updates, you need to fork the repo. This button is on the top-right of the page too.
  4. +
  5. This will copy the repo and take you to your fork, notice that your web-browser’s URL has changed to include your username.
  6. +
  7. Now you can clone your fork to your computer. Find the clone url of your fork on the right hand side of the page and copy it. You can use the https url.
    clone
  8. +
  9. Open a command prompt, in a directory that you want to start the repository (for example in the SUAVE_Project folder), and run the git clone command
    git clone <git url>
    Now you should have the source code.
  10. +
  11. Change directory into the trunk folder and run a developer installation command.
    python3 setup.py develop
    Now you have a developer version of SUAVE installed! You can make changes to the source in this directory and the changes will appear the next time you run python, without having to rebuild or reinstall.
  12. +
  13. Test the installation by changing to any other directory, then start a python shell, and run the command
    >>> import SUAVE
    >>> print(SUAVE.__file__)
    This should print the file path to the SUAVE package init.py file in your trunk directory.
  14. +
+ +

Some Notes

+ +
    +
  • You may need to run a sudo (super user do) command to install SUAVE when working on linux or mac systems: sudo python3 setup.py develop
  • +
  • The same strategies for dealing with write access can be used here, by simply replacing any install keywords with develop
  • +
  • To uninstall the developer version, run the command python3 setup.py develop --uninstall
  • +
+ +


+ +

Managing your repository

+ +

As you make changes to your code, you’ll want to add and commit them to your clone, and push them to your fork. You’ll fetch changes from the upstream remote (the suavecode repository), and merge them into your clone. To send your changes back to the upstream repository, you can submit a pull-request.

+ +

Setting the upstream

+ +

Below is a summary of setting the upstream remote. There are a good references for this process here and here, and more via a google search for “git update fork”.

+ +
    +
  1. Inspect your current “remote”, this is the url of the repository to which your clone listens. + In the directory for the cloned repo, type
    git remote –v and it should show the “origin” directory for “fetch” and “push”. These are the remote urls for your own fork.
  2. +
  3. Add an upstream remote to the main suavecode/SUAVE repository using
    git remote add upstream https://github.com/suavecode/SUAVE.git
  4. +
  5. Run git remote -v again to see the new remotes.
  6. +
  7. Finally, download the code for the upstream remote with
    git fetch upstream.
  8. +
+ +

Changing branches

+ +

You should work on the develop branch in general, it will have the most updated changes from the community.

+ +
    +
  1. Inspect your branches with git branch -a. You’ll see all the branches, for both upstream and origin. Generally you should only work off the origin branches
  2. +
  3. Start a new branch with git branch develop origin/develop. This comand aliases the branch “origin/develop” with the name “develop”.
  4. +
  5. Checkout the branch, git checkout develop.
  6. +
  7. You can see your current branch with, git branch, the one you have checked out will have a star next to it.
  8. +
  9. Commit all your changes to the current branch before checking out another branch, otherwise the changes will be lost.
  10. +
  11. To dump any changes that you don’t want, git stash, will be helpful.
  12. +
+ +

Store changes to your GitHub fork

+ +
    +
  1. Edit the code as you need on your machine
  2. +
  3. Inspect git’s view of the changes you’ve made with git status. This shows what files are new, changed and not yet part of the repo’s history.
  4. +
  5. Add the changed files to your commit with git add <path to file>, or to add all the changes with git add -a (be careful with this one). The add command does not make the changes part of your repo’s history! You can do multiple add commands for example.
  6. +
  7. Commit them to the history on your machine with
    git commit -m 'your message for the commit'
    Make sure to include a nice description. This command only affects your local repository! You can do multiple commits before sending them to the cloud.
  8. +
  9. Push the new commits to GitHub with git push origin. This will send all the commits to your fork on GitHub. This serves as a backup copy for you, and is needed to share the changes with the upstream suavecode repository via pull-requests.
  10. +
+ +

Get new changes from upstream

+ +

In this example the upstream/develop branch is merged into the fork/develop branch.

+ +
    +
  1. Checkout your local develp branch with
    git checkout develop.
  2. +
  3. Fetch updates from the upstream repository with
    git fetch upstream.
  4. +
  5. Merge the changes from the upstream into your fork with
    git merge upstream/develop.
  6. +
  7. Push these changes to your fork on GitHub,
    git push origin master.
  8. +
+ +

Share your changes with upstream

+ +

This creates a nice documentation of the changes that were made. More detail on pull requests can be found here.

+ +
    +
  1. Commit and push all your changes to your fork on GitHub.
  2. +
  3. Open a browser and navigate to your branch on the GitHub website.
  4. +
  5. Click the “Compare and Review” button.
  6. +
  7. Review the changes for any unexpected differences.
  8. +
  9. Click the “Create Pull Request” button.
  10. +
  11. The devs will take a look and merge the request.
  12. +
+ +


+ +

Background on Git

+ +

Git is an open source program for tracking changes in text files. It was written by the author of the Linux operating system, and is the core technology that GitHub, the social and user interface, is built on top of it.

+ +

The term version control is used in Git and other such programs, and refers exactly to what it reads. It allows a group of software developers (the group may comprise one, many or “more than many”) to keep track of changes being made to the software’s code (i.e., versions of code) and have control on the changes (“versions”). This control helps the programmer(s) to decide

+ +
    +
  • Which versions should remain
  • +
  • Which versions need higher priority to fix any bugs or problems
  • +
  • Which versions are ready to be shipped out to customers (“ready for primetime”)
  • +
  • Which versions can be put on the sidelines since they are a brainchild of a super whiz programmer who is simply playing with some cool ideas
  • +
  • Which versions are now obsolete since there are alternate and better software/code available to do the same job (these versions are usually nixed!)
  • +
  • Which versions are too new and require a lot of related work to be done before they can even be brought up for discussions at the weekly meetings
  • +
  • And so on
  • +
+ +

Bottom line is that the concept of version control is mainly to help software development by not losing one’s grip on reality and the primary objectives of the software being developed!

+ +

For those interested in learning more about how version control systems (VCSs) such as Git work, refer to

+ + + +

In addition to Git, there are other popular VCSs such as SVN (http://tortoisesvn.net/ and https://subversion.apache.org/), with their own sets of pros and cons. However, Git was chosen for SUAVE because SUAVE developers felt it can be easily implemented on Linux, Mac and Windows, and offers them a lot of flexibility and control in terms of developing and maintaining multiple parallel versions (“branches”) with each providing further parallelization (“forks”). For more information about the concepts of branching and forking, refer to http://nvie.com/posts/a-successful-git-branching-model/

+ +


+ +

Areas of Development

+ +

Short Term Feature Development

+ +

These are the areas that are under development or suggested for development are available in our Github projects tab. There are two active projects that include feature development. One is the list of items we plan to accomplish for our next release. The other is a general feature development project, which contains features that we would like to have but are not currently priorities for the next release.

+ +

Post to the forum if you’re intersted in working on any of these, or to suggest a new module!

+ +

Long Term Development Goals

+ +

Looking farther into the future, we have some key items envisioned for the next major release of SUAVE. So far these are:

+ +
    +
  • Integration with a standardized parameter storage interface such as CPACS
  • +
+ +

We’re always happy to hear feedback on what our users think is important in this kind of tool, so if you have another idea go ahead and ask about it on our forum.

+ +

Back to Top!

+
+ + +
+ +
+
+
+
+
+ + + + + + + + + + + + + + diff --git a/download/standard_install.html b/download/standard_install.html new file mode 100644 index 00000000..5c185177 --- /dev/null +++ b/download/standard_install.html @@ -0,0 +1,335 @@ + + + + + Simple Install + + + + + + + + + +
+ + + + +
+
+
+
+ +
+
+
+ + + +
+
+ + +

Downloading

+ +

SUAVE comes released as a set of project folders ready for learning and exploration.

+ +

Please take a few seconds to register with us by filling out the form on the pages linked below. Upon registration, you’ll be redirected to the appropriate distribution of the software. The information we collect is used only for usage statistics by the development team. You’ll only be contacted for notification of critical bug fixes and major releases. To get more involved in growing the community, definitely check out the forum. Your support is greatly appreciated, it let’s us build a better tool for everyone!

+ +

Stable Release

+

Download the latest stable release of SUAVE:
+ SUAVE Version 2.5.0

+ +

License

+ +

We want SUAVE to grow with the community, so it’s available under a
LGPL 2.1 License.

+ +

Please contact us if you are interested in re-publishing SUAVE source code as part of a commercial software.

+ +

Tutorials

+ +

We also update our tutorials repository with every release to show new users some of the capabilities and how to use the code. The tutorial files can be found here. If you would like to use these, you may either follow the Github download instructions on the develop page, but using https://github.com/suavecode/Tutorials.git, or you can download the files as a .zip using the “clone or download” button on the Tutorials Github page.

+ +


+ +

Installation

+ +

SUAVE is developed primarily on Python 3. It’s known to work on versions 3.6 and above . Let us know if you find that it works on additonal versions.

+ +

We strongly recommend using a scientific python distribution like Anaconda or Enthought-Canopy. All the package dependencies like scipy and numpy will come pre-packaged and stuff will just work.

+ +

If you don’t have access to a scientific python distribution, you can install the dependent packages separately. Check out the specific dependencies for more information

+ +

Simple Setup

+ +

Once you’ve downloaded the code and prepared the software requrements, you’re ready to install it into python!

+ +
    +
  1. Download and extract the release archive
  2. +
  3. Open the directory SUAVE/trunk
  4. +
  5. Open a command prompt in that directory
  6. +
  7. Run this command: python3 setup.py install
    + If you are on a linux or mac, you may need to run
    sudo python3 setup.py install
  8. +
  9. Change to any other folder, open a python shell, and test the new module with the command import SUAVE
  10. +
+ +

If all goes well, you are now able to import SUAVE into your python projects. If you’ve downloaded the tutorials as well, check out the guides for examples on using thems!

+ +

After trying out the guides you may find you want to make changes to the innards of the package to fit your problem, take a look at the develop notes for how to set this up.

+ +

Have fun!

+ +

If you had trouble installing or need to uninstall, there are some more tips ahead.

+ +


+ +

Dependencies

+ +

Below are the packages that SUAVE expects in order to run the tutorial cases. There are links to guides on using package managers for linux and mac, and python installers for windows. If these fail, check out the source forge links for additional installers or source code.

+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
packagelink
numpylinux, mac, windows, source
scipylinux, mac, windows, source
matplotliblinux, mac, windows, source
piplinux, mac, windows
scikit-learnlinux, mac, windows
plotlylinux, mac, windows
+ +


+ Note: For the windows installers, you can pick the latest version, for Python 3.6, for your architecture (32 or 64bit), and for numpy pick the MKL version (it’s faster).
+ Note: The pip installer above will also install setuptools, a sub-dependency.

+ +

Dealing with Write Access

+ +

You shouldn’t need this part of the guide, unless you are unable to write-access the python site-packages directory. In that case, you can try these approaches to install SUAVE.

+ +

A. Install to local site-packages

+ +

This involves the user install option
+ python3 setup.py install --user

+ +

B. Start a local site-packages folder

+ +

This involves creating a local directory, and setting up your PYTHONPATH environment variable.

+ +
    +
  1. Create a local directory.
    + For example:
    + ~/python-site-packages or
    + C:/Users/your-user-name/python-site-packages
  2. +
  3. Append this path to PYTHONPATH +
      +
    • For Unix operating systems +
        +
      • Append this line to your ~/.bashrc file
        + export PYTHONPATH = $PYTHONPATH:~/python-site-packages
      • +
      • And source the bashrc file
        + $ source ~/.bashrc
      • +
      +
    • +
    • For MacOS operating systems +
        +
      • Append this line to your ~/.bash_profile file
        + export PYTHONPATH = $PYTHONPATH:~/python-site-packages
      • +
      • And source the bashrc file
        + $ source ~/.bash_profile
      • +
      +
    • +
    • For Windows operating systems +
        +
      • Open the start menu and type “environ”, this opens the environment variable editor
      • +
      • Create or edit the PYTHONPATH “User” environment variable, appending the full path to your custom site-package directory, separating multiple paths with semicolons. For example:
        + %PYTHONPATH%;C:/Users/your-user-name/python-site-packages
      • +
      • After this you’ll need to open a new command line window
      • +
      +
    • +
    +
  4. +
  5. Now Install SUAVE
    + Using the example of the custom directoy ~/python-site-packages:
    + python3 setup.py install --prefix=~/python-site-packages
  6. +
+ +

Additional Install Options

+ +

Additional setup options, such as overriding the default install location, can be found with the following commands:
+ python3 setup.py install --help
+ python3 setup.py uninstall --help
+ python3 setup.py develop --help
+ python3 setup.py --help

+ +


+ +

Un-Installation

+ +

SUAVE requires pip to uninstall. An alternate approach is provided further below if pip is not available.

+ +

Un-Installation with pip:

+ +
    +
  1. Navigate to the SUAVE/trunk directory by command line.
  2. +
  3. Run the uninstall command. (On unix platforms, these commands may require a sudo (‘super-user-do’) call.)
    + python3 setup.py uninstall
  4. +
+ +

Alternate Approach:

+

Use this if you don’t have the pip package.

+ +
    +
  1. +

    Find your site-packages folder. + Your site-packages folder is typically located in your python’s install directory, unless you manually created it. You can find it by using the following commands.
    + $ python3
    + >>> import site
    + >>> site.getsitepackages()

    +
  2. +
  3. +

    Manually delete any file including the name “SUAVE”.
    + You may also check the file “easy_install.pth”, if it exists, for references to the SUAVE package, and delete them. Never said this would be pretty… However it is a typical uninstall process for python packages.

    +
  4. +
+ +
+ +
+
+
+
+
+ + + + + + + + + + + + + + \ No newline at end of file diff --git a/doxygen/.DS_Store b/doxygen/.DS_Store new file mode 100644 index 00000000..1bdd58f9 Binary files /dev/null and b/doxygen/.DS_Store differ diff --git a/doxygen/annotated.html b/doxygen/annotated.html index 59cb7900..bb01cd33 100644 --- a/doxygen/annotated.html +++ b/doxygen/annotated.html @@ -1,9 +1,9 @@ - + - + SUAVE: Class List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@
- +
@@ -73,7 +78,9 @@
@@ -116,22 +123,20 @@  CMarkup  NProcess_Geometry  CProcess_Geometry - NResults - CResults - NSU2_Euler - CSU2_Euler - NSU2_Euler_Super - CSU2_Euler_Super - NSU2_inviscid - CSU2_inviscid - NSU2_inviscid_Super - CSU2_inviscid_Super - NSupersonic_OpenVSP_Wave_Drag - CSupersonic_OpenVSP_Wave_Drag - NSupersonic_Zero - CSupersonic_Zero - NVortex_Lattice - CVortex_Lattice + NSU2_Euler + CSU2_Euler + NSU2_Euler_Super + CSU2_Euler_Super + NSU2_inviscid + CSU2_inviscid + NSU2_inviscid_Super + CSU2_inviscid_Super + NSupersonic_OpenVSP_Wave_Drag + CSupersonic_OpenVSP_Wave_Drag + NSupersonic_Zero + CSupersonic_Zero + NVortex_Lattice + CVortex_Lattice  NAnalysis  CAnalysis  CContainer @@ -148,383 +153,491 @@  NEnergy  NEnergy  CEnergy - NGeometry - NGeometry - CGeometry - NLoads - NLoads - CLoads - NMission - NAll_At_Once - CAll_At_Once - NMission - CContainer - CMission - NSegments - NAerodynamic - CAerodynamic - NClimb - NConstant_Dynamic_Pressure_Constant_Angle - CConstant_Dynamic_Pressure_Constant_Angle - NConstant_Dynamic_Pressure_Constant_Rate - CConstant_Dynamic_Pressure_Constant_Rate - NConstant_EAS_Constant_Rate - CConstant_EAS_Constant_Rate - NConstant_Mach_Constant_Angle - CConstant_Mach_Constant_Angle - NConstant_Mach_Constant_Rate - CConstant_Mach_Constant_Rate - NConstant_Mach_Linear_Altitude - CConstant_Mach_Linear_Altitude - NConstant_Speed_Constant_Angle - CConstant_Speed_Constant_Angle - NConstant_Speed_Constant_Angle_Noise - CConstant_Speed_Constant_Angle_Noise - NConstant_Speed_Constant_Rate - CConstant_Speed_Constant_Rate - NConstant_Speed_Linear_Altitude - CConstant_Speed_Linear_Altitude - NConstant_Throttle_Constant_Speed - CConstant_Throttle_Constant_Speed - NLinear_Mach_Constant_Rate - CLinear_Mach_Constant_Rate - NLinear_Speed_Constant_Rate - CLinear_Speed_Constant_Rate - NOptimized - COptimized - NUnknown_Throttle - CUnknown_Throttle - NConditions - NAerodynamics - CAerodynamics - NBasic - CBasic - NConditions - CConditions - NNumerics - CNumerics - NResiduals - CResiduals - NState - CContainer - CState - NUnknowns - CUnknowns - NCruise - NConstant_Acceleration_Constant_Altitude - CConstant_Acceleration_Constant_Altitude - NConstant_Dynamic_Pressure_Constant_Altitude - CConstant_Dynamic_Pressure_Constant_Altitude - NConstant_Dynamic_Pressure_Constant_Altitude_Loiter - CConstant_Dynamic_Pressure_Constant_Altitude_Loiter - NConstant_Mach_Constant_Altitude - CConstant_Mach_Constant_Altitude - NConstant_Mach_Constant_Altitude_Loiter - CConstant_Mach_Constant_Altitude_Loiter - NConstant_Pitch_Rate_Constant_Altitude - CConstant_Pitch_Rate_Constant_Altitude - NConstant_Speed_Constant_Altitude - CConstant_Speed_Constant_Altitude - NConstant_Speed_Constant_Altitude_Loiter - CConstant_Speed_Constant_Altitude_Loiter - NConstant_Throttle_Constant_Altitude - CConstant_Throttle_Constant_Altitude - NDescent - NConstant_EAS_Constant_Rate - CConstant_EAS_Constant_Rate - NConstant_Speed_Constant_Angle - CConstant_Speed_Constant_Angle - NConstant_Speed_Constant_Angle_Noise - CConstant_Speed_Constant_Angle_Noise - NConstant_Speed_Constant_Rate - CConstant_Speed_Constant_Rate - NLinear_Mach_Constant_Rate - CLinear_Mach_Constant_Rate - NUnknown_Throttle - CUnknown_Throttle - NGround - NGround - CGround - NLanding - CLanding - NTakeoff - CTakeoff - NHover - NClimb - CClimb - NDescent - CDescent - NHover - CHover - NSegment - CContainer - CSegment - NSimple - CSimple - NSingle_Point - NSet_Speed_Set_Altitude - CSet_Speed_Set_Altitude - NSet_Speed_Set_Throttle - CSet_Speed_Set_Throttle - NSequential_Segments - CSequential_Segments - NVary_Cruise - NGiven_Weight - CGiven_Weight - NNoise - NFidelity_One - CFidelity_One - NNoise - CNoise - NPlanets - NPlanet - CPlanet - NProcess - CProcess - NSettings - CSettings - NSizing - NSizing - CSizing - NStability - NAVL - CAVL - NFidelity_Zero - CFidelity_Zero - NStability - CStability - NStructures - NStructures - CStructures - NSurrogate - CSurrogate - NVehicle - CVehicle - NWeights - NWeights - CWeights - NWeights_BWB - CWeights_BWB - NWeights_Tube_Wing - CWeights_Tube_Wing - NWeights_UAV - CWeights_UAV - NAttributes - NAirports - NAirport - CAirport - NRunway - CRunway - NAtmospheres - NAtmosphere - CAtmosphere - NEarth - NConstant_Temperature - CConstant_Temperature - NUS_Standard_1976 - CUS_Standard_1976 - NConstants - NComposition - CComposition - NConstant - CConstant - NGases - NAir - CAir - NCO2 - CCO2 - NGas - CGas - NSteam - CSteam - NLiquids - NLiquid - CLiquid - NWater - CWater - NPlanets - NEarth - CEarth - NMars - CMars - NPlanet - CPlanet - NPropellants - NAviation_Gasoline - CAviation_Gasoline - NGaseous_H2 - CGaseous_H2 - NJet_A - CJet_A - NJet_A1 - CJet_A1 - NLiquid_Natural_Gas - CLiquid_Natural_Gas - NPropellant - CPropellant + NMission + NAll_At_Once + CAll_At_Once + NMission + CContainer + CMission + NSegments + NAerodynamic + CAerodynamic + NClimb + NConstant_CAS_Constant_Rate + CConstant_CAS_Constant_Rate + NConstant_Dynamic_Pressure_Constant_Angle + CConstant_Dynamic_Pressure_Constant_Angle + NConstant_Dynamic_Pressure_Constant_Rate + CConstant_Dynamic_Pressure_Constant_Rate + NConstant_EAS_Constant_Rate + CConstant_EAS_Constant_Rate + NConstant_Mach_Constant_Angle + CConstant_Mach_Constant_Angle + NConstant_Mach_Constant_Rate + CConstant_Mach_Constant_Rate + NConstant_Mach_Linear_Altitude + CConstant_Mach_Linear_Altitude + NConstant_Speed_Constant_Angle + CConstant_Speed_Constant_Angle + NConstant_Speed_Constant_Angle_Noise + CConstant_Speed_Constant_Angle_Noise + NConstant_Speed_Constant_Rate + CConstant_Speed_Constant_Rate + NConstant_Speed_Linear_Altitude + CConstant_Speed_Linear_Altitude + NConstant_Throttle_Constant_Speed + CConstant_Throttle_Constant_Speed + NLinear_Mach_Constant_Rate + CLinear_Mach_Constant_Rate + NLinear_Speed_Constant_Rate + CLinear_Speed_Constant_Rate + NOptimized + COptimized + NUnknown_Throttle + CUnknown_Throttle + NConditions + NAerodynamics + CAerodynamics + NBasic + CBasic + NConditions + CConditions + Cexpanded_array + NNumerics + CNumerics + NResiduals + CResiduals + NState + CContainer + CState + NUnknowns + CUnknowns + NCruise + NConstant_Acceleration_Constant_Altitude + CConstant_Acceleration_Constant_Altitude + NConstant_Dynamic_Pressure_Constant_Altitude + CConstant_Dynamic_Pressure_Constant_Altitude + NConstant_Dynamic_Pressure_Constant_Altitude_Loiter + CConstant_Dynamic_Pressure_Constant_Altitude_Loiter + NConstant_Mach_Constant_Altitude + CConstant_Mach_Constant_Altitude + NConstant_Mach_Constant_Altitude_Loiter + CConstant_Mach_Constant_Altitude_Loiter + NConstant_Pitch_Rate_Constant_Altitude + CConstant_Pitch_Rate_Constant_Altitude + NConstant_Speed_Constant_Altitude + CConstant_Speed_Constant_Altitude + NConstant_Speed_Constant_Altitude_Loiter + CConstant_Speed_Constant_Altitude_Loiter + NConstant_Throttle_Constant_Altitude + CConstant_Throttle_Constant_Altitude + NDescent + NConstant_CAS_Constant_Rate + CConstant_CAS_Constant_Rate + NConstant_EAS_Constant_Rate + CConstant_EAS_Constant_Rate + NConstant_Speed_Constant_Angle + CConstant_Speed_Constant_Angle + NConstant_Speed_Constant_Angle_Noise + CConstant_Speed_Constant_Angle_Noise + NConstant_Speed_Constant_Rate + CConstant_Speed_Constant_Rate + NLinear_Mach_Constant_Rate + CLinear_Mach_Constant_Rate + NUnknown_Throttle + CUnknown_Throttle + NGround + NBattery_Charge_Discharge + CBattery_Charge_Discharge + NGround + CGround + NLanding + CLanding + NTakeoff + CTakeoff + NHover + NClimb + CClimb + NDescent + CDescent + NHover + CHover + NSegment + CContainer + CSegment + NSimple + CSimple + NSingle_Point + NSet_Speed_Set_Altitude + CSet_Speed_Set_Altitude + NSet_Speed_Set_Altitude_No_Propulsion + CSet_Speed_Set_Altitude_No_Propulsion + NSet_Speed_Set_Throttle + CSet_Speed_Set_Throttle + NTransition + NConstant_Acceleration_Constant_Angle_Linear_Climb + CConstant_Acceleration_Constant_Angle_Linear_Climb + NConstant_Acceleration_Constant_Pitchrate_Constant_Altitude + CConstant_Acceleration_Constant_Pitchrate_Constant_Altitude + NSequential_Segments + CSequential_Segments + NVariable_Range_Cruise + NGiven_State_of_Charge + CGiven_State_of_Charge + NGiven_Weight + CGiven_Weight + NNoise + NFidelity_One + CFidelity_One + NFidelity_Zero + CFidelity_Zero + NNoise + CNoise + NPlanets + NPlanet + CPlanet + NProcess + CProcess + NPropulsion + NRotor_Wake_Fidelity_One + CRotor_Wake_Fidelity_One + NRotor_Wake_Fidelity_Two + CRotor_Wake_Fidelity_Two + NRotor_Wake_Fidelity_Zero + CRotor_Wake_Fidelity_Zero + NSettings + CSettings + NSizing + NSizing + CSizing + NStability + NAVL + CAVL + NFidelity_Zero + CFidelity_Zero + NStability + CStability + NVehicle + CVehicle + NWeights + NWeights + CWeights + NWeights_BWB + CWeights_BWB + NWeights_eVTOL + CWeights_eVTOL + NWeights_Transport + CWeights_Transport + NWeights_UAV + CWeights_UAV + NAttributes + NAirports + NAirport + CAirport + NAtmospheres + NAtmosphere + CAtmosphere + NEarth + NConstant_Temperature + CConstant_Temperature + NUS_Standard_1976 + CUS_Standard_1976 + NConstants + NComposition + CComposition + NConstant + CConstant + NCryogens + NCryogen + CCryogen + NLiquid_H2 + CLiquid_H2 + NGases + NAir + CAir + NCO2 + CCO2 + NGas + CGas + NSteam + CSteam + NPlanets + NEarth + CEarth + NPlanet + CPlanet + NPropellants + NAviation_Gasoline + CAviation_Gasoline + NGaseous_H2 + CGaseous_H2 + NJet_A + CJet_A + NJet_A1 + CJet_A1 + NJP7 + CJP7 + NLiquid_H2 + CLiquid_H2 + NLiquid_Natural_Gas + CLiquid_Natural_Gas + NLOX_LH2 + CLOX_LH2 + NLOX_RP1 + CLOX_RP1 + NPropellant + CPropellant + NSolids + NAcrylic + CAcrylic + NAluminum + CAluminum + NAluminum_Rib + CAluminum_Rib + NBidirectional_Carbon_Fiber + CBidirectional_Carbon_Fiber + NCarbon_Fiber_Honeycomb + CCarbon_Fiber_Honeycomb + NCopper + CCopper + NEpoxy + CEpoxy + NNickel + CNickel + NPaint + CPaint + NSolid + CSolid + NSteel + CSteel + NUnidirectional_Carbon_Fiber + CUnidirectional_Carbon_Fiber  NComponents - NComponent - CComponent - CContainer - NConfigs - NConfig - CConfig - NCosts - NCosts - CIndustrial_Costs - COperating_Costs - NEnergy - NConverters - NCombustor - CCombustor - NCompression_Nozzle - CCompression_Nozzle - NCompressor - CCompressor - NExpansion_Nozzle - CExpansion_Nozzle - NFan - CFan - NFuel_Cell - CFuel_Cell - NGearbox - CGearbox - NMotor - CMotor - NMotor_Lo_Fid - CMotor_Lo_Fid - NPropeller - CPropeller - NPropeller_Lo_Fid - CPropeller_Lo_Fid - NRam - CRam - NShaft_Power_Off_Take - CShaft_Power_Off_Take - NSolar_Panel - CSolar_Panel
-

Solar_Panel Class

- - NSupersonic_Nozzle - CSupersonic_Nozzle - NTurbine - CTurbine - NDistributors - NElectronic_Speed_Controller - CElectronic_Speed_Controller - NSolar_Logic - CSolar_Logic - NEnergy - CEnergy - NEnergy_Component - CEnergy_Component - NNetworks - NBattery_Ducted_Fan - CBattery_Ducted_Fan - NBattery_Propeller - CBattery_Propeller - NDual_Battery_Ducted_Fan - CDual_Battery_Ducted_Fan - NDucted_Fan - CDucted_Fan - NLift_Forward_Propulsor - CLift_Forward_Propulsor - NPropulsor_Surrogate - CPropulsor_Surrogate - NRamjet - CRamjet - NSolar - CSolar - NSolar_Low_Fidelity - CSolar_Low_Fidelity - NTurbofan - CTurbofan - NTurbojet_Super - CTurbojet_Super - NPeripherals - NAvionics - CAvionics - NPayload - CPayload - NProcesses - NSolar_Radiation - CSolar_Radiation - NThrust - CThrust - NStorages - NBatteries - NBattery - CBattery - NConstant_Mass - NLithium_Ion - CLithium_Ion - NLithium_Sulfur - CLithium_Sulfur - NVariable_Mass - NAluminum_Air - CAluminum_Air - NLithium_Air - CLithium_Air - NEnvelope - CEnvelope - NFuselages - NFuselage - CContainer - CFuselage - NLanding_Gear - NLanding_Gear - CLanding_Gear - NMain_Landing_Gear - CMain_Landing_Gear - NNose_Landing_Gear - CNose_Landing_Gear - NLofted_Body - CCurve - CCurveContainer - CLofted_Body - CSection - CSectionContainer - CSegment - NMass_Properties - CMass_Properties - NPayloads - NCargo - CCargo - NPayload - CContainer - CPayload - NPerson - CPerson - NSatellite - CSatellite - NPhysical_Component - CContainer - CPhysical_Component - NPropulsors - NPropulsor - CContainer - CPropulsor - NSystems - NSystem - CSystem - NWings - NAirfoils - NAirfoil - CAirfoil - NControl_Surface - CControl_Surface - CControl_Surface_Section - NHorizontal_Tail - CHorizontal_Tail - NMain_Wing - CMain_Wing - NSegment - CSegment - CSegmentContainer - NVertical_Tail - CVertical_Tail - NWing - CWing + NAirfoils + NAirfoil + CAirfoil + NComponent + CComponent + CContainer + NConfigs + NConfig + CConfig + NCosts + NCosts + CIndustrial_Costs + COperating_Costs + NEnergy + NCharging + NCharging + CCharging + NConverters + NCombustor + CCombustor + NCompression_Nozzle + CCompression_Nozzle + NCompressor + CCompressor + Nde_Laval_Nozzle + Cde_Laval_Nozzle + NExpansion_Nozzle + CExpansion_Nozzle + NFan + CFan + NFuel_Cell + CFuel_Cell + NGearbox + CGearbox + NGenerator_Zero_Fid + CGenerator_Zero_Fid + NInternal_Combustion_Engine + CInternal_Combustion_Engine + NLift_Rotor + CLift_Rotor + NMotor + CMotor + NMotor_HTS_Rotor + CMotor_HTS_Rotor + NMotor_Lo_Fid + CMotor_Lo_Fid + NPropeller + CPropeller + NPropeller_Lo_Fid + CPropeller_Lo_Fid + NRam + CRam + NRocket_Combustor + CRocket_Combustor + NRotor + CRotor + NShaft_Power_Off_Take + CShaft_Power_Off_Take + NSolar_Panel + CSolar_Panel + NSupersonic_Nozzle + CSupersonic_Nozzle + NTurbine + CTurbine + NTurboelectric + CTurboelectric + NCooling + NCryocooler + CCryocooler + NCryogenic_Heat_Exchanger + CCryogenic_Heat_Exchanger + NDistributors + NCryogenic_Lead + CCryogenic_Lead + NElectronic_Speed_Controller + CElectronic_Speed_Controller + NHTS_DC_Supply + CHTS_DC_Supply + NSolar_Logic + CSolar_Logic + NEnergy_Component + CEnergy_Component + NNetworks + NBattery_Cell_Cycler + CBattery_Cell_Cycler + NBattery_Ducted_Fan + CBattery_Ducted_Fan + NBattery_Propeller + CBattery_Propeller + NDucted_Fan + CDucted_Fan + NInternal_Combustion_Propeller + CInternal_Combustion_Propeller + NInternal_Combustion_Propeller_Constant_Speed + CInternal_Combustion_Propeller_Constant_Speed + NLift_Cruise + CLift_Cruise + NLiquid_Rocket + CLiquid_Rocket + NNetwork + CContainer + CNetwork + NPropulsor_Surrogate + CPropulsor_Surrogate + NPyCycle + CPyCycle + NRamjet + CRamjet + NScramjet + CScramjet + NSerial_Hybrid_Ducted_Fan + CSerial_Hybrid_Ducted_Fan + NSolar + CSolar + NSolar_Low_Fidelity + CSolar_Low_Fidelity + NTurboelectric_HTS_Ducted_Fan + CTurboelectric_HTS_Ducted_Fan + NTurbofan + CTurbofan + NTurbojet_Super + CTurbojet_Super + NPeripherals + NAvionics + CAvionics + NPayload + CPayload + NProcesses + NRocket_Thrust + CRocket_Thrust + NSolar_Radiation + CSolar_Radiation + NThrust + CThrust + NStorages + NBatteries + NBattery + CBattery + NConstant_Mass + NLithium_Ion + CLithium_Ion + NLithium_Ion_LiFePO4_18650 + CLithium_Ion_LiFePO4_18650 + NLithium_Ion_LiNiMnCoO2_18650 + CLithium_Ion_LiNiMnCoO2_18650 + NLithium_Sulfur + CLithium_Sulfur + NVariable_Mass + NAluminum_Air + CAluminum_Air + NLithium_Air + CLithium_Air + NFuel_Tanks + NFuel_Tank + CFuel_Tank + NEnvelope + CEnvelope + NFuselages + NFuselage + CContainer + CFuselage + NLanding_Gear + NLanding_Gear + CLanding_Gear + NMain_Landing_Gear + CMain_Landing_Gear + NNose_Landing_Gear + CNose_Landing_Gear + NLofted_Body + CLofted_Body + CSection + CSection_Container + CSegment + NLofted_Body_Segment + NSegment + CSegment + CSegment_Container + NMass_Properties + CMass_Properties + NNacelles + NNacelle + CNacelle + NPayloads + NPayload + CContainer + CPayload + NPhysical_Component + CContainer + CPhysical_Component + NSystems + NSystem + CSystem + NWings + NAll_Moving_Surface + CAll_Moving_Surface + NControl_Surfaces + NAileron + CAileron + NControl_Surface + CControl_Surface + NElevator + CElevator + NFlap + CFlap + NRudder + CRudder + NSlat + CSlat + NHorizontal_Tail + CHorizontal_Tail + NMain_Wing + CMain_Wing + CSegment_Container + NSegment + CSegment + CSegment_Container + NStabilator + CStabilator + NVertical_Tail + CVertical_Tail + NVertical_Tail_All_Moving + CVertical_Tail_All_Moving + NWing + CContainer + CWing  NCore  NContainer  CContainer @@ -567,94 +680,102 @@

Inputs  NSettings - CAVL_Discretization_Settings - CSettings + CSettings  NWing  CControl_Surface - CSection - CWing - NOptimization - NNexus - CNexus - NPackage_Setups - NTRMM - NTrust_Region - CTrust_Region - NTrust_Region_Optimization - CTrust_Region_Optimization - NSurrogate_Optimization - CSurrogate_Optimization - NPlugins - Npint - Ncompat - CChainMap - Ncontext - CContext - CContextChain - Nmeasurement - CMeasurement - Nquantity - C_Exception - C_Quantity - Ntestsuite - Ntest_contexts - CTestContexts - CTestDefinedContexts - CTestHandler - Ntest_issues - CTestIssues - CTestIssuesNP - Ntest_measurement - CTestMeasurement - Ntest_numpy - CTestBitTwiddlingUfuncs - CTestNumpyMethods - CTestNumpyNotSupported - Ntest_pitheorem - CTestPiTheorem - Ntest_quantity - CTestDimensions - CTestQuantity - Ntest_umath - CTestComparisonUfuncs - CTestFloatingUfuncs - CTestMathUfuncs - CTestTrigUfuncs - CTestUFuncs - Ntest_unit - CTestConverter - CTestDefinition - CTestRegistry - CTestUnitsContainer - Ntest_util - CTestStringProcessor - Cndarray - CTestCase - Nunit - CConverter - CDefinition - CDimensionalityError - CDimensionDefinition - COffsetConverter - CPrefixDefinition - CScaleConverter - CUndefinedUnitError - CUnitDefinition - CUnitRegistry - CUnitsContainer - Nutil - Cndarray - CParserHelper - NSizing - NSizing_Loop - CSizing_Loop - NSurrogate - NSurrogate_Problem - CSurrogate_Problem - NVehicle - CCosts - CVehicle - CVehicle_Mass_Properties + CControl_Surface_Data + CControl_Surface_Results + CSection + CWing + NSupersonic_Zero + NDrag + NCubic_Spline_Blender + CCubic_Spline_Blender + NUtilities + NCubic_Spline_Blender + CCubic_Spline_Blender + NOptimization + NNexus + CNexus + NPackage_Setups + Nadditive_setup + CAdditive_Solver + NTRMM + NTrust_Region + CTrust_Region + NTrust_Region_Optimization + CTrust_Region_Optimization + NSurrogate_Optimization + CSurrogate_Optimization + NPlugins + Npint + Ncompat + CChainMap + Ncontext + CContext + CContextChain + Nmeasurement + CMeasurement + Nquantity + C_Exception + C_Quantity + Ntestsuite + Ntest_contexts + CTestContexts + CTestDefinedContexts + CTestHandler + Ntest_issues + CTestIssues + CTestIssuesNP + Ntest_measurement + CTestMeasurement + Ntest_numpy + CTestBitTwiddlingUfuncs + CTestNumpyMethods + CTestNumpyNotSupported + Ntest_pitheorem + CTestPiTheorem + Ntest_quantity + CTestDimensions + CTestQuantity + Ntest_umath + CTestComparisonUfuncs + CTestFloatingUfuncs + CTestMathUfuncs + CTestTrigUfuncs + CTestUFuncs + Ntest_unit + CTestConverter + CTestDefinition + CTestRegistry + CTestUnitsContainer + Ntest_util + CTestStringProcessor + Cndarray + CTestCase + Nunit + CConverter + CDefinition + CDimensionalityError + CDimensionDefinition + COffsetConverter + CPrefixDefinition + CScaleConverter + CUndefinedUnitError + CUnitDefinition + CUnitRegistry + CUnitsContainer + Nutil + Cndarray + CParserHelper + NSurrogate + NSurrogate_Problem + CSurrogate_Problem + NVehicle + CCosts + CVehicle + CVehicle_Mass_Container + CVehicle_Mass_Properties

@@ -664,7 +785,7 @@

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"classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Conditions_1_1Conditions" ] + [ "Conditions", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Conditions_1_1Conditions.html", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Conditions_1_1Conditions" ], + [ "expanded_array", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Conditions_1_1expanded__array.html", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Conditions_1_1expanded__array" ] ] ], [ "Numerics", null, [ [ "Numerics", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Numerics_1_1Numerics.html", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Numerics_1_1Numerics" ] @@ -200,6 +191,9 @@ var annotated_dup = ] ] ] ], [ "Descent", null, [ + [ "Constant_CAS_Constant_Rate", null, [ + [ "Constant_CAS_Constant_Rate", 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"Ground", null, [ [ "Ground", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Ground_1_1Ground.html", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Ground_1_1Ground" ] ] ], @@ -252,17 +249,31 @@ var annotated_dup = [ "Set_Speed_Set_Altitude", null, [ [ "Set_Speed_Set_Altitude", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Altitude_1_1Set__Speed__Set__Altitude.html", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Altitude_1_1Set__Speed__Set__Altitude" ] ] ], + [ "Set_Speed_Set_Altitude_No_Propulsion", null, [ + [ "Set_Speed_Set_Altitude_No_Propulsion", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Altitude__No_660be05666a18eb7201c7425b4456ff1.html", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Altitude__No_660be05666a18eb7201c7425b4456ff1" ] + ] ], [ "Set_Speed_Set_Throttle", null, [ [ "Set_Speed_Set_Throttle", 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"Propulsion", null, [ + [ "Rotor_Wake_Fidelity_One", null, [ + [ "Rotor_Wake_Fidelity_One", "classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__One_1_1Rotor__Wake__Fidelity__One.html", "classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__One_1_1Rotor__Wake__Fidelity__One" ] + ] ], + [ "Rotor_Wake_Fidelity_Two", null, [ + [ "Rotor_Wake_Fidelity_Two", "classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__Two_1_1Rotor__Wake__Fidelity__Two.html", "classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__Two_1_1Rotor__Wake__Fidelity__Two" ] + ] ], + [ "Rotor_Wake_Fidelity_Zero", null, [ + [ "Rotor_Wake_Fidelity_Zero", "classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__Zero_1_1Rotor__Wake__Fidelity__Zero.html", "classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__Zero_1_1Rotor__Wake__Fidelity__Zero" ] + ] ] + ] ], [ "Settings", null, [ [ "Settings", "classSUAVE_1_1Analyses_1_1Settings_1_1Settings.html", "classSUAVE_1_1Analyses_1_1Settings_1_1Settings" ] ] ], @@ -301,14 +326,6 @@ var annotated_dup = [ "Stability", "classSUAVE_1_1Analyses_1_1Stability_1_1Stability_1_1Stability.html", "classSUAVE_1_1Analyses_1_1Stability_1_1Stability_1_1Stability" ] ] ] ] ], - [ "Structures", null, [ - [ "Structures", null, [ - [ "Structures", "classSUAVE_1_1Analyses_1_1Structures_1_1Structures_1_1Structures.html", "classSUAVE_1_1Analyses_1_1Structures_1_1Structures_1_1Structures" ] - ] ] - ] ], - [ "Surrogate", null, [ - [ "Surrogate", "classSUAVE_1_1Analyses_1_1Surrogate_1_1Surrogate.html", "classSUAVE_1_1Analyses_1_1Surrogate_1_1Surrogate" ] - ] ], [ "Vehicle", null, [ [ "Vehicle", "classSUAVE_1_1Analyses_1_1Vehicle_1_1Vehicle.html", "classSUAVE_1_1Analyses_1_1Vehicle_1_1Vehicle" ] ] ], @@ -319,8 +336,11 @@ var annotated_dup = [ "Weights_BWB", null, [ [ "Weights_BWB", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights__BWB_1_1Weights__BWB.html", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights__BWB_1_1Weights__BWB" ] ] ], - [ "Weights_Tube_Wing", null, [ - [ "Weights_Tube_Wing", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights__Tube__Wing_1_1Weights__Tube__Wing.html", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights__Tube__Wing_1_1Weights__Tube__Wing" ] + [ "Weights_eVTOL", null, [ + [ "Weights_eVTOL", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights__eVTOL_1_1Weights__eVTOL.html", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights__eVTOL_1_1Weights__eVTOL" ] + ] ], + [ "Weights_Transport", null, [ + [ "Weights_Transport", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights__Transport_1_1Weights__Transport.html", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights__Transport_1_1Weights__Transport" ] ] ], [ "Weights_UAV", null, [ [ "Weights_UAV", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights__UAV_1_1Weights__UAV.html", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights__UAV_1_1Weights__UAV" ] @@ -331,9 +351,6 @@ var annotated_dup = [ "Airports", null, [ [ 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] ] ] ] ] ], [ "Components", null, [ + [ "Airfoils", null, [ + [ "Airfoil", null, [ + [ "Airfoil", "classSUAVE_1_1Components_1_1Airfoils_1_1Airfoil_1_1Airfoil.html", "classSUAVE_1_1Components_1_1Airfoils_1_1Airfoil_1_1Airfoil" ] + ] ] + ] ], [ "Component", null, [ [ "Component", "classSUAVE_1_1Components_1_1Component_1_1Component.html", "classSUAVE_1_1Components_1_1Component_1_1Component" ], [ "Container", "classSUAVE_1_1Components_1_1Component_1_1Container.html", null ] @@ -428,6 +497,11 @@ var annotated_dup = ] ] ] ], [ "Energy", null, [ + [ "Charging", null, [ + [ "Charging", null, [ + [ "Charging", "classSUAVE_1_1Components_1_1Energy_1_1Charging_1_1Charging_1_1Charging.html", "classSUAVE_1_1Components_1_1Energy_1_1Charging_1_1Charging_1_1Charging" ] + ] ] + ] ], [ "Converters", null, [ [ "Combustor", null, [ [ "Combustor", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Combustor_1_1Combustor.html", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Combustor_1_1Combustor" ] @@ -438,6 +512,9 @@ var annotated_dup = [ "Compressor", null, [ [ "Compressor", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Compressor_1_1Compressor.html", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Compressor_1_1Compressor" ] ] ], + [ "de_Laval_Nozzle", null, [ + [ "de_Laval_Nozzle", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1de__Laval__Nozzle_1_1de__Laval__Nozzle.html", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1de__Laval__Nozzle_1_1de__Laval__Nozzle" ] + ] ], [ "Expansion_Nozzle", null, [ [ "Expansion_Nozzle", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Expansion__Nozzle_1_1Expansion__Nozzle.html", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Expansion__Nozzle_1_1Expansion__Nozzle" ] ] ], @@ -450,9 +527,21 @@ var annotated_dup = [ "Gearbox", null, [ [ "Gearbox", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Gearbox_1_1Gearbox.html", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Gearbox_1_1Gearbox" ] ] ], + [ "Generator_Zero_Fid", null, [ + [ "Generator_Zero_Fid", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Generator__Zero__Fid_1_1Generator__Zero__Fid.html", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Generator__Zero__Fid_1_1Generator__Zero__Fid" ] + ] ], + [ "Internal_Combustion_Engine", null, [ + [ "Internal_Combustion_Engine", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Internal__Combustion__Engine_1_1Internal__Combustion__Engine.html", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Internal__Combustion__Engine_1_1Internal__Combustion__Engine" ] + ] ], + [ "Lift_Rotor", null, [ + [ "Lift_Rotor", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Lift__Rotor_1_1Lift__Rotor.html", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Lift__Rotor_1_1Lift__Rotor" ] + ] ], [ "Motor", null, [ [ "Motor", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor_1_1Motor.html", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor_1_1Motor" ] ] ], + [ "Motor_HTS_Rotor", null, [ + [ "Motor_HTS_Rotor", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__HTS__Rotor_1_1Motor__HTS__Rotor.html", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__HTS__Rotor_1_1Motor__HTS__Rotor" ] + ] ], [ "Motor_Lo_Fid", null, [ [ "Motor_Lo_Fid", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__Lo__Fid_1_1Motor__Lo__Fid.html", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__Lo__Fid_1_1Motor__Lo__Fid" ] ] ], @@ -465,6 +554,12 @@ var annotated_dup = [ "Ram", null, [ [ "Ram", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Ram_1_1Ram.html", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Ram_1_1Ram" ] ] ], + [ "Rocket_Combustor", null, [ + [ "Rocket_Combustor", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Rocket__Combustor_1_1Rocket__Combustor.html", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Rocket__Combustor_1_1Rocket__Combustor" ] + ] ], + [ "Rotor", null, [ + [ "Rotor", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Rotor_1_1Rotor.html", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Rotor_1_1Rotor" ] + ] ], [ "Shaft_Power_Off_Take", null, [ [ "Shaft_Power_Off_Take", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Shaft__Power__Off__Take_1_1Shaft__Power__Off__Take.html", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Shaft__Power__Off__Take_1_1Shaft__Power__Off__Take" ] ] ], @@ -476,50 +571,89 @@ var annotated_dup = ] ], [ "Turbine", null, [ [ "Turbine", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Turbine_1_1Turbine.html", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Turbine_1_1Turbine" ] + ] ], + [ "Turboelectric", null, [ + [ "Turboelectric", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Turboelectric_1_1Turboelectric.html", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Turboelectric_1_1Turboelectric" ] + ] ] + ] ], + [ "Cooling", null, [ + [ "Cryocooler", null, [ + [ "Cryocooler", "classSUAVE_1_1Components_1_1Energy_1_1Cooling_1_1Cryocooler_1_1Cryocooler.html", "classSUAVE_1_1Components_1_1Energy_1_1Cooling_1_1Cryocooler_1_1Cryocooler" ] + ] ], + [ "Cryogenic_Heat_Exchanger", null, [ + [ "Cryogenic_Heat_Exchanger", "classSUAVE_1_1Components_1_1Energy_1_1Cooling_1_1Cryogenic__Heat__Exchanger_1_1Cryogenic__Heat__Exchanger.html", "classSUAVE_1_1Components_1_1Energy_1_1Cooling_1_1Cryogenic__Heat__Exchanger_1_1Cryogenic__Heat__Exchanger" ] ] ] ] ], [ "Distributors", null, [ + [ "Cryogenic_Lead", null, [ + [ "Cryogenic_Lead", "classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Cryogenic__Lead_1_1Cryogenic__Lead.html", "classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Cryogenic__Lead_1_1Cryogenic__Lead" ] + ] ], [ "Electronic_Speed_Controller", null, [ [ "Electronic_Speed_Controller", "classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Electronic__Speed__Controller_1_1Electronic__Speed__Controller.html", "classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Electronic__Speed__Controller_1_1Electronic__Speed__Controller" ] ] ], + [ "HTS_DC_Supply", null, [ + [ "HTS_DC_Supply", "classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1HTS__DC__Supply_1_1HTS__DC__Supply.html", "classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1HTS__DC__Supply_1_1HTS__DC__Supply" ] + ] ], [ "Solar_Logic", null, [ [ "Solar_Logic", "classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Solar__Logic_1_1Solar__Logic.html", "classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Solar__Logic_1_1Solar__Logic" ] ] ] ] ], - [ "Energy", null, [ - [ "Energy", "classSUAVE_1_1Components_1_1Energy_1_1Energy_1_1Energy.html", "classSUAVE_1_1Components_1_1Energy_1_1Energy_1_1Energy" ] - ] ], [ "Energy_Component", null, [ [ "Energy_Component", "classSUAVE_1_1Components_1_1Energy_1_1Energy__Component_1_1Energy__Component.html", "classSUAVE_1_1Components_1_1Energy_1_1Energy__Component_1_1Energy__Component" ] ] ], [ "Networks", null, [ + [ "Battery_Cell_Cycler", null, [ + [ "Battery_Cell_Cycler", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Cell__Cycler_1_1Battery__Cell__Cycler.html", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Cell__Cycler_1_1Battery__Cell__Cycler" ] + ] ], [ "Battery_Ducted_Fan", null, [ [ "Battery_Ducted_Fan", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Ducted__Fan_1_1Battery__Ducted__Fan.html", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Ducted__Fan_1_1Battery__Ducted__Fan" ] ] ], [ "Battery_Propeller", null, [ [ "Battery_Propeller", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Propeller_1_1Battery__Propeller.html", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Propeller_1_1Battery__Propeller" ] ] ], - [ "Dual_Battery_Ducted_Fan", null, [ - [ "Dual_Battery_Ducted_Fan", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Dual__Battery__Ducted__Fan_1_1Dual__Battery__Ducted__Fan.html", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Dual__Battery__Ducted__Fan_1_1Dual__Battery__Ducted__Fan" ] - ] ], [ "Ducted_Fan", null, [ [ "Ducted_Fan", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ducted__Fan_1_1Ducted__Fan.html", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ducted__Fan_1_1Ducted__Fan" ] ] ], - [ "Lift_Forward_Propulsor", null, [ - [ "Lift_Forward_Propulsor", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Lift__Forward__Propulsor_1_1Lift__Forward__Propulsor.html", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Lift__Forward__Propulsor_1_1Lift__Forward__Propulsor" ] + [ "Internal_Combustion_Propeller", null, [ + [ "Internal_Combustion_Propeller", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Internal__Combustion__Propeller_1_1Internal__Combustion__Propeller.html", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Internal__Combustion__Propeller_1_1Internal__Combustion__Propeller" ] + ] ], + [ "Internal_Combustion_Propeller_Constant_Speed", null, [ + [ "Internal_Combustion_Propeller_Constant_Speed", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Internal__Combustion__Propeller__Constant__Spefd0f47b019fa78b7cc3bc47b5f2c3d76.html", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Internal__Combustion__Propeller__Constant__Spefd0f47b019fa78b7cc3bc47b5f2c3d76" ] + ] ], + [ "Lift_Cruise", null, [ + [ "Lift_Cruise", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Lift__Cruise_1_1Lift__Cruise.html", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Lift__Cruise_1_1Lift__Cruise" ] + ] ], + [ "Liquid_Rocket", null, [ + [ "Liquid_Rocket", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Liquid__Rocket_1_1Liquid__Rocket.html", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Liquid__Rocket_1_1Liquid__Rocket" ] + ] ], + [ "Network", null, [ + [ "Container", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Network_1_1Container.html", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Network_1_1Container" ], + [ "Network", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Network_1_1Network.html", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Network_1_1Network" ] ] ], [ "Propulsor_Surrogate", null, [ [ "Propulsor_Surrogate", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Propulsor__Surrogate_1_1Propulsor__Surrogate.html", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Propulsor__Surrogate_1_1Propulsor__Surrogate" ] ] ], + [ "PyCycle", null, [ + [ "PyCycle", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1PyCycle_1_1PyCycle.html", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1PyCycle_1_1PyCycle" ] + ] ], [ "Ramjet", null, [ [ "Ramjet", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ramjet_1_1Ramjet.html", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ramjet_1_1Ramjet" ] ] ], + [ "Scramjet", null, [ + [ "Scramjet", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Scramjet_1_1Scramjet.html", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Scramjet_1_1Scramjet" ] + ] ], + [ "Serial_Hybrid_Ducted_Fan", null, [ + [ "Serial_Hybrid_Ducted_Fan", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Serial__Hybrid__Ducted__Fan_1_1Serial__Hybrid__Ducted__Fan.html", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Serial__Hybrid__Ducted__Fan_1_1Serial__Hybrid__Ducted__Fan" ] + ] ], [ "Solar", null, [ [ "Solar", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar.html", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar" ] ] ], [ "Solar_Low_Fidelity", null, [ [ "Solar_Low_Fidelity", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar__Low__Fidelity_1_1Solar__Low__Fidelity.html", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar__Low__Fidelity_1_1Solar__Low__Fidelity" ] ] ], + [ "Turboelectric_HTS_Ducted_Fan", null, [ + [ "Turboelectric_HTS_Ducted_Fan", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turboelectric__HTS__Ducted__Fan_1_1Turboelectric__HTS__Ducted__Fan.html", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turboelectric__HTS__Ducted__Fan_1_1Turboelectric__HTS__Ducted__Fan" ] + ] ], [ "Turbofan", null, [ [ "Turbofan", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbofan_1_1Turbofan.html", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbofan_1_1Turbofan" ] ] ], @@ -536,6 +670,9 @@ var annotated_dup = ] ] ] ], [ "Processes", null, [ + [ "Rocket_Thrust", null, [ + [ "Rocket_Thrust", "classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Rocket__Thrust_1_1Rocket__Thrust.html", "classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Rocket__Thrust_1_1Rocket__Thrust" ] + ] ], [ "Solar_Radiation", null, [ [ "Solar_Radiation", "classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Solar__Radiation_1_1Solar__Radiation.html", "classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Solar__Radiation_1_1Solar__Radiation" ] ] ], @@ -552,6 +689,12 @@ var annotated_dup = [ "Lithium_Ion", null, [ [ "Lithium_Ion", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Constant__Mass_1_1Lithium__Ion_1_1Lithium__Ion.html", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Constant__Mass_1_1Lithium__Ion_1_1Lithium__Ion" ] ] ], + [ "Lithium_Ion_LiFePO4_18650", null, [ + [ "Lithium_Ion_LiFePO4_18650", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Constant__Mass_1_1Lithium__Ion__Lc7c774ecc0e754e494e2e31ae8c98a5c.html", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Constant__Mass_1_1Lithium__Ion__Lc7c774ecc0e754e494e2e31ae8c98a5c" ] + ] ], + [ "Lithium_Ion_LiNiMnCoO2_18650", null, [ + [ "Lithium_Ion_LiNiMnCoO2_18650", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Constant__Mass_1_1Lithium__Ion__Ld01c6b6bada918794df8f70f8e6c1443.html", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Constant__Mass_1_1Lithium__Ion__Ld01c6b6bada918794df8f70f8e6c1443" ] + ] ], [ "Lithium_Sulfur", null, [ [ "Lithium_Sulfur", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Constant__Mass_1_1Lithium__Sulfur_1_1Lithium__Sulfur.html", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Constant__Mass_1_1Lithium__Sulfur_1_1Lithium__Sulfur" ] ] ] @@ -564,6 +707,11 @@ var annotated_dup = [ "Lithium_Air", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Variable__Mass_1_1Lithium__Air_1_1Lithium__Air.html", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Variable__Mass_1_1Lithium__Air_1_1Lithium__Air" ] ] ] ] ] + ] ], + [ "Fuel_Tanks", null, [ + [ "Fuel_Tank", null, [ + [ "Fuel_Tank", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Fuel__Tanks_1_1Fuel__Tank_1_1Fuel__Tank.html", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Fuel__Tanks_1_1Fuel__Tank_1_1Fuel__Tank" ] + ] ] ] ] ] ] ] ], @@ -572,7 +720,7 @@ var annotated_dup = ] ], [ "Fuselages", null, [ [ "Fuselage", null, [ - [ "Container", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Container.html", null ], + [ "Container", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Container.html", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Container" ], [ "Fuselage", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage" ] ] ] ] ], @@ -588,70 +736,86 @@ var annotated_dup = ] ] ] ], [ "Lofted_Body", null, [ - [ "Curve", "classSUAVE_1_1Components_1_1Lofted__Body_1_1Curve.html", "classSUAVE_1_1Components_1_1Lofted__Body_1_1Curve" ], - [ "CurveContainer", "classSUAVE_1_1Components_1_1Lofted__Body_1_1CurveContainer.html", null ], [ "Lofted_Body", "classSUAVE_1_1Components_1_1Lofted__Body_1_1Lofted__Body.html", "classSUAVE_1_1Components_1_1Lofted__Body_1_1Lofted__Body" ], [ "Section", "classSUAVE_1_1Components_1_1Lofted__Body_1_1Section.html", "classSUAVE_1_1Components_1_1Lofted__Body_1_1Section" ], - [ "SectionContainer", "classSUAVE_1_1Components_1_1Lofted__Body_1_1SectionContainer.html", null ], + [ "Section_Container", "classSUAVE_1_1Components_1_1Lofted__Body_1_1Section__Container.html", "classSUAVE_1_1Components_1_1Lofted__Body_1_1Section__Container" ], [ "Segment", "classSUAVE_1_1Components_1_1Lofted__Body_1_1Segment.html", "classSUAVE_1_1Components_1_1Lofted__Body_1_1Segment" ] ] ], + [ "Lofted_Body_Segment", null, [ + [ "Segment", null, [ + [ "Segment", "classSUAVE_1_1Components_1_1Lofted__Body__Segment_1_1Segment_1_1Segment.html", "classSUAVE_1_1Components_1_1Lofted__Body__Segment_1_1Segment_1_1Segment" ], + [ "Segment_Container", "classSUAVE_1_1Components_1_1Lofted__Body__Segment_1_1Segment_1_1Segment__Container.html", "classSUAVE_1_1Components_1_1Lofted__Body__Segment_1_1Segment_1_1Segment__Container" ] + ] ] + ] ], [ "Mass_Properties", null, [ [ "Mass_Properties", "classSUAVE_1_1Components_1_1Mass__Properties_1_1Mass__Properties.html", "classSUAVE_1_1Components_1_1Mass__Properties_1_1Mass__Properties" ] ] ], + [ "Nacelles", null, [ + [ "Nacelle", null, [ + [ "Nacelle", "classSUAVE_1_1Components_1_1Nacelles_1_1Nacelle_1_1Nacelle.html", "classSUAVE_1_1Components_1_1Nacelles_1_1Nacelle_1_1Nacelle" ] + ] ] + ] ], [ "Payloads", null, [ - [ "Cargo", null, [ - [ "Cargo", "classSUAVE_1_1Components_1_1Payloads_1_1Cargo_1_1Cargo.html", "classSUAVE_1_1Components_1_1Payloads_1_1Cargo_1_1Cargo" ] - ] ], [ "Payload", null, [ [ "Container", "classSUAVE_1_1Components_1_1Payloads_1_1Payload_1_1Container.html", null ], [ "Payload", "classSUAVE_1_1Components_1_1Payloads_1_1Payload_1_1Payload.html", "classSUAVE_1_1Components_1_1Payloads_1_1Payload_1_1Payload" ] - ] ], - [ "Person", null, [ - [ "Person", "classSUAVE_1_1Components_1_1Payloads_1_1Person_1_1Person.html", "classSUAVE_1_1Components_1_1Payloads_1_1Person_1_1Person" ] - ] ], - [ 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"classSUAVE_1_1Components_1_1Systems_1_1System_1_1System.html", "classSUAVE_1_1Components_1_1Systems_1_1System_1_1System" ] ] ] ] ], [ "Wings", null, [ - [ "Airfoils", null, [ - [ "Airfoil", null, [ - [ "Airfoil", "classSUAVE_1_1Components_1_1Wings_1_1Airfoils_1_1Airfoil_1_1Airfoil.html", "classSUAVE_1_1Components_1_1Wings_1_1Airfoils_1_1Airfoil_1_1Airfoil" ] - ] ] + [ "All_Moving_Surface", null, [ + [ "All_Moving_Surface", "classSUAVE_1_1Components_1_1Wings_1_1All__Moving__Surface_1_1All__Moving__Surface.html", "classSUAVE_1_1Components_1_1Wings_1_1All__Moving__Surface_1_1All__Moving__Surface" ] ] ], - [ "Control_Surface", null, [ - [ "Control_Surface", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surface_1_1Control__Surface.html", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surface_1_1Control__Surface" ], - [ "Control_Surface_Section", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surface_1_1Control__Surface__Section.html", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surface_1_1Control__Surface__Section" ] + [ "Control_Surfaces", null, [ + [ "Aileron", null, [ + [ "Aileron", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Aileron_1_1Aileron.html", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Aileron_1_1Aileron" ] + ] ], + [ "Control_Surface", null, [ + [ "Control_Surface", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Control__Surface_1_1Control__Surface.html", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Control__Surface_1_1Control__Surface" ] + ] ], + [ "Elevator", null, [ + [ "Elevator", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Elevator_1_1Elevator.html", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Elevator_1_1Elevator" ] + ] ], + [ "Flap", null, [ + [ "Flap", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Flap_1_1Flap.html", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Flap_1_1Flap" ] + ] ], + [ "Rudder", null, [ + [ "Rudder", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Rudder_1_1Rudder.html", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Rudder_1_1Rudder" ] + ] ], + [ "Slat", null, [ + [ "Slat", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Slat_1_1Slat.html", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Slat_1_1Slat" ] + ] ] ] ], [ "Horizontal_Tail", null, [ [ "Horizontal_Tail", "classSUAVE_1_1Components_1_1Wings_1_1Horizontal__Tail_1_1Horizontal__Tail.html", "classSUAVE_1_1Components_1_1Wings_1_1Horizontal__Tail_1_1Horizontal__Tail" ] ] ], [ "Main_Wing", null, [ - [ "Main_Wing", "classSUAVE_1_1Components_1_1Wings_1_1Main__Wing_1_1Main__Wing.html", "classSUAVE_1_1Components_1_1Wings_1_1Main__Wing_1_1Main__Wing" ] + [ "Main_Wing", "classSUAVE_1_1Components_1_1Wings_1_1Main__Wing_1_1Main__Wing.html", "classSUAVE_1_1Components_1_1Wings_1_1Main__Wing_1_1Main__Wing" ], + [ "Segment_Container", "classSUAVE_1_1Components_1_1Wings_1_1Main__Wing_1_1Segment__Container.html", "classSUAVE_1_1Components_1_1Wings_1_1Main__Wing_1_1Segment__Container" ] ] ], [ "Segment", null, [ [ "Segment", "classSUAVE_1_1Components_1_1Wings_1_1Segment_1_1Segment.html", "classSUAVE_1_1Components_1_1Wings_1_1Segment_1_1Segment" ], - [ "SegmentContainer", "classSUAVE_1_1Components_1_1Wings_1_1Segment_1_1SegmentContainer.html", null ] + [ "Segment_Container", "classSUAVE_1_1Components_1_1Wings_1_1Segment_1_1Segment__Container.html", "classSUAVE_1_1Components_1_1Wings_1_1Segment_1_1Segment__Container" ] + ] ], + [ "Stabilator", null, [ + [ "Stabilator", "classSUAVE_1_1Components_1_1Wings_1_1Stabilator_1_1Stabilator.html", "classSUAVE_1_1Components_1_1Wings_1_1Stabilator_1_1Stabilator" ] ] ], [ "Vertical_Tail", null, [ [ "Vertical_Tail", "classSUAVE_1_1Components_1_1Wings_1_1Vertical__Tail_1_1Vertical__Tail.html", "classSUAVE_1_1Components_1_1Wings_1_1Vertical__Tail_1_1Vertical__Tail" ] ] ], + [ "Vertical_Tail_All_Moving", null, [ + [ "Vertical_Tail_All_Moving", "classSUAVE_1_1Components_1_1Wings_1_1Vertical__Tail__All__Moving_1_1Vertical__Tail__All__Moving.html", "classSUAVE_1_1Components_1_1Wings_1_1Vertical__Tail__All__Moving_1_1Vertical__Tail__All__Moving" ] + ] ], [ "Wing", null, [ + [ "Container", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Container.html", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Container" ], [ "Wing", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing" ] ] ] ] ] @@ -716,15 +880,28 @@ var annotated_dup = [ "Inputs", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Inputs_1_1Inputs.html", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Inputs_1_1Inputs" ] ] ], [ "Settings", null, [ - [ "AVL_Discretization_Settings", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Settings_1_1AVL__Discretization__Settings.html", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Settings_1_1AVL__Discretization__Settings" ], [ "Settings", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Settings_1_1Settings.html", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Settings_1_1Settings" ] ] ], [ "Wing", null, [ [ "Control_Surface", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface.html", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface" ], + [ "Control_Surface_Data", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface__Data.html", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface__Data" ], + [ "Control_Surface_Results", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface__Results.html", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface__Results" ], [ "Section", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Section.html", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Section" ], [ "Wing", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Wing.html", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Wing" ] ] ] ] ] + ] ], + [ "Supersonic_Zero", null, [ + [ "Drag", null, [ + [ "Cubic_Spline_Blender", null, [ + [ "Cubic_Spline_Blender", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1Supersonic__Zero_1_1Drag_1_1Cubic__Spline__Blender_1_1Cubic__Spline__Blender.html", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1Supersonic__Zero_1_1Drag_1_1Cubic__Spline__Blender_1_1Cubic__Spline__Blender" ] + ] ] + ] ] + ] ] + ] ], + [ "Utilities", null, [ + [ "Cubic_Spline_Blender", null, [ + [ "Cubic_Spline_Blender", "classSUAVE_1_1Methods_1_1Utilities_1_1Cubic__Spline__Blender_1_1Cubic__Spline__Blender.html", "classSUAVE_1_1Methods_1_1Utilities_1_1Cubic__Spline__Blender_1_1Cubic__Spline__Blender" ] ] ] ] ] ] ], @@ -733,6 +910,9 @@ var annotated_dup = [ "Nexus", "classSUAVE_1_1Optimization_1_1Nexus_1_1Nexus.html", "classSUAVE_1_1Optimization_1_1Nexus_1_1Nexus" ] ] ], [ "Package_Setups", null, [ + [ "additive_setup", null, [ + [ "Additive_Solver", "classSUAVE_1_1Optimization_1_1Package__Setups_1_1additive__setup_1_1Additive__Solver.html", "classSUAVE_1_1Optimization_1_1Package__Setups_1_1additive__setup_1_1Additive__Solver" ] + ] ], [ "TRMM", null, [ [ "Trust_Region", null, [ [ "Trust_Region", "classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region_1_1Trust__Region.html", "classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region_1_1Trust__Region" ] @@ -825,11 +1005,6 @@ var annotated_dup = ] ] ] ] ] ], - [ "Sizing", null, [ - [ "Sizing_Loop", null, [ - [ "Sizing_Loop", "classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.html", "classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop" ] - ] ] - ] ], [ "Surrogate", null, [ [ "Surrogate_Problem", null, [ [ "Surrogate_Problem", "classSUAVE_1_1Surrogate_1_1Surrogate__Problem_1_1Surrogate__Problem.html", "classSUAVE_1_1Surrogate_1_1Surrogate__Problem_1_1Surrogate__Problem" ] @@ -838,6 +1013,7 @@ var annotated_dup = [ "Vehicle", null, [ [ "Costs", "classSUAVE_1_1Vehicle_1_1Costs.html", "classSUAVE_1_1Vehicle_1_1Costs" ], [ "Vehicle", "classSUAVE_1_1Vehicle_1_1Vehicle.html", "classSUAVE_1_1Vehicle_1_1Vehicle" ], + [ "Vehicle_Mass_Container", "classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Container.html", "classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Container" ], [ "Vehicle_Mass_Properties", "classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties.html", "classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties" ] ] ] ] ] diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AERODAS_1_1AERODAS-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AERODAS_1_1AERODAS-members.html index efd9f766..6e0176c5 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AERODAS_1_1AERODAS-members.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AERODAS_1_1AERODAS-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@
- +
@@ -73,7 +78,9 @@
@@ -98,21 +105,20 @@

This is the complete list of members for SUAVE.Analyses.Aerodynamics.AERODAS.AERODAS, including all inherited members.

- + - - - - - - - - - - - - - + + + + + + + + + + + +
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Aerodynamics.AERODAS.AERODAS
compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
compute_forces(self, conditions)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
evaluate(self, state)SUAVE.Analyses.Aerodynamics.Markup.Markup
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
geometry (defined in SUAVE.Analyses.Aerodynamics.Markup.Markup)SUAVE.Analyses.Aerodynamics.Markup.Markup
initialize(self)SUAVE.Analyses.Aerodynamics.Markup.Markup
SUAVE::Analyses::Aerodynamics::Aerodynamics::Aerodynamics.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
process (defined in SUAVE.Analyses.Aerodynamics.Markup.Markup)SUAVE.Analyses.Aerodynamics.Markup.Markup
settings (defined in SUAVE.Analyses.Aerodynamics.Markup.Markup)SUAVE.Analyses.Aerodynamics.Markup.Markup
tag (defined in SUAVE.Analyses.Aerodynamics.AERODAS.AERODAS)SUAVE.Analyses.Aerodynamics.AERODAS.AERODAS
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
evaluate(self, state)SUAVE.Analyses.Aerodynamics.Markup.Markup
SUAVE::Analyses::Analysis::Analysis.evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
SUAVE::Analyses::Analysis::Analysis.finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
geometry (defined in SUAVE.Analyses.Aerodynamics.Markup.Markup)SUAVE.Analyses.Aerodynamics.Markup.Markup
initialize(self)SUAVE.Analyses.Aerodynamics.Markup.Markup
SUAVE::Analyses::Aerodynamics::Aerodynamics::Aerodynamics.initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
process (defined in SUAVE.Analyses.Aerodynamics.Markup.Markup)SUAVE.Analyses.Aerodynamics.Markup.Markup
settings (defined in SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
tag (defined in SUAVE.Analyses.Aerodynamics.AERODAS.AERODAS)SUAVE.Analyses.Aerodynamics.AERODAS.AERODAS
@@ -120,7 +126,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AERODAS_1_1AERODAS.html b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AERODAS_1_1AERODAS.html index 79139661..5a2bfa93 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AERODAS_1_1AERODAS.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AERODAS_1_1AERODAS.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Aerodynamics.AERODAS.AERODAS Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@
- +
@@ -73,7 +78,9 @@
@@ -108,42 +115,32 @@ SUAVE.Analyses.Aerodynamics.Markup.Markup SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics SUAVE.Analyses.Analysis.Analysis - -
+ + - - - - - - - - - - - - - - - - - - - - + + + + + + + + + +

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Aerodynamics.Markup.Markup
def __defaults__ (self)
 
def evaluate (self, state)
 
def initialize (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
def __defaults__ (self)
 
def evaluate (self, state)
 
def finalize (self)
 
def compute_forces (self, conditions)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
@@ -157,9 +154,6 @@ - - @@ -226,6 +220,8 @@

SUAVE.Analyses.Aerodynamics.Markup.Markup.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL_1_1AVL-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL_1_1AVL-members.html index 920686ec..6475b14e 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL_1_1AVL-members.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL_1_1AVL-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Attributes

 geometry
 
settings
 
 process
 
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -98,22 +105,21 @@

This is the complete list of members for SUAVE.Analyses.Aerodynamics.AVL.AVL, including all inherited members.

- + - - - - - - - - - - - - - - + + + + + + + + + + + + +
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Aerodynamics.AVL.AVL
compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
compute_forces(self, conditions)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
evaluate(self, state)SUAVE.Analyses.Aerodynamics.Markup.Markup
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize (defined in SUAVE.Analyses.Aerodynamics.AVL.AVL)SUAVE.Analyses.Aerodynamics.AVL.AVLstatic
SUAVE::Analyses::Aerodynamics::Markup::Markup.finalize(self)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
geometry (defined in SUAVE.Analyses.Aerodynamics.Markup.Markup)SUAVE.Analyses.Aerodynamics.Markup.Markup
initialize(self)SUAVE.Analyses.Aerodynamics.AVL.AVL
SUAVE::Analyses::Aerodynamics::Aerodynamics::Aerodynamics.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
process (defined in SUAVE.Analyses.Aerodynamics.Markup.Markup)SUAVE.Analyses.Aerodynamics.Markup.Markup
settings (defined in SUAVE.Analyses.Aerodynamics.Markup.Markup)SUAVE.Analyses.Aerodynamics.Markup.Markup
tag (defined in SUAVE.Analyses.Aerodynamics.AVL.AVL)SUAVE.Analyses.Aerodynamics.AVL.AVL
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
evaluate(self, state)SUAVE.Analyses.Aerodynamics.Markup.Markup
SUAVE::Analyses::Analysis::Analysis.evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize (defined in SUAVE.Analyses.Aerodynamics.AVL.AVL)SUAVE.Analyses.Aerodynamics.AVL.AVLstatic
SUAVE::Analyses::Aerodynamics::Markup::Markup.finalize(self)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
SUAVE::Analyses::Analysis::Analysis.finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
geometry (defined in SUAVE.Analyses.Aerodynamics.Markup.Markup)SUAVE.Analyses.Aerodynamics.Markup.Markup
initialize(self)SUAVE.Analyses.Aerodynamics.AVL.AVL
SUAVE::Analyses::Aerodynamics::Aerodynamics::Aerodynamics.initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
process (defined in SUAVE.Analyses.Aerodynamics.Markup.Markup)SUAVE.Analyses.Aerodynamics.Markup.Markup
settings (defined in SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
tag (defined in SUAVE.Analyses.Aerodynamics.AVL.AVL)SUAVE.Analyses.Aerodynamics.AVL.AVL
@@ -121,7 +127,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL_1_1AVL.html b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL_1_1AVL.html index 7ee25b04..76758191 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL_1_1AVL.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL_1_1AVL.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Aerodynamics.AVL.AVL Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -109,8 +116,8 @@ SUAVE.Analyses.Aerodynamics.Markup.Markup SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics SUAVE.Analyses.Analysis.Analysis - -
+ + @@ -119,34 +126,22 @@ - - - - - - - - - - - - - - - - - - - - - - + + + + + + + + + +

Public Member Functions

def initialize (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Aerodynamics.Markup.Markup
def __defaults__ (self)
 
def evaluate (self, state)
 
def initialize (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
def __defaults__ (self)
 
def evaluate (self, state)
 
def finalize (self)
 
def compute_forces (self, conditions)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
@@ -160,9 +155,6 @@ - - @@ -234,6 +226,8 @@

SUAVE.Analyses.Aerodynamics.Markup.Markup.

+ @@ -268,6 +262,8 @@

SUAVE.Analyses.Aerodynamics.Markup.Markup.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL__Inviscid_1_1AVL__Inviscid-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL__Inviscid_1_1AVL__Inviscid-members.html index 10ed0252..397beac4 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL__Inviscid_1_1AVL__Inviscid-members.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL__Inviscid_1_1AVL__Inviscid-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Attributes

 geometry
 
settings
 
 process
 
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -99,32 +106,31 @@

This is the complete list of members for SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid, including all inherited members.

- - - + + + - - + + - - + + - - - - - - - - - + + + + + + + +
__defaults__(self)SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid
aerodynamics (defined in SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics)SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics
build_surrogate(self)SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid
compile(self)SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
aero_derivatives (defined in SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics)SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics
aerodynamics (defined in SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics)SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics
build_surrogate(self)SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid
current_status (defined in SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid)SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid
energies (defined in SUAVE.Analyses.Mission.Segments.Conditions.Basic.Basic)SUAVE.Analyses.Mission.Segments.Conditions.Basic.Basic
evaluate(self, state, settings, geometry)SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid
evaluate_conditions(self, run_conditions)SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid
expand_rows(self, rows)SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
evaluate_conditions(self, run_conditions, trim_aircraft)SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid
expand_rows(self, rows, override=False)SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
frames (defined in SUAVE.Analyses.Mission.Segments.Conditions.Basic.Basic)SUAVE.Analyses.Mission.Segments.Conditions.Basic.Basic
freestream (defined in SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics)SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics
geometry (defined in SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid)SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid
initialize(self)SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid
keep_files (defined in SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid)SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid
initialize(self, number_spanwise_vortices, number_chordwise_vortices, keep_files, save_regression_results, regression_flag, print_output, trim_aircraft, side_slip_angle, roll_rate_coefficient, pitch_rate_coefficient, lift_coefficient)SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid
noise (defined in SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics)SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics
ones_row(self, cols)SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
ones_row_m1(self, cols)SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
ones_row_m2(self, cols)SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
propulsion (defined in SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics)SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics
regression_flag (defined in SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid)SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid
sample_training(self)SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid
settings (defined in SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid)SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid
stability (defined in SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics)SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics
surrogates (defined in SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid)SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid
tag (defined in SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid)SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid
training (defined in SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid)SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid
training_file (defined in SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid)SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid
weights (defined in SUAVE.Analyses.Mission.Segments.Conditions.Basic.Basic)SUAVE.Analyses.Mission.Segments.Conditions.Basic.Basic
sample_training(self)SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid
settings (defined in SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid)SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid
stability (defined in SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics)SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics
surrogates (defined in SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid)SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid
tag (defined in SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid)SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid
training (defined in SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid)SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid
training_file (defined in SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid)SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid
weights (defined in SUAVE.Analyses.Mission.Segments.Conditions.Basic.Basic)SUAVE.Analyses.Mission.Segments.Conditions.Basic.Basic
@@ -132,7 +138,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL__Inviscid_1_1AVL__Inviscid.html b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL__Inviscid_1_1AVL__Inviscid.html index 7f424cae..66546c0c 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL__Inviscid_1_1AVL__Inviscid.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL__Inviscid_1_1AVL__Inviscid.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -108,29 +115,23 @@ SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics SUAVE.Analyses.Mission.Segments.Conditions.Basic.Basic SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions - -
+ + - - + + - - - - - - - - + + @@ -138,28 +139,23 @@ - - - - + +

Public Member Functions

def __defaults__ (self)
 
def initialize (self)
 
def initialize (self, number_spanwise_vortices, number_chordwise_vortices, keep_files, save_regression_results, regression_flag, print_output, trim_aircraft, side_slip_angle, roll_rate_coefficient, pitch_rate_coefficient, lift_coefficient)
 
def evaluate (self, state, settings, geometry)
 
def sample_training (self)
 
def build_surrogate (self)
 
def evaluate_conditions (self, run_conditions)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Conditions.Basic.Basic
def __defaults__ (self)
 
def evaluate_conditions (self, run_conditions, trim_aircraft)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
def ones_row (self, cols)
 
 
def ones_row_m2 (self, cols)
 
def expand_rows (self, rows)
 
def compile (self)
 
def expand_rows (self, rows, override=False)
 
- - - - + + @@ -169,9 +165,6 @@ - - @@ -185,9 +178,15 @@ + + + + @@ -201,6 +200,9 @@ + +

Public Attributes

 tag
 
keep_files
 
settings
 
 current_status
 
 geometry
 
settings
 
 training
 
 surrogates
 
regression_flag
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics
 tag
 stability
 
aero_derivatives
 
 propulsion
 
noise
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Conditions.Basic.Basic
 tag
 energies
 
noise
 

Detailed Description

This builds a surrogate and computes lift using AVL.
@@ -243,6 +245,8 @@ 

SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics.

+

@@ -261,23 +265,20 @@

Builds a surrogate based on sample evalations using a Guassian process.
-
 Assumptions:
 None
-
 Source:
 N/A
-
 Inputs:
 self.training.
-  coefficients     [-] CL and CD
-  grid_points      [radians,-] angles of attack and mach numbers 
-
+  coefficients             [-] CL and CD
+  span efficiency factor   [-] e 
+  grid_points              [radians,-] angles of attack and Mach numbers 
 Outputs:
 self.surrogates.
-  lift_coefficient <Guassian process surrogate>
-  drag_coefficient <Guassian process surrogate>
-
+  lift_coefficient        
+  drag_coefficient        
+  span_efficiency_factor  
 Properties Used:
 No others
 
@@ -336,16 +337,17 @@

-

◆ evaluate_conditions()

+ +

◆ evaluate_conditions()

@@ -360,7 +362,13 @@

  - run_conditions  + run_conditions, + + + + +   + trim_aircraft  @@ -399,8 +407,8 @@

-

◆ initialize()

+ +

◆ initialize()

diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL__Inviscid_1_1AVL__Inviscid.js b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL__Inviscid_1_1AVL__Inviscid.js index 06bdc6a9..fd051160 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL__Inviscid_1_1AVL__Inviscid.js +++ b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL__Inviscid_1_1AVL__Inviscid.js @@ -3,13 +3,11 @@ var classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL__Inviscid_1_1AVL__Inviscid = [ "__defaults__", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL__Inviscid_1_1AVL__Inviscid.html#a2674aeb739fbede3df8174cc5971117c", null ], [ "build_surrogate", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL__Inviscid_1_1AVL__Inviscid.html#aa2a251b450d7a8bad81203841b9367e8", null ], [ "evaluate", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL__Inviscid_1_1AVL__Inviscid.html#a5239bbcd5e0f5bcef56f07626ff903d5", null ], - [ "evaluate_conditions", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL__Inviscid_1_1AVL__Inviscid.html#a55e806c99124a4651a2bd74cd27b73a2", null ], - [ "initialize", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL__Inviscid_1_1AVL__Inviscid.html#a2c9bfba28deb4c834ead25ce3af9ba01", null ], + [ "evaluate_conditions", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL__Inviscid_1_1AVL__Inviscid.html#af20601d3fc0173ea8ab26791ff404715", null ], + [ "initialize", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL__Inviscid_1_1AVL__Inviscid.html#a52cae32f61a9a15c3a20f661e1e46a36", null ], [ "sample_training", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL__Inviscid_1_1AVL__Inviscid.html#a8a56e051851235864dc8839d57ed9023", null ], [ "current_status", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL__Inviscid_1_1AVL__Inviscid.html#ad8d7881165eb8c63bd430a38f1f38a21", null ], [ "geometry", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL__Inviscid_1_1AVL__Inviscid.html#ab3413e0de53e813c992c5693fe668c9b", null ], - [ "keep_files", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL__Inviscid_1_1AVL__Inviscid.html#ac204dd9a499b67b481b39e4e8a5db082", null ], - [ "regression_flag", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL__Inviscid_1_1AVL__Inviscid.html#ad1c94fdf93f1b71429a2988e70af7d0c", null ], [ "settings", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL__Inviscid_1_1AVL__Inviscid.html#a2bc68b59e7ead5a51ef3ab08c738b5fb", null ], [ "surrogates", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL__Inviscid_1_1AVL__Inviscid.html#a8b545d9a8168b3ae0da29f0319dc3b44", null ], [ "tag", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1AVL__Inviscid_1_1AVL__Inviscid.html#a9bdf600c35e259c1a8b4a7f79628dcf0", null ], diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Aerodynamics_1_1Aerodynamics-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Aerodynamics_1_1Aerodynamics-members.html index 4cdc1236..1834d9c9 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Aerodynamics_1_1Aerodynamics-members.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Aerodynamics_1_1Aerodynamics-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@
- +

@@ -73,7 +78,9 @@
@@ -98,19 +105,18 @@

This is the complete list of members for SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics, including all inherited members.

- + - - - - - - - - - - - + + + + + + + + + +
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
compute_forces(self, conditions)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
evaluate(self, state)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
geometry (defined in SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
settings (defined in SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
tag (defined in SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
evaluate(self, state)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
SUAVE::Analyses::Analysis::Analysis.evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
SUAVE::Analyses::Analysis::Analysis.finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
geometry (defined in SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
settings (defined in SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
tag (defined in SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
@@ -118,7 +124,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Aerodynamics_1_1Aerodynamics.html b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Aerodynamics_1_1Aerodynamics.html index badbdf92..0d4bf1b5 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Aerodynamics_1_1Aerodynamics.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Aerodynamics_1_1Aerodynamics.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -118,8 +125,8 @@ SUAVE.Analyses.Aerodynamics.SU2_Euler_Super.SU2_Euler_Super SUAVE.Analyses.Aerodynamics.Supersonic_OpenVSP_Wave_Drag.Supersonic_OpenVSP_Wave_Drag SUAVE.Analyses.Aerodynamics.Supersonic_Zero.Supersonic_Zero - -
+ + @@ -129,21 +136,17 @@ - - - - - - - - - - - - - - + + + + + + + + + +

Public Member Functions

 
def finalize (self)
 
def compute_forces (self, conditions)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
@@ -209,56 +212,10 @@

-

◆ compute_forces()

- -
-
-

Public Attributes

- - - - - - - - - - - - - - - - - -
def SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics.compute_forces ( self,
 conditions 
)
- @@ -303,6 +260,8 @@

SUAVE.Analyses.Aerodynamics.Markup.Markup.

+ @@ -350,7 +309,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Aerodynamics_1_1Aerodynamics.js b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Aerodynamics_1_1Aerodynamics.js index 02c203b0..aeb2d143 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Aerodynamics_1_1Aerodynamics.js +++ b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Aerodynamics_1_1Aerodynamics.js @@ -1,7 +1,6 @@ var classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Aerodynamics_1_1Aerodynamics = [ [ "__defaults__", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Aerodynamics_1_1Aerodynamics.html#a102129619dc160ce8f979301029b3921", null ], - [ "compute_forces", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Aerodynamics_1_1Aerodynamics.html#a6702f0aabc084054884871464a89261b", null ], [ "evaluate", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Aerodynamics_1_1Aerodynamics.html#a9684f9fe2c620a8715c73a4a43319fa1", null ], [ "finalize", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Aerodynamics_1_1Aerodynamics.html#afc822038b10ccbcb3cefdb1a416d137f", null ], [ "geometry", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Aerodynamics_1_1Aerodynamics.html#a1d2366be5c23f5d574e37280b708e67b", null ], diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Fidelity__Zero_1_1Fidelity__Zero-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Fidelity__Zero_1_1Fidelity__Zero-members.html index d69aef59..a7a158b6 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Fidelity__Zero_1_1Fidelity__Zero-members.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Fidelity__Zero_1_1Fidelity__Zero-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -98,21 +105,20 @@

This is the complete list of members for SUAVE.Analyses.Aerodynamics.Fidelity_Zero.Fidelity_Zero, including all inherited members.

- + - - - - - - - - - - - - - + + + + + + + + + + + +
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Aerodynamics.Fidelity_Zero.Fidelity_Zero
compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
compute_forces(self, conditions)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
evaluate(self, state)SUAVE.Analyses.Aerodynamics.Markup.Markup
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
geometry (defined in SUAVE.Analyses.Aerodynamics.Markup.Markup)SUAVE.Analyses.Aerodynamics.Markup.Markup
initialize(self)SUAVE.Analyses.Aerodynamics.Fidelity_Zero.Fidelity_Zero
SUAVE::Analyses::Aerodynamics::Aerodynamics::Aerodynamics.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
process (defined in SUAVE.Analyses.Aerodynamics.Markup.Markup)SUAVE.Analyses.Aerodynamics.Markup.Markup
settings (defined in SUAVE.Analyses.Aerodynamics.Markup.Markup)SUAVE.Analyses.Aerodynamics.Markup.Markup
tag (defined in SUAVE.Analyses.Aerodynamics.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Aerodynamics.Fidelity_Zero.Fidelity_Zero
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
evaluate(self, state)SUAVE.Analyses.Aerodynamics.Markup.Markup
SUAVE::Analyses::Analysis::Analysis.evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
SUAVE::Analyses::Analysis::Analysis.finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
geometry (defined in SUAVE.Analyses.Aerodynamics.Markup.Markup)SUAVE.Analyses.Aerodynamics.Markup.Markup
initialize(self)SUAVE.Analyses.Aerodynamics.Fidelity_Zero.Fidelity_Zero
SUAVE::Analyses::Aerodynamics::Aerodynamics::Aerodynamics.initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
process (defined in SUAVE.Analyses.Aerodynamics.Markup.Markup)SUAVE.Analyses.Aerodynamics.Markup.Markup
settings (defined in SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
tag (defined in SUAVE.Analyses.Aerodynamics.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Aerodynamics.Fidelity_Zero.Fidelity_Zero
@@ -120,7 +126,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Fidelity__Zero_1_1Fidelity__Zero.html b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Fidelity__Zero_1_1Fidelity__Zero.html index 3e50c2b9..6514d17c 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Fidelity__Zero_1_1Fidelity__Zero.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Fidelity__Zero_1_1Fidelity__Zero.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Aerodynamics.Fidelity_Zero.Fidelity_Zero Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -108,8 +115,8 @@ SUAVE.Analyses.Aerodynamics.Markup.Markup SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics SUAVE.Analyses.Analysis.Analysis - -
+ + @@ -118,34 +125,22 @@ - - - - - - - - - - - - - - - - - - - - - - + + + + + + + + + +

Public Member Functions

def initialize (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Aerodynamics.Markup.Markup
def __defaults__ (self)
 
def evaluate (self, state)
 
def initialize (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
def __defaults__ (self)
 
def evaluate (self, state)
 
def finalize (self)
 
def compute_forces (self, conditions)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
@@ -159,9 +154,6 @@ - - @@ -227,6 +219,8 @@

SUAVE.Analyses.Aerodynamics.Markup.Markup.

+ @@ -261,6 +255,8 @@

SUAVE.Analyses.Aerodynamics.Markup.Markup.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Lifting__Line_1_1Lifting__Line-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Lifting__Line_1_1Lifting__Line-members.html index 1ff3b14a..79774a22 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Lifting__Line_1_1Lifting__Line-members.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Lifting__Line_1_1Lifting__Line-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Attributes

 geometry
 
settings
 
 process
 
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -98,25 +105,24 @@

This is the complete list of members for SUAVE.Analyses.Aerodynamics.Lifting_Line.Lifting_Line, including all inherited members.

- + - - - - - - - - - - - - - - - - + + + + + + + + + + + + + + +
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Aerodynamics.Lifting_Line.Lifting_Line
build_surrogate(self)SUAVE.Analyses.Aerodynamics.Lifting_Line.Lifting_Line
compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
compute_forces(self, conditions)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
evaluate(self, state, settings, geometry)SUAVE.Analyses.Aerodynamics.Lifting_Line.Lifting_Line
SUAVE::Analyses::Aerodynamics::Aerodynamics::Aerodynamics.evaluate(self, state)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
geometry (defined in SUAVE.Analyses.Aerodynamics.Lifting_Line.Lifting_Line)SUAVE.Analyses.Aerodynamics.Lifting_Line.Lifting_Line
initialize(self)SUAVE.Analyses.Aerodynamics.Lifting_Line.Lifting_Line
SUAVE::Analyses::Aerodynamics::Aerodynamics::Aerodynamics.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
sample_training(self)SUAVE.Analyses.Aerodynamics.Lifting_Line.Lifting_Line
settings (defined in SUAVE.Analyses.Aerodynamics.Lifting_Line.Lifting_Line)SUAVE.Analyses.Aerodynamics.Lifting_Line.Lifting_Line
surrogates (defined in SUAVE.Analyses.Aerodynamics.Lifting_Line.Lifting_Line)SUAVE.Analyses.Aerodynamics.Lifting_Line.Lifting_Line
tag (defined in SUAVE.Analyses.Aerodynamics.Lifting_Line.Lifting_Line)SUAVE.Analyses.Aerodynamics.Lifting_Line.Lifting_Line
training (defined in SUAVE.Analyses.Aerodynamics.Lifting_Line.Lifting_Line)SUAVE.Analyses.Aerodynamics.Lifting_Line.Lifting_Line
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
evaluate(self, state, settings, geometry)SUAVE.Analyses.Aerodynamics.Lifting_Line.Lifting_Line
SUAVE::Analyses::Aerodynamics::Aerodynamics::Aerodynamics.evaluate(self, state)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
SUAVE::Analyses::Analysis::Analysis.evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
SUAVE::Analyses::Analysis::Analysis.finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
geometry (defined in SUAVE.Analyses.Aerodynamics.Lifting_Line.Lifting_Line)SUAVE.Analyses.Aerodynamics.Lifting_Line.Lifting_Line
initialize(self, use_surrogate, n_sw, n_cw, propeller_wake_model, mf, mn, dcs)SUAVE.Analyses.Aerodynamics.Lifting_Line.Lifting_Line
SUAVE::Analyses::Aerodynamics::Aerodynamics::Aerodynamics.initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
sample_training(self)SUAVE.Analyses.Aerodynamics.Lifting_Line.Lifting_Line
settings (defined in SUAVE.Analyses.Aerodynamics.Lifting_Line.Lifting_Line)SUAVE.Analyses.Aerodynamics.Lifting_Line.Lifting_Line
surrogates (defined in SUAVE.Analyses.Aerodynamics.Lifting_Line.Lifting_Line)SUAVE.Analyses.Aerodynamics.Lifting_Line.Lifting_Line
tag (defined in SUAVE.Analyses.Aerodynamics.Lifting_Line.Lifting_Line)SUAVE.Analyses.Aerodynamics.Lifting_Line.Lifting_Line
training (defined in SUAVE.Analyses.Aerodynamics.Lifting_Line.Lifting_Line)SUAVE.Analyses.Aerodynamics.Lifting_Line.Lifting_Line
@@ -124,7 +130,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Lifting__Line_1_1Lifting__Line.html b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Lifting__Line_1_1Lifting__Line.html index 841da0e1..1ef4a9b6 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Lifting__Line_1_1Lifting__Line.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Lifting__Line_1_1Lifting__Line.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Aerodynamics.Lifting_Line.Lifting_Line Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -107,15 +114,15 @@ SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics SUAVE.Analyses.Analysis.Analysis - -
+ + - - + + @@ -123,27 +130,21 @@ - - - - - - - - - - - - - - - - + + + + + + + + + +

Public Member Functions

def __defaults__ (self)
 
def initialize (self)
 
def initialize (self, use_surrogate, n_sw, n_cw, propeller_wake_model, mf, mn, dcs)
 
def evaluate (self, state, settings, geometry)
 
def sample_training (self)
def build_surrogate (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
def __defaults__ (self)
 
def evaluate (self, state)
 
def finalize (self)
 
def compute_forces (self, conditions)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
@@ -224,6 +225,8 @@

SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics.

+ @@ -263,6 +266,8 @@

-

◆ initialize()

+ +

◆ initialize()

- + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +

Public Attributes

(  self)self,
 use_surrogate,
 n_sw,
 n_cw,
 propeller_wake_model,
 mf,
 mn,
 dcs 
)
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Lifting__Line_1_1Lifting__Line.js b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Lifting__Line_1_1Lifting__Line.js index 2624c0ed..ecf95833 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Lifting__Line_1_1Lifting__Line.js +++ b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Lifting__Line_1_1Lifting__Line.js @@ -3,7 +3,7 @@ var classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Lifting__Line_1_1Lifting__Line = [ "__defaults__", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Lifting__Line_1_1Lifting__Line.html#abc3ceb23a334289decd8250a64881afa", null ], [ "build_surrogate", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Lifting__Line_1_1Lifting__Line.html#a0e018378b71e78bff538a63240cdfbf5", null ], [ "evaluate", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Lifting__Line_1_1Lifting__Line.html#aa30085741f0c13bd0dbbd791143ce8da", null ], - [ "initialize", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Lifting__Line_1_1Lifting__Line.html#a24eef2a2fd44e3c63b79c37d459b5093", null ], + [ "initialize", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Lifting__Line_1_1Lifting__Line.html#a2fcec3d2ae76562440b15041e0ddf04f", null ], [ "sample_training", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Lifting__Line_1_1Lifting__Line.html#a9d59f0ce54639d4ed61e8b57b46cfd0f", null ], [ "geometry", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Lifting__Line_1_1Lifting__Line.html#ae80fbcc2cd5c3e91f1df6b3a78370a94", null ], [ "settings", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Lifting__Line_1_1Lifting__Line.html#a0977b1b2a920ad1a843555615f9aa3e8", null ], diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Markup_1_1Markup-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Markup_1_1Markup-members.html index 3a7aef03..fa71cd61 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Markup_1_1Markup-members.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Markup_1_1Markup-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -98,21 +105,20 @@

This is the complete list of members for SUAVE.Analyses.Aerodynamics.Markup.Markup, including all inherited members.

- + - - - - - - - - - - - - - + + + + + + + + + + + +
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Aerodynamics.Markup.Markup
compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
compute_forces(self, conditions)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
evaluate(self, state)SUAVE.Analyses.Aerodynamics.Markup.Markup
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
geometry (defined in SUAVE.Analyses.Aerodynamics.Markup.Markup)SUAVE.Analyses.Aerodynamics.Markup.Markup
initialize(self)SUAVE.Analyses.Aerodynamics.Markup.Markup
SUAVE::Analyses::Aerodynamics::Aerodynamics::Aerodynamics.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
process (defined in SUAVE.Analyses.Aerodynamics.Markup.Markup)SUAVE.Analyses.Aerodynamics.Markup.Markup
settings (defined in SUAVE.Analyses.Aerodynamics.Markup.Markup)SUAVE.Analyses.Aerodynamics.Markup.Markup
tag (defined in SUAVE.Analyses.Aerodynamics.Markup.Markup)SUAVE.Analyses.Aerodynamics.Markup.Markup
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
evaluate(self, state)SUAVE.Analyses.Aerodynamics.Markup.Markup
SUAVE::Analyses::Analysis::Analysis.evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
SUAVE::Analyses::Analysis::Analysis.finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
geometry (defined in SUAVE.Analyses.Aerodynamics.Markup.Markup)SUAVE.Analyses.Aerodynamics.Markup.Markup
initialize(self)SUAVE.Analyses.Aerodynamics.Markup.Markup
SUAVE::Analyses::Aerodynamics::Aerodynamics::Aerodynamics.initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
process (defined in SUAVE.Analyses.Aerodynamics.Markup.Markup)SUAVE.Analyses.Aerodynamics.Markup.Markup
settings (defined in SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
tag (defined in SUAVE.Analyses.Aerodynamics.Markup.Markup)SUAVE.Analyses.Aerodynamics.Markup.Markup
@@ -120,7 +126,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Markup_1_1Markup.html b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Markup_1_1Markup.html index 018122f9..6bfde685 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Markup_1_1Markup.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Markup_1_1Markup.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Aerodynamics.Markup.Markup Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -114,8 +121,8 @@ SUAVE.Analyses.Aerodynamics.SU2_Euler_Super.SU2_Euler_Super SUAVE.Analyses.Aerodynamics.Supersonic_OpenVSP_Wave_Drag.Supersonic_OpenVSP_Wave_Drag SUAVE.Analyses.Aerodynamics.Supersonic_Zero.Supersonic_Zero - -
+ + @@ -126,27 +133,19 @@ - - - - - - - - - - - - - - - - - - + + + + + + + + + +

Public Member Functions

def initialize (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
def __defaults__ (self)
 
def evaluate (self, state)
 
def finalize (self)
 
def compute_forces (self, conditions)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
@@ -156,9 +155,6 @@ - - @@ -224,6 +220,10 @@

SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics.

+ +

Reimplemented in SUAVE.Analyses.Aerodynamics.SU2_Euler_Super.SU2_Euler_Super, SUAVE.Analyses.Aerodynamics.SU2_Euler.SU2_Euler, SUAVE.Analyses.Aerodynamics.Fidelity_Zero.Fidelity_Zero, SUAVE.Analyses.Aerodynamics.Supersonic_OpenVSP_Wave_Drag.Supersonic_OpenVSP_Wave_Drag, SUAVE.Analyses.Aerodynamics.Supersonic_Zero.Supersonic_Zero, SUAVE.Analyses.Aerodynamics.AVL.AVL, and SUAVE.Analyses.Aerodynamics.AERODAS.AERODAS.

+ @@ -269,6 +269,8 @@

SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics.

+ @@ -303,6 +305,8 @@

SUAVE.Analyses.Aerodynamics.Supersonic_Zero.Supersonic_Zero, SUAVE.Analyses.Aerodynamics.Fidelity_Zero.Fidelity_Zero, SUAVE.Analyses.Aerodynamics.AVL.AVL, SUAVE.Analyses.Aerodynamics.SU2_Euler.SU2_Euler, SUAVE.Analyses.Aerodynamics.SU2_Euler_Super.SU2_Euler_Super, and SUAVE.Analyses.Aerodynamics.Supersonic_OpenVSP_Wave_Drag.Supersonic_OpenVSP_Wave_Drag.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Markup_1_1Markup.js b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Markup_1_1Markup.js index d2773ef7..aaa40e62 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Markup_1_1Markup.js +++ b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Markup_1_1Markup.js @@ -5,6 +5,5 @@ var classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Markup_1_1Markup = [ "initialize", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Markup_1_1Markup.html#ae245433bcbe8036e917c4f0b4d21f7d2", null ], [ "geometry", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Markup_1_1Markup.html#a665085a816238c4015570a5b7a960791", null ], [ "process", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Markup_1_1Markup.html#ab4fdd63d93a0248bd487e6e9626bf3c3", null ], - [ "settings", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Markup_1_1Markup.html#a48fb50f5fb9852e928eb6e3161e03b97", null ], [ "tag", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Markup_1_1Markup.html#a73c36817237275ada1b38de1b17f647b", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Process__Geometry_1_1Process__Geometry-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Process__Geometry_1_1Process__Geometry-members.html index 54fe0111..e507f69b 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Process__Geometry_1_1Process__Geometry-members.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Process__Geometry_1_1Process__Geometry-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Attributes

 geometry
 
settings
 
 process
 
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -111,7 +118,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Process__Geometry_1_1Process__Geometry.html b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Process__Geometry_1_1Process__Geometry.html index 197abb9a..a7c19f7a 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Process__Geometry_1_1Process__Geometry.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Process__Geometry_1_1Process__Geometry.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Aerodynamics.Process_Geometry.Process_Geometry Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -106,8 +113,8 @@ SUAVE.Analyses.Process.Process - -
+ + @@ -116,10 +123,10 @@ - - - - + + + +

Public Member Functions

def evaluate (self, state, settings, geometry)
 
- Public Member Functions inherited from SUAVE.Analyses.Process.Process
def evaluate (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def evaluate (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
@@ -254,7 +261,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Results_1_1Results-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Results_1_1Results-members.html deleted file mode 100644 index bb677baf..00000000 --- a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Results_1_1Results-members.html +++ /dev/null @@ -1,117 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
-

Static Public Attributes

- - - - - - - -
-
SUAVE -  1.1.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
- - - - - -
- -
-
-
- -
- -
-
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SUAVE.Analyses.Aerodynamics.Results.Results Member List
-
- -
- - - - diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Results_1_1Results.html b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Results_1_1Results.html deleted file mode 100644 index 788b3a47..00000000 --- a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Results_1_1Results.html +++ /dev/null @@ -1,189 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Aerodynamics.Results.Results Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.1.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
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- -
- -
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- -
- -
- -
-
SUAVE.Analyses.Aerodynamics.Results.Results Class Reference
-
-
-
-Inheritance diagram for SUAVE.Analyses.Aerodynamics.Results.Results:
-
-
- - - -
- - - - -

-Public Member Functions

def __defaults__ (self)
 
- - - - - - - - - -

-Public Attributes

lift_coefficient
 
drag_coefficient
 
lift_force_vector
 
drag_force_vector
 
-

Detailed Description

-
A class for storing aerodynamic results.
-
-Assumptions:
-None
-
-Source:
-N/A
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Aerodynamics.Results.Results.__defaults__ ( self)
-
-
This sets the default values for the results.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Analyses/Aerodynamics/Results.py
  • -
-
-
- - - - diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Results_1_1Results.js b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Results_1_1Results.js deleted file mode 100644 index 9019bdc7..00000000 --- a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Results_1_1Results.js +++ /dev/null @@ -1,8 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Results_1_1Results = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Results_1_1Results.html#a6551eed89371b92d55be76da3790a0ad", null ], - [ "drag_coefficient", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Results_1_1Results.html#a6365a549c4318ab31ee88413aee9db73", null ], - [ "drag_force_vector", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Results_1_1Results.html#aaeb551a3283ce47264ab96346139747f", null ], - [ "lift_coefficient", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Results_1_1Results.html#a3bb03ae797eb7dd2284c87bc3460a410", null ], - [ "lift_force_vector", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Results_1_1Results.html#a9c4f578990cf7afea65efed34822885e", null ] -]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Results_1_1Results.png b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Results_1_1Results.png deleted file mode 100644 index 6bd7195a..00000000 Binary files a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Results_1_1Results.png and /dev/null differ diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__Euler_1_1SU2__Euler-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__Euler_1_1SU2__Euler-members.html index eb145deb..6c0efbfe 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__Euler_1_1SU2__Euler-members.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__Euler_1_1SU2__Euler-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -98,21 +105,20 @@

This is the complete list of members for SUAVE.Analyses.Aerodynamics.SU2_Euler.SU2_Euler, including all inherited members.

- + - - - - - - - - - - - - - + + + + + + + + + + + +
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Aerodynamics.SU2_Euler.SU2_Euler
compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
compute_forces(self, conditions)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
evaluate(self, state)SUAVE.Analyses.Aerodynamics.Markup.Markup
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
geometry (defined in SUAVE.Analyses.Aerodynamics.Markup.Markup)SUAVE.Analyses.Aerodynamics.Markup.Markup
initialize(self)SUAVE.Analyses.Aerodynamics.SU2_Euler.SU2_Euler
SUAVE::Analyses::Aerodynamics::Aerodynamics::Aerodynamics.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
process (defined in SUAVE.Analyses.Aerodynamics.Markup.Markup)SUAVE.Analyses.Aerodynamics.Markup.Markup
settings (defined in SUAVE.Analyses.Aerodynamics.Markup.Markup)SUAVE.Analyses.Aerodynamics.Markup.Markup
tag (defined in SUAVE.Analyses.Aerodynamics.SU2_Euler.SU2_Euler)SUAVE.Analyses.Aerodynamics.SU2_Euler.SU2_Euler
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
evaluate(self, state)SUAVE.Analyses.Aerodynamics.Markup.Markup
SUAVE::Analyses::Analysis::Analysis.evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
SUAVE::Analyses::Analysis::Analysis.finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
geometry (defined in SUAVE.Analyses.Aerodynamics.Markup.Markup)SUAVE.Analyses.Aerodynamics.Markup.Markup
initialize(self)SUAVE.Analyses.Aerodynamics.SU2_Euler.SU2_Euler
SUAVE::Analyses::Aerodynamics::Aerodynamics::Aerodynamics.initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
process (defined in SUAVE.Analyses.Aerodynamics.Markup.Markup)SUAVE.Analyses.Aerodynamics.Markup.Markup
settings (defined in SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
tag (defined in SUAVE.Analyses.Aerodynamics.SU2_Euler.SU2_Euler)SUAVE.Analyses.Aerodynamics.SU2_Euler.SU2_Euler
@@ -120,7 +126,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__Euler_1_1SU2__Euler.html b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__Euler_1_1SU2__Euler.html index 18405e92..57c3b03b 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__Euler_1_1SU2__Euler.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__Euler_1_1SU2__Euler.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Aerodynamics.SU2_Euler.SU2_Euler Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -108,8 +115,8 @@ SUAVE.Analyses.Aerodynamics.Markup.Markup SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics SUAVE.Analyses.Analysis.Analysis - -
+ + @@ -118,34 +125,22 @@ - - - - - - - - - - - - - - - - - - - - - - + + + + + + + + + +

Public Member Functions

def initialize (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Aerodynamics.Markup.Markup
def __defaults__ (self)
 
def evaluate (self, state)
 
def initialize (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
def __defaults__ (self)
 
def evaluate (self, state)
 
def finalize (self)
 
def compute_forces (self, conditions)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
@@ -159,9 +154,6 @@ - - @@ -227,6 +219,8 @@

SUAVE.Analyses.Aerodynamics.Markup.Markup.

+ @@ -267,6 +261,8 @@

SUAVE.Analyses.Aerodynamics.Markup.Markup.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__Euler__Super_1_1SU2__Euler__Super-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__Euler__Super_1_1SU2__Euler__Super-members.html index 4670581e..9599996b 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__Euler__Super_1_1SU2__Euler__Super-members.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__Euler__Super_1_1SU2__Euler__Super-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Attributes

 geometry
 
settings
 
 process
 
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -98,21 +105,20 @@

This is the complete list of members for SUAVE.Analyses.Aerodynamics.SU2_Euler_Super.SU2_Euler_Super, including all inherited members.

- + - - - - - - - - - - - - - + + + + + + + + + + + +
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Aerodynamics.SU2_Euler_Super.SU2_Euler_Super
compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
compute_forces(self, conditions)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
evaluate(self, state)SUAVE.Analyses.Aerodynamics.Markup.Markup
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
geometry (defined in SUAVE.Analyses.Aerodynamics.Markup.Markup)SUAVE.Analyses.Aerodynamics.Markup.Markup
initialize(self)SUAVE.Analyses.Aerodynamics.SU2_Euler_Super.SU2_Euler_Super
SUAVE::Analyses::Aerodynamics::Aerodynamics::Aerodynamics.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
process (defined in SUAVE.Analyses.Aerodynamics.Markup.Markup)SUAVE.Analyses.Aerodynamics.Markup.Markup
settings (defined in SUAVE.Analyses.Aerodynamics.Markup.Markup)SUAVE.Analyses.Aerodynamics.Markup.Markup
tag (defined in SUAVE.Analyses.Aerodynamics.SU2_Euler_Super.SU2_Euler_Super)SUAVE.Analyses.Aerodynamics.SU2_Euler_Super.SU2_Euler_Super
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
evaluate(self, state)SUAVE.Analyses.Aerodynamics.Markup.Markup
SUAVE::Analyses::Analysis::Analysis.evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
SUAVE::Analyses::Analysis::Analysis.finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
geometry (defined in SUAVE.Analyses.Aerodynamics.Markup.Markup)SUAVE.Analyses.Aerodynamics.Markup.Markup
initialize(self)SUAVE.Analyses.Aerodynamics.SU2_Euler_Super.SU2_Euler_Super
SUAVE::Analyses::Aerodynamics::Aerodynamics::Aerodynamics.initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
process (defined in SUAVE.Analyses.Aerodynamics.Markup.Markup)SUAVE.Analyses.Aerodynamics.Markup.Markup
settings (defined in SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
tag (defined in SUAVE.Analyses.Aerodynamics.SU2_Euler_Super.SU2_Euler_Super)SUAVE.Analyses.Aerodynamics.SU2_Euler_Super.SU2_Euler_Super
@@ -120,7 +126,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__Euler__Super_1_1SU2__Euler__Super.html b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__Euler__Super_1_1SU2__Euler__Super.html index 08cba358..58494777 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__Euler__Super_1_1SU2__Euler__Super.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__Euler__Super_1_1SU2__Euler__Super.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Aerodynamics.SU2_Euler_Super.SU2_Euler_Super Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -108,8 +115,8 @@ SUAVE.Analyses.Aerodynamics.Markup.Markup SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics SUAVE.Analyses.Analysis.Analysis - -
+ + @@ -118,34 +125,22 @@ - - - - - - - - - - - - - - - - - - - - - - + + + + + + + + + +

Public Member Functions

def initialize (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Aerodynamics.Markup.Markup
def __defaults__ (self)
 
def evaluate (self, state)
 
def initialize (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
def __defaults__ (self)
 
def evaluate (self, state)
 
def finalize (self)
 
def compute_forces (self, conditions)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
@@ -159,9 +154,6 @@ - - @@ -227,6 +219,8 @@

SUAVE.Analyses.Aerodynamics.Markup.Markup.

+ @@ -267,6 +261,8 @@

SUAVE.Analyses.Aerodynamics.Markup.Markup.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__inviscid_1_1SU2__inviscid-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__inviscid_1_1SU2__inviscid-members.html index 6a5d5ee1..242cb2f5 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__inviscid_1_1SU2__inviscid-members.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__inviscid_1_1SU2__inviscid-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Attributes

 geometry
 
settings
 
 process
 
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -98,26 +105,25 @@

This is the complete list of members for SUAVE.Analyses.Aerodynamics.SU2_inviscid.SU2_inviscid, including all inherited members.

- + - - - - - - - - - - - - - - - - - + + + + + + + + + + + + + + + +
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Aerodynamics.SU2_inviscid.SU2_inviscid
build_surrogate(self)SUAVE.Analyses.Aerodynamics.SU2_inviscid.SU2_inviscid
compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
compute_forces(self, conditions)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
evaluate(self, state, settings, geometry)SUAVE.Analyses.Aerodynamics.SU2_inviscid.SU2_inviscid
SUAVE::Analyses::Aerodynamics::Aerodynamics::Aerodynamics.evaluate(self, state)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
geometry (defined in SUAVE.Analyses.Aerodynamics.SU2_inviscid.SU2_inviscid)SUAVE.Analyses.Aerodynamics.SU2_inviscid.SU2_inviscid
initialize(self)SUAVE.Analyses.Aerodynamics.SU2_inviscid.SU2_inviscid
SUAVE::Analyses::Aerodynamics::Aerodynamics::Aerodynamics.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
sample_training(self)SUAVE.Analyses.Aerodynamics.SU2_inviscid.SU2_inviscid
settings (defined in SUAVE.Analyses.Aerodynamics.SU2_inviscid.SU2_inviscid)SUAVE.Analyses.Aerodynamics.SU2_inviscid.SU2_inviscid
surrogates (defined in SUAVE.Analyses.Aerodynamics.SU2_inviscid.SU2_inviscid)SUAVE.Analyses.Aerodynamics.SU2_inviscid.SU2_inviscid
tag (defined in SUAVE.Analyses.Aerodynamics.SU2_inviscid.SU2_inviscid)SUAVE.Analyses.Aerodynamics.SU2_inviscid.SU2_inviscid
training (defined in SUAVE.Analyses.Aerodynamics.SU2_inviscid.SU2_inviscid)SUAVE.Analyses.Aerodynamics.SU2_inviscid.SU2_inviscid
training_file (defined in SUAVE.Analyses.Aerodynamics.SU2_inviscid.SU2_inviscid)SUAVE.Analyses.Aerodynamics.SU2_inviscid.SU2_inviscid
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
evaluate(self, state, settings, geometry)SUAVE.Analyses.Aerodynamics.SU2_inviscid.SU2_inviscid
SUAVE::Analyses::Aerodynamics::Aerodynamics::Aerodynamics.evaluate(self, state)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
SUAVE::Analyses::Analysis::Analysis.evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
SUAVE::Analyses::Analysis::Analysis.finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
geometry (defined in SUAVE.Analyses.Aerodynamics.SU2_inviscid.SU2_inviscid)SUAVE.Analyses.Aerodynamics.SU2_inviscid.SU2_inviscid
initialize(self)SUAVE.Analyses.Aerodynamics.SU2_inviscid.SU2_inviscid
SUAVE::Analyses::Aerodynamics::Aerodynamics::Aerodynamics.initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
sample_training(self)SUAVE.Analyses.Aerodynamics.SU2_inviscid.SU2_inviscid
settings (defined in SUAVE.Analyses.Aerodynamics.SU2_inviscid.SU2_inviscid)SUAVE.Analyses.Aerodynamics.SU2_inviscid.SU2_inviscid
surrogates (defined in SUAVE.Analyses.Aerodynamics.SU2_inviscid.SU2_inviscid)SUAVE.Analyses.Aerodynamics.SU2_inviscid.SU2_inviscid
tag (defined in SUAVE.Analyses.Aerodynamics.SU2_inviscid.SU2_inviscid)SUAVE.Analyses.Aerodynamics.SU2_inviscid.SU2_inviscid
training (defined in SUAVE.Analyses.Aerodynamics.SU2_inviscid.SU2_inviscid)SUAVE.Analyses.Aerodynamics.SU2_inviscid.SU2_inviscid
training_file (defined in SUAVE.Analyses.Aerodynamics.SU2_inviscid.SU2_inviscid)SUAVE.Analyses.Aerodynamics.SU2_inviscid.SU2_inviscid
@@ -125,7 +131,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__inviscid_1_1SU2__inviscid.html b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__inviscid_1_1SU2__inviscid.html index 444dff03..d33fcf8d 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__inviscid_1_1SU2__inviscid.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__inviscid_1_1SU2__inviscid.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Aerodynamics.SU2_inviscid.SU2_inviscid Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -107,8 +114,8 @@ SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics SUAVE.Analyses.Analysis.Analysis - -
+ + @@ -123,27 +130,21 @@ - - - - - - - - - - - - - - - - + + + + + + + + + +

Public Member Functions

def build_surrogate (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
def __defaults__ (self)
 
def evaluate (self, state)
 
def finalize (self)
 
def compute_forces (self, conditions)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
@@ -227,6 +228,8 @@

SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics.

+ @@ -413,7 +416,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__inviscid__Super_1_1SU2__inviscid__Super-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__inviscid__Super_1_1SU2__inviscid__Super-members.html index 434d567b..689b546b 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__inviscid__Super_1_1SU2__inviscid__Super-members.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__inviscid__Super_1_1SU2__inviscid__Super-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Attributes

SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -98,26 +105,25 @@

This is the complete list of members for SUAVE.Analyses.Aerodynamics.SU2_inviscid_Super.SU2_inviscid_Super, including all inherited members.

- + - - - - - - - - - - - - - - - - - + + + + + + + + + + + + + + + +
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Aerodynamics.SU2_inviscid_Super.SU2_inviscid_Super
build_surrogate(self)SUAVE.Analyses.Aerodynamics.SU2_inviscid_Super.SU2_inviscid_Super
compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
compute_forces(self, conditions)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
evaluate(self, state, settings, geometry)SUAVE.Analyses.Aerodynamics.SU2_inviscid_Super.SU2_inviscid_Super
SUAVE::Analyses::Aerodynamics::Aerodynamics::Aerodynamics.evaluate(self, state)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
geometry (defined in SUAVE.Analyses.Aerodynamics.SU2_inviscid_Super.SU2_inviscid_Super)SUAVE.Analyses.Aerodynamics.SU2_inviscid_Super.SU2_inviscid_Super
initialize(self)SUAVE.Analyses.Aerodynamics.SU2_inviscid_Super.SU2_inviscid_Super
SUAVE::Analyses::Aerodynamics::Aerodynamics::Aerodynamics.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
sample_training(self)SUAVE.Analyses.Aerodynamics.SU2_inviscid_Super.SU2_inviscid_Super
settings (defined in SUAVE.Analyses.Aerodynamics.SU2_inviscid_Super.SU2_inviscid_Super)SUAVE.Analyses.Aerodynamics.SU2_inviscid_Super.SU2_inviscid_Super
surrogates (defined in SUAVE.Analyses.Aerodynamics.SU2_inviscid_Super.SU2_inviscid_Super)SUAVE.Analyses.Aerodynamics.SU2_inviscid_Super.SU2_inviscid_Super
tag (defined in SUAVE.Analyses.Aerodynamics.SU2_inviscid_Super.SU2_inviscid_Super)SUAVE.Analyses.Aerodynamics.SU2_inviscid_Super.SU2_inviscid_Super
training (defined in SUAVE.Analyses.Aerodynamics.SU2_inviscid_Super.SU2_inviscid_Super)SUAVE.Analyses.Aerodynamics.SU2_inviscid_Super.SU2_inviscid_Super
training_file (defined in SUAVE.Analyses.Aerodynamics.SU2_inviscid_Super.SU2_inviscid_Super)SUAVE.Analyses.Aerodynamics.SU2_inviscid_Super.SU2_inviscid_Super
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
evaluate(self, state, settings, geometry)SUAVE.Analyses.Aerodynamics.SU2_inviscid_Super.SU2_inviscid_Super
SUAVE::Analyses::Aerodynamics::Aerodynamics::Aerodynamics.evaluate(self, state)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
SUAVE::Analyses::Analysis::Analysis.evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
SUAVE::Analyses::Analysis::Analysis.finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
geometry (defined in SUAVE.Analyses.Aerodynamics.SU2_inviscid_Super.SU2_inviscid_Super)SUAVE.Analyses.Aerodynamics.SU2_inviscid_Super.SU2_inviscid_Super
initialize(self)SUAVE.Analyses.Aerodynamics.SU2_inviscid_Super.SU2_inviscid_Super
SUAVE::Analyses::Aerodynamics::Aerodynamics::Aerodynamics.initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
sample_training(self)SUAVE.Analyses.Aerodynamics.SU2_inviscid_Super.SU2_inviscid_Super
settings (defined in SUAVE.Analyses.Aerodynamics.SU2_inviscid_Super.SU2_inviscid_Super)SUAVE.Analyses.Aerodynamics.SU2_inviscid_Super.SU2_inviscid_Super
surrogates (defined in SUAVE.Analyses.Aerodynamics.SU2_inviscid_Super.SU2_inviscid_Super)SUAVE.Analyses.Aerodynamics.SU2_inviscid_Super.SU2_inviscid_Super
tag (defined in SUAVE.Analyses.Aerodynamics.SU2_inviscid_Super.SU2_inviscid_Super)SUAVE.Analyses.Aerodynamics.SU2_inviscid_Super.SU2_inviscid_Super
training (defined in SUAVE.Analyses.Aerodynamics.SU2_inviscid_Super.SU2_inviscid_Super)SUAVE.Analyses.Aerodynamics.SU2_inviscid_Super.SU2_inviscid_Super
training_file (defined in SUAVE.Analyses.Aerodynamics.SU2_inviscid_Super.SU2_inviscid_Super)SUAVE.Analyses.Aerodynamics.SU2_inviscid_Super.SU2_inviscid_Super
@@ -125,7 +131,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__inviscid__Super_1_1SU2__inviscid__Super.html b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__inviscid__Super_1_1SU2__inviscid__Super.html index 6020d10c..8d01dd64 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__inviscid__Super_1_1SU2__inviscid__Super.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1SU2__inviscid__Super_1_1SU2__inviscid__Super.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Aerodynamics.SU2_inviscid_Super.SU2_inviscid_Super Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -107,8 +114,8 @@ SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics SUAVE.Analyses.Analysis.Analysis - -
+ + @@ -123,27 +130,21 @@ - - - - - - - - - - - - - - - - + + + + + + + + + +

Public Member Functions

def build_surrogate (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
def __defaults__ (self)
 
def evaluate (self, state)
 
def finalize (self)
 
def compute_forces (self, conditions)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
@@ -227,6 +228,8 @@

SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics.

+ @@ -413,7 +416,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Supersonic__OpenVSP__Wave__Drag_1_1Supersonic__OpenVSP__Wave__Drag-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Supersonic__OpenVSP__Wave__Drag_1_1Supersonic__OpenVSP__Wave__Drag-members.html index ac587261..82b8c83e 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Supersonic__OpenVSP__Wave__Drag_1_1Supersonic__OpenVSP__Wave__Drag-members.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Supersonic__OpenVSP__Wave__Drag_1_1Supersonic__OpenVSP__Wave__Drag-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Attributes

SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -98,21 +105,20 @@

This is the complete list of members for SUAVE.Analyses.Aerodynamics.Supersonic_OpenVSP_Wave_Drag.Supersonic_OpenVSP_Wave_Drag, including all inherited members.

- + - - - - - - - - - - - - - + + + + + + + + + + + +
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Aerodynamics.Supersonic_OpenVSP_Wave_Drag.Supersonic_OpenVSP_Wave_Drag
compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
compute_forces(self, conditions)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
evaluate(self, state)SUAVE.Analyses.Aerodynamics.Markup.Markup
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
geometry (defined in SUAVE.Analyses.Aerodynamics.Markup.Markup)SUAVE.Analyses.Aerodynamics.Markup.Markup
initialize(self)SUAVE.Analyses.Aerodynamics.Supersonic_OpenVSP_Wave_Drag.Supersonic_OpenVSP_Wave_Drag
SUAVE::Analyses::Aerodynamics::Aerodynamics::Aerodynamics.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
process (defined in SUAVE.Analyses.Aerodynamics.Markup.Markup)SUAVE.Analyses.Aerodynamics.Markup.Markup
settings (defined in SUAVE.Analyses.Aerodynamics.Markup.Markup)SUAVE.Analyses.Aerodynamics.Markup.Markup
tag (defined in SUAVE.Analyses.Aerodynamics.Supersonic_OpenVSP_Wave_Drag.Supersonic_OpenVSP_Wave_Drag)SUAVE.Analyses.Aerodynamics.Supersonic_OpenVSP_Wave_Drag.Supersonic_OpenVSP_Wave_Drag
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
evaluate(self, state)SUAVE.Analyses.Aerodynamics.Markup.Markup
SUAVE::Analyses::Analysis::Analysis.evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
SUAVE::Analyses::Analysis::Analysis.finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
geometry (defined in SUAVE.Analyses.Aerodynamics.Markup.Markup)SUAVE.Analyses.Aerodynamics.Markup.Markup
initialize(self)SUAVE.Analyses.Aerodynamics.Supersonic_OpenVSP_Wave_Drag.Supersonic_OpenVSP_Wave_Drag
SUAVE::Analyses::Aerodynamics::Aerodynamics::Aerodynamics.initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
process (defined in SUAVE.Analyses.Aerodynamics.Markup.Markup)SUAVE.Analyses.Aerodynamics.Markup.Markup
settings (defined in SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
tag (defined in SUAVE.Analyses.Aerodynamics.Supersonic_OpenVSP_Wave_Drag.Supersonic_OpenVSP_Wave_Drag)SUAVE.Analyses.Aerodynamics.Supersonic_OpenVSP_Wave_Drag.Supersonic_OpenVSP_Wave_Drag
@@ -120,7 +126,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Supersonic__OpenVSP__Wave__Drag_1_1Supersonic__OpenVSP__Wave__Drag.html b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Supersonic__OpenVSP__Wave__Drag_1_1Supersonic__OpenVSP__Wave__Drag.html index 2c69454c..7f29634f 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Supersonic__OpenVSP__Wave__Drag_1_1Supersonic__OpenVSP__Wave__Drag.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Supersonic__OpenVSP__Wave__Drag_1_1Supersonic__OpenVSP__Wave__Drag.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Aerodynamics.Supersonic_OpenVSP_Wave_Drag.Supersonic_OpenVSP_Wave_Drag Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -108,8 +115,8 @@ SUAVE.Analyses.Aerodynamics.Markup.Markup SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics SUAVE.Analyses.Analysis.Analysis - -
+ + @@ -118,34 +125,22 @@ - - - - - - - - - - - - - - - - - - - - - - + + + + + + + + + +

Public Member Functions

def initialize (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Aerodynamics.Markup.Markup
def __defaults__ (self)
 
def evaluate (self, state)
 
def initialize (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
def __defaults__ (self)
 
def evaluate (self, state)
 
def finalize (self)
 
def compute_forces (self, conditions)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
@@ -159,9 +154,6 @@ - - @@ -227,6 +219,8 @@

SUAVE.Analyses.Aerodynamics.Markup.Markup.

+ @@ -261,6 +255,8 @@

SUAVE.Analyses.Aerodynamics.Markup.Markup.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Supersonic__Zero_1_1Supersonic__Zero-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Supersonic__Zero_1_1Supersonic__Zero-members.html index 4bd94b5c..23e2ea46 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Supersonic__Zero_1_1Supersonic__Zero-members.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Supersonic__Zero_1_1Supersonic__Zero-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Attributes

 geometry
 
settings
 
 process
 
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -98,22 +105,21 @@

This is the complete list of members for SUAVE.Analyses.Aerodynamics.Supersonic_Zero.Supersonic_Zero, including all inherited members.

- + - - - - - - - - - - - - - - + + + + + + + + + + + + +
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Aerodynamics.Supersonic_Zero.Supersonic_Zero
compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
compute_forces(self, conditions)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
evaluate(self, state)SUAVE.Analyses.Aerodynamics.Markup.Markup
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize (defined in SUAVE.Analyses.Aerodynamics.Supersonic_Zero.Supersonic_Zero)SUAVE.Analyses.Aerodynamics.Supersonic_Zero.Supersonic_Zerostatic
SUAVE::Analyses::Aerodynamics::Markup::Markup.finalize(self)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
geometry (defined in SUAVE.Analyses.Aerodynamics.Markup.Markup)SUAVE.Analyses.Aerodynamics.Markup.Markup
initialize(self)SUAVE.Analyses.Aerodynamics.Supersonic_Zero.Supersonic_Zero
SUAVE::Analyses::Aerodynamics::Aerodynamics::Aerodynamics.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
process (defined in SUAVE.Analyses.Aerodynamics.Markup.Markup)SUAVE.Analyses.Aerodynamics.Markup.Markup
settings (defined in SUAVE.Analyses.Aerodynamics.Markup.Markup)SUAVE.Analyses.Aerodynamics.Markup.Markup
tag (defined in SUAVE.Analyses.Aerodynamics.Supersonic_Zero.Supersonic_Zero)SUAVE.Analyses.Aerodynamics.Supersonic_Zero.Supersonic_Zero
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
evaluate(self, state)SUAVE.Analyses.Aerodynamics.Markup.Markup
SUAVE::Analyses::Analysis::Analysis.evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize (defined in SUAVE.Analyses.Aerodynamics.Supersonic_Zero.Supersonic_Zero)SUAVE.Analyses.Aerodynamics.Supersonic_Zero.Supersonic_Zerostatic
SUAVE::Analyses::Aerodynamics::Markup::Markup.finalize(self)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
SUAVE::Analyses::Analysis::Analysis.finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
geometry (defined in SUAVE.Analyses.Aerodynamics.Markup.Markup)SUAVE.Analyses.Aerodynamics.Markup.Markup
initialize(self)SUAVE.Analyses.Aerodynamics.Supersonic_Zero.Supersonic_Zero
SUAVE::Analyses::Aerodynamics::Aerodynamics::Aerodynamics.initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
process (defined in SUAVE.Analyses.Aerodynamics.Markup.Markup)SUAVE.Analyses.Aerodynamics.Markup.Markup
settings (defined in SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
tag (defined in SUAVE.Analyses.Aerodynamics.Supersonic_Zero.Supersonic_Zero)SUAVE.Analyses.Aerodynamics.Supersonic_Zero.Supersonic_Zero
@@ -121,7 +127,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Supersonic__Zero_1_1Supersonic__Zero.html b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Supersonic__Zero_1_1Supersonic__Zero.html index d25cc4f3..2be6ba9f 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Supersonic__Zero_1_1Supersonic__Zero.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Supersonic__Zero_1_1Supersonic__Zero.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Aerodynamics.Supersonic_Zero.Supersonic_Zero Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -109,8 +116,8 @@ SUAVE.Analyses.Aerodynamics.Markup.Markup SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics SUAVE.Analyses.Analysis.Analysis - -
+ + @@ -119,34 +126,22 @@ - - - - - - - - - - - - - - - - - - - - - - + + + + + + + + + +

Public Member Functions

def initialize (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Aerodynamics.Markup.Markup
def __defaults__ (self)
 
def evaluate (self, state)
 
def initialize (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
def __defaults__ (self)
 
def evaluate (self, state)
 
def finalize (self)
 
def compute_forces (self, conditions)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
@@ -160,9 +155,6 @@ - - @@ -223,7 +215,9 @@

SUAVE.Analyses.Aerodynamics.Markup.Markup.

+ @@ -268,6 +264,8 @@

SUAVE.Analyses.Aerodynamics.Markup.Markup.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Vortex__Lattice_1_1Vortex__Lattice-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Vortex__Lattice_1_1Vortex__Lattice-members.html index 636ec858..0f39479f 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Vortex__Lattice_1_1Vortex__Lattice-members.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Vortex__Lattice_1_1Vortex__Lattice-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Attributes

 geometry
 
settings
 
 process
 
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -98,25 +105,30 @@

This is the complete list of members for SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice, including all inherited members.

- + - - - - - - - - - - - - - - - - + + + + + + + + + + + + + + + + + + + + +
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice
build_surrogate(self)SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice
compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
compute_forces(self, conditions)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
evaluate(self, state, settings, geometry)SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice
SUAVE::Analyses::Aerodynamics::Aerodynamics::Aerodynamics.evaluate(self, state)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
geometry (defined in SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice)SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice
initialize(self)SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice
SUAVE::Analyses::Aerodynamics::Aerodynamics::Aerodynamics.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
sample_training(self)SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice
settings (defined in SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice)SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice
surrogates (defined in SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice)SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice
tag (defined in SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice)SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice
training (defined in SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice)SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
evaluate (defined in SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice)SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice
SUAVE::Analyses::Aerodynamics::Aerodynamics::Aerodynamics.evaluate(self, state)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
SUAVE::Analyses::Analysis::Analysis.evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
evaluate_no_surrogate(self, state, settings, geometry)SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice
evaluate_surrogate(self, state, settings, geometry)SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self)SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
SUAVE::Analyses::Analysis::Analysis.finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
geometry (defined in SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice)SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice
hsub_max (defined in SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice)SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice
hsub_min (defined in SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice)SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice
hsup_max (defined in SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice)SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice
hsup_min (defined in SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice)SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice
initialize(self, use_surrogate, n_sw, n_cw, propeller_wake_model, mf, mn, dcs)SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice
SUAVE::Analyses::Aerodynamics::Aerodynamics::Aerodynamics.initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
sample_training(self)SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice
settings (defined in SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice)SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice
surrogates (defined in SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice)SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice
tag (defined in SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice)SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice
training (defined in SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice)SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice
@@ -124,7 +136,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Vortex__Lattice_1_1Vortex__Lattice.html b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Vortex__Lattice_1_1Vortex__Lattice.html index 109b6e3b..e38f8d55 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Vortex__Lattice_1_1Vortex__Lattice.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Vortex__Lattice_1_1Vortex__Lattice.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -107,43 +114,39 @@ SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics SUAVE.Analyses.Analysis.Analysis - -
+ + - - - - + + + + + + - - - - - - - - - - - - - - - - + + + + + + + + + +

Public Member Functions

def __defaults__ (self)
 
def initialize (self)
 
def evaluate (self, state, settings, geometry)
 
def initialize (self, use_surrogate, n_sw, n_cw, propeller_wake_model, mf, mn, dcs)
 
def evaluate_surrogate (self, state, settings, geometry)
 
def evaluate_no_surrogate (self, state, settings, geometry)
 
def sample_training (self)
 
def build_surrogate (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
def __defaults__ (self)
 
def evaluate (self, state)
 
def finalize (self)
 
def compute_forces (self, conditions)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
@@ -159,9 +162,24 @@ + + + + + + + + + + @@ -224,6 +242,8 @@

SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics.

+ @@ -254,26 +274,99 @@

-

◆ evaluate()

+ +

◆ evaluate_no_surrogate()

Public Attributes

 training
 
hsub_min
 
hsub_max
 
hsup_min
 
hsup_max
 
 surrogates
 
evaluate
 
- Public Attributes inherited from SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
 tag
- + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice.evaluate def SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice.evaluate_no_surrogate ( self,
 state,
 settings,
 geometry 
)
+
+
Evaluates lift and drag directly using VLM
+
+Assumptions:
+no changes to initial geometry or settings
+
+Source:
+N/A
+
+Inputs:
+state.conditions.
+  angle_of_attack                         [radians]
+  
+Outputs:
+conditions.aerodynamics.lift_breakdown.
+  inviscid_wings_lift[wings.*.tag]        [-] CL (wing specific)
+  inviscid_wings_lift.total               [-] CL
+  inviscid_wings_sectional                [-] Cly  
+  compressible_wing                       [-] CL (wing specific)
+conditions.aerodynamics.drag_breakdown.induced.
+  total                                   [-] CDi 
+  inviscid                                [-] CDi 
+  wings_sectional_drag                    [-] CDiy (wing specific)
+  induced.inviscid_wings                  [-] CDi  (wing specific)        
+    
+conditions.aerodynamics.
+  pressure_coefficient                    [-] CP
+ 
+Properties Used:
+self.surrogates.
+  lift_coefficient                        [-] CL
+  wing_lift_coefficient[wings.*.tag]      [-] CL (wing specific)
+
+
+ + +

◆ evaluate_surrogate()

+ +
+
+ + + @@ -318,21 +411,25 @@

-

◆ initialize()

+ +

◆ initialize()

- + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice.evaluate_surrogate (   self, (  self)self,
 use_surrogate,
 n_sw,
 n_cw,
 propeller_wake_model,
 mf,
 mn,
 dcs 
)
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Vortex__Lattice_1_1Vortex__Lattice.js b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Vortex__Lattice_1_1Vortex__Lattice.js index d0e1fbc1..54736ff4 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Vortex__Lattice_1_1Vortex__Lattice.js +++ b/doxygen/classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Vortex__Lattice_1_1Vortex__Lattice.js @@ -2,10 +2,16 @@ var classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Vortex__Lattice_1_1Vortex__Lattice [ [ "__defaults__", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Vortex__Lattice_1_1Vortex__Lattice.html#a626460308767892310bb8ec904f3d3b9", null ], [ "build_surrogate", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Vortex__Lattice_1_1Vortex__Lattice.html#a707b374ab283c62f6f1d4fe917854875", null ], - [ "evaluate", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Vortex__Lattice_1_1Vortex__Lattice.html#a655b0e93dd39403e711bc83c054cfef2", null ], - [ "initialize", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Vortex__Lattice_1_1Vortex__Lattice.html#ad5c19cbcf11eb96e5e5a5d3273784076", null ], + [ "evaluate_no_surrogate", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Vortex__Lattice_1_1Vortex__Lattice.html#a3348cade0e95c87c6079e600c4d49998", null ], + [ "evaluate_surrogate", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Vortex__Lattice_1_1Vortex__Lattice.html#a9d5f494416aa8357db4805bdbe843229", null ], + [ "initialize", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Vortex__Lattice_1_1Vortex__Lattice.html#a8002c8b452ee81424d933d6b1a86d9b3", null ], [ "sample_training", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Vortex__Lattice_1_1Vortex__Lattice.html#aa7a6045fc661f688b4aad3bf9e426950", null ], + [ "evaluate", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Vortex__Lattice_1_1Vortex__Lattice.html#ae7ca21090e24ffb3170e160efb29084a", null ], [ "geometry", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Vortex__Lattice_1_1Vortex__Lattice.html#a070b444364458c846683fb0870d4fd40", null ], + [ "hsub_max", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Vortex__Lattice_1_1Vortex__Lattice.html#a98e7bf0ab41177da2ecef966515e8aa6", null ], + [ "hsub_min", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Vortex__Lattice_1_1Vortex__Lattice.html#ae533b087904b041638128a28bfedbeac", null ], + [ "hsup_max", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Vortex__Lattice_1_1Vortex__Lattice.html#a6af73cb26552c05b1050c53b7e3cac01", null ], + [ "hsup_min", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Vortex__Lattice_1_1Vortex__Lattice.html#a7d2881b16742a185002e29a17c86acd4", null ], [ "settings", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Vortex__Lattice_1_1Vortex__Lattice.html#a8bea7e1ceb61e329dadd4e96a2999d91", null ], [ "surrogates", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Vortex__Lattice_1_1Vortex__Lattice.html#a2f3f00161e75df559ec9a6a1d8bdf4d4", null ], [ "tag", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Vortex__Lattice_1_1Vortex__Lattice.html#adb9e4b35657faa29fb812ae901d4a937", null ], diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Analysis_1_1Analysis-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Analysis_1_1Analysis-members.html index 34a72847..6677f55b 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Analysis_1_1Analysis-members.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Analysis_1_1Analysis-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@
- +
@@ -73,7 +78,9 @@
@@ -114,7 +121,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Analysis_1_1Analysis.html b/doxygen/classSUAVE_1_1Analyses_1_1Analysis_1_1Analysis.html index bd8c4b2f..5727b62c 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Analysis_1_1Analysis.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Analysis_1_1Analysis.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Analysis.Analysis Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -109,33 +116,29 @@ SUAVE.Analyses.Atmospheric.Atmospheric.Atmospheric SUAVE.Analyses.Costs.Costs.Costs SUAVE.Analyses.Energy.Energy.Energy -SUAVE.Analyses.Geometry.Geometry.Geometry -SUAVE.Analyses.Loads.Loads.Loads -SUAVE.Analyses.Mission.Segments.Segment.Segment -SUAVE.Analyses.Noise.Noise.Noise -SUAVE.Analyses.Planets.Planet.Planet -SUAVE.Analyses.Sizing.Sizing.Sizing -SUAVE.Analyses.Stability.Stability.Stability -SUAVE.Analyses.Structures.Structures.Structures -SUAVE.Analyses.Surrogate.Surrogate -SUAVE.Analyses.Weights.Weights.Weights - -
+SUAVE.Analyses.Mission.Segments.Segment.Segment +SUAVE.Analyses.Noise.Noise.Noise +SUAVE.Analyses.Planets.Planet.Planet +SUAVE.Analyses.Sizing.Sizing.Sizing +SUAVE.Analyses.Stability.Stability.Stability +SUAVE.Analyses.Weights.Weights.Weights + + - - - - - - - - - - + + + + + + + + + +

Public Member Functions

def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
@@ -160,8 +163,8 @@ Source: N/A

Member Function Documentation

- -

◆ __call__()

+ +

◆ __call__()

@@ -175,13 +178,13 @@

- + - + @@ -240,10 +243,12 @@

SUAVE.Analyses.Mission.Segments.Segment.Container, SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground, SUAVE.Analyses.Stability.AVL.AVL, SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice, SUAVE.Analyses.Noise.Fidelity_One.Fidelity_One, SUAVE.Analyses.Mission.Segments.Climb.Optimized.Optimized, SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero, SUAVE.Analyses.Mission.Segments.Ground.Landing.Landing, SUAVE.Analyses.Mission.Segments.Ground.Takeoff.Takeoff, SUAVE.Analyses.Aerodynamics.SU2_inviscid.SU2_inviscid, SUAVE.Analyses.Atmospheric.US_Standard_1976.US_Standard_1976, SUAVE.Analyses.Mission.Segments.Climb.Constant_Throttle_Constant_Speed.Constant_Throttle_Constant_Speed, SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle, SUAVE.Analyses.Mission.Segments.Cruise.Constant_Throttle_Constant_Altitude.Constant_Throttle_Constant_Altitude, SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude.Set_Speed_Set_Altitude, SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude_No_Propulsion.Set_Speed_Set_Altitude_No_Propulsion, SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Throttle.Set_Speed_Set_Throttle, SUAVE.Analyses.Aerodynamics.SU2_Euler_Super.SU2_Euler_Super, SUAVE.Analyses.Aerodynamics.SU2_inviscid_Super.SU2_inviscid_Super, SUAVE.Analyses.Atmospheric.Constant_Temperature.Constant_Temperature, SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude, SUAVE.Analyses.Weights.Weights_eVTOL.Weights_eVTOL, SUAVE.Analyses.Aerodynamics.SU2_Euler.SU2_Euler, SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Linear_Altitude.Constant_Speed_Linear_Altitude, SUAVE.Analyses.Mission.Segments.Descent.Unknown_Throttle.Unknown_Throttle, SUAVE.Analyses.Mission.Segments.Transition.Constant_Acceleration_Constant_Pitchrate_Constant_Altitude.Constant_Acceleration_Constant_Pitchrate_Constant_Altitude, SUAVE.Analyses.Aerodynamics.Fidelity_Zero.Fidelity_Zero, SUAVE.Analyses.Mission.Segments.Cruise.Constant_Acceleration_Constant_Altitude.Constant_Acceleration_Constant_Altitude, SUAVE.Analyses.Mission.Segments.Cruise.Constant_Pitch_Rate_Constant_Altitude.Constant_Pitch_Rate_Constant_Altitude, SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise, SUAVE.Analyses.Mission.Segments.Transition.Constant_Acceleration_Constant_Angle_Linear_Climb.Constant_Acceleration_Constant_Angle_Linear_Climb, SUAVE.Analyses.Weights.Weights_Transport.Weights_Transport, SUAVE.Analyses.Aerodynamics.Supersonic_OpenVSP_Wave_Drag.Supersonic_OpenVSP_Wave_Drag, SUAVE.Analyses.Mission.Segments.Hover.Climb.Climb, SUAVE.Analyses.Mission.Segments.Hover.Descent.Descent, SUAVE.Analyses.Mission.Segments.Hover.Hover.Hover, SUAVE.Analyses.Aerodynamics.Supersonic_Zero.Supersonic_Zero, SUAVE.Analyses.Weights.Weights.Weights, SUAVE.Analyses.Weights.Weights_BWB.Weights_BWB, SUAVE.Analyses.Weights.Weights_UAV.Weights_UAV, SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise, SUAVE.Analyses.Aerodynamics.AVL.AVL, SUAVE.Analyses.Mission.Segments.Climb.Constant_CAS_Constant_Rate.Constant_CAS_Constant_Rate, SUAVE.Analyses.Mission.Segments.Climb.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate, SUAVE.Analyses.Mission.Segments.Descent.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate, SUAVE.Analyses.Mission.Segments.Descent.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate, SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Angle.Constant_Dynamic_Pressure_Constant_Angle, SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Angle.Constant_Mach_Constant_Angle, SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Rate.Constant_Mach_Constant_Rate, SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle, SUAVE.Analyses.Mission.Segments.Climb.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate, SUAVE.Analyses.Mission.Segments.Climb.Linear_Speed_Constant_Rate.Linear_Speed_Constant_Rate, SUAVE.Analyses.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude_Loiter.Constant_Dynamic_Pressure_Constant_Altitude_Loiter, SUAVE.Analyses.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude_Loiter.Constant_Mach_Constant_Altitude_Loiter, SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude_Loiter.Constant_Speed_Constant_Altitude_Loiter, SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle, SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic, SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Linear_Altitude.Constant_Mach_Linear_Altitude, SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate, SUAVE.Analyses.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude.Constant_Dynamic_Pressure_Constant_Altitude, SUAVE.Analyses.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude.Constant_Mach_Constant_Altitude, SUAVE.Analyses.Mission.Segments.Segment.Segment, SUAVE.Analyses.Aerodynamics.AERODAS.AERODAS, SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Rate.Constant_Dynamic_Pressure_Constant_Rate, SUAVE.Analyses.Mission.Segments.Simple.Simple, SUAVE.Analyses.Noise.Fidelity_Zero.Fidelity_Zero, SUAVE.Analyses.Aerodynamics.Lifting_Line.Lifting_Line, SUAVE.Analyses.Aerodynamics.Markup.Markup, SUAVE.Analyses.Atmospheric.Atmospheric.Atmospheric, SUAVE.Analyses.Mission.Segments.Ground.Battery_Charge_Discharge.Battery_Charge_Discharge, SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics, SUAVE.Analyses.Noise.Noise.Noise, SUAVE.Analyses.Costs.Costs.Costs, SUAVE.Analyses.Mission.Segments.Descent.Constant_CAS_Constant_Rate.Constant_CAS_Constant_Rate, SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate, SUAVE.Analyses.Stability.Stability.Stability, SUAVE.Analyses.Planets.Planet.Planet, SUAVE.Analyses.Sizing.Sizing.Sizing, and SUAVE.Analyses.Energy.Energy.Energy.

+ - -

◆ compile()

+ +

◆ compile()

@@ -257,13 +262,13 @@

- + - + @@ -292,8 +297,8 @@

-

◆ evaluate()

+ +

◆ evaluate()

@@ -307,13 +312,13 @@

- + - + @@ -341,8 +346,8 @@

-

◆ finalize()

+ +

◆ finalize()

@@ -356,13 +361,13 @@

- + - + @@ -390,8 +395,8 @@

-

◆ initialize()

+ +

◆ initialize()

@@ -405,13 +410,13 @@

- + - + @@ -450,7 +455,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Analysis_1_1Analysis.js b/doxygen/classSUAVE_1_1Analyses_1_1Analysis_1_1Analysis.js index 792694b1..f77d4473 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Analysis_1_1Analysis.js +++ b/doxygen/classSUAVE_1_1Analyses_1_1Analysis_1_1Analysis.js @@ -1,11 +1,11 @@ var classSUAVE_1_1Analyses_1_1Analysis_1_1Analysis = [ - [ "__call__", "classSUAVE_1_1Analyses_1_1Analysis_1_1Analysis.html#afeeaf88c2424003602f1a4c0503ed4fd", null ], + [ "__call__", "classSUAVE_1_1Analyses_1_1Analysis_1_1Analysis.html#ae5813c73fa29c7dd6fb999b6a265fb60", null ], [ "__defaults__", "classSUAVE_1_1Analyses_1_1Analysis_1_1Analysis.html#ab23ae346b8d6ad343384bc9b0f3bb712", null ], - [ "compile", "classSUAVE_1_1Analyses_1_1Analysis_1_1Analysis.html#ae1183f13918b2bdcb0bf6d0aa94ef4f8", null ], - [ "evaluate", "classSUAVE_1_1Analyses_1_1Analysis_1_1Analysis.html#a0c950af6a4ce899d2a29fccef38f47d7", null ], - [ "finalize", "classSUAVE_1_1Analyses_1_1Analysis_1_1Analysis.html#a070b60f6b134baf09c60583901c5176a", null ], - [ "initialize", "classSUAVE_1_1Analyses_1_1Analysis_1_1Analysis.html#a460a311d6ac29134ff52b7bec21b13f5", null ], + [ "compile", "classSUAVE_1_1Analyses_1_1Analysis_1_1Analysis.html#a33b2657e98251b7ec3a201edfd51c1f7", null ], + [ "evaluate", "classSUAVE_1_1Analyses_1_1Analysis_1_1Analysis.html#a16d3d5ec27475d3bd228ad03ea9358aa", null ], + [ "finalize", "classSUAVE_1_1Analyses_1_1Analysis_1_1Analysis.html#a644094b6eebfa2710b27204563808fd3", null ], + [ "initialize", "classSUAVE_1_1Analyses_1_1Analysis_1_1Analysis.html#a28621453cc992ab64118d243b333d8c2", null ], [ "features", "classSUAVE_1_1Analyses_1_1Analysis_1_1Analysis.html#ad4391599de0c0ccb845a5eb4c31a7247", null ], [ "settings", "classSUAVE_1_1Analyses_1_1Analysis_1_1Analysis.html#aec47523bf171175d934cdbbb23e53327", null ], [ "tag", "classSUAVE_1_1Analyses_1_1Analysis_1_1Analysis.html#ad2dbbc94e7f1e2518410e2f8a1ea5af3", null ] diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Analysis_1_1Analysis.png b/doxygen/classSUAVE_1_1Analyses_1_1Analysis_1_1Analysis.png index 2d01b9f3..8fba2f58 100644 Binary files a/doxygen/classSUAVE_1_1Analyses_1_1Analysis_1_1Analysis.png and b/doxygen/classSUAVE_1_1Analyses_1_1Analysis_1_1Analysis.png differ diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Analysis_1_1Container-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Analysis_1_1Container-members.html index 1fca3e02..f1d478e1 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Analysis_1_1Container-members.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Analysis_1_1Container-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Attributes

  args,
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  args,
 **  kwarg 
  args,
 **  kwarg 
  args,
 **  kwarg 
  args,
 **  kwarg 
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -98,11 +105,11 @@

This is the complete list of members for SUAVE.Analyses.Analysis.Container, including all inherited members.

- - - - - + + + + +
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Container
compile(self, args, kwarg)SUAVE.Analyses.Analysis.Container
evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Container
finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Container
initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Container
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Container
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Container
evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Container
finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Container
initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Container
@@ -110,7 +117,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Analysis_1_1Container.html b/doxygen/classSUAVE_1_1Analyses_1_1Analysis_1_1Container.html index 50f16e70..9cdf16eb 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Analysis_1_1Container.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Analysis_1_1Container.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Analysis.Container Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -105,21 +112,21 @@ SUAVE.Analyses.Vehicle.Vehicle - -
+ + - - - - - - - - - - + + + + + + + + + +

Public Member Functions

def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 

Detailed Description

SUAVE.Analyses.Analysis.Container()
@@ -132,8 +139,8 @@
         Source:
         N/A
 

Member Function Documentation

- -

◆ __call__()

+ +

◆ __call__()

@@ -147,13 +154,13 @@

-   + *  args, -   + **  kwarg  @@ -181,8 +188,8 @@

-

◆ compile()

+ +

◆ compile()

@@ -196,13 +203,13 @@

-   + *  args, -   + **  kwarg  @@ -231,8 +238,8 @@

-

◆ evaluate()

+ +

◆ evaluate()

@@ -246,13 +253,13 @@

-   + *  args, -   + **  kwarg  @@ -281,8 +288,8 @@

-

◆ finalize()

+ +

◆ finalize()

@@ -296,13 +303,13 @@

-   + *  args, -   + **  kwarg  @@ -331,8 +338,8 @@

-

◆ initialize()

+ +

◆ initialize()

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SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@
- +

@@ -73,7 +78,9 @@
@@ -115,7 +122,7 @@
    + doxygen 1.8.15

diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Atmospheric_1_1Atmospheric_1_1Atmospheric.html b/doxygen/classSUAVE_1_1Analyses_1_1Atmospheric_1_1Atmospheric_1_1Atmospheric.html index 38076c41..424fe6be 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Atmospheric_1_1Atmospheric_1_1Atmospheric.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Atmospheric_1_1Atmospheric_1_1Atmospheric.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Atmospheric.Atmospheric.Atmospheric Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@
- +

@@ -73,7 +78,9 @@
@@ -107,8 +114,8 @@ SUAVE.Analyses.Analysis.Analysis SUAVE.Analyses.Atmospheric.Constant_Temperature.Constant_Temperature SUAVE.Analyses.Atmospheric.US_Standard_1976.US_Standard_1976 - -

+ +
@@ -117,18 +124,16 @@ - - - - - - - - - - - - + + + + + + + + + +

Public Member Functions

def compute_values (self, altitude)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
@@ -185,6 +190,10 @@

SUAVE.Analyses.Analysis.Analysis.

+ +

Reimplemented in SUAVE.Analyses.Atmospheric.US_Standard_1976.US_Standard_1976, and SUAVE.Analyses.Atmospheric.Constant_Temperature.Constant_Temperature.

+ @@ -226,7 +235,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Atmospheric_1_1Constant__Temperature_1_1Constant__Temperature-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Atmospheric_1_1Constant__Temperature_1_1Constant__Temperature-members.html index fe76a9b8..136a63a8 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Atmospheric_1_1Constant__Temperature_1_1Constant__Temperature-members.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Atmospheric_1_1Constant__Temperature_1_1Constant__Temperature-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Additional Inherited Members

SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -116,7 +123,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Atmospheric_1_1Constant__Temperature_1_1Constant__Temperature.html b/doxygen/classSUAVE_1_1Analyses_1_1Atmospheric_1_1Constant__Temperature_1_1Constant__Temperature.html index d60352fd..ffc52694 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Atmospheric_1_1Constant__Temperature_1_1Constant__Temperature.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Atmospheric_1_1Constant__Temperature_1_1Constant__Temperature.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Atmospheric.Constant_Temperature.Constant_Temperature Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -106,8 +113,8 @@ SUAVE.Analyses.Atmospheric.Atmospheric.Atmospheric SUAVE.Analyses.Analysis.Analysis - -
+ + @@ -116,23 +123,19 @@ - - - - - - - - - - - - - - + + + + + + + + + +

Public Member Functions

def compute_values (self, altitude, temperature=288.15)
 
- Public Member Functions inherited from SUAVE.Analyses.Atmospheric.Atmospheric.Atmospheric
def __defaults__ (self)
 
def compute_values (self, altitude)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
@@ -188,6 +191,8 @@

SUAVE.Analyses.Atmospheric.Atmospheric.Atmospheric.

+ @@ -239,6 +244,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Atmospheric_1_1US__Standard__1976_1_1US__Standard__1976-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Atmospheric_1_1US__Standard__1976_1_1US__Standard__1976-members.html index 0b1eb74f..53694fba 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Atmospheric_1_1US__Standard__1976_1_1US__Standard__1976-members.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Atmospheric_1_1US__Standard__1976_1_1US__Standard__1976-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Additional Inherited Members

SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -116,7 +123,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Atmospheric_1_1US__Standard__1976_1_1US__Standard__1976.html b/doxygen/classSUAVE_1_1Analyses_1_1Atmospheric_1_1US__Standard__1976_1_1US__Standard__1976.html index 2fbececb..ede0bc49 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Atmospheric_1_1US__Standard__1976_1_1US__Standard__1976.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Atmospheric_1_1US__Standard__1976_1_1US__Standard__1976.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Atmospheric.US_Standard_1976.US_Standard_1976 Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -106,8 +113,8 @@ SUAVE.Analyses.Atmospheric.Atmospheric.Atmospheric SUAVE.Analyses.Analysis.Analysis - -
+ + @@ -116,23 +123,19 @@ - - - - - - - - - - - - - - + + + + + + + + + +

Public Member Functions

def compute_values (self, altitude, temperature_deviation=0.0, var_gamma=False)
 
- Public Member Functions inherited from SUAVE.Analyses.Atmospheric.Atmospheric.Atmospheric
def __defaults__ (self)
 
def compute_values (self, altitude)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
@@ -188,6 +191,8 @@

SUAVE.Analyses.Atmospheric.Atmospheric.Atmospheric.

+ @@ -245,7 +250,10 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Costs_1_1Costs_1_1Costs-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Costs_1_1Costs_1_1Costs-members.html index 4638c053..eea01547 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Costs_1_1Costs_1_1Costs-members.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Costs_1_1Costs_1_1Costs-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Additional Inherited Members

SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -98,14 +105,14 @@

This is the complete list of members for SUAVE.Analyses.Costs.Costs.Costs, including all inherited members.

- + - + - + - - + + @@ -116,7 +123,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Costs_1_1Costs_1_1Costs.html b/doxygen/classSUAVE_1_1Analyses_1_1Costs_1_1Costs_1_1Costs.html index 950aabfb..1c16efaa 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Costs_1_1Costs_1_1Costs.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Costs_1_1Costs_1_1Costs.html @@ -1,9 +1,9 @@ - + - +SUAVE: SUAVE.Analyses.Costs.Costs.Costs Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ @@ -57,9 +60,11 @@
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Costs.Costs.Costs
compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
evaluate(self, conditions=None)SUAVE.Analyses.Costs.Costs.Costs
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
SUAVE::Analyses::Analysis::Analysis.evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
settings (defined in SUAVE.Analyses.Costs.Costs.Costs)SUAVE.Analyses.Costs.Costs.Costs
tag (defined in SUAVE.Analyses.Costs.Costs.Costs)SUAVE.Analyses.Costs.Costs.Costs
vehicle (defined in SUAVE.Analyses.Costs.Costs.Costs)SUAVE.Analyses.Costs.Costs.Costs
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -106,8 +113,8 @@ SUAVE.Analyses.Analysis.Analysis - -
+ + @@ -116,18 +123,16 @@ - - - - - - - - - - - - + + + + + + + + + +

Public Member Functions

def evaluate (self, conditions=None)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
@@ -193,6 +198,8 @@

SUAVE.Analyses.Analysis.Analysis.

+ @@ -253,7 +260,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Energy_1_1Energy_1_1Energy-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Energy_1_1Energy_1_1Energy-members.html index 5ddcb636..d3afdf4f 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Energy_1_1Energy_1_1Energy-members.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Energy_1_1Energy_1_1Energy-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Attributes

SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -98,14 +105,14 @@

This is the complete list of members for SUAVE.Analyses.Energy.Energy.Energy, including all inherited members.

- + - - + + - - + + @@ -116,7 +123,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Energy_1_1Energy_1_1Energy.html b/doxygen/classSUAVE_1_1Analyses_1_1Energy_1_1Energy_1_1Energy.html index 298e507f..9075f6d2 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Energy_1_1Energy_1_1Energy.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Energy_1_1Energy_1_1Energy.html @@ -1,9 +1,9 @@ - + - +SUAVE: SUAVE.Analyses.Energy.Energy.Energy Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ @@ -57,9 +60,11 @@
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Energy.Energy.Energy
compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
evaluate_thrust(self, state)SUAVE.Analyses.Energy.Energy.Energy
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
network (defined in SUAVE.Analyses.Energy.Energy.Energy)SUAVE.Analyses.Energy.Energy.Energy
settings (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
tag (defined in SUAVE.Analyses.Energy.Energy.Energy)SUAVE.Analyses.Energy.Energy.Energy
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -106,8 +113,8 @@ SUAVE.Analyses.Analysis.Analysis - -
+ + @@ -116,18 +123,16 @@ - - - - - - - - - - - - + + + + + + + + + +

Public Member Functions

def evaluate_thrust (self, state)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
@@ -183,6 +188,8 @@

SUAVE.Analyses.Analysis.Analysis.

+ @@ -239,7 +246,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Geometry_1_1Geometry_1_1Geometry-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Geometry_1_1Geometry_1_1Geometry-members.html deleted file mode 100644 index 07eb6a19..00000000 --- a/doxygen/classSUAVE_1_1Analyses_1_1Geometry_1_1Geometry_1_1Geometry-members.html +++ /dev/null @@ -1,122 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
-

Public Attributes

- - - - - - - -
-
SUAVE -  1.1.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
- - - - - -
- -
-
-
- - - - - - diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Geometry_1_1Geometry_1_1Geometry.html b/doxygen/classSUAVE_1_1Analyses_1_1Geometry_1_1Geometry_1_1Geometry.html deleted file mode 100644 index 5bb5223d..00000000 --- a/doxygen/classSUAVE_1_1Analyses_1_1Geometry_1_1Geometry_1_1Geometry.html +++ /dev/null @@ -1,263 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Geometry.Geometry.Geometry Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.1.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
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-
- - - -
-
- -
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-
- -
- -
-
- - -
- -
- -
- -
-
SUAVE.Analyses.Geometry.Geometry.Geometry Class Reference
-
-
-
-Inheritance diagram for SUAVE.Analyses.Geometry.Geometry.Geometry:
-
-
- - -SUAVE.Analyses.Analysis.Analysis - -
- - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def evaluate (self, condtitions)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - -

-Public Attributes

tag
 
features
 
settings
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
This class defines the geometry data structure of an aircraft in SUAVE
-
-Assumptions:
-    None
-
-Source:
-    N/A
-
-Inputs:
-    None
-    
-Outputs:
-    None
-
-Properties Used:
-     N/A
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Geometry.Geometry.Geometry.__defaults__ ( self)
-
-
This sets the default values and methods for the analysis.
-    
-Assumptions:
-None
-    
-Source:
-N/A
-    
-Inputs:
-None
-    
-Outputs:
-None
-    
-Properties Used:
-N/A
-
-
- -

◆ evaluate()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Analyses.Geometry.Geometry.Geometry.evaluate ( self,
 condtitions 
)
-
-
Evaluate the Geometry analysis.
-    
-Assumptions:
-None
-    
-Source:
-N/A
-    
-Inputs:
-None
-    
-Outputs:
-Results of the Geometry Analysis
-    
-Properties Used:
-N/A                
-
-
-
The documentation for this class was generated from the following file:
    -
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Analyses/Geometry/Geometry.py
  • -
-
-
- - - - diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Geometry_1_1Geometry_1_1Geometry.js b/doxygen/classSUAVE_1_1Analyses_1_1Geometry_1_1Geometry_1_1Geometry.js deleted file mode 100644 index 19129616..00000000 --- a/doxygen/classSUAVE_1_1Analyses_1_1Geometry_1_1Geometry_1_1Geometry.js +++ /dev/null @@ -1,8 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Geometry_1_1Geometry_1_1Geometry = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Geometry_1_1Geometry_1_1Geometry.html#a1a40c89afab7d7ffe8d4285404f8abe1", null ], - [ "evaluate", "classSUAVE_1_1Analyses_1_1Geometry_1_1Geometry_1_1Geometry.html#a99ed99c2c0e6b8b2238cd146e757a901", null ], - [ "features", "classSUAVE_1_1Analyses_1_1Geometry_1_1Geometry_1_1Geometry.html#ae56f32a3e01434eb2015b785d05161f9", null ], - [ "settings", "classSUAVE_1_1Analyses_1_1Geometry_1_1Geometry_1_1Geometry.html#af0bdc7654e079d4a1cf5f999463c0dd9", null ], - [ "tag", "classSUAVE_1_1Analyses_1_1Geometry_1_1Geometry_1_1Geometry.html#af366e60e7e3c21cafbfd7121bc6d14a7", null ] -]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Geometry_1_1Geometry_1_1Geometry.png b/doxygen/classSUAVE_1_1Analyses_1_1Geometry_1_1Geometry_1_1Geometry.png deleted file mode 100644 index 1c2c2b6d..00000000 Binary files a/doxygen/classSUAVE_1_1Analyses_1_1Geometry_1_1Geometry_1_1Geometry.png and /dev/null differ diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Loads_1_1Loads_1_1Loads-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Loads_1_1Loads_1_1Loads-members.html deleted file mode 100644 index 3a6ccf14..00000000 --- a/doxygen/classSUAVE_1_1Analyses_1_1Loads_1_1Loads_1_1Loads-members.html +++ /dev/null @@ -1,122 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.1.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
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-
-
- - - -
-
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-
-
- - - - - - diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Loads_1_1Loads_1_1Loads.html b/doxygen/classSUAVE_1_1Analyses_1_1Loads_1_1Loads_1_1Loads.html deleted file mode 100644 index d59be7e0..00000000 --- a/doxygen/classSUAVE_1_1Analyses_1_1Loads_1_1Loads_1_1Loads.html +++ /dev/null @@ -1,248 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Loads.Loads.Loads Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.1.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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- -
- -
-
- - -
- -
- -
- -
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SUAVE.Analyses.Loads.Loads.Loads Class Reference
-
-
-
-Inheritance diagram for SUAVE.Analyses.Loads.Loads.Loads:
-
-
- - -SUAVE.Analyses.Analysis.Analysis - -
- - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def evaluate (self, condtitions)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - -

-Public Attributes

tag
 
features
 
settings
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
SUAVE.Analyses.Loads.Loads()
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Loads.Loads.Loads.__defaults__ ( self)
-
-
This sets the default values and methods for the analysis.
-    
-Assumptions:
-None
-    
-Source:
-N/A
-    
-Inputs:
-None
-    
-Outputs:
-None
-    
-Properties Used:
-N/A
-
-
- -

◆ evaluate()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Analyses.Loads.Loads.Loads.evaluate ( self,
 condtitions 
)
-
-
Evaluate the Loads analysis.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-Results of the Loads Analysis
-
-Properties Used:
-N/A                
-
-
-
The documentation for this class was generated from the following file:
    -
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Analyses/Loads/Loads.py
  • -
-
-
- - - - diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Loads_1_1Loads_1_1Loads.js b/doxygen/classSUAVE_1_1Analyses_1_1Loads_1_1Loads_1_1Loads.js deleted file mode 100644 index 1ce9891a..00000000 --- a/doxygen/classSUAVE_1_1Analyses_1_1Loads_1_1Loads_1_1Loads.js +++ /dev/null @@ -1,8 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Loads_1_1Loads_1_1Loads = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Loads_1_1Loads_1_1Loads.html#af04f84783a1e7fcdbf586a62ba1594fa", null ], - [ "evaluate", "classSUAVE_1_1Analyses_1_1Loads_1_1Loads_1_1Loads.html#a53fd89d7710bec62997cddccadf4bc0d", null ], - [ "features", "classSUAVE_1_1Analyses_1_1Loads_1_1Loads_1_1Loads.html#a916c9fe322cb2fab9aa523f359b5d50f", null ], - [ "settings", "classSUAVE_1_1Analyses_1_1Loads_1_1Loads_1_1Loads.html#a62d27d9a4b737eb28fd3dea7daf0b031", null ], - [ "tag", "classSUAVE_1_1Analyses_1_1Loads_1_1Loads_1_1Loads.html#a3f369a27818738ee1f515f717ccc47e0", null ] -]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Loads_1_1Loads_1_1Loads.png b/doxygen/classSUAVE_1_1Analyses_1_1Loads_1_1Loads_1_1Loads.png deleted file mode 100644 index 10a4f9d1..00000000 Binary files a/doxygen/classSUAVE_1_1Analyses_1_1Loads_1_1Loads_1_1Loads.png and /dev/null differ diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1All__At__Once_1_1All__At__Once-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1All__At__Once_1_1All__At__Once-members.html index 13d2931f..340a54e6 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1All__At__Once_1_1All__At__Once-members.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1All__At__Once_1_1All__At__Once-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -108,7 +115,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1All__At__Once_1_1All__At__Once.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1All__At__Once_1_1All__At__Once.html index b56ad264..2a60aa2b 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1All__At__Once_1_1All__At__Once.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1All__At__Once_1_1All__At__Once.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Mission.All_At_Once.All_At_Once Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -105,18 +112,17 @@
-SUAVE.Analyses.Mission.Mission.Mission -SUAVE.Analyses.Mission.Vary_Cruise.Given_Weight.Given_Weight - -
+SUAVE.Analyses.Mission.Mission.Mission +SUAVE.Analyses.Mission.Variable_Range_Cruise.Given_State_of_Charge.Given_State_of_Charge +SUAVE.Analyses.Mission.Variable_Range_Cruise.Given_Weight.Given_Weight + + - -

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Mission.Mission
def __defaults__ (self)
 
def finalize (self)
 
@@ -170,6 +176,10 @@

SUAVE.Analyses.Mission.Mission.Mission.

+ +

Reimplemented in SUAVE.Analyses.Mission.Variable_Range_Cruise.Given_State_of_Charge.Given_State_of_Charge, and SUAVE.Analyses.Mission.Variable_Range_Cruise.Given_Weight.Given_Weight.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1All__At__Once_1_1All__At__Once.png b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1All__At__Once_1_1All__At__Once.png index c2eaf256..baa0be4f 100644 Binary files a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1All__At__Once_1_1All__At__Once.png and b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1All__At__Once_1_1All__At__Once.png differ diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Mission_1_1Container-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Mission_1_1Container-members.html index fc73a337..65d6b1d2 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Mission_1_1Container-members.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Mission_1_1Container-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -107,7 +114,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Mission_1_1Container.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Mission_1_1Container.html index 7cbe422f..46ec3a66 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Mission_1_1Container.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Mission_1_1Container.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Mission.Mission.Container Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -102,9 +109,7 @@ Inheritance diagram for SUAVE.Analyses.Mission.Mission.Container:
- - - +
@@ -57,9 +60,11 @@

@@ -211,7 +216,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Mission_1_1Mission-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Mission_1_1Mission-members.html index b734d2ab..53192a49 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Mission_1_1Mission-members.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Mission_1_1Mission-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -108,7 +115,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Mission_1_1Mission.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Mission_1_1Mission.html index fc2afb7d..8aed1f6b 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Mission_1_1Mission.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Mission_1_1Mission.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Mission.Mission.Mission Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -105,11 +112,12 @@
-SUAVE.Analyses.Mission.All_At_Once.All_At_Once -SUAVE.Analyses.Mission.Sequential_Segments.Sequential_Segments -SUAVE.Analyses.Mission.Vary_Cruise.Given_Weight.Given_Weight - -
+SUAVE.Analyses.Mission.All_At_Once.All_At_Once +SUAVE.Analyses.Mission.Sequential_Segments.Sequential_Segments +SUAVE.Analyses.Mission.Variable_Range_Cruise.Given_State_of_Charge.Given_State_of_Charge +SUAVE.Analyses.Mission.Variable_Range_Cruise.Given_Weight.Given_Weight + + @@ -165,6 +173,8 @@

SUAVE.Analyses.Mission.Sequential_Segments.Sequential_Segments, SUAVE.Analyses.Mission.All_At_Once.All_At_Once, SUAVE.Analyses.Mission.Variable_Range_Cruise.Given_State_of_Charge.Given_State_of_Charge, and SUAVE.Analyses.Mission.Variable_Range_Cruise.Given_Weight.Given_Weight.

+ @@ -212,7 +222,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Mission_1_1Mission.png b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Mission_1_1Mission.png index 7694e3f1..eac05ffc 100644 Binary files a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Mission_1_1Mission.png and b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Mission_1_1Mission.png differ diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Aerodynamic_1_1Aerodynamic-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Aerodynamic_1_1Aerodynamic-members.html index 3c5ea15b..f0be810c 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Aerodynamic_1_1Aerodynamic-members.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Aerodynamic_1_1Aerodynamic-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Member Functions

SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -98,25 +105,26 @@

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic, including all inherited members.

- + - - + + - + - - - - - - - - - - + + + + + + + + + + +
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
conditions (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
SUAVE::Analyses::Analysis::Analysis.evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
finalize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
merged(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
@@ -124,7 +132,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Aerodynamic_1_1Aerodynamic.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Aerodynamic_1_1Aerodynamic.html index 3065df6c..e01d3ea7 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Aerodynamic_1_1Aerodynamic.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Aerodynamic_1_1Aerodynamic.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -105,60 +112,57 @@
-SUAVE.Analyses.Mission.Segments.Simple.Simple -SUAVE.Analyses.Mission.Segments.Segment.Segment -SUAVE.Analyses.Analysis.Analysis -SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Linear_Altitude.Constant_Speed_Linear_Altitude -SUAVE.Analyses.Mission.Segments.Climb.Constant_Throttle_Constant_Speed.Constant_Throttle_Constant_Speed -SUAVE.Analyses.Mission.Segments.Climb.Optimized.Optimized -SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle -SUAVE.Analyses.Mission.Segments.Cruise.Constant_Acceleration_Constant_Altitude.Constant_Acceleration_Constant_Altitude -SUAVE.Analyses.Mission.Segments.Cruise.Constant_Pitch_Rate_Constant_Altitude.Constant_Pitch_Rate_Constant_Altitude -SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude -SUAVE.Analyses.Mission.Segments.Cruise.Constant_Throttle_Constant_Altitude.Constant_Throttle_Constant_Altitude -SUAVE.Analyses.Mission.Segments.Descent.Unknown_Throttle.Unknown_Throttle -SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground -SUAVE.Analyses.Mission.Segments.Hover.Hover.Hover -SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude.Set_Speed_Set_Altitude -SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Throttle.Set_Speed_Set_Throttle - -
+SUAVE.Analyses.Mission.Segments.Simple.Simple +SUAVE.Analyses.Mission.Segments.Segment.Segment +SUAVE.Analyses.Analysis.Analysis +SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Linear_Altitude.Constant_Speed_Linear_Altitude +SUAVE.Analyses.Mission.Segments.Climb.Constant_Throttle_Constant_Speed.Constant_Throttle_Constant_Speed +SUAVE.Analyses.Mission.Segments.Climb.Optimized.Optimized +SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle +SUAVE.Analyses.Mission.Segments.Cruise.Constant_Acceleration_Constant_Altitude.Constant_Acceleration_Constant_Altitude +SUAVE.Analyses.Mission.Segments.Cruise.Constant_Pitch_Rate_Constant_Altitude.Constant_Pitch_Rate_Constant_Altitude +SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude +SUAVE.Analyses.Mission.Segments.Cruise.Constant_Throttle_Constant_Altitude.Constant_Throttle_Constant_Altitude +SUAVE.Analyses.Mission.Segments.Descent.Unknown_Throttle.Unknown_Throttle +SUAVE.Analyses.Mission.Segments.Ground.Battery_Charge_Discharge.Battery_Charge_Discharge +SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground +SUAVE.Analyses.Mission.Segments.Hover.Hover.Hover +SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude.Set_Speed_Set_Altitude +SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude_No_Propulsion.Set_Speed_Set_Altitude_No_Propulsion +SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Throttle.Set_Speed_Set_Throttle +SUAVE.Analyses.Mission.Segments.Transition.Constant_Acceleration_Constant_Angle_Linear_Climb.Constant_Acceleration_Constant_Angle_Linear_Climb +SUAVE.Analyses.Mission.Segments.Transition.Constant_Acceleration_Constant_Pitchrate_Constant_Altitude.Constant_Acceleration_Constant_Pitchrate_Constant_Altitude + + - - - - - - - + + - - - - - - + + + + + + - - - - - - - - - - - - + + + + + + + + + +

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def initialize (self)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def iterate (self)
 
def finalize (self)
 
def evaluate (self, state=None)
 
def merged (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
@@ -178,6 +182,9 @@ + + @@ -190,7 +197,7 @@

Public Attributes

 process
 
conditions
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
 tag
 

Detailed Description

-
Thethird basic piece of a mission which each segment will expand upon
+
The third basic piece of a mission which each segment will expand upon
 
     Assumptions:
     There's a detailed process flow outline in defaults. A mission must be solved in that order.
@@ -231,6 +238,10 @@ 

SUAVE.Analyses.Mission.Segments.Simple.Simple.

+ +

Reimplemented in SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground, SUAVE.Analyses.Mission.Segments.Climb.Optimized.Optimized, SUAVE.Analyses.Mission.Segments.Ground.Landing.Landing, SUAVE.Analyses.Mission.Segments.Ground.Takeoff.Takeoff, SUAVE.Analyses.Mission.Segments.Climb.Constant_Throttle_Constant_Speed.Constant_Throttle_Constant_Speed, SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle, SUAVE.Analyses.Mission.Segments.Cruise.Constant_Throttle_Constant_Altitude.Constant_Throttle_Constant_Altitude, SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude.Set_Speed_Set_Altitude, SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude_No_Propulsion.Set_Speed_Set_Altitude_No_Propulsion, SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Throttle.Set_Speed_Set_Throttle, SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude, SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Linear_Altitude.Constant_Speed_Linear_Altitude, SUAVE.Analyses.Mission.Segments.Descent.Unknown_Throttle.Unknown_Throttle, SUAVE.Analyses.Mission.Segments.Transition.Constant_Acceleration_Constant_Pitchrate_Constant_Altitude.Constant_Acceleration_Constant_Pitchrate_Constant_Altitude, SUAVE.Analyses.Mission.Segments.Cruise.Constant_Acceleration_Constant_Altitude.Constant_Acceleration_Constant_Altitude, SUAVE.Analyses.Mission.Segments.Cruise.Constant_Pitch_Rate_Constant_Altitude.Constant_Pitch_Rate_Constant_Altitude, SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise, SUAVE.Analyses.Mission.Segments.Transition.Constant_Acceleration_Constant_Angle_Linear_Climb.Constant_Acceleration_Constant_Angle_Linear_Climb, SUAVE.Analyses.Mission.Segments.Hover.Climb.Climb, SUAVE.Analyses.Mission.Segments.Hover.Descent.Descent, SUAVE.Analyses.Mission.Segments.Hover.Hover.Hover, SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise, SUAVE.Analyses.Mission.Segments.Climb.Constant_CAS_Constant_Rate.Constant_CAS_Constant_Rate, SUAVE.Analyses.Mission.Segments.Climb.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate, SUAVE.Analyses.Mission.Segments.Descent.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate, SUAVE.Analyses.Mission.Segments.Descent.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate, SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Angle.Constant_Dynamic_Pressure_Constant_Angle, SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Angle.Constant_Mach_Constant_Angle, SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Rate.Constant_Mach_Constant_Rate, SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle, SUAVE.Analyses.Mission.Segments.Climb.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate, SUAVE.Analyses.Mission.Segments.Climb.Linear_Speed_Constant_Rate.Linear_Speed_Constant_Rate, SUAVE.Analyses.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude_Loiter.Constant_Dynamic_Pressure_Constant_Altitude_Loiter, SUAVE.Analyses.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude_Loiter.Constant_Mach_Constant_Altitude_Loiter, SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude_Loiter.Constant_Speed_Constant_Altitude_Loiter, SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle, SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Linear_Altitude.Constant_Mach_Linear_Altitude, SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate, SUAVE.Analyses.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude.Constant_Dynamic_Pressure_Constant_Altitude, SUAVE.Analyses.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude.Constant_Mach_Constant_Altitude, SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Rate.Constant_Dynamic_Pressure_Constant_Rate, SUAVE.Analyses.Mission.Segments.Ground.Battery_Charge_Discharge.Battery_Charge_Discharge, SUAVE.Analyses.Mission.Segments.Descent.Constant_CAS_Constant_Rate.Constant_CAS_Constant_Rate, and SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate.

+


The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Aerodynamic_1_1Aerodynamic.png b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Aerodynamic_1_1Aerodynamic.png index 02c915a6..92020daa 100644 Binary files a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Aerodynamic_1_1Aerodynamic.png and b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Aerodynamic_1_1Aerodynamic.png differ diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__CAS__Constant__Rate_1_1Const85f25d7e10b8daeddf8a4b88ac659586.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__CAS__Constant__Rate_1_1Const85f25d7e10b8daeddf8a4b88ac659586.html new file mode 100644 index 00000000..c7f8027b --- /dev/null +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__CAS__Constant__Rate_1_1Const85f25d7e10b8daeddf8a4b88ac659586.html @@ -0,0 +1,144 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
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+ + +
+ +
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SUAVE.Analyses.Mission.Segments.Climb.Constant_CAS_Constant_Rate.Constant_CAS_Constant_Rate Member List
+
+
+ +

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Climb.Constant_CAS_Constant_Rate.Constant_CAS_Constant_Rate, including all inherited members.

+ + + + + + + + + + + + + + + + + + + + + + + + + + +
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Climb.Constant_CAS_Constant_Rate.Constant_CAS_Constant_Rate
altitude_end (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_CAS_Constant_Rate.Constant_CAS_Constant_Rate)SUAVE.Analyses.Mission.Segments.Climb.Constant_CAS_Constant_Rate.Constant_CAS_Constant_Rate
altitude_start (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_CAS_Constant_Rate.Constant_CAS_Constant_Rate)SUAVE.Analyses.Mission.Segments.Climb.Constant_CAS_Constant_Rate.Constant_CAS_Constant_Rate
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
calibrated_air_speed (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_CAS_Constant_Rate.Constant_CAS_Constant_Rate)SUAVE.Analyses.Mission.Segments.Climb.Constant_CAS_Constant_Rate.Constant_CAS_Constant_Rate
climb_rate (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_CAS_Constant_Rate.Constant_CAS_Constant_Rate)SUAVE.Analyses.Mission.Segments.Climb.Constant_CAS_Constant_Rate.Constant_CAS_Constant_Rate
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
conditions (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
merged(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
true_course (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_CAS_Constant_Rate.Constant_CAS_Constant_Rate)SUAVE.Analyses.Mission.Segments.Climb.Constant_CAS_Constant_Rate.Constant_CAS_Constant_Rate
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__CAS__Constant__Rate_1_1Constant__CAS__Constant__Rate.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__CAS__Constant__Rate_1_1Constant__CAS__Constant__Rate.html new file mode 100644 index 00000000..f53985de --- /dev/null +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__CAS__Constant__Rate_1_1Constant__CAS__Constant__Rate.html @@ -0,0 +1,270 @@ + + + + + + + +SUAVE: SUAVE.Analyses.Mission.Segments.Climb.Constant_CAS_Constant_Rate.Constant_CAS_Constant_Rate Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
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+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Analyses.Mission.Segments.Climb.Constant_CAS_Constant_Rate.Constant_CAS_Constant_Rate Class Reference
+
+
+
+Inheritance diagram for SUAVE.Analyses.Mission.Segments.Climb.Constant_CAS_Constant_Rate.Constant_CAS_Constant_Rate:
+
+
+ + +SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle +SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic +SUAVE.Analyses.Mission.Segments.Simple.Simple +SUAVE.Analyses.Mission.Segments.Segment.Segment +SUAVE.Analyses.Analysis.Analysis + +
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def initialize (self)
 
def converge (self, state)
 
def iterate (self)
 
def finalize (self)
 
def evaluate (self, state=None)
 
def merged (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Attributes

altitude_start
 
altitude_end
 
climb_rate
 
calibrated_air_speed
 
true_course
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle
altitude_start
 
altitude_end
 
true_course
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
temperature_deviation
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
settings
 
state
 
analyses
 
process
 
conditions
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
+

Detailed Description

+
Climb at a constant Calibrated Airspeed (CAS) at a constant rate.
+
+    Assumptions:
+    None
+    
+    Source:
+    None
+

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Analyses.Mission.Segments.Climb.Constant_CAS_Constant_Rate.Constant_CAS_Constant_Rate.__defaults__ ( self)
+
+
This sets the default solver flow. Anything in here can be modified after initializing a segment.
+    
+    Assumptions:
+    None
+    
+    Source:
+    N/A
+    
+    Inputs:
+    None
+    
+    Outputs:
+    None
+    
+    Properties Used:
+    None
+
+

Reimplemented from SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle.

+ +
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Analyses/Mission/Segments/Climb/Constant_CAS_Constant_Rate.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__CAS__Constant__Rate_1_1Constant__CAS__Constant__Rate.js b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__CAS__Constant__Rate_1_1Constant__CAS__Constant__Rate.js new file mode 100644 index 00000000..94df5e0e --- /dev/null +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__CAS__Constant__Rate_1_1Constant__CAS__Constant__Rate.js @@ -0,0 +1,9 @@ +var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__CAS__Constant__Rate_1_1Constant__CAS__Constant__Rate = +[ + [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__CAS__Constant__Rate_1_1Constant__CAS__Constant__Rate.html#a67648adcfd80860c4547d8542140045d", null ], + [ "altitude_end", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__CAS__Constant__Rate_1_1Constant__CAS__Constant__Rate.html#a7e6109ee21130902524024e44bfe46b7", null ], + [ "altitude_start", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__CAS__Constant__Rate_1_1Constant__CAS__Constant__Rate.html#a8a3c287e13cc48b3bfd1a57f987902fc", null ], + [ "calibrated_air_speed", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__CAS__Constant__Rate_1_1Constant__CAS__Constant__Rate.html#a331a4f64462f27c2b6be5c2a4adafe57", null ], + [ "climb_rate", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__CAS__Constant__Rate_1_1Constant__CAS__Constant__Rate.html#a27b556c513b45a755d63e7dc2fc575ae", null ], + [ "true_course", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__CAS__Constant__Rate_1_1Constant__CAS__Constant__Rate.html#aece316b151733f0ad318fa76ffa44203", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__CAS__Constant__Rate_1_1Constant__CAS__Constant__Rate.png b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__CAS__Constant__Rate_1_1Constant__CAS__Constant__Rate.png new file mode 100644 index 00000000..dad9f117 Binary files /dev/null and b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__CAS__Constant__Rate_1_1Constant__CAS__Constant__Rate.png differ diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_0c868b4d8a039afb6f97eb86309f635e.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_0c868b4d8a039afb6f97eb86309f635e.html index ec31a52d..22d8574e 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_0c868b4d8a039afb6f97eb86309f635e.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_0c868b4d8a039afb6f97eb86309f635e.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -98,29 +105,31 @@

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Rate.Constant_Dynamic_Pressure_Constant_Rate, including all inherited members.

- + - - + + - + - - - - - - - - - - + + + + + + + + + + + +
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Rate.Constant_Dynamic_Pressure_Constant_Rate
altitude_end (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Rate.Constant_Dynamic_Pressure_Constant_Rate)SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Rate.Constant_Dynamic_Pressure_Constant_Rate
altitude_start (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Rate.Constant_Dynamic_Pressure_Constant_Rate)SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Rate.Constant_Dynamic_Pressure_Constant_Rate
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
climb_rate (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Rate.Constant_Dynamic_Pressure_Constant_Rate)SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Rate.Constant_Dynamic_Pressure_Constant_Rate
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
conditions (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
dynamic_pressure (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Rate.Constant_Dynamic_Pressure_Constant_Rate)SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Rate.Constant_Dynamic_Pressure_Constant_Rate
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
SUAVE::Analyses::Analysis::Analysis.evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
finalize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
merged(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
true_course (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Rate.Constant_Dynamic_Pressure_Constant_Rate)SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Rate.Constant_Dynamic_Pressure_Constant_Rate
@@ -128,7 +137,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_1a3019722a97e8cea99fa0e052a34a68.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_1a3019722a97e8cea99fa0e052a34a68.html index 6edc585c..754798bb 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_1a3019722a97e8cea99fa0e052a34a68.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_1a3019722a97e8cea99fa0e052a34a68.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Rate.Constant_Dynamic_Pressure_Constant_Rate Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -110,50 +117,37 @@ SUAVE.Analyses.Mission.Segments.Simple.Simple SUAVE.Analyses.Mission.Segments.Segment.Segment SUAVE.Analyses.Analysis.Analysis - -
+ + - - - - - - - - - - - - - + + - - - - - - + + + + + + - - - - - - - - - - - - + + + + + + + + + +

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def initialize (self)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def iterate (self)
 
def finalize (self)
 
def evaluate (self, state=None)
 
def merged (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
@@ -169,6 +163,9 @@ + + @@ -176,6 +173,9 @@ + + @@ -193,6 +193,9 @@ + + @@ -245,6 +248,8 @@

SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_1a3019722a97e8cea99fa0e052a34a68.js b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_1a3019722a97e8cea99fa0e052a34a68.js index 95a71d76..6396182e 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_1a3019722a97e8cea99fa0e052a34a68.js +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_1a3019722a97e8cea99fa0e052a34a68.js @@ -4,5 +4,6 @@ var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic_ [ "altitude_end", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_1a3019722a97e8cea99fa0e052a34a68.html#abb17767b2b4bbe63066f3f992c3ff5ea", null ], [ "altitude_start", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_1a3019722a97e8cea99fa0e052a34a68.html#a097ba6b578f8563acadd802d75edbb4f", null ], [ "climb_rate", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_1a3019722a97e8cea99fa0e052a34a68.html#a441914c37efbf0b4ee7680408eb159db", null ], - [ "dynamic_pressure", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_1a3019722a97e8cea99fa0e052a34a68.html#ad3f9933f7b8cda2f2b962ef2da11f19d", null ] + [ "dynamic_pressure", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_1a3019722a97e8cea99fa0e052a34a68.html#ad3f9933f7b8cda2f2b962ef2da11f19d", null ], + [ "true_course", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_1a3019722a97e8cea99fa0e052a34a68.html#a7abcad81a21468da4431a531a7b541ec", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_61b566f355ab199459fb54d7274e572f.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_61b566f355ab199459fb54d7274e572f.html index f8060fff..642b67d8 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_61b566f355ab199459fb54d7274e572f.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_61b566f355ab199459fb54d7274e572f.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Angle.Constant_Dynamic_Pressure_Constant_Angle Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Attributes

 dynamic_pressure
 
true_course
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle
 altitude_start
 altitude_end
 
true_course
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
 temperature_deviation
 process
 
conditions
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
 tag
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -110,50 +117,37 @@ SUAVE.Analyses.Mission.Segments.Simple.Simple SUAVE.Analyses.Mission.Segments.Segment.Segment SUAVE.Analyses.Analysis.Analysis - -
+ + - - - - - - - - - - - - - + + - - - - - - + + + + + + - - - - - - - - - - - - + + + + + + + + + +

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def initialize (self)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def iterate (self)
 
def finalize (self)
 
def evaluate (self, state=None)
 
def merged (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
@@ -169,6 +163,9 @@ + + @@ -176,6 +173,9 @@ + + @@ -193,6 +193,9 @@ + + @@ -246,6 +249,8 @@

SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_61b566f355ab199459fb54d7274e572f.js b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_61b566f355ab199459fb54d7274e572f.js index e2730409..4921df07 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_61b566f355ab199459fb54d7274e572f.js +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_61b566f355ab199459fb54d7274e572f.js @@ -4,5 +4,6 @@ var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic_ [ "altitude_end", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_61b566f355ab199459fb54d7274e572f.html#acbde920a943796262c2a8a33d4c2ca7c", null ], [ "altitude_start", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_61b566f355ab199459fb54d7274e572f.html#af9dae09118f0cb83578c8ea0628f4ac3", null ], [ "climb_angle", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_61b566f355ab199459fb54d7274e572f.html#a850b859796a2e86d3b00db3fa0af7155", null ], - [ "dynamic_pressure", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_61b566f355ab199459fb54d7274e572f.html#ad57b2f5e25c189c0d5ef42c19bb55ede", null ] + [ "dynamic_pressure", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_61b566f355ab199459fb54d7274e572f.html#ad57b2f5e25c189c0d5ef42c19bb55ede", null ], + [ "true_course", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_61b566f355ab199459fb54d7274e572f.html#aeafae464216a6d5c98a3a9ff7df6552c", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_d4885eddc1dc9286bf80c906e9327ed4.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_d4885eddc1dc9286bf80c906e9327ed4.html index 514140c2..511d09d8 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_d4885eddc1dc9286bf80c906e9327ed4.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Dynamic__Pressure__Constant_d4885eddc1dc9286bf80c906e9327ed4.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Attributes

 dynamic_pressure
 
true_course
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle
 altitude_start
 altitude_end
 
true_course
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
 temperature_deviation
 process
 
conditions
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
 tag
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -98,29 +105,31 @@

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Angle.Constant_Dynamic_Pressure_Constant_Angle, including all inherited members.

- + - - + + - + - - - - - - - - - - + + + + + + + + + + + +
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Angle.Constant_Dynamic_Pressure_Constant_Angle
altitude_end (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Angle.Constant_Dynamic_Pressure_Constant_Angle)SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Angle.Constant_Dynamic_Pressure_Constant_Angle
altitude_start (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Angle.Constant_Dynamic_Pressure_Constant_Angle)SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Angle.Constant_Dynamic_Pressure_Constant_Angle
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
climb_angle (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Angle.Constant_Dynamic_Pressure_Constant_Angle)SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Angle.Constant_Dynamic_Pressure_Constant_Angle
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
conditions (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
dynamic_pressure (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Angle.Constant_Dynamic_Pressure_Constant_Angle)SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Angle.Constant_Dynamic_Pressure_Constant_Angle
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
SUAVE::Analyses::Analysis::Analysis.evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
finalize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
merged(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
true_course (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Angle.Constant_Dynamic_Pressure_Constant_Angle)SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Angle.Constant_Dynamic_Pressure_Constant_Angle
@@ -128,7 +137,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__EAS__Constant__Rate_1_1Const472497e5093c13e072d3d7a0c8f99d2a.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__EAS__Constant__Rate_1_1Const472497e5093c13e072d3d7a0c8f99d2a.html index cb6042b7..14ef4646 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__EAS__Constant__Rate_1_1Const472497e5093c13e072d3d7a0c8f99d2a.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__EAS__Constant__Rate_1_1Const472497e5093c13e072d3d7a0c8f99d2a.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -98,29 +105,31 @@

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Climb.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate, including all inherited members.

- + - - + + - + - - - - - - - - - - + + + + + + + + + + + +
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Climb.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate
altitude_end (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate)SUAVE.Analyses.Mission.Segments.Climb.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate
altitude_start (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate)SUAVE.Analyses.Mission.Segments.Climb.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
climb_rate (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate)SUAVE.Analyses.Mission.Segments.Climb.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
conditions (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
equivalent_air_speed (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate)SUAVE.Analyses.Mission.Segments.Climb.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
SUAVE::Analyses::Analysis::Analysis.evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
finalize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
merged(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
true_course (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate)SUAVE.Analyses.Mission.Segments.Climb.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate
@@ -128,7 +137,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__EAS__Constant__Rate_1_1Constant__EAS__Constant__Rate.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__EAS__Constant__Rate_1_1Constant__EAS__Constant__Rate.html index 1d9ecf77..2d5d47ef 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__EAS__Constant__Rate_1_1Constant__EAS__Constant__Rate.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__EAS__Constant__Rate_1_1Constant__EAS__Constant__Rate.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Mission.Segments.Climb.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -110,50 +117,37 @@ SUAVE.Analyses.Mission.Segments.Simple.Simple SUAVE.Analyses.Mission.Segments.Segment.Segment SUAVE.Analyses.Analysis.Analysis - -
+ + - - - - - - - - - - - - - + + - - - - - - + + + + + + - - - - - - - - - - - - + + + + + + + + + +

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def initialize (self)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def iterate (self)
 
def finalize (self)
 
def evaluate (self, state=None)
 
def merged (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
@@ -169,6 +163,9 @@ + + @@ -176,6 +173,9 @@ + + @@ -193,6 +193,9 @@ + + @@ -245,6 +248,8 @@

SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__EAS__Constant__Rate_1_1Constant__EAS__Constant__Rate.js b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__EAS__Constant__Rate_1_1Constant__EAS__Constant__Rate.js index 21173593..7a104d28 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__EAS__Constant__Rate_1_1Constant__EAS__Constant__Rate.js +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__EAS__Constant__Rate_1_1Constant__EAS__Constant__Rate.js @@ -4,5 +4,6 @@ var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__EAS__Con [ "altitude_end", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__EAS__Constant__Rate_1_1Constant__EAS__Constant__Rate.html#a1652a172541f5bba885b3abb05b40976", null ], [ "altitude_start", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__EAS__Constant__Rate_1_1Constant__EAS__Constant__Rate.html#acc48821a55eb9c46ab29603feb7aa529", null ], [ "climb_rate", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__EAS__Constant__Rate_1_1Constant__EAS__Constant__Rate.html#a71acc84d4b08d62fcb031e85c5d2b294", null ], - [ "equivalent_air_speed", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__EAS__Constant__Rate_1_1Constant__EAS__Constant__Rate.html#afc67dc595e4933d3bec86d31a221e47c", null ] + [ "equivalent_air_speed", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__EAS__Constant__Rate_1_1Constant__EAS__Constant__Rate.html#afc67dc595e4933d3bec86d31a221e47c", null ], + [ "true_course", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__EAS__Constant__Rate_1_1Constant__EAS__Constant__Rate.html#a8e911446a16b84295074e677160e32d2", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Angle_1_1Cond98340f1a23497f281dfc038523d4030.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Angle_1_1Cond98340f1a23497f281dfc038523d4030.html index b87a7c90..b9b5b31a 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Angle_1_1Cond98340f1a23497f281dfc038523d4030.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Angle_1_1Cond98340f1a23497f281dfc038523d4030.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Attributes

 equivalent_air_speed
 
true_course
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle
 altitude_start
 altitude_end
 
true_course
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
 temperature_deviation
 process
 
conditions
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
 tag
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -98,29 +105,31 @@

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Angle.Constant_Mach_Constant_Angle, including all inherited members.

- + - - + + - + - - - - - + + + + + - - - - - + + + + + + +
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Angle.Constant_Mach_Constant_Angle
altitude_end (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Angle.Constant_Mach_Constant_Angle)SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Angle.Constant_Mach_Constant_Angle
altitude_start (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Angle.Constant_Mach_Constant_Angle)SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Angle.Constant_Mach_Constant_Angle
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
climb_angle (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Angle.Constant_Mach_Constant_Angle)SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Angle.Constant_Mach_Constant_Angle
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
conditions (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
SUAVE::Analyses::Analysis::Analysis.evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
finalize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
mach (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Angle.Constant_Mach_Constant_Angle)SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Angle.Constant_Mach_Constant_Angle
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
merged(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
true_course (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Angle.Constant_Mach_Constant_Angle)SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Angle.Constant_Mach_Constant_Angle
@@ -128,7 +137,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Angle_1_1Constant__Mach__Constant__Angle.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Angle_1_1Constant__Mach__Constant__Angle.html index 4d56b944..9920652d 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Angle_1_1Constant__Mach__Constant__Angle.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Angle_1_1Constant__Mach__Constant__Angle.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Angle.Constant_Mach_Constant_Angle Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -110,50 +117,37 @@ SUAVE.Analyses.Mission.Segments.Simple.Simple SUAVE.Analyses.Mission.Segments.Segment.Segment SUAVE.Analyses.Analysis.Analysis - -
+ + - - - - - - - - - - - - - + + - - - - - - + + + + + + - - - - - - - - - - - - + + + + + + + + + +

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def initialize (self)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def iterate (self)
 
def finalize (self)
 
def evaluate (self, state=None)
 
def merged (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
@@ -169,6 +163,9 @@ + + @@ -176,6 +173,9 @@ + + @@ -193,6 +193,9 @@ + + @@ -246,6 +249,8 @@

SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Angle_1_1Constant__Mach__Constant__Angle.js b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Angle_1_1Constant__Mach__Constant__Angle.js index eebd2e2f..22ecba53 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Angle_1_1Constant__Mach__Constant__Angle.js +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Angle_1_1Constant__Mach__Constant__Angle.js @@ -4,5 +4,6 @@ var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Co [ "altitude_end", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Angle_1_1Constant__Mach__Constant__Angle.html#a2db347c82878d9ba79771ddd4643eb78", null ], [ "altitude_start", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Angle_1_1Constant__Mach__Constant__Angle.html#a37f860123e25f89ff15c79df7eb58de9", null ], [ "climb_angle", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Angle_1_1Constant__Mach__Constant__Angle.html#ade53ee4189ecd0ab2a8f77b974ec5f15", null ], - [ "mach", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Angle_1_1Constant__Mach__Constant__Angle.html#a6765373b2bf85eb7955b411ea5daf00c", null ] + [ "mach", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Angle_1_1Constant__Mach__Constant__Angle.html#a6765373b2bf85eb7955b411ea5daf00c", null ], + [ "true_course", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Angle_1_1Constant__Mach__Constant__Angle.html#a1328a7be58ab100275a516e93a9fa509", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Rate_1_1Conseeda9394fcf076a53ee13c4c243a002b.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Rate_1_1Conseeda9394fcf076a53ee13c4c243a002b.html index e9f0e75f..199392ae 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Rate_1_1Conseeda9394fcf076a53ee13c4c243a002b.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Rate_1_1Conseeda9394fcf076a53ee13c4c243a002b.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Attributes

 mach
 
true_course
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle
 altitude_start
 altitude_end
 
true_course
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
 temperature_deviation
 process
 
conditions
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
 tag
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -98,29 +105,31 @@

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Rate.Constant_Mach_Constant_Rate, including all inherited members.

- + - - + + - + - - - - - + + + + + - - - - - + + + + + + +
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Rate.Constant_Mach_Constant_Rate
altitude_end (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Rate.Constant_Mach_Constant_Rate)SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Rate.Constant_Mach_Constant_Rate
altitude_start (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Rate.Constant_Mach_Constant_Rate)SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Rate.Constant_Mach_Constant_Rate
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
climb_rate (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Rate.Constant_Mach_Constant_Rate)SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Rate.Constant_Mach_Constant_Rate
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
conditions (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
SUAVE::Analyses::Analysis::Analysis.evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
finalize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
mach_number (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Rate.Constant_Mach_Constant_Rate)SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Rate.Constant_Mach_Constant_Rate
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
merged(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
true_course (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Rate.Constant_Mach_Constant_Rate)SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Rate.Constant_Mach_Constant_Rate
@@ -128,7 +137,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Rate_1_1Constant__Mach__Constant__Rate.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Rate_1_1Constant__Mach__Constant__Rate.html index c9b0f6e5..795c4578 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Rate_1_1Constant__Mach__Constant__Rate.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Rate_1_1Constant__Mach__Constant__Rate.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Rate.Constant_Mach_Constant_Rate Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -110,50 +117,37 @@ SUAVE.Analyses.Mission.Segments.Simple.Simple SUAVE.Analyses.Mission.Segments.Segment.Segment SUAVE.Analyses.Analysis.Analysis - -
+ + - - - - - - - - - - - - - + + - - - - - - + + + + + + - - - - - - - - - - - - + + + + + + + + + +

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def initialize (self)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def iterate (self)
 
def finalize (self)
 
def evaluate (self, state=None)
 
def merged (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
@@ -169,6 +163,9 @@ + + @@ -176,6 +173,9 @@ + + @@ -193,6 +193,9 @@ + + @@ -245,6 +248,8 @@

SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Rate_1_1Constant__Mach__Constant__Rate.js b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Rate_1_1Constant__Mach__Constant__Rate.js index b437dbc0..95e69eae 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Rate_1_1Constant__Mach__Constant__Rate.js +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Rate_1_1Constant__Mach__Constant__Rate.js @@ -4,5 +4,6 @@ var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Co [ "altitude_end", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Rate_1_1Constant__Mach__Constant__Rate.html#a3236f8ba3d3fa8ce6fba1794f1a640c5", null ], [ "altitude_start", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Rate_1_1Constant__Mach__Constant__Rate.html#ae0abdda540025af275b11c4642e61a26", null ], [ "climb_rate", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Rate_1_1Constant__Mach__Constant__Rate.html#a919a255bb7c36308039fa83652ee4b52", null ], - [ "mach_number", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Rate_1_1Constant__Mach__Constant__Rate.html#a34c5ca143790bf7f3d2de5c64549fe13", null ] + [ "mach_number", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Rate_1_1Constant__Mach__Constant__Rate.html#a34c5ca143790bf7f3d2de5c64549fe13", null ], + [ "true_course", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Constant__Rate_1_1Constant__Mach__Constant__Rate.html#a9dd0f4824a263ad6034c7d9d3323bc9c", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Linear__Altitude_1_1Co8c4ee3be4a98ae94054df578da4a2738.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Linear__Altitude_1_1Co8c4ee3be4a98ae94054df578da4a2738.html index 08680ead..d7fb3c05 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Linear__Altitude_1_1Co8c4ee3be4a98ae94054df578da4a2738.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Linear__Altitude_1_1Co8c4ee3be4a98ae94054df578da4a2738.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Attributes

 mach_number
 
true_course
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle
 altitude_start
 altitude_end
 
true_course
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
 temperature_deviation
 process
 
conditions
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
 tag
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -98,31 +105,33 @@

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Linear_Altitude.Constant_Mach_Linear_Altitude, including all inherited members.

- + - - + + - + - - - - - + + + + + - - - - - + + + + + + +
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Linear_Altitude.Constant_Mach_Linear_Altitude
air_speed (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Linear_Altitude.Constant_Speed_Linear_Altitude)SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Linear_Altitude.Constant_Speed_Linear_Altitude
altitude (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Linear_Altitude.Constant_Mach_Linear_Altitude)SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Linear_Altitude.Constant_Mach_Linear_Altitude
altitude_end (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Linear_Altitude.Constant_Mach_Linear_Altitude)SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Linear_Altitude.Constant_Mach_Linear_Altitude
altitude_start (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Linear_Altitude.Constant_Mach_Linear_Altitude)SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Linear_Altitude.Constant_Mach_Linear_Altitude
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
conditions (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
distance (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Linear_Altitude.Constant_Mach_Linear_Altitude)SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Linear_Altitude.Constant_Mach_Linear_Altitude
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
SUAVE::Analyses::Analysis::Analysis.evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
finalize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
mach (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Linear_Altitude.Constant_Mach_Linear_Altitude)SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Linear_Altitude.Constant_Mach_Linear_Altitude
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
merged(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
true_course (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Linear_Altitude.Constant_Mach_Linear_Altitude)SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Linear_Altitude.Constant_Mach_Linear_Altitude
@@ -130,7 +139,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Linear__Altitude_1_1Constant__Mach__Linear__Altitude.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Linear__Altitude_1_1Constant__Mach__Linear__Altitude.html index 6200eeba..394a8d43 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Linear__Altitude_1_1Constant__Mach__Linear__Altitude.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Linear__Altitude_1_1Constant__Mach__Linear__Altitude.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Linear_Altitude.Constant_Mach_Linear_Altitude Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -110,50 +117,37 @@ SUAVE.Analyses.Mission.Segments.Simple.Simple SUAVE.Analyses.Mission.Segments.Segment.Segment SUAVE.Analyses.Analysis.Analysis - -
+ + - - - - - - - - - - - - - + + - - - - - - + + + + + + - - - - - - - - - - - - + + + + + + + + + +

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Linear_Altitude.Constant_Speed_Linear_Altitude
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def initialize (self)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def iterate (self)
 
def finalize (self)
 
def evaluate (self, state=None)
 
def merged (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
@@ -172,6 +166,9 @@ + + @@ -188,6 +185,9 @@ + + @@ -205,6 +205,9 @@ + + @@ -257,6 +260,8 @@

SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Linear_Altitude.Constant_Speed_Linear_Altitude.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Linear__Altitude_1_1Constant__Mach__Linear__Altitude.js b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Linear__Altitude_1_1Constant__Mach__Linear__Altitude.js index 285a614d..1fb022f7 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Linear__Altitude_1_1Constant__Mach__Linear__Altitude.js +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Linear__Altitude_1_1Constant__Mach__Linear__Altitude.js @@ -5,5 +5,6 @@ var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Li [ "altitude_end", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Linear__Altitude_1_1Constant__Mach__Linear__Altitude.html#af4b0b41792a4349fe840f4d576afe7f1", null ], [ "altitude_start", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Linear__Altitude_1_1Constant__Mach__Linear__Altitude.html#aed0f90918954a0e628428626496a00ee", null ], [ "distance", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Linear__Altitude_1_1Constant__Mach__Linear__Altitude.html#a598c889032ae65c0ba75235d5267e3e4", null ], - [ "mach", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Linear__Altitude_1_1Constant__Mach__Linear__Altitude.html#aeb0f2f830a113f193a40fba4b6de704f", null ] + [ "mach", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Linear__Altitude_1_1Constant__Mach__Linear__Altitude.html#aeb0f2f830a113f193a40fba4b6de704f", null ], + [ "true_course", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Mach__Linear__Altitude_1_1Constant__Mach__Linear__Altitude.html#a09fb7031a99010cfbefe4d86a5bb7e5b", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle_1_1Coe49fde66af63b5086460e1537e678aaa.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle_1_1Coe49fde66af63b5086460e1537e678aaa.html index 0b5907ae..35217bcc 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle_1_1Coe49fde66af63b5086460e1537e678aaa.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle_1_1Coe49fde66af63b5086460e1537e678aaa.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Attributes

 altitude_end
 
true_course
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Linear_Altitude.Constant_Speed_Linear_Altitude
 altitude
 altitude_end
 
true_course
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
 temperature_deviation
 process
 
conditions
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
 tag
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -98,29 +105,31 @@

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle, including all inherited members.

- + - - + + - + - - - - - - - - - - + + + + + + + + + + + +
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle
air_speed (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle)SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle
altitude_end (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle)SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle
altitude_start (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle)SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
climb_angle (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle)SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
conditions (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
SUAVE::Analyses::Analysis::Analysis.evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
finalize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
merged(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
true_course (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle)SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle
@@ -128,7 +137,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle_1_1Constant__Speed__Constant__Angle.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle_1_1Constant__Speed__Constant__Angle.html index c7e86244..254c3e46 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle_1_1Constant__Speed__Constant__Angle.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle_1_1Constant__Speed__Constant__Angle.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -110,50 +117,37 @@ SUAVE.Analyses.Mission.Segments.Simple.Simple SUAVE.Analyses.Mission.Segments.Segment.Segment SUAVE.Analyses.Analysis.Analysis - -
+ + - - - - - - - - - - - - - + + - - - - - - + + + + + + - - - - - - - - - - - - + + + + + + + + + +

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def initialize (self)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def iterate (self)
 
def finalize (self)
 
def evaluate (self, state=None)
 
def merged (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
@@ -169,6 +163,9 @@ + + @@ -176,6 +173,9 @@ + + @@ -193,6 +193,9 @@ + + @@ -246,6 +249,8 @@

SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle_1_1Constant__Speed__Constant__Angle.js b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle_1_1Constant__Speed__Constant__Angle.js index cd11c1a4..066682d8 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle_1_1Constant__Speed__Constant__Angle.js +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle_1_1Constant__Speed__Constant__Angle.js @@ -4,5 +4,6 @@ var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__C [ "air_speed", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle_1_1Constant__Speed__Constant__Angle.html#a074bc5776c3c78d43d5abb0a074a0156", null ], [ "altitude_end", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle_1_1Constant__Speed__Constant__Angle.html#a5900968ee69b00b5f8e6b98f2da57e41", null ], [ "altitude_start", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle_1_1Constant__Speed__Constant__Angle.html#acd39a3fecffc510bd6a15027cf48bedf", null ], - [ "climb_angle", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle_1_1Constant__Speed__Constant__Angle.html#a3562b40f80a73b2a9a99f92ccb1168b4", null ] + [ "climb_angle", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle_1_1Constant__Speed__Constant__Angle.html#a3562b40f80a73b2a9a99f92ccb1168b4", null ], + [ "true_course", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle_1_1Constant__Speed__Constant__Angle.html#a136b314afaddf561535f3804a9335a07", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle__Noisb1704f4c5e6114d87007dadfc99b2d01.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle__Noisb1704f4c5e6114d87007dadfc99b2d01.html index 7036e882..5d7cc181 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle__Noisb1704f4c5e6114d87007dadfc99b2d01.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle__Noisb1704f4c5e6114d87007dadfc99b2d01.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Attributes

 air_speed
 
true_course
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle
 altitude_start
 altitude_end
 
true_course
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
 temperature_deviation
 process
 
conditions
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
 tag
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -98,29 +105,31 @@

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise, including all inherited members.

- + - - + + - + - - - - - - - - - - + + + + + + + + + + + +
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise
air_speed (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise)SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise
altitude_end (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise)SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise
altitude_start (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise)SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
climb_angle (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise)SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
conditions (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
SUAVE::Analyses::Analysis::Analysis.evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
finalize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
merged(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
true_course (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise)SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise
@@ -128,7 +137,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle__Noise1165f03ba148155cea33a06b04b964a.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle__Noise1165f03ba148155cea33a06b04b964a.html index f8e27576..863c6804 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle__Noise1165f03ba148155cea33a06b04b964a.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle__Noise1165f03ba148155cea33a06b04b964a.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -110,50 +117,37 @@ SUAVE.Analyses.Mission.Segments.Simple.Simple SUAVE.Analyses.Mission.Segments.Segment.Segment SUAVE.Analyses.Analysis.Analysis - -
+ + - - - - - - - - - - - - - + + - - - - - - + + + + + + - - - - - - - - - - - - + + + + + + + + + +

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def initialize (self)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def iterate (self)
 
def finalize (self)
 
def evaluate (self, state=None)
 
def merged (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
@@ -169,6 +163,9 @@ + + @@ -176,6 +173,9 @@ + + @@ -193,6 +193,9 @@ + + @@ -248,6 +251,8 @@

SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle__Noise1165f03ba148155cea33a06b04b964a.js b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle__Noise1165f03ba148155cea33a06b04b964a.js index 12b655af..2b040618 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle__Noise1165f03ba148155cea33a06b04b964a.js +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle__Noise1165f03ba148155cea33a06b04b964a.js @@ -4,5 +4,6 @@ var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__C [ "air_speed", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle__Noise1165f03ba148155cea33a06b04b964a.html#a161831d0de82de6d65ec640cbd216709", null ], [ "altitude_end", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle__Noise1165f03ba148155cea33a06b04b964a.html#ae5b755e424fa9fd62430622c061525f9", null ], [ "altitude_start", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle__Noise1165f03ba148155cea33a06b04b964a.html#a0184a53853849f128c2c0da67d38a9b0", null ], - [ "climb_angle", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle__Noise1165f03ba148155cea33a06b04b964a.html#a115cf7a64f4135636271660181b097cf", null ] + [ "climb_angle", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle__Noise1165f03ba148155cea33a06b04b964a.html#a115cf7a64f4135636271660181b097cf", null ], + [ "true_course", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Angle__Noise1165f03ba148155cea33a06b04b964a.html#ab5eb867868cfd9f241d9dea68e8cce7e", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Rate_1_1Con98f50eb7047227d427afc04f6619e235.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Rate_1_1Con98f50eb7047227d427afc04f6619e235.html index 99e1db18..49d50aa2 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Rate_1_1Con98f50eb7047227d427afc04f6619e235.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Rate_1_1Con98f50eb7047227d427afc04f6619e235.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Attributes

 air_speed
 
true_course
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle
 altitude_start
 altitude_end
 
true_course
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
 temperature_deviation
 process
 
conditions
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
 tag
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -98,29 +105,31 @@

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate, including all inherited members.

- + - - + + - + - - - - - - - - - - + + + + + + + + + + + +
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate
air_speed (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate)SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate
altitude_end (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate)SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate
altitude_start (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate)SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
climb_rate (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate)SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
conditions (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
SUAVE::Analyses::Analysis::Analysis.evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
finalize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
merged(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
true_course (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate)SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate
@@ -128,7 +137,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Rate_1_1Constant__Speed__Constant__Rate.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Rate_1_1Constant__Speed__Constant__Rate.html index aa9a3227..22bc925e 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Rate_1_1Constant__Speed__Constant__Rate.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Rate_1_1Constant__Speed__Constant__Rate.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -110,50 +117,37 @@ SUAVE.Analyses.Mission.Segments.Simple.Simple SUAVE.Analyses.Mission.Segments.Segment.Segment SUAVE.Analyses.Analysis.Analysis - -
+ + - - - - - - - - - - - - - + + - - - - - - + + + + + + - - - - - - - - - - - - + + + + + + + + + +

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def initialize (self)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def iterate (self)
 
def finalize (self)
 
def evaluate (self, state=None)
 
def merged (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
@@ -169,6 +163,9 @@ + + @@ -176,6 +173,9 @@ + + @@ -193,6 +193,9 @@ + + @@ -245,6 +248,8 @@

SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Rate_1_1Constant__Speed__Constant__Rate.js b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Rate_1_1Constant__Speed__Constant__Rate.js index 82101723..5c3aaf13 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Rate_1_1Constant__Speed__Constant__Rate.js +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Rate_1_1Constant__Speed__Constant__Rate.js @@ -4,5 +4,6 @@ var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__C [ "air_speed", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Rate_1_1Constant__Speed__Constant__Rate.html#a2218ec53554f8babfc14a0589d370408", null ], [ "altitude_end", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Rate_1_1Constant__Speed__Constant__Rate.html#a97099b1d5412945f7ff501505ba97b12", null ], [ "altitude_start", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Rate_1_1Constant__Speed__Constant__Rate.html#a814302292a45ce0a0473d8bfcd44b7cc", null ], - [ "climb_rate", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Rate_1_1Constant__Speed__Constant__Rate.html#a5e77679758ffc9ab01462176a1bce1b0", null ] + [ "climb_rate", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Rate_1_1Constant__Speed__Constant__Rate.html#a5e77679758ffc9ab01462176a1bce1b0", null ], + [ "true_course", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Constant__Rate_1_1Constant__Speed__Constant__Rate.html#a071386f19ae816b44e99fa3a2aa31b3d", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Linear__Altitude_1_1Ca70c2a81d5de0f61273c53f05124d5dd.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Linear__Altitude_1_1Ca70c2a81d5de0f61273c53f05124d5dd.html index 7c43bd20..c4f57ea9 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Linear__Altitude_1_1Ca70c2a81d5de0f61273c53f05124d5dd.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Linear__Altitude_1_1Ca70c2a81d5de0f61273c53f05124d5dd.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Attributes

 air_speed
 
true_course
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle
 altitude_start
 altitude_end
 
true_course
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
 temperature_deviation
 process
 
conditions
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
 tag
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -98,30 +105,32 @@

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Linear_Altitude.Constant_Speed_Linear_Altitude, including all inherited members.

- + - - + + - + - - - - - - - - - - + + + + + + + + + + + +
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Linear_Altitude.Constant_Speed_Linear_Altitude
air_speed (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Linear_Altitude.Constant_Speed_Linear_Altitude)SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Linear_Altitude.Constant_Speed_Linear_Altitude
altitude (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Linear_Altitude.Constant_Speed_Linear_Altitude)SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Linear_Altitude.Constant_Speed_Linear_Altitude
altitude_end (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Linear_Altitude.Constant_Speed_Linear_Altitude)SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Linear_Altitude.Constant_Speed_Linear_Altitude
altitude_start (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Linear_Altitude.Constant_Speed_Linear_Altitude)SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Linear_Altitude.Constant_Speed_Linear_Altitude
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
conditions (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
distance (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Linear_Altitude.Constant_Speed_Linear_Altitude)SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Linear_Altitude.Constant_Speed_Linear_Altitude
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
SUAVE::Analyses::Analysis::Analysis.evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
finalize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
merged(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
true_course (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Linear_Altitude.Constant_Speed_Linear_Altitude)SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Linear_Altitude.Constant_Speed_Linear_Altitude
@@ -129,7 +138,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Linear__Altitude_1_1Cd58dc6a2d95bb161e2208f5800fce872.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Linear__Altitude_1_1Cd58dc6a2d95bb161e2208f5800fce872.html index 5acacf26..7b7d2a2d 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Linear__Altitude_1_1Cd58dc6a2d95bb161e2208f5800fce872.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Linear__Altitude_1_1Cd58dc6a2d95bb161e2208f5800fce872.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Linear_Altitude.Constant_Speed_Linear_Altitude Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -110,47 +117,37 @@ SUAVE.Analyses.Mission.Segments.Segment.Segment SUAVE.Analyses.Analysis.Analysis SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Linear_Altitude.Constant_Mach_Linear_Altitude - -
+ + - - - - - - - - - - + + - - - - - - + + + + + + - - - - - - - - - - - - + + + + + + + + + +

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def initialize (self)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def iterate (self)
 
def finalize (self)
 
def evaluate (self, state=None)
 
def merged (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
@@ -169,6 +166,9 @@ + + @@ -186,6 +186,9 @@ + + @@ -238,6 +241,10 @@

SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic.

+ +

Reimplemented in SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Linear_Altitude.Constant_Mach_Linear_Altitude.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Linear__Altitude_1_1Cd58dc6a2d95bb161e2208f5800fce872.js b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Linear__Altitude_1_1Cd58dc6a2d95bb161e2208f5800fce872.js index 84f247be..79ecefcf 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Linear__Altitude_1_1Cd58dc6a2d95bb161e2208f5800fce872.js +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Linear__Altitude_1_1Cd58dc6a2d95bb161e2208f5800fce872.js @@ -5,5 +5,6 @@ var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__L [ "altitude", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Linear__Altitude_1_1Cd58dc6a2d95bb161e2208f5800fce872.html#adb1446a8119c9f34de761caaf968ec7f", null ], [ "altitude_end", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Linear__Altitude_1_1Cd58dc6a2d95bb161e2208f5800fce872.html#a304bd6683ad9ed770e264ed4b59034a8", null ], [ "altitude_start", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Linear__Altitude_1_1Cd58dc6a2d95bb161e2208f5800fce872.html#a93a5d2af10c184dd576bc49c4ea2e83d", null ], - [ "distance", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Linear__Altitude_1_1Cd58dc6a2d95bb161e2208f5800fce872.html#afb62ff5eb7a8c0218df365d003c83985", null ] + [ "distance", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Linear__Altitude_1_1Cd58dc6a2d95bb161e2208f5800fce872.html#afb62ff5eb7a8c0218df365d003c83985", null ], + [ "true_course", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Speed__Linear__Altitude_1_1Cd58dc6a2d95bb161e2208f5800fce872.html#a56b3c073658c367a9de5ca70c7ddec8a", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Throttle__Constant__Speed_1_02b90ea2f234e748373e0a5403527689.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Throttle__Constant__Speed_1_02b90ea2f234e748373e0a5403527689.html index 4c20d6f1..594b2af1 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Throttle__Constant__Speed_1_02b90ea2f234e748373e0a5403527689.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Throttle__Constant__Speed_1_02b90ea2f234e748373e0a5403527689.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Mission.Segments.Climb.Constant_Throttle_Constant_Speed.Constant_Throttle_Constant_Speed Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Attributes

 altitude_end
 
true_course
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
 temperature_deviation
 process
 
conditions
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
 tag
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -109,47 +116,37 @@ SUAVE.Analyses.Mission.Segments.Simple.Simple SUAVE.Analyses.Mission.Segments.Segment.Segment SUAVE.Analyses.Analysis.Analysis - -
+ + - - - - - - - - - - + + - - - - - - + + + + + + - - - - - - - - - - - - + + + + + + + + + +

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def initialize (self)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def iterate (self)
 
def finalize (self)
 
def evaluate (self, state=None)
 
def merged (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
@@ -165,6 +162,9 @@ + + @@ -182,6 +182,9 @@ + + @@ -236,6 +239,8 @@

SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Throttle__Constant__Speed_1_02b90ea2f234e748373e0a5403527689.js b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Throttle__Constant__Speed_1_02b90ea2f234e748373e0a5403527689.js index 19854a95..cda03293 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Throttle__Constant__Speed_1_02b90ea2f234e748373e0a5403527689.js +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Throttle__Constant__Speed_1_02b90ea2f234e748373e0a5403527689.js @@ -4,5 +4,6 @@ var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Throttle [ "air_speed", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Throttle__Constant__Speed_1_02b90ea2f234e748373e0a5403527689.html#af44c9d2cbda7ae3ad64fb5ae259dbcbe", null ], [ "altitude_end", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Throttle__Constant__Speed_1_02b90ea2f234e748373e0a5403527689.html#a0b0300d65d3255bb5b13b05b40054b07", null ], [ "altitude_start", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Throttle__Constant__Speed_1_02b90ea2f234e748373e0a5403527689.html#aac4ecf672f3b9c52d65b994f5bd4884d", null ], - [ "throttle", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Throttle__Constant__Speed_1_02b90ea2f234e748373e0a5403527689.html#a73996582edfad573155a4c142bc2d53e", null ] + [ "throttle", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Throttle__Constant__Speed_1_02b90ea2f234e748373e0a5403527689.html#a73996582edfad573155a4c142bc2d53e", null ], + [ "true_course", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Throttle__Constant__Speed_1_02b90ea2f234e748373e0a5403527689.html#ab914c8539e446f7f9359bcc3d94b0e7d", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Throttle__Constant__Speed_1_5630685c5adb656512896887ec47e0bf.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Throttle__Constant__Speed_1_5630685c5adb656512896887ec47e0bf.html index 8aabc07e..3713bd7d 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Throttle__Constant__Speed_1_5630685c5adb656512896887ec47e0bf.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Throttle__Constant__Speed_1_5630685c5adb656512896887ec47e0bf.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Attributes

 air_speed
 
true_course
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
 temperature_deviation
 process
 
conditions
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
 tag
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -98,29 +105,31 @@

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Climb.Constant_Throttle_Constant_Speed.Constant_Throttle_Constant_Speed, including all inherited members.

- + - - + + - + - - - - - - - - - - - + + + + + + + + + + + + +
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Climb.Constant_Throttle_Constant_Speed.Constant_Throttle_Constant_Speed
air_speed (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Throttle_Constant_Speed.Constant_Throttle_Constant_Speed)SUAVE.Analyses.Mission.Segments.Climb.Constant_Throttle_Constant_Speed.Constant_Throttle_Constant_Speed
altitude_end (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Throttle_Constant_Speed.Constant_Throttle_Constant_Speed)SUAVE.Analyses.Mission.Segments.Climb.Constant_Throttle_Constant_Speed.Constant_Throttle_Constant_Speed
altitude_start (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Throttle_Constant_Speed.Constant_Throttle_Constant_Speed)SUAVE.Analyses.Mission.Segments.Climb.Constant_Throttle_Constant_Speed.Constant_Throttle_Constant_Speed
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
conditions (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
SUAVE::Analyses::Analysis::Analysis.evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
throttle (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Throttle_Constant_Speed.Constant_Throttle_Constant_Speed)SUAVE.Analyses.Mission.Segments.Climb.Constant_Throttle_Constant_Speed.Constant_Throttle_Constant_Speed
finalize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
merged(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
throttle (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Throttle_Constant_Speed.Constant_Throttle_Constant_Speed)SUAVE.Analyses.Mission.Segments.Climb.Constant_Throttle_Constant_Speed.Constant_Throttle_Constant_Speed
true_course (defined in SUAVE.Analyses.Mission.Segments.Climb.Constant_Throttle_Constant_Speed.Constant_Throttle_Constant_Speed)SUAVE.Analyses.Mission.Segments.Climb.Constant_Throttle_Constant_Speed.Constant_Throttle_Constant_Speed
@@ -128,7 +137,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Mach__Constant__Rate_1_1Linear__Mach__Constant__Rate-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Mach__Constant__Rate_1_1Linear__Mach__Constant__Rate-members.html index 3409678e..9042394f 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Mach__Constant__Rate_1_1Linear__Mach__Constant__Rate-members.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Mach__Constant__Rate_1_1Linear__Mach__Constant__Rate-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -98,30 +105,32 @@

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Climb.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate, including all inherited members.

- + - - + + - + - - - - - + + + + + - - - - - + + + + + + +
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Climb.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate
altitude_end (defined in SUAVE.Analyses.Mission.Segments.Climb.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate)SUAVE.Analyses.Mission.Segments.Climb.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate
altitude_start (defined in SUAVE.Analyses.Mission.Segments.Climb.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate)SUAVE.Analyses.Mission.Segments.Climb.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
climb_rate (defined in SUAVE.Analyses.Mission.Segments.Climb.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate)SUAVE.Analyses.Mission.Segments.Climb.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
conditions (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
SUAVE::Analyses::Analysis::Analysis.evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
finalize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
mach_end (defined in SUAVE.Analyses.Mission.Segments.Climb.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate)SUAVE.Analyses.Mission.Segments.Climb.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate
mach_start (defined in SUAVE.Analyses.Mission.Segments.Climb.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate)SUAVE.Analyses.Mission.Segments.Climb.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
merged(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
true_course (defined in SUAVE.Analyses.Mission.Segments.Climb.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate)SUAVE.Analyses.Mission.Segments.Climb.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate
@@ -129,7 +138,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Mach__Constant__Rate_1_1Linear__Mach__Constant__Rate.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Mach__Constant__Rate_1_1Linear__Mach__Constant__Rate.html index 6fa78a55..e5cab012 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Mach__Constant__Rate_1_1Linear__Mach__Constant__Rate.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Mach__Constant__Rate_1_1Linear__Mach__Constant__Rate.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Mission.Segments.Climb.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -110,50 +117,37 @@ SUAVE.Analyses.Mission.Segments.Simple.Simple SUAVE.Analyses.Mission.Segments.Segment.Segment SUAVE.Analyses.Analysis.Analysis - -
+ + - - - - - - - - - - - - - + + - - - - - - + + + + + + - - - - - - - - - - - - + + + + + + + + + +

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def initialize (self)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def iterate (self)
 
def finalize (self)
 
def evaluate (self, state=None)
 
def merged (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
@@ -172,6 +166,9 @@ + + @@ -179,6 +176,9 @@ + + @@ -196,6 +196,9 @@ + + @@ -248,6 +251,8 @@

SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Mach__Constant__Rate_1_1Linear__Mach__Constant__Rate.js b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Mach__Constant__Rate_1_1Linear__Mach__Constant__Rate.js index 0a2632a8..aa876383 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Mach__Constant__Rate_1_1Linear__Mach__Constant__Rate.js +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Mach__Constant__Rate_1_1Linear__Mach__Constant__Rate.js @@ -5,5 +5,6 @@ var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Mach__Cons [ "altitude_start", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Mach__Constant__Rate_1_1Linear__Mach__Constant__Rate.html#a9a66ce5c5769a5a7b3a2d6f368b3e7b3", null ], [ "climb_rate", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Mach__Constant__Rate_1_1Linear__Mach__Constant__Rate.html#a40a318890ae82ec9d0e010a1f6303723", null ], [ "mach_end", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Mach__Constant__Rate_1_1Linear__Mach__Constant__Rate.html#a07701c31258186edd0c40d33d2a83d10", null ], - [ "mach_start", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Mach__Constant__Rate_1_1Linear__Mach__Constant__Rate.html#ae33f23541e9729e7bed9e0331b036be6", null ] + [ "mach_start", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Mach__Constant__Rate_1_1Linear__Mach__Constant__Rate.html#ae33f23541e9729e7bed9e0331b036be6", null ], + [ "true_course", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Mach__Constant__Rate_1_1Linear__Mach__Constant__Rate.html#af3556e315d9a0fe9373676af143ebf20", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Speed__Constant__Rate_1_1Linea129dd2dcbc0fcf0bb1dbc899f23a2fdd.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Speed__Constant__Rate_1_1Linea129dd2dcbc0fcf0bb1dbc899f23a2fdd.html index 0cfa4c30..d40b1850 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Speed__Constant__Rate_1_1Linea129dd2dcbc0fcf0bb1dbc899f23a2fdd.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Speed__Constant__Rate_1_1Linea129dd2dcbc0fcf0bb1dbc899f23a2fdd.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Attributes

 mach_start
 
true_course
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle
 altitude_start
 altitude_end
 
true_course
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
 temperature_deviation
 process
 
conditions
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
 tag
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -98,7 +105,7 @@

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Climb.Linear_Speed_Constant_Rate.Linear_Speed_Constant_Rate, including all inherited members.

- + @@ -106,22 +113,24 @@ - - + + - + - - - - - - - - - - + + + + + + + + + + + +
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Climb.Linear_Speed_Constant_Rate.Linear_Speed_Constant_Rate
air_speed_end (defined in SUAVE.Analyses.Mission.Segments.Climb.Linear_Speed_Constant_Rate.Linear_Speed_Constant_Rate)SUAVE.Analyses.Mission.Segments.Climb.Linear_Speed_Constant_Rate.Linear_Speed_Constant_Rate
air_speed_start (defined in SUAVE.Analyses.Mission.Segments.Climb.Linear_Speed_Constant_Rate.Linear_Speed_Constant_Rate)SUAVE.Analyses.Mission.Segments.Climb.Linear_Speed_Constant_Rate.Linear_Speed_Constant_Rate
altitude_start (defined in SUAVE.Analyses.Mission.Segments.Climb.Linear_Speed_Constant_Rate.Linear_Speed_Constant_Rate)SUAVE.Analyses.Mission.Segments.Climb.Linear_Speed_Constant_Rate.Linear_Speed_Constant_Rate
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
climb_rate (defined in SUAVE.Analyses.Mission.Segments.Climb.Linear_Speed_Constant_Rate.Linear_Speed_Constant_Rate)SUAVE.Analyses.Mission.Segments.Climb.Linear_Speed_Constant_Rate.Linear_Speed_Constant_Rate
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
conditions (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
SUAVE::Analyses::Analysis::Analysis.evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
finalize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
merged(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
true_course (defined in SUAVE.Analyses.Mission.Segments.Climb.Linear_Speed_Constant_Rate.Linear_Speed_Constant_Rate)SUAVE.Analyses.Mission.Segments.Climb.Linear_Speed_Constant_Rate.Linear_Speed_Constant_Rate
@@ -129,7 +138,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Speed__Constant__Rate_1_1Linear__Speed__Constant__Rate.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Speed__Constant__Rate_1_1Linear__Speed__Constant__Rate.html index eb42f545..8ae7e965 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Speed__Constant__Rate_1_1Linear__Speed__Constant__Rate.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Speed__Constant__Rate_1_1Linear__Speed__Constant__Rate.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Mission.Segments.Climb.Linear_Speed_Constant_Rate.Linear_Speed_Constant_Rate Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -110,50 +117,37 @@ SUAVE.Analyses.Mission.Segments.Simple.Simple SUAVE.Analyses.Mission.Segments.Segment.Segment SUAVE.Analyses.Analysis.Analysis - -
+ + - - - - - - - - - - - - - + + - - - - - - + + + + + + - - - - - - - - - - - - + + + + + + + + + +

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def initialize (self)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def iterate (self)
 
def finalize (self)
 
def evaluate (self, state=None)
 
def merged (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
@@ -172,6 +166,9 @@ + + @@ -179,6 +176,9 @@ + + @@ -196,6 +196,9 @@ + + @@ -248,6 +251,8 @@

SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Speed__Constant__Rate_1_1Linear__Speed__Constant__Rate.js b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Speed__Constant__Rate_1_1Linear__Speed__Constant__Rate.js index 60760d11..e0f3e309 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Speed__Constant__Rate_1_1Linear__Speed__Constant__Rate.js +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Speed__Constant__Rate_1_1Linear__Speed__Constant__Rate.js @@ -5,5 +5,6 @@ var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Speed__Con [ "air_speed_start", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Speed__Constant__Rate_1_1Linear__Speed__Constant__Rate.html#ace9b207639faf169ec2b5d7232d2f851", null ], [ "altitude_end", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Speed__Constant__Rate_1_1Linear__Speed__Constant__Rate.html#aa472350edc7ccf74fe26d9b6b282dfc0", null ], [ "altitude_start", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Speed__Constant__Rate_1_1Linear__Speed__Constant__Rate.html#a18ed8f645570ccad3f87bf352ae76ad7", null ], - [ "climb_rate", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Speed__Constant__Rate_1_1Linear__Speed__Constant__Rate.html#a49fd27c4734fca69a5810b6406cb5b29", null ] + [ "climb_rate", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Speed__Constant__Rate_1_1Linear__Speed__Constant__Rate.html#a49fd27c4734fca69a5810b6406cb5b29", null ], + [ "true_course", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Linear__Speed__Constant__Rate_1_1Linear__Speed__Constant__Rate.html#ae70b1894a6f5bcfae007691ed0f4dd32", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Optimized_1_1Optimized-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Optimized_1_1Optimized-members.html index 0a5c024f..43ff428f 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Optimized_1_1Optimized-members.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Optimized_1_1Optimized-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Attributes

 air_speed_end
 
true_course
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle
 altitude_start
 altitude_end
 
true_course
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
 temperature_deviation
 process
 
conditions
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
 tag
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -98,7 +105,7 @@

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Climb.Optimized.Optimized, including all inherited members.

- + @@ -106,26 +113,28 @@ - - - - - - - - - - - - - - - - - - - - + + + + + + + + + + + + + + + + + + + + + +
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Climb.Optimized.Optimized
air_speed_end (defined in SUAVE.Analyses.Mission.Segments.Climb.Optimized.Optimized)SUAVE.Analyses.Mission.Segments.Climb.Optimized.Optimized
air_speed_start (defined in SUAVE.Analyses.Mission.Segments.Climb.Optimized.Optimized)SUAVE.Analyses.Mission.Segments.Climb.Optimized.Optimized
altitude_end (defined in SUAVE.Analyses.Mission.Segments.Climb.Optimized.Optimized)SUAVE.Analyses.Mission.Segments.Climb.Optimized.Optimized
altitude_start (defined in SUAVE.Analyses.Mission.Segments.Climb.Optimized.Optimized)SUAVE.Analyses.Mission.Segments.Climb.Optimized.Optimized
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
CL_limit (defined in SUAVE.Analyses.Mission.Segments.Climb.Optimized.Optimized)SUAVE.Analyses.Mission.Segments.Climb.Optimized.Optimized
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
minimize (defined in SUAVE.Analyses.Mission.Segments.Climb.Optimized.Optimized)SUAVE.Analyses.Mission.Segments.Climb.Optimized.Optimized
objective (defined in SUAVE.Analyses.Mission.Segments.Climb.Optimized.Optimized)SUAVE.Analyses.Mission.Segments.Climb.Optimized.Optimized
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
seed_climb_rate (defined in SUAVE.Analyses.Mission.Segments.Climb.Optimized.Optimized)SUAVE.Analyses.Mission.Segments.Climb.Optimized.Optimized
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
conditions (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
lift_coefficient_limit (defined in SUAVE.Analyses.Mission.Segments.Climb.Optimized.Optimized)SUAVE.Analyses.Mission.Segments.Climb.Optimized.Optimized
merged(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
minimize (defined in SUAVE.Analyses.Mission.Segments.Climb.Optimized.Optimized)SUAVE.Analyses.Mission.Segments.Climb.Optimized.Optimized
objective (defined in SUAVE.Analyses.Mission.Segments.Climb.Optimized.Optimized)SUAVE.Analyses.Mission.Segments.Climb.Optimized.Optimized
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
seed_climb_rate (defined in SUAVE.Analyses.Mission.Segments.Climb.Optimized.Optimized)SUAVE.Analyses.Mission.Segments.Climb.Optimized.Optimized
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
true_course (defined in SUAVE.Analyses.Mission.Segments.Climb.Optimized.Optimized)SUAVE.Analyses.Mission.Segments.Climb.Optimized.Optimized
@@ -133,7 +142,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Optimized_1_1Optimized.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Optimized_1_1Optimized.html index dc47d834..74edffbe 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Optimized_1_1Optimized.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Optimized_1_1Optimized.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Mission.Segments.Climb.Optimized.Optimized Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -109,47 +116,37 @@ SUAVE.Analyses.Mission.Segments.Simple.Simple SUAVE.Analyses.Mission.Segments.Segment.Segment SUAVE.Analyses.Analysis.Analysis - -
+ + - - - - - - - - - - + + - - - - - - + + + + + + - - - - - - - - - - - - + + + + + + + + + +

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def initialize (self)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def iterate (self)
 
def finalize (self)
 
def evaluate (self, state=None)
 
def merged (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
@@ -171,15 +168,18 @@ - - + + + + @@ -197,6 +197,9 @@ + + @@ -258,6 +261,8 @@

SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Optimized_1_1Optimized.js b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Optimized_1_1Optimized.js index 3a6037e6..ab0a7c16 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Optimized_1_1Optimized.js +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Optimized_1_1Optimized.js @@ -6,8 +6,9 @@ var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Optimized_1_1Optim [ "algorithm", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Optimized_1_1Optimized.html#add4e2c2ac32d02c3f60af84ff003dd13", null ], [ "altitude_end", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Optimized_1_1Optimized.html#a67c54349794979fface04e372950d873", null ], [ "altitude_start", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Optimized_1_1Optimized.html#ab5897ad1dd6b81818ed7fb3e327fc966", null ], - [ "CL_limit", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Optimized_1_1Optimized.html#a4264e59908c0bfbd8d108aa29ac26390", null ], + [ "lift_coefficient_limit", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Optimized_1_1Optimized.html#a4bedff47f5f538e355e2eb412b217550", null ], [ "minimize", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Optimized_1_1Optimized.html#a76881a8d85487cf9895c5fedf03c73af", null ], [ "objective", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Optimized_1_1Optimized.html#a2fc312d71dbe50df791b4a39236a843d", null ], - [ "seed_climb_rate", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Optimized_1_1Optimized.html#a7b31e6a6176ef917ee71d0979a7200fd", null ] + [ "seed_climb_rate", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Optimized_1_1Optimized.html#a7b31e6a6176ef917ee71d0979a7200fd", null ], + [ "true_course", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Optimized_1_1Optimized.html#a99a803c7da9ff1095489dd8bb376e6ca", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Unknown__Throttle_1_1Unknown__Throttle-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Unknown__Throttle_1_1Unknown__Throttle-members.html index 2c4c1b2b..8d08f608 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Unknown__Throttle_1_1Unknown__Throttle-members.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Unknown__Throttle_1_1Unknown__Throttle-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Attributes

 minimize
 
CL_limit
 
lift_coefficient_limit
 
 seed_climb_rate
 
 algorithm
 
true_course
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
 temperature_deviation
 process
 
conditions
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
 tag
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -98,27 +105,29 @@

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle, including all inherited members.

- + - - + + - + - - - - - - - - - - + + + + + + + + + + + +
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle
altitude_end (defined in SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle)SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle
altitude_start (defined in SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle)SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
conditions (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
SUAVE::Analyses::Analysis::Analysis.evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
finalize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
merged(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
true_course (defined in SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle)SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle
@@ -126,7 +135,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Unknown__Throttle_1_1Unknown__Throttle.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Unknown__Throttle_1_1Unknown__Throttle.html index 40299b8f..8052f5d6 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Unknown__Throttle_1_1Unknown__Throttle.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Unknown__Throttle_1_1Unknown__Throttle.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -109,61 +116,53 @@ SUAVE.Analyses.Mission.Segments.Simple.Simple SUAVE.Analyses.Mission.Segments.Segment.Segment SUAVE.Analyses.Analysis.Analysis -SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Angle.Constant_Dynamic_Pressure_Constant_Angle -SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Rate.Constant_Dynamic_Pressure_Constant_Rate -SUAVE.Analyses.Mission.Segments.Climb.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate -SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Angle.Constant_Mach_Constant_Angle -SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Rate.Constant_Mach_Constant_Rate -SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle -SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise -SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate -SUAVE.Analyses.Mission.Segments.Climb.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate -SUAVE.Analyses.Mission.Segments.Climb.Linear_Speed_Constant_Rate.Linear_Speed_Constant_Rate -SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle -SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise -SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate -SUAVE.Analyses.Mission.Segments.Descent.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate - -
+SUAVE.Analyses.Mission.Segments.Climb.Constant_CAS_Constant_Rate.Constant_CAS_Constant_Rate +SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Angle.Constant_Dynamic_Pressure_Constant_Angle +SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Rate.Constant_Dynamic_Pressure_Constant_Rate +SUAVE.Analyses.Mission.Segments.Climb.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate +SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Angle.Constant_Mach_Constant_Angle +SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Rate.Constant_Mach_Constant_Rate +SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle +SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise +SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate +SUAVE.Analyses.Mission.Segments.Climb.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate +SUAVE.Analyses.Mission.Segments.Climb.Linear_Speed_Constant_Rate.Linear_Speed_Constant_Rate +SUAVE.Analyses.Mission.Segments.Descent.Constant_CAS_Constant_Rate.Constant_CAS_Constant_Rate +SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle +SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise +SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate +SUAVE.Analyses.Mission.Segments.Descent.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate + + - - - - - - - - - - + + - - - - - - + + + + + + - - - - - - - - - - - - + + + + + + + + + +

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def initialize (self)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def iterate (self)
 
def finalize (self)
 
def evaluate (self, state=None)
 
def merged (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
@@ -173,6 +172,9 @@ + + @@ -190,6 +192,9 @@ + + @@ -243,6 +248,10 @@

SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic.

+ +

Reimplemented in SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise, SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise, SUAVE.Analyses.Mission.Segments.Climb.Constant_CAS_Constant_Rate.Constant_CAS_Constant_Rate, SUAVE.Analyses.Mission.Segments.Climb.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate, SUAVE.Analyses.Mission.Segments.Descent.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate, SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Angle.Constant_Dynamic_Pressure_Constant_Angle, SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Angle.Constant_Mach_Constant_Angle, SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Rate.Constant_Mach_Constant_Rate, SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle, SUAVE.Analyses.Mission.Segments.Climb.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate, SUAVE.Analyses.Mission.Segments.Climb.Linear_Speed_Constant_Rate.Linear_Speed_Constant_Rate, SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle, SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate, SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Rate.Constant_Dynamic_Pressure_Constant_Rate, SUAVE.Analyses.Mission.Segments.Descent.Constant_CAS_Constant_Rate.Constant_CAS_Constant_Rate, and SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Unknown__Throttle_1_1Unknown__Throttle.js b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Unknown__Throttle_1_1Unknown__Throttle.js index 89fb5b57..a9d67b95 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Unknown__Throttle_1_1Unknown__Throttle.js +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Unknown__Throttle_1_1Unknown__Throttle.js @@ -2,5 +2,6 @@ var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Unknown__Throttle_ [ [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Unknown__Throttle_1_1Unknown__Throttle.html#a5541c59036630b00676c81954b6ac2b0", null ], [ "altitude_end", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Unknown__Throttle_1_1Unknown__Throttle.html#a4163a7f22f1abbff8d4917ae5ef7c812", null ], - [ "altitude_start", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Unknown__Throttle_1_1Unknown__Throttle.html#a5d376c4c6c5076d614862ca1f78ebbae", null ] + [ "altitude_start", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Unknown__Throttle_1_1Unknown__Throttle.html#a5d376c4c6c5076d614862ca1f78ebbae", null ], + [ "true_course", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Unknown__Throttle_1_1Unknown__Throttle.html#a748a298e9de83a7e4f57d2ccefbf7777", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Unknown__Throttle_1_1Unknown__Throttle.png b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Unknown__Throttle_1_1Unknown__Throttle.png index 2b867b0b..1c17efc0 100644 Binary files a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Unknown__Throttle_1_1Unknown__Throttle.png and b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Unknown__Throttle_1_1Unknown__Throttle.png differ diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Aerodynamics_1_1Aerodynamics-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Aerodynamics_1_1Aerodynamics-members.html index 78dca720..84809394 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Aerodynamics_1_1Aerodynamics-members.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Aerodynamics_1_1Aerodynamics-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Attributes

 altitude_end
 
true_course
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
 temperature_deviation
 process
 
conditions
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
 tag
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -99,19 +106,20 @@

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics, including all inherited members.

- - + + - + - - - - - - - + + + + + + + +
__defaults__(self)SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics
aerodynamics (defined in SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics)SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics
compile(self)SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
aero_derivatives (defined in SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics)SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics
aerodynamics (defined in SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics)SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics
energies (defined in SUAVE.Analyses.Mission.Segments.Conditions.Basic.Basic)SUAVE.Analyses.Mission.Segments.Conditions.Basic.Basic
expand_rows(self, rows)SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
expand_rows(self, rows, override=False)SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
frames (defined in SUAVE.Analyses.Mission.Segments.Conditions.Basic.Basic)SUAVE.Analyses.Mission.Segments.Conditions.Basic.Basic
freestream (defined in SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics)SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics
ones_row(self, cols)SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
ones_row_m1(self, cols)SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
ones_row_m2(self, cols)SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
propulsion (defined in SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics)SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics
stability (defined in SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics)SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics
tag (defined in SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics)SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics
weights (defined in SUAVE.Analyses.Mission.Segments.Conditions.Basic.Basic)SUAVE.Analyses.Mission.Segments.Conditions.Basic.Basic
noise (defined in SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics)SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics
ones_row(self, cols)SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
ones_row_m1(self, cols)SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
ones_row_m2(self, cols)SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
propulsion (defined in SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics)SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics
stability (defined in SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics)SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics
tag (defined in SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics)SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics
weights (defined in SUAVE.Analyses.Mission.Segments.Conditions.Basic.Basic)SUAVE.Analyses.Mission.Segments.Conditions.Basic.Basic
@@ -119,7 +127,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Aerodynamics_1_1Aerodynamics.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Aerodynamics_1_1Aerodynamics.html index 90ddcb60..9f5e574f 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Aerodynamics_1_1Aerodynamics.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Aerodynamics_1_1Aerodynamics.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -108,16 +115,13 @@ SUAVE.Analyses.Mission.Segments.Conditions.Basic.Basic SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid - -
+ + - - - @@ -125,10 +129,8 @@ - - - - + +

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Conditions.Basic.Basic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
def ones_row (self, cols)
 
 
def ones_row_m2 (self, cols)
 
def expand_rows (self, rows)
 
def compile (self)
 
def expand_rows (self, rows, override=False)
 
@@ -144,9 +146,15 @@ + + + + @@ -160,6 +168,9 @@ + +

Public Attributes

 stability
 
aero_derivatives
 
 propulsion
 
noise
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Conditions.Basic.Basic
 tag
 energies
 
noise
 

Detailed Description

This builds upon Basic, which itself builds on conditions, to add the data structure for aerodynamic mission analyses.
@@ -202,6 +213,10 @@ 

SUAVE.Analyses.Mission.Segments.Conditions.Basic.Basic.

+ +

Reimplemented in SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid.

+


The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Aerodynamics_1_1Aerodynamics.js b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Aerodynamics_1_1Aerodynamics.js index ad5df9b5..b797279e 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Aerodynamics_1_1Aerodynamics.js +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Aerodynamics_1_1Aerodynamics.js @@ -1,8 +1,10 @@ var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Aerodynamics_1_1Aerodynamics = [ [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Aerodynamics_1_1Aerodynamics.html#a9ec64a71eda479dcc96205ddf7f5e5ab", null ], + [ "aero_derivatives", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Aerodynamics_1_1Aerodynamics.html#ac028ef8c2c143ee129dfab2f5c978961", null ], [ "aerodynamics", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Aerodynamics_1_1Aerodynamics.html#a07fe15613d8fc3bc3db2c7374b0ea8c3", null ], [ "freestream", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Aerodynamics_1_1Aerodynamics.html#a139f1fce458dda0ca1ce1fdf46ed1365", null ], + [ "noise", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Aerodynamics_1_1Aerodynamics.html#a626718038897e77f0da4192c4beecded", null ], [ "propulsion", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Aerodynamics_1_1Aerodynamics.html#accc2c5673276771640f4386881624a8f", null ], [ "stability", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Aerodynamics_1_1Aerodynamics.html#a1d1900314c6bf1ec5e76cb6bd1b9acbf", null ], [ "tag", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Aerodynamics_1_1Aerodynamics.html#a13da6892fa732bdd73c6943955a0880f", null ] diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Basic_1_1Basic-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Basic_1_1Basic-members.html index f8d9291e..07fe0ceb 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Basic_1_1Basic-members.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Basic_1_1Basic-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -99,10 +106,10 @@

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Conditions.Basic.Basic, including all inherited members.

- - - - + + + + @@ -115,7 +122,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Basic_1_1Basic.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Basic_1_1Basic.html index 9940257a..2c40701d 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Basic_1_1Basic.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Basic_1_1Basic.html @@ -1,9 +1,9 @@ - + - +SUAVE: SUAVE.Analyses.Mission.Segments.Conditions.Basic.Basic Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ @@ -57,9 +60,11 @@
__defaults__(self)SUAVE.Analyses.Mission.Segments.Conditions.Basic.Basic
compile(self)SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
energies (defined in SUAVE.Analyses.Mission.Segments.Conditions.Basic.Basic)SUAVE.Analyses.Mission.Segments.Conditions.Basic.Basic
expand_rows(self, rows)SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
frames (defined in SUAVE.Analyses.Mission.Segments.Conditions.Basic.Basic)SUAVE.Analyses.Mission.Segments.Conditions.Basic.Basic
energies (defined in SUAVE.Analyses.Mission.Segments.Conditions.Basic.Basic)SUAVE.Analyses.Mission.Segments.Conditions.Basic.Basic
expand_rows(self, rows, override=False)SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
frames (defined in SUAVE.Analyses.Mission.Segments.Conditions.Basic.Basic)SUAVE.Analyses.Mission.Segments.Conditions.Basic.Basic
noise (defined in SUAVE.Analyses.Mission.Segments.Conditions.Basic.Basic)SUAVE.Analyses.Mission.Segments.Conditions.Basic.Basic
ones_row(self, cols)SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
ones_row_m1(self, cols)SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
ones_row_m2(self, cols)SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -108,8 +115,8 @@ SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid - -
+ + @@ -122,10 +129,8 @@ - - - - + +

Public Member Functions

 
def ones_row_m2 (self, cols)
 
def expand_rows (self, rows)
 
def compile (self)
 
def expand_rows (self, rows, override=False)
 
@@ -141,6 +146,9 @@ + +

Public Attributes

 energies
 
noise
 

Detailed Description

Basic builds upon conditions to add the mission data structure. Here frames and weights are added.
@@ -183,6 +191,8 @@ 

SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid, and SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics.

+


The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Basic_1_1Basic.js b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Basic_1_1Basic.js index d520621c..de1cd058 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Basic_1_1Basic.js +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Basic_1_1Basic.js @@ -3,6 +3,7 @@ var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Basic_1_1Basi [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Basic_1_1Basic.html#a33cf70b301c2bd4dec84cdf25e0d4654", null ], [ "energies", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Basic_1_1Basic.html#ad76601aa5a94ec946eb91150a546bf8e", null ], [ "frames", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Basic_1_1Basic.html#a97e7b9dac9d400c0849a3eb266c085ab", null ], + [ "noise", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Basic_1_1Basic.html#ab027ccf1001b6092fe3f7f25bb356c2e", null ], [ "tag", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Basic_1_1Basic.html#ae8c92aa04bb8f8c0071610aeb08ed6fc", null ], [ "weights", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Basic_1_1Basic.html#aa57f1b5fa9100be9fad142509009b15a", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Conditions_1_1Conditions-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Conditions_1_1Conditions-members.html index 32548db9..b8af45b3 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Conditions_1_1Conditions-members.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Conditions_1_1Conditions-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -110,7 +116,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Conditions_1_1Conditions.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Conditions_1_1Conditions.html index 6d2104b8..8f9a5842 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Conditions_1_1Conditions.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Conditions_1_1Conditions.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -112,8 +119,8 @@ SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics SUAVE.Analyses.Mission.Segments.Conditions.State.Container SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid - -
+ + @@ -123,10 +130,8 @@ - - - - + +

Public Member Functions

 
def ones_row_m2 (self, cols)
 
def expand_rows (self, rows)
 
def compile (self)
 
def expand_rows (self, rows, override=False)
 

Detailed Description

Conditions are the magic Data that contains the information about the vehicle in flight.
@@ -139,57 +144,29 @@
     Source:
     None   
 

Member Function Documentation

- -

◆ compile()

+ +

◆ expand_rows()

- + - - + -
def SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions.compile def SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions.expand_rows (  self)self,
-
-
This is a call to expand_rows above...
-
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
- -

◆ expand_rows()

- -
-
- - - + + - + - + @@ -199,7 +176,7 @@

Makes a 1-D array the right size. Often used after a mission is initialized to size out the vectors to the
-    right size.
+    right size. Will not overwrite an array if it already exists, unless override is True.
 
     Assumptions:
     None
@@ -208,7 +185,8 @@ 

SUAVE.Analyses.Mission.Segments.Conditions.State.State.

+ @@ -361,7 +341,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Conditions_1_1Conditions.js b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Conditions_1_1Conditions.js index 7fa27476..5bec9e9e 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Conditions_1_1Conditions.js +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Conditions_1_1Conditions.js @@ -1,7 +1,6 @@ var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Conditions_1_1Conditions = [ - [ "compile", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Conditions_1_1Conditions.html#a68b9ddbff2a79ba6f82113b6fff779ed", null ], - [ "expand_rows", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Conditions_1_1Conditions.html#a03f3ac82ade9b5c1d59c975a08e7f3d6", null ], + [ "expand_rows", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Conditions_1_1Conditions.html#a118401c99d5286b01b63a01959a96fa8", null ], [ "ones_row", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Conditions_1_1Conditions.html#a52e41e484aba6222e3b6bf431812280a", null ], [ "ones_row_m1", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Conditions_1_1Conditions.html#ab683000137a722593d20fd2453d2377a", null ], [ "ones_row_m2", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Conditions_1_1Conditions.html#a630662cbe9f70d6bb5a72a7561d8cb8c", null ] diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Conditions_1_1expanded__array-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Conditions_1_1expanded__array-members.html new file mode 100644 index 00000000..2840a7b1 --- /dev/null +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Conditions_1_1expanded__array-members.html @@ -0,0 +1,124 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+

def SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions.expand_rows (  self, rows,
 rows override = False 
+ + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ + + + + + diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Conditions_1_1expanded__array.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Conditions_1_1expanded__array.html new file mode 100644 index 00000000..be8ddaf5 --- /dev/null +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Conditions_1_1expanded__array.html @@ -0,0 +1,376 @@ + + + + + + + +SUAVE: SUAVE.Analyses.Mission.Segments.Conditions.Conditions.expanded_array Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Analyses.Mission.Segments.Conditions.Conditions.expanded_array Class Reference
+
+
+
+Inheritance diagram for SUAVE.Analyses.Mission.Segments.Conditions.Conditions.expanded_array:
+
+
+ +
+ + + + + + + + + + + + +

+Public Member Functions

def __init__ (self, cols, adjustment)
 
def resize (self, rows)
 
def __call__ (self)
 
def __mul__ (self, other)
 
def __rmul__ (self, other)
 
+

Detailed Description

+
This is an array that will expand later when the mission is initialized. It is called specifically by conditions
+
+    Assumptions:
+    None
+    
+    Source:
+    None   
+

Constructor & Destructor Documentation

+ +

◆ __init__()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Analyses.Mission.Segments.Conditions.Conditions.expanded_array.__init__ ( self,
 cols,
 adjustment 
)
+
+
Initialization that sets expansion later
+
+    Assumptions:
+    None
+
+    Source:
+    N/A
+
+    Inputs:
+    self
+    cols       - columns                          [int]
+    adjustment - how much smaller                 [int]
+
+    Outputs:
+    N/A
+    
+    Properties Used:
+    N/A
+
+
+
+

Member Function Documentation

+ +

◆ __call__()

+ +
+
+ + + + + + + + +
def SUAVE.Analyses.Mission.Segments.Conditions.Conditions.expanded_array.__call__ ( self)
+
+
This returns the value and shape of the array as is
+
+    Assumptions:
+    None
+
+    Source:
+    N/A
+
+    Inputs:
+    self
+
+    Outputs:
+    np.array   - properly sized                   [array]
+    
+    Properties Used:
+    N/A
+
+
+
+ +

◆ __mul__()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Analyses.Mission.Segments.Conditions.Conditions.expanded_array.__mul__ ( self,
 other 
)
+
+
Performs multiplication and returns self
+
+    Assumptions:
+    None
+
+    Source:
+    N/A
+
+    Inputs:
+    self
+    other      - something can be multiplied      [float]
+
+    Outputs:
+    self
+    
+    Properties Used:
+    N/A
+
+
+
+ +

◆ __rmul__()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Analyses.Mission.Segments.Conditions.Conditions.expanded_array.__rmul__ ( self,
 other 
)
+
+
Performs multiplication and returns self
+
+    Assumptions:
+    None
+
+    Source:
+    N/A
+
+    Inputs:
+    self
+    other      - something can be multiplied      [float]
+
+    Outputs:
+    self
+    
+    Properties Used:
+    N/A
+
+
+
+ +

◆ resize()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Analyses.Mission.Segments.Conditions.Conditions.expanded_array.resize ( self,
 rows 
)
+
+
This function actually completes the resizing. After this it's no longer an expanded array. That way it
+    doesn't propogate virally. That means if one wishes to resize later the conditions need to be reset.
+
+    Assumptions:
+    None
+
+    Source:
+    N/A
+
+    Inputs:
+    self
+    rows       - rows                             [int]
+    v          - values (really self)             [int]
+
+    Outputs:
+    np.array   - properly sized                   [array]
+    
+    Properties Used:
+    N/A
+
+
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Analyses/Mission/Segments/Conditions/Conditions.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Conditions_1_1expanded__array.js b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Conditions_1_1expanded__array.js new file mode 100644 index 00000000..b565dcc6 --- /dev/null +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Conditions_1_1expanded__array.js @@ -0,0 +1,8 @@ +var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Conditions_1_1expanded__array = +[ + [ "__init__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Conditions_1_1expanded__array.html#a4f91e2cbb089004320db280bc12657cb", null ], + [ "__call__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Conditions_1_1expanded__array.html#aa22029d1d83d36ce7f21fecb9f85fd04", null ], + [ "__mul__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Conditions_1_1expanded__array.html#af9ec18b00b3e12f2940d7eeec307f936", null ], + [ "__rmul__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Conditions_1_1expanded__array.html#a8d7fc85a0697847201da3fabca7cddf1", null ], + [ "resize", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Conditions_1_1expanded__array.html#abbb9798dd8d76638b74c10f58dd8ca4d", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Conditions_1_1expanded__array.png b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Conditions_1_1expanded__array.png new file mode 100644 index 00000000..2b84edcd Binary files /dev/null and b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Conditions_1_1expanded__array.png differ diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Numerics_1_1Numerics-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Numerics_1_1Numerics-members.html index b220e187..eb06c888 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Numerics_1_1Numerics-members.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Numerics_1_1Numerics-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -99,19 +106,19 @@

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Conditions.Numerics.Numerics, including all inherited members.

- - - - - + + + + + - - - + + +
__defaults__(self)SUAVE.Analyses.Mission.Segments.Conditions.Numerics.Numerics
compile(self)SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
converged (defined in SUAVE.Analyses.Mission.Segments.Conditions.Numerics.Numerics)SUAVE.Analyses.Mission.Segments.Conditions.Numerics.Numerics
dimensionless (defined in SUAVE.Analyses.Mission.Segments.Conditions.Numerics.Numerics)SUAVE.Analyses.Mission.Segments.Conditions.Numerics.Numerics
discretization_method (defined in SUAVE.Analyses.Mission.Segments.Conditions.Numerics.Numerics)SUAVE.Analyses.Mission.Segments.Conditions.Numerics.Numerics
expand_rows(self, rows)SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
converged (defined in SUAVE.Analyses.Mission.Segments.Conditions.Numerics.Numerics)SUAVE.Analyses.Mission.Segments.Conditions.Numerics.Numerics
dimensionless (defined in SUAVE.Analyses.Mission.Segments.Conditions.Numerics.Numerics)SUAVE.Analyses.Mission.Segments.Conditions.Numerics.Numerics
discretization_method (defined in SUAVE.Analyses.Mission.Segments.Conditions.Numerics.Numerics)SUAVE.Analyses.Mission.Segments.Conditions.Numerics.Numerics
expand_rows(self, rows, override=False)SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
max_evaluations (defined in SUAVE.Analyses.Mission.Segments.Conditions.Numerics.Numerics)SUAVE.Analyses.Mission.Segments.Conditions.Numerics.Numerics
number_control_points (defined in SUAVE.Analyses.Mission.Segments.Conditions.Numerics.Numerics)SUAVE.Analyses.Mission.Segments.Conditions.Numerics.Numerics
ones_row(self, cols)SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
ones_row_m1(self, cols)SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
ones_row_m2(self, cols)SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
solver_jacobian (defined in SUAVE.Analyses.Mission.Segments.Conditions.Numerics.Numerics)SUAVE.Analyses.Mission.Segments.Conditions.Numerics.Numerics
tag (defined in SUAVE.Analyses.Mission.Segments.Conditions.Numerics.Numerics)SUAVE.Analyses.Mission.Segments.Conditions.Numerics.Numerics
time (defined in SUAVE.Analyses.Mission.Segments.Conditions.Numerics.Numerics)SUAVE.Analyses.Mission.Segments.Conditions.Numerics.Numerics
tolerance_boundary_conditions (defined in SUAVE.Analyses.Mission.Segments.Conditions.Numerics.Numerics)SUAVE.Analyses.Mission.Segments.Conditions.Numerics.Numerics
step_size (defined in SUAVE.Analyses.Mission.Segments.Conditions.Numerics.Numerics)SUAVE.Analyses.Mission.Segments.Conditions.Numerics.Numerics
tag (defined in SUAVE.Analyses.Mission.Segments.Conditions.Numerics.Numerics)SUAVE.Analyses.Mission.Segments.Conditions.Numerics.Numerics
time (defined in SUAVE.Analyses.Mission.Segments.Conditions.Numerics.Numerics)SUAVE.Analyses.Mission.Segments.Conditions.Numerics.Numerics
tolerance_solution (defined in SUAVE.Analyses.Mission.Segments.Conditions.Numerics.Numerics)SUAVE.Analyses.Mission.Segments.Conditions.Numerics.Numerics
@@ -120,7 +127,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Numerics_1_1Numerics.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Numerics_1_1Numerics.html index 8a725c2a..2e4306b8 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Numerics_1_1Numerics.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Numerics_1_1Numerics.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Mission.Segments.Conditions.Numerics.Numerics Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -106,8 +113,8 @@ SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions - -
+ + @@ -120,10 +127,8 @@ - - - - + +

Public Member Functions

 
def ones_row_m2 (self, cols)
 
def expand_rows (self, rows)
 
def compile (self)
 
def expand_rows (self, rows, override=False)
 
@@ -142,12 +147,15 @@ - - + + + + @@ -209,7 +217,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Numerics_1_1Numerics.js b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Numerics_1_1Numerics.js index cbae8437..c4cc4d4d 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Numerics_1_1Numerics.js +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Numerics_1_1Numerics.js @@ -4,10 +4,11 @@ var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Numerics_1_1N [ "converged", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Numerics_1_1Numerics.html#ae2bab85cf81c9e246a0df1c513561a41", null ], [ "dimensionless", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Numerics_1_1Numerics.html#a95220cd690832d99121b6e69e9147a37", null ], [ "discretization_method", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Numerics_1_1Numerics.html#a133ace39fb9764fc9a12059adce59254", null ], + [ "max_evaluations", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Numerics_1_1Numerics.html#ad8a887dd8188a97d0df901c96230fd8c", null ], [ "number_control_points", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Numerics_1_1Numerics.html#a97aeaf47ad936d48abaef004187cecc4", null ], [ "solver_jacobian", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Numerics_1_1Numerics.html#a7561d89f9d24e31e15504fddec3db13e", null ], + [ "step_size", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Numerics_1_1Numerics.html#a4adef8d2cc8acb4a2c4726025f1c4892", null ], [ "tag", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Numerics_1_1Numerics.html#aa7c571767bdb92e05cf2e5898a56f0ae", null ], [ "time", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Numerics_1_1Numerics.html#ab7cf6d3161d03acdb40e2ab9a3f0d354", null ], - [ "tolerance_boundary_conditions", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Numerics_1_1Numerics.html#a08ec8c2273d4d99758849a8202d96e35", null ], [ "tolerance_solution", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Numerics_1_1Numerics.html#ae026b6b1f8fb29b69ddbc0729f441aed", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Residuals_1_1Residuals-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Residuals_1_1Residuals-members.html index d2aed939..833c1f05 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Residuals_1_1Residuals-members.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Residuals_1_1Residuals-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Attributes

 tolerance_solution
 
tolerance_boundary_conditions
 
 converged
 
max_evaluations
 
step_size
 
 dimensionless
 
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -112,7 +118,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Residuals_1_1Residuals.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Residuals_1_1Residuals.html index e35d959a..8edad570 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Residuals_1_1Residuals.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Residuals_1_1Residuals.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Mission.Segments.Conditions.Residuals.Residuals Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -106,8 +113,8 @@ SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions - -
+ + @@ -120,10 +127,8 @@ - - - - + +

Public Member Functions

 
def ones_row_m2 (self, cols)
 
def expand_rows (self, rows)
 
def compile (self)
 
def expand_rows (self, rows, override=False)
 
@@ -185,7 +190,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1State_1_1Container-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1State_1_1Container-members.html index 3824d5fa..5272528b 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1State_1_1Container-members.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1State_1_1Container-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Attributes

SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -99,17 +106,17 @@

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Conditions.State.Container, including all inherited members.

- - - - - - - - - - - + + + + + + + + + + +
__defaults__(self)SUAVE.Analyses.Mission.Segments.Conditions.State.Container
compile(self)SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
conditions (defined in SUAVE.Analyses.Mission.Segments.Conditions.State.State)SUAVE.Analyses.Mission.Segments.Conditions.State.State
expand_rows(self, rows)SUAVE.Analyses.Mission.Segments.Conditions.State.State
initials (defined in SUAVE.Analyses.Mission.Segments.Conditions.State.State)SUAVE.Analyses.Mission.Segments.Conditions.State.State
merged(self)SUAVE.Analyses.Mission.Segments.Conditions.State.Container
numerics (defined in SUAVE.Analyses.Mission.Segments.Conditions.State.State)SUAVE.Analyses.Mission.Segments.Conditions.State.State
ones_row(self, cols)SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
ones_row_m1(self, cols)SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
ones_row_m2(self, cols)SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
residuals (defined in SUAVE.Analyses.Mission.Segments.Conditions.State.State)SUAVE.Analyses.Mission.Segments.Conditions.State.State
segments (defined in SUAVE.Analyses.Mission.Segments.Conditions.State.Container)SUAVE.Analyses.Mission.Segments.Conditions.State.Container
conditions (defined in SUAVE.Analyses.Mission.Segments.Conditions.State.State)SUAVE.Analyses.Mission.Segments.Conditions.State.State
expand_rows(self, rows, override=False)SUAVE.Analyses.Mission.Segments.Conditions.State.State
initials (defined in SUAVE.Analyses.Mission.Segments.Conditions.State.State)SUAVE.Analyses.Mission.Segments.Conditions.State.State
merged(self)SUAVE.Analyses.Mission.Segments.Conditions.State.Container
numerics (defined in SUAVE.Analyses.Mission.Segments.Conditions.State.State)SUAVE.Analyses.Mission.Segments.Conditions.State.State
ones_row(self, cols)SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
ones_row_m1(self, cols)SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
ones_row_m2(self, cols)SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
residuals (defined in SUAVE.Analyses.Mission.Segments.Conditions.State.State)SUAVE.Analyses.Mission.Segments.Conditions.State.State
segments (defined in SUAVE.Analyses.Mission.Segments.Conditions.State.Container)SUAVE.Analyses.Mission.Segments.Conditions.State.Container
tag (defined in SUAVE.Analyses.Mission.Segments.Conditions.State.State)SUAVE.Analyses.Mission.Segments.Conditions.State.State
unknowns (defined in SUAVE.Analyses.Mission.Segments.Conditions.State.State)SUAVE.Analyses.Mission.Segments.Conditions.State.State
@@ -118,7 +125,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1State_1_1Container.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1State_1_1Container.html index 0a01f77f..9b5e67af 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1State_1_1Container.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1State_1_1Container.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Mission.Segments.Conditions.State.Container Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -107,8 +114,8 @@ SUAVE.Analyses.Mission.Segments.Conditions.State.State SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions - -
+ + @@ -117,10 +124,8 @@ - - - - + + @@ -128,10 +133,6 @@ - - - -

Public Member Functions

def merged (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Conditions.State.State
def __defaults__ (self)
 
def expand_rows (self, rows)
 
def expand_rows (self, rows, override=False)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
def ones_row (self, cols)
 
 
def ones_row_m2 (self, cols)
 
def expand_rows (self, rows)
 
def compile (self)
 
@@ -139,6 +140,9 @@   + + @@ -188,6 +192,8 @@

SUAVE.Analyses.Mission.Segments.Conditions.State.State.

+ @@ -235,7 +241,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1State_1_1State-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1State_1_1State-members.html index be0ab4d1..75f1b17d 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1State_1_1State-members.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1State_1_1State-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Attributes

segments
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Conditions.State.State
tag
 
 unknowns
 
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -99,15 +106,15 @@

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Conditions.State.State, including all inherited members.

- - - - - - - - - + + + + + + + + +
__defaults__(self)SUAVE.Analyses.Mission.Segments.Conditions.State.State
compile(self)SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
conditions (defined in SUAVE.Analyses.Mission.Segments.Conditions.State.State)SUAVE.Analyses.Mission.Segments.Conditions.State.State
expand_rows(self, rows)SUAVE.Analyses.Mission.Segments.Conditions.State.State
initials (defined in SUAVE.Analyses.Mission.Segments.Conditions.State.State)SUAVE.Analyses.Mission.Segments.Conditions.State.State
numerics (defined in SUAVE.Analyses.Mission.Segments.Conditions.State.State)SUAVE.Analyses.Mission.Segments.Conditions.State.State
ones_row(self, cols)SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
ones_row_m1(self, cols)SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
ones_row_m2(self, cols)SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
residuals (defined in SUAVE.Analyses.Mission.Segments.Conditions.State.State)SUAVE.Analyses.Mission.Segments.Conditions.State.State
conditions (defined in SUAVE.Analyses.Mission.Segments.Conditions.State.State)SUAVE.Analyses.Mission.Segments.Conditions.State.State
expand_rows(self, rows, override=False)SUAVE.Analyses.Mission.Segments.Conditions.State.State
initials (defined in SUAVE.Analyses.Mission.Segments.Conditions.State.State)SUAVE.Analyses.Mission.Segments.Conditions.State.State
numerics (defined in SUAVE.Analyses.Mission.Segments.Conditions.State.State)SUAVE.Analyses.Mission.Segments.Conditions.State.State
ones_row(self, cols)SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
ones_row_m1(self, cols)SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
ones_row_m2(self, cols)SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
residuals (defined in SUAVE.Analyses.Mission.Segments.Conditions.State.State)SUAVE.Analyses.Mission.Segments.Conditions.State.State
tag (defined in SUAVE.Analyses.Mission.Segments.Conditions.State.State)SUAVE.Analyses.Mission.Segments.Conditions.State.State
unknowns (defined in SUAVE.Analyses.Mission.Segments.Conditions.State.State)SUAVE.Analyses.Mission.Segments.Conditions.State.State
@@ -116,7 +123,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1State_1_1State.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1State_1_1State.html index 15b7c40c..f01d10c8 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1State_1_1State.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1State_1_1State.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Mission.Segments.Conditions.State.State Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -107,15 +114,15 @@ SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions SUAVE.Analyses.Mission.Segments.Conditions.State.Container - -
+ + - - + + @@ -123,13 +130,12 @@ - - - -

Public Member Functions

def __defaults__ (self)
 
def expand_rows (self, rows)
 
def expand_rows (self, rows, override=False)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
def ones_row (self, cols)
 
 
def ones_row_m2 (self, cols)
 
def expand_rows (self, rows)
 
def compile (self)
 
+ + @@ -187,10 +193,12 @@

SUAVE.Analyses.Mission.Segments.Conditions.State.Container.

+ - -

◆ expand_rows()

+ +

◆ expand_rows()

@@ -205,7 +213,13 @@

- + + + + + + + @@ -215,7 +229,7 @@

Makes a 1-D array the right size. Often used after a mission is initialized to size out the vectors to the
-    right size.
+    right size. Will not overwrite an array if it already exists, unless override is True.
 
     Assumptions:
     Doesn't expand initials or numerics
@@ -232,6 +246,8 @@ 

SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1State_1_1State.js b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1State_1_1State.js index d7d1fb9b..554b8de5 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1State_1_1State.js +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1State_1_1State.js @@ -1,10 +1,11 @@ var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1State_1_1State = [ [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1State_1_1State.html#a9d59416b9049579bf19c234c3ab863d2", null ], - [ "expand_rows", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1State_1_1State.html#af4ea11668dee52410256e88a59854557", null ], + [ "expand_rows", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1State_1_1State.html#a707224b0cc6b96270c2a85ce85b6b59f", null ], [ "conditions", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1State_1_1State.html#a51990a4ffb54a995b7ea76c2a05637f7", null ], [ "initials", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1State_1_1State.html#acb90768b54f38ef26e41276b3b12d420", null ], [ "numerics", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1State_1_1State.html#a48045b581e869d5a67a53422d6843a77", null ], [ "residuals", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1State_1_1State.html#ab2154a0f530fdbef75be6a5e6c983167", null ], + [ "tag", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1State_1_1State.html#a67ce0bac4bd0d3a2ece9c8a754484e9d", null ], [ "unknowns", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1State_1_1State.html#a9bc1d1dddf44b75b0b1a41bc86b7c098", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Unknowns_1_1Unknowns-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Unknowns_1_1Unknowns-members.html index aa0e09ea..ec429182 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Unknowns_1_1Unknowns-members.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Unknowns_1_1Unknowns-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Attributes

tag
 
 unknowns
 
 rows rows,
 override = False 
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -112,7 +118,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Unknowns_1_1Unknowns.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Unknowns_1_1Unknowns.html index a933709f..9f3ed4a5 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Unknowns_1_1Unknowns.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Conditions_1_1Unknowns_1_1Unknowns.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Mission.Segments.Conditions.Unknowns.Unknowns Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -106,8 +113,8 @@ SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions - -
+ + @@ -120,10 +127,8 @@ - - - - + +

Public Member Functions

 
def ones_row_m2 (self, cols)
 
def expand_rows (self, rows)
 
def compile (self)
 
def expand_rows (self, rows, override=False)
 
@@ -185,7 +190,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Acceleration__Constant__Alt225ba2acb5f380a25088694295eaa3d1.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Acceleration__Constant__Alt225ba2acb5f380a25088694295eaa3d1.html index aa72d57b..6e477b34 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Acceleration__Constant__Alt225ba2acb5f380a25088694295eaa3d1.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Acceleration__Constant__Alt225ba2acb5f380a25088694295eaa3d1.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Mission.Segments.Cruise.Constant_Acceleration_Constant_Altitude.Constant_Acceleration_Constant_Altitude Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Attributes

SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -109,47 +116,37 @@ SUAVE.Analyses.Mission.Segments.Simple.Simple SUAVE.Analyses.Mission.Segments.Segment.Segment SUAVE.Analyses.Analysis.Analysis - -
+ + - - - - - - - - - - + + - - - - - - + + + + + + - - - - - - - - - - - - + + + + + + + + + +

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def initialize (self)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def iterate (self)
 
def finalize (self)
 
def evaluate (self, state=None)
 
def merged (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
@@ -165,6 +162,9 @@ + + @@ -182,6 +182,9 @@ + + @@ -234,6 +237,8 @@

SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Acceleration__Constant__Alt225ba2acb5f380a25088694295eaa3d1.js b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Acceleration__Constant__Alt225ba2acb5f380a25088694295eaa3d1.js index bca8da1c..42ff4bb8 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Acceleration__Constant__Alt225ba2acb5f380a25088694295eaa3d1.js +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Acceleration__Constant__Alt225ba2acb5f380a25088694295eaa3d1.js @@ -4,5 +4,6 @@ var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Acceler [ "acceleration", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Acceleration__Constant__Alt225ba2acb5f380a25088694295eaa3d1.html#a4dedcb5da3a186801fe8bed343c15064", null ], [ "air_speed_end", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Acceleration__Constant__Alt225ba2acb5f380a25088694295eaa3d1.html#a181b8f25335143d630bdcde21aef34e1", null ], [ "air_speed_start", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Acceleration__Constant__Alt225ba2acb5f380a25088694295eaa3d1.html#a69bd0b9baa712be94fa0042a4ea06358", null ], - [ "altitude", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Acceleration__Constant__Alt225ba2acb5f380a25088694295eaa3d1.html#a0ae8df4bb939228da3fb65bfc7966dca", null ] + [ "altitude", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Acceleration__Constant__Alt225ba2acb5f380a25088694295eaa3d1.html#a0ae8df4bb939228da3fb65bfc7966dca", null ], + [ "true_course", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Acceleration__Constant__Alt225ba2acb5f380a25088694295eaa3d1.html#af73bf53fbf7498124e51c163e22b77c3", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Acceleration__Constant__Altc5bd13c236150cb4a8fa295678e1052a.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Acceleration__Constant__Altc5bd13c236150cb4a8fa295678e1052a.html index 808396f6..f28b30fa 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Acceleration__Constant__Altc5bd13c236150cb4a8fa295678e1052a.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Acceleration__Constant__Altc5bd13c236150cb4a8fa295678e1052a.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Attributes

 air_speed_end
 
true_course
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
 temperature_deviation
 process
 
conditions
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
 tag
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -98,29 +105,31 @@

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Cruise.Constant_Acceleration_Constant_Altitude.Constant_Acceleration_Constant_Altitude, including all inherited members.

- + - - + + - + - - - - - - - - - - + + + + + + + + + + + +
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Acceleration_Constant_Altitude.Constant_Acceleration_Constant_Altitude
acceleration (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Acceleration_Constant_Altitude.Constant_Acceleration_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Acceleration_Constant_Altitude.Constant_Acceleration_Constant_Altitude
air_speed_end (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Acceleration_Constant_Altitude.Constant_Acceleration_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Acceleration_Constant_Altitude.Constant_Acceleration_Constant_Altitude
air_speed_start (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Acceleration_Constant_Altitude.Constant_Acceleration_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Acceleration_Constant_Altitude.Constant_Acceleration_Constant_Altitude
altitude (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Acceleration_Constant_Altitude.Constant_Acceleration_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Acceleration_Constant_Altitude.Constant_Acceleration_Constant_Altitude
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
conditions (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
SUAVE::Analyses::Analysis::Analysis.evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
finalize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
merged(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
true_course (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Acceleration_Constant_Altitude.Constant_Acceleration_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Acceleration_Constant_Altitude.Constant_Acceleration_Constant_Altitude
@@ -128,7 +137,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Dynamic__Pressure__Constant84b22d8b7fd8c219ab957928dcda16dd.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Dynamic__Pressure__Constant84b22d8b7fd8c219ab957928dcda16dd.html index 129444a1..7c651ed4 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Dynamic__Pressure__Constant84b22d8b7fd8c219ab957928dcda16dd.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Dynamic__Pressure__Constant84b22d8b7fd8c219ab957928dcda16dd.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -98,29 +105,31 @@

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude.Constant_Dynamic_Pressure_Constant_Altitude, including all inherited members.

- + - - + + - + - - - - - - - - - - + + + + + + + + + + + +
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude.Constant_Dynamic_Pressure_Constant_Altitude
air_speed (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude
altitude (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude.Constant_Dynamic_Pressure_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude.Constant_Dynamic_Pressure_Constant_Altitude
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
conditions (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
distance (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude.Constant_Dynamic_Pressure_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude.Constant_Dynamic_Pressure_Constant_Altitude
dynamic_pressure (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude.Constant_Dynamic_Pressure_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude.Constant_Dynamic_Pressure_Constant_Altitude
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
SUAVE::Analyses::Analysis::Analysis.evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
finalize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
merged(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
true_course (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude.Constant_Dynamic_Pressure_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude.Constant_Dynamic_Pressure_Constant_Altitude
@@ -128,7 +137,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Dynamic__Pressure__Constantd2bb54c5a6fd36eef28de53402e08b72.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Dynamic__Pressure__Constantd2bb54c5a6fd36eef28de53402e08b72.html index 33642fb6..fc464665 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Dynamic__Pressure__Constantd2bb54c5a6fd36eef28de53402e08b72.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Dynamic__Pressure__Constantd2bb54c5a6fd36eef28de53402e08b72.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude_Loiter.Constant_Dynamic_Pressure_Constant_Altitude_Loiter Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -110,50 +117,37 @@ SUAVE.Analyses.Mission.Segments.Simple.Simple SUAVE.Analyses.Mission.Segments.Segment.Segment SUAVE.Analyses.Analysis.Analysis - -
+ + - - - - - - - - - - - - - + + - - - - - - + + + + + + - - - - - - - - - - - - + + + + + + + + + +

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def initialize (self)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def iterate (self)
 
def finalize (self)
 
def evaluate (self, state=None)
 
def merged (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
@@ -166,6 +160,9 @@ + + @@ -176,6 +173,9 @@ + + @@ -193,6 +193,9 @@ + + @@ -246,6 +249,8 @@

SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Dynamic__Pressure__Constantd2bb54c5a6fd36eef28de53402e08b72.js b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Dynamic__Pressure__Constantd2bb54c5a6fd36eef28de53402e08b72.js index 7a7ac1e1..357e8e71 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Dynamic__Pressure__Constantd2bb54c5a6fd36eef28de53402e08b72.js +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Dynamic__Pressure__Constantd2bb54c5a6fd36eef28de53402e08b72.js @@ -3,5 +3,6 @@ var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Dynamic [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Dynamic__Pressure__Constantd2bb54c5a6fd36eef28de53402e08b72.html#aabba3d5f5adec918ddab99fcb697f664", null ], [ "altitude", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Dynamic__Pressure__Constantd2bb54c5a6fd36eef28de53402e08b72.html#a6cd8072c64c355f52edc3a5d85ae3049", null ], [ "dynamic_pressure", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Dynamic__Pressure__Constantd2bb54c5a6fd36eef28de53402e08b72.html#aef00f6c3292b2ceb71184b45e08bc6e6", null ], - [ "time", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Dynamic__Pressure__Constantd2bb54c5a6fd36eef28de53402e08b72.html#a91cbf24af9bbc2c3b1b10679306bca8e", null ] + [ "time", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Dynamic__Pressure__Constantd2bb54c5a6fd36eef28de53402e08b72.html#a91cbf24af9bbc2c3b1b10679306bca8e", null ], + [ "true_course", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Dynamic__Pressure__Constantd2bb54c5a6fd36eef28de53402e08b72.html#a0cd5d1e9d291364e574f40c9a9813b92", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Dynamic__Pressure__Constantd76ab8dcac489a382504762fcf2af994.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Dynamic__Pressure__Constantd76ab8dcac489a382504762fcf2af994.html index 6d03db59..d7465164 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Dynamic__Pressure__Constantd76ab8dcac489a382504762fcf2af994.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Dynamic__Pressure__Constantd76ab8dcac489a382504762fcf2af994.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude.Constant_Dynamic_Pressure_Constant_Altitude Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Attributes

 time
 
true_course
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude
 altitude
 distance
 
true_course
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
 temperature_deviation
 process
 
conditions
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
 tag
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -110,50 +117,37 @@ SUAVE.Analyses.Mission.Segments.Simple.Simple SUAVE.Analyses.Mission.Segments.Segment.Segment SUAVE.Analyses.Analysis.Analysis - -
+ + - - - - - - - - - - - - - + + - - - - - - + + + + + + - - - - - - - - - - - - + + + + + + + + + +

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def initialize (self)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def iterate (self)
 
def finalize (self)
 
def evaluate (self, state=None)
 
def merged (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
@@ -166,6 +160,9 @@ + + @@ -176,6 +173,9 @@ + + @@ -193,6 +193,9 @@ + + @@ -245,6 +248,8 @@

SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Dynamic__Pressure__Constantd76ab8dcac489a382504762fcf2af994.js b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Dynamic__Pressure__Constantd76ab8dcac489a382504762fcf2af994.js index 934d2fa1..e320d9c0 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Dynamic__Pressure__Constantd76ab8dcac489a382504762fcf2af994.js +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Dynamic__Pressure__Constantd76ab8dcac489a382504762fcf2af994.js @@ -3,5 +3,6 @@ var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Dynamic [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Dynamic__Pressure__Constantd76ab8dcac489a382504762fcf2af994.html#ab1723f047fa6d695e59f2d664b433e4a", null ], [ "altitude", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Dynamic__Pressure__Constantd76ab8dcac489a382504762fcf2af994.html#a2f69bc726928d18ce67c085726d0177b", null ], [ "distance", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Dynamic__Pressure__Constantd76ab8dcac489a382504762fcf2af994.html#a9abea90b164a73098a749e1a11557e95", null ], - [ "dynamic_pressure", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Dynamic__Pressure__Constantd76ab8dcac489a382504762fcf2af994.html#a0eb01c172c4f38d2be4d6222d052a2ae", null ] + [ "dynamic_pressure", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Dynamic__Pressure__Constantd76ab8dcac489a382504762fcf2af994.html#a0eb01c172c4f38d2be4d6222d052a2ae", null ], + [ "true_course", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Dynamic__Pressure__Constantd76ab8dcac489a382504762fcf2af994.html#a78f6bcdda8cd5517b1dcfde919a3b9ab", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Dynamic__Pressure__Constantf201c867d7444b46c0d67cf04180e6b4.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Dynamic__Pressure__Constantf201c867d7444b46c0d67cf04180e6b4.html index 72233013..15988d3d 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Dynamic__Pressure__Constantf201c867d7444b46c0d67cf04180e6b4.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Dynamic__Pressure__Constantf201c867d7444b46c0d67cf04180e6b4.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Attributes

 distance
 
true_course
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude
 altitude
 distance
 
true_course
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
 temperature_deviation
 process
 
conditions
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
 tag
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -98,30 +105,32 @@

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude_Loiter.Constant_Dynamic_Pressure_Constant_Altitude_Loiter, including all inherited members.

- + - - + + - + - - - - - - - - - - - + + + + + + + + + + + + +
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude_Loiter.Constant_Dynamic_Pressure_Constant_Altitude_Loiter
air_speed (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude
altitude (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude_Loiter.Constant_Dynamic_Pressure_Constant_Altitude_Loiter)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude_Loiter.Constant_Dynamic_Pressure_Constant_Altitude_Loiter
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
conditions (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
distance (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude
dynamic_pressure (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude_Loiter.Constant_Dynamic_Pressure_Constant_Altitude_Loiter)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude_Loiter.Constant_Dynamic_Pressure_Constant_Altitude_Loiter
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
SUAVE::Analyses::Analysis::Analysis.evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
time (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude_Loiter.Constant_Dynamic_Pressure_Constant_Altitude_Loiter)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude_Loiter.Constant_Dynamic_Pressure_Constant_Altitude_Loiter
finalize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
merged(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
time (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude_Loiter.Constant_Dynamic_Pressure_Constant_Altitude_Loiter)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude_Loiter.Constant_Dynamic_Pressure_Constant_Altitude_Loiter
true_course (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude_Loiter.Constant_Dynamic_Pressure_Constant_Altitude_Loiter)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude_Loiter.Constant_Dynamic_Pressure_Constant_Altitude_Loiter
@@ -129,7 +138,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Mach__Constant__Altitude_1_5e827e2c08a67cbe4900629aad1dc2d8.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Mach__Constant__Altitude_1_5e827e2c08a67cbe4900629aad1dc2d8.html index a0cf3f3c..dcee158e 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Mach__Constant__Altitude_1_5e827e2c08a67cbe4900629aad1dc2d8.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Mach__Constant__Altitude_1_5e827e2c08a67cbe4900629aad1dc2d8.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude.Constant_Mach_Constant_Altitude Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -110,50 +117,37 @@ SUAVE.Analyses.Mission.Segments.Simple.Simple SUAVE.Analyses.Mission.Segments.Segment.Segment SUAVE.Analyses.Analysis.Analysis - -
+ + - - - - - - - - - - - - - + + - - - - - - + + + + + + - - - - - - - - - - - - + + + + + + + + + +

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def initialize (self)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def iterate (self)
 
def finalize (self)
 
def evaluate (self, state=None)
 
def merged (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
@@ -166,6 +160,9 @@ + + @@ -176,6 +173,9 @@ + + @@ -193,6 +193,9 @@ + + @@ -245,6 +248,8 @@

SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Mach__Constant__Altitude_1_5e827e2c08a67cbe4900629aad1dc2d8.js b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Mach__Constant__Altitude_1_5e827e2c08a67cbe4900629aad1dc2d8.js index a9082707..bc61cbc9 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Mach__Constant__Altitude_1_5e827e2c08a67cbe4900629aad1dc2d8.js +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Mach__Constant__Altitude_1_5e827e2c08a67cbe4900629aad1dc2d8.js @@ -3,5 +3,6 @@ var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Mach__C [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Mach__Constant__Altitude_1_5e827e2c08a67cbe4900629aad1dc2d8.html#a7d8b2b080993d6463d0fe6802cbb420d", null ], [ "altitude", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Mach__Constant__Altitude_1_5e827e2c08a67cbe4900629aad1dc2d8.html#a19f94bf5f6fb32ca8d1620e31c50f16f", null ], [ "distance", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Mach__Constant__Altitude_1_5e827e2c08a67cbe4900629aad1dc2d8.html#a9f5f25d0a706c222a47183d9453b0557", null ], - [ "mach", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Mach__Constant__Altitude_1_5e827e2c08a67cbe4900629aad1dc2d8.html#a2222cb39160b743fdeac2c9a606ee74b", null ] + [ "mach", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Mach__Constant__Altitude_1_5e827e2c08a67cbe4900629aad1dc2d8.html#a2222cb39160b743fdeac2c9a606ee74b", null ], + [ "true_course", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Mach__Constant__Altitude_1_5e827e2c08a67cbe4900629aad1dc2d8.html#af4dffbc648d5bd22aa2f6d21113a6610", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Mach__Constant__Altitude_1_b588333bf5d262abe2e6a6f7a38d9137.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Mach__Constant__Altitude_1_b588333bf5d262abe2e6a6f7a38d9137.html index 5a56f897..9182bafb 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Mach__Constant__Altitude_1_b588333bf5d262abe2e6a6f7a38d9137.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Mach__Constant__Altitude_1_b588333bf5d262abe2e6a6f7a38d9137.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Attributes

 distance
 
true_course
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude
 altitude
 distance
 
true_course
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
 temperature_deviation
 process
 
conditions
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
 tag
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -98,29 +105,31 @@

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude.Constant_Mach_Constant_Altitude, including all inherited members.

- + - - + + - + - - - - - + + + + + - - - - - + + + + + + +
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude.Constant_Mach_Constant_Altitude
air_speed (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude
altitude (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude.Constant_Mach_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude.Constant_Mach_Constant_Altitude
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
conditions (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
distance (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude.Constant_Mach_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude.Constant_Mach_Constant_Altitude
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
SUAVE::Analyses::Analysis::Analysis.evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
finalize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
mach (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude.Constant_Mach_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude.Constant_Mach_Constant_Altitude
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
merged(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
true_course (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude.Constant_Mach_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude.Constant_Mach_Constant_Altitude
@@ -128,7 +137,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Mach__Constant__Altitude__L04d64fe23756079239c105324cc22cfa.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Mach__Constant__Altitude__L04d64fe23756079239c105324cc22cfa.html index 3a09250f..bafb731d 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Mach__Constant__Altitude__L04d64fe23756079239c105324cc22cfa.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Mach__Constant__Altitude__L04d64fe23756079239c105324cc22cfa.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -98,30 +105,32 @@

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude_Loiter.Constant_Mach_Constant_Altitude_Loiter, including all inherited members.

- + - - + + - + - - - - - + + + + + - - - - - - + + + + + + + +
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude_Loiter.Constant_Mach_Constant_Altitude_Loiter
air_speed (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude
altitude (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude_Loiter.Constant_Mach_Constant_Altitude_Loiter)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude_Loiter.Constant_Mach_Constant_Altitude_Loiter
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
conditions (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
distance (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
SUAVE::Analyses::Analysis::Analysis.evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
finalize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
mach (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude_Loiter.Constant_Mach_Constant_Altitude_Loiter)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude_Loiter.Constant_Mach_Constant_Altitude_Loiter
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
time (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude_Loiter.Constant_Mach_Constant_Altitude_Loiter)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude_Loiter.Constant_Mach_Constant_Altitude_Loiter
merged(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
time (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude_Loiter.Constant_Mach_Constant_Altitude_Loiter)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude_Loiter.Constant_Mach_Constant_Altitude_Loiter
true_course (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude_Loiter.Constant_Mach_Constant_Altitude_Loiter)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude_Loiter.Constant_Mach_Constant_Altitude_Loiter
@@ -129,7 +138,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Mach__Constant__Altitude__Le692539278d1a1cd0f056698409097dd.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Mach__Constant__Altitude__Le692539278d1a1cd0f056698409097dd.html index acfa15d3..6a5c5847 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Mach__Constant__Altitude__Le692539278d1a1cd0f056698409097dd.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Mach__Constant__Altitude__Le692539278d1a1cd0f056698409097dd.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude_Loiter.Constant_Mach_Constant_Altitude_Loiter Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -110,50 +117,37 @@ SUAVE.Analyses.Mission.Segments.Simple.Simple SUAVE.Analyses.Mission.Segments.Segment.Segment SUAVE.Analyses.Analysis.Analysis - -
+ + - - - - - - - - - - - - - + + - - - - - - + + + + + + - - - - - - - - - - - - + + + + + + + + + +

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def initialize (self)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def iterate (self)
 
def finalize (self)
 
def evaluate (self, state=None)
 
def merged (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
@@ -166,6 +160,9 @@ + + @@ -176,6 +173,9 @@ + + @@ -193,6 +193,9 @@ + + @@ -246,6 +249,8 @@

SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Mach__Constant__Altitude__Le692539278d1a1cd0f056698409097dd.js b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Mach__Constant__Altitude__Le692539278d1a1cd0f056698409097dd.js index 42329cc9..8226442a 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Mach__Constant__Altitude__Le692539278d1a1cd0f056698409097dd.js +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Mach__Constant__Altitude__Le692539278d1a1cd0f056698409097dd.js @@ -3,5 +3,6 @@ var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Mach__C [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Mach__Constant__Altitude__Le692539278d1a1cd0f056698409097dd.html#a5f06895f4371cca8ef17c0bd8ee0cfb3", null ], [ "altitude", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Mach__Constant__Altitude__Le692539278d1a1cd0f056698409097dd.html#a82967e479b30719add91689c5a5cee18", null ], [ "mach", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Mach__Constant__Altitude__Le692539278d1a1cd0f056698409097dd.html#adebcb0da04687157bd0833a1cedbbb07", null ], - [ "time", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Mach__Constant__Altitude__Le692539278d1a1cd0f056698409097dd.html#a1aa527b23bae81dfec302f67f54fed28", null ] + [ "time", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Mach__Constant__Altitude__Le692539278d1a1cd0f056698409097dd.html#a1aa527b23bae81dfec302f67f54fed28", null ], + [ "true_course", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Mach__Constant__Altitude__Le692539278d1a1cd0f056698409097dd.html#afdcbc2447c4b0f1cac35f703523a0806", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Pitch__Rate__Constant__Altibd22332dfa289fcd31fd0f99549c1e3e.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Pitch__Rate__Constant__Altibd22332dfa289fcd31fd0f99549c1e3e.html index d1feba36..e2ba9589 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Pitch__Rate__Constant__Altibd22332dfa289fcd31fd0f99549c1e3e.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Pitch__Rate__Constant__Altibd22332dfa289fcd31fd0f99549c1e3e.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Attributes

 time
 
true_course
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude
 altitude
 distance
 
true_course
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
 temperature_deviation
 process
 
conditions
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
 tag
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -98,29 +105,31 @@

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Cruise.Constant_Pitch_Rate_Constant_Altitude.Constant_Pitch_Rate_Constant_Altitude, including all inherited members.

- + - - + + - + - - - - - - - - - - - - - + + + + + + + + + + + + + + +
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Pitch_Rate_Constant_Altitude.Constant_Pitch_Rate_Constant_Altitude
altitude (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Pitch_Rate_Constant_Altitude.Constant_Pitch_Rate_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Pitch_Rate_Constant_Altitude.Constant_Pitch_Rate_Constant_Altitude
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
conditions (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
SUAVE::Analyses::Analysis::Analysis.evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
pitch_final (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Pitch_Rate_Constant_Altitude.Constant_Pitch_Rate_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Pitch_Rate_Constant_Altitude.Constant_Pitch_Rate_Constant_Altitude
pitch_initial (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Pitch_Rate_Constant_Altitude.Constant_Pitch_Rate_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Pitch_Rate_Constant_Altitude.Constant_Pitch_Rate_Constant_Altitude
pitch_rate (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Pitch_Rate_Constant_Altitude.Constant_Pitch_Rate_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Pitch_Rate_Constant_Altitude.Constant_Pitch_Rate_Constant_Altitude
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
finalize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
merged(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
pitch_final (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Pitch_Rate_Constant_Altitude.Constant_Pitch_Rate_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Pitch_Rate_Constant_Altitude.Constant_Pitch_Rate_Constant_Altitude
pitch_initial (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Pitch_Rate_Constant_Altitude.Constant_Pitch_Rate_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Pitch_Rate_Constant_Altitude.Constant_Pitch_Rate_Constant_Altitude
pitch_rate (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Pitch_Rate_Constant_Altitude.Constant_Pitch_Rate_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Pitch_Rate_Constant_Altitude.Constant_Pitch_Rate_Constant_Altitude
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
true_course (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Pitch_Rate_Constant_Altitude.Constant_Pitch_Rate_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Pitch_Rate_Constant_Altitude.Constant_Pitch_Rate_Constant_Altitude
@@ -128,7 +137,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Pitch__Rate__Constant__Altid7ab7e269824a308d0bb2c170f87d30a.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Pitch__Rate__Constant__Altid7ab7e269824a308d0bb2c170f87d30a.html index 4b42df02..f4a6903d 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Pitch__Rate__Constant__Altid7ab7e269824a308d0bb2c170f87d30a.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Pitch__Rate__Constant__Altid7ab7e269824a308d0bb2c170f87d30a.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Mission.Segments.Cruise.Constant_Pitch_Rate_Constant_Altitude.Constant_Pitch_Rate_Constant_Altitude Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -109,47 +116,37 @@ SUAVE.Analyses.Mission.Segments.Simple.Simple SUAVE.Analyses.Mission.Segments.Segment.Segment SUAVE.Analyses.Analysis.Analysis - -
+ + - - - - - - - - - - + + - - - - - - + + + + + + - - - - - - - - - - - - + + + + + + + + + +

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def initialize (self)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def iterate (self)
 
def finalize (self)
 
def evaluate (self, state=None)
 
def merged (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
@@ -165,6 +162,9 @@ + + @@ -182,6 +182,9 @@ + + @@ -235,6 +238,8 @@

SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Pitch__Rate__Constant__Altid7ab7e269824a308d0bb2c170f87d30a.js b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Pitch__Rate__Constant__Altid7ab7e269824a308d0bb2c170f87d30a.js index 8c0ee50a..521e5aa7 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Pitch__Rate__Constant__Altid7ab7e269824a308d0bb2c170f87d30a.js +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Pitch__Rate__Constant__Altid7ab7e269824a308d0bb2c170f87d30a.js @@ -4,5 +4,6 @@ var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Pitch__ [ "altitude", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Pitch__Rate__Constant__Altid7ab7e269824a308d0bb2c170f87d30a.html#a60e7db8c65bcd47fef2515d628127ff4", null ], [ "pitch_final", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Pitch__Rate__Constant__Altid7ab7e269824a308d0bb2c170f87d30a.html#a4df3f000a979b05ffcc771abaa8c052e", null ], [ "pitch_initial", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Pitch__Rate__Constant__Altid7ab7e269824a308d0bb2c170f87d30a.html#a0a711421b2c1ff525b4a1aa237694d40", null ], - [ "pitch_rate", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Pitch__Rate__Constant__Altid7ab7e269824a308d0bb2c170f87d30a.html#a33165c08eb8d491c4ffcbbe4ba9ef2e1", null ] + [ "pitch_rate", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Pitch__Rate__Constant__Altid7ab7e269824a308d0bb2c170f87d30a.html#a33165c08eb8d491c4ffcbbe4ba9ef2e1", null ], + [ "true_course", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Pitch__Rate__Constant__Altid7ab7e269824a308d0bb2c170f87d30a.html#aac34f4da146248081c294da05c098724", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Speed__Constant__Altitude_18f564c6bb76b2115e1fb0b0989b88720.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Speed__Constant__Altitude_18f564c6bb76b2115e1fb0b0989b88720.html index 78da10f2..d7047460 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Speed__Constant__Altitude_18f564c6bb76b2115e1fb0b0989b88720.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Speed__Constant__Altitude_18f564c6bb76b2115e1fb0b0989b88720.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Attributes

 pitch_final
 
true_course
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
 temperature_deviation
 process
 
conditions
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
 tag
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -98,28 +105,30 @@

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude, including all inherited members.

- + - - + + - + - - - - - - - - - - + + + + + + + + + + + +
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude
air_speed (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude
altitude (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
conditions (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
distance (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
SUAVE::Analyses::Analysis::Analysis.evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
finalize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
merged(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
true_course (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude
@@ -127,7 +136,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Speed__Constant__Altitude_1f9238ad770ff99e466228b3c4a43d18b.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Speed__Constant__Altitude_1f9238ad770ff99e466228b3c4a43d18b.html index a08e2898..71e58b1e 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Speed__Constant__Altitude_1f9238ad770ff99e466228b3c4a43d18b.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Speed__Constant__Altitude_1f9238ad770ff99e466228b3c4a43d18b.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -114,47 +121,37 @@ SUAVE.Analyses.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude.Constant_Mach_Constant_Altitude SUAVE.Analyses.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude_Loiter.Constant_Mach_Constant_Altitude_Loiter SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude_Loiter.Constant_Speed_Constant_Altitude_Loiter - -
+ + - - - - - - - - - - + + - - - - - - + + + + + + - - - - - - - - - - - - + + + + + + + + + +

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def initialize (self)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def iterate (self)
 
def finalize (self)
 
def evaluate (self, state=None)
 
def merged (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
@@ -167,6 +164,9 @@ + + @@ -184,6 +184,9 @@ + + @@ -237,6 +240,10 @@

SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic.

+ +

Reimplemented in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude_Loiter.Constant_Dynamic_Pressure_Constant_Altitude_Loiter, SUAVE.Analyses.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude_Loiter.Constant_Mach_Constant_Altitude_Loiter, SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude_Loiter.Constant_Speed_Constant_Altitude_Loiter, SUAVE.Analyses.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude.Constant_Dynamic_Pressure_Constant_Altitude, and SUAVE.Analyses.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude.Constant_Mach_Constant_Altitude.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Speed__Constant__Altitude_1f9238ad770ff99e466228b3c4a43d18b.js b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Speed__Constant__Altitude_1f9238ad770ff99e466228b3c4a43d18b.js index b2a41361..f466959f 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Speed__Constant__Altitude_1f9238ad770ff99e466228b3c4a43d18b.js +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Speed__Constant__Altitude_1f9238ad770ff99e466228b3c4a43d18b.js @@ -3,5 +3,6 @@ var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Speed__ [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Speed__Constant__Altitude_1f9238ad770ff99e466228b3c4a43d18b.html#ac08d33a39d5aac732a1834dc4c34a033", null ], [ "air_speed", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Speed__Constant__Altitude_1f9238ad770ff99e466228b3c4a43d18b.html#a894853f8ec11e54beaf3ce8c69424441", null ], [ "altitude", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Speed__Constant__Altitude_1f9238ad770ff99e466228b3c4a43d18b.html#a3fef73e1e7145c5524bb8c149f92a216", null ], - [ "distance", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Speed__Constant__Altitude_1f9238ad770ff99e466228b3c4a43d18b.html#a19e019305903b3b2c83f96894694912a", null ] + [ "distance", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Speed__Constant__Altitude_1f9238ad770ff99e466228b3c4a43d18b.html#a19e019305903b3b2c83f96894694912a", null ], + [ "true_course", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Speed__Constant__Altitude_1f9238ad770ff99e466228b3c4a43d18b.html#a1c710338347061f4d253e265295ee518", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Speed__Constant__Altitude__467b5797fe6882a2f528d361be26a113.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Speed__Constant__Altitude__467b5797fe6882a2f528d361be26a113.html index b3092b28..9865f6c5 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Speed__Constant__Altitude__467b5797fe6882a2f528d361be26a113.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Speed__Constant__Altitude__467b5797fe6882a2f528d361be26a113.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Attributes

 distance
 
true_course
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
 temperature_deviation
 process
 
conditions
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
 tag
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -98,29 +105,31 @@

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude_Loiter.Constant_Speed_Constant_Altitude_Loiter, including all inherited members.

- + - - + + - + - - - - - - - - - - - + + + + + + + + + + + + +
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude_Loiter.Constant_Speed_Constant_Altitude_Loiter
air_speed (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude_Loiter.Constant_Speed_Constant_Altitude_Loiter)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude_Loiter.Constant_Speed_Constant_Altitude_Loiter
altitude (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude_Loiter.Constant_Speed_Constant_Altitude_Loiter)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude_Loiter.Constant_Speed_Constant_Altitude_Loiter
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
conditions (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
distance (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
SUAVE::Analyses::Analysis::Analysis.evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
time (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude_Loiter.Constant_Speed_Constant_Altitude_Loiter)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude_Loiter.Constant_Speed_Constant_Altitude_Loiter
finalize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
merged(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
time (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude_Loiter.Constant_Speed_Constant_Altitude_Loiter)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude_Loiter.Constant_Speed_Constant_Altitude_Loiter
true_course (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude_Loiter.Constant_Speed_Constant_Altitude_Loiter)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude_Loiter.Constant_Speed_Constant_Altitude_Loiter
@@ -128,7 +137,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Speed__Constant__Altitude__fa03d2425e79228138954539409d2195.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Speed__Constant__Altitude__fa03d2425e79228138954539409d2195.html index bdd0b869..0e577ff5 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Speed__Constant__Altitude__fa03d2425e79228138954539409d2195.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Speed__Constant__Altitude__fa03d2425e79228138954539409d2195.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude_Loiter.Constant_Speed_Constant_Altitude_Loiter Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -110,50 +117,37 @@ SUAVE.Analyses.Mission.Segments.Simple.Simple SUAVE.Analyses.Mission.Segments.Segment.Segment SUAVE.Analyses.Analysis.Analysis - -
+ + - - - - - - - - - - - - - + + - - - - - - + + + + + + - - - - - - - - - - - - + + + + + + + + + +

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def initialize (self)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def iterate (self)
 
def finalize (self)
 
def evaluate (self, state=None)
 
def merged (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
@@ -166,6 +160,9 @@ + + @@ -176,6 +173,9 @@ + + @@ -193,6 +193,9 @@ + + @@ -246,6 +249,8 @@

SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Speed__Constant__Altitude__fa03d2425e79228138954539409d2195.js b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Speed__Constant__Altitude__fa03d2425e79228138954539409d2195.js index b31afef8..866cecc1 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Speed__Constant__Altitude__fa03d2425e79228138954539409d2195.js +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Speed__Constant__Altitude__fa03d2425e79228138954539409d2195.js @@ -3,5 +3,6 @@ var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Speed__ [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Speed__Constant__Altitude__fa03d2425e79228138954539409d2195.html#a4958b4d5ef63b8904d06aa5aac837509", null ], [ "air_speed", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Speed__Constant__Altitude__fa03d2425e79228138954539409d2195.html#a73c7b378aa0b5718c378b6b5c761e8df", null ], [ "altitude", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Speed__Constant__Altitude__fa03d2425e79228138954539409d2195.html#ac661b21ede548701bac1dd471d52c5e9", null ], - [ "time", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Speed__Constant__Altitude__fa03d2425e79228138954539409d2195.html#a01ff1a698df40df8ab82a6bd94676a36", null ] + [ "time", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Speed__Constant__Altitude__fa03d2425e79228138954539409d2195.html#a01ff1a698df40df8ab82a6bd94676a36", null ], + [ "true_course", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Speed__Constant__Altitude__fa03d2425e79228138954539409d2195.html#a24994b7a1be2fe1ff1d5a86215e1d7d8", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Throttle__Constant__Altitud087b9361606d9421bb3adf969d22c3d7.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Throttle__Constant__Altitud087b9361606d9421bb3adf969d22c3d7.html index 8ab558be..b4d89c7b 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Throttle__Constant__Altitud087b9361606d9421bb3adf969d22c3d7.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Throttle__Constant__Altitud087b9361606d9421bb3adf969d22c3d7.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Mission.Segments.Cruise.Constant_Throttle_Constant_Altitude.Constant_Throttle_Constant_Altitude Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Attributes

 time
 
true_course
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude
 altitude
 distance
 
true_course
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
 temperature_deviation
 process
 
conditions
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
 tag
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -109,47 +116,37 @@ SUAVE.Analyses.Mission.Segments.Simple.Simple SUAVE.Analyses.Mission.Segments.Segment.Segment SUAVE.Analyses.Analysis.Analysis - -
+ + - - - - - - - - - - + + - - - - - - + + + + + + - - - - - - - - - - - - + + + + + + + + + +

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def initialize (self)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def iterate (self)
 
def finalize (self)
 
def evaluate (self, state=None)
 
def merged (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
@@ -165,6 +162,9 @@ + + @@ -182,6 +182,9 @@ + + @@ -234,6 +237,8 @@

SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Throttle__Constant__Altitud087b9361606d9421bb3adf969d22c3d7.js b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Throttle__Constant__Altitud087b9361606d9421bb3adf969d22c3d7.js index ec6baa02..bf95f04f 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Throttle__Constant__Altitud087b9361606d9421bb3adf969d22c3d7.js +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Throttle__Constant__Altitud087b9361606d9421bb3adf969d22c3d7.js @@ -4,5 +4,6 @@ var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Throttl [ "air_speed_end", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Throttle__Constant__Altitud087b9361606d9421bb3adf969d22c3d7.html#a8ac186fce3147771184f518da49309e9", null ], [ "air_speed_start", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Throttle__Constant__Altitud087b9361606d9421bb3adf969d22c3d7.html#a211059093e2b63971f53b3b29cbe2cc1", null ], [ "altitude", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Throttle__Constant__Altitud087b9361606d9421bb3adf969d22c3d7.html#a0acce9610081c654dc2d9eefb0033e79", null ], - [ "throttle", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Throttle__Constant__Altitud087b9361606d9421bb3adf969d22c3d7.html#a9c3834d7b80dbf89ee79ef10d8909c8f", null ] + [ "throttle", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Throttle__Constant__Altitud087b9361606d9421bb3adf969d22c3d7.html#a9c3834d7b80dbf89ee79ef10d8909c8f", null ], + [ "true_course", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Throttle__Constant__Altitud087b9361606d9421bb3adf969d22c3d7.html#a3b46263af6744883af0f2d4d81016970", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Throttle__Constant__Altitudce228370873e346df4c962017addcbe3.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Throttle__Constant__Altitudce228370873e346df4c962017addcbe3.html index bbff8af3..4774122a 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Throttle__Constant__Altitudce228370873e346df4c962017addcbe3.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Cruise_1_1Constant__Throttle__Constant__Altitudce228370873e346df4c962017addcbe3.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Attributes

 air_speed_end
 
true_course
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
 temperature_deviation
 process
 
conditions
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
 tag
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -98,29 +105,31 @@

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Cruise.Constant_Throttle_Constant_Altitude.Constant_Throttle_Constant_Altitude, including all inherited members.

- + - - + + - + - - - - - - - - - - - + + + + + + + + + + + + +
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Throttle_Constant_Altitude.Constant_Throttle_Constant_Altitude
air_speed_end (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Throttle_Constant_Altitude.Constant_Throttle_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Throttle_Constant_Altitude.Constant_Throttle_Constant_Altitude
air_speed_start (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Throttle_Constant_Altitude.Constant_Throttle_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Throttle_Constant_Altitude.Constant_Throttle_Constant_Altitude
altitude (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Throttle_Constant_Altitude.Constant_Throttle_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Throttle_Constant_Altitude.Constant_Throttle_Constant_Altitude
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
conditions (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
SUAVE::Analyses::Analysis::Analysis.evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
throttle (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Throttle_Constant_Altitude.Constant_Throttle_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Throttle_Constant_Altitude.Constant_Throttle_Constant_Altitude
finalize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
merged(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
throttle (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Throttle_Constant_Altitude.Constant_Throttle_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Throttle_Constant_Altitude.Constant_Throttle_Constant_Altitude
true_course (defined in SUAVE.Analyses.Mission.Segments.Cruise.Constant_Throttle_Constant_Altitude.Constant_Throttle_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Cruise.Constant_Throttle_Constant_Altitude.Constant_Throttle_Constant_Altitude
@@ -128,7 +137,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__CAS__Constant__Rate_1_1Confd26ed3dfcec3513c23c67af3a4cb435.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__CAS__Constant__Rate_1_1Confd26ed3dfcec3513c23c67af3a4cb435.html new file mode 100644 index 00000000..a2dcebcd --- /dev/null +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__CAS__Constant__Rate_1_1Confd26ed3dfcec3513c23c67af3a4cb435.html @@ -0,0 +1,144 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
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+
SUAVE.Analyses.Mission.Segments.Descent.Constant_CAS_Constant_Rate.Constant_CAS_Constant_Rate Member List
+
+
+ +

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Descent.Constant_CAS_Constant_Rate.Constant_CAS_Constant_Rate, including all inherited members.

+ + + + + + + + + + + + + + + + + + + + + + + + + + +
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Descent.Constant_CAS_Constant_Rate.Constant_CAS_Constant_Rate
altitude_end (defined in SUAVE.Analyses.Mission.Segments.Descent.Constant_CAS_Constant_Rate.Constant_CAS_Constant_Rate)SUAVE.Analyses.Mission.Segments.Descent.Constant_CAS_Constant_Rate.Constant_CAS_Constant_Rate
altitude_start (defined in SUAVE.Analyses.Mission.Segments.Descent.Constant_CAS_Constant_Rate.Constant_CAS_Constant_Rate)SUAVE.Analyses.Mission.Segments.Descent.Constant_CAS_Constant_Rate.Constant_CAS_Constant_Rate
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
calibrated_airspeed (defined in SUAVE.Analyses.Mission.Segments.Descent.Constant_CAS_Constant_Rate.Constant_CAS_Constant_Rate)SUAVE.Analyses.Mission.Segments.Descent.Constant_CAS_Constant_Rate.Constant_CAS_Constant_Rate
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
conditions (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
descent_rate (defined in SUAVE.Analyses.Mission.Segments.Descent.Constant_CAS_Constant_Rate.Constant_CAS_Constant_Rate)SUAVE.Analyses.Mission.Segments.Descent.Constant_CAS_Constant_Rate.Constant_CAS_Constant_Rate
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
merged(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
true_course (defined in SUAVE.Analyses.Mission.Segments.Descent.Constant_CAS_Constant_Rate.Constant_CAS_Constant_Rate)SUAVE.Analyses.Mission.Segments.Descent.Constant_CAS_Constant_Rate.Constant_CAS_Constant_Rate
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__CAS__Constant__Rate_1_1Constant__CAS__Constant__Rate.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__CAS__Constant__Rate_1_1Constant__CAS__Constant__Rate.html new file mode 100644 index 00000000..5c6d78bb --- /dev/null +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__CAS__Constant__Rate_1_1Constant__CAS__Constant__Rate.html @@ -0,0 +1,262 @@ + + + + + + + +SUAVE: SUAVE.Analyses.Mission.Segments.Descent.Constant_CAS_Constant_Rate.Constant_CAS_Constant_Rate Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Analyses.Mission.Segments.Descent.Constant_CAS_Constant_Rate.Constant_CAS_Constant_Rate Class Reference
+
+
+
+Inheritance diagram for SUAVE.Analyses.Mission.Segments.Descent.Constant_CAS_Constant_Rate.Constant_CAS_Constant_Rate:
+
+
+ + +SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle +SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic +SUAVE.Analyses.Mission.Segments.Simple.Simple +SUAVE.Analyses.Mission.Segments.Segment.Segment +SUAVE.Analyses.Analysis.Analysis + +
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def initialize (self)
 
def converge (self, state)
 
def iterate (self)
 
def finalize (self)
 
def evaluate (self, state=None)
 
def merged (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Attributes

altitude_start
 
altitude_end
 
descent_rate
 
calibrated_airspeed
 
true_course
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle
altitude_start
 
altitude_end
 
true_course
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
temperature_deviation
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
settings
 
state
 
analyses
 
process
 
conditions
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
+

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Analyses.Mission.Segments.Descent.Constant_CAS_Constant_Rate.Constant_CAS_Constant_Rate.__defaults__ ( self)
+
+
This sets the default solver flow. Anything in here can be modified after initializing a segment.
+    
+    Assumptions:
+    None
+    
+    Source:
+    N/A
+    
+    Inputs:
+    None
+    
+    Outputs:
+    None
+    
+    Properties Used:
+    None
+
+

Reimplemented from SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle.

+ +
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Analyses/Mission/Segments/Descent/Constant_CAS_Constant_Rate.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__CAS__Constant__Rate_1_1Constant__CAS__Constant__Rate.js b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__CAS__Constant__Rate_1_1Constant__CAS__Constant__Rate.js new file mode 100644 index 00000000..1b84fa56 --- /dev/null +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__CAS__Constant__Rate_1_1Constant__CAS__Constant__Rate.js @@ -0,0 +1,9 @@ +var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__CAS__Constant__Rate_1_1Constant__CAS__Constant__Rate = +[ + [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__CAS__Constant__Rate_1_1Constant__CAS__Constant__Rate.html#ae7f3e00ae8cf3f69347dc5ddc90deec0", null ], + [ "altitude_end", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__CAS__Constant__Rate_1_1Constant__CAS__Constant__Rate.html#a279b6c675188bf2d3fb5f6e54626138f", null ], + [ "altitude_start", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__CAS__Constant__Rate_1_1Constant__CAS__Constant__Rate.html#a4fd055a4f4738de0f8c601b56c420bd2", null ], + [ "calibrated_airspeed", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__CAS__Constant__Rate_1_1Constant__CAS__Constant__Rate.html#a3786a0dfe8e33ed58e0edd3d6bd904ee", null ], + [ "descent_rate", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__CAS__Constant__Rate_1_1Constant__CAS__Constant__Rate.html#ae788bc897eee529fd21767ad212a1f54", null ], + [ "true_course", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__CAS__Constant__Rate_1_1Constant__CAS__Constant__Rate.html#a76dea8d7261a288d395ee0121a2509d5", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__CAS__Constant__Rate_1_1Constant__CAS__Constant__Rate.png b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__CAS__Constant__Rate_1_1Constant__CAS__Constant__Rate.png new file mode 100644 index 00000000..59a9e572 Binary files /dev/null and b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__CAS__Constant__Rate_1_1Constant__CAS__Constant__Rate.png differ diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__EAS__Constant__Rate_1_1Con60fcaf9d1adb0d2602b65938abb41d71.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__EAS__Constant__Rate_1_1Con60fcaf9d1adb0d2602b65938abb41d71.html index c71a20e8..68ed5497 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__EAS__Constant__Rate_1_1Con60fcaf9d1adb0d2602b65938abb41d71.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__EAS__Constant__Rate_1_1Con60fcaf9d1adb0d2602b65938abb41d71.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -98,29 +105,31 @@

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Descent.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate, including all inherited members.

- + - - + + - + - - - - - - - - - - + + + + + + + + + + + +
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Descent.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate
altitude_end (defined in SUAVE.Analyses.Mission.Segments.Descent.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate)SUAVE.Analyses.Mission.Segments.Descent.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate
altitude_start (defined in SUAVE.Analyses.Mission.Segments.Descent.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate)SUAVE.Analyses.Mission.Segments.Descent.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
conditions (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
descent_rate (defined in SUAVE.Analyses.Mission.Segments.Descent.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate)SUAVE.Analyses.Mission.Segments.Descent.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate
equivalent_air_speed (defined in SUAVE.Analyses.Mission.Segments.Descent.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate)SUAVE.Analyses.Mission.Segments.Descent.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
SUAVE::Analyses::Analysis::Analysis.evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
finalize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
merged(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
true_course (defined in SUAVE.Analyses.Mission.Segments.Descent.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate)SUAVE.Analyses.Mission.Segments.Descent.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate
@@ -128,7 +137,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__EAS__Constant__Rate_1_1Constant__EAS__Constant__Rate.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__EAS__Constant__Rate_1_1Constant__EAS__Constant__Rate.html index 88fc4853..e19be453 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__EAS__Constant__Rate_1_1Constant__EAS__Constant__Rate.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__EAS__Constant__Rate_1_1Constant__EAS__Constant__Rate.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Mission.Segments.Descent.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -110,50 +117,37 @@ SUAVE.Analyses.Mission.Segments.Simple.Simple SUAVE.Analyses.Mission.Segments.Segment.Segment SUAVE.Analyses.Analysis.Analysis - -
+ + - - - - - - - - - - - - - + + - - - - - - + + + + + + - - - - - - - - - - - - + + + + + + + + + +

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Descent.Unknown_Throttle.Unknown_Throttle
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def initialize (self)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def iterate (self)
 
def finalize (self)
 
def evaluate (self, state=None)
 
def merged (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
@@ -169,6 +163,9 @@ + + @@ -176,6 +173,9 @@ + + @@ -193,6 +193,9 @@ + + @@ -245,6 +248,8 @@

SUAVE.Analyses.Mission.Segments.Descent.Unknown_Throttle.Unknown_Throttle.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__EAS__Constant__Rate_1_1Constant__EAS__Constant__Rate.js b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__EAS__Constant__Rate_1_1Constant__EAS__Constant__Rate.js index d53a26c1..39eb1bc1 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__EAS__Constant__Rate_1_1Constant__EAS__Constant__Rate.js +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__EAS__Constant__Rate_1_1Constant__EAS__Constant__Rate.js @@ -4,5 +4,6 @@ var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__EAS__C [ "altitude_end", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__EAS__Constant__Rate_1_1Constant__EAS__Constant__Rate.html#ae75a8b7764cc805f814f91291bac2e3f", null ], [ "altitude_start", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__EAS__Constant__Rate_1_1Constant__EAS__Constant__Rate.html#a939e431f3199b662d851509bb58ae2e4", null ], [ "descent_rate", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__EAS__Constant__Rate_1_1Constant__EAS__Constant__Rate.html#aaa9430333d797a3a4e139072db72a148", null ], - [ "equivalent_air_speed", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__EAS__Constant__Rate_1_1Constant__EAS__Constant__Rate.html#a13dc0023d967eaa2c500d9d541b29cb5", null ] + [ "equivalent_air_speed", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__EAS__Constant__Rate_1_1Constant__EAS__Constant__Rate.html#a13dc0023d967eaa2c500d9d541b29cb5", null ], + [ "true_course", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__EAS__Constant__Rate_1_1Constant__EAS__Constant__Rate.html#adf37341276e9508b4fa4e52a5dbfc045", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Angle_1_113016f07454f53dbac238312756446d6.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Angle_1_113016f07454f53dbac238312756446d6.html index f3734b09..ea32bb2d 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Angle_1_113016f07454f53dbac238312756446d6.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Angle_1_113016f07454f53dbac238312756446d6.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Attributes

 equivalent_air_speed
 
true_course
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Descent.Unknown_Throttle.Unknown_Throttle
 altitude_start
 altitude_end
 
true_course
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
 temperature_deviation
 process
 
conditions
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
 tag
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -110,50 +117,37 @@ SUAVE.Analyses.Mission.Segments.Simple.Simple SUAVE.Analyses.Mission.Segments.Segment.Segment SUAVE.Analyses.Analysis.Analysis - -
+ + - - - - - - - - - - - - - + + - - - - - - + + + + + + - - - - - - - - - - - - + + + + + + + + + +

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def initialize (self)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def iterate (self)
 
def finalize (self)
 
def evaluate (self, state=None)
 
def merged (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
@@ -169,6 +163,9 @@ + + @@ -176,6 +173,9 @@ + + @@ -193,6 +193,9 @@ + + @@ -245,6 +248,8 @@

SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Angle_1_113016f07454f53dbac238312756446d6.js b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Angle_1_113016f07454f53dbac238312756446d6.js index 04eb783b..08c7e5be 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Angle_1_113016f07454f53dbac238312756446d6.js +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Angle_1_113016f07454f53dbac238312756446d6.js @@ -4,5 +4,6 @@ var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed_ [ "air_speed", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Angle_1_113016f07454f53dbac238312756446d6.html#ab65eb0ec80ac2813a4680da642ae6fa7", null ], [ "altitude_end", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Angle_1_113016f07454f53dbac238312756446d6.html#a3f3a26a19a34597691602e182e61ab00", null ], [ "altitude_start", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Angle_1_113016f07454f53dbac238312756446d6.html#afb7d66ea4d3e838ee14b6a6305249dcf", null ], - [ "descent_angle", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Angle_1_113016f07454f53dbac238312756446d6.html#a5e3e5ccf847de44bad50edc23fba581c", null ] + [ "descent_angle", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Angle_1_113016f07454f53dbac238312756446d6.html#a5e3e5ccf847de44bad50edc23fba581c", null ], + [ "true_course", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Angle_1_113016f07454f53dbac238312756446d6.html#a7dfb8ec0d6dbf4cfa931227ef54e8c91", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Angle_1_13c1191d3d0ed5ed2722fffd200c9b64b.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Angle_1_13c1191d3d0ed5ed2722fffd200c9b64b.html index 3455e206..6a6d465d 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Angle_1_13c1191d3d0ed5ed2722fffd200c9b64b.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Angle_1_13c1191d3d0ed5ed2722fffd200c9b64b.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Attributes

 air_speed
 
true_course
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle
 altitude_start
 altitude_end
 
true_course
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
 temperature_deviation
 process
 
conditions
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
 tag
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -98,29 +105,31 @@

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle, including all inherited members.

- + - - + + - + - - - - - - - - - - + + + + + + + + + + + +
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle
air_speed (defined in SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle)SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle
altitude_end (defined in SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle)SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle
altitude_start (defined in SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle)SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
conditions (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
descent_angle (defined in SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle)SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
SUAVE::Analyses::Analysis::Analysis.evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
finalize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
merged(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
true_course (defined in SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle)SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle
@@ -128,7 +137,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Angle__No6c766c7d7f943d7125da304d9336dbfa.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Angle__No6c766c7d7f943d7125da304d9336dbfa.html index ab6e9e2b..5169b474 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Angle__No6c766c7d7f943d7125da304d9336dbfa.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Angle__No6c766c7d7f943d7125da304d9336dbfa.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -98,29 +105,31 @@

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise, including all inherited members.

- + - - + + - + - - - - - - - - - - + + + + + + + + + + + +
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise
air_speed (defined in SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise)SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise
altitude_end (defined in SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise)SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise
altitude_start (defined in SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise)SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
conditions (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
descent_angle (defined in SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise)SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
SUAVE::Analyses::Analysis::Analysis.evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
finalize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
merged(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
true_course (defined in SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise)SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise
@@ -128,7 +137,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Angle__Noa39040ebc44f8c6e229921b8045d6b6f.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Angle__Noa39040ebc44f8c6e229921b8045d6b6f.html index 79505fa2..5e16859d 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Angle__Noa39040ebc44f8c6e229921b8045d6b6f.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Angle__Noa39040ebc44f8c6e229921b8045d6b6f.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -110,50 +117,37 @@ SUAVE.Analyses.Mission.Segments.Simple.Simple SUAVE.Analyses.Mission.Segments.Segment.Segment SUAVE.Analyses.Analysis.Analysis - -
+ + - - - - - - - - - - - - - + + - - - - - - + + + + + + - - - - - - - - - - - - + + + + + + + + + +

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def initialize (self)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def iterate (self)
 
def finalize (self)
 
def evaluate (self, state=None)
 
def merged (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
@@ -169,6 +163,9 @@ + + @@ -176,6 +173,9 @@ + + @@ -193,6 +193,9 @@ + + @@ -248,6 +251,8 @@

SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Angle__Noa39040ebc44f8c6e229921b8045d6b6f.js b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Angle__Noa39040ebc44f8c6e229921b8045d6b6f.js index b288e6a8..e4c4d7aa 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Angle__Noa39040ebc44f8c6e229921b8045d6b6f.js +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Angle__Noa39040ebc44f8c6e229921b8045d6b6f.js @@ -4,5 +4,6 @@ var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed_ [ "air_speed", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Angle__Noa39040ebc44f8c6e229921b8045d6b6f.html#af66140022cbea56991c3f88adaea59be", null ], [ "altitude_end", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Angle__Noa39040ebc44f8c6e229921b8045d6b6f.html#a011563a86d73b0e7312bed11ac2f879b", null ], [ "altitude_start", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Angle__Noa39040ebc44f8c6e229921b8045d6b6f.html#af57ecd953a16afef65696a89019164b0", null ], - [ "descent_angle", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Angle__Noa39040ebc44f8c6e229921b8045d6b6f.html#aaf205b9f40404808ae7d5e990b5b6fbb", null ] + [ "descent_angle", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Angle__Noa39040ebc44f8c6e229921b8045d6b6f.html#aaf205b9f40404808ae7d5e990b5b6fbb", null ], + [ "true_course", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Angle__Noa39040ebc44f8c6e229921b8045d6b6f.html#a86283fc0ed1f9189c80da64360a2fc63", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Rate_1_1Ca2f684fae436846bc06d2f2771b7a319.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Rate_1_1Ca2f684fae436846bc06d2f2771b7a319.html index 388bdf3a..4d0411f2 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Rate_1_1Ca2f684fae436846bc06d2f2771b7a319.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Rate_1_1Ca2f684fae436846bc06d2f2771b7a319.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Attributes

 air_speed
 
true_course
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle
 altitude_start
 altitude_end
 
true_course
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
 temperature_deviation
 process
 
conditions
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
 tag
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -98,29 +105,31 @@

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate, including all inherited members.

- + - - + + - + - - - - - - - - - - + + + + + + + + + + + +
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate
air_speed (defined in SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate)SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate
altitude_end (defined in SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate)SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate
altitude_start (defined in SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate)SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
conditions (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
descent_rate (defined in SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate)SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
SUAVE::Analyses::Analysis::Analysis.evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
finalize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
merged(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
true_course (defined in SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate)SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate
@@ -128,7 +137,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Rate_1_1Constant__Speed__Constant__Rate.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Rate_1_1Constant__Speed__Constant__Rate.html index 0b96a9b8..9e7b944e 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Rate_1_1Constant__Speed__Constant__Rate.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Rate_1_1Constant__Speed__Constant__Rate.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -110,50 +117,37 @@ SUAVE.Analyses.Mission.Segments.Simple.Simple SUAVE.Analyses.Mission.Segments.Segment.Segment SUAVE.Analyses.Analysis.Analysis - -
+ + - - - - - - - - - - - - - + + - - - - - - + + + + + + - - - - - - - - - - - - + + + + + + + + + +

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def initialize (self)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def iterate (self)
 
def finalize (self)
 
def evaluate (self, state=None)
 
def merged (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
@@ -169,6 +163,9 @@ + + @@ -176,6 +173,9 @@ + + @@ -193,6 +193,9 @@ + + @@ -237,6 +240,8 @@

SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Rate_1_1Constant__Speed__Constant__Rate.js b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Rate_1_1Constant__Speed__Constant__Rate.js index d8880637..7673684f 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Rate_1_1Constant__Speed__Constant__Rate.js +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Rate_1_1Constant__Speed__Constant__Rate.js @@ -4,5 +4,6 @@ var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed_ [ "air_speed", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Rate_1_1Constant__Speed__Constant__Rate.html#a343792d9b4f79b994002a2c30833b5c0", null ], [ "altitude_end", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Rate_1_1Constant__Speed__Constant__Rate.html#a1f6f7fd6634fc2c64a6fe418fdaa75d1", null ], [ "altitude_start", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Rate_1_1Constant__Speed__Constant__Rate.html#ae8d2f863a4a89e7a80bbfcdce7120813", null ], - [ "descent_rate", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Rate_1_1Constant__Speed__Constant__Rate.html#a17b5479e0213916e6bab9828d1f15c3a", null ] + [ "descent_rate", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Rate_1_1Constant__Speed__Constant__Rate.html#a17b5479e0213916e6bab9828d1f15c3a", null ], + [ "true_course", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Constant__Speed__Constant__Rate_1_1Constant__Speed__Constant__Rate.html#a204a6d204b0ff1af83cb183a72830d72", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Linear__Mach__Constant__Rate_1_1Linear__Mach__Constant__Rate.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Linear__Mach__Constant__Rate_1_1Linear__Mach__Constant__Rate.html index 988b8ba7..d1b0ca2b 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Linear__Mach__Constant__Rate_1_1Linear__Mach__Constant__Rate.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Linear__Mach__Constant__Rate_1_1Linear__Mach__Constant__Rate.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Mission.Segments.Descent.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Attributes

 air_speed
 
true_course
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle
 altitude_start
 altitude_end
 
true_course
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
 temperature_deviation
 process
 
conditions
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
 tag
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -110,50 +117,37 @@ SUAVE.Analyses.Mission.Segments.Simple.Simple SUAVE.Analyses.Mission.Segments.Segment.Segment SUAVE.Analyses.Analysis.Analysis - -
+ + - - - - - - - - - - - - - + + - - - - - - + + + + + + - - - - - - - - - - - - + + + + + + + + + +

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def initialize (self)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def iterate (self)
 
def finalize (self)
 
def evaluate (self, state=None)
 
def merged (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
@@ -172,6 +166,9 @@ + + @@ -179,6 +176,9 @@ + + @@ -196,6 +196,9 @@ + + @@ -249,6 +252,8 @@

SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Linear__Mach__Constant__Rate_1_1Linear__Mach__Constant__Rate.js b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Linear__Mach__Constant__Rate_1_1Linear__Mach__Constant__Rate.js index b827dc59..872f152a 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Linear__Mach__Constant__Rate_1_1Linear__Mach__Constant__Rate.js +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Linear__Mach__Constant__Rate_1_1Linear__Mach__Constant__Rate.js @@ -5,5 +5,6 @@ var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Linear__Mach__Co [ "altitude_start", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Linear__Mach__Constant__Rate_1_1Linear__Mach__Constant__Rate.html#a55f9dbc099bdc473c3ad9a9fd42d053d", null ], [ "descent_rate", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Linear__Mach__Constant__Rate_1_1Linear__Mach__Constant__Rate.html#af6e11ece5e9b8b1a222581a528bb506c", null ], [ "mach_end", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Linear__Mach__Constant__Rate_1_1Linear__Mach__Constant__Rate.html#aafbc811cbfe78bcd603a7f6cc2af6e48", null ], - [ "mach_start", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Linear__Mach__Constant__Rate_1_1Linear__Mach__Constant__Rate.html#aa056e902972480320d0ced21d1789840", null ] + [ "mach_start", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Linear__Mach__Constant__Rate_1_1Linear__Mach__Constant__Rate.html#aa056e902972480320d0ced21d1789840", null ], + [ "true_course", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Linear__Mach__Constant__Rate_1_1Linear__Mach__Constant__Rate.html#a0ce445461ef1a4ef8ff357249f201091", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Linear__Mach__Constant__Rate_1_1Linec3b1df3c7852606c53bfd248df7e005e.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Linear__Mach__Constant__Rate_1_1Linec3b1df3c7852606c53bfd248df7e005e.html index a9121091..c5621a2c 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Linear__Mach__Constant__Rate_1_1Linec3b1df3c7852606c53bfd248df7e005e.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Linear__Mach__Constant__Rate_1_1Linec3b1df3c7852606c53bfd248df7e005e.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Attributes

 mach_start
 
true_course
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle
 altitude_start
 altitude_end
 
true_course
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
 temperature_deviation
 process
 
conditions
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
 tag
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -98,30 +105,32 @@

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Descent.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate, including all inherited members.

- + - - + + - + - - - - - + + + + + - - - - - + + + + + + +
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Descent.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate
altitude_end (defined in SUAVE.Analyses.Mission.Segments.Descent.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate)SUAVE.Analyses.Mission.Segments.Descent.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate
altitude_start (defined in SUAVE.Analyses.Mission.Segments.Descent.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate)SUAVE.Analyses.Mission.Segments.Descent.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
conditions (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
descent_rate (defined in SUAVE.Analyses.Mission.Segments.Descent.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate)SUAVE.Analyses.Mission.Segments.Descent.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
SUAVE::Analyses::Analysis::Analysis.evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
finalize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
mach_end (defined in SUAVE.Analyses.Mission.Segments.Descent.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate)SUAVE.Analyses.Mission.Segments.Descent.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate
mach_start (defined in SUAVE.Analyses.Mission.Segments.Descent.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate)SUAVE.Analyses.Mission.Segments.Descent.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
merged(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
true_course (defined in SUAVE.Analyses.Mission.Segments.Descent.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate)SUAVE.Analyses.Mission.Segments.Descent.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate
@@ -129,7 +138,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Unknown__Throttle_1_1Unknown__Throttle-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Unknown__Throttle_1_1Unknown__Throttle-members.html index bd31be8b..d87d111c 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Unknown__Throttle_1_1Unknown__Throttle-members.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Unknown__Throttle_1_1Unknown__Throttle-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -98,27 +105,29 @@

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Descent.Unknown_Throttle.Unknown_Throttle, including all inherited members.

- + - - + + - + - - - - - - - - - - + + + + + + + + + + + +
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Descent.Unknown_Throttle.Unknown_Throttle
altitude_end (defined in SUAVE.Analyses.Mission.Segments.Descent.Unknown_Throttle.Unknown_Throttle)SUAVE.Analyses.Mission.Segments.Descent.Unknown_Throttle.Unknown_Throttle
altitude_start (defined in SUAVE.Analyses.Mission.Segments.Descent.Unknown_Throttle.Unknown_Throttle)SUAVE.Analyses.Mission.Segments.Descent.Unknown_Throttle.Unknown_Throttle
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
conditions (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
SUAVE::Analyses::Analysis::Analysis.evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
finalize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
merged(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
true_course (defined in SUAVE.Analyses.Mission.Segments.Descent.Unknown_Throttle.Unknown_Throttle)SUAVE.Analyses.Mission.Segments.Descent.Unknown_Throttle.Unknown_Throttle
@@ -126,7 +135,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Unknown__Throttle_1_1Unknown__Throttle.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Unknown__Throttle_1_1Unknown__Throttle.html index a7fd18b8..cb83216b 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Unknown__Throttle_1_1Unknown__Throttle.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Unknown__Throttle_1_1Unknown__Throttle.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Mission.Segments.Descent.Unknown_Throttle.Unknown_Throttle Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -110,47 +117,37 @@ SUAVE.Analyses.Mission.Segments.Segment.Segment SUAVE.Analyses.Analysis.Analysis SUAVE.Analyses.Mission.Segments.Descent.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate - -
+ + - - - - - - - - - - + + - - - - - - + + + + + + - - - - - - - - - - - - + + + + + + + + + +

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def initialize (self)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def iterate (self)
 
def finalize (self)
 
def evaluate (self, state=None)
 
def merged (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
@@ -160,6 +157,9 @@ + + @@ -177,6 +177,9 @@ + + @@ -230,6 +233,10 @@

SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic.

+ +

Reimplemented in SUAVE.Analyses.Mission.Segments.Descent.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Unknown__Throttle_1_1Unknown__Throttle.js b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Unknown__Throttle_1_1Unknown__Throttle.js index 93209e5b..cb2954c1 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Unknown__Throttle_1_1Unknown__Throttle.js +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Unknown__Throttle_1_1Unknown__Throttle.js @@ -2,5 +2,6 @@ var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Unknown__Throttl [ [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Unknown__Throttle_1_1Unknown__Throttle.html#ad3184a3e2dd7b80e19e34e9977878749", null ], [ "altitude_end", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Unknown__Throttle_1_1Unknown__Throttle.html#a4fd0667c8d4690b702cf8936c158208d", null ], - [ "altitude_start", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Unknown__Throttle_1_1Unknown__Throttle.html#af2248d48041ebf36c2c16beacdf215a4", null ] + [ "altitude_start", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Unknown__Throttle_1_1Unknown__Throttle.html#af2248d48041ebf36c2c16beacdf215a4", null ], + [ "true_course", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Descent_1_1Unknown__Throttle_1_1Unknown__Throttle.html#a429c3ae5f3a199b2ac749ad93179899e", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Battery__Charge__Discharge_1_1Battery__Charge__Discharge-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Battery__Charge__Discharge_1_1Battery__Charge__Discharge-members.html new file mode 100644 index 00000000..590996fe --- /dev/null +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Battery__Charge__Discharge_1_1Battery__Charge__Discharge-members.html @@ -0,0 +1,144 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+

Public Attributes

 altitude_end
 
true_course
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
 temperature_deviation
 process
 
conditions
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
 tag
+ + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+ + + + + +
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
SUAVE.Analyses.Mission.Segments.Ground.Battery_Charge_Discharge.Battery_Charge_Discharge Member List
+
+
+ +

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Ground.Battery_Charge_Discharge.Battery_Charge_Discharge, including all inherited members.

+ + + + + + + + + + + + + + + + + + + + + + + + + + +
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Ground.Battery_Charge_Discharge.Battery_Charge_Discharge
altitude (defined in SUAVE.Analyses.Mission.Segments.Ground.Battery_Charge_Discharge.Battery_Charge_Discharge)SUAVE.Analyses.Mission.Segments.Ground.Battery_Charge_Discharge.Battery_Charge_Discharge
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
battery_discharge (defined in SUAVE.Analyses.Mission.Segments.Ground.Battery_Charge_Discharge.Battery_Charge_Discharge)SUAVE.Analyses.Mission.Segments.Ground.Battery_Charge_Discharge.Battery_Charge_Discharge
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
conditions (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
merged(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
overcharge_contingency (defined in SUAVE.Analyses.Mission.Segments.Ground.Battery_Charge_Discharge.Battery_Charge_Discharge)SUAVE.Analyses.Mission.Segments.Ground.Battery_Charge_Discharge.Battery_Charge_Discharge
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
time (defined in SUAVE.Analyses.Mission.Segments.Ground.Battery_Charge_Discharge.Battery_Charge_Discharge)SUAVE.Analyses.Mission.Segments.Ground.Battery_Charge_Discharge.Battery_Charge_Discharge
true_course (defined in SUAVE.Analyses.Mission.Segments.Ground.Battery_Charge_Discharge.Battery_Charge_Discharge)SUAVE.Analyses.Mission.Segments.Ground.Battery_Charge_Discharge.Battery_Charge_Discharge
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Battery__Charge__Discharge_1_1Battery__Charge__Discharge.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Battery__Charge__Discharge_1_1Battery__Charge__Discharge.html new file mode 100644 index 00000000..f40bbb2e --- /dev/null +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Battery__Charge__Discharge_1_1Battery__Charge__Discharge.html @@ -0,0 +1,251 @@ + + + + + + + +SUAVE: SUAVE.Analyses.Mission.Segments.Ground.Battery_Charge_Discharge.Battery_Charge_Discharge Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Analyses.Mission.Segments.Ground.Battery_Charge_Discharge.Battery_Charge_Discharge Class Reference
+
+
+
+Inheritance diagram for SUAVE.Analyses.Mission.Segments.Ground.Battery_Charge_Discharge.Battery_Charge_Discharge:
+
+
+ + +SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic +SUAVE.Analyses.Mission.Segments.Simple.Simple +SUAVE.Analyses.Mission.Segments.Segment.Segment +SUAVE.Analyses.Analysis.Analysis + +
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def initialize (self)
 
def converge (self, state)
 
def iterate (self)
 
def finalize (self)
 
def evaluate (self, state=None)
 
def merged (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Attributes

altitude
 
time
 
overcharge_contingency
 
battery_discharge
 
true_course
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
temperature_deviation
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
settings
 
state
 
analyses
 
process
 
conditions
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
+

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Analyses.Mission.Segments.Ground.Battery_Charge_Discharge.Battery_Charge_Discharge.__defaults__ ( self)
+
+
This sets the default solver flow. Anything in here can be modified after initializing a segment.
+    
+    Assumptions:
+    None
+    
+    Source:
+    N/A
+    
+    Inputs:
+    None
+    
+    Outputs:
+    None
+    
+    Properties Used:
+    None
+
+

Reimplemented from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic.

+ +
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Analyses/Mission/Segments/Ground/Battery_Charge_Discharge.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Battery__Charge__Discharge_1_1Battery__Charge__Discharge.js b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Battery__Charge__Discharge_1_1Battery__Charge__Discharge.js new file mode 100644 index 00000000..09e10ab3 --- /dev/null +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Battery__Charge__Discharge_1_1Battery__Charge__Discharge.js @@ -0,0 +1,9 @@ +var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Battery__Charge__Discharge_1_1Battery__Charge__Discharge = +[ + [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Battery__Charge__Discharge_1_1Battery__Charge__Discharge.html#acb69c5943a5c7149acf6733465103a94", null ], + [ "altitude", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Battery__Charge__Discharge_1_1Battery__Charge__Discharge.html#af7281c1cc59fc9cdbc965dd12888e186", null ], + [ "battery_discharge", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Battery__Charge__Discharge_1_1Battery__Charge__Discharge.html#a5c7ba82499268df17b19597412cad40f", null ], + [ "overcharge_contingency", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Battery__Charge__Discharge_1_1Battery__Charge__Discharge.html#a0ae982acb7774bba4e341c152218e247", null ], + [ "time", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Battery__Charge__Discharge_1_1Battery__Charge__Discharge.html#ad3942c04bdc8cd98db8761d59b733d67", null ], + [ "true_course", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Battery__Charge__Discharge_1_1Battery__Charge__Discharge.html#a8475c93de8863044e3ed4c7d4488fe86", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Battery__Charge__Discharge_1_1Battery__Charge__Discharge.png b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Battery__Charge__Discharge_1_1Battery__Charge__Discharge.png new file mode 100644 index 00000000..72bb5d7b Binary files /dev/null and b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Battery__Charge__Discharge_1_1Battery__Charge__Discharge.png differ diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Ground_1_1Ground-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Ground_1_1Ground-members.html index f55482c8..bea6ab77 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Ground_1_1Ground-members.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Ground_1_1Ground-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -98,30 +105,33 @@

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground, including all inherited members.

- + - - - - - - - - - - - - - - + + + + + + + + + + + + + + + + - - + + +
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
friction_coefficient (defined in SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground)SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground
ground_incline (defined in SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground)SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
altitude (defined in SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground)SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
conditions (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
friction_coefficient (defined in SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground)SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground
ground_incline (defined in SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground)SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground
initialize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
merged(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
throttle (defined in SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground)SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground
velocity_end (defined in SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground)SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground
velocity_start (defined in SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground)SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground
true_course (defined in SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground)SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground
velocity_end (defined in SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground)SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground
velocity_start (defined in SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground)SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground
@@ -129,7 +139,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Ground_1_1Ground.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Ground_1_1Ground.html index d16ea43b..556584c4 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Ground_1_1Ground.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Ground_1_1Ground.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -111,47 +118,37 @@ SUAVE.Analyses.Analysis.Analysis SUAVE.Analyses.Mission.Segments.Ground.Landing.Landing SUAVE.Analyses.Mission.Segments.Ground.Takeoff.Takeoff - -
+ + - - - - - - - - - - + + - - - - - - + + + + + + - - - - - - - - - - - - + + + + + + + + + +

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def initialize (self)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def iterate (self)
 
def finalize (self)
 
def evaluate (self, state=None)
 
def merged (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
@@ -170,6 +167,12 @@ + + + + @@ -187,6 +190,9 @@ + + @@ -248,6 +254,10 @@

SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic.

+ +

Reimplemented in SUAVE.Analyses.Mission.Segments.Ground.Landing.Landing, and SUAVE.Analyses.Mission.Segments.Ground.Takeoff.Takeoff.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Ground_1_1Ground.js b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Ground_1_1Ground.js index f51a2481..d4080fc0 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Ground_1_1Ground.js +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Ground_1_1Ground.js @@ -1,9 +1,11 @@ var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Ground_1_1Ground = [ [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Ground_1_1Ground.html#a6f38f44f721bb677895014bf41e7f943", null ], + [ "altitude", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Ground_1_1Ground.html#a40beb15590cf75f03ee36a58a410a0a9", null ], [ "friction_coefficient", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Ground_1_1Ground.html#ab464f078ee2c739e3752a9f8eb2d0138", null ], [ "ground_incline", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Ground_1_1Ground.html#a6c8d24e8dff25fd1e76317107c787261", null ], [ "throttle", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Ground_1_1Ground.html#ad700f1e66d0496426a5cf6a9f08fdfe8", null ], + [ "true_course", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Ground_1_1Ground.html#a160cbfa168fcc981d1d2fc0ba8b34b36", null ], [ "velocity_end", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Ground_1_1Ground.html#a0cdc0346e4d35f90948231559f21304a", null ], [ "velocity_start", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Ground_1_1Ground.html#af92084c59eb4341c8aef909f32b33aa8", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Landing_1_1Landing-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Landing_1_1Landing-members.html index 23ff7276..2a9b7d66 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Landing_1_1Landing-members.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Landing_1_1Landing-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Attributes

 velocity_end
 
altitude
 
true_course
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
 temperature_deviation
 process
 
conditions
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
 tag
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -98,30 +105,33 @@

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Ground.Landing.Landing, including all inherited members.

- + - - - - - - - - - - - - - - + + + + + + + + + + + + + + + + - - + + +
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Ground.Landing.Landing
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
friction_coefficient (defined in SUAVE.Analyses.Mission.Segments.Ground.Landing.Landing)SUAVE.Analyses.Mission.Segments.Ground.Landing.Landing
ground_incline (defined in SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground)SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
altitude (defined in SUAVE.Analyses.Mission.Segments.Ground.Landing.Landing)SUAVE.Analyses.Mission.Segments.Ground.Landing.Landing
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
conditions (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
friction_coefficient (defined in SUAVE.Analyses.Mission.Segments.Ground.Landing.Landing)SUAVE.Analyses.Mission.Segments.Ground.Landing.Landing
ground_incline (defined in SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground)SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground
initialize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
merged(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
throttle (defined in SUAVE.Analyses.Mission.Segments.Ground.Landing.Landing)SUAVE.Analyses.Mission.Segments.Ground.Landing.Landing
velocity_end (defined in SUAVE.Analyses.Mission.Segments.Ground.Landing.Landing)SUAVE.Analyses.Mission.Segments.Ground.Landing.Landing
velocity_start (defined in SUAVE.Analyses.Mission.Segments.Ground.Landing.Landing)SUAVE.Analyses.Mission.Segments.Ground.Landing.Landing
true_course (defined in SUAVE.Analyses.Mission.Segments.Ground.Landing.Landing)SUAVE.Analyses.Mission.Segments.Ground.Landing.Landing
velocity_end (defined in SUAVE.Analyses.Mission.Segments.Ground.Landing.Landing)SUAVE.Analyses.Mission.Segments.Ground.Landing.Landing
velocity_start (defined in SUAVE.Analyses.Mission.Segments.Ground.Landing.Landing)SUAVE.Analyses.Mission.Segments.Ground.Landing.Landing
@@ -129,7 +139,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Landing_1_1Landing.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Landing_1_1Landing.html index 36e70085..39f12b55 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Landing_1_1Landing.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Landing_1_1Landing.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Mission.Segments.Ground.Landing.Landing Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -110,50 +117,37 @@ SUAVE.Analyses.Mission.Segments.Simple.Simple SUAVE.Analyses.Mission.Segments.Segment.Segment SUAVE.Analyses.Analysis.Analysis - -
+ + - - - - - - - - - - - - - + + - - - - - - + + + + + + - - - - - - - - - - - - + + + + + + + + + +

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def initialize (self)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def iterate (self)
 
def finalize (self)
 
def evaluate (self, state=None)
 
def merged (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
@@ -169,6 +163,12 @@ + + + + @@ -185,6 +185,12 @@ + + + + @@ -202,6 +208,9 @@ + + @@ -263,6 +272,8 @@

SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Landing_1_1Landing.js b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Landing_1_1Landing.js index aa294e63..a7d1e797 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Landing_1_1Landing.js +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Landing_1_1Landing.js @@ -1,8 +1,10 @@ var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Landing_1_1Landing = [ [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Landing_1_1Landing.html#a72dcf1c5eb695dfb5496ab15b1fadf89", null ], + [ "altitude", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Landing_1_1Landing.html#ac572d004077acdac4195f2e36aa6f5d6", null ], [ "friction_coefficient", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Landing_1_1Landing.html#aeb35b4252ace3965b9cf636f4dde25b1", null ], [ "throttle", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Landing_1_1Landing.html#a588dfb3c26a66472501cabd36a8aaaec", null ], + [ "true_course", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Landing_1_1Landing.html#a6ca34063b925b13f1e8cf2b619388b45", null ], [ "velocity_end", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Landing_1_1Landing.html#a7ffa35d28ce048a76380dfb48a9fb3b5", null ], [ "velocity_start", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Landing_1_1Landing.html#a31af2911950e8226415dcfd098cc9649", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Takeoff_1_1Takeoff-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Takeoff_1_1Takeoff-members.html index 86f06cec..f866c25c 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Takeoff_1_1Takeoff-members.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Takeoff_1_1Takeoff-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Attributes

 throttle
 
altitude
 
true_course
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground
 ground_incline
 velocity_end
 
altitude
 
true_course
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
 temperature_deviation
 process
 
conditions
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
 tag
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -98,30 +105,33 @@

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Ground.Takeoff.Takeoff, including all inherited members.

- + - - - - - - - - - - - - - - + + + + + + + + + + + + + + + + - - + + +
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Ground.Takeoff.Takeoff
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
friction_coefficient (defined in SUAVE.Analyses.Mission.Segments.Ground.Takeoff.Takeoff)SUAVE.Analyses.Mission.Segments.Ground.Takeoff.Takeoff
ground_incline (defined in SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground)SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
altitude (defined in SUAVE.Analyses.Mission.Segments.Ground.Takeoff.Takeoff)SUAVE.Analyses.Mission.Segments.Ground.Takeoff.Takeoff
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
conditions (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
friction_coefficient (defined in SUAVE.Analyses.Mission.Segments.Ground.Takeoff.Takeoff)SUAVE.Analyses.Mission.Segments.Ground.Takeoff.Takeoff
ground_incline (defined in SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground)SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground
initialize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
merged(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
throttle (defined in SUAVE.Analyses.Mission.Segments.Ground.Takeoff.Takeoff)SUAVE.Analyses.Mission.Segments.Ground.Takeoff.Takeoff
velocity_end (defined in SUAVE.Analyses.Mission.Segments.Ground.Takeoff.Takeoff)SUAVE.Analyses.Mission.Segments.Ground.Takeoff.Takeoff
velocity_start (defined in SUAVE.Analyses.Mission.Segments.Ground.Takeoff.Takeoff)SUAVE.Analyses.Mission.Segments.Ground.Takeoff.Takeoff
true_course (defined in SUAVE.Analyses.Mission.Segments.Ground.Takeoff.Takeoff)SUAVE.Analyses.Mission.Segments.Ground.Takeoff.Takeoff
velocity_end (defined in SUAVE.Analyses.Mission.Segments.Ground.Takeoff.Takeoff)SUAVE.Analyses.Mission.Segments.Ground.Takeoff.Takeoff
velocity_start (defined in SUAVE.Analyses.Mission.Segments.Ground.Takeoff.Takeoff)SUAVE.Analyses.Mission.Segments.Ground.Takeoff.Takeoff
@@ -129,7 +139,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Takeoff_1_1Takeoff.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Takeoff_1_1Takeoff.html index 5c0a209c..71220f14 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Takeoff_1_1Takeoff.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Takeoff_1_1Takeoff.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Mission.Segments.Ground.Takeoff.Takeoff Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -110,50 +117,37 @@ SUAVE.Analyses.Mission.Segments.Simple.Simple SUAVE.Analyses.Mission.Segments.Segment.Segment SUAVE.Analyses.Analysis.Analysis - -
+ + - - - - - - - - - - - - - + + - - - - - - + + + + + + - - - - - - - - - - - - + + + + + + + + + +

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def initialize (self)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def iterate (self)
 
def finalize (self)
 
def evaluate (self, state=None)
 
def merged (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
@@ -169,6 +163,12 @@ + + + + @@ -185,6 +185,12 @@ + + + + @@ -202,6 +208,9 @@ + + @@ -263,6 +272,8 @@

SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Takeoff_1_1Takeoff.js b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Takeoff_1_1Takeoff.js index e5f8cb00..685a77e9 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Takeoff_1_1Takeoff.js +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Takeoff_1_1Takeoff.js @@ -1,8 +1,10 @@ var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Takeoff_1_1Takeoff = [ [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Takeoff_1_1Takeoff.html#ae81502ad7f17cf737e304adbd9195140", null ], + [ "altitude", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Takeoff_1_1Takeoff.html#af785ae9eac10cae904f2af1bf4ac9788", null ], [ "friction_coefficient", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Takeoff_1_1Takeoff.html#a9b960ebffa99dc7aa77c0a4e3cde453c", null ], [ "throttle", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Takeoff_1_1Takeoff.html#a9c715fcf97335e66e47382d416f2cab0", null ], + [ "true_course", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Takeoff_1_1Takeoff.html#ab2388f80093a647c7725d539e98582eb", null ], [ "velocity_end", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Takeoff_1_1Takeoff.html#abb5a7876221072baa4f2ed7bcbdeaa69", null ], [ "velocity_start", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Ground_1_1Takeoff_1_1Takeoff.html#abe0789c18abb310302ff523386487cc5", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Climb_1_1Climb-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Climb_1_1Climb-members.html index 7e8d1470..6ab8f1a3 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Climb_1_1Climb-members.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Climb_1_1Climb-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Attributes

 throttle
 
altitude
 
true_course
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground
 ground_incline
 velocity_end
 
altitude
 
true_course
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
 temperature_deviation
 process
 
conditions
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
 tag
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -98,30 +105,32 @@

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Hover.Climb.Climb, including all inherited members.

- + - - + + - + - - - - - - - - - - - + + + + + + + + + + + + +
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Hover.Climb.Climb
altitude (defined in SUAVE.Analyses.Mission.Segments.Hover.Hover.Hover)SUAVE.Analyses.Mission.Segments.Hover.Hover.Hover
altitude_end (defined in SUAVE.Analyses.Mission.Segments.Hover.Climb.Climb)SUAVE.Analyses.Mission.Segments.Hover.Climb.Climb
altitude_start (defined in SUAVE.Analyses.Mission.Segments.Hover.Climb.Climb)SUAVE.Analyses.Mission.Segments.Hover.Climb.Climb
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
climb_rate (defined in SUAVE.Analyses.Mission.Segments.Hover.Climb.Climb)SUAVE.Analyses.Mission.Segments.Hover.Climb.Climb
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
conditions (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
SUAVE::Analyses::Analysis::Analysis.evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
time (defined in SUAVE.Analyses.Mission.Segments.Hover.Hover.Hover)SUAVE.Analyses.Mission.Segments.Hover.Hover.Hover
finalize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
merged(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
time (defined in SUAVE.Analyses.Mission.Segments.Hover.Hover.Hover)SUAVE.Analyses.Mission.Segments.Hover.Hover.Hover
true_course (defined in SUAVE.Analyses.Mission.Segments.Hover.Climb.Climb)SUAVE.Analyses.Mission.Segments.Hover.Climb.Climb
@@ -129,7 +138,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Climb_1_1Climb.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Climb_1_1Climb.html index e0692f01..13b749dc 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Climb_1_1Climb.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Climb_1_1Climb.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Mission.Segments.Hover.Climb.Climb Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -110,50 +117,37 @@ SUAVE.Analyses.Mission.Segments.Simple.Simple SUAVE.Analyses.Mission.Segments.Segment.Segment SUAVE.Analyses.Analysis.Analysis - -
+ + - - - - - - - - - - - - - + + - - - - - - + + + + + + - - - - - - - - - - - - + + + + + + + + + +

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Hover.Hover.Hover
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def initialize (self)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def iterate (self)
 
def finalize (self)
 
def evaluate (self, state=None)
 
def merged (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
@@ -166,6 +160,9 @@ + + @@ -173,6 +170,9 @@ + + @@ -190,6 +190,9 @@ + + @@ -242,6 +245,8 @@

SUAVE.Analyses.Mission.Segments.Hover.Hover.Hover.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Climb_1_1Climb.js b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Climb_1_1Climb.js index 0f896950..95f80a2f 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Climb_1_1Climb.js +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Climb_1_1Climb.js @@ -3,5 +3,6 @@ var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Climb_1_1Climb = [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Climb_1_1Climb.html#a233064e0afad5ed01ac48ae3b48bbadd", null ], [ "altitude_end", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Climb_1_1Climb.html#a955d04a352b94d270e55212d079de955", null ], [ "altitude_start", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Climb_1_1Climb.html#a927c7c629a6350300bd748d1f5715a63", null ], - [ "climb_rate", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Climb_1_1Climb.html#a6153d33484e9e525785f64cab8bfaece", null ] + [ "climb_rate", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Climb_1_1Climb.html#a6153d33484e9e525785f64cab8bfaece", null ], + [ "true_course", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Climb_1_1Climb.html#abb26815e10cc83500b445902ba9b1f8e", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Descent_1_1Descent-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Descent_1_1Descent-members.html index 6458e000..0546327f 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Descent_1_1Descent-members.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Descent_1_1Descent-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Attributes

 climb_rate
 
true_course
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Hover.Hover.Hover
 altitude
 time
 
true_course
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
 temperature_deviation
 process
 
conditions
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
 tag
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -98,30 +105,32 @@

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Hover.Descent.Descent, including all inherited members.

- + - - + + - + - - - - - - - - - - - + + + + + + + + + + + + +
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Hover.Descent.Descent
altitude (defined in SUAVE.Analyses.Mission.Segments.Hover.Hover.Hover)SUAVE.Analyses.Mission.Segments.Hover.Hover.Hover
altitude_end (defined in SUAVE.Analyses.Mission.Segments.Hover.Descent.Descent)SUAVE.Analyses.Mission.Segments.Hover.Descent.Descent
altitude_start (defined in SUAVE.Analyses.Mission.Segments.Hover.Descent.Descent)SUAVE.Analyses.Mission.Segments.Hover.Descent.Descent
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
conditions (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
descent_rate (defined in SUAVE.Analyses.Mission.Segments.Hover.Descent.Descent)SUAVE.Analyses.Mission.Segments.Hover.Descent.Descent
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
SUAVE::Analyses::Analysis::Analysis.evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
time (defined in SUAVE.Analyses.Mission.Segments.Hover.Hover.Hover)SUAVE.Analyses.Mission.Segments.Hover.Hover.Hover
finalize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
merged(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
time (defined in SUAVE.Analyses.Mission.Segments.Hover.Hover.Hover)SUAVE.Analyses.Mission.Segments.Hover.Hover.Hover
true_course (defined in SUAVE.Analyses.Mission.Segments.Hover.Descent.Descent)SUAVE.Analyses.Mission.Segments.Hover.Descent.Descent
@@ -129,7 +138,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Descent_1_1Descent.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Descent_1_1Descent.html index 8b8c205c..92000382 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Descent_1_1Descent.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Descent_1_1Descent.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Mission.Segments.Hover.Descent.Descent Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -110,50 +117,37 @@ SUAVE.Analyses.Mission.Segments.Simple.Simple SUAVE.Analyses.Mission.Segments.Segment.Segment SUAVE.Analyses.Analysis.Analysis - -
+ + - - - - - - - - - - - - - + + - - - - - - + + + + + + - - - - - - - - - - - - + + + + + + + + + +

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Hover.Hover.Hover
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def initialize (self)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def iterate (self)
 
def finalize (self)
 
def evaluate (self, state=None)
 
def merged (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
@@ -166,6 +160,9 @@ + + @@ -173,6 +170,9 @@ + + @@ -190,6 +190,9 @@ + + @@ -242,6 +245,8 @@

SUAVE.Analyses.Mission.Segments.Hover.Hover.Hover.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Descent_1_1Descent.js b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Descent_1_1Descent.js index e5c18e65..58b21b1c 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Descent_1_1Descent.js +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Descent_1_1Descent.js @@ -3,5 +3,6 @@ var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Descent_1_1Descent [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Descent_1_1Descent.html#aa0c504cca16b88e4441f11853b8d9a26", null ], [ "altitude_end", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Descent_1_1Descent.html#a1ff421c11066e8f449d486678644b34d", null ], [ "altitude_start", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Descent_1_1Descent.html#a182d95a39be2ec5e4079cfeb99d3804e", null ], - [ "descent_rate", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Descent_1_1Descent.html#a891ceac6c0178b9090ea3ef750af9a98", null ] + [ "descent_rate", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Descent_1_1Descent.html#a891ceac6c0178b9090ea3ef750af9a98", null ], + [ "true_course", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Descent_1_1Descent.html#abc9a9f81eee392979c45a8bc8767aa92", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Hover_1_1Hover-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Hover_1_1Hover-members.html index 559d7ffd..feb47613 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Hover_1_1Hover-members.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Hover_1_1Hover-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Attributes

 descent_rate
 
true_course
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Hover.Hover.Hover
 altitude
 time
 
true_course
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
 temperature_deviation
 process
 
conditions
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
 tag
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -98,27 +105,29 @@

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Hover.Hover.Hover, including all inherited members.

- + - - + + - + - - - - - - - - - - - + + + + + + + + + + + + +
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Hover.Hover.Hover
altitude (defined in SUAVE.Analyses.Mission.Segments.Hover.Hover.Hover)SUAVE.Analyses.Mission.Segments.Hover.Hover.Hover
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
conditions (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
SUAVE::Analyses::Analysis::Analysis.evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
time (defined in SUAVE.Analyses.Mission.Segments.Hover.Hover.Hover)SUAVE.Analyses.Mission.Segments.Hover.Hover.Hover
finalize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
merged(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
time (defined in SUAVE.Analyses.Mission.Segments.Hover.Hover.Hover)SUAVE.Analyses.Mission.Segments.Hover.Hover.Hover
true_course (defined in SUAVE.Analyses.Mission.Segments.Hover.Hover.Hover)SUAVE.Analyses.Mission.Segments.Hover.Hover.Hover
@@ -126,7 +135,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Hover_1_1Hover.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Hover_1_1Hover.html index 469ee000..144b7963 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Hover_1_1Hover.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Hover_1_1Hover.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Mission.Segments.Hover.Hover.Hover Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -111,47 +118,37 @@ SUAVE.Analyses.Analysis.Analysis SUAVE.Analyses.Mission.Segments.Hover.Climb.Climb SUAVE.Analyses.Mission.Segments.Hover.Descent.Descent - -
+ + - - - - - - - - - - + + - - - - - - + + + + + + - - - - - - - - - - - - + + + + + + + + + +

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def initialize (self)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def iterate (self)
 
def finalize (self)
 
def evaluate (self, state=None)
 
def merged (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
@@ -161,6 +158,9 @@ + + @@ -178,6 +178,9 @@ + + @@ -230,6 +233,10 @@

SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic.

+ +

Reimplemented in SUAVE.Analyses.Mission.Segments.Hover.Climb.Climb, and SUAVE.Analyses.Mission.Segments.Hover.Descent.Descent.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Hover_1_1Hover.js b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Hover_1_1Hover.js index e1467e9e..b01dd17f 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Hover_1_1Hover.js +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Hover_1_1Hover.js @@ -2,5 +2,6 @@ var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Hover_1_1Hover = [ [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Hover_1_1Hover.html#aef1b2403e95d5c378a8e1b2042d6c0b7", null ], [ "altitude", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Hover_1_1Hover.html#a45e8c7bd4c4dba0cb97d345652d8dbed", null ], - [ "time", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Hover_1_1Hover.html#a322ba5bbad48036bef5f2fbc65544f8c", null ] + [ "time", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Hover_1_1Hover.html#a322ba5bbad48036bef5f2fbc65544f8c", null ], + [ "true_course", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Hover_1_1Hover_1_1Hover.html#a6bce99c93be4300ec08df198b16b70b5", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Container-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Container-members.html index 8d1885c4..251e3e83 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Container-members.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Container-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Attributes

 time
 
true_course
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
 temperature_deviation
 process
 
conditions
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
 tag
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -98,26 +105,27 @@

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Segment.Container, including all inherited members.

- + - - + + - + - - - - - - - - - - + + + + + + + + + + +
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Segment.Container
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
append_segment(self, segment)SUAVE.Analyses.Mission.Segments.Segment.Container
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
conditions (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
SUAVE::Analyses::Analysis::Analysis.evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
segments (defined in SUAVE.Analyses.Mission.Segments.Segment.Container)SUAVE.Analyses.Mission.Segments.Segment.Container
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Container)SUAVE.Analyses.Mission.Segments.Segment.Container
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
merged(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
segments (defined in SUAVE.Analyses.Mission.Segments.Segment.Container)SUAVE.Analyses.Mission.Segments.Segment.Container
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Container)SUAVE.Analyses.Mission.Segments.Segment.Container
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
@@ -125,7 +133,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Container.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Container.html index daeadfc3..fded7ff3 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Container.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Container.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Mission.Segments.Segment.Container Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -107,8 +114,8 @@ SUAVE.Analyses.Mission.Segments.Segment.Segment SUAVE.Analyses.Analysis.Analysis - -
+ + @@ -117,33 +124,29 @@ - - - - + + - - - - - - + + + + + + - - - - - - - - - - - - + + + + + + + + + +

Public Member Functions

def append_segment (self, segment)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def initialize (self)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def iterate (self)
 
def finalize (self)
 
def evaluate (self, state=None)
 
def merged (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
@@ -166,6 +169,9 @@ + + @@ -218,6 +224,8 @@

SUAVE.Analyses.Mission.Segments.Segment.Segment.

+ @@ -275,7 +283,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Segment-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Segment-members.html index 31c0a2c3..344e2ce8 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Segment-members.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Segment-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Attributes

 process
 
conditions
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
 tag
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -98,24 +105,25 @@

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Segment.Segment, including all inherited members.

- + - - + + - + - - - - - - - - - + + + + + + + + + +
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
conditions (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
SUAVE::Analyses::Analysis::Analysis.evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
merged(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
@@ -123,7 +131,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Segment.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Segment.html index 5b0a6291..41b01e31 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Segment.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Segment.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Mission.Segments.Segment.Segment Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -105,55 +112,57 @@
-SUAVE.Analyses.Analysis.Analysis -SUAVE.Analyses.Mission.Segments.Segment.Container -SUAVE.Analyses.Mission.Segments.Simple.Simple -SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic -SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Linear_Altitude.Constant_Speed_Linear_Altitude -SUAVE.Analyses.Mission.Segments.Climb.Constant_Throttle_Constant_Speed.Constant_Throttle_Constant_Speed -SUAVE.Analyses.Mission.Segments.Climb.Optimized.Optimized -SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle -SUAVE.Analyses.Mission.Segments.Cruise.Constant_Acceleration_Constant_Altitude.Constant_Acceleration_Constant_Altitude -SUAVE.Analyses.Mission.Segments.Cruise.Constant_Pitch_Rate_Constant_Altitude.Constant_Pitch_Rate_Constant_Altitude -SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude -SUAVE.Analyses.Mission.Segments.Cruise.Constant_Throttle_Constant_Altitude.Constant_Throttle_Constant_Altitude -SUAVE.Analyses.Mission.Segments.Descent.Unknown_Throttle.Unknown_Throttle -SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground -SUAVE.Analyses.Mission.Segments.Hover.Hover.Hover -SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude.Set_Speed_Set_Altitude -SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Throttle.Set_Speed_Set_Throttle - -
+SUAVE.Analyses.Analysis.Analysis +SUAVE.Analyses.Mission.Segments.Segment.Container +SUAVE.Analyses.Mission.Segments.Simple.Simple +SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic +SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Linear_Altitude.Constant_Speed_Linear_Altitude +SUAVE.Analyses.Mission.Segments.Climb.Constant_Throttle_Constant_Speed.Constant_Throttle_Constant_Speed +SUAVE.Analyses.Mission.Segments.Climb.Optimized.Optimized +SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle +SUAVE.Analyses.Mission.Segments.Cruise.Constant_Acceleration_Constant_Altitude.Constant_Acceleration_Constant_Altitude +SUAVE.Analyses.Mission.Segments.Cruise.Constant_Pitch_Rate_Constant_Altitude.Constant_Pitch_Rate_Constant_Altitude +SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude +SUAVE.Analyses.Mission.Segments.Cruise.Constant_Throttle_Constant_Altitude.Constant_Throttle_Constant_Altitude +SUAVE.Analyses.Mission.Segments.Descent.Unknown_Throttle.Unknown_Throttle +SUAVE.Analyses.Mission.Segments.Ground.Battery_Charge_Discharge.Battery_Charge_Discharge +SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground +SUAVE.Analyses.Mission.Segments.Hover.Hover.Hover +SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude.Set_Speed_Set_Altitude +SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude_No_Propulsion.Set_Speed_Set_Altitude_No_Propulsion +SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Throttle.Set_Speed_Set_Throttle +SUAVE.Analyses.Mission.Segments.Transition.Constant_Acceleration_Constant_Angle_Linear_Climb.Constant_Acceleration_Constant_Angle_Linear_Climb +SUAVE.Analyses.Mission.Segments.Transition.Constant_Acceleration_Constant_Pitchrate_Constant_Altitude.Constant_Acceleration_Constant_Pitchrate_Constant_Altitude + + - - + + - - - - - - + + + + + + - - - - - - - - - - - - + + + + + + + + + +

Public Member Functions

def __defaults__ (self)
 
def initialize (self, state)
 
def initialize (self)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def iterate (self)
 
def finalize (self)
 
def evaluate (self, state=None)
 
def merged (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
@@ -169,6 +178,9 @@ + + @@ -221,40 +233,10 @@

-

◆ compile()

+

Reimplemented from SUAVE.Analyses.Analysis.Analysis.

+ +

Reimplemented in SUAVE.Analyses.Mission.Segments.Segment.Container, SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground, SUAVE.Analyses.Mission.Segments.Climb.Optimized.Optimized, SUAVE.Analyses.Mission.Segments.Ground.Landing.Landing, SUAVE.Analyses.Mission.Segments.Ground.Takeoff.Takeoff, SUAVE.Analyses.Mission.Segments.Climb.Constant_Throttle_Constant_Speed.Constant_Throttle_Constant_Speed, SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle, SUAVE.Analyses.Mission.Segments.Cruise.Constant_Throttle_Constant_Altitude.Constant_Throttle_Constant_Altitude, SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude.Set_Speed_Set_Altitude, SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude_No_Propulsion.Set_Speed_Set_Altitude_No_Propulsion, SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Throttle.Set_Speed_Set_Throttle, SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude, SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Linear_Altitude.Constant_Speed_Linear_Altitude, SUAVE.Analyses.Mission.Segments.Descent.Unknown_Throttle.Unknown_Throttle, SUAVE.Analyses.Mission.Segments.Transition.Constant_Acceleration_Constant_Pitchrate_Constant_Altitude.Constant_Acceleration_Constant_Pitchrate_Constant_Altitude, SUAVE.Analyses.Mission.Segments.Cruise.Constant_Acceleration_Constant_Altitude.Constant_Acceleration_Constant_Altitude, SUAVE.Analyses.Mission.Segments.Cruise.Constant_Pitch_Rate_Constant_Altitude.Constant_Pitch_Rate_Constant_Altitude, SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise, SUAVE.Analyses.Mission.Segments.Transition.Constant_Acceleration_Constant_Angle_Linear_Climb.Constant_Acceleration_Constant_Angle_Linear_Climb, SUAVE.Analyses.Mission.Segments.Hover.Climb.Climb, SUAVE.Analyses.Mission.Segments.Hover.Descent.Descent, SUAVE.Analyses.Mission.Segments.Hover.Hover.Hover, SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise, SUAVE.Analyses.Mission.Segments.Climb.Constant_CAS_Constant_Rate.Constant_CAS_Constant_Rate, SUAVE.Analyses.Mission.Segments.Climb.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate, SUAVE.Analyses.Mission.Segments.Descent.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate, SUAVE.Analyses.Mission.Segments.Descent.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate, SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Angle.Constant_Dynamic_Pressure_Constant_Angle, SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Angle.Constant_Mach_Constant_Angle, SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Rate.Constant_Mach_Constant_Rate, SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle, SUAVE.Analyses.Mission.Segments.Climb.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate, SUAVE.Analyses.Mission.Segments.Climb.Linear_Speed_Constant_Rate.Linear_Speed_Constant_Rate, SUAVE.Analyses.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude_Loiter.Constant_Dynamic_Pressure_Constant_Altitude_Loiter, SUAVE.Analyses.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude_Loiter.Constant_Mach_Constant_Altitude_Loiter, SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude_Loiter.Constant_Speed_Constant_Altitude_Loiter, SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle, SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic, SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Linear_Altitude.Constant_Mach_Linear_Altitude, SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate, SUAVE.Analyses.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude.Constant_Dynamic_Pressure_Constant_Altitude, SUAVE.Analyses.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude.Constant_Mach_Constant_Altitude, SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Rate.Constant_Dynamic_Pressure_Constant_Rate, SUAVE.Analyses.Mission.Segments.Simple.Simple, SUAVE.Analyses.Mission.Segments.Ground.Battery_Charge_Discharge.Battery_Charge_Discharge, SUAVE.Analyses.Mission.Segments.Descent.Constant_CAS_Constant_Rate.Constant_CAS_Constant_Rate, and SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate.

-
-
-

Public Attributes

 process
 
conditions
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
 tag
- - - - - - - -
def SUAVE.Analyses.Mission.Segments.Segment.Segment.compile ( self)
-
-
This does nothing
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    State  [Data()]
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
@@ -345,8 +327,8 @@

-

◆ finalize()

+ +

◆ finalize()

@@ -389,8 +361,8 @@

-

◆ initialize()

+ +

◆ initialize()

@@ -433,8 +395,8 @@

-

◆ iterate()

+ +

◆ iterate()

@@ -477,6 +429,40 @@

+

◆ merged()

+ +
+
+ + + + + + + + +
def SUAVE.Analyses.Mission.Segments.Segment.Segment.merged ( self)
+
+
Combines the states of multiple segments
+    
+    Assumptions:
+    None
+    
+    Source:
+    N/A
+    
+    Inputs:
+    None
+    
+    Outputs:
+    state_out [State()]
+    
+    Properties Used:
+    None
+
+
+

The documentation for this class was generated from the following file:
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Analyses/Mission/Segments/Segment.py
@@ -488,7 +474,7 @@

SUAVE + doxygen 1.8.15

diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Segment.js b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Segment.js index d12f232e..828fdc07 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Segment.js +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Segment.js @@ -1,13 +1,14 @@ var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Segment = [ [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Segment.html#aedc70c28743a1190d7b5b773d8b2b548", null ], - [ "compile", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Segment.html#aec843c0340b90e2c9b8f9cb94821b285", null ], [ "converge", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Segment.html#a4175e96a7e4e98d141c3cdb0500dfe88", null ], [ "evaluate", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Segment.html#a473372a75a561da7d96c9295b87db9a1", null ], - [ "finalize", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Segment.html#a0e2bf84e3c5b3e100b7386d1010755e5", null ], - [ "initialize", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Segment.html#acf1d0173938f3aa4ca3ad09c2422bee7", null ], - [ "iterate", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Segment.html#abe02a0e410fe1e801ba5695c617599d9", null ], + [ "finalize", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Segment.html#aff1929fe616e571238044187976708f8", null ], + [ "initialize", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Segment.html#ac1efae3755cf09bc4074de2b8f0d384d", null ], + [ "iterate", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Segment.html#a91e0c868326bac7136e8e53b123d12b3", null ], + [ "merged", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Segment.html#a1aa95e802ed5bd775fc4410cbe64dd23", null ], [ "analyses", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Segment.html#a48471a8adc5732e6a2132075d4e7e604", null ], + [ "conditions", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Segment.html#adf7fee48d4584636779c77dd886b8c19", null ], [ "process", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Segment.html#a6d5fcdf31038cb9d460812c9b5760bb5", null ], [ "settings", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Segment.html#a6633aaa7cae9aba9d6efdb0213869c2b", null ], [ "state", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Segment.html#a9e2d7e168109e4cd1f29669c0f906ccb", null ] diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Segment.png b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Segment.png index 6adc9c91..84060bf0 100644 Binary files a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Segment.png and b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Segment.png differ diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Simple_1_1Simple-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Simple_1_1Simple-members.html index 726fefbf..047ede42 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Simple_1_1Simple-members.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Simple_1_1Simple-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@
- +
@@ -73,7 +78,9 @@
@@ -98,24 +105,25 @@

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Simple.Simple, including all inherited members.

- + - - + + - + - - - - - - - - - + + + + + + + + + +
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Simple.Simple
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
conditions (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
SUAVE::Analyses::Analysis::Analysis.evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
merged(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
@@ -123,7 +131,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Simple_1_1Simple.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Simple_1_1Simple.html index 5f60e8df..0bc3d5fb 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Simple_1_1Simple.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Simple_1_1Simple.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Mission.Segments.Simple.Simple Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -104,57 +111,57 @@
-SUAVE.Analyses.Mission.Segments.Segment.Segment -SUAVE.Analyses.Analysis.Analysis -SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic -SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Linear_Altitude.Constant_Speed_Linear_Altitude -SUAVE.Analyses.Mission.Segments.Climb.Constant_Throttle_Constant_Speed.Constant_Throttle_Constant_Speed -SUAVE.Analyses.Mission.Segments.Climb.Optimized.Optimized -SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle -SUAVE.Analyses.Mission.Segments.Cruise.Constant_Acceleration_Constant_Altitude.Constant_Acceleration_Constant_Altitude -SUAVE.Analyses.Mission.Segments.Cruise.Constant_Pitch_Rate_Constant_Altitude.Constant_Pitch_Rate_Constant_Altitude -SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude -SUAVE.Analyses.Mission.Segments.Cruise.Constant_Throttle_Constant_Altitude.Constant_Throttle_Constant_Altitude -SUAVE.Analyses.Mission.Segments.Descent.Unknown_Throttle.Unknown_Throttle -SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground -SUAVE.Analyses.Mission.Segments.Hover.Hover.Hover -SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude.Set_Speed_Set_Altitude -SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Throttle.Set_Speed_Set_Throttle - -
+SUAVE.Analyses.Mission.Segments.Segment.Segment +SUAVE.Analyses.Analysis.Analysis +SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic +SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Linear_Altitude.Constant_Speed_Linear_Altitude +SUAVE.Analyses.Mission.Segments.Climb.Constant_Throttle_Constant_Speed.Constant_Throttle_Constant_Speed +SUAVE.Analyses.Mission.Segments.Climb.Optimized.Optimized +SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle +SUAVE.Analyses.Mission.Segments.Cruise.Constant_Acceleration_Constant_Altitude.Constant_Acceleration_Constant_Altitude +SUAVE.Analyses.Mission.Segments.Cruise.Constant_Pitch_Rate_Constant_Altitude.Constant_Pitch_Rate_Constant_Altitude +SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude +SUAVE.Analyses.Mission.Segments.Cruise.Constant_Throttle_Constant_Altitude.Constant_Throttle_Constant_Altitude +SUAVE.Analyses.Mission.Segments.Descent.Unknown_Throttle.Unknown_Throttle +SUAVE.Analyses.Mission.Segments.Ground.Battery_Charge_Discharge.Battery_Charge_Discharge +SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground +SUAVE.Analyses.Mission.Segments.Hover.Hover.Hover +SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude.Set_Speed_Set_Altitude +SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude_No_Propulsion.Set_Speed_Set_Altitude_No_Propulsion +SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Throttle.Set_Speed_Set_Throttle +SUAVE.Analyses.Mission.Segments.Transition.Constant_Acceleration_Constant_Angle_Linear_Climb.Constant_Acceleration_Constant_Angle_Linear_Climb +SUAVE.Analyses.Mission.Segments.Transition.Constant_Acceleration_Constant_Pitchrate_Constant_Altitude.Constant_Acceleration_Constant_Pitchrate_Constant_Altitude + + - - - - + + - - - - - - + + + + + + - - - - - - - - - - - - + + + + + + + + + +

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def initialize (self)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def iterate (self)
 
def finalize (self)
 
def evaluate (self, state=None)
 
def merged (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
@@ -171,6 +178,9 @@ + + @@ -223,6 +233,10 @@

SUAVE.Analyses.Mission.Segments.Segment.Segment.

+ +

Reimplemented in SUAVE.Analyses.Mission.Segments.Ground.Ground.Ground, SUAVE.Analyses.Mission.Segments.Climb.Optimized.Optimized, SUAVE.Analyses.Mission.Segments.Ground.Landing.Landing, SUAVE.Analyses.Mission.Segments.Ground.Takeoff.Takeoff, SUAVE.Analyses.Mission.Segments.Climb.Constant_Throttle_Constant_Speed.Constant_Throttle_Constant_Speed, SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle, SUAVE.Analyses.Mission.Segments.Cruise.Constant_Throttle_Constant_Altitude.Constant_Throttle_Constant_Altitude, SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude.Set_Speed_Set_Altitude, SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude_No_Propulsion.Set_Speed_Set_Altitude_No_Propulsion, SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Throttle.Set_Speed_Set_Throttle, SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude, SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Linear_Altitude.Constant_Speed_Linear_Altitude, SUAVE.Analyses.Mission.Segments.Descent.Unknown_Throttle.Unknown_Throttle, SUAVE.Analyses.Mission.Segments.Transition.Constant_Acceleration_Constant_Pitchrate_Constant_Altitude.Constant_Acceleration_Constant_Pitchrate_Constant_Altitude, SUAVE.Analyses.Mission.Segments.Cruise.Constant_Acceleration_Constant_Altitude.Constant_Acceleration_Constant_Altitude, SUAVE.Analyses.Mission.Segments.Cruise.Constant_Pitch_Rate_Constant_Altitude.Constant_Pitch_Rate_Constant_Altitude, SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise, SUAVE.Analyses.Mission.Segments.Transition.Constant_Acceleration_Constant_Angle_Linear_Climb.Constant_Acceleration_Constant_Angle_Linear_Climb, SUAVE.Analyses.Mission.Segments.Hover.Climb.Climb, SUAVE.Analyses.Mission.Segments.Hover.Descent.Descent, SUAVE.Analyses.Mission.Segments.Hover.Hover.Hover, SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle_Noise.Constant_Speed_Constant_Angle_Noise, SUAVE.Analyses.Mission.Segments.Climb.Constant_CAS_Constant_Rate.Constant_CAS_Constant_Rate, SUAVE.Analyses.Mission.Segments.Climb.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate, SUAVE.Analyses.Mission.Segments.Descent.Constant_EAS_Constant_Rate.Constant_EAS_Constant_Rate, SUAVE.Analyses.Mission.Segments.Descent.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate, SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Angle.Constant_Dynamic_Pressure_Constant_Angle, SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Angle.Constant_Mach_Constant_Angle, SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Constant_Rate.Constant_Mach_Constant_Rate, SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle, SUAVE.Analyses.Mission.Segments.Climb.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate, SUAVE.Analyses.Mission.Segments.Climb.Linear_Speed_Constant_Rate.Linear_Speed_Constant_Rate, SUAVE.Analyses.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude_Loiter.Constant_Dynamic_Pressure_Constant_Altitude_Loiter, SUAVE.Analyses.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude_Loiter.Constant_Mach_Constant_Altitude_Loiter, SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude_Loiter.Constant_Speed_Constant_Altitude_Loiter, SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle.Constant_Speed_Constant_Angle, SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic, SUAVE.Analyses.Mission.Segments.Climb.Constant_Mach_Linear_Altitude.Constant_Mach_Linear_Altitude, SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate, SUAVE.Analyses.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude.Constant_Dynamic_Pressure_Constant_Altitude, SUAVE.Analyses.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude.Constant_Mach_Constant_Altitude, SUAVE.Analyses.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Rate.Constant_Dynamic_Pressure_Constant_Rate, SUAVE.Analyses.Mission.Segments.Ground.Battery_Charge_Discharge.Battery_Charge_Discharge, SUAVE.Analyses.Mission.Segments.Descent.Constant_CAS_Constant_Rate.Constant_CAS_Constant_Rate, and SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Rate.Constant_Speed_Constant_Rate.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Simple_1_1Simple.png b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Simple_1_1Simple.png index 596f06fd..5f0485fc 100644 Binary files a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Simple_1_1Simple.png and b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Simple_1_1Simple.png differ diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Altitude_1_1Seae0052171c39704a97e8acae6ffdafb.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Altitude_1_1Seae0052171c39704a97e8acae6ffdafb.html index 5b87059b..a33d9c0e 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Altitude_1_1Seae0052171c39704a97e8acae6ffdafb.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Altitude_1_1Seae0052171c39704a97e8acae6ffdafb.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Additional Inherited Members

 process
 
conditions
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
 tag
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -98,30 +105,31 @@

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude.Set_Speed_Set_Altitude, including all inherited members.

- + - - + + - + - - - - - - - - - - - - + + + + + + + + + + + + +
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude.Set_Speed_Set_Altitude
air_speed (defined in SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude.Set_Speed_Set_Altitude)SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude.Set_Speed_Set_Altitude
altitude (defined in SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude.Set_Speed_Set_Altitude)SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude.Set_Speed_Set_Altitude
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
conditions (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
distance (defined in SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude.Set_Speed_Set_Altitude)SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude.Set_Speed_Set_Altitude
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
SUAVE::Analyses::Analysis::Analysis.evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
x_accel (defined in SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude.Set_Speed_Set_Altitude)SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude.Set_Speed_Set_Altitude
z_accel (defined in SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude.Set_Speed_Set_Altitude)SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude.Set_Speed_Set_Altitude
finalize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
merged(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
x_accel (defined in SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude.Set_Speed_Set_Altitude)SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude.Set_Speed_Set_Altitude
z_accel (defined in SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude.Set_Speed_Set_Altitude)SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude.Set_Speed_Set_Altitude
@@ -129,7 +137,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Altitude_1_1Set__Speed__Set__Altitude.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Altitude_1_1Set__Speed__Set__Altitude.html index 6c7ff812..0b6e22c9 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Altitude_1_1Set__Speed__Set__Altitude.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Altitude_1_1Set__Speed__Set__Altitude.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude.Set_Speed_Set_Altitude Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -109,47 +116,37 @@ SUAVE.Analyses.Mission.Segments.Simple.Simple SUAVE.Analyses.Mission.Segments.Segment.Segment SUAVE.Analyses.Analysis.Analysis - -
+ + - - - - - - - - - - + + - - - - - - + + + + + + - - - - - - - - - - - - + + + + + + + + + +

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def initialize (self)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def iterate (self)
 
def finalize (self)
 
def evaluate (self, state=None)
 
def merged (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
@@ -185,6 +182,9 @@ + + @@ -238,6 +238,8 @@

SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Altitude__No_660be05666a18eb7201c7425b4456ff1.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Altitude__No_660be05666a18eb7201c7425b4456ff1.html new file mode 100644 index 00000000..706724f6 --- /dev/null +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Altitude__No_660be05666a18eb7201c7425b4456ff1.html @@ -0,0 +1,257 @@ + + + + + + + +SUAVE: SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude_No_Propulsion.Set_Speed_Set_Altitude_No_Propulsion Class Reference + + + + + + + + + + + + + + + +
+
+

Public Attributes

 process
 
conditions
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
 tag
+ + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+ + + + + +
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude_No_Propulsion.Set_Speed_Set_Altitude_No_Propulsion Class Reference
+
+
+
+Inheritance diagram for SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude_No_Propulsion.Set_Speed_Set_Altitude_No_Propulsion:
+
+
+ + +SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic +SUAVE.Analyses.Mission.Segments.Simple.Simple +SUAVE.Analyses.Mission.Segments.Segment.Segment +SUAVE.Analyses.Analysis.Analysis + +
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def initialize (self)
 
def converge (self, state)
 
def iterate (self)
 
def finalize (self)
 
def evaluate (self, state=None)
 
def merged (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Attributes

altitude
 
air_speed
 
distance
 
z_accel
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
temperature_deviation
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
settings
 
state
 
analyses
 
process
 
conditions
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
+

Detailed Description

+
This is a segment that is solved using a single point. A snapshot in time.
+    We fix the speed and altitude. Throttle is solved from those.
+
+    Assumptions:
+    None
+    
+    Source:
+    None
+

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude_No_Propulsion.Set_Speed_Set_Altitude_No_Propulsion.__defaults__ ( self)
+
+
This sets the default solver flow. Anything in here can be modified after initializing a segment.
+    
+    Assumptions:
+    None
+    
+    Source:
+    N/A
+    
+    Inputs:
+    None
+    
+    Outputs:
+    None
+    
+    Properties Used:
+    None
+
+

Reimplemented from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic.

+ +
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Analyses/Mission/Segments/Single_Point/Set_Speed_Set_Altitude_No_Propulsion.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Altitude__No_660be05666a18eb7201c7425b4456ff1.js b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Altitude__No_660be05666a18eb7201c7425b4456ff1.js new file mode 100644 index 00000000..81ed155b --- /dev/null +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Altitude__No_660be05666a18eb7201c7425b4456ff1.js @@ -0,0 +1,8 @@ +var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Altitude__No_660be05666a18eb7201c7425b4456ff1 = +[ + [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Altitude__No_660be05666a18eb7201c7425b4456ff1.html#a1d0bccee24392981b447353a6a6e58bd", null ], + [ "air_speed", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Altitude__No_660be05666a18eb7201c7425b4456ff1.html#a77412ee8002a16d1cc1b07fe89909fae", null ], + [ "altitude", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Altitude__No_660be05666a18eb7201c7425b4456ff1.html#a8205a608d30e1d4e730618d89de852fc", null ], + [ "distance", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Altitude__No_660be05666a18eb7201c7425b4456ff1.html#adb78847a4e63ce7211c4b53bc425d8fd", null ], + [ "z_accel", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Altitude__No_660be05666a18eb7201c7425b4456ff1.html#a102fad69c2663702f98dd82dbff6dbfd", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Altitude__No_660be05666a18eb7201c7425b4456ff1.png b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Altitude__No_660be05666a18eb7201c7425b4456ff1.png new file mode 100644 index 00000000..d64c1063 Binary files /dev/null and b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Altitude__No_660be05666a18eb7201c7425b4456ff1.png differ diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Altitude__No_9bd0765ba208bc26d0aa0ea5b6e3dff8.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Altitude__No_9bd0765ba208bc26d0aa0ea5b6e3dff8.html new file mode 100644 index 00000000..41483671 --- /dev/null +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Altitude__No_9bd0765ba208bc26d0aa0ea5b6e3dff8.html @@ -0,0 +1,143 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude_No_Propulsion.Set_Speed_Set_Altitude_No_Propulsion Member List
+
+
+ +

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude_No_Propulsion.Set_Speed_Set_Altitude_No_Propulsion, including all inherited members.

+ + + + + + + + + + + + + + + + + + + + + + + + + +
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude_No_Propulsion.Set_Speed_Set_Altitude_No_Propulsion
air_speed (defined in SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude_No_Propulsion.Set_Speed_Set_Altitude_No_Propulsion)SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude_No_Propulsion.Set_Speed_Set_Altitude_No_Propulsion
altitude (defined in SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude_No_Propulsion.Set_Speed_Set_Altitude_No_Propulsion)SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude_No_Propulsion.Set_Speed_Set_Altitude_No_Propulsion
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
conditions (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
distance (defined in SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude_No_Propulsion.Set_Speed_Set_Altitude_No_Propulsion)SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude_No_Propulsion.Set_Speed_Set_Altitude_No_Propulsion
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
merged(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
z_accel (defined in SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude_No_Propulsion.Set_Speed_Set_Altitude_No_Propulsion)SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude_No_Propulsion.Set_Speed_Set_Altitude_No_Propulsion
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Throttle_1_1S9161113e971a925856bf4082306f653a.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Throttle_1_1S9161113e971a925856bf4082306f653a.html index 3406dd43..32ee846c 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Throttle_1_1S9161113e971a925856bf4082306f653a.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Throttle_1_1S9161113e971a925856bf4082306f653a.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -98,29 +105,30 @@

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Throttle.Set_Speed_Set_Throttle, including all inherited members.

- + - - + + - + - - - - - - - - - - - - + + + + + + + + + + + + +
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Throttle.Set_Speed_Set_Throttle
air_speed (defined in SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Throttle.Set_Speed_Set_Throttle)SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Throttle.Set_Speed_Set_Throttle
altitude (defined in SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Throttle.Set_Speed_Set_Throttle)SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Throttle.Set_Speed_Set_Throttle
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
compile(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
conditions (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
SUAVE::Analyses::Analysis::Analysis.evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
throttle (defined in SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Throttle.Set_Speed_Set_Throttle)SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Throttle.Set_Speed_Set_Throttle
z_accel (defined in SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Throttle.Set_Speed_Set_Throttle)SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Throttle.Set_Speed_Set_Throttle
finalize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
merged(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
throttle (defined in SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Throttle.Set_Speed_Set_Throttle)SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Throttle.Set_Speed_Set_Throttle
z_accel (defined in SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Throttle.Set_Speed_Set_Throttle)SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Throttle.Set_Speed_Set_Throttle
@@ -128,7 +136,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Throttle_1_1Set__Speed__Set__Throttle.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Throttle_1_1Set__Speed__Set__Throttle.html index ea81ad95..823a3972 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Throttle_1_1Set__Speed__Set__Throttle.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Throttle_1_1Set__Speed__Set__Throttle.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Throttle.Set_Speed_Set_Throttle Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -109,47 +116,37 @@ SUAVE.Analyses.Mission.Segments.Simple.Simple SUAVE.Analyses.Mission.Segments.Segment.Segment SUAVE.Analyses.Analysis.Analysis - -
+ + - - - - - - - - - - + + - - - - - - + + + + + + - - - - - - - - - - - - + + + + + + + + + +

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Simple.Simple
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def __defaults__ (self)
 
def initialize (self, state)
 
def initialize (self)
 
def converge (self, state)
 
def iterate (self, state)
 
def finalize (self, state)
 
def compile (self)
 
def iterate (self)
 
def finalize (self)
 
def evaluate (self, state=None)
 
def merged (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
@@ -182,6 +179,9 @@ + + @@ -235,6 +235,8 @@

SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Transition_1_1Constant__Acceleration__Constant_2295952caac21c4a49a6ece0c9d2ce15.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Transition_1_1Constant__Acceleration__Constant_2295952caac21c4a49a6ece0c9d2ce15.html new file mode 100644 index 00000000..b6dbe712 --- /dev/null +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Transition_1_1Constant__Acceleration__Constant_2295952caac21c4a49a6ece0c9d2ce15.html @@ -0,0 +1,265 @@ + + + + + + + +SUAVE: SUAVE.Analyses.Mission.Segments.Transition.Constant_Acceleration_Constant_Angle_Linear_Climb.Constant_Acceleration_Constant_Angle_Linear_Climb Class Reference + + + + + + + + + + + + + + + +
+
+

Public Attributes

 process
 
conditions
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
 tag
+ + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+ + + + + +
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Analyses.Mission.Segments.Transition.Constant_Acceleration_Constant_Angle_Linear_Climb.Constant_Acceleration_Constant_Angle_Linear_Climb Class Reference
+
+
+
+Inheritance diagram for SUAVE.Analyses.Mission.Segments.Transition.Constant_Acceleration_Constant_Angle_Linear_Climb.Constant_Acceleration_Constant_Angle_Linear_Climb:
+
+
+ + +SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic +SUAVE.Analyses.Mission.Segments.Simple.Simple +SUAVE.Analyses.Mission.Segments.Segment.Segment +SUAVE.Analyses.Analysis.Analysis + +
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def initialize (self)
 
def converge (self, state)
 
def iterate (self)
 
def finalize (self)
 
def evaluate (self, state=None)
 
def merged (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Attributes

altitude_start
 
altitude_end
 
climb_angle
 
acceleration
 
pitch_initial
 
pitch_final
 
true_course
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
temperature_deviation
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
settings
 
state
 
analyses
 
process
 
conditions
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
+

Detailed Description

+
Vehicle accelerates at a constant rate between two airspeeds.
+
+    Assumptions:
+    None
+    
+    Source:
+    None
+

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Analyses.Mission.Segments.Transition.Constant_Acceleration_Constant_Angle_Linear_Climb.Constant_Acceleration_Constant_Angle_Linear_Climb.__defaults__ ( self)
+
+
This sets the default solver flow. Anything in here can be modified after initializing a segment.
+    
+    Assumptions:
+    None
+    
+    Source:
+    N/A
+    
+    Inputs:
+    None
+    
+    Outputs:
+    None
+    
+    Properties Used:
+    None
+
+

Reimplemented from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic.

+ +
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Analyses/Mission/Segments/Transition/Constant_Acceleration_Constant_Angle_Linear_Climb.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Transition_1_1Constant__Acceleration__Constant_2295952caac21c4a49a6ece0c9d2ce15.js b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Transition_1_1Constant__Acceleration__Constant_2295952caac21c4a49a6ece0c9d2ce15.js new file mode 100644 index 00000000..d3fd1ff0 --- /dev/null +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Transition_1_1Constant__Acceleration__Constant_2295952caac21c4a49a6ece0c9d2ce15.js @@ -0,0 +1,11 @@ +var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Transition_1_1Constant__Acceleration__Constant_2295952caac21c4a49a6ece0c9d2ce15 = +[ + [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Transition_1_1Constant__Acceleration__Constant_2295952caac21c4a49a6ece0c9d2ce15.html#a401f5d5529d22d5bb1030815a8e23535", null ], + [ "acceleration", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Transition_1_1Constant__Acceleration__Constant_2295952caac21c4a49a6ece0c9d2ce15.html#ace5a252f6ba01615cbe914e35e4f6e18", null ], + [ "altitude_end", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Transition_1_1Constant__Acceleration__Constant_2295952caac21c4a49a6ece0c9d2ce15.html#a30f50c155d138d070c7adb42369f767f", null ], + [ "altitude_start", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Transition_1_1Constant__Acceleration__Constant_2295952caac21c4a49a6ece0c9d2ce15.html#a793d6afc8124dc9108e5803c99d08810", null ], + [ "climb_angle", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Transition_1_1Constant__Acceleration__Constant_2295952caac21c4a49a6ece0c9d2ce15.html#ac3049b06489d272c11719565230ef478", null ], + [ "pitch_final", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Transition_1_1Constant__Acceleration__Constant_2295952caac21c4a49a6ece0c9d2ce15.html#a5159c089bfa470004259d49311abf2c4", null ], + [ "pitch_initial", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Transition_1_1Constant__Acceleration__Constant_2295952caac21c4a49a6ece0c9d2ce15.html#a466b4c626cb3ef2bbea23bbc6f6cb9a5", null ], + [ "true_course", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Transition_1_1Constant__Acceleration__Constant_2295952caac21c4a49a6ece0c9d2ce15.html#afcc7bb3471f3a6c045c178796f0bfd0a", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Transition_1_1Constant__Acceleration__Constant_2295952caac21c4a49a6ece0c9d2ce15.png b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Transition_1_1Constant__Acceleration__Constant_2295952caac21c4a49a6ece0c9d2ce15.png new file mode 100644 index 00000000..2546d868 Binary files /dev/null and b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Transition_1_1Constant__Acceleration__Constant_2295952caac21c4a49a6ece0c9d2ce15.png differ diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Transition_1_1Constant__Acceleration__Constant_5193e56b55371497cdd7346b5b49e506.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Transition_1_1Constant__Acceleration__Constant_5193e56b55371497cdd7346b5b49e506.html new file mode 100644 index 00000000..6ce9660a --- /dev/null +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Transition_1_1Constant__Acceleration__Constant_5193e56b55371497cdd7346b5b49e506.html @@ -0,0 +1,265 @@ + + + + + + + +SUAVE: SUAVE.Analyses.Mission.Segments.Transition.Constant_Acceleration_Constant_Pitchrate_Constant_Altitude.Constant_Acceleration_Constant_Pitchrate_Constant_Altitude Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Analyses.Mission.Segments.Transition.Constant_Acceleration_Constant_Pitchrate_Constant_Altitude.Constant_Acceleration_Constant_Pitchrate_Constant_Altitude Class Reference
+
+
+
+Inheritance diagram for SUAVE.Analyses.Mission.Segments.Transition.Constant_Acceleration_Constant_Pitchrate_Constant_Altitude.Constant_Acceleration_Constant_Pitchrate_Constant_Altitude:
+
+
+ + +SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic +SUAVE.Analyses.Mission.Segments.Simple.Simple +SUAVE.Analyses.Mission.Segments.Segment.Segment +SUAVE.Analyses.Analysis.Analysis + +
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def initialize (self)
 
def converge (self, state)
 
def iterate (self)
 
def finalize (self)
 
def evaluate (self, state=None)
 
def merged (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Attributes

altitude
 
acceleration
 
air_speed_start
 
air_speed_end
 
pitch_initial
 
pitch_final
 
true_course
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
temperature_deviation
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
settings
 
state
 
analyses
 
process
 
conditions
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
+

Detailed Description

+
Vehicle accelerates at a constant rate between two airspeeds.
+
+    Assumptions:
+    None
+    
+    Source:
+    None
+

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Analyses.Mission.Segments.Transition.Constant_Acceleration_Constant_Pitchrate_Constant_Altitude.Constant_Acceleration_Constant_Pitchrate_Constant_Altitude.__defaults__ ( self)
+
+
This sets the default solver flow. Anything in here can be modified after initializing a segment.
+    
+    Assumptions:
+    None
+    
+    Source:
+    N/A
+    
+    Inputs:
+    None
+    
+    Outputs:
+    None
+    
+    Properties Used:
+    None
+
+

Reimplemented from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic.

+ +
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Analyses/Mission/Segments/Transition/Constant_Acceleration_Constant_Pitchrate_Constant_Altitude.py
  • +
+
+
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+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
SUAVE.Analyses.Mission.Segments.Transition.Constant_Acceleration_Constant_Pitchrate_Constant_Altitude.Constant_Acceleration_Constant_Pitchrate_Constant_Altitude Member List
+
+
+ +

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Transition.Constant_Acceleration_Constant_Pitchrate_Constant_Altitude.Constant_Acceleration_Constant_Pitchrate_Constant_Altitude, including all inherited members.

+ + + + + + + + + + + + + + + + + + + + + + + + + + + + +
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Transition.Constant_Acceleration_Constant_Pitchrate_Constant_Altitude.Constant_Acceleration_Constant_Pitchrate_Constant_Altitude
acceleration (defined in SUAVE.Analyses.Mission.Segments.Transition.Constant_Acceleration_Constant_Pitchrate_Constant_Altitude.Constant_Acceleration_Constant_Pitchrate_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Transition.Constant_Acceleration_Constant_Pitchrate_Constant_Altitude.Constant_Acceleration_Constant_Pitchrate_Constant_Altitude
air_speed_end (defined in SUAVE.Analyses.Mission.Segments.Transition.Constant_Acceleration_Constant_Pitchrate_Constant_Altitude.Constant_Acceleration_Constant_Pitchrate_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Transition.Constant_Acceleration_Constant_Pitchrate_Constant_Altitude.Constant_Acceleration_Constant_Pitchrate_Constant_Altitude
air_speed_start (defined in SUAVE.Analyses.Mission.Segments.Transition.Constant_Acceleration_Constant_Pitchrate_Constant_Altitude.Constant_Acceleration_Constant_Pitchrate_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Transition.Constant_Acceleration_Constant_Pitchrate_Constant_Altitude.Constant_Acceleration_Constant_Pitchrate_Constant_Altitude
altitude (defined in SUAVE.Analyses.Mission.Segments.Transition.Constant_Acceleration_Constant_Pitchrate_Constant_Altitude.Constant_Acceleration_Constant_Pitchrate_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Transition.Constant_Acceleration_Constant_Pitchrate_Constant_Altitude.Constant_Acceleration_Constant_Pitchrate_Constant_Altitude
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
conditions (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
merged(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
pitch_final (defined in SUAVE.Analyses.Mission.Segments.Transition.Constant_Acceleration_Constant_Pitchrate_Constant_Altitude.Constant_Acceleration_Constant_Pitchrate_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Transition.Constant_Acceleration_Constant_Pitchrate_Constant_Altitude.Constant_Acceleration_Constant_Pitchrate_Constant_Altitude
pitch_initial (defined in SUAVE.Analyses.Mission.Segments.Transition.Constant_Acceleration_Constant_Pitchrate_Constant_Altitude.Constant_Acceleration_Constant_Pitchrate_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Transition.Constant_Acceleration_Constant_Pitchrate_Constant_Altitude.Constant_Acceleration_Constant_Pitchrate_Constant_Altitude
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
true_course (defined in SUAVE.Analyses.Mission.Segments.Transition.Constant_Acceleration_Constant_Pitchrate_Constant_Altitude.Constant_Acceleration_Constant_Pitchrate_Constant_Altitude)SUAVE.Analyses.Mission.Segments.Transition.Constant_Acceleration_Constant_Pitchrate_Constant_Altitude.Constant_Acceleration_Constant_Pitchrate_Constant_Altitude
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Transition_1_1Constant__Acceleration__Constant_779d6cdebc6ee1f0c6757bec4a79156d.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Transition_1_1Constant__Acceleration__Constant_779d6cdebc6ee1f0c6757bec4a79156d.html new file mode 100644 index 00000000..adb64446 --- /dev/null +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Transition_1_1Constant__Acceleration__Constant_779d6cdebc6ee1f0c6757bec4a79156d.html @@ -0,0 +1,146 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
SUAVE.Analyses.Mission.Segments.Transition.Constant_Acceleration_Constant_Angle_Linear_Climb.Constant_Acceleration_Constant_Angle_Linear_Climb Member List
+
+
+ +

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Transition.Constant_Acceleration_Constant_Angle_Linear_Climb.Constant_Acceleration_Constant_Angle_Linear_Climb, including all inherited members.

+ + + + + + + + + + + + + + + + + + + + + + + + + + + + +
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Transition.Constant_Acceleration_Constant_Angle_Linear_Climb.Constant_Acceleration_Constant_Angle_Linear_Climb
acceleration (defined in SUAVE.Analyses.Mission.Segments.Transition.Constant_Acceleration_Constant_Angle_Linear_Climb.Constant_Acceleration_Constant_Angle_Linear_Climb)SUAVE.Analyses.Mission.Segments.Transition.Constant_Acceleration_Constant_Angle_Linear_Climb.Constant_Acceleration_Constant_Angle_Linear_Climb
altitude_end (defined in SUAVE.Analyses.Mission.Segments.Transition.Constant_Acceleration_Constant_Angle_Linear_Climb.Constant_Acceleration_Constant_Angle_Linear_Climb)SUAVE.Analyses.Mission.Segments.Transition.Constant_Acceleration_Constant_Angle_Linear_Climb.Constant_Acceleration_Constant_Angle_Linear_Climb
altitude_start (defined in SUAVE.Analyses.Mission.Segments.Transition.Constant_Acceleration_Constant_Angle_Linear_Climb.Constant_Acceleration_Constant_Angle_Linear_Climb)SUAVE.Analyses.Mission.Segments.Transition.Constant_Acceleration_Constant_Angle_Linear_Climb.Constant_Acceleration_Constant_Angle_Linear_Climb
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
climb_angle (defined in SUAVE.Analyses.Mission.Segments.Transition.Constant_Acceleration_Constant_Angle_Linear_Climb.Constant_Acceleration_Constant_Angle_Linear_Climb)SUAVE.Analyses.Mission.Segments.Transition.Constant_Acceleration_Constant_Angle_Linear_Climb.Constant_Acceleration_Constant_Angle_Linear_Climb
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
conditions (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
merged(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
pitch_final (defined in SUAVE.Analyses.Mission.Segments.Transition.Constant_Acceleration_Constant_Angle_Linear_Climb.Constant_Acceleration_Constant_Angle_Linear_Climb)SUAVE.Analyses.Mission.Segments.Transition.Constant_Acceleration_Constant_Angle_Linear_Climb.Constant_Acceleration_Constant_Angle_Linear_Climb
pitch_initial (defined in SUAVE.Analyses.Mission.Segments.Transition.Constant_Acceleration_Constant_Angle_Linear_Climb.Constant_Acceleration_Constant_Angle_Linear_Climb)SUAVE.Analyses.Mission.Segments.Transition.Constant_Acceleration_Constant_Angle_Linear_Climb.Constant_Acceleration_Constant_Angle_Linear_Climb
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
true_course (defined in SUAVE.Analyses.Mission.Segments.Transition.Constant_Acceleration_Constant_Angle_Linear_Climb.Constant_Acceleration_Constant_Angle_Linear_Climb)SUAVE.Analyses.Mission.Segments.Transition.Constant_Acceleration_Constant_Angle_Linear_Climb.Constant_Acceleration_Constant_Angle_Linear_Climb
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Transition_1_1Lift__Cruise__Optimized_1_1Lift__Cruise__Optimized-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Transition_1_1Lift__Cruise__Optimized_1_1Lift__Cruise__Optimized-members.html new file mode 100644 index 00000000..cdcfb98e --- /dev/null +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Transition_1_1Lift__Cruise__Optimized_1_1Lift__Cruise__Optimized-members.html @@ -0,0 +1,149 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.0 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
SUAVE.Analyses.Mission.Segments.Transition.Lift_Cruise_Optimized.Lift_Cruise_Optimized Member List
+
+
+ +

This is the complete list of members for SUAVE.Analyses.Mission.Segments.Transition.Lift_Cruise_Optimized.Lift_Cruise_Optimized, including all inherited members.

+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Mission.Segments.Transition.Lift_Cruise_Optimized.Lift_Cruise_Optimized
acceleration (defined in SUAVE.Analyses.Mission.Segments.Transition.Lift_Cruise_Optimized.Lift_Cruise_Optimized)SUAVE.Analyses.Mission.Segments.Transition.Lift_Cruise_Optimized.Lift_Cruise_Optimized
air_speed_end (defined in SUAVE.Analyses.Mission.Segments.Transition.Lift_Cruise_Optimized.Lift_Cruise_Optimized)SUAVE.Analyses.Mission.Segments.Transition.Lift_Cruise_Optimized.Lift_Cruise_Optimized
air_speed_start (defined in SUAVE.Analyses.Mission.Segments.Transition.Lift_Cruise_Optimized.Lift_Cruise_Optimized)SUAVE.Analyses.Mission.Segments.Transition.Lift_Cruise_Optimized.Lift_Cruise_Optimized
algorithm (defined in SUAVE.Analyses.Mission.Segments.Transition.Lift_Cruise_Optimized.Lift_Cruise_Optimized)SUAVE.Analyses.Mission.Segments.Transition.Lift_Cruise_Optimized.Lift_Cruise_Optimized
altitude (defined in SUAVE.Analyses.Mission.Segments.Transition.Lift_Cruise_Optimized.Lift_Cruise_Optimized)SUAVE.Analyses.Mission.Segments.Transition.Lift_Cruise_Optimized.Lift_Cruise_Optimized
analyses (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
conditions (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
converge(self, state)SUAVE.Analyses.Mission.Segments.Segment.Segment
evaluate(self, state=None)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
SUAVE::Analyses::Analysis::Analysis.initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
iterate(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
lift_coefficient_limit (defined in SUAVE.Analyses.Mission.Segments.Transition.Lift_Cruise_Optimized.Lift_Cruise_Optimized)SUAVE.Analyses.Mission.Segments.Transition.Lift_Cruise_Optimized.Lift_Cruise_Optimized
merged(self)SUAVE.Analyses.Mission.Segments.Segment.Segment
minimize (defined in SUAVE.Analyses.Mission.Segments.Transition.Lift_Cruise_Optimized.Lift_Cruise_Optimized)SUAVE.Analyses.Mission.Segments.Transition.Lift_Cruise_Optimized.Lift_Cruise_Optimized
objective (defined in SUAVE.Analyses.Mission.Segments.Transition.Lift_Cruise_Optimized.Lift_Cruise_Optimized)SUAVE.Analyses.Mission.Segments.Transition.Lift_Cruise_Optimized.Lift_Cruise_Optimized
pitch_final (defined in SUAVE.Analyses.Mission.Segments.Transition.Lift_Cruise_Optimized.Lift_Cruise_Optimized)SUAVE.Analyses.Mission.Segments.Transition.Lift_Cruise_Optimized.Lift_Cruise_Optimized
pitch_initial (defined in SUAVE.Analyses.Mission.Segments.Transition.Lift_Cruise_Optimized.Lift_Cruise_Optimized)SUAVE.Analyses.Mission.Segments.Transition.Lift_Cruise_Optimized.Lift_Cruise_Optimized
process (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
settings (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
state (defined in SUAVE.Analyses.Mission.Segments.Segment.Segment)SUAVE.Analyses.Mission.Segments.Segment.Segment
tag (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
temperature_deviation (defined in SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic)SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Transition_1_1Lift__Cruise__Optimized_1_1Lift__Cruise__Optimized.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Transition_1_1Lift__Cruise__Optimized_1_1Lift__Cruise__Optimized.html new file mode 100644 index 00000000..0e8884a6 --- /dev/null +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Transition_1_1Lift__Cruise__Optimized_1_1Lift__Cruise__Optimized.html @@ -0,0 +1,282 @@ + + + + + + + +SUAVE: SUAVE.Analyses.Mission.Segments.Transition.Lift_Cruise_Optimized.Lift_Cruise_Optimized Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.0 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Analyses.Mission.Segments.Transition.Lift_Cruise_Optimized.Lift_Cruise_Optimized Class Reference
+
+
+
+Inheritance diagram for SUAVE.Analyses.Mission.Segments.Transition.Lift_Cruise_Optimized.Lift_Cruise_Optimized:
+
+
+ + +SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic +SUAVE.Analyses.Mission.Segments.Simple.Simple +SUAVE.Analyses.Mission.Segments.Segment.Segment +SUAVE.Analyses.Analysis.Analysis + +
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
def initialize (self)
 
def converge (self, state)
 
def iterate (self)
 
def finalize (self)
 
def evaluate (self, state=None)
 
def merged (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Attributes

altitude
 
air_speed_start
 
air_speed_end
 
acceleration
 
pitch_initial
 
pitch_final
 
objective
 
minimize
 
lift_coefficient_limit
 
algorithm
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic
temperature_deviation
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment
settings
 
state
 
analyses
 
process
 
conditions
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
+

Detailed Description

+
Optimize your transition segment. This is useful if you're not sure how your vehicle should transition.
+    You can set any conditions parameter as the objective, for example setting time to transition or vehicle mass
+    
+    The ending airspeed is an optional parameter.
+    
+    This segment takes far longer to run than a normal segment. Wrapping this into a vehicle optimization
+    has not yet been tested for robustness.
+    
+
+    Assumptions:
+    Can use SNOPT if you have it installed through PyOpt. But defaults to SLSQP through 
+    Runs a linear true airspeed mission first to initialize conditions.
+    
+    Source:
+    None
+

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Analyses.Mission.Segments.Transition.Lift_Cruise_Optimized.Lift_Cruise_Optimized.__defaults__ ( self)
+
+
This sets the default solver flow. Anything in here can be modified after initializing a segment.
+    
+    Assumptions:
+    None
+    
+    Source:
+    N/A
+    
+    Inputs:
+    None
+    
+    Outputs:
+    None
+    
+    Properties Used:
+    None
+
+

Reimplemented from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic.

+ +
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Analyses/Mission/Segments/Transition/Lift_Cruise_Optimized.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Transition_1_1Lift__Cruise__Optimized_1_1Lift__Cruise__Optimized.js b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Transition_1_1Lift__Cruise__Optimized_1_1Lift__Cruise__Optimized.js new file mode 100644 index 00000000..5a587416 --- /dev/null +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Transition_1_1Lift__Cruise__Optimized_1_1Lift__Cruise__Optimized.js @@ -0,0 +1,14 @@ +var classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Transition_1_1Lift__Cruise__Optimized_1_1Lift__Cruise__Optimized = +[ + [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Transition_1_1Lift__Cruise__Optimized_1_1Lift__Cruise__Optimized.html#a8047ff3e217855c0f0e950d5cfae04db", null ], + [ "acceleration", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Transition_1_1Lift__Cruise__Optimized_1_1Lift__Cruise__Optimized.html#a55a825c39771fdb665311fde8194b4e7", null ], + [ "air_speed_end", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Transition_1_1Lift__Cruise__Optimized_1_1Lift__Cruise__Optimized.html#ab58366d01c8eb975728613711f50f7a3", null ], + [ "air_speed_start", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Transition_1_1Lift__Cruise__Optimized_1_1Lift__Cruise__Optimized.html#ac7a423db483b7c756b62f7cbdce8b7c7", null ], + [ "algorithm", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Transition_1_1Lift__Cruise__Optimized_1_1Lift__Cruise__Optimized.html#a853713c88b018dd90e0b48cab1376835", null ], + [ "altitude", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Transition_1_1Lift__Cruise__Optimized_1_1Lift__Cruise__Optimized.html#ad8f75cf7ae24590cc6ab59c121ed6bc6", null ], + [ "lift_coefficient_limit", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Transition_1_1Lift__Cruise__Optimized_1_1Lift__Cruise__Optimized.html#a26c5539eb661f371b9eec3c63d65ac5f", null ], + [ "minimize", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Transition_1_1Lift__Cruise__Optimized_1_1Lift__Cruise__Optimized.html#aa74a394797aa602d85cfc4e07b8ae8c6", null ], + [ "objective", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Transition_1_1Lift__Cruise__Optimized_1_1Lift__Cruise__Optimized.html#aedc95207b06ead454af30d7323a03609", null ], + [ "pitch_final", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Transition_1_1Lift__Cruise__Optimized_1_1Lift__Cruise__Optimized.html#a1bb20f2ced6f9258a6079804266fac01", null ], + [ "pitch_initial", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Transition_1_1Lift__Cruise__Optimized_1_1Lift__Cruise__Optimized.html#aab7b983a694eaa152c61e2ff819ba67b", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Transition_1_1Lift__Cruise__Optimized_1_1Lift__Cruise__Optimized.png b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Transition_1_1Lift__Cruise__Optimized_1_1Lift__Cruise__Optimized.png new file mode 100644 index 00000000..286cd4c0 Binary files /dev/null and b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Transition_1_1Lift__Cruise__Optimized_1_1Lift__Cruise__Optimized.png differ diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Sequential__Segments_1_1Sequential__Segments-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Sequential__Segments_1_1Sequential__Segments-members.html index 1e358538..65df2bf4 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Sequential__Segments_1_1Sequential__Segments-members.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Sequential__Segments_1_1Sequential__Segments-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -108,7 +115,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Sequential__Segments_1_1Sequential__Segments.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Sequential__Segments_1_1Sequential__Segments.html index 0fbc330f..bee2a19c 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Sequential__Segments_1_1Sequential__Segments.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Sequential__Segments_1_1Sequential__Segments.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Mission.Sequential_Segments.Sequential_Segments Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -106,16 +113,14 @@ SUAVE.Analyses.Mission.Mission.Mission - -
+ + - -

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Mission.Mission
def __defaults__ (self)
 
def finalize (self)
 
@@ -170,6 +175,8 @@

SUAVE.Analyses.Mission.Mission.Mission.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Variable__Range__Cruise_1_1Given__State__of__Charge_1_1Given__State__of__Charge-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Variable__Range__Cruise_1_1Given__State__of__Charge_1_1Given__State__of__Charge-members.html new file mode 100644 index 00000000..e78737c0 --- /dev/null +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Variable__Range__Cruise_1_1Given__State__of__Charge_1_1Given__State__of__Charge-members.html @@ -0,0 +1,124 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+

+ + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+ + + + + +
+ +
+
+
+ + + + + + diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Variable__Range__Cruise_1_1Given__State__of__Charge_1_1Given__State__of__Charge.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Variable__Range__Cruise_1_1Given__State__of__Charge_1_1Given__State__of__Charge.html new file mode 100644 index 00000000..ee072dbb --- /dev/null +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Variable__Range__Cruise_1_1Given__State__of__Charge_1_1Given__State__of__Charge.html @@ -0,0 +1,208 @@ + + + + + + + +SUAVE: SUAVE.Analyses.Mission.Variable_Range_Cruise.Given_State_of_Charge.Given_State_of_Charge Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Analyses.Mission.Variable_Range_Cruise.Given_State_of_Charge.Given_State_of_Charge Class Reference
+
+
+
+Inheritance diagram for SUAVE.Analyses.Mission.Variable_Range_Cruise.Given_State_of_Charge.Given_State_of_Charge:
+
+
+ + +SUAVE.Analyses.Mission.All_At_Once.All_At_Once +SUAVE.Analyses.Mission.Mission.Mission + +
+ + + + + + + +

+Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Mission.Mission
def finalize (self)
 
+ + + + + + + + + + + + + +

+Public Attributes

tag
 
cruise_tag
 
target_state_of_charge
 
- Public Attributes inherited from SUAVE.Analyses.Mission.All_At_Once.All_At_Once
tag
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Mission.Mission
tag
 
+

Detailed Description

+
Given a target landing state of charge, select the cruise distance by adding a residual to the mission
+
+    Assumptions:
+    None
+    
+    Source:
+    None
+

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Analyses.Mission.Variable_Range_Cruise.Given_State_of_Charge.Given_State_of_Charge.__defaults__ ( self)
+
+
This sets the default flow of methods for the mission.
+    
+    Assumptions:
+    None
+    
+    Source:
+    N/A
+    
+    Inputs:
+    None
+    
+    Outputs:
+    None
+    
+    Properties Used:
+    None
+
+

Reimplemented from SUAVE.Analyses.Mission.All_At_Once.All_At_Once.

+ +
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Analyses/Mission/Variable_Range_Cruise/Given_State_of_Charge.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Variable__Range__Cruise_1_1Given__State__of__Charge_1_1Given__State__of__Charge.js b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Variable__Range__Cruise_1_1Given__State__of__Charge_1_1Given__State__of__Charge.js new file mode 100644 index 00000000..ea8c66f8 --- /dev/null +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Variable__Range__Cruise_1_1Given__State__of__Charge_1_1Given__State__of__Charge.js @@ -0,0 +1,7 @@ +var classSUAVE_1_1Analyses_1_1Mission_1_1Variable__Range__Cruise_1_1Given__State__of__Charge_1_1Given__State__of__Charge = +[ + [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Variable__Range__Cruise_1_1Given__State__of__Charge_1_1Given__State__of__Charge.html#a3fae1bf1e0476aece365806fd5b39614", null ], + [ "cruise_tag", "classSUAVE_1_1Analyses_1_1Mission_1_1Variable__Range__Cruise_1_1Given__State__of__Charge_1_1Given__State__of__Charge.html#ae21182c08c54b93a50170ef4bf95f768", null ], + [ "tag", "classSUAVE_1_1Analyses_1_1Mission_1_1Variable__Range__Cruise_1_1Given__State__of__Charge_1_1Given__State__of__Charge.html#a5a80b993ad6a9fcecfb6b575a323d779", null ], + [ "target_state_of_charge", "classSUAVE_1_1Analyses_1_1Mission_1_1Variable__Range__Cruise_1_1Given__State__of__Charge_1_1Given__State__of__Charge.html#aab454dfb1ccbb647b0bd794c3b5fbf61", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Variable__Range__Cruise_1_1Given__State__of__Charge_1_1Given__State__of__Charge.png b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Variable__Range__Cruise_1_1Given__State__of__Charge_1_1Given__State__of__Charge.png new file mode 100644 index 00000000..fe4db552 Binary files /dev/null and b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Variable__Range__Cruise_1_1Given__State__of__Charge_1_1Given__State__of__Charge.png differ diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Variable__Range__Cruise_1_1Given__Weight_1_1Given__Weight-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Variable__Range__Cruise_1_1Given__Weight_1_1Given__Weight-members.html new file mode 100644 index 00000000..b0829304 --- /dev/null +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Variable__Range__Cruise_1_1Given__Weight_1_1Given__Weight-members.html @@ -0,0 +1,124 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ + + + + + diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Variable__Range__Cruise_1_1Given__Weight_1_1Given__Weight.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Variable__Range__Cruise_1_1Given__Weight_1_1Given__Weight.html new file mode 100644 index 00000000..64ef1c52 --- /dev/null +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Variable__Range__Cruise_1_1Given__Weight_1_1Given__Weight.html @@ -0,0 +1,208 @@ + + + + + + + +SUAVE: SUAVE.Analyses.Mission.Variable_Range_Cruise.Given_Weight.Given_Weight Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Analyses.Mission.Variable_Range_Cruise.Given_Weight.Given_Weight Class Reference
+
+
+
+Inheritance diagram for SUAVE.Analyses.Mission.Variable_Range_Cruise.Given_Weight.Given_Weight:
+
+
+ + +SUAVE.Analyses.Mission.All_At_Once.All_At_Once +SUAVE.Analyses.Mission.Mission.Mission + +
+ + + + + + + +

+Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Mission.Mission
def finalize (self)
 
+ + + + + + + + + + + + + +

+Public Attributes

tag
 
cruise_tag
 
target_landing_weight
 
- Public Attributes inherited from SUAVE.Analyses.Mission.All_At_Once.All_At_Once
tag
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Mission.Mission
tag
 
+

Detailed Description

+
Given a target landing weight, select the cruise distance by adding a residual to the mission
+
+    Assumptions:
+    None
+    
+    Source:
+    None
+

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Analyses.Mission.Variable_Range_Cruise.Given_Weight.Given_Weight.__defaults__ ( self)
+
+
This sets the default flow of methods for the mission.
+    
+    Assumptions:
+    None
+    
+    Source:
+    N/A
+    
+    Inputs:
+    None
+    
+    Outputs:
+    None
+    
+    Properties Used:
+    None
+
+

Reimplemented from SUAVE.Analyses.Mission.All_At_Once.All_At_Once.

+ +
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Analyses/Mission/Variable_Range_Cruise/Given_Weight.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Variable__Range__Cruise_1_1Given__Weight_1_1Given__Weight.js b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Variable__Range__Cruise_1_1Given__Weight_1_1Given__Weight.js new file mode 100644 index 00000000..8693f968 --- /dev/null +++ b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Variable__Range__Cruise_1_1Given__Weight_1_1Given__Weight.js @@ -0,0 +1,7 @@ +var classSUAVE_1_1Analyses_1_1Mission_1_1Variable__Range__Cruise_1_1Given__Weight_1_1Given__Weight = +[ + [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Variable__Range__Cruise_1_1Given__Weight_1_1Given__Weight.html#ac11e2f06212d7ca99f18ea439ea6ac6d", null ], + [ "cruise_tag", "classSUAVE_1_1Analyses_1_1Mission_1_1Variable__Range__Cruise_1_1Given__Weight_1_1Given__Weight.html#ad03931160cff349f00e331c7def686e1", null ], + [ "tag", "classSUAVE_1_1Analyses_1_1Mission_1_1Variable__Range__Cruise_1_1Given__Weight_1_1Given__Weight.html#aa085fe87c7711a73ee55bff814d0c172", null ], + [ "target_landing_weight", "classSUAVE_1_1Analyses_1_1Mission_1_1Variable__Range__Cruise_1_1Given__Weight_1_1Given__Weight.html#a6fffa88f32c7e650fe103ecd9792feae", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Variable__Range__Cruise_1_1Given__Weight_1_1Given__Weight.png b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Variable__Range__Cruise_1_1Given__Weight_1_1Given__Weight.png new file mode 100644 index 00000000..a5f72ec6 Binary files /dev/null and b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Variable__Range__Cruise_1_1Given__Weight_1_1Given__Weight.png differ diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Vary__Cruise_1_1Given__Weight_1_1Given__Weight-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Vary__Cruise_1_1Given__Weight_1_1Given__Weight-members.html deleted file mode 100644 index 230f6c49..00000000 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Vary__Cruise_1_1Given__Weight_1_1Given__Weight-members.html +++ /dev/null @@ -1,117 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.1.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
-
- - - -
-
- -
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-
- - - - - - diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Vary__Cruise_1_1Given__Weight_1_1Given__Weight.html b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Vary__Cruise_1_1Given__Weight_1_1Given__Weight.html deleted file mode 100644 index 87a41c3e..00000000 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Vary__Cruise_1_1Given__Weight_1_1Given__Weight.html +++ /dev/null @@ -1,204 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Mission.Vary_Cruise.Given_Weight.Given_Weight Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.1.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
-
- - - -
-
- -
-
-
- -
- -
-
- - -
- -
- -
- -
-
SUAVE.Analyses.Mission.Vary_Cruise.Given_Weight.Given_Weight Class Reference
-
-
-
-Inheritance diagram for SUAVE.Analyses.Mission.Vary_Cruise.Given_Weight.Given_Weight:
-
-
- - -SUAVE.Analyses.Mission.All_At_Once.All_At_Once -SUAVE.Analyses.Mission.Mission.Mission - -
- - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.All_At_Once.All_At_Once
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Mission.Mission.Mission
def __defaults__ (self)
 
def finalize (self)
 
- - - - - - - - - - - - - -

-Public Attributes

tag
 
cruise_tag
 
target_landing_weight
 
- Public Attributes inherited from SUAVE.Analyses.Mission.All_At_Once.All_At_Once
tag
 
- Public Attributes inherited from SUAVE.Analyses.Mission.Mission.Mission
tag
 
-

Detailed Description

-
Given a target landing weight, select the cruise distance by adding a residual to the mission
-
-    Assumptions:
-    None
-    
-    Source:
-    None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Mission.Vary_Cruise.Given_Weight.Given_Weight.__defaults__ ( self)
-
-
This sets the default flow of methods for the mission.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Analyses/Mission/Vary_Cruise/Given_Weight.py
  • -
-
-
- - - - diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Vary__Cruise_1_1Given__Weight_1_1Given__Weight.js b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Vary__Cruise_1_1Given__Weight_1_1Given__Weight.js deleted file mode 100644 index 79080260..00000000 --- a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Vary__Cruise_1_1Given__Weight_1_1Given__Weight.js +++ /dev/null @@ -1,7 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Mission_1_1Vary__Cruise_1_1Given__Weight_1_1Given__Weight = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Vary__Cruise_1_1Given__Weight_1_1Given__Weight.html#ac60d1f362c0cc1eaaf492e10d0b8ba6a", null ], - [ "cruise_tag", "classSUAVE_1_1Analyses_1_1Mission_1_1Vary__Cruise_1_1Given__Weight_1_1Given__Weight.html#a14ab04f5d7d961209255a699a70b6b62", null ], - [ "tag", "classSUAVE_1_1Analyses_1_1Mission_1_1Vary__Cruise_1_1Given__Weight_1_1Given__Weight.html#ac5f18745abd92ac299b698fb51d5ed30", null ], - [ "target_landing_weight", "classSUAVE_1_1Analyses_1_1Mission_1_1Vary__Cruise_1_1Given__Weight_1_1Given__Weight.html#a2ce21cf5b37d2b76f76c4984d2f5ead4", null ] -]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Vary__Cruise_1_1Given__Weight_1_1Given__Weight.png b/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Vary__Cruise_1_1Given__Weight_1_1Given__Weight.png deleted file mode 100644 index 4badeecc..00000000 Binary files a/doxygen/classSUAVE_1_1Analyses_1_1Mission_1_1Vary__Cruise_1_1Given__Weight_1_1Given__Weight.png and /dev/null differ diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Noise_1_1Fidelity__One_1_1Fidelity__One-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Noise_1_1Fidelity__One_1_1Fidelity__One-members.html index 59b67f87..2a06ad04 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Noise_1_1Fidelity__One_1_1Fidelity__One-members.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Noise_1_1Fidelity__One_1_1Fidelity__One-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -98,18 +105,19 @@

This is the complete list of members for SUAVE.Analyses.Noise.Fidelity_One.Fidelity_One, including all inherited members.

- + - + - - - - - - - - + + + + + + + + +
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Noise.Fidelity_One.Fidelity_One
compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
evaluate(self, state)SUAVE.Analyses.Noise.Noise.Noise
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self)SUAVE.Analyses.Noise.Noise.Noise
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
geometry (defined in SUAVE.Analyses.Noise.Noise.Noise)SUAVE.Analyses.Noise.Noise.Noise
initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
settings (defined in SUAVE.Analyses.Noise.Noise.Noise)SUAVE.Analyses.Noise.Noise.Noise
tag (defined in SUAVE.Analyses.Noise.Fidelity_One.Fidelity_One)SUAVE.Analyses.Noise.Fidelity_One.Fidelity_One
SUAVE::Analyses::Analysis::Analysis.evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
evaluate_noise(self, segment)SUAVE.Analyses.Noise.Fidelity_One.Fidelity_One
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self)SUAVE.Analyses.Noise.Noise.Noise
SUAVE::Analyses::Analysis::Analysis.finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
geometry (defined in SUAVE.Analyses.Noise.Noise.Noise)SUAVE.Analyses.Noise.Noise.Noise
initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
settings (defined in SUAVE.Analyses.Noise.Noise.Noise)SUAVE.Analyses.Noise.Noise.Noise
tag (defined in SUAVE.Analyses.Noise.Noise.Noise)SUAVE.Analyses.Noise.Noise.Noise
@@ -117,7 +125,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Noise_1_1Fidelity__One_1_1Fidelity__One.html b/doxygen/classSUAVE_1_1Analyses_1_1Noise_1_1Fidelity__One_1_1Fidelity__One.html index 03f5110e..901c26b2 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Noise_1_1Fidelity__One_1_1Fidelity__One.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Noise_1_1Fidelity__One_1_1Fidelity__One.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Noise.Fidelity_One.Fidelity_One Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -93,7 +100,6 @@
SUAVE.Analyses.Noise.Fidelity_One.Fidelity_One Class Reference
@@ -107,39 +113,34 @@ SUAVE.Analyses.Noise.Noise.Noise SUAVE.Analyses.Analysis.Analysis - -
+ + + + - - - - - - - - - - - - - - + + + + + + + + + +

Public Member Functions

def __defaults__ (self)
 
def evaluate_noise (self, segment)
 
- Public Member Functions inherited from SUAVE.Analyses.Noise.Noise.Noise
def __defaults__ (self)
 
def evaluate (self, state)
 
def finalize (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
- - - + @@ -190,7 +191,8 @@

This sets the default values for the analysis. Assumptions: -None +Ground microphone angles start in front of the aircraft (0 deg) and sweep in a lateral direction +to the starboard wing and around to the tail (180 deg) Source: N/A @@ -204,6 +206,53 @@

SUAVE.Analyses.Noise.Noise.Noise.

+ + + + +

◆ evaluate_noise()

+ +
+
+

-Public Attributes

tag
 

+Additional Inherited Members

- Public Attributes inherited from SUAVE.Analyses.Noise.Noise.Noise
 tag
+ + + + + + + + + + + + + + + + + +
def SUAVE.Analyses.Noise.Fidelity_One.Fidelity_One.evaluate_noise ( self,
 segment 
)
+
+
Process vehicle to setup geometry, condititon and configuration
+    
+Assumptions:
+None
+    
+Source:
+N/4
+    
+Inputs:
+self.settings.
+    center_frequencies  - 1/3 octave band frequencies   [unitless]
+    
+Outputs:
+None
+    
+Properties Used:
+self.geometry
+

The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Noise_1_1Fidelity__One_1_1Fidelity__One.js b/doxygen/classSUAVE_1_1Analyses_1_1Noise_1_1Fidelity__One_1_1Fidelity__One.js index e8c69fad..6c0c94de 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Noise_1_1Fidelity__One_1_1Fidelity__One.js +++ b/doxygen/classSUAVE_1_1Analyses_1_1Noise_1_1Fidelity__One_1_1Fidelity__One.js @@ -1,5 +1,5 @@ var classSUAVE_1_1Analyses_1_1Noise_1_1Fidelity__One_1_1Fidelity__One = [ [ "__defaults__", "classSUAVE_1_1Analyses_1_1Noise_1_1Fidelity__One_1_1Fidelity__One.html#a60572d766f474ddcd227997f1ebb450d", null ], - [ "tag", "classSUAVE_1_1Analyses_1_1Noise_1_1Fidelity__One_1_1Fidelity__One.html#a67874a2ed5da3cb341240e47337a65e3", null ] + [ "evaluate_noise", "classSUAVE_1_1Analyses_1_1Noise_1_1Fidelity__One_1_1Fidelity__One.html#ae95ae6e876825f7433962b4e3b6bde67", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Noise_1_1Fidelity__Zero_1_1Fidelity__Zero-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Noise_1_1Fidelity__Zero_1_1Fidelity__Zero-members.html new file mode 100644 index 00000000..0d93cf64 --- /dev/null +++ b/doxygen/classSUAVE_1_1Analyses_1_1Noise_1_1Fidelity__Zero_1_1Fidelity__Zero-members.html @@ -0,0 +1,135 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
SUAVE.Analyses.Noise.Fidelity_Zero.Fidelity_Zero Member List
+
+
+ +

This is the complete list of members for SUAVE.Analyses.Noise.Fidelity_Zero.Fidelity_Zero, including all inherited members.

+ + + + + + + + + + + + + + + + + +
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Noise.Fidelity_Zero.Fidelity_Zero
approach (defined in SUAVE.Analyses.Noise.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Noise.Fidelity_Zero.Fidelity_Zero
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
evaluate(self, state)SUAVE.Analyses.Noise.Noise.Noise
SUAVE::Analyses::Analysis::Analysis.evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
evaluate_noise(self, conditions)SUAVE.Analyses.Noise.Fidelity_Zero.Fidelity_Zero
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self)SUAVE.Analyses.Noise.Fidelity_Zero.Fidelity_Zero
SUAVE::Analyses::Analysis::Analysis.finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
flyover (defined in SUAVE.Analyses.Noise.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Noise.Fidelity_Zero.Fidelity_Zero
geometry (defined in SUAVE.Analyses.Noise.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Noise.Fidelity_Zero.Fidelity_Zero
initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
settings (defined in SUAVE.Analyses.Noise.Noise.Noise)SUAVE.Analyses.Noise.Noise.Noise
sideline (defined in SUAVE.Analyses.Noise.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Noise.Fidelity_Zero.Fidelity_Zero
tag (defined in SUAVE.Analyses.Noise.Noise.Noise)SUAVE.Analyses.Noise.Noise.Noise
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Noise_1_1Fidelity__Zero_1_1Fidelity__Zero.html b/doxygen/classSUAVE_1_1Analyses_1_1Noise_1_1Fidelity__Zero_1_1Fidelity__Zero.html new file mode 100644 index 00000000..becb9301 --- /dev/null +++ b/doxygen/classSUAVE_1_1Analyses_1_1Noise_1_1Fidelity__Zero_1_1Fidelity__Zero.html @@ -0,0 +1,320 @@ + + + + + + + +SUAVE: SUAVE.Analyses.Noise.Fidelity_Zero.Fidelity_Zero Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Analyses.Noise.Fidelity_Zero.Fidelity_Zero Class Reference
+
+
+
+Inheritance diagram for SUAVE.Analyses.Noise.Fidelity_Zero.Fidelity_Zero:
+
+
+ + +SUAVE.Analyses.Noise.Noise.Noise +SUAVE.Analyses.Analysis.Analysis + +
+ + + + + + + + + + + + + + + + + + + + + + +

+Public Member Functions

def __defaults__ (self)
 
def finalize (self)
 
def evaluate_noise (self, conditions)
 
- Public Member Functions inherited from SUAVE.Analyses.Noise.Noise.Noise
def evaluate (self, state)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
+ + + + + + + + + + + + + + + + + + + + + + + +

+Public Attributes

geometry
 
flyover
 
approach
 
sideline
 
- Public Attributes inherited from SUAVE.Analyses.Noise.Noise.Noise
tag
 
geometry
 
settings
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
+

Detailed Description

+
SUAVE.Analyses.Noise.Fidelity_Zero()
+
+    The Fidelity Zero Noise Analysis Class
+    
+        Assumptions:
+        None
+        
+        Source:
+        N/A
+

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Analyses.Noise.Fidelity_Zero.Fidelity_Zero.__defaults__ ( self)
+
+
This sets the default values for the analysis.
+
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+None
+
+Output:
+None
+
+Properties Used:
+N/A
+
+

Reimplemented from SUAVE.Analyses.Noise.Noise.Noise.

+ +
+
+ +

◆ evaluate_noise()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Analyses.Noise.Fidelity_Zero.Fidelity_Zero.evaluate_noise ( self,
 conditions 
)
+
+
Process vehicle to setup geometry, condititon and configuration
+    
+Assumptions:
+None
+    
+Source:
+N/4
+    
+Inputs:
+conditions - DataDict() of aerodynamic conditions
+results    - DataDict() of moment coeffients and stability and body axis derivatives
+    
+Outputs:
+None
+    
+Properties Used:
+self.geometry
+
+
+ +

◆ finalize()

+ +
+
+ + + + + + + + +
def SUAVE.Analyses.Noise.Fidelity_Zero.Fidelity_Zero.finalize ( self)
+
+
Finalizes the surrogate needed for lift calculation.
+    
+Assumptions:
+None
+    
+Source:
+N/A
+    
+Inputs:
+None
+    
+Outputs:
+None
+    
+Properties Used: 
+None
+
+

Reimplemented from SUAVE.Analyses.Noise.Noise.Noise.

+ +
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Analyses/Noise/Fidelity_Zero.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Noise_1_1Fidelity__Zero_1_1Fidelity__Zero.js b/doxygen/classSUAVE_1_1Analyses_1_1Noise_1_1Fidelity__Zero_1_1Fidelity__Zero.js new file mode 100644 index 00000000..132b298e --- /dev/null +++ b/doxygen/classSUAVE_1_1Analyses_1_1Noise_1_1Fidelity__Zero_1_1Fidelity__Zero.js @@ -0,0 +1,10 @@ +var classSUAVE_1_1Analyses_1_1Noise_1_1Fidelity__Zero_1_1Fidelity__Zero = +[ + [ "__defaults__", "classSUAVE_1_1Analyses_1_1Noise_1_1Fidelity__Zero_1_1Fidelity__Zero.html#a1b0a90516ded275d601f0a5eefa243cd", null ], + [ "evaluate_noise", "classSUAVE_1_1Analyses_1_1Noise_1_1Fidelity__Zero_1_1Fidelity__Zero.html#ae2c099a81fee24ac113e935054d338e9", null ], + [ "finalize", "classSUAVE_1_1Analyses_1_1Noise_1_1Fidelity__Zero_1_1Fidelity__Zero.html#af6276c3ec824f958ef4bcdebd63159a9", null ], + [ "approach", "classSUAVE_1_1Analyses_1_1Noise_1_1Fidelity__Zero_1_1Fidelity__Zero.html#aaca9e4e515716dca59ca5afe0e92cd9b", null ], + [ "flyover", "classSUAVE_1_1Analyses_1_1Noise_1_1Fidelity__Zero_1_1Fidelity__Zero.html#ac201d710ac96f14d10ff67faa07179ed", null ], + [ "geometry", "classSUAVE_1_1Analyses_1_1Noise_1_1Fidelity__Zero_1_1Fidelity__Zero.html#a34ebf3c5e12d238eb6953669b2f0344d", null ], + [ "sideline", "classSUAVE_1_1Analyses_1_1Noise_1_1Fidelity__Zero_1_1Fidelity__Zero.html#a83b0d3ff33ef841adf818d403cb24644", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Noise_1_1Fidelity__Zero_1_1Fidelity__Zero.png b/doxygen/classSUAVE_1_1Analyses_1_1Noise_1_1Fidelity__Zero_1_1Fidelity__Zero.png new file mode 100644 index 00000000..22c3aeb2 Binary files /dev/null and b/doxygen/classSUAVE_1_1Analyses_1_1Noise_1_1Fidelity__Zero_1_1Fidelity__Zero.png differ diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Noise_1_1Noise_1_1Noise-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Noise_1_1Noise_1_1Noise-members.html index 9bc25127..17ae0d66 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Noise_1_1Noise_1_1Noise-members.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Noise_1_1Noise_1_1Noise-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -117,7 +124,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Noise_1_1Noise_1_1Noise.html b/doxygen/classSUAVE_1_1Analyses_1_1Noise_1_1Noise_1_1Noise.html index b25adc12..5c11f963 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Noise_1_1Noise_1_1Noise.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Noise_1_1Noise_1_1Noise.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Noise.Noise.Noise Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -105,10 +112,11 @@
-SUAVE.Analyses.Analysis.Analysis -SUAVE.Analyses.Noise.Fidelity_One.Fidelity_One - -
+SUAVE.Analyses.Analysis.Analysis +SUAVE.Analyses.Noise.Fidelity_One.Fidelity_One +SUAVE.Analyses.Noise.Fidelity_Zero.Fidelity_Zero + + @@ -119,18 +127,16 @@ - - - - - - - - - - - - + + + + + + + + + +

Public Member Functions

def finalize (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
@@ -196,6 +202,10 @@

SUAVE.Analyses.Analysis.Analysis.

+ +

Reimplemented in SUAVE.Analyses.Noise.Fidelity_One.Fidelity_One, and SUAVE.Analyses.Noise.Fidelity_Zero.Fidelity_Zero.

+ @@ -274,6 +284,8 @@

SUAVE.Analyses.Noise.Fidelity_Zero.Fidelity_Zero.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Noise_1_1Noise_1_1Noise.png b/doxygen/classSUAVE_1_1Analyses_1_1Noise_1_1Noise_1_1Noise.png index 8a514c38..f38c9732 100644 Binary files a/doxygen/classSUAVE_1_1Analyses_1_1Noise_1_1Noise_1_1Noise.png and b/doxygen/classSUAVE_1_1Analyses_1_1Noise_1_1Noise_1_1Noise.png differ diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Planets_1_1Planet_1_1Planet-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Planets_1_1Planet_1_1Planet-members.html index 0cea2bf7..cc482711 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Planets_1_1Planet_1_1Planet-members.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Planets_1_1Planet_1_1Planet-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Attributes

SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -114,7 +121,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Planets_1_1Planet_1_1Planet.html b/doxygen/classSUAVE_1_1Analyses_1_1Planets_1_1Planet_1_1Planet.html index f9df8920..999beb87 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Planets_1_1Planet_1_1Planet.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Planets_1_1Planet_1_1Planet.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Planets.Planet.Planet Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -106,26 +113,24 @@ SUAVE.Analyses.Analysis.Analysis - -
+ + - - - - - - - - - - - - + + + + + + + + + +

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
@@ -183,6 +188,8 @@

SUAVE.Analyses.Analysis.Analysis.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Process_1_1Process-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Process_1_1Process-members.html index 62b683e9..7779a054 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Process_1_1Process-members.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Process_1_1Process-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Attributes

SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -98,8 +105,8 @@

This is the complete list of members for SUAVE.Analyses.Process.Process, including all inherited members.

- - + +
__call__(self, args, kwarg)SUAVE.Analyses.Process.Process
evaluate(self, args, kwarg)SUAVE.Analyses.Process.Process
__call__(self, *args, **kwarg)SUAVE.Analyses.Process.Process
evaluate(self, *args, **kwarg)SUAVE.Analyses.Process.Process
verbose (defined in SUAVE.Analyses.Process.Process)SUAVE.Analyses.Process.Processstatic
@@ -108,7 +115,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Process_1_1Process.html b/doxygen/classSUAVE_1_1Analyses_1_1Process_1_1Process.html index d127b481..8e4f0c2d 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Process_1_1Process.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Process_1_1Process.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Process.Process Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -106,15 +113,15 @@ SUAVE.Analyses.Aerodynamics.Process_Geometry.Process_Geometry - -
+ + - - - - + + + +

Public Member Functions

def evaluate (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def evaluate (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
@@ -133,8 +140,8 @@ Source: N/A

Member Function Documentation

- -

◆ __call__()

+ +

◆ __call__()

@@ -148,13 +155,13 @@

- + - + @@ -182,8 +189,8 @@

-

◆ evaluate()

+ +

◆ evaluate()

@@ -197,13 +204,13 @@

- + - + @@ -243,7 +250,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Process_1_1Process.js b/doxygen/classSUAVE_1_1Analyses_1_1Process_1_1Process.js index e4c124f7..ac85ec12 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Process_1_1Process.js +++ b/doxygen/classSUAVE_1_1Analyses_1_1Process_1_1Process.js @@ -1,5 +1,5 @@ var classSUAVE_1_1Analyses_1_1Process_1_1Process = [ - [ "__call__", "classSUAVE_1_1Analyses_1_1Process_1_1Process.html#af4161c87be7d7b6c2ace43ca2ecad54e", null ], - [ "evaluate", "classSUAVE_1_1Analyses_1_1Process_1_1Process.html#a85d9cc1c2a36047100d9ce8abee28bda", null ] + [ "__call__", "classSUAVE_1_1Analyses_1_1Process_1_1Process.html#a52be80007c80252af1aca26453f65b10", null ], + [ "evaluate", "classSUAVE_1_1Analyses_1_1Process_1_1Process.html#adc5a542daa2ea034c52865c7d8b05aff", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__One_1_1Rotor__Wake__Fidelity__One-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__One_1_1Rotor__Wake__Fidelity__One-members.html new file mode 100644 index 00000000..8a7cfc07 --- /dev/null +++ b/doxygen/classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__One_1_1Rotor__Wake__Fidelity__One-members.html @@ -0,0 +1,146 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+

Static Public Attributes

  args,
 **  kwarg 
  args,
 **  kwarg 
+ + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+ + + + + +
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_One.Rotor_Wake_Fidelity_One Member List
+
+
+ +

This is the complete list of members for SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_One.Rotor_Wake_Fidelity_One, including all inherited members.

+ + + + + + + + + + + + + + + + + + + + + + + + + + + + +
__defaults__(self)SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_One.Rotor_Wake_Fidelity_One
axial_velocity_convergence_tolerance (defined in SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_One.Rotor_Wake_Fidelity_One)SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_One.Rotor_Wake_Fidelity_One
evaluate(self, rotor, wake_inputs, conditions)SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_One.Rotor_Wake_Fidelity_One
evaluate_slipstream(self, rotor, geometry, ctrl_pts, wing_instance=None)SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_One.Rotor_Wake_Fidelity_One
evaluate_wake_velocities(self, rotor, VD, num_ctrl_pts)SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_One.Rotor_Wake_Fidelity_One
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
initialize(self, rotor, conditions)SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_One.Rotor_Wake_Fidelity_One
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
maximum_convergence_iteration (defined in SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_One.Rotor_Wake_Fidelity_One)SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_One.Rotor_Wake_Fidelity_One
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
semi_prescribed_converge (defined in SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_One.Rotor_Wake_Fidelity_One)SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_One.Rotor_Wake_Fidelity_One
shift_wake_VD(self, wVD, offset)SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_One.Rotor_Wake_Fidelity_One
slipstream (defined in SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_One.Rotor_Wake_Fidelity_One)SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_One.Rotor_Wake_Fidelity_One
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_One.Rotor_Wake_Fidelity_One)SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_One.Rotor_Wake_Fidelity_One
verbose (defined in SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_One.Rotor_Wake_Fidelity_One)SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_One.Rotor_Wake_Fidelity_One
vortex_distribution (defined in SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_One.Rotor_Wake_Fidelity_One)SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_One.Rotor_Wake_Fidelity_One
vtk_save_flag (defined in SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_One.Rotor_Wake_Fidelity_One)SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_One.Rotor_Wake_Fidelity_One
vtk_save_loc (defined in SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_One.Rotor_Wake_Fidelity_One)SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_One.Rotor_Wake_Fidelity_One
wake_method (defined in SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_One.Rotor_Wake_Fidelity_One)SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_One.Rotor_Wake_Fidelity_One
wake_method_fidelity (defined in SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_One.Rotor_Wake_Fidelity_One)SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_One.Rotor_Wake_Fidelity_One
wake_settings (defined in SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_One.Rotor_Wake_Fidelity_One)SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_One.Rotor_Wake_Fidelity_One
wake_vortex_distribution (defined in SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_One.Rotor_Wake_Fidelity_One)SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_One.Rotor_Wake_Fidelity_One
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__One_1_1Rotor__Wake__Fidelity__One.html b/doxygen/classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__One_1_1Rotor__Wake__Fidelity__One.html new file mode 100644 index 00000000..96deaa40 --- /dev/null +++ b/doxygen/classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__One_1_1Rotor__Wake__Fidelity__One.html @@ -0,0 +1,571 @@ + + + + + + + +SUAVE: SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_One.Rotor_Wake_Fidelity_One Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_One.Rotor_Wake_Fidelity_One Class Reference
+
+
+
+Inheritance diagram for SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_One.Rotor_Wake_Fidelity_One:
+
+
+ + +SUAVE.Components.Energy.Energy_Component.Energy_Component +SUAVE.Components.Physical_Component.Physical_Component +SUAVE.Components.Component.Component + +
+ + + + + + + + + + + + + + +

+Public Member Functions

def __defaults__ (self)
 
def initialize (self, rotor, conditions)
 
def evaluate (self, rotor, wake_inputs, conditions)
 
def evaluate_slipstream (self, rotor, geometry, ctrl_pts, wing_instance=None)
 
def evaluate_wake_velocities (self, rotor, VD, num_ctrl_pts)
 
def shift_wake_VD (self, wVD, offset)
 
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Attributes

tag
 
wake_method
 
wake_vortex_distribution
 
wake_method_fidelity
 
semi_prescribed_converge
 
vtk_save_flag
 
vtk_save_loc
 
wake_settings
 
maximum_convergence_iteration
 
axial_velocity_convergence_tolerance
 
slipstream
 
verbose
 
vortex_distribution
 
- Public Attributes inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
inputs
 
outputs
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 
+

Detailed Description

+
SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_One()
+
+The Fidelity One Rotor Wake Class
+Uses a semi-prescribed vortex wake (PVW) model of the rotor wake
+
+Assumptions:
+None
+
+Source:
+None
+

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_One.Rotor_Wake_Fidelity_One.__defaults__ ( self)
+
+
This sets the default values for the component to function.
+
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+None
+
+Outputs:
+None
+
+Properties Used:
+None
+
+

Reimplemented from SUAVE.Components.Energy.Energy_Component.Energy_Component.

+ +
+
+ +

◆ evaluate()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_One.Rotor_Wake_Fidelity_One.evaluate ( self,
 rotor,
 wake_inputs,
 conditions 
)
+
+
Wake evaluation is performed using a semi-prescribed vortex wake (PVW) method for Fidelity One.
+
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+   self         - rotor wake
+   rotor        - SUAVE rotor
+   wake_inputs.
+      Ua        - Axial velocity
+      Ut        - Tangential velocity
+      r         - radius distribution
+   conditions   - conditions
+   
+   
+Outputs:
+   va  - axially-induced velocity from rotor wake
+   vt  - tangentially-induced velocity from rotor wake
+
+Properties Used:
+None
+
+
+
+ +

◆ evaluate_slipstream()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_One.Rotor_Wake_Fidelity_One.evaluate_slipstream ( self,
 rotor,
 geometry,
 ctrl_pts,
 wing_instance = None 
)
+
+
Evaluates the velocities induced by the rotor on a specified wing of the vehicle.
+If no wing instance is specified, uses main wing or last available wing in geometry.
+
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+   self         - rotor wake
+   rotor        - rotor
+   geometry     - vehicle geometry
+   
+Outputs:
+   wake_V_ind   - induced velocity from rotor wake at (VD.XC, VD.YC, VD.ZC)
+
+Properties Used:
+None
+
+
+
+ +

◆ evaluate_wake_velocities()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_One.Rotor_Wake_Fidelity_One.evaluate_wake_velocities ( self,
 rotor,
 VD,
 num_ctrl_pts 
)
+
+
Links the rotor wake to compute the wake-induced velocities at the vortex distribution
+control points.
+
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+   self         - rotor wake
+   rotor        - rotor
+   VD           - vortex distribution
+   num_ctrl_pts - number of analysis control points
+   
+Outputs:
+   prop_V_wake_ind  - induced velocity from rotor wake at (VD.XC, VD.YC, VD.ZC)
+
+Properties Used:
+None
+
+
+
+ +

◆ initialize()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_One.Rotor_Wake_Fidelity_One.initialize ( self,
 rotor,
 conditions 
)
+
+
Initializes the rotor by evaluating the BET once. This is required for generating the 
+circulation strengths for the vortex distribution in the prescribed vortex wake, and the 
+initial wake shape, which relies on the axial inflow induced by the wake at the rotor disc.
+
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+   self         - rotor wake
+   rotor        - SUAVE rotor
+   conditions   - conditions
+   
+   
+Outputs:
+None
+
+Properties Used:
+None
+
+
+ +

◆ shift_wake_VD()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_One.Rotor_Wake_Fidelity_One.shift_wake_VD ( self,
 wVD,
 offset 
)
+
+
This shifts the wake by the (x,y,z) coordinates of the offset. 
+This is useful for rotors with identical wakes that can be reused and shifted without regeneration.
+
+Assumptions
+None
+
+Source:
+N/A
+
+Inputs:
+wVD    - wake vortex distribution
+offset - (x,y,z) offset distances
+
+Outputs
+None
+
+Properties Used
+None
+
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Analyses/Propulsion/Rotor_Wake_Fidelity_One.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__One_1_1Rotor__Wake__Fidelity__One.js b/doxygen/classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__One_1_1Rotor__Wake__Fidelity__One.js new file mode 100644 index 00000000..b22a7d32 --- /dev/null +++ b/doxygen/classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__One_1_1Rotor__Wake__Fidelity__One.js @@ -0,0 +1,22 @@ +var classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__One_1_1Rotor__Wake__Fidelity__One = +[ + [ "__defaults__", "classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__One_1_1Rotor__Wake__Fidelity__One.html#a9f54fadb95e9f51087030b970b1124ec", null ], + [ "evaluate", "classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__One_1_1Rotor__Wake__Fidelity__One.html#aa4fdeeec634d4073e9c7058578f456dc", null ], + [ "evaluate_slipstream", "classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__One_1_1Rotor__Wake__Fidelity__One.html#a2d342edbaeded9cd28f6f025fa699944", null ], + [ "evaluate_wake_velocities", "classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__One_1_1Rotor__Wake__Fidelity__One.html#a301648eff0d7c712b3536515578f765f", null ], + [ "initialize", "classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__One_1_1Rotor__Wake__Fidelity__One.html#a8976c68a4ac86aa98b141ce52d542232", null ], + [ "shift_wake_VD", "classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__One_1_1Rotor__Wake__Fidelity__One.html#a4e7b9bbcd7d32ce67a4119105a28c5e4", null ], + [ "axial_velocity_convergence_tolerance", "classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__One_1_1Rotor__Wake__Fidelity__One.html#ad8127263a0b57e877f25ce164e714275", null ], + [ "maximum_convergence_iteration", "classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__One_1_1Rotor__Wake__Fidelity__One.html#a9fc272817c076f3ab33e8e7fca6808a6", null ], + [ "semi_prescribed_converge", "classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__One_1_1Rotor__Wake__Fidelity__One.html#acc3b89a779aff4e34637e53336d96016", null ], + [ "slipstream", "classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__One_1_1Rotor__Wake__Fidelity__One.html#a5a0e6ede820af50fb4c013dc80b200ed", null ], + [ "tag", "classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__One_1_1Rotor__Wake__Fidelity__One.html#ab2d3bfcac72f3acdf3c238265924555a", null ], + [ "verbose", "classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__One_1_1Rotor__Wake__Fidelity__One.html#ad772fee2a2e58f0ce37c16b00fd04286", null ], + [ "vortex_distribution", "classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__One_1_1Rotor__Wake__Fidelity__One.html#afaf5664d463f34680a6a1b993311d12f", null ], + [ "vtk_save_flag", "classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__One_1_1Rotor__Wake__Fidelity__One.html#a2b1f84fb6d5c2e470019c53c5b2e7563", null ], + [ "vtk_save_loc", "classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__One_1_1Rotor__Wake__Fidelity__One.html#afaba73ee9328d49e9e44b2c9caef2d16", null ], + [ "wake_method", "classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__One_1_1Rotor__Wake__Fidelity__One.html#a937023d49501c0ea9a5d3b7f1d27217e", null ], + [ "wake_method_fidelity", "classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__One_1_1Rotor__Wake__Fidelity__One.html#a9041023345e09877061f4bef8e2ebea5", null ], + [ "wake_settings", "classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__One_1_1Rotor__Wake__Fidelity__One.html#aded43b30ab095684f25574c51989e789", null ], + [ "wake_vortex_distribution", "classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__One_1_1Rotor__Wake__Fidelity__One.html#a6aa1b342eafca053e50def1d02bf0248", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__One_1_1Rotor__Wake__Fidelity__One.png b/doxygen/classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__One_1_1Rotor__Wake__Fidelity__One.png new file mode 100644 index 00000000..7e229b8e Binary files /dev/null and b/doxygen/classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__One_1_1Rotor__Wake__Fidelity__One.png differ diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__Two_1_1Rotor__Wake__Fidelity__Two-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__Two_1_1Rotor__Wake__Fidelity__Two-members.html new file mode 100644 index 00000000..b918539c --- /dev/null +++ b/doxygen/classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__Two_1_1Rotor__Wake__Fidelity__Two-members.html @@ -0,0 +1,132 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_Two.Rotor_Wake_Fidelity_Two Member List
+
+
+ +

This is the complete list of members for SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_Two.Rotor_Wake_Fidelity_Two, including all inherited members.

+ + + + + + + + + + + + + + +
__defaults__(self)SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_Two.Rotor_Wake_Fidelity_Two
evaluate(self, rotor, U, Ua, Ut, PSI, omega, beta, c, r, R, B, a, nu, a_loc, a_geo, cl_sur, cd_sur, ctrl_pts, Nr, Na, tc, use_2d_analysis, conditions)SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_Two.Rotor_Wake_Fidelity_Two
external_inflow (defined in SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_Two.Rotor_Wake_Fidelity_Two)SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_Two.Rotor_Wake_Fidelity_Two
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_Two.Rotor_Wake_Fidelity_Two)SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_Two.Rotor_Wake_Fidelity_Two
wake_method (defined in SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_Two.Rotor_Wake_Fidelity_Two)SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_Two.Rotor_Wake_Fidelity_Two
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__Two_1_1Rotor__Wake__Fidelity__Two.html b/doxygen/classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__Two_1_1Rotor__Wake__Fidelity__Two.html new file mode 100644 index 00000000..170ad664 --- /dev/null +++ b/doxygen/classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__Two_1_1Rotor__Wake__Fidelity__Two.html @@ -0,0 +1,410 @@ + + + + + + + +SUAVE: SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_Two.Rotor_Wake_Fidelity_Two Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_Two.Rotor_Wake_Fidelity_Two Class Reference
+
+
+
+Inheritance diagram for SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_Two.Rotor_Wake_Fidelity_Two:
+
+
+ + +SUAVE.Components.Energy.Energy_Component.Energy_Component +SUAVE.Components.Physical_Component.Physical_Component +SUAVE.Components.Component.Component + +
+ + + + + + +

+Public Member Functions

def __defaults__ (self)
 
def evaluate (self, rotor, U, Ua, Ut, PSI, omega, beta, c, r, R, B, a, nu, a_loc, a_geo, cl_sur, cd_sur, ctrl_pts, Nr, Na, tc, use_2d_analysis, conditions)
 
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Attributes

tag
 
wake_method
 
external_inflow
 
- Public Attributes inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
inputs
 
outputs
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 
+

Detailed Description

+
This is a general rotor wake component. 
+
+Assumptions:
+None
+
+Source:
+None
+

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_Two.Rotor_Wake_Fidelity_Two.__defaults__ ( self)
+
+
This sets the default values for the component to function.
+
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+None
+
+Outputs:
+None
+
+Properties Used:
+None
+
+

Reimplemented from SUAVE.Components.Energy.Energy_Component.Energy_Component.

+ +
+
+ +

◆ evaluate()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_Two.Rotor_Wake_Fidelity_Two.evaluate ( self,
 rotor,
 U,
 Ua,
 Ut,
 PSI,
 omega,
 beta,
 c,
 r,
 R,
 B,
 a,
 nu,
 a_loc,
 a_geo,
 cl_sur,
 cd_sur,
 ctrl_pts,
 Nr,
 Na,
 tc,
 use_2d_analysis,
 conditions 
)
+
+
Wake evaluation is performed using an externally-applied inflow field at the rotor.
+This requires an external solver to generate the inflow to the rotor, which must have been appended to the 
+rotor wake as wake.external_flow.va and wake.external_flow.vt. This is then used within the BET.
+   
+   
+Assumptions:
+   Assumes external inflow is provided with shape (Nr_external,Na_external), where Nr_external is the number
+   of radial stations at which the inflow is provided and Na_external is the number of azimuthal stations.
+   
+   Assumes external radial stations matches the rotor radial stations
+   Assumes azimuth stations are evenly spaced 
+   
+Outputs of this function include the inflow velocities induced by rotor wake:
+   va  - axially-induced velocity from rotor wake
+   vt  - tangentially-induced velocity from rotor wake
+
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Analyses/Propulsion/Rotor_Wake_Fidelity_Two.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__Two_1_1Rotor__Wake__Fidelity__Two.js b/doxygen/classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__Two_1_1Rotor__Wake__Fidelity__Two.js new file mode 100644 index 00000000..5261bdee --- /dev/null +++ b/doxygen/classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__Two_1_1Rotor__Wake__Fidelity__Two.js @@ -0,0 +1,8 @@ +var classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__Two_1_1Rotor__Wake__Fidelity__Two = +[ + [ "__defaults__", "classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__Two_1_1Rotor__Wake__Fidelity__Two.html#acd1b1bbfe7958e1c296b8e1caed90485", null ], + [ "evaluate", "classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__Two_1_1Rotor__Wake__Fidelity__Two.html#a5610d98bdf9f2865a93538b414196468", null ], + [ "external_inflow", "classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__Two_1_1Rotor__Wake__Fidelity__Two.html#a14929869dcc895801e83ca141995e39a", null ], + [ "tag", "classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__Two_1_1Rotor__Wake__Fidelity__Two.html#aa9adfcce75fc1537705b30bac597cba3", null ], + [ "wake_method", "classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__Two_1_1Rotor__Wake__Fidelity__Two.html#ad7389f1c3ee2132490ee97f1d46348a2", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__Two_1_1Rotor__Wake__Fidelity__Two.png b/doxygen/classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__Two_1_1Rotor__Wake__Fidelity__Two.png new file mode 100644 index 00000000..a9b78556 Binary files /dev/null and b/doxygen/classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__Two_1_1Rotor__Wake__Fidelity__Two.png differ diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__Zero_1_1Rotor__Wake__Fidelity__Zero-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__Zero_1_1Rotor__Wake__Fidelity__Zero-members.html new file mode 100644 index 00000000..0f51e6a7 --- /dev/null +++ b/doxygen/classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__Zero_1_1Rotor__Wake__Fidelity__Zero-members.html @@ -0,0 +1,133 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_Zero.Rotor_Wake_Fidelity_Zero Member List
+
+
+ +

This is the complete list of members for SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_Zero.Rotor_Wake_Fidelity_Zero, including all inherited members.

+ + + + + + + + + + + + + + + +
__defaults__(self)SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_Zero.Rotor_Wake_Fidelity_Zero
evaluate(self, rotor, wake_inputs, conditions)SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_Zero.Rotor_Wake_Fidelity_Zero
evaluate_slipstream(self, rotor, geometry, ctrl_pts, wing_instance=None)SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_Zero.Rotor_Wake_Fidelity_Zero
evaluate_wake_velocities(self, rotor, evaluation_points, ctrl_pts)SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_Zero.Rotor_Wake_Fidelity_Zero
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_Zero.Rotor_Wake_Fidelity_Zero)SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_Zero.Rotor_Wake_Fidelity_Zero
wake_method (defined in SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_Zero.Rotor_Wake_Fidelity_Zero)SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_Zero.Rotor_Wake_Fidelity_Zero
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__Zero_1_1Rotor__Wake__Fidelity__Zero.html b/doxygen/classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__Zero_1_1Rotor__Wake__Fidelity__Zero.html new file mode 100644 index 00000000..7e7b4125 --- /dev/null +++ b/doxygen/classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__Zero_1_1Rotor__Wake__Fidelity__Zero.html @@ -0,0 +1,426 @@ + + + + + + + +SUAVE: SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_Zero.Rotor_Wake_Fidelity_Zero Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_Zero.Rotor_Wake_Fidelity_Zero Class Reference
+
+
+
+Inheritance diagram for SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_Zero.Rotor_Wake_Fidelity_Zero:
+
+
+ + +SUAVE.Components.Energy.Energy_Component.Energy_Component +SUAVE.Components.Physical_Component.Physical_Component +SUAVE.Components.Component.Component + +
+ + + + + + + + + + +

+Public Member Functions

def __defaults__ (self)
 
def evaluate (self, rotor, wake_inputs, conditions)
 
def evaluate_slipstream (self, rotor, geometry, ctrl_pts, wing_instance=None)
 
def evaluate_wake_velocities (self, rotor, evaluation_points, ctrl_pts)
 
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Attributes

tag
 
wake_method
 
- Public Attributes inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
inputs
 
outputs
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 
+

Detailed Description

+
This is a general rotor wake component. 
+
+Assumptions:
+None
+
+Source:
+None
+

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_Zero.Rotor_Wake_Fidelity_Zero.__defaults__ ( self)
+
+
This sets the default values for the component to function.
+
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+None
+
+Outputs:
+None
+
+Properties Used:
+None
+
+

Reimplemented from SUAVE.Components.Energy.Energy_Component.Energy_Component.

+ +
+
+ +

◆ evaluate()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_Zero.Rotor_Wake_Fidelity_Zero.evaluate ( self,
 rotor,
 wake_inputs,
 conditions 
)
+
+
Wake evaluation is performed using a simplified vortex wake method for Fidelity Zero, 
+following Helmholtz vortex theory.
+
+Assumptions:
+None
+
+Source:
+Drela, M. "Qprop Formulation", MIT AeroAstro, June 2006
+http://web.mit.edu/drela/Public/web/qprop/qprop_theory.pdf
+
+Inputs:
+   self         - rotor wake
+   rotor        - SUAVE rotor
+   wake_inputs.
+      Ua        - Axial velocity
+      Ut        - Tangential velocity
+      r         - radius distribution
+   conditions   - conditions
+   
+   
+Outputs:
+   va  - axially-induced velocity from rotor wake
+   vt  - tangentially-induced velocity from rotor wake
+
+Properties Used:
+None
+
+
+ +

◆ evaluate_slipstream()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_Zero.Rotor_Wake_Fidelity_Zero.evaluate_slipstream ( self,
 rotor,
 geometry,
 ctrl_pts,
 wing_instance = None 
)
+
+
Evaluates the velocities induced by the rotor on a specified wing of the vehicle.
+If no wing instance is specified, uses main wing or last available wing in geometry.
+
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+   self         - rotor wake
+   rotor        - rotor
+   geometry     - vehicle geometry
+   
+Outputs:
+   wake_V_ind   - induced velocity from rotor wake at (VD.XC, VD.YC, VD.ZC)
+
+Properties Used:
+None
+
+
+
+ +

◆ evaluate_wake_velocities()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_Zero.Rotor_Wake_Fidelity_Zero.evaluate_wake_velocities ( self,
 rotor,
 evaluation_points,
 ctrl_pts 
)
+
+
Links the rotor wake to compute the wake-induced velocities at the specified
+evaluation points.
+
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+   self               - rotor wake
+   rotor              - rotor
+   evaluation_points  - points at which to evaluate the rotor wake-induced velocities 
+   
+Outputs:
+   prop_V_wake_ind  - induced velocity from rotor wake at (VD.XC, VD.YC, VD.ZC)
+
+Properties Used:
+None
+
+
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Analyses/Propulsion/Rotor_Wake_Fidelity_Zero.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__Zero_1_1Rotor__Wake__Fidelity__Zero.js b/doxygen/classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__Zero_1_1Rotor__Wake__Fidelity__Zero.js new file mode 100644 index 00000000..e4510c63 --- /dev/null +++ b/doxygen/classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__Zero_1_1Rotor__Wake__Fidelity__Zero.js @@ -0,0 +1,9 @@ +var classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__Zero_1_1Rotor__Wake__Fidelity__Zero = +[ + [ "__defaults__", "classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__Zero_1_1Rotor__Wake__Fidelity__Zero.html#a7c605a3a16053975a2f18600b95b60eb", null ], + [ "evaluate", "classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__Zero_1_1Rotor__Wake__Fidelity__Zero.html#a573933e135afd72d9fcbd98e7047fbb9", null ], + [ "evaluate_slipstream", "classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__Zero_1_1Rotor__Wake__Fidelity__Zero.html#af2dd817c0cdd57a07396a589d61d6cc3", null ], + [ "evaluate_wake_velocities", "classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__Zero_1_1Rotor__Wake__Fidelity__Zero.html#a22245c24ec50b24daf05a7550e1f1e4c", null ], + [ "tag", "classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__Zero_1_1Rotor__Wake__Fidelity__Zero.html#a9831a472900baad7c64b758787d644f9", null ], + [ "wake_method", "classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__Zero_1_1Rotor__Wake__Fidelity__Zero.html#a65991a8da01ff66921e807c4d96c0dbc", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__Zero_1_1Rotor__Wake__Fidelity__Zero.png b/doxygen/classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__Zero_1_1Rotor__Wake__Fidelity__Zero.png new file mode 100644 index 00000000..537273bf Binary files /dev/null and b/doxygen/classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__Zero_1_1Rotor__Wake__Fidelity__Zero.png differ diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Settings_1_1Settings-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Settings_1_1Settings-members.html index f07914e7..6e475625 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Settings_1_1Settings-members.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Settings_1_1Settings-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -108,7 +115,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Settings_1_1Settings.html b/doxygen/classSUAVE_1_1Analyses_1_1Settings_1_1Settings.html index e5dbbffb..6e526587 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Settings_1_1Settings.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Settings_1_1Settings.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Settings.Settings Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -103,9 +110,7 @@ Inheritance diagram for SUAVE.Analyses.Settings.Settings:
- - - +
@@ -57,9 +60,11 @@

@@ -177,7 +182,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Sizing_1_1Sizing_1_1Sizing-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Sizing_1_1Sizing_1_1Sizing-members.html index 67aef28f..531c0d3d 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Sizing_1_1Sizing_1_1Sizing-members.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Sizing_1_1Sizing_1_1Sizing-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -115,7 +122,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Sizing_1_1Sizing_1_1Sizing.html b/doxygen/classSUAVE_1_1Analyses_1_1Sizing_1_1Sizing_1_1Sizing.html index e859883b..ac8fd67d 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Sizing_1_1Sizing_1_1Sizing.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Sizing_1_1Sizing_1_1Sizing.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Sizing.Sizing.Sizing Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -106,8 +113,8 @@ SUAVE.Analyses.Analysis.Analysis - -
+ + @@ -116,18 +123,16 @@ - - - - - - - - - - - - + + + + + + + + + +

Public Member Functions

def evaluate (self, conditions)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
@@ -186,6 +191,8 @@

SUAVE.Analyses.Analysis.Analysis.

+ @@ -243,7 +250,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1AVL_1_1AVL-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1AVL_1_1AVL-members.html index 9a3c29f2..416ce5c4 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1AVL_1_1AVL-members.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1AVL_1_1AVL-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Attributes

SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -99,29 +106,26 @@

This is the complete list of members for SUAVE.Analyses.Stability.AVL.AVL, including all inherited members.

- + - + - - + + - + - - - + - - - - - + + + +
__call__(self, conditions)SUAVE.Analyses.Stability.AVL.AVL
SUAVE::Analyses::Stability::Stability::Stability.__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
SUAVE::Analyses::Stability::Stability::Stability.__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Stability.AVL.AVL
build_surrogate(self)SUAVE.Analyses.Stability.AVL.AVL
compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
configuration (defined in SUAVE.Analyses.Stability.AVL.AVL)SUAVE.Analyses.Stability.AVL.AVL
current_status (defined in SUAVE.Analyses.Stability.AVL.AVL)SUAVE.Analyses.Stability.AVL.AVL
evaluate(self, conditions)SUAVE.Analyses.Stability.Stability.Stability
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
evaluate_conditions(self, run_conditions)SUAVE.Analyses.Stability.AVL.AVL
SUAVE::Analyses::Analysis::Analysis.evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
evaluate_conditions(self, run_conditions, trim_aircraft)SUAVE.Analyses.Stability.AVL.AVL
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self)SUAVE.Analyses.Stability.AVL.AVL
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
SUAVE::Analyses::Analysis::Analysis.finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
geometry (defined in SUAVE.Analyses.Stability.AVL.AVL)SUAVE.Analyses.Stability.AVL.AVL
initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
keep_files (defined in SUAVE.Analyses.Stability.AVL.AVL)SUAVE.Analyses.Stability.AVL.AVL
regression_flag (defined in SUAVE.Analyses.Stability.AVL.AVL)SUAVE.Analyses.Stability.AVL.AVL
initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
sample_training(self)SUAVE.Analyses.Stability.AVL.AVL
settings (defined in SUAVE.Analyses.Stability.AVL.AVL)SUAVE.Analyses.Stability.AVL.AVL
stability_model (defined in SUAVE.Analyses.Stability.AVL.AVL)SUAVE.Analyses.Stability.AVL.AVL
surrogates (defined in SUAVE.Analyses.Stability.AVL.AVL)SUAVE.Analyses.Stability.AVL.AVL
tag (defined in SUAVE.Analyses.Stability.AVL.AVL)SUAVE.Analyses.Stability.AVL.AVL
training (defined in SUAVE.Analyses.Stability.AVL.AVL)SUAVE.Analyses.Stability.AVL.AVL
training_file (defined in SUAVE.Analyses.Stability.AVL.AVL)SUAVE.Analyses.Stability.AVL.AVL
surrogates (defined in SUAVE.Analyses.Stability.AVL.AVL)SUAVE.Analyses.Stability.AVL.AVL
tag (defined in SUAVE.Analyses.Stability.AVL.AVL)SUAVE.Analyses.Stability.AVL.AVL
training (defined in SUAVE.Analyses.Stability.AVL.AVL)SUAVE.Analyses.Stability.AVL.AVL
training_file (defined in SUAVE.Analyses.Stability.AVL.AVL)SUAVE.Analyses.Stability.AVL.AVL
@@ -129,7 +133,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1AVL_1_1AVL.html b/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1AVL_1_1AVL.html index 6966be84..447df19a 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1AVL_1_1AVL.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1AVL_1_1AVL.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Stability.AVL.AVL Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -107,8 +114,8 @@ SUAVE.Analyses.Stability.Stability.Stability SUAVE.Analyses.Analysis.Analysis - -
+ + @@ -122,43 +129,37 @@ - - + + - - - - - - - - - - - - - - - - + + + + + + + + + +

Public Member Functions

 
def build_surrogate (self)
 
def evaluate_conditions (self, run_conditions)
 
def evaluate_conditions (self, run_conditions, trim_aircraft)
 
- Public Member Functions inherited from SUAVE.Analyses.Stability.Stability.Stability
def __defaults__ (self)
 
def evaluate (self, conditions)
 
def finalize (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
- - - - + + + + @@ -171,15 +172,6 @@ - - - - - - @@ -235,7 +227,7 @@

-
Evaluates moment coefficient, stability deriviatives and neutral point using available surrogates.
+
Evaluates moment coefficient, stability and body axis deriviatives and neutral point using available surrogates.
 
 Assumptions:
 None
@@ -250,8 +242,8 @@ 

SUAVE.Analyses.Stability.Stability.Stability.

+ @@ -323,22 +316,22 @@

-

◆ evaluate_conditions()

+ +

◆ evaluate_conditions()

@@ -353,7 +346,13 @@

- + + + + + + + @@ -419,11 +418,13 @@

SUAVE.Analyses.Stability.Stability.Stability.

+ @@ -456,7 +457,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1AVL_1_1AVL.js b/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1AVL_1_1AVL.js index ac14af12..a0060aba 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1AVL_1_1AVL.js +++ b/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1AVL_1_1AVL.js @@ -3,16 +3,13 @@ var classSUAVE_1_1Analyses_1_1Stability_1_1AVL_1_1AVL = [ "__call__", "classSUAVE_1_1Analyses_1_1Stability_1_1AVL_1_1AVL.html#ae7f5a136d4f914773b415c5c017b176d", null ], [ "__defaults__", "classSUAVE_1_1Analyses_1_1Stability_1_1AVL_1_1AVL.html#a9f37075e2a9c2fbc72f7cd566644e76f", null ], [ "build_surrogate", "classSUAVE_1_1Analyses_1_1Stability_1_1AVL_1_1AVL.html#a5347926425ec1203182205229dc97d64", null ], - [ "evaluate_conditions", "classSUAVE_1_1Analyses_1_1Stability_1_1AVL_1_1AVL.html#a657bb443e967af278f6c71dd9984e51f", null ], + [ "evaluate_conditions", "classSUAVE_1_1Analyses_1_1Stability_1_1AVL_1_1AVL.html#acb082048b7b042c5d9e94907df4ed41c", null ], [ "finalize", "classSUAVE_1_1Analyses_1_1Stability_1_1AVL_1_1AVL.html#af45ebff1bbb70f893a8acf375a3bf22b", null ], [ "sample_training", "classSUAVE_1_1Analyses_1_1Stability_1_1AVL_1_1AVL.html#a562e6b7c59034a322413caecdaf20a0b", null ], [ "configuration", "classSUAVE_1_1Analyses_1_1Stability_1_1AVL_1_1AVL.html#a8eea7bc16140884d265413b200d0b8d4", null ], [ "current_status", "classSUAVE_1_1Analyses_1_1Stability_1_1AVL_1_1AVL.html#a5e02a873dd1c9343fd8aad6958cc6745", null ], [ "geometry", "classSUAVE_1_1Analyses_1_1Stability_1_1AVL_1_1AVL.html#a986baf42d99f5aceecd129b0e96dfeef", null ], - [ "keep_files", "classSUAVE_1_1Analyses_1_1Stability_1_1AVL_1_1AVL.html#afa2cccd337ca32296250e3a064452d2e", null ], - [ "regression_flag", "classSUAVE_1_1Analyses_1_1Stability_1_1AVL_1_1AVL.html#ad5d2e9deaab9a701dc9d2f507a1a6aad", null ], [ "settings", "classSUAVE_1_1Analyses_1_1Stability_1_1AVL_1_1AVL.html#a7166eeacc3407b0cf419bd38540d2bce", null ], - [ "stability_model", "classSUAVE_1_1Analyses_1_1Stability_1_1AVL_1_1AVL.html#a5df82e27a841c273c87e0ad921e694e0", null ], [ "surrogates", "classSUAVE_1_1Analyses_1_1Stability_1_1AVL_1_1AVL.html#a0531b41b4becb72563a55c5a1a512064", null ], [ "tag", "classSUAVE_1_1Analyses_1_1Stability_1_1AVL_1_1AVL.html#acb0b333f0664e897af228b7636682b7b", null ], [ "training", "classSUAVE_1_1Analyses_1_1Stability_1_1AVL_1_1AVL.html#a93ec6a80598d06260202387cdc472a85", null ], diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1Fidelity__Zero_1_1Fidelity__Zero-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1Fidelity__Zero_1_1Fidelity__Zero-members.html index b331ec46..71cf73cd 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1Fidelity__Zero_1_1Fidelity__Zero-members.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1Fidelity__Zero_1_1Fidelity__Zero-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Attributes

 tag
 
keep_files
 
settings
 
 current_status
 
geometry
 
settings
 
 training
 
 configuration
 
geometry
 
stability_model
 
regression_flag
 
- Public Attributes inherited from SUAVE.Analyses.Stability.Stability.Stability
 tag
 run_conditions run_conditions,
 trim_aircraft 
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -99,57 +106,19 @@

This is the complete list of members for SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero, including all inherited members.

- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - + + + + + + + + + + + - - - - - - - +
__call__(self, conditions)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero
SUAVE::Analyses::Stability::Stability::Stability.__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self) (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero
cDw (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
cl_beta (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
cl_p (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
cl_psi (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
cl_r (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
cL_u (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
cm_alpha_dot (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
cm_q (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
cn_beta (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
cn_r (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
configurationSUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
cx_alpha (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
cx_u (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
cy_beta (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
cy_phi (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
cz_alpha (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
cz_alpha_dot (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
cz_q (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
cz_u (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
damping_ratio (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
dutch_roll (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
dynamic (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
evaluate(self, conditions)SUAVE.Analyses.Stability.Stability.Stability
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self) (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
fuel (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
geometrySUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
l_t (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
l_v (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
lateral_directional (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
longitudinal (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
mass (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
mass_properties (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
natural_frequency (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
phugoid (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
results (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
roll_tau (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
SUAVE::Analyses::Stability::Stability::Stability.__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
configuration (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero
evaluate(self, conditions)SUAVE.Analyses.Stability.Stability.Stability
SUAVE::Analyses::Analysis::Analysis.evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero
SUAVE::Analyses::Analysis::Analysis.finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
geometry (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero
initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
settings (defined in SUAVE.Analyses.Stability.Stability.Stability)SUAVE.Analyses.Stability.Stability.Stability
short_period (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
spiral_tau (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
stability_model (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
static (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
static_margin (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
tag (defined in SUAVE.Analyses.Stability.Stability.Stability)SUAVE.Analyses.Stability.Stability.Stability
theta (defined in SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero)SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zerostatic
tag (defined in SUAVE.Analyses.Stability.Stability.Stability)SUAVE.Analyses.Stability.Stability.Stability
@@ -157,7 +126,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1Fidelity__Zero_1_1Fidelity__Zero.html b/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1Fidelity__Zero_1_1Fidelity__Zero.html index 9de0622f..5042e596 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1Fidelity__Zero_1_1Fidelity__Zero.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1Fidelity__Zero_1_1Fidelity__Zero.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -93,7 +100,7 @@
SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero Class Reference
@@ -107,163 +114,40 @@ SUAVE.Analyses.Stability.Stability.Stability SUAVE.Analyses.Analysis.Analysis - -
+ + - + - + - - - - - - - - - - - - - - - - + + + + + + + + + +

Public Member Functions

-def __defaults__ (self)
def __defaults__ (self)
 
-def finalize (self)
def finalize (self)
 
def __call__ (self, conditions)
 
- Public Member Functions inherited from SUAVE.Analyses.Stability.Stability.Stability
def __defaults__ (self)
 
def evaluate (self, conditions)
 
def finalize (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
- - + + - + - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Static Public Attributes

 configuration = self.configuration

+Public Attributes

configuration
 
 geometry = self.geometry
geometry
 
stability_model = self.stability_model
 
short_period
 
natural_frequency
 
damping_ratio
 
phugoid
 
roll_tau
 
spiral_tau
 
dutch_roll
 
mass_properties
 
fuel = SUAVE.Components.Physical_Component()
 
mass
 
cn_beta
 
static_margin
 
cDw = aero.drag_breakdown.parasite['main_wing'].parasite_drag_coefficient
 
l_v = geometry.wings['vertical_stabilizer'].origin[0] + geometry.wings['vertical_stabilizer'].aerodynamic_center[0] - geometry.wings['main_wing'].origin[0] - geometry.wings['main_wing'].aerodynamic_center[0]
 
cn_r
 
cl_p
 
cl_beta
 
cy_beta
 
l_t = geometry.wings['horizontal_stabilizer'].origin[0] + geometry.wings['horizontal_stabilizer'].aerodynamic_center[0] - geometry.wings['main_wing'].origin[0] - geometry.wings['main_wing'].aerodynamic_center[0]
 
cm_q
 
cm_alpha_dot
 
cz_alpha
 
cy_phi
 
cl_r
 
theta = conditions.frames.wind.body_rotations[:,1]
 
cl_psi
 
cL_u
 
cz_u
 
cz_alpha_dot
 
cz_q
 
cx_u
 
cx_alpha
 
lateral_directional = Full_Linearized_Equations.lateral_directional(velocity, static_stability.cn_beta , Sref, density, Span, configuration.mass_properties.moments_of_inertia.tensor[2][2], dynamic_stability.cn_r, configuration.mass_properties.moments_of_inertia.tensor[0][0], dynamic_stability.cl_p, configuration.mass_properties.moments_of_inertia.tensor[0][2], dynamic_stability.cl_r, dynamic_stability.cl_beta, dynamic_stability.cn_p, dynamic_stability.cy_phi, dynamic_stability.cy_psi, dynamic_stability.cy_beta, conditions.weights.total_mass)
 
longitudinal = Full_Linearized_Equations.longitudinal(velocity, density, Sref, mac, dynamic_stability.cm_q, dynamic_stability.cz_alpha, conditions.weights.total_mass, static_stability.cm_alpha, configuration.mass_properties.moments_of_inertia.tensor[1][1], dynamic_stability.cm_alpha_dot, dynamic_stability.cz_u, dynamic_stability.cz_alpha_dot, dynamic_stability.cz_q, -aero.lift_coefficient, theta, dynamic_stability.cx_u, dynamic_stability.cx_alpha)
 
results = Data()
 
static
 
dynamic
 
- @@ -320,43 +204,39 @@

Process vehicle to setup geometry, condititon and configuration
-    
+
 Assumptions:
 None
-       
+
 Source:
-    N/A
+N/4
 
-    Inputs:
+Inputs:
 conditions - DataDict() of aerodynamic conditions
-results    - DataDict() of moment coeffients and stability derivatives
+results    - DataDict() of moment coeffients and stability and body axis derivatives
 
-    Outputs:
-    None
- 
-    Properties Used:
-    self.geometry
+Outputs: +None + +Properties Used: +self.geometry + -

Member Data Documentation

-
-

◆ configuration

+ +

◆ __defaults__()

-

-Additional Inherited Members

- Public Attributes inherited from SUAVE.Analyses.Stability.Stability.Stability
 tag
- - - - -
- + + + + +
SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero.configuration = self.configurationdef SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero.__defaults__ ( self)
-
-static
This sets the default values and methods for the analysis.
 
@@ -375,26 +255,24 @@ 

SUAVE.Analyses.Stability.Stability.Stability.

+

- -

◆ geometry

+ +

◆ finalize()

- - - - - -
- + + + + +
SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero.geometry = self.geometrydef SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero.finalize ( self)
-
-static
Finalizes the surrogate needed for lift calculation.
 
@@ -413,6 +291,8 @@ 

SUAVE.Analyses.Stability.Stability.Stability.

+


The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1Fidelity__Zero_1_1Fidelity__Zero.js b/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1Fidelity__Zero_1_1Fidelity__Zero.js index b3f89a9e..01b631aa 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1Fidelity__Zero_1_1Fidelity__Zero.js +++ b/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1Fidelity__Zero_1_1Fidelity__Zero.js @@ -2,5 +2,7 @@ var classSUAVE_1_1Analyses_1_1Stability_1_1Fidelity__Zero_1_1Fidelity__Zero = [ [ "__call__", "classSUAVE_1_1Analyses_1_1Stability_1_1Fidelity__Zero_1_1Fidelity__Zero.html#acbce9b7e47bacb187aa72ba799652b5a", null ], [ "__defaults__", "classSUAVE_1_1Analyses_1_1Stability_1_1Fidelity__Zero_1_1Fidelity__Zero.html#abf23a7cc154b9b9cf5f7a54b2e7d746d", null ], - [ "finalize", "classSUAVE_1_1Analyses_1_1Stability_1_1Fidelity__Zero_1_1Fidelity__Zero.html#a8aca95c7e34ed2d1edffd84bd1c666e0", null ] + [ "finalize", "classSUAVE_1_1Analyses_1_1Stability_1_1Fidelity__Zero_1_1Fidelity__Zero.html#a8aca95c7e34ed2d1edffd84bd1c666e0", null ], + [ "configuration", "classSUAVE_1_1Analyses_1_1Stability_1_1Fidelity__Zero_1_1Fidelity__Zero.html#abe2bec1edafc16f467d0820d9be8c7bd", null ], + [ "geometry", "classSUAVE_1_1Analyses_1_1Stability_1_1Fidelity__Zero_1_1Fidelity__Zero.html#a12aff85dcdb231a271e89e02070b17c7", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1Stability_1_1Stability-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1Stability_1_1Stability-members.html index cf8777c8..45a9636c 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1Stability_1_1Stability-members.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1Stability_1_1Stability-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -98,16 +105,16 @@

This is the complete list of members for SUAVE.Analyses.Stability.Stability.Stability, including all inherited members.

- + - + - + - + - +
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Stability.Stability.Stability
compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
evaluate(self, conditions)SUAVE.Analyses.Stability.Stability.Stability
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
SUAVE::Analyses::Analysis::Analysis.evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self)SUAVE.Analyses.Stability.Stability.Stability
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
SUAVE::Analyses::Analysis::Analysis.finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
geometry (defined in SUAVE.Analyses.Stability.Stability.Stability)SUAVE.Analyses.Stability.Stability.Stability
initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
settings (defined in SUAVE.Analyses.Stability.Stability.Stability)SUAVE.Analyses.Stability.Stability.Stability
tag (defined in SUAVE.Analyses.Stability.Stability.Stability)SUAVE.Analyses.Stability.Stability.Stability
@@ -117,7 +124,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1Stability_1_1Stability.html b/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1Stability_1_1Stability.html index 7f66d9fa..598dfcb2 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1Stability_1_1Stability.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Stability_1_1Stability_1_1Stability.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Stability.Stability.Stability Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -108,8 +115,8 @@ SUAVE.Analyses.Analysis.Analysis SUAVE.Analyses.Stability.AVL.AVL SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero - -
+ + @@ -120,18 +127,16 @@ - - - - - - - - - - - - + + + + + + + + + +

Public Member Functions

def finalize (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
@@ -174,7 +179,7 @@

This sets the default values and methods for the analysis.
-    
+
 Assumptions:
 None
 
@@ -190,6 +195,10 @@ 

SUAVE.Analyses.Analysis.Analysis.

+ +

Reimplemented in SUAVE.Analyses.Stability.AVL.AVL, and SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero.

+ @@ -218,7 +227,7 @@

Evaluate the stability analysis.
-    
+
 Assumptions:
 None
 
@@ -252,7 +261,7 @@ 

Finalize the stability analysis.
-    
+
 Assumptions:
 None
 
@@ -268,6 +277,8 @@ 

SUAVE.Analyses.Stability.AVL.AVL, and SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Structures_1_1Structures_1_1Structures-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Structures_1_1Structures_1_1Structures-members.html deleted file mode 100644 index a71a9c39..00000000 --- a/doxygen/classSUAVE_1_1Analyses_1_1Structures_1_1Structures_1_1Structures-members.html +++ /dev/null @@ -1,122 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
-

Public Attributes

- - - - - - - -
-
SUAVE -  1.1.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
- - - - - -
- -
-
-
- - - - - - diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Structures_1_1Structures_1_1Structures.html b/doxygen/classSUAVE_1_1Analyses_1_1Structures_1_1Structures_1_1Structures.html deleted file mode 100644 index 881e80e7..00000000 --- a/doxygen/classSUAVE_1_1Analyses_1_1Structures_1_1Structures_1_1Structures.html +++ /dev/null @@ -1,248 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Structures.Structures.Structures Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.1.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
-
- - - -
-
- -
-
-
- -
- -
-
- - -
- -
- -
- -
-
SUAVE.Analyses.Structures.Structures.Structures Class Reference
-
-
-
-Inheritance diagram for SUAVE.Analyses.Structures.Structures.Structures:
-
-
- - -SUAVE.Analyses.Analysis.Analysis - -
- - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def evaluate (self, conditions)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - -

-Public Attributes

tag
 
features
 
settings
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
SUAVE.Analyses.Structures.Structures()
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Structures.Structures.Structures.__defaults__ ( self)
-
-
This sets the default values and methods for the analysis.
-    
-Assumptions:
-None
-    
-Source:
-N/A
-    
-Inputs:
-None
-    
-Outputs:
-None
-    
-Properties Used:
-N/A
-
-
- -

◆ evaluate()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Analyses.Structures.Structures.Structures.evaluate ( self,
 conditions 
)
-
-
Evaluate the Structures analysis.
-    
-Assumptions:
-None
-    
-Source:
-N/A
-    
-Inputs:
-None
-    
-Outputs:
-Results of the Structures Analysis
-    
-Properties Used:
-N/A                
-
-
-
The documentation for this class was generated from the following file:
    -
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Analyses/Structures/Structures.py
  • -
-
-
- - - - diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Structures_1_1Structures_1_1Structures.js b/doxygen/classSUAVE_1_1Analyses_1_1Structures_1_1Structures_1_1Structures.js deleted file mode 100644 index bd3dc201..00000000 --- a/doxygen/classSUAVE_1_1Analyses_1_1Structures_1_1Structures_1_1Structures.js +++ /dev/null @@ -1,8 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Structures_1_1Structures_1_1Structures = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Structures_1_1Structures_1_1Structures.html#af4900ed36ae06effa0ecb10080e0a667", null ], - [ "evaluate", "classSUAVE_1_1Analyses_1_1Structures_1_1Structures_1_1Structures.html#ab08fe047a6db230f0029c0d99f8d44f7", null ], - [ "features", "classSUAVE_1_1Analyses_1_1Structures_1_1Structures_1_1Structures.html#a4de2b7356404f1e4d38b3509bf8dc9ad", null ], - [ "settings", "classSUAVE_1_1Analyses_1_1Structures_1_1Structures_1_1Structures.html#a7010fe6e6c8eee4c11c401441855d3ae", null ], - [ "tag", "classSUAVE_1_1Analyses_1_1Structures_1_1Structures_1_1Structures.html#a8a7a57d3440fa99c345d107250296f5e", null ] -]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Structures_1_1Structures_1_1Structures.png b/doxygen/classSUAVE_1_1Analyses_1_1Structures_1_1Structures_1_1Structures.png deleted file mode 100644 index 9c85adf2..00000000 Binary files a/doxygen/classSUAVE_1_1Analyses_1_1Structures_1_1Structures_1_1Structures.png and /dev/null differ diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Surrogate_1_1Surrogate-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Surrogate_1_1Surrogate-members.html deleted file mode 100644 index dc0d2c1f..00000000 --- a/doxygen/classSUAVE_1_1Analyses_1_1Surrogate_1_1Surrogate-members.html +++ /dev/null @@ -1,127 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.1.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
-
- - - -
-
- -
-
-
- - - - - - diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Surrogate_1_1Surrogate.html b/doxygen/classSUAVE_1_1Analyses_1_1Surrogate_1_1Surrogate.html deleted file mode 100644 index 52cc3446..00000000 --- a/doxygen/classSUAVE_1_1Analyses_1_1Surrogate_1_1Surrogate.html +++ /dev/null @@ -1,360 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Surrogate.Surrogate Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.1.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
-
- - - -
-
- -
-
-
- -
- -
-
- - -
- -
- -
- -
-
SUAVE.Analyses.Surrogate.Surrogate Class Reference
-
-
-
-Inheritance diagram for SUAVE.Analyses.Surrogate.Surrogate:
-
-
- - -SUAVE.Analyses.Analysis.Analysis - -
- - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def finalize (self)
 
def sample_training (self)
 
def build_surrogate (self)
 
def evaluate (self, state)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - -

-Public Attributes

training
 
surrogates
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
SUAVE.Analyses.Surrogate()
-
-    The Top Level Surrogate Class
-    
-        Assumptions:
-        None
-        
-        Source:
-        N/A
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Surrogate.Surrogate.__defaults__ ( self)
-
-
This sets the default values for the surrogate.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
- -

◆ build_surrogate()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Surrogate.Surrogate.build_surrogate ( self)
-
-
This is used to build the surrogate based on previous training.
-       
-Assumptions:
-None
-       
-Source:
-N/A
-       
-Inputs:
-None
-       
-Outputs:
-None
-       
-Properties Used:
-N/A
-
-
- -

◆ evaluate()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Analyses.Surrogate.Surrogate.evaluate ( self,
 state 
)
-
-
This is used to evaluate the surrogate.
-               
-Assumptions:
-None
-               
-Source:
-N/A
-               
-Inputs:
-None
-               
-Outputs:
-Results of the surrogate model
-               
-Properties Used:
-N/A
-
-
- -

◆ finalize()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Surrogate.Surrogate.finalize ( self)
-
-
This is used to finalize the surrogate's training and build
-   the final surrogate.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
- -

◆ sample_training()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Surrogate.Surrogate.sample_training ( self)
-
-
This is used to train the surrogate on the sampled data
-   according the optimization plan.
-       
-Assumptions:
-None
-       
-Source:
-N/A
-       
-Inputs:
-None
-       
-Outputs:
-None
-       
-Properties Used:
-N/A
-
-
-
The documentation for this class was generated from the following file:
    -
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Analyses/Surrogate.py
  • -
-
-
- - - - diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Surrogate_1_1Surrogate.js b/doxygen/classSUAVE_1_1Analyses_1_1Surrogate_1_1Surrogate.js deleted file mode 100644 index f5f31e04..00000000 --- a/doxygen/classSUAVE_1_1Analyses_1_1Surrogate_1_1Surrogate.js +++ /dev/null @@ -1,10 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Surrogate_1_1Surrogate = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Surrogate_1_1Surrogate.html#a63d74ea95e3ee3d75b421763b1b7eab0", null ], - [ "build_surrogate", "classSUAVE_1_1Analyses_1_1Surrogate_1_1Surrogate.html#ae64ef8c0d281e8bf19f00ffaa42e1ad6", null ], - [ "evaluate", "classSUAVE_1_1Analyses_1_1Surrogate_1_1Surrogate.html#abbabba1804ca34f98a001e05a97e9438", null ], - [ "finalize", "classSUAVE_1_1Analyses_1_1Surrogate_1_1Surrogate.html#ab1a1e389cc333127b68d622554f188c0", null ], - [ "sample_training", "classSUAVE_1_1Analyses_1_1Surrogate_1_1Surrogate.html#a7fd280baca4ac2ad8a73e4858b2c3906", null ], - [ "surrogates", "classSUAVE_1_1Analyses_1_1Surrogate_1_1Surrogate.html#a1728feddc45a65ba7a71ee8ba510fb70", null ], - [ "training", "classSUAVE_1_1Analyses_1_1Surrogate_1_1Surrogate.html#a24906c9735ddd0f6775997b00bcab98e", null ] -]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Surrogate_1_1Surrogate.png b/doxygen/classSUAVE_1_1Analyses_1_1Surrogate_1_1Surrogate.png deleted file mode 100644 index f60487b9..00000000 Binary files a/doxygen/classSUAVE_1_1Analyses_1_1Surrogate_1_1Surrogate.png and /dev/null differ diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Vehicle_1_1Vehicle-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Vehicle_1_1Vehicle-members.html index 6f8f84bd..7d30bf0b 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Vehicle_1_1Vehicle-members.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Vehicle_1_1Vehicle-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -98,19 +105,19 @@

This is the complete list of members for SUAVE.Analyses.Vehicle.Vehicle, including all inherited members.

- + - + - + - - + + - + @@ -123,7 +130,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Vehicle_1_1Vehicle.html b/doxygen/classSUAVE_1_1Analyses_1_1Vehicle_1_1Vehicle.html index c4c48393..2e0df474 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Vehicle_1_1Vehicle.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Vehicle_1_1Vehicle.html @@ -1,9 +1,9 @@ - + - +SUAVE: SUAVE.Analyses.Vehicle.Vehicle Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ @@ -57,9 +60,11 @@
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Container
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Container
__defaults__(self)SUAVE.Analyses.Vehicle.Vehicle
__init__(self, args, kwarg)SUAVE.Analyses.Vehicle.Vehicle
__init__(self, *args, **kwarg)SUAVE.Analyses.Vehicle.Vehicle
aerodynamics (defined in SUAVE.Analyses.Vehicle.Vehicle)SUAVE.Analyses.Vehicle.Vehicle
append(self, analysis)SUAVE.Analyses.Vehicle.Vehicle
atmosphere (defined in SUAVE.Analyses.Vehicle.Vehicle)SUAVE.Analyses.Vehicle.Vehicle
compile(self, args, kwarg)SUAVE.Analyses.Analysis.Container
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Container
costs (defined in SUAVE.Analyses.Vehicle.Vehicle)SUAVE.Analyses.Vehicle.Vehicle
energy (defined in SUAVE.Analyses.Vehicle.Vehicle)SUAVE.Analyses.Vehicle.Vehicle
evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Container
finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Container
evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Container
finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Container
get_root(self, analysis)SUAVE.Analyses.Vehicle.Vehicle
initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Container
initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Container
noise (defined in SUAVE.Analyses.Vehicle.Vehicle)SUAVE.Analyses.Vehicle.Vehicle
planet (defined in SUAVE.Analyses.Vehicle.Vehicle)SUAVE.Analyses.Vehicle.Vehicle
sizing (defined in SUAVE.Analyses.Vehicle.Vehicle)SUAVE.Analyses.Vehicle.Vehicle
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -106,8 +113,8 @@ SUAVE.Analyses.Analysis.Container - -
+ + @@ -115,21 +122,21 @@ - - + + - - - - - - - - - - + + + + + + + + + +

Public Member Functions

 
def append (self, analysis)
 
def __init__ (self, args, kwarg)
 
def __init__ (self, *args, **kwarg)
 
def get_root (self, analysis)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Container
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
@@ -172,8 +179,8 @@ Source: N/A

Constructor & Destructor Documentation

- -

◆ __init__()

+ +

◆ __init__()

@@ -187,13 +194,13 @@

- + - + @@ -357,7 +364,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Vehicle_1_1Vehicle.js b/doxygen/classSUAVE_1_1Analyses_1_1Vehicle_1_1Vehicle.js index 5ba9c378..ac5a8d8a 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Vehicle_1_1Vehicle.js +++ b/doxygen/classSUAVE_1_1Analyses_1_1Vehicle_1_1Vehicle.js @@ -1,6 +1,6 @@ var classSUAVE_1_1Analyses_1_1Vehicle_1_1Vehicle = [ - [ "__init__", "classSUAVE_1_1Analyses_1_1Vehicle_1_1Vehicle.html#aac80b206b29af7818940de54f437ebec", null ], + [ "__init__", "classSUAVE_1_1Analyses_1_1Vehicle_1_1Vehicle.html#a20dcf0e9da5171dfd224aa0558fd70e9", null ], [ "__defaults__", "classSUAVE_1_1Analyses_1_1Vehicle_1_1Vehicle.html#a6fbadfc951c25c01c181e75c8b07db75", null ], [ "append", "classSUAVE_1_1Analyses_1_1Vehicle_1_1Vehicle.html#a47da109afe71d431d2c6e31b12ce51e9", null ], [ "get_root", "classSUAVE_1_1Analyses_1_1Vehicle_1_1Vehicle.html#a7432f659914e8bc502addeb53b571bc8", null ], diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights_1_1Weights-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights_1_1Weights-members.html index f1afd9d0..eaafc57f 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights_1_1Weights-members.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights_1_1Weights-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Attributes

  args,
 **  kwarg 
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -98,18 +105,19 @@

This is the complete list of members for SUAVE.Analyses.Weights.Weights.Weights, including all inherited members.

- + - - - + + + - - - - - + + + + + +
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Weights.Weights.Weights
compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
evaluate(self)SUAVE.Analyses.Weights.Weights.Weights
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
evaluate(self, conditions=None)SUAVE.Analyses.Weights.Weights.Weights
SUAVE::Analyses::Analysis::Analysis.evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self)SUAVE.Analyses.Weights.Weights.Weights
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
settings (defined in SUAVE.Analyses.Weights.Weights.Weights)SUAVE.Analyses.Weights.Weights.Weights
tag (defined in SUAVE.Analyses.Weights.Weights.Weights)SUAVE.Analyses.Weights.Weights.Weights
vehicle (defined in SUAVE.Analyses.Weights.Weights.Weights)SUAVE.Analyses.Weights.Weights.Weights
SUAVE::Analyses::Analysis::Analysis.finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
mass_properties (defined in SUAVE.Analyses.Weights.Weights.Weights)SUAVE.Analyses.Weights.Weights.Weights
settings (defined in SUAVE.Analyses.Weights.Weights.Weights)SUAVE.Analyses.Weights.Weights.Weights
tag (defined in SUAVE.Analyses.Weights.Weights.Weights)SUAVE.Analyses.Weights.Weights.Weights
vehicle (defined in SUAVE.Analyses.Weights.Weights.Weights)SUAVE.Analyses.Weights.Weights.Weights
@@ -117,7 +125,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights_1_1Weights.html b/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights_1_1Weights.html index 8993bff8..00c54497 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights_1_1Weights.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights_1_1Weights.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Weights.Weights.Weights Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -105,34 +112,33 @@
-SUAVE.Analyses.Analysis.Analysis -SUAVE.Analyses.Weights.Weights_BWB.Weights_BWB -SUAVE.Analyses.Weights.Weights_Tube_Wing.Weights_Tube_Wing -SUAVE.Analyses.Weights.Weights_UAV.Weights_UAV - -
+SUAVE.Analyses.Analysis.Analysis +SUAVE.Analyses.Weights.Weights_BWB.Weights_BWB +SUAVE.Analyses.Weights.Weights_eVTOL.Weights_eVTOL +SUAVE.Analyses.Weights.Weights_Transport.Weights_Transport +SUAVE.Analyses.Weights.Weights_UAV.Weights_UAV + + - - + + - - - - - - - - - - - - + + + + + + + + + +

Public Member Functions

def __defaults__ (self)
 
def evaluate (self)
 
def evaluate (self, conditions=None)
 
def finalize (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
@@ -145,6 +151,9 @@ + + @@ -207,10 +216,14 @@

SUAVE.Analyses.Analysis.Analysis.

+ +

Reimplemented in SUAVE.Analyses.Weights.Weights_eVTOL.Weights_eVTOL, SUAVE.Analyses.Weights.Weights_Transport.Weights_Transport, SUAVE.Analyses.Weights.Weights_BWB.Weights_BWB, and SUAVE.Analyses.Weights.Weights_UAV.Weights_UAV.

+ - -

◆ evaluate()

+ +

◆ evaluate()

- + + + + + + + + + + +

Public Attributes

 settings
 
mass_properties
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
 tag
(  self)self,
 conditions = None 
)
@@ -262,16 +290,16 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights_1_1Weights.js b/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights_1_1Weights.js index f92bb97e..eb57bab9 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights_1_1Weights.js +++ b/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights_1_1Weights.js @@ -1,8 +1,9 @@ var classSUAVE_1_1Analyses_1_1Weights_1_1Weights_1_1Weights = [ [ "__defaults__", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights_1_1Weights.html#a86cc65bf0c5930a39233813eff22a7d6", null ], - [ "evaluate", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights_1_1Weights.html#ac9645a2ebbd1e56c398e1f4c140aa92b", null ], + [ "evaluate", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights_1_1Weights.html#aa2c8b86cbf9af657fb07037bdd0393e5", null ], [ "finalize", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights_1_1Weights.html#a7baa0de30c63153a9d786f962678efc0", null ], + [ "mass_properties", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights_1_1Weights.html#a4059dcac59bddc7f07b9334e007387a7", null ], [ "settings", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights_1_1Weights.html#a99617252b6aabe071d5d227009e46faf", null ], [ "tag", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights_1_1Weights.html#a50368d1720b2d063aa80c22144adb0e6", null ], [ "vehicle", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights_1_1Weights.html#aa9247e038c8fffe1d74089cbf3204751", null ] diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights_1_1Weights.png b/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights_1_1Weights.png index 0f76726e..5fc1791e 100644 Binary files a/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights_1_1Weights.png and b/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights_1_1Weights.png differ diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__BWB_1_1Weights__BWB-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__BWB_1_1Weights__BWB-members.html index 175a8b73..54758ac3 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__BWB_1_1Weights__BWB-members.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__BWB_1_1Weights__BWB-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -98,20 +105,19 @@

This is the complete list of members for SUAVE.Analyses.Weights.Weights_BWB.Weights_BWB, including all inherited members.

- + - - - - - - - - - - - - + + + + + + + + + + +
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Weights.Weights_BWB.Weights_BWB
compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
evaluate(self, conditions=None)SUAVE.Analyses.Weights.Weights_BWB.Weights_BWB
SUAVE::Analyses::Weights::Weights::Weights.evaluate(self)SUAVE.Analyses.Weights.Weights.Weights
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self)SUAVE.Analyses.Weights.Weights_BWB.Weights_BWB
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
mass_properties (defined in SUAVE.Analyses.Weights.Weights_BWB.Weights_BWB)SUAVE.Analyses.Weights.Weights_BWB.Weights_BWB
settings (defined in SUAVE.Analyses.Weights.Weights_BWB.Weights_BWB)SUAVE.Analyses.Weights.Weights_BWB.Weights_BWB
tag (defined in SUAVE.Analyses.Weights.Weights_BWB.Weights_BWB)SUAVE.Analyses.Weights.Weights_BWB.Weights_BWB
vehicle (defined in SUAVE.Analyses.Weights.Weights_BWB.Weights_BWB)SUAVE.Analyses.Weights.Weights_BWB.Weights_BWB
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
evaluate(self, conditions=None)SUAVE.Analyses.Weights.Weights.Weights
SUAVE::Analyses::Analysis::Analysis.evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self)SUAVE.Analyses.Weights.Weights.Weights
SUAVE::Analyses::Analysis::Analysis.finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
mass_properties (defined in SUAVE.Analyses.Weights.Weights.Weights)SUAVE.Analyses.Weights.Weights.Weights
settings (defined in SUAVE.Analyses.Weights.Weights_BWB.Weights_BWB)SUAVE.Analyses.Weights.Weights_BWB.Weights_BWB
tag (defined in SUAVE.Analyses.Weights.Weights_BWB.Weights_BWB)SUAVE.Analyses.Weights.Weights_BWB.Weights_BWB
vehicle (defined in SUAVE.Analyses.Weights.Weights_BWB.Weights_BWB)SUAVE.Analyses.Weights.Weights_BWB.Weights_BWB
@@ -119,7 +125,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__BWB_1_1Weights__BWB.html b/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__BWB_1_1Weights__BWB.html index abea9502..4f9e4728 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__BWB_1_1Weights__BWB.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__BWB_1_1Weights__BWB.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Weights.Weights_BWB.Weights_BWB Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -107,37 +114,29 @@ SUAVE.Analyses.Weights.Weights.Weights SUAVE.Analyses.Analysis.Analysis - -
+ + - - - - - - - - + + - - - - - - - - - - - - + + + + + + + + + +

Public Member Functions

def __defaults__ (self)
 
def evaluate (self, conditions=None)
 
def finalize (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Weights.Weights.Weights
def __defaults__ (self)
 
def evaluate (self)
 
def evaluate (self, conditions=None)
 
def finalize (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
@@ -150,9 +149,6 @@ - - @@ -163,6 +159,9 @@ + + @@ -224,83 +223,8 @@

-

◆ evaluate()

- -
-
-

Public Attributes

 settings
 
mass_properties
 
- Public Attributes inherited from SUAVE.Analyses.Weights.Weights.Weights
 tag
 settings
 
mass_properties
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
 tag
- - - - - - - - - - - - - - - - - -
def SUAVE.Analyses.Weights.Weights_BWB.Weights_BWB.evaluate ( self,
 conditions = None 
)
-
-
Evaluate the weight analysis.
-    
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-results
-
-Properties Used:
-N/A
-
-
- - -

◆ finalize()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Weights.Weights_BWB.Weights_BWB.finalize ( self)
-
-
Finalize the weight analysis.
-    
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
+

Reimplemented from SUAVE.Analyses.Weights.Weights.Weights.

-Outputs: -None - -Properties Used: -N/A

The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__BWB_1_1Weights__BWB.js b/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__BWB_1_1Weights__BWB.js index 21a411ed..cfc85ec4 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__BWB_1_1Weights__BWB.js +++ b/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__BWB_1_1Weights__BWB.js @@ -1,9 +1,6 @@ var classSUAVE_1_1Analyses_1_1Weights_1_1Weights__BWB_1_1Weights__BWB = [ [ "__defaults__", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights__BWB_1_1Weights__BWB.html#a9b49241023c3d24a518d49adeed118b1", null ], - [ "evaluate", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights__BWB_1_1Weights__BWB.html#a430f1609a90328f8e742f6549f71b26d", null ], - [ "finalize", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights__BWB_1_1Weights__BWB.html#a6045a46a2240c16d562c6206f6f61778", null ], - [ "mass_properties", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights__BWB_1_1Weights__BWB.html#a83f284897ffee3e8ec2fc6e229eac08f", null ], [ "settings", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights__BWB_1_1Weights__BWB.html#a26bc811bcc5941a70f37a53381c66787", null ], [ "tag", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights__BWB_1_1Weights__BWB.html#a63b040cecfd2d1adcad13a91cad5f4b5", null ], [ "vehicle", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights__BWB_1_1Weights__BWB.html#a9a5d8ea00331456f8a423aa1d2562c34", null ] diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__Transport_1_1Weights__Transport-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__Transport_1_1Weights__Transport-members.html new file mode 100644 index 00000000..9833a4af --- /dev/null +++ b/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__Transport_1_1Weights__Transport-members.html @@ -0,0 +1,132 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ + + + + + diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__Transport_1_1Weights__Transport.html b/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__Transport_1_1Weights__Transport.html new file mode 100644 index 00000000..07f2cdda --- /dev/null +++ b/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__Transport_1_1Weights__Transport.html @@ -0,0 +1,292 @@ + + + + + + + +SUAVE: SUAVE.Analyses.Weights.Weights_Transport.Weights_Transport Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Analyses.Weights.Weights_Transport.Weights_Transport Class Reference
+
+
+
+Inheritance diagram for SUAVE.Analyses.Weights.Weights_Transport.Weights_Transport:
+
+
+ + +SUAVE.Analyses.Weights.Weights.Weights +SUAVE.Analyses.Analysis.Analysis + +
+ + + + + + + + + + + + + + + + + + + + +

+Public Member Functions

def __defaults__ (self)
 
def evaluate (self, method="New SUAVE")
 
- Public Member Functions inherited from SUAVE.Analyses.Weights.Weights.Weights
def finalize (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
+ + + + + + + + + + + + + + + + + + + + + + + +

+Public Attributes

tag
 
vehicle
 
settings
 
- Public Attributes inherited from SUAVE.Analyses.Weights.Weights.Weights
tag
 
vehicle
 
settings
 
mass_properties
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
+

Detailed Description

+
This is class that evaluates the weight of Transport class aircraft
+
+Assumptions:
+    None
+
+Source:
+    N/A
+
+Inputs:
+    None
+
+Outputs:
+    None
+
+Properties Used:
+     N/A
+

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Analyses.Weights.Weights_Transport.Weights_Transport.__defaults__ ( self)
+
+
This sets the default values and methods for the tube and wing
+aircraft weight analysis.
+
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+None
+
+Outputs:
+None
+
+Properties Used:
+N/A
+
+

Reimplemented from SUAVE.Analyses.Weights.Weights.Weights.

+ +
+
+ +

◆ evaluate()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Analyses.Weights.Weights_Transport.Weights_Transport.evaluate ( self,
 method = "New SUAVE" 
)
+
+
Evaluate the weight analysis.
+
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+None
+
+Outputs:
+results
+
+Properties Used:
+N/A
+
+

Reimplemented from SUAVE.Analyses.Weights.Weights.Weights.

+ +
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Analyses/Weights/Weights_Transport.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__Transport_1_1Weights__Transport.js b/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__Transport_1_1Weights__Transport.js new file mode 100644 index 00000000..384e5526 --- /dev/null +++ b/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__Transport_1_1Weights__Transport.js @@ -0,0 +1,8 @@ +var classSUAVE_1_1Analyses_1_1Weights_1_1Weights__Transport_1_1Weights__Transport = +[ + [ "__defaults__", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights__Transport_1_1Weights__Transport.html#a303298fbe4f19da03bd43a0f1d1de213", null ], + [ "evaluate", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights__Transport_1_1Weights__Transport.html#a3b575ef1cee0ed80c5cb8430cc8f8003", null ], + [ "settings", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights__Transport_1_1Weights__Transport.html#a98566d7e523849d2ede9af081039eab6", null ], + [ "tag", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights__Transport_1_1Weights__Transport.html#a9a3ca86c9a77f77e64205ccf15416c8d", null ], + [ "vehicle", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights__Transport_1_1Weights__Transport.html#adadf4bd31e3c3c61740dd32267eb4c71", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__Transport_1_1Weights__Transport.png b/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__Transport_1_1Weights__Transport.png new file mode 100644 index 00000000..7bd830b2 Binary files /dev/null and b/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__Transport_1_1Weights__Transport.png differ diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__Tube__Wing_1_1Weights__Tube__Wing-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__Tube__Wing_1_1Weights__Tube__Wing-members.html deleted file mode 100644 index 78041351..00000000 --- a/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__Tube__Wing_1_1Weights__Tube__Wing-members.html +++ /dev/null @@ -1,126 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.1.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
-
- - - -
-
- -
-
-
- -
- -
-
- - -
- -
- -
-
-
SUAVE.Analyses.Weights.Weights_Tube_Wing.Weights_Tube_Wing Member List
-
-
- -

This is the complete list of members for SUAVE.Analyses.Weights.Weights_Tube_Wing.Weights_Tube_Wing, including all inherited members.

- - - - - - - - - - - - - - - -
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Weights.Weights_Tube_Wing.Weights_Tube_Wing
compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
evaluate(self, conditions=None)SUAVE.Analyses.Weights.Weights_Tube_Wing.Weights_Tube_Wing
SUAVE::Analyses::Weights::Weights::Weights.evaluate(self)SUAVE.Analyses.Weights.Weights.Weights
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self)SUAVE.Analyses.Weights.Weights_Tube_Wing.Weights_Tube_Wing
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
mass_properties (defined in SUAVE.Analyses.Weights.Weights_Tube_Wing.Weights_Tube_Wing)SUAVE.Analyses.Weights.Weights_Tube_Wing.Weights_Tube_Wing
settings (defined in SUAVE.Analyses.Weights.Weights_Tube_Wing.Weights_Tube_Wing)SUAVE.Analyses.Weights.Weights_Tube_Wing.Weights_Tube_Wing
tag (defined in SUAVE.Analyses.Weights.Weights_Tube_Wing.Weights_Tube_Wing)SUAVE.Analyses.Weights.Weights_Tube_Wing.Weights_Tube_Wing
vehicle (defined in SUAVE.Analyses.Weights.Weights_Tube_Wing.Weights_Tube_Wing)SUAVE.Analyses.Weights.Weights_Tube_Wing.Weights_Tube_Wing
-
- - - - diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__Tube__Wing_1_1Weights__Tube__Wing.html b/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__Tube__Wing_1_1Weights__Tube__Wing.html deleted file mode 100644 index 5cd5a93c..00000000 --- a/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__Tube__Wing_1_1Weights__Tube__Wing.html +++ /dev/null @@ -1,323 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Analyses.Weights.Weights_Tube_Wing.Weights_Tube_Wing Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.1.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
-
- - - -
-
- -
-
-
- -
- -
-
- - -
- -
- -
- -
-
SUAVE.Analyses.Weights.Weights_Tube_Wing.Weights_Tube_Wing Class Reference
-
-
-
-Inheritance diagram for SUAVE.Analyses.Weights.Weights_Tube_Wing.Weights_Tube_Wing:
-
-
- - -SUAVE.Analyses.Weights.Weights.Weights -SUAVE.Analyses.Analysis.Analysis - -
- - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def evaluate (self, conditions=None)
 
def finalize (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Weights.Weights.Weights
def __defaults__ (self)
 
def evaluate (self)
 
def finalize (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
- - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

tag
 
vehicle
 
settings
 
mass_properties
 
- Public Attributes inherited from SUAVE.Analyses.Weights.Weights.Weights
tag
 
vehicle
 
settings
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
-

Detailed Description

-
This is class that evaluates the weight of Tube and Wing aircraft
-
-Assumptions:
-    None
-
-Source:
-    N/A
-
-Inputs:
-    None
-  
-Outputs:
-    None
-    
-Properties Used:
-     N/A
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Weights.Weights_Tube_Wing.Weights_Tube_Wing.__defaults__ ( self)
-
-
This sets the default values and methods for the tube and wing 
-aircraft weight analysis.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
-
- -

◆ evaluate()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Analyses.Weights.Weights_Tube_Wing.Weights_Tube_Wing.evaluate ( self,
 conditions = None 
)
-
-
Evaluate the weight analysis.
-    
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-results
-
-Properties Used:
-N/A
-
-
-
- -

◆ finalize()

- -
-
- - - - - - - - -
def SUAVE.Analyses.Weights.Weights_Tube_Wing.Weights_Tube_Wing.finalize ( self)
-
-
Finalize the weight analysis.
-    
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Analyses/Weights/Weights_Tube_Wing.py
  • -
-
-
- - - - diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__Tube__Wing_1_1Weights__Tube__Wing.js b/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__Tube__Wing_1_1Weights__Tube__Wing.js deleted file mode 100644 index c676a04d..00000000 --- a/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__Tube__Wing_1_1Weights__Tube__Wing.js +++ /dev/null @@ -1,10 +0,0 @@ -var classSUAVE_1_1Analyses_1_1Weights_1_1Weights__Tube__Wing_1_1Weights__Tube__Wing = -[ - [ "__defaults__", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights__Tube__Wing_1_1Weights__Tube__Wing.html#a0ac33c072e13422a12ecdbb92c7852d9", null ], - [ "evaluate", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights__Tube__Wing_1_1Weights__Tube__Wing.html#ad35348c45018dccd149502cb3fc6f651", null ], - [ "finalize", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights__Tube__Wing_1_1Weights__Tube__Wing.html#a63e58bfa4de1fba841192378ad8ddf66", null ], - [ "mass_properties", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights__Tube__Wing_1_1Weights__Tube__Wing.html#a759f242a10f3e0a4290a8dbc55321508", null ], - [ "settings", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights__Tube__Wing_1_1Weights__Tube__Wing.html#aabb5d1da81c78511840076358db78a6f", null ], - [ "tag", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights__Tube__Wing_1_1Weights__Tube__Wing.html#a51e51ed65132fc1b36d5c05b184d18e6", null ], - [ "vehicle", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights__Tube__Wing_1_1Weights__Tube__Wing.html#af64e9c01c287f9ede9b477893a0f0cd8", null ] -]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__Tube__Wing_1_1Weights__Tube__Wing.png b/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__Tube__Wing_1_1Weights__Tube__Wing.png deleted file mode 100644 index 6ac4fb5e..00000000 Binary files a/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__Tube__Wing_1_1Weights__Tube__Wing.png and /dev/null differ diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__UAV_1_1Weights__UAV-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__UAV_1_1Weights__UAV-members.html index fd24e944..7a0c42d0 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__UAV_1_1Weights__UAV-members.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__UAV_1_1Weights__UAV-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -98,20 +105,19 @@

This is the complete list of members for SUAVE.Analyses.Weights.Weights_UAV.Weights_UAV, including all inherited members.

- + - - - - - - - - - - - - + + + + + + + + + + +
__call__(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
__call__(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
__defaults__(self)SUAVE.Analyses.Weights.Weights_UAV.Weights_UAV
compile(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
evaluate(self, conditions=None)SUAVE.Analyses.Weights.Weights_UAV.Weights_UAV
SUAVE::Analyses::Weights::Weights::Weights.evaluate(self)SUAVE.Analyses.Weights.Weights.Weights
SUAVE::Analyses::Analysis::Analysis.evaluate(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self)SUAVE.Analyses.Weights.Weights_UAV.Weights_UAV
SUAVE::Analyses::Analysis::Analysis.finalize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, args, kwarg)SUAVE.Analyses.Analysis.Analysis
mass_properties (defined in SUAVE.Analyses.Weights.Weights_UAV.Weights_UAV)SUAVE.Analyses.Weights.Weights_UAV.Weights_UAV
settings (defined in SUAVE.Analyses.Weights.Weights_UAV.Weights_UAV)SUAVE.Analyses.Weights.Weights_UAV.Weights_UAV
tag (defined in SUAVE.Analyses.Weights.Weights_UAV.Weights_UAV)SUAVE.Analyses.Weights.Weights_UAV.Weights_UAV
vehicle (defined in SUAVE.Analyses.Weights.Weights_UAV.Weights_UAV)SUAVE.Analyses.Weights.Weights_UAV.Weights_UAV
compile(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
evaluate(self, conditions=None)SUAVE.Analyses.Weights.Weights.Weights
SUAVE::Analyses::Analysis::Analysis.evaluate(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
features (defined in SUAVE.Analyses.Analysis.Analysis)SUAVE.Analyses.Analysis.Analysis
finalize(self)SUAVE.Analyses.Weights.Weights.Weights
SUAVE::Analyses::Analysis::Analysis.finalize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
initialize(self, *args, **kwarg)SUAVE.Analyses.Analysis.Analysis
mass_properties (defined in SUAVE.Analyses.Weights.Weights.Weights)SUAVE.Analyses.Weights.Weights.Weights
settings (defined in SUAVE.Analyses.Weights.Weights_UAV.Weights_UAV)SUAVE.Analyses.Weights.Weights_UAV.Weights_UAV
tag (defined in SUAVE.Analyses.Weights.Weights_UAV.Weights_UAV)SUAVE.Analyses.Weights.Weights_UAV.Weights_UAV
vehicle (defined in SUAVE.Analyses.Weights.Weights_UAV.Weights_UAV)SUAVE.Analyses.Weights.Weights_UAV.Weights_UAV
@@ -119,7 +125,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__UAV_1_1Weights__UAV.html b/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__UAV_1_1Weights__UAV.html index 9ccbeff5..283f09f6 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__UAV_1_1Weights__UAV.html +++ b/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__UAV_1_1Weights__UAV.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Analyses.Weights.Weights_UAV.Weights_UAV Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -107,37 +114,29 @@ SUAVE.Analyses.Weights.Weights.Weights SUAVE.Analyses.Analysis.Analysis - -
+ + - - - - - - - - + + - - - - - - - - - - - - + + + + + + + + + +

Public Member Functions

def __defaults__ (self)
 
def evaluate (self, conditions=None)
 
def finalize (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Weights.Weights.Weights
def __defaults__ (self)
 
def evaluate (self)
 
def evaluate (self, conditions=None)
 
def finalize (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def __defaults__ (self)
 
def compile (self, args, kwarg)
 
def initialize (self, args, kwarg)
 
def evaluate (self, args, kwarg)
 
def finalize (self, args, kwarg)
 
def __call__ (self, args, kwarg)
 
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
@@ -150,9 +149,6 @@ - - @@ -163,6 +159,9 @@ + + @@ -224,84 +223,8 @@

-

◆ evaluate()

- -
-
-

Public Attributes

 settings
 
mass_properties
 
- Public Attributes inherited from SUAVE.Analyses.Weights.Weights.Weights
 tag
 settings
 
mass_properties
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
 tag
- - - - - - - - - - - - - - - - - -
def SUAVE.Analyses.Weights.Weights_UAV.Weights_UAV.evaluate ( self,
 conditions = None 
)
-
-
Evaluate the weight analysis.
-    
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-results
-
-Properties Used:
-N/A
-
-
- - -

◆ finalize()

+

Reimplemented from SUAVE.Analyses.Weights.Weights.Weights.

-
-
- - - - - - - - -
def SUAVE.Analyses.Weights.Weights_UAV.Weights_UAV.finalize ( self)
-
-
Finalize the weight analysis.
-    
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-

The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__UAV_1_1Weights__UAV.js b/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__UAV_1_1Weights__UAV.js index 59cb0230..d3a8fece 100644 --- a/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__UAV_1_1Weights__UAV.js +++ b/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__UAV_1_1Weights__UAV.js @@ -1,9 +1,6 @@ var classSUAVE_1_1Analyses_1_1Weights_1_1Weights__UAV_1_1Weights__UAV = [ [ "__defaults__", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights__UAV_1_1Weights__UAV.html#aab27bc0adcb4cef4b858359180f446fb", null ], - [ "evaluate", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights__UAV_1_1Weights__UAV.html#a024fb6f0e56a5f8ed417c66dc8f03da1", null ], - [ "finalize", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights__UAV_1_1Weights__UAV.html#a9b0a34e0576380cea29e321b7457633b", null ], - [ "mass_properties", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights__UAV_1_1Weights__UAV.html#a9d1b4383e0cc6e638356850d2d7c6c8b", null ], [ "settings", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights__UAV_1_1Weights__UAV.html#a0fdd37d1c7f22da4f19c1e74d2cfe928", null ], [ "tag", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights__UAV_1_1Weights__UAV.html#ad48a29ba78115b5a6f32b759ce5ddd39", null ], [ "vehicle", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights__UAV_1_1Weights__UAV.html#ac1e4b37a1a54b147233300cdba8b07f3", null ] diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__eVTOL_1_1Weights__eVTOL-members.html b/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__eVTOL_1_1Weights__eVTOL-members.html new file mode 100644 index 00000000..d465b54a --- /dev/null +++ b/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__eVTOL_1_1Weights__eVTOL-members.html @@ -0,0 +1,132 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ + + + + + diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__eVTOL_1_1Weights__eVTOL.html b/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__eVTOL_1_1Weights__eVTOL.html new file mode 100644 index 00000000..41587cc5 --- /dev/null +++ b/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__eVTOL_1_1Weights__eVTOL.html @@ -0,0 +1,245 @@ + + + + + + + +SUAVE: SUAVE.Analyses.Weights.Weights_eVTOL.Weights_eVTOL Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Analyses.Weights.Weights_eVTOL.Weights_eVTOL Class Reference
+
+
+
+Inheritance diagram for SUAVE.Analyses.Weights.Weights_eVTOL.Weights_eVTOL:
+
+
+ + +SUAVE.Analyses.Weights.Weights.Weights +SUAVE.Analyses.Analysis.Analysis + +
+ + + + + + + + + + + + + + + + + + + + +

+Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Weights.Weights.Weights
def evaluate (self, conditions=None)
 
def finalize (self)
 
- Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def compile (self, *args, **kwarg)
 
def initialize (self, *args, **kwarg)
 
def evaluate (self, *args, **kwarg)
 
def finalize (self, *args, **kwarg)
 
def __call__ (self, *args, **kwarg)
 
+ + + + + + + + + + + + + + + + + + + + + + + +

+Public Attributes

tag
 
vehicle
 
settings
 
- Public Attributes inherited from SUAVE.Analyses.Weights.Weights.Weights
tag
 
vehicle
 
settings
 
mass_properties
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
tag
 
features
 
settings
 
+

Detailed Description

+
This is class that evaluates the weight of an eVTOL aircraft
+
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+N/A
+
+Outputs:
+N/A
+
+Properties Used:
+N/A
+

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Analyses.Weights.Weights_eVTOL.Weights_eVTOL.__defaults__ ( self)
+
+
Sets the default parameters for an eVTOL weight analysis
+
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+N/A
+
+Outputs:
+N/A
+
+Properties Used:
+N/A
+
+

Reimplemented from SUAVE.Analyses.Weights.Weights.Weights.

+ +
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Analyses/Weights/Weights_eVTOL.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__eVTOL_1_1Weights__eVTOL.js b/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__eVTOL_1_1Weights__eVTOL.js new file mode 100644 index 00000000..663b7fe8 --- /dev/null +++ b/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__eVTOL_1_1Weights__eVTOL.js @@ -0,0 +1,7 @@ +var classSUAVE_1_1Analyses_1_1Weights_1_1Weights__eVTOL_1_1Weights__eVTOL = +[ + [ "__defaults__", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights__eVTOL_1_1Weights__eVTOL.html#a183e182de58dfe445a9b07c60b77b55b", null ], + [ "settings", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights__eVTOL_1_1Weights__eVTOL.html#a9a37bbe94d679928989fbb06547a729f", null ], + [ "tag", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights__eVTOL_1_1Weights__eVTOL.html#a5c92e2a9a58fd70d814acd0135384f1a", null ], + [ "vehicle", "classSUAVE_1_1Analyses_1_1Weights_1_1Weights__eVTOL_1_1Weights__eVTOL.html#afbeb26dc90206ccacb14cb85e41303cf", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__eVTOL_1_1Weights__eVTOL.png b/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__eVTOL_1_1Weights__eVTOL.png new file mode 100644 index 00000000..d453bd50 Binary files /dev/null and b/doxygen/classSUAVE_1_1Analyses_1_1Weights_1_1Weights__eVTOL_1_1Weights__eVTOL.png differ diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Airports_1_1Airport_1_1Airport-members.html b/doxygen/classSUAVE_1_1Attributes_1_1Airports_1_1Airport_1_1Airport-members.html index 75067ab7..13ceec38 100644 --- a/doxygen/classSUAVE_1_1Attributes_1_1Airports_1_1Airport_1_1Airport-members.html +++ b/doxygen/classSUAVE_1_1Attributes_1_1Airports_1_1Airport_1_1Airport-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -110,7 +117,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Airports_1_1Airport_1_1Airport.html b/doxygen/classSUAVE_1_1Attributes_1_1Airports_1_1Airport_1_1Airport.html index 6d938784..82d62980 100644 --- a/doxygen/classSUAVE_1_1Attributes_1_1Airports_1_1Airport_1_1Airport.html +++ b/doxygen/classSUAVE_1_1Attributes_1_1Airports_1_1Airport_1_1Airport.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Attributes.Airports.Airport.Airport Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -103,9 +110,7 @@ Inheritance diagram for SUAVE.Attributes.Airports.Airport.Airport:
- - - +
@@ -57,9 +60,11 @@

@@ -182,7 +187,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Airports_1_1Runway_1_1Runway-members.html b/doxygen/classSUAVE_1_1Attributes_1_1Airports_1_1Runway_1_1Runway-members.html deleted file mode 100644 index 78209f76..00000000 --- a/doxygen/classSUAVE_1_1Attributes_1_1Airports_1_1Runway_1_1Runway-members.html +++ /dev/null @@ -1,114 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.1.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
-
- - - -
-
- -
-
-
- -
- -
-
- - -
- -
- -
-
-
SUAVE.Attributes.Airports.Runway.Runway Member List
-
- -
- - - - diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Airports_1_1Runway_1_1Runway.html b/doxygen/classSUAVE_1_1Attributes_1_1Airports_1_1Runway_1_1Runway.html deleted file mode 100644 index 0a81adb9..00000000 --- a/doxygen/classSUAVE_1_1Attributes_1_1Airports_1_1Runway_1_1Runway.html +++ /dev/null @@ -1,180 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Attributes.Airports.Runway.Runway Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.1.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
-
- - - -
-
- -
-
-
- -
- -
-
- - -
- -
- -
- -
-
SUAVE.Attributes.Airports.Runway.Runway Class Reference
-
-
-
-Inheritance diagram for SUAVE.Attributes.Airports.Runway.Runway:
-
-
- - - -
- - - - -

-Public Member Functions

def __defaults__ (self)
 
- - - -

-Public Attributes

tag
 
-

Detailed Description

-
A basic runway.
-
-Assumptions:
-None
-
-Source:
-None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Attributes.Airports.Runway.Runway.__defaults__ ( self)
-
-
This sets the default values.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Attributes/Airports/Runway.py
  • -
-
-
- - - - diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Airports_1_1Runway_1_1Runway.js b/doxygen/classSUAVE_1_1Attributes_1_1Airports_1_1Runway_1_1Runway.js deleted file mode 100644 index 510affb2..00000000 --- a/doxygen/classSUAVE_1_1Attributes_1_1Airports_1_1Runway_1_1Runway.js +++ /dev/null @@ -1,5 +0,0 @@ -var classSUAVE_1_1Attributes_1_1Airports_1_1Runway_1_1Runway = -[ - [ "__defaults__", "classSUAVE_1_1Attributes_1_1Airports_1_1Runway_1_1Runway.html#a952b090516a9563fc9f040c891493737", null ], - [ "tag", "classSUAVE_1_1Attributes_1_1Airports_1_1Runway_1_1Runway.html#a90f4ba576b4d5091fb0ce8caf86bf9e3", null ] -]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Airports_1_1Runway_1_1Runway.png b/doxygen/classSUAVE_1_1Attributes_1_1Airports_1_1Runway_1_1Runway.png deleted file mode 100644 index b6a7bc2d..00000000 Binary files a/doxygen/classSUAVE_1_1Attributes_1_1Airports_1_1Runway_1_1Runway.png and /dev/null differ diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Atmospheres_1_1Atmosphere_1_1Atmosphere-members.html b/doxygen/classSUAVE_1_1Attributes_1_1Atmospheres_1_1Atmosphere_1_1Atmosphere-members.html index 38becb50..2c10a511 100644 --- a/doxygen/classSUAVE_1_1Attributes_1_1Atmospheres_1_1Atmosphere_1_1Atmosphere-members.html +++ b/doxygen/classSUAVE_1_1Attributes_1_1Atmospheres_1_1Atmosphere_1_1Atmosphere-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -108,7 +115,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Atmospheres_1_1Atmosphere_1_1Atmosphere.html b/doxygen/classSUAVE_1_1Attributes_1_1Atmospheres_1_1Atmosphere_1_1Atmosphere.html index a8a814a4..15eef0a4 100644 --- a/doxygen/classSUAVE_1_1Attributes_1_1Atmospheres_1_1Atmosphere_1_1Atmosphere.html +++ b/doxygen/classSUAVE_1_1Attributes_1_1Atmospheres_1_1Atmosphere_1_1Atmosphere.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Attributes.Atmospheres.Atmosphere.Atmosphere Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -107,8 +114,8 @@ SUAVE.Attributes.Atmospheres.Earth.Constant_Temperature.Constant_Temperature SUAVE.Attributes.Atmospheres.Earth.US_Standard_1976.US_Standard_1976 - -
+ + @@ -165,6 +172,8 @@

SUAVE.Attributes.Atmospheres.Earth.US_Standard_1976.US_Standard_1976, and SUAVE.Attributes.Atmospheres.Earth.Constant_Temperature.Constant_Temperature.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Atmospheres_1_1Earth_1_1Constant__Temperature_1_1Constant__Temperature-members.html b/doxygen/classSUAVE_1_1Attributes_1_1Atmospheres_1_1Earth_1_1Constant__Temperature_1_1Constant__Temperature-members.html index 12279a6f..0c995c85 100644 --- a/doxygen/classSUAVE_1_1Attributes_1_1Atmospheres_1_1Earth_1_1Constant__Temperature_1_1Constant__Temperature-members.html +++ b/doxygen/classSUAVE_1_1Attributes_1_1Atmospheres_1_1Earth_1_1Constant__Temperature_1_1Constant__Temperature-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Member Functions

SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -111,7 +118,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Atmospheres_1_1Earth_1_1Constant__Temperature_1_1Constant__Temperature.html b/doxygen/classSUAVE_1_1Attributes_1_1Atmospheres_1_1Earth_1_1Constant__Temperature_1_1Constant__Temperature.html index fd1056f3..313f98f7 100644 --- a/doxygen/classSUAVE_1_1Attributes_1_1Atmospheres_1_1Earth_1_1Constant__Temperature_1_1Constant__Temperature.html +++ b/doxygen/classSUAVE_1_1Attributes_1_1Atmospheres_1_1Earth_1_1Constant__Temperature_1_1Constant__Temperature.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Attributes.Atmospheres.Earth.Constant_Temperature.Constant_Temperature Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -106,16 +113,13 @@ SUAVE.Attributes.Atmospheres.Atmosphere.Atmosphere - -
+ + - - -

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Attributes.Atmospheres.Atmosphere.Atmosphere
def __defaults__ (self)
 
@@ -177,6 +181,8 @@

SUAVE.Attributes.Atmospheres.Atmosphere.Atmosphere.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Atmospheres_1_1Earth_1_1US__Standard__1976_1_1US__Standard__1976-members.html b/doxygen/classSUAVE_1_1Attributes_1_1Atmospheres_1_1Earth_1_1US__Standard__1976_1_1US__Standard__1976-members.html index 6dcbf0c1..c4c88354 100644 --- a/doxygen/classSUAVE_1_1Attributes_1_1Atmospheres_1_1Earth_1_1US__Standard__1976_1_1US__Standard__1976-members.html +++ b/doxygen/classSUAVE_1_1Attributes_1_1Atmospheres_1_1Earth_1_1US__Standard__1976_1_1US__Standard__1976-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Attributes

SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -111,7 +118,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Atmospheres_1_1Earth_1_1US__Standard__1976_1_1US__Standard__1976.html b/doxygen/classSUAVE_1_1Attributes_1_1Atmospheres_1_1Earth_1_1US__Standard__1976_1_1US__Standard__1976.html index 2b0d57f8..3b690500 100644 --- a/doxygen/classSUAVE_1_1Attributes_1_1Atmospheres_1_1Earth_1_1US__Standard__1976_1_1US__Standard__1976.html +++ b/doxygen/classSUAVE_1_1Attributes_1_1Atmospheres_1_1Earth_1_1US__Standard__1976_1_1US__Standard__1976.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Attributes.Atmospheres.Earth.US_Standard_1976.US_Standard_1976 Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -106,16 +113,13 @@ SUAVE.Attributes.Atmospheres.Atmosphere.Atmosphere - -
+ + - - -

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Attributes.Atmospheres.Atmosphere.Atmosphere
def __defaults__ (self)
 
@@ -180,6 +184,8 @@

SUAVE.Attributes.Atmospheres.Atmosphere.Atmosphere.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Constants_1_1Composition_1_1Composition-members.html b/doxygen/classSUAVE_1_1Attributes_1_1Constants_1_1Composition_1_1Composition-members.html index 37372d4e..4b933794 100644 --- a/doxygen/classSUAVE_1_1Attributes_1_1Constants_1_1Composition_1_1Composition-members.html +++ b/doxygen/classSUAVE_1_1Attributes_1_1Constants_1_1Composition_1_1Composition-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Attributes

SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -108,7 +115,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Constants_1_1Composition_1_1Composition.html b/doxygen/classSUAVE_1_1Attributes_1_1Constants_1_1Composition_1_1Composition.html index 7679ca0c..4dab842b 100644 --- a/doxygen/classSUAVE_1_1Attributes_1_1Constants_1_1Composition_1_1Composition.html +++ b/doxygen/classSUAVE_1_1Attributes_1_1Constants_1_1Composition_1_1Composition.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Attributes.Constants.Composition.Composition Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -106,8 +113,8 @@ SUAVE.Attributes.Constants.Constant.Constant - -
+ + @@ -115,9 +122,6 @@ - - -

Public Member Functions

 
def __check__ (self)
 
- Public Member Functions inherited from SUAVE.Attributes.Constants.Constant.Constant
def __defaults__ (self)
 
@@ -201,6 +205,8 @@

SUAVE.Attributes.Constants.Constant.Constant.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Constants_1_1Constant_1_1Constant-members.html b/doxygen/classSUAVE_1_1Attributes_1_1Constants_1_1Constant_1_1Constant-members.html index 4d2b75b5..bc076a9d 100644 --- a/doxygen/classSUAVE_1_1Attributes_1_1Constants_1_1Constant_1_1Constant-members.html +++ b/doxygen/classSUAVE_1_1Attributes_1_1Constants_1_1Constant_1_1Constant-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Attributes

SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -106,7 +113,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Constants_1_1Constant_1_1Constant.html b/doxygen/classSUAVE_1_1Attributes_1_1Constants_1_1Constant_1_1Constant.html index 22b7e5c6..4ed7a145 100644 --- a/doxygen/classSUAVE_1_1Attributes_1_1Constants_1_1Constant_1_1Constant.html +++ b/doxygen/classSUAVE_1_1Attributes_1_1Constants_1_1Constant_1_1Constant.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Attributes.Constants.Constant.Constant Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -106,10 +113,9 @@ SUAVE.Attributes.Constants.Composition.Composition SUAVE.Attributes.Planets.Planet.Planet -SUAVE.Attributes.Planets.Earth.Earth -SUAVE.Attributes.Planets.Mars.Mars - -
+SUAVE.Attributes.Planets.Earth.Earth + + @@ -157,6 +163,8 @@

SUAVE.Attributes.Constants.Composition.Composition, SUAVE.Attributes.Planets.Earth.Earth, and SUAVE.Attributes.Planets.Planet.Planet.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Constants_1_1Constant_1_1Constant.png b/doxygen/classSUAVE_1_1Attributes_1_1Constants_1_1Constant_1_1Constant.png index f4fef294..e8ccffeb 100644 Binary files a/doxygen/classSUAVE_1_1Attributes_1_1Constants_1_1Constant_1_1Constant.png and b/doxygen/classSUAVE_1_1Attributes_1_1Constants_1_1Constant_1_1Constant.png differ diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Cryogens_1_1Cryogen_1_1Cryogen-members.html b/doxygen/classSUAVE_1_1Attributes_1_1Cryogens_1_1Cryogen_1_1Cryogen-members.html new file mode 100644 index 00000000..3aff2f88 --- /dev/null +++ b/doxygen/classSUAVE_1_1Attributes_1_1Cryogens_1_1Cryogen_1_1Cryogen-members.html @@ -0,0 +1,125 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+

Public Member Functions

+ + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+ + + + + +
+ +
+
+
+ + + + + + diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Cryogens_1_1Cryogen_1_1Cryogen.html b/doxygen/classSUAVE_1_1Attributes_1_1Cryogens_1_1Cryogen_1_1Cryogen.html new file mode 100644 index 00000000..a41c787d --- /dev/null +++ b/doxygen/classSUAVE_1_1Attributes_1_1Cryogens_1_1Cryogen_1_1Cryogen.html @@ -0,0 +1,202 @@ + + + + + + + +SUAVE: SUAVE.Attributes.Cryogens.Cryogen.Cryogen Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Attributes.Cryogens.Cryogen.Cryogen Class Reference
+
+
+
+Inheritance diagram for SUAVE.Attributes.Cryogens.Cryogen.Cryogen:
+
+
+ + +SUAVE.Attributes.Cryogens.Liquid_H2.Liquid_H2 + +
+ + + + +

+Public Member Functions

def __defaults__ (self)
 
+ + + + + + + + + + + +

+Public Attributes

tag
 
density
 
specific_energy
 
energy_density
 
temperatures
 
+

Detailed Description

+
Holds values for a cryogen
+
+Assumptions:
+None
+
+Source:
+None
+

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Attributes.Cryogens.Cryogen.Cryogen.__defaults__ ( self)
+
+
This sets the default values.
+
+Assumptions:
+None
+
+Source:
+Values commonly available
+
+Inputs:
+None
+
+Outputs:
+None
+
+Properties Used:
+None
+
+

Reimplemented in SUAVE.Attributes.Cryogens.Liquid_H2.Liquid_H2.

+ +
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Attributes/Cryogens/Cryogen.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Cryogens_1_1Cryogen_1_1Cryogen.js b/doxygen/classSUAVE_1_1Attributes_1_1Cryogens_1_1Cryogen_1_1Cryogen.js new file mode 100644 index 00000000..2177e7de --- /dev/null +++ b/doxygen/classSUAVE_1_1Attributes_1_1Cryogens_1_1Cryogen_1_1Cryogen.js @@ -0,0 +1,9 @@ +var classSUAVE_1_1Attributes_1_1Cryogens_1_1Cryogen_1_1Cryogen = +[ + [ "__defaults__", "classSUAVE_1_1Attributes_1_1Cryogens_1_1Cryogen_1_1Cryogen.html#a6695bd894a18c4606c3152f1e02a7cb8", null ], + [ "density", "classSUAVE_1_1Attributes_1_1Cryogens_1_1Cryogen_1_1Cryogen.html#a1f2a64574576781c4ec69cb07dc4e970", null ], + [ "energy_density", "classSUAVE_1_1Attributes_1_1Cryogens_1_1Cryogen_1_1Cryogen.html#aff97f38e154ad4e4f73be178cfb03c30", null ], + [ "specific_energy", "classSUAVE_1_1Attributes_1_1Cryogens_1_1Cryogen_1_1Cryogen.html#a3409badeb47caa3af5a020a48962702e", null ], + [ "tag", "classSUAVE_1_1Attributes_1_1Cryogens_1_1Cryogen_1_1Cryogen.html#aadc789e0b77af5c884190512d386c15f", null ], + [ "temperatures", "classSUAVE_1_1Attributes_1_1Cryogens_1_1Cryogen_1_1Cryogen.html#a046182673df6f86f9037544fa16f1dda", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Cryogens_1_1Cryogen_1_1Cryogen.png b/doxygen/classSUAVE_1_1Attributes_1_1Cryogens_1_1Cryogen_1_1Cryogen.png new file mode 100644 index 00000000..11e4234e Binary files /dev/null and b/doxygen/classSUAVE_1_1Attributes_1_1Cryogens_1_1Cryogen_1_1Cryogen.png differ diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Cryogens_1_1Liquid__H2_1_1Liquid__H2-members.html b/doxygen/classSUAVE_1_1Attributes_1_1Cryogens_1_1Liquid__H2_1_1Liquid__H2-members.html new file mode 100644 index 00000000..7df498ee --- /dev/null +++ b/doxygen/classSUAVE_1_1Attributes_1_1Cryogens_1_1Liquid__H2_1_1Liquid__H2-members.html @@ -0,0 +1,150 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
SUAVE.Attributes.Cryogens.Liquid_H2.Liquid_H2 Member List
+
+
+ +

This is the complete list of members for SUAVE.Attributes.Cryogens.Liquid_H2.Liquid_H2, including all inherited members.

+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
__defaults__(self)SUAVE.Attributes.Cryogens.Liquid_H2.Liquid_H2
antoine_A (defined in SUAVE.Attributes.Cryogens.Liquid_H2.Liquid_H2)SUAVE.Attributes.Cryogens.Liquid_H2.Liquid_H2
antoine_B (defined in SUAVE.Attributes.Cryogens.Liquid_H2.Liquid_H2)SUAVE.Attributes.Cryogens.Liquid_H2.Liquid_H2
antoine_C (defined in SUAVE.Attributes.Cryogens.Liquid_H2.Liquid_H2)SUAVE.Attributes.Cryogens.Liquid_H2.Liquid_H2
antoine_maxT (defined in SUAVE.Attributes.Cryogens.Liquid_H2.Liquid_H2)SUAVE.Attributes.Cryogens.Liquid_H2.Liquid_H2
antoine_minT (defined in SUAVE.Attributes.Cryogens.Liquid_H2.Liquid_H2)SUAVE.Attributes.Cryogens.Liquid_H2.Liquid_H2
density (defined in SUAVE.Attributes.Cryogens.Liquid_H2.Liquid_H2)SUAVE.Attributes.Cryogens.Liquid_H2.Liquid_H2
energy_density (defined in SUAVE.Attributes.Cryogens.Liquid_H2.Liquid_H2)SUAVE.Attributes.Cryogens.Liquid_H2.Liquid_H2
GCP_C0 (defined in SUAVE.Attributes.Cryogens.Liquid_H2.Liquid_H2)SUAVE.Attributes.Cryogens.Liquid_H2.Liquid_H2
GCP_C1 (defined in SUAVE.Attributes.Cryogens.Liquid_H2.Liquid_H2)SUAVE.Attributes.Cryogens.Liquid_H2.Liquid_H2
GCP_C2 (defined in SUAVE.Attributes.Cryogens.Liquid_H2.Liquid_H2)SUAVE.Attributes.Cryogens.Liquid_H2.Liquid_H2
GCP_C3 (defined in SUAVE.Attributes.Cryogens.Liquid_H2.Liquid_H2)SUAVE.Attributes.Cryogens.Liquid_H2.Liquid_H2
GCP_maxT (defined in SUAVE.Attributes.Cryogens.Liquid_H2.Liquid_H2)SUAVE.Attributes.Cryogens.Liquid_H2.Liquid_H2
GCP_minT (defined in SUAVE.Attributes.Cryogens.Liquid_H2.Liquid_H2)SUAVE.Attributes.Cryogens.Liquid_H2.Liquid_H2
H_C0 (defined in SUAVE.Attributes.Cryogens.Liquid_H2.Liquid_H2)SUAVE.Attributes.Cryogens.Liquid_H2.Liquid_H2
H_C1 (defined in SUAVE.Attributes.Cryogens.Liquid_H2.Liquid_H2)SUAVE.Attributes.Cryogens.Liquid_H2.Liquid_H2
H_C2 (defined in SUAVE.Attributes.Cryogens.Liquid_H2.Liquid_H2)SUAVE.Attributes.Cryogens.Liquid_H2.Liquid_H2
H_C3 (defined in SUAVE.Attributes.Cryogens.Liquid_H2.Liquid_H2)SUAVE.Attributes.Cryogens.Liquid_H2.Liquid_H2
H_maxP (defined in SUAVE.Attributes.Cryogens.Liquid_H2.Liquid_H2)SUAVE.Attributes.Cryogens.Liquid_H2.Liquid_H2
H_minP (defined in SUAVE.Attributes.Cryogens.Liquid_H2.Liquid_H2)SUAVE.Attributes.Cryogens.Liquid_H2.Liquid_H2
LCP_C0 (defined in SUAVE.Attributes.Cryogens.Liquid_H2.Liquid_H2)SUAVE.Attributes.Cryogens.Liquid_H2.Liquid_H2
LCP_C1 (defined in SUAVE.Attributes.Cryogens.Liquid_H2.Liquid_H2)SUAVE.Attributes.Cryogens.Liquid_H2.Liquid_H2
LCP_C2 (defined in SUAVE.Attributes.Cryogens.Liquid_H2.Liquid_H2)SUAVE.Attributes.Cryogens.Liquid_H2.Liquid_H2
LCP_C3 (defined in SUAVE.Attributes.Cryogens.Liquid_H2.Liquid_H2)SUAVE.Attributes.Cryogens.Liquid_H2.Liquid_H2
LCP_maxT (defined in SUAVE.Attributes.Cryogens.Liquid_H2.Liquid_H2)SUAVE.Attributes.Cryogens.Liquid_H2.Liquid_H2
LCP_minT (defined in SUAVE.Attributes.Cryogens.Liquid_H2.Liquid_H2)SUAVE.Attributes.Cryogens.Liquid_H2.Liquid_H2
specific_energy (defined in SUAVE.Attributes.Cryogens.Liquid_H2.Liquid_H2)SUAVE.Attributes.Cryogens.Liquid_H2.Liquid_H2
specific_heat (defined in SUAVE.Attributes.Cryogens.Liquid_H2.Liquid_H2)SUAVE.Attributes.Cryogens.Liquid_H2.Liquid_H2
tag (defined in SUAVE.Attributes.Cryogens.Liquid_H2.Liquid_H2)SUAVE.Attributes.Cryogens.Liquid_H2.Liquid_H2
temperatures (defined in SUAVE.Attributes.Cryogens.Cryogen.Cryogen)SUAVE.Attributes.Cryogens.Cryogen.Cryogen
vaporization_enthalpy (defined in SUAVE.Attributes.Cryogens.Liquid_H2.Liquid_H2)SUAVE.Attributes.Cryogens.Liquid_H2.Liquid_H2
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Cryogens_1_1Liquid__H2_1_1Liquid__H2.html b/doxygen/classSUAVE_1_1Attributes_1_1Cryogens_1_1Liquid__H2_1_1Liquid__H2.html new file mode 100644 index 00000000..664dba9c --- /dev/null +++ b/doxygen/classSUAVE_1_1Attributes_1_1Cryogens_1_1Liquid__H2_1_1Liquid__H2.html @@ -0,0 +1,290 @@ + + + + + + + +SUAVE: SUAVE.Attributes.Cryogens.Liquid_H2.Liquid_H2 Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Attributes.Cryogens.Liquid_H2.Liquid_H2 Class Reference
+
+
+
+Inheritance diagram for SUAVE.Attributes.Cryogens.Liquid_H2.Liquid_H2:
+
+
+ + +SUAVE.Attributes.Cryogens.Cryogen.Cryogen + +
+ + + + +

+Public Member Functions

def __defaults__ (self)
 
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Attributes

tag
 
density
 
specific_energy
 
energy_density
 
vaporization_enthalpy
 
specific_heat
 
LCP_C0
 
LCP_C1
 
LCP_C2
 
LCP_C3
 
LCP_minT
 
LCP_maxT
 
GCP_C0
 
GCP_C1
 
GCP_C2
 
GCP_C3
 
GCP_minT
 
GCP_maxT
 
antoine_A
 
antoine_B
 
antoine_C
 
antoine_minT
 
antoine_maxT
 
H_C0
 
H_C1
 
H_C2
 
H_C3
 
H_minP
 
H_maxP
 
- Public Attributes inherited from SUAVE.Attributes.Cryogens.Cryogen.Cryogen
tag
 
density
 
specific_energy
 
energy_density
 
temperatures
 
+

Detailed Description

+
Holds values for this cryogen
+
+Assumptions:
+None
+
+Source:
+Ekin - Experimental Techniques for Low Temperature Measurements, ISBN 0-19-857054-6
+NIST Chemistry Webbook
+

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Attributes.Cryogens.Liquid_H2.Liquid_H2.__defaults__ ( self)
+
+
This sets the default values.
+
+Assumptions:
+Ambient Pressure
+
+Source:
+
+Inputs:
+None
+
+Outputs:
+None
+
+Properties Used:
+None
+
+

Reimplemented from SUAVE.Attributes.Cryogens.Cryogen.Cryogen.

+ +
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Attributes/Cryogens/Liquid_H2.py
  • +
+
+
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SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -114,7 +125,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1Air_1_1Air.html b/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1Air_1_1Air.html index a85c2319..5186b05e 100644 --- a/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1Air_1_1Air.html +++ b/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1Air_1_1Air.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Attributes.Gases.Air.Air Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -106,8 +113,8 @@ SUAVE.Attributes.Gases.Gas.Gas - -
+ + @@ -123,19 +130,29 @@ - - - + + + +

Public Member Functions

 
def compute_absolute_viscosity (self, T=300., p=101325.)
 
- Public Member Functions inherited from SUAVE.Attributes.Gases.Gas.Gas
def __defaults__ (self)
 
def compute_thermal_conductivity (self, T=300., p=101325.)
 
def compute_prandtl_number (self, T=300.)
 
+ + + + + + @@ -187,6 +204,8 @@

SUAVE.Attributes.Gases.Gas.Gas.

+ @@ -402,6 +421,51 @@

+

◆ compute_prandtl_number()

+ +
+
+

Public Attributes

tag
 
 molecular_mass
 
 gas_specific_constant
 
specific_heat_capacity
 
- Public Attributes inherited from SUAVE.Attributes.Gases.Gas.Gas
tag
 
 molecular_mass
 
+ + + + + + + + + + + + + + + + + +
def SUAVE.Attributes.Gases.Air.Air.compute_prandtl_number ( self,
 T = 300. 
)
+
+
Compute the prandtl number 
+    
+Assumptions: 
+
+Source:
+N/A
+
+Inputs:
+specific_heat_capacity [J/kgK]
+absolute viscosity     [kg/(m-s)]
+thermal conductivity   [W/(m-K)]
+
+Outputs:
+prandtl number         [unitless]
+
 Properties Used:
 None
 
@@ -466,6 +530,56 @@

+

◆ compute_thermal_conductivity()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Attributes.Gases.Air.Air.compute_thermal_conductivity ( self,
 T = 300.,
 p = 101325. 
)
+
+
Compute the thermal conductivity
+    
+Assumptions:
+Properties computed at 1 bar (14.5 psia)
+
+Source:
+https://www.engineeringtoolbox.com/air-properties-viscosity-conductivity-heat-capacity-d_1509.html 
+
+Inputs:
+T                  [K]       - Temperature
+
+Outputs:
+thermal conductivity [W/(m-K)]
+
+Properties Used:
+None
+
+
+

The documentation for this class was generated from the following file:
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Attributes/Gases/Air.py
@@ -477,7 +591,7 @@

SUAVE + doxygen 1.8.15

diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1Air_1_1Air.js b/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1Air_1_1Air.js index ba6ad1d2..16d1d761 100644 --- a/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1Air_1_1Air.js +++ b/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1Air_1_1Air.js @@ -5,7 +5,11 @@ var classSUAVE_1_1Attributes_1_1Gases_1_1Air_1_1Air = [ "compute_cp", "classSUAVE_1_1Attributes_1_1Gases_1_1Air_1_1Air.html#af2049f5193f71254180aa25263b253a9", null ], [ "compute_density", "classSUAVE_1_1Attributes_1_1Gases_1_1Air_1_1Air.html#a7e7724b5a0f3b55f1d22207de5eb95c3", null ], [ "compute_gamma", "classSUAVE_1_1Attributes_1_1Gases_1_1Air_1_1Air.html#a30b8f6bcf3ad36115e67d482ec406602", null ], + [ "compute_prandtl_number", "classSUAVE_1_1Attributes_1_1Gases_1_1Air_1_1Air.html#a8b971e95f9452e799a97df4562c0be3f", null ], [ "compute_speed_of_sound", "classSUAVE_1_1Attributes_1_1Gases_1_1Air_1_1Air.html#a86d93dc502a49cdf39a1d8f063021776", null ], + [ "compute_thermal_conductivity", "classSUAVE_1_1Attributes_1_1Gases_1_1Air_1_1Air.html#a60bddea705c18fc66874956b7b0693ee", null ], [ "gas_specific_constant", "classSUAVE_1_1Attributes_1_1Gases_1_1Air_1_1Air.html#a971ac13cf64d6a8c4e5e184e3cee8666", null ], - [ "molecular_mass", "classSUAVE_1_1Attributes_1_1Gases_1_1Air_1_1Air.html#afb2bd7b10f13b0aa8d9a1fd2b78d9309", null ] + [ "molecular_mass", "classSUAVE_1_1Attributes_1_1Gases_1_1Air_1_1Air.html#afb2bd7b10f13b0aa8d9a1fd2b78d9309", null ], + [ "specific_heat_capacity", "classSUAVE_1_1Attributes_1_1Gases_1_1Air_1_1Air.html#a598d6233a65ab1ef033edd7e85611c9b", null ], + [ "tag", "classSUAVE_1_1Attributes_1_1Gases_1_1Air_1_1Air.html#a849d84b197c029d5c4d17df55af0dec9", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1CO2_1_1CO2-members.html b/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1CO2_1_1CO2-members.html index c045441f..05352216 100644 --- a/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1CO2_1_1CO2-members.html +++ b/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1CO2_1_1CO2-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -109,7 +117,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1CO2_1_1CO2.html b/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1CO2_1_1CO2.html index 7e99ecc9..a3da7f7c 100644 --- a/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1CO2_1_1CO2.html +++ b/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1CO2_1_1CO2.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Attributes.Gases.CO2.CO2 Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -106,19 +113,19 @@ SUAVE.Attributes.Gases.Gas.Gas - -
+ + - - -

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Attributes.Gases.Gas.Gas
def __defaults__ (self)
 
+ + @@ -126,6 +133,9 @@   + + @@ -177,6 +187,8 @@

SUAVE.Attributes.Gases.Gas.Gas.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1CO2_1_1CO2.js b/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1CO2_1_1CO2.js index 4f69edc3..80743551 100644 --- a/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1CO2_1_1CO2.js +++ b/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1CO2_1_1CO2.js @@ -2,5 +2,6 @@ var classSUAVE_1_1Attributes_1_1Gases_1_1CO2_1_1CO2 = [ [ "__defaults__", "classSUAVE_1_1Attributes_1_1Gases_1_1CO2_1_1CO2.html#af5f8d34d26d75384069a564e850c26cf", null ], [ "gas_specific_constant", "classSUAVE_1_1Attributes_1_1Gases_1_1CO2_1_1CO2.html#a2f45f35a4c6870cef5748765f10b6a95", null ], - [ "molecular_mass", "classSUAVE_1_1Attributes_1_1Gases_1_1CO2_1_1CO2.html#ac6f75e5944b60254978d9815a738d333", null ] + [ "molecular_mass", "classSUAVE_1_1Attributes_1_1Gases_1_1CO2_1_1CO2.html#ac6f75e5944b60254978d9815a738d333", null ], + [ "tag", "classSUAVE_1_1Attributes_1_1Gases_1_1CO2_1_1CO2.html#a46659782a6d23b2db21a550817f55c76", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1Gas_1_1Gas-members.html b/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1Gas_1_1Gas-members.html index 6b02ab08..3e7439b2 100644 --- a/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1Gas_1_1Gas-members.html +++ b/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1Gas_1_1Gas-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Attributes

tag
 
 molecular_mass
 
gas_specific_constant
 
- Public Attributes inherited from SUAVE.Attributes.Gases.Gas.Gas
tag
 
 molecular_mass
 
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -109,7 +117,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1Gas_1_1Gas.html b/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1Gas_1_1Gas.html index a5d4cd8b..7299e0c3 100644 --- a/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1Gas_1_1Gas.html +++ b/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1Gas_1_1Gas.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Attributes.Gases.Gas.Gas Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -108,8 +115,8 @@ SUAVE.Attributes.Gases.Air.Air SUAVE.Attributes.Gases.CO2.CO2 SUAVE.Attributes.Gases.Steam.Steam - -
+ + @@ -118,6 +125,9 @@

Public Member Functions

+ + @@ -169,6 +179,8 @@

SUAVE.Attributes.Gases.Air.Air, SUAVE.Attributes.Gases.Steam.Steam, and SUAVE.Attributes.Gases.CO2.CO2.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1Gas_1_1Gas.js b/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1Gas_1_1Gas.js index 43f40b8d..bbb23932 100644 --- a/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1Gas_1_1Gas.js +++ b/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1Gas_1_1Gas.js @@ -3,5 +3,6 @@ var classSUAVE_1_1Attributes_1_1Gases_1_1Gas_1_1Gas = [ "__defaults__", "classSUAVE_1_1Attributes_1_1Gases_1_1Gas_1_1Gas.html#a57159410d8c1a8e43da05f8faa255288", null ], [ "composition", "classSUAVE_1_1Attributes_1_1Gases_1_1Gas_1_1Gas.html#a890da3c2d8264228bcb0ac9936d16e35", null ], [ "gas_specific_constant", "classSUAVE_1_1Attributes_1_1Gases_1_1Gas_1_1Gas.html#a9472faacd37b54512bd462b4ec467f70", null ], - [ "molecular_mass", "classSUAVE_1_1Attributes_1_1Gases_1_1Gas_1_1Gas.html#af1a58498a684124a1bddd171eed7a8af", null ] + [ "molecular_mass", "classSUAVE_1_1Attributes_1_1Gases_1_1Gas_1_1Gas.html#af1a58498a684124a1bddd171eed7a8af", null ], + [ "tag", "classSUAVE_1_1Attributes_1_1Gases_1_1Gas_1_1Gas.html#a4115a2705cde25362b9746f2b6931a58", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1Steam_1_1Steam-members.html b/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1Steam_1_1Steam-members.html index b0f513ef..e2dcc1dd 100644 --- a/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1Steam_1_1Steam-members.html +++ b/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1Steam_1_1Steam-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Attributes

tag
 
 molecular_mass
 
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -115,7 +123,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1Steam_1_1Steam.html b/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1Steam_1_1Steam.html index 6466ef4d..3f544ad1 100644 --- a/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1Steam_1_1Steam.html +++ b/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1Steam_1_1Steam.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Attributes.Gases.Steam.Steam Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -106,8 +113,8 @@ SUAVE.Attributes.Gases.Gas.Gas - -
+ + @@ -125,12 +132,12 @@ - - -

Public Member Functions

 
def compute_absolute_viscosity (self, T=300, p=101325)
 
- Public Member Functions inherited from SUAVE.Attributes.Gases.Gas.Gas
def __defaults__ (self)
 
+ + @@ -138,6 +145,9 @@   + + @@ -189,6 +199,8 @@

SUAVE.Attributes.Gases.Gas.Gas.

+ @@ -501,7 +513,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1Steam_1_1Steam.js b/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1Steam_1_1Steam.js index 309fcbac..9f6bf1dd 100644 --- a/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1Steam_1_1Steam.js +++ b/doxygen/classSUAVE_1_1Attributes_1_1Gases_1_1Steam_1_1Steam.js @@ -8,5 +8,6 @@ var classSUAVE_1_1Attributes_1_1Gases_1_1Steam_1_1Steam = [ "compute_gamma", "classSUAVE_1_1Attributes_1_1Gases_1_1Steam_1_1Steam.html#a66d54aac1e188e801ca276ca2d48fdd8", null ], [ "compute_speed_of_sound", "classSUAVE_1_1Attributes_1_1Gases_1_1Steam_1_1Steam.html#a86ba9c1313cae71b544a4be1edf05bad", null ], [ "gas_specific_constant", "classSUAVE_1_1Attributes_1_1Gases_1_1Steam_1_1Steam.html#ab45dc8c7c1186e41c21deb0a2ff1d82e", null ], - [ "molecular_mass", "classSUAVE_1_1Attributes_1_1Gases_1_1Steam_1_1Steam.html#a54398bd1c5ff2db7e010ce52851621b0", null ] + [ "molecular_mass", "classSUAVE_1_1Attributes_1_1Gases_1_1Steam_1_1Steam.html#a54398bd1c5ff2db7e010ce52851621b0", null ], + [ "tag", "classSUAVE_1_1Attributes_1_1Gases_1_1Steam_1_1Steam.html#a0bb346fc022f10b6a2575b9472678e41", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Liquids_1_1Liquid_1_1Liquid-members.html b/doxygen/classSUAVE_1_1Attributes_1_1Liquids_1_1Liquid_1_1Liquid-members.html deleted file mode 100644 index f2d8d0bc..00000000 --- a/doxygen/classSUAVE_1_1Attributes_1_1Liquids_1_1Liquid_1_1Liquid-members.html +++ /dev/null @@ -1,118 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
-

Public Attributes

tag
 
 molecular_mass
 
gas_specific_constant
 
- Public Attributes inherited from SUAVE.Attributes.Gases.Gas.Gas
tag
 
 molecular_mass
 
- - - - - - - -
-
SUAVE -  1.1.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Attributes.Liquids.Liquid.Liquid Member List
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-
- - - - - - - - -
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SUAVE -  1.1.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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- -
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SUAVE.Attributes.Liquids.Liquid.Liquid Class Reference
-
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-
-Inheritance diagram for SUAVE.Attributes.Liquids.Liquid.Liquid:
-
-
- - -SUAVE.Attributes.Liquids.Water.Water - -
- - - - -

-Public Member Functions

def __defaults__ (self)
 
- - - - - - - - - - - -

-Public Attributes

molecular_mass
 
composition
 
heat_of_vaporization
 
density
 
boiling_point
 
-

Detailed Description

-
Base class for liquids
-
-Assumptions:
-None
-
-Source:
-None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Attributes.Liquids.Liquid.Liquid.__defaults__ ( self)
-
-
This sets the default values.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Attributes/Liquids/Liquid.py
  • -
-
-
- - - - diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Liquids_1_1Liquid_1_1Liquid.js b/doxygen/classSUAVE_1_1Attributes_1_1Liquids_1_1Liquid_1_1Liquid.js deleted file mode 100644 index a4c906e4..00000000 --- a/doxygen/classSUAVE_1_1Attributes_1_1Liquids_1_1Liquid_1_1Liquid.js +++ /dev/null @@ -1,9 +0,0 @@ -var classSUAVE_1_1Attributes_1_1Liquids_1_1Liquid_1_1Liquid = -[ - [ "__defaults__", "classSUAVE_1_1Attributes_1_1Liquids_1_1Liquid_1_1Liquid.html#a7a914b29e3f95b7e3077924fdab26b75", null ], - [ "boiling_point", "classSUAVE_1_1Attributes_1_1Liquids_1_1Liquid_1_1Liquid.html#a12a13ffeb5bb6578b37361055d5338c2", null ], - [ "composition", "classSUAVE_1_1Attributes_1_1Liquids_1_1Liquid_1_1Liquid.html#a31ff0cf7acd5fda18cb2b60d83af9621", null ], - [ "density", "classSUAVE_1_1Attributes_1_1Liquids_1_1Liquid_1_1Liquid.html#a2d467e83e2ffebbb799f88c27acf279e", null ], - [ "heat_of_vaporization", "classSUAVE_1_1Attributes_1_1Liquids_1_1Liquid_1_1Liquid.html#a85f870a09a056ef2b1eedd43899c9a2c", null ], - [ "molecular_mass", "classSUAVE_1_1Attributes_1_1Liquids_1_1Liquid_1_1Liquid.html#a08a7c2c7a09bfda8f90e5e5a7185df2f", null ] -]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Liquids_1_1Liquid_1_1Liquid.png b/doxygen/classSUAVE_1_1Attributes_1_1Liquids_1_1Liquid_1_1Liquid.png deleted file mode 100644 index 50ce6562..00000000 Binary files a/doxygen/classSUAVE_1_1Attributes_1_1Liquids_1_1Liquid_1_1Liquid.png and /dev/null differ diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Liquids_1_1Water_1_1Water-members.html b/doxygen/classSUAVE_1_1Attributes_1_1Liquids_1_1Water_1_1Water-members.html deleted file mode 100644 index 189fc30d..00000000 --- a/doxygen/classSUAVE_1_1Attributes_1_1Liquids_1_1Water_1_1Water-members.html +++ /dev/null @@ -1,120 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.1.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Attributes.Liquids.Water.Water Member List
-
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- - - - diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Liquids_1_1Water_1_1Water.html b/doxygen/classSUAVE_1_1Attributes_1_1Liquids_1_1Water_1_1Water.html deleted file mode 100644 index 2c7e4ea8..00000000 --- a/doxygen/classSUAVE_1_1Attributes_1_1Liquids_1_1Water_1_1Water.html +++ /dev/null @@ -1,315 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Attributes.Liquids.Water.Water Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.1.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Attributes.Liquids.Water.Water Class Reference
-
-
-
-Inheritance diagram for SUAVE.Attributes.Liquids.Water.Water:
-
-
- - -SUAVE.Attributes.Liquids.Liquid.Liquid - -
- - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def compute_cp (self, temperature=300, pressure=101325)
 
def compute_absolute_viscosity (self, temperature=300, pressure=101325)
 
- Public Member Functions inherited from SUAVE.Attributes.Liquids.Liquid.Liquid
def __defaults__ (self)
 
- - - - - - - - - - - - - - - - - - - - -

-Public Attributes

molecular_mass
 
heat_of_vaporization
 
density
 
boiling_point
 
- Public Attributes inherited from SUAVE.Attributes.Liquids.Liquid.Liquid
molecular_mass
 
composition
 
heat_of_vaporization
 
density
 
boiling_point
 
-

Detailed Description

-
Holds constants and functions that compute properties for water.
-
-Assumptions:
-None
-
-Source:
-None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Attributes.Liquids.Water.Water.__defaults__ ( self)
-
-
This sets the default values.
-
-Assumptions:
-None
-
-Source:
-Values commonly available
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-None
-
-
-
- -

◆ compute_absolute_viscosity()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Attributes.Liquids.Water.Water.compute_absolute_viscosity ( self,
 temperature = 300,
 pressure = 101325 
)
-
-
Compute the absolute (dynamic) viscosity. Model accurate to within 
-2.5% between 0 C and 370C
-    
-Assumptions:
-None
-
-Source:
-Engineering Fluid Mechanics, Al-Shemmeri, pg. 18
-
-Inputs:
-temperature  [K]
-
-Outputs:
-mu           [kg/(m-s)]
-
-Properties Used:
-None
-
-
-
- -

◆ compute_cp()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Attributes.Liquids.Water.Water.compute_cp ( self,
 temperature = 300,
 pressure = 101325 
)
-
-
Computes Cp by 4th-order polynomial data fit:
-cp(T) = c1*T^4 + c2*T^3 + c3*T^2 + c4*T+c
-    
-Assumptions:
-278 K < T < 373.15 K
-
-Source:
-Unknown
-
-Inputs:
-temperature    [K]
-
-Outputs:
-cp             [J/kg-K]
-
-Properties Used:
-None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Attributes/Liquids/Water.py
  • -
-
-
- - - - diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Liquids_1_1Water_1_1Water.js b/doxygen/classSUAVE_1_1Attributes_1_1Liquids_1_1Water_1_1Water.js deleted file mode 100644 index ee54d6e5..00000000 --- a/doxygen/classSUAVE_1_1Attributes_1_1Liquids_1_1Water_1_1Water.js +++ /dev/null @@ -1,10 +0,0 @@ -var classSUAVE_1_1Attributes_1_1Liquids_1_1Water_1_1Water = -[ - [ "__defaults__", "classSUAVE_1_1Attributes_1_1Liquids_1_1Water_1_1Water.html#a26e34166234e5e4e859b1518457236f6", null ], - [ "compute_absolute_viscosity", "classSUAVE_1_1Attributes_1_1Liquids_1_1Water_1_1Water.html#afed25d8331b81ad9da36630f1c9ce0d8", null ], - [ "compute_cp", "classSUAVE_1_1Attributes_1_1Liquids_1_1Water_1_1Water.html#a2f39eb3e6e84ed4134aa572bccb21261", null ], - [ "boiling_point", "classSUAVE_1_1Attributes_1_1Liquids_1_1Water_1_1Water.html#a448bd07a86d29731585666cc182ec2eb", null ], - [ "density", "classSUAVE_1_1Attributes_1_1Liquids_1_1Water_1_1Water.html#ac5f6687060722912a9faa90a640913eb", null ], - [ "heat_of_vaporization", "classSUAVE_1_1Attributes_1_1Liquids_1_1Water_1_1Water.html#ae5986eb8fb5b5bef379c1ae53ac9c65b", null ], - [ "molecular_mass", "classSUAVE_1_1Attributes_1_1Liquids_1_1Water_1_1Water.html#a4121d521d9f3a398495d406c42c67348", null ] -]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Liquids_1_1Water_1_1Water.png b/doxygen/classSUAVE_1_1Attributes_1_1Liquids_1_1Water_1_1Water.png deleted file mode 100644 index a0501367..00000000 Binary files a/doxygen/classSUAVE_1_1Attributes_1_1Liquids_1_1Water_1_1Water.png and /dev/null differ diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Planets_1_1Earth_1_1Earth-members.html b/doxygen/classSUAVE_1_1Attributes_1_1Planets_1_1Earth_1_1Earth-members.html index 03f367b1..caad6ce3 100644 --- a/doxygen/classSUAVE_1_1Attributes_1_1Planets_1_1Earth_1_1Earth-members.html +++ b/doxygen/classSUAVE_1_1Attributes_1_1Planets_1_1Earth_1_1Earth-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -111,7 +119,7 @@
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SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -107,19 +114,15 @@ SUAVE.Attributes.Planets.Planet.Planet SUAVE.Attributes.Constants.Constant.Constant - -
+ + - - - - - - + +

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Attributes.Planets.Planet.Planet
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Attributes.Constants.Constant.Constant
def __defaults__ (self)
 
def compute_gravity (self, H=0.0)
 
@@ -187,6 +190,50 @@

SUAVE.Attributes.Planets.Planet.Planet.

+ + + + +

◆ compute_gravity()

+ +
+
+

Public Attributes

+ + + + + + + + + + + + + + + + + +
def SUAVE.Attributes.Planets.Earth.Earth.compute_gravity ( self,
 H = 0.0 
)
+
+
Compute the gravitational acceleration at altitude
+    
+Assumptions:      
+
+Source:
+
+Inputs:
+H     [m] (Altitude)
+
+Outputs:
+g     [m/(s^2)] (Gravity)
+
 Properties Used:
 None
 
@@ -203,7 +250,7 @@

SUAVE + doxygen 1.8.15

diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Planets_1_1Earth_1_1Earth.js b/doxygen/classSUAVE_1_1Attributes_1_1Planets_1_1Earth_1_1Earth.js index bc1b22cd..cee9287c 100644 --- a/doxygen/classSUAVE_1_1Attributes_1_1Planets_1_1Earth_1_1Earth.js +++ b/doxygen/classSUAVE_1_1Attributes_1_1Planets_1_1Earth_1_1Earth.js @@ -1,6 +1,7 @@ var classSUAVE_1_1Attributes_1_1Planets_1_1Earth_1_1Earth = [ [ "__defaults__", "classSUAVE_1_1Attributes_1_1Planets_1_1Earth_1_1Earth.html#af9d701e61dcaa8db64215d233dbab41e", null ], + [ "compute_gravity", "classSUAVE_1_1Attributes_1_1Planets_1_1Earth_1_1Earth.html#a5b855aafeb2f8305e1c40dba7347a529", null ], [ "HitchHikersGuide", "classSUAVE_1_1Attributes_1_1Planets_1_1Earth_1_1Earth.html#ab7c1fd327fdcc282f3c074679ac7b4f5", null ], [ "mass", "classSUAVE_1_1Attributes_1_1Planets_1_1Earth_1_1Earth.html#ab153ac9436b492099517ed685efcddbf", null ], [ "mean_radius", "classSUAVE_1_1Attributes_1_1Planets_1_1Earth_1_1Earth.html#a6f45b05a9497a24d54cf3f11c1d0aeba", null ], diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Planets_1_1Mars_1_1Mars-members.html b/doxygen/classSUAVE_1_1Attributes_1_1Planets_1_1Mars_1_1Mars-members.html deleted file mode 100644 index 9bc39744..00000000 --- a/doxygen/classSUAVE_1_1Attributes_1_1Planets_1_1Mars_1_1Mars-members.html +++ /dev/null @@ -1,116 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.1.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Attributes.Planets.Mars.Mars Member List
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SUAVE.Attributes.Planets.Mars.Mars Class Reference
-
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-Inheritance diagram for SUAVE.Attributes.Planets.Mars.Mars:
-
-
- - -SUAVE.Attributes.Planets.Planet.Planet -SUAVE.Attributes.Constants.Constant.Constant - -
- - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Attributes.Planets.Planet.Planet
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Attributes.Constants.Constant.Constant
def __defaults__ (self)
 
- - - - - - - - - - - - - - -

-Public Attributes

mass
 
mean_radius
 
sea_level_gravity
 
- Public Attributes inherited from SUAVE.Attributes.Planets.Planet.Planet
mass
 
mean_radius
 
sea_level_gravity
 
-

Detailed Description

-
Holds constants for Earth
-
-Assumptions:
-None
-
-Source:
-None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Attributes.Planets.Mars.Mars.__defaults__ ( self)
-
-
This sets the default values.
-
-Assumptions:
-None
-
-Source:
-Values commonly available
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Attributes/Planets/Mars.py
  • -
-
-
- - - - diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Planets_1_1Mars_1_1Mars.js b/doxygen/classSUAVE_1_1Attributes_1_1Planets_1_1Mars_1_1Mars.js deleted file mode 100644 index c1341386..00000000 --- a/doxygen/classSUAVE_1_1Attributes_1_1Planets_1_1Mars_1_1Mars.js +++ /dev/null @@ -1,7 +0,0 @@ -var classSUAVE_1_1Attributes_1_1Planets_1_1Mars_1_1Mars = -[ - [ "__defaults__", "classSUAVE_1_1Attributes_1_1Planets_1_1Mars_1_1Mars.html#a6a69df61b3f4613a5bb317eafe141525", null ], - [ "mass", "classSUAVE_1_1Attributes_1_1Planets_1_1Mars_1_1Mars.html#a86e73c31eea6ce54a0ac517234181eff", null ], - [ "mean_radius", "classSUAVE_1_1Attributes_1_1Planets_1_1Mars_1_1Mars.html#a843cbafebe8b18e69b4cc8d8590bd69b", null ], - [ "sea_level_gravity", "classSUAVE_1_1Attributes_1_1Planets_1_1Mars_1_1Mars.html#aa4c5f4ccd0aa0f3e036b016dcb48917a", null ] -]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Planets_1_1Mars_1_1Mars.png b/doxygen/classSUAVE_1_1Attributes_1_1Planets_1_1Mars_1_1Mars.png deleted file mode 100644 index 02d77db5..00000000 Binary files a/doxygen/classSUAVE_1_1Attributes_1_1Planets_1_1Mars_1_1Mars.png and /dev/null differ diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Planets_1_1Planet_1_1Planet-members.html b/doxygen/classSUAVE_1_1Attributes_1_1Planets_1_1Planet_1_1Planet-members.html index aae8d429..abde3099 100644 --- a/doxygen/classSUAVE_1_1Attributes_1_1Planets_1_1Planet_1_1Planet-members.html +++ b/doxygen/classSUAVE_1_1Attributes_1_1Planets_1_1Planet_1_1Planet-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -109,7 +116,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Planets_1_1Planet_1_1Planet.html b/doxygen/classSUAVE_1_1Attributes_1_1Planets_1_1Planet_1_1Planet.html index fa93bf56..8399a97e 100644 --- a/doxygen/classSUAVE_1_1Attributes_1_1Planets_1_1Planet_1_1Planet.html +++ b/doxygen/classSUAVE_1_1Attributes_1_1Planets_1_1Planet_1_1Planet.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Attributes.Planets.Planet.Planet Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -105,19 +112,15 @@
-SUAVE.Attributes.Constants.Constant.Constant +SUAVE.Attributes.Constants.Constant.Constant SUAVE.Attributes.Planets.Earth.Earth -SUAVE.Attributes.Planets.Mars.Mars - -
+ + - - -

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Attributes.Constants.Constant.Constant
def __defaults__ (self)
 
@@ -172,6 +175,10 @@

SUAVE.Attributes.Constants.Constant.Constant.

+ +

Reimplemented in SUAVE.Attributes.Planets.Earth.Earth.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Planets_1_1Planet_1_1Planet.png b/doxygen/classSUAVE_1_1Attributes_1_1Planets_1_1Planet_1_1Planet.png index 759855b7..848ffc8a 100644 Binary files a/doxygen/classSUAVE_1_1Attributes_1_1Planets_1_1Planet_1_1Planet.png and b/doxygen/classSUAVE_1_1Attributes_1_1Planets_1_1Planet_1_1Planet.png differ diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Aviation__Gasoline_1_1Aviation__Gasoline-members.html b/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Aviation__Gasoline_1_1Aviation__Gasoline-members.html index 814bc910..15b0a469 100644 --- a/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Aviation__Gasoline_1_1Aviation__Gasoline-members.html +++ b/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Aviation__Gasoline_1_1Aviation__Gasoline-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Attributes

SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -113,7 +120,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Aviation__Gasoline_1_1Aviation__Gasoline.html b/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Aviation__Gasoline_1_1Aviation__Gasoline.html index 3cbff4aa..587b0b60 100644 --- a/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Aviation__Gasoline_1_1Aviation__Gasoline.html +++ b/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Aviation__Gasoline_1_1Aviation__Gasoline.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Attributes.Propellants.Aviation_Gasoline.Aviation_Gasoline Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -106,16 +113,13 @@ SUAVE.Attributes.Propellants.Propellant.Propellant - -
+ + - - -

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Attributes.Propellants.Propellant.Propellant
def __defaults__ (self)
 
@@ -192,6 +196,8 @@

SUAVE.Attributes.Propellants.Propellant.Propellant.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Gaseous__H2_1_1Gaseous__H2-members.html b/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Gaseous__H2_1_1Gaseous__H2-members.html index 5f68bca2..7860472d 100644 --- a/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Gaseous__H2_1_1Gaseous__H2-members.html +++ b/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Gaseous__H2_1_1Gaseous__H2-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Attributes

SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -119,7 +126,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Gaseous__H2_1_1Gaseous__H2.html b/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Gaseous__H2_1_1Gaseous__H2.html index 9d602f5d..84371617 100644 --- a/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Gaseous__H2_1_1Gaseous__H2.html +++ b/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Gaseous__H2_1_1Gaseous__H2.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Attributes.Propellants.Gaseous_H2.Gaseous_H2 Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -106,16 +113,13 @@ SUAVE.Attributes.Propellants.Propellant.Propellant - -
+ + - - -

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Attributes.Propellants.Propellant.Propellant
def __defaults__ (self)
 
@@ -219,6 +223,8 @@

SUAVE.Attributes.Propellants.Propellant.Propellant.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1JP7_1_1JP7-members.html b/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1JP7_1_1JP7-members.html new file mode 100644 index 00000000..3c23e9c7 --- /dev/null +++ b/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1JP7_1_1JP7-members.html @@ -0,0 +1,128 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+

Public Attributes

+ + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+ + + + + +
+ +
+
+
+ + + + + + diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1JP7_1_1JP7.html b/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1JP7_1_1JP7.html new file mode 100644 index 00000000..fb7f336f --- /dev/null +++ b/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1JP7_1_1JP7.html @@ -0,0 +1,228 @@ + + + + + + + +SUAVE: SUAVE.Attributes.Propellants.JP7.JP7 Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Attributes.Propellants.JP7.JP7 Class Reference
+
+
+
+Inheritance diagram for SUAVE.Attributes.Propellants.JP7.JP7:
+
+
+ + +SUAVE.Attributes.Propellants.Propellant.Propellant + +
+ + + + +

+Public Member Functions

def __defaults__ (self)
 
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Attributes

tag
 
reactant
 
density
 
specific_energy
 
energy_density
 
stoichiometric_fuel_to_air
 
- Public Attributes inherited from SUAVE.Attributes.Propellants.Propellant.Propellant
tag
 
reactant
 
density
 
specific_energy
 
energy_density
 
max_mass_fraction
 
temperatures
 
+

Detailed Description

+
Holds values for this propellant
+
+Assumptions:
+None
+
+Source:
+None
+

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Attributes.Propellants.JP7.JP7.__defaults__ ( self)
+
+
This sets the default values.
+
+Assumptions:
+None
+
+Source:
+Values commonly available
+http://arc.uta.edu/publications/td_files/Kristen%20Roberts%20MS.pdf
+
+Inputs:
+None
+
+Outputs:
+None
+
+Properties Used:
+None
+
+

Reimplemented from SUAVE.Attributes.Propellants.Propellant.Propellant.

+ +
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Attributes/Propellants/JP7.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1JP7_1_1JP7.js b/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1JP7_1_1JP7.js new file mode 100644 index 00000000..8a1125d9 --- /dev/null +++ b/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1JP7_1_1JP7.js @@ -0,0 +1,10 @@ +var classSUAVE_1_1Attributes_1_1Propellants_1_1JP7_1_1JP7 = +[ + [ "__defaults__", "classSUAVE_1_1Attributes_1_1Propellants_1_1JP7_1_1JP7.html#ad0757efe06736068c77790cf606e7806", null ], + [ "density", "classSUAVE_1_1Attributes_1_1Propellants_1_1JP7_1_1JP7.html#a82cc774dc3186add2b9f40e444e6ffa0", null ], + [ "energy_density", "classSUAVE_1_1Attributes_1_1Propellants_1_1JP7_1_1JP7.html#a2ccbd01e00dd169116a7c4abaa8f0bdb", null ], + [ "reactant", "classSUAVE_1_1Attributes_1_1Propellants_1_1JP7_1_1JP7.html#aa3130d12915d5e62564bac7c714ca499", null ], + [ "specific_energy", "classSUAVE_1_1Attributes_1_1Propellants_1_1JP7_1_1JP7.html#af937b3ceb9aef35bb5013fd3515c80bf", null ], + [ "stoichiometric_fuel_to_air", "classSUAVE_1_1Attributes_1_1Propellants_1_1JP7_1_1JP7.html#a5cca8d3bc78b3b254fcbb02db2b82d5c", null ], + [ "tag", "classSUAVE_1_1Attributes_1_1Propellants_1_1JP7_1_1JP7.html#a6d6350825080116292c1f19d1dc8a908", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1JP7_1_1JP7.png b/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1JP7_1_1JP7.png new file mode 100644 index 00000000..9d276cbb Binary files /dev/null and b/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1JP7_1_1JP7.png differ diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Jet__A1_1_1Jet__A1-members.html b/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Jet__A1_1_1Jet__A1-members.html index 210ee02d..72deca78 100644 --- a/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Jet__A1_1_1Jet__A1-members.html +++ b/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Jet__A1_1_1Jet__A1-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -113,7 +120,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Jet__A1_1_1Jet__A1.html b/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Jet__A1_1_1Jet__A1.html index 3b4cc9d2..f5671973 100644 --- a/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Jet__A1_1_1Jet__A1.html +++ b/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Jet__A1_1_1Jet__A1.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Attributes.Propellants.Jet_A1.Jet_A1 Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -106,16 +113,13 @@ SUAVE.Attributes.Propellants.Propellant.Propellant - -
+ + - - -

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Attributes.Propellants.Propellant.Propellant
def __defaults__ (self)
 
@@ -201,6 +205,8 @@

SUAVE.Attributes.Propellants.Propellant.Propellant.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Jet__A_1_1Jet__A-members.html b/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Jet__A_1_1Jet__A-members.html index 5ccba693..105b2eb9 100644 --- a/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Jet__A_1_1Jet__A-members.html +++ b/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Jet__A_1_1Jet__A-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Attributes

SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -113,7 +120,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Jet__A_1_1Jet__A.html b/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Jet__A_1_1Jet__A.html index 66415f69..9f7bec53 100644 --- a/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Jet__A_1_1Jet__A.html +++ b/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Jet__A_1_1Jet__A.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Attributes.Propellants.Jet_A.Jet_A Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -106,16 +113,13 @@ SUAVE.Attributes.Propellants.Propellant.Propellant - -
+ + - - -

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Attributes.Propellants.Propellant.Propellant
def __defaults__ (self)
 
@@ -201,6 +205,8 @@

SUAVE.Attributes.Propellants.Propellant.Propellant.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1LOX__LH2_1_1LOX__LH2-members.html b/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1LOX__LH2_1_1LOX__LH2-members.html new file mode 100644 index 00000000..8c77a922 --- /dev/null +++ b/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1LOX__LH2_1_1LOX__LH2-members.html @@ -0,0 +1,131 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+

Public Attributes

+ + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+ + + + + +
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
SUAVE.Attributes.Propellants.LOX_LH2.LOX_LH2 Member List
+
+
+ +

This is the complete list of members for SUAVE.Attributes.Propellants.LOX_LH2.LOX_LH2, including all inherited members.

+ + + + + + + + + + + + + +
__defaults__(self)SUAVE.Attributes.Propellants.LOX_LH2.LOX_LH2
combustion_temperature (defined in SUAVE.Attributes.Propellants.LOX_LH2.LOX_LH2)SUAVE.Attributes.Propellants.LOX_LH2.LOX_LH2
density (defined in SUAVE.Attributes.Propellants.Propellant.Propellant)SUAVE.Attributes.Propellants.Propellant.Propellant
energy_density (defined in SUAVE.Attributes.Propellants.Propellant.Propellant)SUAVE.Attributes.Propellants.Propellant.Propellant
gas_specific_constant (defined in SUAVE.Attributes.Propellants.LOX_LH2.LOX_LH2)SUAVE.Attributes.Propellants.LOX_LH2.LOX_LH2
isentropic_expansion_factor (defined in SUAVE.Attributes.Propellants.LOX_LH2.LOX_LH2)SUAVE.Attributes.Propellants.LOX_LH2.LOX_LH2
max_mass_fraction (defined in SUAVE.Attributes.Propellants.Propellant.Propellant)SUAVE.Attributes.Propellants.Propellant.Propellant
molecular_weight (defined in SUAVE.Attributes.Propellants.LOX_LH2.LOX_LH2)SUAVE.Attributes.Propellants.LOX_LH2.LOX_LH2
reactant (defined in SUAVE.Attributes.Propellants.Propellant.Propellant)SUAVE.Attributes.Propellants.Propellant.Propellant
specific_energy (defined in SUAVE.Attributes.Propellants.Propellant.Propellant)SUAVE.Attributes.Propellants.Propellant.Propellant
tag (defined in SUAVE.Attributes.Propellants.LOX_LH2.LOX_LH2)SUAVE.Attributes.Propellants.LOX_LH2.LOX_LH2
temperatures (defined in SUAVE.Attributes.Propellants.Propellant.Propellant)SUAVE.Attributes.Propellants.Propellant.Propellant
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1LOX__LH2_1_1LOX__LH2.html b/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1LOX__LH2_1_1LOX__LH2.html new file mode 100644 index 00000000..f96f22c9 --- /dev/null +++ b/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1LOX__LH2_1_1LOX__LH2.html @@ -0,0 +1,226 @@ + + + + + + + +SUAVE: SUAVE.Attributes.Propellants.LOX_LH2.LOX_LH2 Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Attributes.Propellants.LOX_LH2.LOX_LH2 Class Reference
+
+
+
+Inheritance diagram for SUAVE.Attributes.Propellants.LOX_LH2.LOX_LH2:
+
+
+ + +SUAVE.Attributes.Propellants.Propellant.Propellant + +
+ + + + +

+Public Member Functions

def __defaults__ (self)
 
+ + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Attributes

tag
 
molecular_weight
 
isentropic_expansion_factor
 
combustion_temperature
 
gas_specific_constant
 
- Public Attributes inherited from SUAVE.Attributes.Propellants.Propellant.Propellant
tag
 
reactant
 
density
 
specific_energy
 
energy_density
 
max_mass_fraction
 
temperatures
 
+

Detailed Description

+
Holds values for this propellant
+
+Assumptions:
+At an O/F ratio 5.50
+
+
+Source:
+Sutton, Rocket Propulsion Elements
+Using CEA
+

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Attributes.Propellants.LOX_LH2.LOX_LH2.__defaults__ ( self)
+
+
This sets the default values.
+
+Assumptions:
+None
+
+Source:
+Values commonly available
+
+Inputs:
+None
+
+Outputs:
+None
+
+Properties Used:
+None
+
+

Reimplemented from SUAVE.Attributes.Propellants.Propellant.Propellant.

+ +
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Attributes/Propellants/LOX_LH2.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1LOX__LH2_1_1LOX__LH2.js b/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1LOX__LH2_1_1LOX__LH2.js new file mode 100644 index 00000000..d9bf6e60 --- /dev/null +++ b/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1LOX__LH2_1_1LOX__LH2.js @@ -0,0 +1,9 @@ +var classSUAVE_1_1Attributes_1_1Propellants_1_1LOX__LH2_1_1LOX__LH2 = +[ + [ "__defaults__", "classSUAVE_1_1Attributes_1_1Propellants_1_1LOX__LH2_1_1LOX__LH2.html#ae82e8e7a003e59288401d09673b34948", null ], + [ "combustion_temperature", "classSUAVE_1_1Attributes_1_1Propellants_1_1LOX__LH2_1_1LOX__LH2.html#a74d3078c28c6969a06f715dff6dc0b20", null ], + [ "gas_specific_constant", "classSUAVE_1_1Attributes_1_1Propellants_1_1LOX__LH2_1_1LOX__LH2.html#aef32d8df329a09635093454fc90e4e1a", null ], + [ "isentropic_expansion_factor", "classSUAVE_1_1Attributes_1_1Propellants_1_1LOX__LH2_1_1LOX__LH2.html#a98e00b09f11347a0054da3af2dcd350f", null ], + [ "molecular_weight", "classSUAVE_1_1Attributes_1_1Propellants_1_1LOX__LH2_1_1LOX__LH2.html#a7f0069642cdb7c6d5303c8c031240f16", null ], + [ "tag", "classSUAVE_1_1Attributes_1_1Propellants_1_1LOX__LH2_1_1LOX__LH2.html#a6b0f35b1b6071d7a2f8dcbb51af23833", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1LOX__LH2_1_1LOX__LH2.png b/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1LOX__LH2_1_1LOX__LH2.png new file mode 100644 index 00000000..01ed8735 Binary files /dev/null and b/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1LOX__LH2_1_1LOX__LH2.png differ diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1LOX__RP1_1_1LOX__RP1-members.html b/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1LOX__RP1_1_1LOX__RP1-members.html new file mode 100644 index 00000000..ca9a912a --- /dev/null +++ b/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1LOX__RP1_1_1LOX__RP1-members.html @@ -0,0 +1,131 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
SUAVE.Attributes.Propellants.LOX_RP1.LOX_RP1 Member List
+
+
+ +

This is the complete list of members for SUAVE.Attributes.Propellants.LOX_RP1.LOX_RP1, including all inherited members.

+ + + + + + + + + + + + + +
__defaults__(self)SUAVE.Attributes.Propellants.LOX_RP1.LOX_RP1
combustion_temperature (defined in SUAVE.Attributes.Propellants.LOX_RP1.LOX_RP1)SUAVE.Attributes.Propellants.LOX_RP1.LOX_RP1
density (defined in SUAVE.Attributes.Propellants.Propellant.Propellant)SUAVE.Attributes.Propellants.Propellant.Propellant
energy_density (defined in SUAVE.Attributes.Propellants.Propellant.Propellant)SUAVE.Attributes.Propellants.Propellant.Propellant
gas_specific_constant (defined in SUAVE.Attributes.Propellants.LOX_RP1.LOX_RP1)SUAVE.Attributes.Propellants.LOX_RP1.LOX_RP1
isentropic_expansion_factor (defined in SUAVE.Attributes.Propellants.LOX_RP1.LOX_RP1)SUAVE.Attributes.Propellants.LOX_RP1.LOX_RP1
max_mass_fraction (defined in SUAVE.Attributes.Propellants.Propellant.Propellant)SUAVE.Attributes.Propellants.Propellant.Propellant
molecular_weight (defined in SUAVE.Attributes.Propellants.LOX_RP1.LOX_RP1)SUAVE.Attributes.Propellants.LOX_RP1.LOX_RP1
reactant (defined in SUAVE.Attributes.Propellants.Propellant.Propellant)SUAVE.Attributes.Propellants.Propellant.Propellant
specific_energy (defined in SUAVE.Attributes.Propellants.Propellant.Propellant)SUAVE.Attributes.Propellants.Propellant.Propellant
tag (defined in SUAVE.Attributes.Propellants.LOX_RP1.LOX_RP1)SUAVE.Attributes.Propellants.LOX_RP1.LOX_RP1
temperatures (defined in SUAVE.Attributes.Propellants.Propellant.Propellant)SUAVE.Attributes.Propellants.Propellant.Propellant
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1LOX__RP1_1_1LOX__RP1.html b/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1LOX__RP1_1_1LOX__RP1.html new file mode 100644 index 00000000..0f1081a2 --- /dev/null +++ b/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1LOX__RP1_1_1LOX__RP1.html @@ -0,0 +1,225 @@ + + + + + + + +SUAVE: SUAVE.Attributes.Propellants.LOX_RP1.LOX_RP1 Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Attributes.Propellants.LOX_RP1.LOX_RP1 Class Reference
+
+
+
+Inheritance diagram for SUAVE.Attributes.Propellants.LOX_RP1.LOX_RP1:
+
+
+ + +SUAVE.Attributes.Propellants.Propellant.Propellant + +
+ + + + +

+Public Member Functions

def __defaults__ (self)
 
+ + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Attributes

tag
 
molecular_weight
 
isentropic_expansion_factor
 
combustion_temperature
 
gas_specific_constant
 
- Public Attributes inherited from SUAVE.Attributes.Propellants.Propellant.Propellant
tag
 
reactant
 
density
 
specific_energy
 
energy_density
 
max_mass_fraction
 
temperatures
 
+

Detailed Description

+
Holds values for this propellant
+
+Assumptions:
+At an O/F ratio 2.27
+
+
+Source:
+Sutton, Rocket Propulsion Elements
+

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Attributes.Propellants.LOX_RP1.LOX_RP1.__defaults__ ( self)
+
+
This sets the default values.
+
+Assumptions:
+None
+
+Source:
+Values commonly available
+
+Inputs:
+None
+
+Outputs:
+None
+
+Properties Used:
+None
+
+

Reimplemented from SUAVE.Attributes.Propellants.Propellant.Propellant.

+ +
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Attributes/Propellants/LOX_RP1.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1LOX__RP1_1_1LOX__RP1.js b/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1LOX__RP1_1_1LOX__RP1.js new file mode 100644 index 00000000..3fbd90a4 --- /dev/null +++ b/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1LOX__RP1_1_1LOX__RP1.js @@ -0,0 +1,9 @@ +var classSUAVE_1_1Attributes_1_1Propellants_1_1LOX__RP1_1_1LOX__RP1 = +[ + [ "__defaults__", "classSUAVE_1_1Attributes_1_1Propellants_1_1LOX__RP1_1_1LOX__RP1.html#a8f27620f062b1b056b6d7750a4ed395b", null ], + [ "combustion_temperature", "classSUAVE_1_1Attributes_1_1Propellants_1_1LOX__RP1_1_1LOX__RP1.html#a362b63a87e282adeacd33919e38dd4ee", null ], + [ "gas_specific_constant", "classSUAVE_1_1Attributes_1_1Propellants_1_1LOX__RP1_1_1LOX__RP1.html#aded36257ce4cd2fd1aca2be59b834b83", null ], + [ "isentropic_expansion_factor", "classSUAVE_1_1Attributes_1_1Propellants_1_1LOX__RP1_1_1LOX__RP1.html#a6af2a390885f93458ad523ced7239c27", null ], + [ "molecular_weight", "classSUAVE_1_1Attributes_1_1Propellants_1_1LOX__RP1_1_1LOX__RP1.html#a1505aaa1e9ac08658568a54fb9a8d011", null ], + [ "tag", "classSUAVE_1_1Attributes_1_1Propellants_1_1LOX__RP1_1_1LOX__RP1.html#a61ee6fe740a00ac16d92452c500616b8", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1LOX__RP1_1_1LOX__RP1.png b/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1LOX__RP1_1_1LOX__RP1.png new file mode 100644 index 00000000..b74976ac Binary files /dev/null and b/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1LOX__RP1_1_1LOX__RP1.png differ diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Liquid__H2_1_1Liquid__H2-members.html b/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Liquid__H2_1_1Liquid__H2-members.html similarity index 77% rename from _site/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Liquid__H2_1_1Liquid__H2-members.html rename to doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Liquid__H2_1_1Liquid__H2-members.html index c0eba360..2c7958b2 100644 --- a/_site/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Liquid__H2_1_1Liquid__H2-members.html +++ b/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Liquid__H2_1_1Liquid__H2-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.0.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -113,7 +121,7 @@
    + doxygen 1.8.15
diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Liquid__H2_1_1Liquid__H2.html b/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Liquid__H2_1_1Liquid__H2.html similarity index 90% rename from _site/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Liquid__H2_1_1Liquid__H2.html rename to doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Liquid__H2_1_1Liquid__H2.html index 77f7ff90..cbd27a87 100644 --- a/_site/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Liquid__H2_1_1Liquid__H2.html +++ b/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Liquid__H2_1_1Liquid__H2.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Attributes.Propellants.Liquid_H2.Liquid_H2 Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.0.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -106,16 +113,13 @@ SUAVE.Attributes.Propellants.Propellant.Propellant - -
+ + - - -

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Attributes.Propellants.Propellant.Propellant
def __defaults__ (self)
 
@@ -134,6 +138,9 @@ + + @@ -188,6 +195,7 @@

SUAVE.Attributes.Propellants.Propellant.Propellant.

+
The documentation for this class was generated from the following file:
    -
  • /home/tim/Documents/SUAVE/trunk/SUAVE/Attributes/Propellants/Liquid_H2.py
  • +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Attributes/Propellants/Liquid_H2.py
@@ -211,7 +221,7 @@

SUAVE + doxygen 1.8.15 diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Liquid__H2_1_1Liquid__H2.js b/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Liquid__H2_1_1Liquid__H2.js similarity index 85% rename from _site/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Liquid__H2_1_1Liquid__H2.js rename to doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Liquid__H2_1_1Liquid__H2.js index 76e744a3..5aca3025 100644 --- a/_site/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Liquid__H2_1_1Liquid__H2.js +++ b/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Liquid__H2_1_1Liquid__H2.js @@ -5,5 +5,6 @@ var classSUAVE_1_1Attributes_1_1Propellants_1_1Liquid__H2_1_1Liquid__H2 = [ "energy_density", "classSUAVE_1_1Attributes_1_1Propellants_1_1Liquid__H2_1_1Liquid__H2.html#a3721d9c07826ab7617a0755078a0fef3", null ], [ "reactant", "classSUAVE_1_1Attributes_1_1Propellants_1_1Liquid__H2_1_1Liquid__H2.html#a595763fd177b028276ebe8dca0529c50", null ], [ "specific_energy", "classSUAVE_1_1Attributes_1_1Propellants_1_1Liquid__H2_1_1Liquid__H2.html#a0f4a5fad35d915b576b584c18077ff23", null ], + [ "stoichiometric_fuel_to_air", "classSUAVE_1_1Attributes_1_1Propellants_1_1Liquid__H2_1_1Liquid__H2.html#acd677a9fedbcc6546be500b389578d18", null ], [ "tag", "classSUAVE_1_1Attributes_1_1Propellants_1_1Liquid__H2_1_1Liquid__H2.html#a23fdac9fe8cf1bd831ff54039de65266", null ] ]; \ No newline at end of file diff --git a/_site/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Liquid__H2_1_1Liquid__H2.png b/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Liquid__H2_1_1Liquid__H2.png similarity index 100% rename from _site/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Liquid__H2_1_1Liquid__H2.png rename to doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Liquid__H2_1_1Liquid__H2.png diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Liquid__Natural__Gas_1_1Liquid__Natural__Gas-members.html b/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Liquid__Natural__Gas_1_1Liquid__Natural__Gas-members.html index 6b25dd27..455d2b5d 100644 --- a/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Liquid__Natural__Gas_1_1Liquid__Natural__Gas-members.html +++ b/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Liquid__Natural__Gas_1_1Liquid__Natural__Gas-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Attributes

 energy_density
 
stoichiometric_fuel_to_air
 
- Public Attributes inherited from SUAVE.Attributes.Propellants.Propellant.Propellant
 tag
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -113,7 +120,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Liquid__Natural__Gas_1_1Liquid__Natural__Gas.html b/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Liquid__Natural__Gas_1_1Liquid__Natural__Gas.html index f490b166..e980ed1b 100644 --- a/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Liquid__Natural__Gas_1_1Liquid__Natural__Gas.html +++ b/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Liquid__Natural__Gas_1_1Liquid__Natural__Gas.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Attributes.Propellants.Liquid_Natural_Gas.Liquid_Natural_Gas Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -106,16 +113,13 @@ SUAVE.Attributes.Propellants.Propellant.Propellant - -
+ + - - -

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Attributes.Propellants.Propellant.Propellant
def __defaults__ (self)
 
@@ -198,6 +202,8 @@

SUAVE.Attributes.Propellants.Propellant.Propellant.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Propellant_1_1Propellant-members.html b/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Propellant_1_1Propellant-members.html index d223728a..3010be5c 100644 --- a/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Propellant_1_1Propellant-members.html +++ b/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Propellant_1_1Propellant-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Attributes

SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -113,7 +120,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Propellant_1_1Propellant.html b/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Propellant_1_1Propellant.html index 27cb6dbb..15f89602 100644 --- a/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Propellant_1_1Propellant.html +++ b/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Propellant_1_1Propellant.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Attributes.Propellants.Propellant.Propellant Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -105,13 +112,17 @@
-SUAVE.Attributes.Propellants.Aviation_Gasoline.Aviation_Gasoline -SUAVE.Attributes.Propellants.Gaseous_H2.Gaseous_H2 -SUAVE.Attributes.Propellants.Jet_A1.Jet_A1 -SUAVE.Attributes.Propellants.Jet_A.Jet_A -SUAVE.Attributes.Propellants.Liquid_Natural_Gas.Liquid_Natural_Gas - -
+SUAVE.Attributes.Propellants.Aviation_Gasoline.Aviation_Gasoline +SUAVE.Attributes.Propellants.Gaseous_H2.Gaseous_H2 +SUAVE.Attributes.Propellants.Jet_A1.Jet_A1 +SUAVE.Attributes.Propellants.Jet_A.Jet_A +SUAVE.Attributes.Propellants.JP7.JP7 +SUAVE.Attributes.Propellants.Liquid_H2.Liquid_H2 +SUAVE.Attributes.Propellants.Liquid_Natural_Gas.Liquid_Natural_Gas +SUAVE.Attributes.Propellants.LOX_LH2.LOX_LH2 +SUAVE.Attributes.Propellants.LOX_RP1.LOX_RP1 + + @@ -183,6 +194,8 @@

SUAVE.Attributes.Propellants.LOX_LH2.LOX_LH2, SUAVE.Attributes.Propellants.Jet_A.Jet_A, SUAVE.Attributes.Propellants.Jet_A1.Jet_A1, SUAVE.Attributes.Propellants.Liquid_H2.Liquid_H2, SUAVE.Attributes.Propellants.LOX_RP1.LOX_RP1, SUAVE.Attributes.Propellants.Aviation_Gasoline.Aviation_Gasoline, SUAVE.Attributes.Propellants.Gaseous_H2.Gaseous_H2, SUAVE.Attributes.Propellants.JP7.JP7, and SUAVE.Attributes.Propellants.Liquid_Natural_Gas.Liquid_Natural_Gas.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Propellant_1_1Propellant.png b/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Propellant_1_1Propellant.png index 54805770..2a54784c 100644 Binary files a/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Propellant_1_1Propellant.png and b/doxygen/classSUAVE_1_1Attributes_1_1Propellants_1_1Propellant_1_1Propellant.png differ diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Acrylic_1_1Acrylic-members.html b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Acrylic_1_1Acrylic-members.html new file mode 100644 index 00000000..3c904ee5 --- /dev/null +++ b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Acrylic_1_1Acrylic-members.html @@ -0,0 +1,128 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+

Public Member Functions

+ + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+ + + + + +
+ +
+
+
+ + + + + + diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Acrylic_1_1Acrylic.html b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Acrylic_1_1Acrylic.html new file mode 100644 index 00000000..19102b9b --- /dev/null +++ b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Acrylic_1_1Acrylic.html @@ -0,0 +1,245 @@ + + + + + + + +SUAVE: SUAVE.Attributes.Solids.Acrylic.Acrylic Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Attributes.Solids.Acrylic.Acrylic Class Reference
+
+
+
+Inheritance diagram for SUAVE.Attributes.Solids.Acrylic.Acrylic:
+
+
+ + +SUAVE.Attributes.Solids.Solid.Solid + +
+ + + + +

+Public Member Functions

def __defaults__ (self)
 
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Attributes

ultimate_tensile_strength
 
ultimate_shear_strength
 
ultimate_bearing_strength
 
yield_tensile_strength
 
yield_shear_strength
 
yield_bearing_strength
 
minimum_gage_thickness
 
density
 
- Public Attributes inherited from SUAVE.Attributes.Solids.Solid.Solid
ultimate_tensile_strength
 
ultimate_shear_strength
 
ultimate_bearing_strength
 
yield_tensile_strength
 
yield_shear_strength
 
yield_bearing_strength
 
minimum_gage_thickness
 
density
 
+

Detailed Description

+
Physical Constants Specific to Polymethyl Methacrylate
+
+Assumptions:
+None
+
+Source:
+MatWeb (Median of Mfg. Reported Values)
+
+Inputs:
+N/A
+
+Outputs:
+N/A
+
+Properties Used:
+None
+

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Attributes.Solids.Acrylic.Acrylic.__defaults__ ( self)
+
+
Sets material properties at instantiation.
+
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+N/A
+
+Outputs:
+N/A
+
+Properties Used:
+None
+
+

Reimplemented from SUAVE.Attributes.Solids.Solid.Solid.

+ +
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Attributes/Solids/Acrylic.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Acrylic_1_1Acrylic.js b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Acrylic_1_1Acrylic.js new file mode 100644 index 00000000..60395485 --- /dev/null +++ b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Acrylic_1_1Acrylic.js @@ -0,0 +1,12 @@ +var classSUAVE_1_1Attributes_1_1Solids_1_1Acrylic_1_1Acrylic = +[ + [ "__defaults__", "classSUAVE_1_1Attributes_1_1Solids_1_1Acrylic_1_1Acrylic.html#a6ff998c78ddeec2d5a729319d66b819d", null ], + [ "density", "classSUAVE_1_1Attributes_1_1Solids_1_1Acrylic_1_1Acrylic.html#a0c464f0043aeab56718fb69a2fae82f7", null ], + [ "minimum_gage_thickness", "classSUAVE_1_1Attributes_1_1Solids_1_1Acrylic_1_1Acrylic.html#a93b3c08da317c2913e779bbb14012539", null ], + [ "ultimate_bearing_strength", "classSUAVE_1_1Attributes_1_1Solids_1_1Acrylic_1_1Acrylic.html#a8ef918c1d1fca10bd5ffb7159e68aa4b", null ], + [ "ultimate_shear_strength", "classSUAVE_1_1Attributes_1_1Solids_1_1Acrylic_1_1Acrylic.html#af9b6a826fa424252ee3a26a5bcfbc481", null ], + [ "ultimate_tensile_strength", "classSUAVE_1_1Attributes_1_1Solids_1_1Acrylic_1_1Acrylic.html#ab96dbe2f05f99c5cec5ee879231635fa", null ], + [ "yield_bearing_strength", "classSUAVE_1_1Attributes_1_1Solids_1_1Acrylic_1_1Acrylic.html#aca4cf50f9ed7d0f3936fc8244b620594", null ], + [ "yield_shear_strength", "classSUAVE_1_1Attributes_1_1Solids_1_1Acrylic_1_1Acrylic.html#a78854907c6fb91e6787eff55277a7833", null ], + [ "yield_tensile_strength", "classSUAVE_1_1Attributes_1_1Solids_1_1Acrylic_1_1Acrylic.html#adf745b79faeed0535bcbca4e2ce8859d", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Acrylic_1_1Acrylic.png b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Acrylic_1_1Acrylic.png new file mode 100644 index 00000000..08c0f9fa Binary files /dev/null and b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Acrylic_1_1Acrylic.png differ diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Aluminum_1_1Aluminum-members.html b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Aluminum_1_1Aluminum-members.html new file mode 100644 index 00000000..71401ddb --- /dev/null +++ b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Aluminum_1_1Aluminum-members.html @@ -0,0 +1,128 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ + + + + + diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Aluminum_1_1Aluminum.html b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Aluminum_1_1Aluminum.html new file mode 100644 index 00000000..62dac4d8 --- /dev/null +++ b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Aluminum_1_1Aluminum.html @@ -0,0 +1,248 @@ + + + + + + + +SUAVE: SUAVE.Attributes.Solids.Aluminum.Aluminum Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Attributes.Solids.Aluminum.Aluminum Class Reference
+
+
+
+Inheritance diagram for SUAVE.Attributes.Solids.Aluminum.Aluminum:
+
+
+ + +SUAVE.Attributes.Solids.Solid.Solid +SUAVE.Attributes.Solids.Aluminum_Rib.Aluminum_Rib + +
+ + + + +

+Public Member Functions

def __defaults__ (self)
 
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Attributes

ultimate_tensile_strength
 
ultimate_shear_strength
 
ultimate_bearing_strength
 
yield_tensile_strength
 
yield_shear_strength
 
yield_bearing_strength
 
minimum_gage_thickness
 
density
 
- Public Attributes inherited from SUAVE.Attributes.Solids.Solid.Solid
ultimate_tensile_strength
 
ultimate_shear_strength
 
ultimate_bearing_strength
 
yield_tensile_strength
 
yield_shear_strength
 
yield_bearing_strength
 
minimum_gage_thickness
 
density
 
+

Detailed Description

+
Physical Constants Specific to 6061-T6 Aluminum
+
+Assumptions:
+None
+
+Source:
+MatWeb (Median of Mfg. Reported Values)
+
+Inputs:
+N/A
+
+Outputs:
+N/A
+
+Properties Used:
+None
+

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Attributes.Solids.Aluminum.Aluminum.__defaults__ ( self)
+
+
Sets material properties at instantiation.
+
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+N/A
+
+Outputs:
+N/A
+
+Properties Used:
+None
+
+

Reimplemented from SUAVE.Attributes.Solids.Solid.Solid.

+ +

Reimplemented in SUAVE.Attributes.Solids.Aluminum_Rib.Aluminum_Rib.

+ +
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Attributes/Solids/Aluminum.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Aluminum_1_1Aluminum.js b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Aluminum_1_1Aluminum.js new file mode 100644 index 00000000..5b94c3f4 --- /dev/null +++ b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Aluminum_1_1Aluminum.js @@ -0,0 +1,12 @@ +var classSUAVE_1_1Attributes_1_1Solids_1_1Aluminum_1_1Aluminum = +[ + [ "__defaults__", "classSUAVE_1_1Attributes_1_1Solids_1_1Aluminum_1_1Aluminum.html#a349fa9ae86a7a7830a178078b8cc7937", null ], + [ "density", "classSUAVE_1_1Attributes_1_1Solids_1_1Aluminum_1_1Aluminum.html#a1b39718875a1cd9675010e4b2c4fe47c", null ], + [ "minimum_gage_thickness", "classSUAVE_1_1Attributes_1_1Solids_1_1Aluminum_1_1Aluminum.html#ae36bd38d7c980bf89ed1d23f273761bd", null ], + [ "ultimate_bearing_strength", "classSUAVE_1_1Attributes_1_1Solids_1_1Aluminum_1_1Aluminum.html#a823c5489248e947282a2c5a39962a9a9", null ], + [ "ultimate_shear_strength", "classSUAVE_1_1Attributes_1_1Solids_1_1Aluminum_1_1Aluminum.html#a0661718ff5b9903e816b3b9ca12880c9", null ], + [ "ultimate_tensile_strength", "classSUAVE_1_1Attributes_1_1Solids_1_1Aluminum_1_1Aluminum.html#a5daeff62f51e23e2ab7c973bac51f9b7", null ], + [ "yield_bearing_strength", "classSUAVE_1_1Attributes_1_1Solids_1_1Aluminum_1_1Aluminum.html#a96db694dedc9b9fb3c0cf9924e7f06fb", null ], + [ "yield_shear_strength", "classSUAVE_1_1Attributes_1_1Solids_1_1Aluminum_1_1Aluminum.html#af4a716c9cdc669eb6be1059dfe65959f", null ], + [ "yield_tensile_strength", "classSUAVE_1_1Attributes_1_1Solids_1_1Aluminum_1_1Aluminum.html#a7b0645247730b0b4b973b30cc918977e", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Aluminum_1_1Aluminum.png b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Aluminum_1_1Aluminum.png new file mode 100644 index 00000000..f7372569 Binary files /dev/null and b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Aluminum_1_1Aluminum.png differ diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Aluminum__Rib_1_1Aluminum__Rib-members.html b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Aluminum__Rib_1_1Aluminum__Rib-members.html new file mode 100644 index 00000000..c216b34a --- /dev/null +++ b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Aluminum__Rib_1_1Aluminum__Rib-members.html @@ -0,0 +1,129 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ + + + + + diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Aluminum__Rib_1_1Aluminum__Rib.html b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Aluminum__Rib_1_1Aluminum__Rib.html new file mode 100644 index 00000000..7c68810e --- /dev/null +++ b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Aluminum__Rib_1_1Aluminum__Rib.html @@ -0,0 +1,253 @@ + + + + + + + +SUAVE: SUAVE.Attributes.Solids.Aluminum_Rib.Aluminum_Rib Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Attributes.Solids.Aluminum_Rib.Aluminum_Rib Class Reference
+
+
+
+Inheritance diagram for SUAVE.Attributes.Solids.Aluminum_Rib.Aluminum_Rib:
+
+
+ + +SUAVE.Attributes.Solids.Aluminum.Aluminum +SUAVE.Attributes.Solids.Solid.Solid + +
+ + + + +

+Public Member Functions

def __defaults__ (self)
 
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Attributes

minimum_gage_thickness
 
minimum_width
 
- Public Attributes inherited from SUAVE.Attributes.Solids.Aluminum.Aluminum
ultimate_tensile_strength
 
ultimate_shear_strength
 
ultimate_bearing_strength
 
yield_tensile_strength
 
yield_shear_strength
 
yield_bearing_strength
 
minimum_gage_thickness
 
density
 
- Public Attributes inherited from SUAVE.Attributes.Solids.Solid.Solid
ultimate_tensile_strength
 
ultimate_shear_strength
 
ultimate_bearing_strength
 
yield_tensile_strength
 
yield_shear_strength
 
yield_bearing_strength
 
minimum_gage_thickness
 
density
 
+

Detailed Description

+
Physical Constants Specific to 6061-T6 Aluminum Ribs
+
+Assumptions:
+Limit of machining capability for precision components
+
+Source:
+None
+
+Inputs:
+N/A
+
+Outputs:
+N/A
+
+Properties Used:
+None
+

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Attributes.Solids.Aluminum_Rib.Aluminum_Rib.__defaults__ ( self)
+
+
Sets material properties at instantiation.
+
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+N/A
+
+Outputs:
+N/A
+
+Properties Used:
+None
+
+

Reimplemented from SUAVE.Attributes.Solids.Aluminum.Aluminum.

+ +
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Attributes/Solids/Aluminum_Rib.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Aluminum__Rib_1_1Aluminum__Rib.js b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Aluminum__Rib_1_1Aluminum__Rib.js new file mode 100644 index 00000000..b7327a1b --- /dev/null +++ b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Aluminum__Rib_1_1Aluminum__Rib.js @@ -0,0 +1,6 @@ +var classSUAVE_1_1Attributes_1_1Solids_1_1Aluminum__Rib_1_1Aluminum__Rib = +[ + [ "__defaults__", "classSUAVE_1_1Attributes_1_1Solids_1_1Aluminum__Rib_1_1Aluminum__Rib.html#ad3e8bd5238d5f439d9374882a8409ee4", null ], + [ "minimum_gage_thickness", "classSUAVE_1_1Attributes_1_1Solids_1_1Aluminum__Rib_1_1Aluminum__Rib.html#aae2a5e192ea053d295e699e9d07e121f", null ], + [ "minimum_width", "classSUAVE_1_1Attributes_1_1Solids_1_1Aluminum__Rib_1_1Aluminum__Rib.html#ac0dbe30411a0116dcf8518d4bfd46bae", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Aluminum__Rib_1_1Aluminum__Rib.png b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Aluminum__Rib_1_1Aluminum__Rib.png new file mode 100644 index 00000000..4d086720 Binary files /dev/null and b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Aluminum__Rib_1_1Aluminum__Rib.png differ diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Bidirectional__Carbon__Fiber_1_1Bidirectional__Carbon__Fiber-members.html b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Bidirectional__Carbon__Fiber_1_1Bidirectional__Carbon__Fiber-members.html new file mode 100644 index 00000000..0b487ef6 --- /dev/null +++ b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Bidirectional__Carbon__Fiber_1_1Bidirectional__Carbon__Fiber-members.html @@ -0,0 +1,128 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
SUAVE.Attributes.Solids.Bidirectional_Carbon_Fiber.Bidirectional_Carbon_Fiber Member List
+
+
+ +

This is the complete list of members for SUAVE.Attributes.Solids.Bidirectional_Carbon_Fiber.Bidirectional_Carbon_Fiber, including all inherited members.

+ + + + + + + + + + +
__defaults__(self)SUAVE.Attributes.Solids.Bidirectional_Carbon_Fiber.Bidirectional_Carbon_Fiber
density (defined in SUAVE.Attributes.Solids.Bidirectional_Carbon_Fiber.Bidirectional_Carbon_Fiber)SUAVE.Attributes.Solids.Bidirectional_Carbon_Fiber.Bidirectional_Carbon_Fiber
minimum_gage_thickness (defined in SUAVE.Attributes.Solids.Bidirectional_Carbon_Fiber.Bidirectional_Carbon_Fiber)SUAVE.Attributes.Solids.Bidirectional_Carbon_Fiber.Bidirectional_Carbon_Fiber
ultimate_bearing_strength (defined in SUAVE.Attributes.Solids.Bidirectional_Carbon_Fiber.Bidirectional_Carbon_Fiber)SUAVE.Attributes.Solids.Bidirectional_Carbon_Fiber.Bidirectional_Carbon_Fiber
ultimate_shear_strength (defined in SUAVE.Attributes.Solids.Bidirectional_Carbon_Fiber.Bidirectional_Carbon_Fiber)SUAVE.Attributes.Solids.Bidirectional_Carbon_Fiber.Bidirectional_Carbon_Fiber
ultimate_tensile_strength (defined in SUAVE.Attributes.Solids.Bidirectional_Carbon_Fiber.Bidirectional_Carbon_Fiber)SUAVE.Attributes.Solids.Bidirectional_Carbon_Fiber.Bidirectional_Carbon_Fiber
yield_bearing_strength (defined in SUAVE.Attributes.Solids.Bidirectional_Carbon_Fiber.Bidirectional_Carbon_Fiber)SUAVE.Attributes.Solids.Bidirectional_Carbon_Fiber.Bidirectional_Carbon_Fiber
yield_shear_strength (defined in SUAVE.Attributes.Solids.Bidirectional_Carbon_Fiber.Bidirectional_Carbon_Fiber)SUAVE.Attributes.Solids.Bidirectional_Carbon_Fiber.Bidirectional_Carbon_Fiber
yield_tensile_strength (defined in SUAVE.Attributes.Solids.Bidirectional_Carbon_Fiber.Bidirectional_Carbon_Fiber)SUAVE.Attributes.Solids.Bidirectional_Carbon_Fiber.Bidirectional_Carbon_Fiber
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Bidirectional__Carbon__Fiber_1_1Bidirectional__Carbon__Fiber.html b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Bidirectional__Carbon__Fiber_1_1Bidirectional__Carbon__Fiber.html new file mode 100644 index 00000000..4d94ffd2 --- /dev/null +++ b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Bidirectional__Carbon__Fiber_1_1Bidirectional__Carbon__Fiber.html @@ -0,0 +1,245 @@ + + + + + + + +SUAVE: SUAVE.Attributes.Solids.Bidirectional_Carbon_Fiber.Bidirectional_Carbon_Fiber Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Attributes.Solids.Bidirectional_Carbon_Fiber.Bidirectional_Carbon_Fiber Class Reference
+
+
+
+Inheritance diagram for SUAVE.Attributes.Solids.Bidirectional_Carbon_Fiber.Bidirectional_Carbon_Fiber:
+
+
+ + +SUAVE.Attributes.Solids.Solid.Solid + +
+ + + + +

+Public Member Functions

def __defaults__ (self)
 
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Attributes

ultimate_tensile_strength
 
ultimate_shear_strength
 
ultimate_bearing_strength
 
yield_tensile_strength
 
yield_shear_strength
 
yield_bearing_strength
 
minimum_gage_thickness
 
density
 
- Public Attributes inherited from SUAVE.Attributes.Solids.Solid.Solid
ultimate_tensile_strength
 
ultimate_shear_strength
 
ultimate_bearing_strength
 
yield_tensile_strength
 
yield_shear_strength
 
yield_bearing_strength
 
minimum_gage_thickness
 
density
 
+

Detailed Description

+
Physical Constants Specific to Bidirectional Carbon Fiber
+
+Assumptions:
+None
+
+Source:
+MatWeb (Median of Mfg. Reported Values)
+
+Inputs:
+N/A
+
+Outputs:
+N/A
+
+Properties Used:
+None
+

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Attributes.Solids.Bidirectional_Carbon_Fiber.Bidirectional_Carbon_Fiber.__defaults__ ( self)
+
+
Sets material properties at instantiation.
+
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+N/A
+
+Outputs:
+N/A
+
+Properties Used:
+None
+
+

Reimplemented from SUAVE.Attributes.Solids.Solid.Solid.

+ +
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Attributes/Solids/Bidirectional_Carbon_Fiber.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Bidirectional__Carbon__Fiber_1_1Bidirectional__Carbon__Fiber.js b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Bidirectional__Carbon__Fiber_1_1Bidirectional__Carbon__Fiber.js new file mode 100644 index 00000000..d6514ea8 --- /dev/null +++ b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Bidirectional__Carbon__Fiber_1_1Bidirectional__Carbon__Fiber.js @@ -0,0 +1,12 @@ +var classSUAVE_1_1Attributes_1_1Solids_1_1Bidirectional__Carbon__Fiber_1_1Bidirectional__Carbon__Fiber = +[ + [ "__defaults__", "classSUAVE_1_1Attributes_1_1Solids_1_1Bidirectional__Carbon__Fiber_1_1Bidirectional__Carbon__Fiber.html#a4e7fb620f6914a56da7393d9576cdc4e", null ], + [ "density", "classSUAVE_1_1Attributes_1_1Solids_1_1Bidirectional__Carbon__Fiber_1_1Bidirectional__Carbon__Fiber.html#af35adf9aec78d28834f83226eca0cfbc", null ], + [ "minimum_gage_thickness", "classSUAVE_1_1Attributes_1_1Solids_1_1Bidirectional__Carbon__Fiber_1_1Bidirectional__Carbon__Fiber.html#ab32347e36add05b552d690ecbd487f43", null ], + [ "ultimate_bearing_strength", "classSUAVE_1_1Attributes_1_1Solids_1_1Bidirectional__Carbon__Fiber_1_1Bidirectional__Carbon__Fiber.html#a5da7fac5220e65cfff22011f31ba932f", null ], + [ "ultimate_shear_strength", "classSUAVE_1_1Attributes_1_1Solids_1_1Bidirectional__Carbon__Fiber_1_1Bidirectional__Carbon__Fiber.html#ae47a27d2c0b994e93de1d10291b5fbef", null ], + [ "ultimate_tensile_strength", "classSUAVE_1_1Attributes_1_1Solids_1_1Bidirectional__Carbon__Fiber_1_1Bidirectional__Carbon__Fiber.html#aa7badee7c702f89dbd474af9bb572a92", null ], + [ "yield_bearing_strength", "classSUAVE_1_1Attributes_1_1Solids_1_1Bidirectional__Carbon__Fiber_1_1Bidirectional__Carbon__Fiber.html#a59eb5dc4bf05fc7a60c0b3e798554802", null ], + [ "yield_shear_strength", "classSUAVE_1_1Attributes_1_1Solids_1_1Bidirectional__Carbon__Fiber_1_1Bidirectional__Carbon__Fiber.html#a520bca31856a47404d82220a7f5f66bd", null ], + [ "yield_tensile_strength", "classSUAVE_1_1Attributes_1_1Solids_1_1Bidirectional__Carbon__Fiber_1_1Bidirectional__Carbon__Fiber.html#af6844a957288ceb1b97275cc899d8e49", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Bidirectional__Carbon__Fiber_1_1Bidirectional__Carbon__Fiber.png b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Bidirectional__Carbon__Fiber_1_1Bidirectional__Carbon__Fiber.png new file mode 100644 index 00000000..e3bce3e3 Binary files /dev/null and b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Bidirectional__Carbon__Fiber_1_1Bidirectional__Carbon__Fiber.png differ diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Carbon__Fiber__Honeycomb_1_1Carbon__Fiber__Honeycomb-members.html b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Carbon__Fiber__Honeycomb_1_1Carbon__Fiber__Honeycomb-members.html new file mode 100644 index 00000000..f709129b --- /dev/null +++ b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Carbon__Fiber__Honeycomb_1_1Carbon__Fiber__Honeycomb-members.html @@ -0,0 +1,128 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
SUAVE.Attributes.Solids.Carbon_Fiber_Honeycomb.Carbon_Fiber_Honeycomb Member List
+
+
+ +

This is the complete list of members for SUAVE.Attributes.Solids.Carbon_Fiber_Honeycomb.Carbon_Fiber_Honeycomb, including all inherited members.

+ + + + + + + + + + +
__defaults__(self)SUAVE.Attributes.Solids.Carbon_Fiber_Honeycomb.Carbon_Fiber_Honeycomb
density (defined in SUAVE.Attributes.Solids.Carbon_Fiber_Honeycomb.Carbon_Fiber_Honeycomb)SUAVE.Attributes.Solids.Carbon_Fiber_Honeycomb.Carbon_Fiber_Honeycomb
minimum_gage_thickness (defined in SUAVE.Attributes.Solids.Carbon_Fiber_Honeycomb.Carbon_Fiber_Honeycomb)SUAVE.Attributes.Solids.Carbon_Fiber_Honeycomb.Carbon_Fiber_Honeycomb
ultimate_bearing_strength (defined in SUAVE.Attributes.Solids.Carbon_Fiber_Honeycomb.Carbon_Fiber_Honeycomb)SUAVE.Attributes.Solids.Carbon_Fiber_Honeycomb.Carbon_Fiber_Honeycomb
ultimate_shear_strength (defined in SUAVE.Attributes.Solids.Carbon_Fiber_Honeycomb.Carbon_Fiber_Honeycomb)SUAVE.Attributes.Solids.Carbon_Fiber_Honeycomb.Carbon_Fiber_Honeycomb
ultimate_tensile_strength (defined in SUAVE.Attributes.Solids.Carbon_Fiber_Honeycomb.Carbon_Fiber_Honeycomb)SUAVE.Attributes.Solids.Carbon_Fiber_Honeycomb.Carbon_Fiber_Honeycomb
yield_bearing_strength (defined in SUAVE.Attributes.Solids.Carbon_Fiber_Honeycomb.Carbon_Fiber_Honeycomb)SUAVE.Attributes.Solids.Carbon_Fiber_Honeycomb.Carbon_Fiber_Honeycomb
yield_shear_strength (defined in SUAVE.Attributes.Solids.Carbon_Fiber_Honeycomb.Carbon_Fiber_Honeycomb)SUAVE.Attributes.Solids.Carbon_Fiber_Honeycomb.Carbon_Fiber_Honeycomb
yield_tensile_strength (defined in SUAVE.Attributes.Solids.Carbon_Fiber_Honeycomb.Carbon_Fiber_Honeycomb)SUAVE.Attributes.Solids.Carbon_Fiber_Honeycomb.Carbon_Fiber_Honeycomb
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Carbon__Fiber__Honeycomb_1_1Carbon__Fiber__Honeycomb.html b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Carbon__Fiber__Honeycomb_1_1Carbon__Fiber__Honeycomb.html new file mode 100644 index 00000000..161b653c --- /dev/null +++ b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Carbon__Fiber__Honeycomb_1_1Carbon__Fiber__Honeycomb.html @@ -0,0 +1,245 @@ + + + + + + + +SUAVE: SUAVE.Attributes.Solids.Carbon_Fiber_Honeycomb.Carbon_Fiber_Honeycomb Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Attributes.Solids.Carbon_Fiber_Honeycomb.Carbon_Fiber_Honeycomb Class Reference
+
+
+
+Inheritance diagram for SUAVE.Attributes.Solids.Carbon_Fiber_Honeycomb.Carbon_Fiber_Honeycomb:
+
+
+ + +SUAVE.Attributes.Solids.Solid.Solid + +
+ + + + +

+Public Member Functions

def __defaults__ (self)
 
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Attributes

ultimate_tensile_strength
 
ultimate_shear_strength
 
ultimate_bearing_strength
 
yield_tensile_strength
 
yield_shear_strength
 
yield_bearing_strength
 
minimum_gage_thickness
 
density
 
- Public Attributes inherited from SUAVE.Attributes.Solids.Solid.Solid
ultimate_tensile_strength
 
ultimate_shear_strength
 
ultimate_bearing_strength
 
yield_tensile_strength
 
yield_shear_strength
 
yield_bearing_strength
 
minimum_gage_thickness
 
density
 
+

Detailed Description

+
Physical Constants Specific to Carbon Fiber Honeycomb Core Material
+
+Assumptions:
+None
+
+Source:
+MatWeb (Median of Mfg. Reported Values)
+
+Inputs:
+N/A
+
+Outputs:
+N/A
+
+Properties Used:
+None
+

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Attributes.Solids.Carbon_Fiber_Honeycomb.Carbon_Fiber_Honeycomb.__defaults__ ( self)
+
+
Sets material properties at instantiation.
+
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+N/A
+
+Outputs:
+N/A
+
+Properties Used:
+None
+
+

Reimplemented from SUAVE.Attributes.Solids.Solid.Solid.

+ +
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Attributes/Solids/Carbon_Fiber_Honeycomb.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Carbon__Fiber__Honeycomb_1_1Carbon__Fiber__Honeycomb.js b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Carbon__Fiber__Honeycomb_1_1Carbon__Fiber__Honeycomb.js new file mode 100644 index 00000000..e98b03c7 --- /dev/null +++ b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Carbon__Fiber__Honeycomb_1_1Carbon__Fiber__Honeycomb.js @@ -0,0 +1,12 @@ +var classSUAVE_1_1Attributes_1_1Solids_1_1Carbon__Fiber__Honeycomb_1_1Carbon__Fiber__Honeycomb = +[ + [ "__defaults__", "classSUAVE_1_1Attributes_1_1Solids_1_1Carbon__Fiber__Honeycomb_1_1Carbon__Fiber__Honeycomb.html#aaf7dbab48a406423a6192ef66cf61786", null ], + [ "density", "classSUAVE_1_1Attributes_1_1Solids_1_1Carbon__Fiber__Honeycomb_1_1Carbon__Fiber__Honeycomb.html#aa80fadc3c5ffcb53a52e05018c85e3af", null ], + [ "minimum_gage_thickness", "classSUAVE_1_1Attributes_1_1Solids_1_1Carbon__Fiber__Honeycomb_1_1Carbon__Fiber__Honeycomb.html#a87fd099ce82ead9ba1501046828b1805", null ], + [ "ultimate_bearing_strength", "classSUAVE_1_1Attributes_1_1Solids_1_1Carbon__Fiber__Honeycomb_1_1Carbon__Fiber__Honeycomb.html#a2e877144788db8956c6969801f5ff24f", null ], + [ "ultimate_shear_strength", "classSUAVE_1_1Attributes_1_1Solids_1_1Carbon__Fiber__Honeycomb_1_1Carbon__Fiber__Honeycomb.html#a6938a96edd26d1d870f9cce3b7d32166", null ], + [ "ultimate_tensile_strength", "classSUAVE_1_1Attributes_1_1Solids_1_1Carbon__Fiber__Honeycomb_1_1Carbon__Fiber__Honeycomb.html#a8e8e60346c66dabf0fc18deb07870a4b", null ], + [ "yield_bearing_strength", "classSUAVE_1_1Attributes_1_1Solids_1_1Carbon__Fiber__Honeycomb_1_1Carbon__Fiber__Honeycomb.html#a5fca5d9eb0fd88c936d827de9add8aa2", null ], + [ "yield_shear_strength", "classSUAVE_1_1Attributes_1_1Solids_1_1Carbon__Fiber__Honeycomb_1_1Carbon__Fiber__Honeycomb.html#ad3459034612b3213130cf5833259c5ce", null ], + [ "yield_tensile_strength", "classSUAVE_1_1Attributes_1_1Solids_1_1Carbon__Fiber__Honeycomb_1_1Carbon__Fiber__Honeycomb.html#aec56b41e6392065e7f9c3da84f2f36d7", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Carbon__Fiber__Honeycomb_1_1Carbon__Fiber__Honeycomb.png b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Carbon__Fiber__Honeycomb_1_1Carbon__Fiber__Honeycomb.png new file mode 100644 index 00000000..04f35f75 Binary files /dev/null and b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Carbon__Fiber__Honeycomb_1_1Carbon__Fiber__Honeycomb.png differ diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Copper_1_1Copper-members.html b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Copper_1_1Copper-members.html new file mode 100644 index 00000000..5092b361 --- /dev/null +++ b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Copper_1_1Copper-members.html @@ -0,0 +1,134 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
SUAVE.Attributes.Solids.Copper.Copper Member List
+
+
+ +

This is the complete list of members for SUAVE.Attributes.Solids.Copper.Copper, including all inherited members.

+ + + + + + + + + + + + + + + + +
__defaults__(self)SUAVE.Attributes.Solids.Copper.Copper
c_electrical (defined in SUAVE.Attributes.Solids.Copper.Copper)SUAVE.Attributes.Solids.Copper.Copper
c_thermal (defined in SUAVE.Attributes.Solids.Copper.Copper)SUAVE.Attributes.Solids.Copper.Copper
conductivity_electrical (defined in SUAVE.Attributes.Solids.Copper.Copper)SUAVE.Attributes.Solids.Copper.Copper
conductivity_thermal (defined in SUAVE.Attributes.Solids.Copper.Copper)SUAVE.Attributes.Solids.Copper.Copper
density (defined in SUAVE.Attributes.Solids.Copper.Copper)SUAVE.Attributes.Solids.Copper.Copper
electrical_conductivity(self, temperature) (defined in SUAVE.Attributes.Solids.Copper.Copper)SUAVE.Attributes.Solids.Copper.Copper
minimum_gage_thickness (defined in SUAVE.Attributes.Solids.Solid.Solid)SUAVE.Attributes.Solids.Solid.Solid
thermal_conductivity(self, temperature) (defined in SUAVE.Attributes.Solids.Copper.Copper)SUAVE.Attributes.Solids.Copper.Copper
ultimate_bearing_strength (defined in SUAVE.Attributes.Solids.Solid.Solid)SUAVE.Attributes.Solids.Solid.Solid
ultimate_shear_strength (defined in SUAVE.Attributes.Solids.Solid.Solid)SUAVE.Attributes.Solids.Solid.Solid
ultimate_tensile_strength (defined in SUAVE.Attributes.Solids.Solid.Solid)SUAVE.Attributes.Solids.Solid.Solid
yield_bearing_strength (defined in SUAVE.Attributes.Solids.Solid.Solid)SUAVE.Attributes.Solids.Solid.Solid
yield_shear_strength (defined in SUAVE.Attributes.Solids.Solid.Solid)SUAVE.Attributes.Solids.Solid.Solid
yield_tensile_strength (defined in SUAVE.Attributes.Solids.Solid.Solid)SUAVE.Attributes.Solids.Solid.Solid
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Copper_1_1Copper.html b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Copper_1_1Copper.html new file mode 100644 index 00000000..08cbd855 --- /dev/null +++ b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Copper_1_1Copper.html @@ -0,0 +1,243 @@ + + + + + + + +SUAVE: SUAVE.Attributes.Solids.Copper.Copper Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Attributes.Solids.Copper.Copper Class Reference
+
+
+
+Inheritance diagram for SUAVE.Attributes.Solids.Copper.Copper:
+
+
+ + +SUAVE.Attributes.Solids.Solid.Solid + +
+ + + + + + + + +

+Public Member Functions

def __defaults__ (self)
 
+def thermal_conductivity (self, temperature)
 
+def electrical_conductivity (self, temperature)
 
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Attributes

density
 
conductivity_electrical
 
conductivity_thermal
 
c_thermal
 
c_electrical
 
- Public Attributes inherited from SUAVE.Attributes.Solids.Solid.Solid
ultimate_tensile_strength
 
ultimate_shear_strength
 
ultimate_bearing_strength
 
yield_tensile_strength
 
yield_shear_strength
 
yield_bearing_strength
 
minimum_gage_thickness
 
density
 
+

Detailed Description

+
Physical Constants Specific to copper RRR=50 OFHC
+
+Assumptions:
+None
+
+Source:
+"PROPERTIES OF SELECTED MATERIALS AT CRYOGENIC TEMPERATURES" Peter E. Bradley and Ray Radebaugh
+"A copper resistance temperature scale" Dauphinee, TM and Preston-Thomas, H
+
+Inputs:
+N/A
+
+Outputs:
+N/A
+
+Properties Used:
+None
+

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Attributes.Solids.Copper.Copper.__defaults__ ( self)
+
+
Sets material properties at instantiation.
+
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+N/A
+
+Outputs:
+N/A
+
+Properties Used:
+None
+
+

Reimplemented from SUAVE.Attributes.Solids.Solid.Solid.

+ +
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Attributes/Solids/Copper.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Copper_1_1Copper.js b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Copper_1_1Copper.js new file mode 100644 index 00000000..ac664343 --- /dev/null +++ b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Copper_1_1Copper.js @@ -0,0 +1,11 @@ +var classSUAVE_1_1Attributes_1_1Solids_1_1Copper_1_1Copper = +[ + [ "__defaults__", "classSUAVE_1_1Attributes_1_1Solids_1_1Copper_1_1Copper.html#a49c8243b50ea8137e53db738dcd0b785", null ], + [ "electrical_conductivity", "classSUAVE_1_1Attributes_1_1Solids_1_1Copper_1_1Copper.html#ab9f615efb53b9ee95df148b32dbb9090", null ], + [ "thermal_conductivity", "classSUAVE_1_1Attributes_1_1Solids_1_1Copper_1_1Copper.html#ade1632b63a9a1cc65812bcfc7d62571d", null ], + [ "c_electrical", "classSUAVE_1_1Attributes_1_1Solids_1_1Copper_1_1Copper.html#a16f402fa6fd77748b3fcae739bb5d486", null ], + [ "c_thermal", "classSUAVE_1_1Attributes_1_1Solids_1_1Copper_1_1Copper.html#adb5207421e0a2f3222fbb6979bd1237b", null ], + [ "conductivity_electrical", "classSUAVE_1_1Attributes_1_1Solids_1_1Copper_1_1Copper.html#a7494ee5b85c6fd161cebf0c76f61c684", null ], + [ "conductivity_thermal", "classSUAVE_1_1Attributes_1_1Solids_1_1Copper_1_1Copper.html#a7964f7b4405b46df2317250b333a91af", null ], + [ "density", "classSUAVE_1_1Attributes_1_1Solids_1_1Copper_1_1Copper.html#a09a7f9820d0adb88f3e52f527d1179e4", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Copper_1_1Copper.png b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Copper_1_1Copper.png new file mode 100644 index 00000000..4b4c4a32 Binary files /dev/null and b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Copper_1_1Copper.png differ diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Epoxy_1_1Epoxy-members.html b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Epoxy_1_1Epoxy-members.html new file mode 100644 index 00000000..280587b4 --- /dev/null +++ b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Epoxy_1_1Epoxy-members.html @@ -0,0 +1,128 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
SUAVE.Attributes.Solids.Epoxy.Epoxy Member List
+
+ +
+ + + + diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Epoxy_1_1Epoxy.html b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Epoxy_1_1Epoxy.html new file mode 100644 index 00000000..3288765b --- /dev/null +++ b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Epoxy_1_1Epoxy.html @@ -0,0 +1,245 @@ + + + + + + + +SUAVE: SUAVE.Attributes.Solids.Epoxy.Epoxy Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Attributes.Solids.Epoxy.Epoxy Class Reference
+
+
+
+Inheritance diagram for SUAVE.Attributes.Solids.Epoxy.Epoxy:
+
+
+ + +SUAVE.Attributes.Solids.Solid.Solid + +
+ + + + +

+Public Member Functions

def __defaults__ (self)
 
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Attributes

ultimate_tensile_strength
 
ultimate_shear_strength
 
ultimate_bearing_strength
 
yield_tensile_strength
 
yield_shear_strength
 
yield_bearing_strength
 
minimum_gage_thickness
 
density
 
- Public Attributes inherited from SUAVE.Attributes.Solids.Solid.Solid
ultimate_tensile_strength
 
ultimate_shear_strength
 
ultimate_bearing_strength
 
yield_tensile_strength
 
yield_shear_strength
 
yield_bearing_strength
 
minimum_gage_thickness
 
density
 
+

Detailed Description

+
Physical Constants Specific to Epoxy Resin
+
+Assumptions:
+None
+
+Source:
+MatWeb (Median of Mfg. Reported Values)
+
+Inputs:
+N/A
+
+Outputs:
+N/A
+
+Properties Used:
+None
+

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Attributes.Solids.Epoxy.Epoxy.__defaults__ ( self)
+
+
Sets material properties at instantiation.
+
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+N/A
+
+Outputs:
+N/A
+
+Properties Used:
+None
+
+

Reimplemented from SUAVE.Attributes.Solids.Solid.Solid.

+ +
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Attributes/Solids/Epoxy.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Epoxy_1_1Epoxy.js b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Epoxy_1_1Epoxy.js new file mode 100644 index 00000000..90c43a32 --- /dev/null +++ b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Epoxy_1_1Epoxy.js @@ -0,0 +1,12 @@ +var classSUAVE_1_1Attributes_1_1Solids_1_1Epoxy_1_1Epoxy = +[ + [ "__defaults__", "classSUAVE_1_1Attributes_1_1Solids_1_1Epoxy_1_1Epoxy.html#a01abb5240dac553f3f5b5d406b9e8664", null ], + [ "density", "classSUAVE_1_1Attributes_1_1Solids_1_1Epoxy_1_1Epoxy.html#a245e5bfc71571d80624003464b8c13a5", null ], + [ "minimum_gage_thickness", "classSUAVE_1_1Attributes_1_1Solids_1_1Epoxy_1_1Epoxy.html#a03831c61ba5f1b7f05d7b8425af6a234", null ], + [ "ultimate_bearing_strength", "classSUAVE_1_1Attributes_1_1Solids_1_1Epoxy_1_1Epoxy.html#a00de7948a65261baf7c3c013906e43c6", null ], + [ "ultimate_shear_strength", "classSUAVE_1_1Attributes_1_1Solids_1_1Epoxy_1_1Epoxy.html#a37d87a04045035867e2d212273180e48", null ], + [ "ultimate_tensile_strength", "classSUAVE_1_1Attributes_1_1Solids_1_1Epoxy_1_1Epoxy.html#a7db428c7daf56f9ea398d45ad56e6b0e", null ], + [ "yield_bearing_strength", "classSUAVE_1_1Attributes_1_1Solids_1_1Epoxy_1_1Epoxy.html#a2f6d66b51093df02fcb752b0547b27f1", null ], + [ "yield_shear_strength", "classSUAVE_1_1Attributes_1_1Solids_1_1Epoxy_1_1Epoxy.html#a4e0cfe994d04603bc524b3d2b788c24a", null ], + [ "yield_tensile_strength", "classSUAVE_1_1Attributes_1_1Solids_1_1Epoxy_1_1Epoxy.html#a9cecd71d2f9f50705cffc9ee9d9944d7", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Epoxy_1_1Epoxy.png b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Epoxy_1_1Epoxy.png new file mode 100644 index 00000000..32d32aab Binary files /dev/null and b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Epoxy_1_1Epoxy.png differ diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Nickel_1_1Nickel-members.html b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Nickel_1_1Nickel-members.html new file mode 100644 index 00000000..9a5079e5 --- /dev/null +++ b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Nickel_1_1Nickel-members.html @@ -0,0 +1,128 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
SUAVE.Attributes.Solids.Nickel.Nickel Member List
+
+ +
+ + + + diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Nickel_1_1Nickel.html b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Nickel_1_1Nickel.html new file mode 100644 index 00000000..27acb314 --- /dev/null +++ b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Nickel_1_1Nickel.html @@ -0,0 +1,245 @@ + + + + + + + +SUAVE: SUAVE.Attributes.Solids.Nickel.Nickel Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Attributes.Solids.Nickel.Nickel Class Reference
+
+
+
+Inheritance diagram for SUAVE.Attributes.Solids.Nickel.Nickel:
+
+
+ + +SUAVE.Attributes.Solids.Solid.Solid + +
+ + + + +

+Public Member Functions

def __defaults__ (self)
 
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Attributes

ultimate_tensile_strength
 
ultimate_shear_strength
 
ultimate_bearing_strength
 
yield_tensile_strength
 
yield_shear_strength
 
yield_bearing_strength
 
minimum_gage_thickness
 
density
 
- Public Attributes inherited from SUAVE.Attributes.Solids.Solid.Solid
ultimate_tensile_strength
 
ultimate_shear_strength
 
ultimate_bearing_strength
 
yield_tensile_strength
 
yield_shear_strength
 
yield_bearing_strength
 
minimum_gage_thickness
 
density
 
+

Detailed Description

+
Physical Constants Specific to Nickel/Cobalt Chromoly Alloy
+
+Assumptions:
+None
+
+Source:
+MatWeb (Median of Mfg. Reported Values)
+
+Inputs:
+N/A
+
+Outputs:
+N/A
+
+Properties Used:
+None
+

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Attributes.Solids.Nickel.Nickel.__defaults__ ( self)
+
+
Sets material properties at instantiation.
+
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+N/A
+
+Outputs:
+N/A
+
+Properties Used:
+None
+
+

Reimplemented from SUAVE.Attributes.Solids.Solid.Solid.

+ +
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Attributes/Solids/Nickel.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Nickel_1_1Nickel.js b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Nickel_1_1Nickel.js new file mode 100644 index 00000000..899c51b7 --- /dev/null +++ b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Nickel_1_1Nickel.js @@ -0,0 +1,12 @@ +var classSUAVE_1_1Attributes_1_1Solids_1_1Nickel_1_1Nickel = +[ + [ "__defaults__", "classSUAVE_1_1Attributes_1_1Solids_1_1Nickel_1_1Nickel.html#a08aa94f22993f8ced8f24e55540f7c6e", null ], + [ "density", "classSUAVE_1_1Attributes_1_1Solids_1_1Nickel_1_1Nickel.html#a3cec818e9b95d4638c0acf59527daee5", null ], + [ "minimum_gage_thickness", "classSUAVE_1_1Attributes_1_1Solids_1_1Nickel_1_1Nickel.html#a77575e00af88ed5f89c4ace198b1363e", null ], + [ "ultimate_bearing_strength", "classSUAVE_1_1Attributes_1_1Solids_1_1Nickel_1_1Nickel.html#ab714bac5a9c06c44bab22d734261954f", null ], + [ "ultimate_shear_strength", "classSUAVE_1_1Attributes_1_1Solids_1_1Nickel_1_1Nickel.html#af63ac11df8c46ba0101f071cf5dcc781", null ], + [ "ultimate_tensile_strength", "classSUAVE_1_1Attributes_1_1Solids_1_1Nickel_1_1Nickel.html#a4e5520342d9ab210126007569822bd0a", null ], + [ "yield_bearing_strength", "classSUAVE_1_1Attributes_1_1Solids_1_1Nickel_1_1Nickel.html#aec2f835362c2ae3f7add09ff5dda0251", null ], + [ "yield_shear_strength", "classSUAVE_1_1Attributes_1_1Solids_1_1Nickel_1_1Nickel.html#afd7bbad806de6d417e36452e265de148", null ], + [ "yield_tensile_strength", "classSUAVE_1_1Attributes_1_1Solids_1_1Nickel_1_1Nickel.html#af928e7453d39db15764f925a82c4caf7", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Nickel_1_1Nickel.png b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Nickel_1_1Nickel.png new file mode 100644 index 00000000..ed01cfc0 Binary files /dev/null and b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Nickel_1_1Nickel.png differ diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Paint_1_1Paint-members.html b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Paint_1_1Paint-members.html new file mode 100644 index 00000000..2b706187 --- /dev/null +++ b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Paint_1_1Paint-members.html @@ -0,0 +1,128 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
SUAVE.Attributes.Solids.Paint.Paint Member List
+
+ +
+ + + + diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Paint_1_1Paint.html b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Paint_1_1Paint.html new file mode 100644 index 00000000..3bfa8461 --- /dev/null +++ b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Paint_1_1Paint.html @@ -0,0 +1,245 @@ + + + + + + + +SUAVE: SUAVE.Attributes.Solids.Paint.Paint Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Attributes.Solids.Paint.Paint Class Reference
+
+
+
+Inheritance diagram for SUAVE.Attributes.Solids.Paint.Paint:
+
+
+ + +SUAVE.Attributes.Solids.Solid.Solid + +
+ + + + +

+Public Member Functions

def __defaults__ (self)
 
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Attributes

ultimate_tensile_strength
 
ultimate_shear_strength
 
ultimate_bearing_strength
 
yield_tensile_strength
 
yield_shear_strength
 
yield_bearing_strength
 
minimum_gage_thickness
 
density
 
- Public Attributes inherited from SUAVE.Attributes.Solids.Solid.Solid
ultimate_tensile_strength
 
ultimate_shear_strength
 
ultimate_bearing_strength
 
yield_tensile_strength
 
yield_shear_strength
 
yield_bearing_strength
 
minimum_gage_thickness
 
density
 
+

Detailed Description

+
Physical Constants Specific to Paint/Vinyl Surface Coverings
+
+Assumptions:
+None
+
+Source:
+MatWeb (Median of Mfg. Reported Values)
+
+Inputs:
+N/A
+
+Outputs:
+N/A
+
+Properties Used:
+None
+

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Attributes.Solids.Paint.Paint.__defaults__ ( self)
+
+
Sets material properties at instantiation.
+
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+N/A
+
+Outputs:
+N/A
+
+Properties Used:
+None
+
+

Reimplemented from SUAVE.Attributes.Solids.Solid.Solid.

+ +
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Attributes/Solids/Paint.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Paint_1_1Paint.js b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Paint_1_1Paint.js new file mode 100644 index 00000000..2bd1da3b --- /dev/null +++ b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Paint_1_1Paint.js @@ -0,0 +1,12 @@ +var classSUAVE_1_1Attributes_1_1Solids_1_1Paint_1_1Paint = +[ + [ "__defaults__", "classSUAVE_1_1Attributes_1_1Solids_1_1Paint_1_1Paint.html#acdd78a527c2e3f8ba716f16386e93d76", null ], + [ "density", "classSUAVE_1_1Attributes_1_1Solids_1_1Paint_1_1Paint.html#ac7c67e65f242527228681198e339a8bd", null ], + [ "minimum_gage_thickness", "classSUAVE_1_1Attributes_1_1Solids_1_1Paint_1_1Paint.html#a0eff7d7e0661390dbbf7e9e0656bc429", null ], + [ "ultimate_bearing_strength", "classSUAVE_1_1Attributes_1_1Solids_1_1Paint_1_1Paint.html#afc756caf3e2aeb9e3281d75910c7787f", null ], + [ "ultimate_shear_strength", "classSUAVE_1_1Attributes_1_1Solids_1_1Paint_1_1Paint.html#a819418320950acf2b27a1b7c74af3b0d", null ], + [ "ultimate_tensile_strength", "classSUAVE_1_1Attributes_1_1Solids_1_1Paint_1_1Paint.html#a9e9999eb718032fce23e3c79bd73b1eb", null ], + [ "yield_bearing_strength", "classSUAVE_1_1Attributes_1_1Solids_1_1Paint_1_1Paint.html#a29547ee894c9ee36a5a89dc5567f16a6", null ], + [ "yield_shear_strength", "classSUAVE_1_1Attributes_1_1Solids_1_1Paint_1_1Paint.html#aab885746c417665c27dbb270e6f66167", null ], + [ "yield_tensile_strength", "classSUAVE_1_1Attributes_1_1Solids_1_1Paint_1_1Paint.html#a1d51e0e2ff87e3daf55b1509382b155a", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Paint_1_1Paint.png b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Paint_1_1Paint.png new file mode 100644 index 00000000..2f2e3a5b Binary files /dev/null and b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Paint_1_1Paint.png differ diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Solid_1_1Solid-members.html b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Solid_1_1Solid-members.html new file mode 100644 index 00000000..5b9daf0e --- /dev/null +++ b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Solid_1_1Solid-members.html @@ -0,0 +1,128 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
SUAVE.Attributes.Solids.Solid.Solid Member List
+
+ +
+ + + + diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Solid_1_1Solid.html b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Solid_1_1Solid.html new file mode 100644 index 00000000..8930dedb --- /dev/null +++ b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Solid_1_1Solid.html @@ -0,0 +1,228 @@ + + + + + + + +SUAVE: SUAVE.Attributes.Solids.Solid.Solid Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Attributes.Solids.Solid.Solid Class Reference
+
+
+
+Inheritance diagram for SUAVE.Attributes.Solids.Solid.Solid:
+
+
+ + +SUAVE.Attributes.Solids.Acrylic.Acrylic +SUAVE.Attributes.Solids.Aluminum.Aluminum +SUAVE.Attributes.Solids.Bidirectional_Carbon_Fiber.Bidirectional_Carbon_Fiber +SUAVE.Attributes.Solids.Carbon_Fiber_Honeycomb.Carbon_Fiber_Honeycomb +SUAVE.Attributes.Solids.Copper.Copper +SUAVE.Attributes.Solids.Epoxy.Epoxy +SUAVE.Attributes.Solids.Nickel.Nickel +SUAVE.Attributes.Solids.Paint.Paint +SUAVE.Attributes.Solids.Steel.Steel +SUAVE.Attributes.Solids.Unidirectional_Carbon_Fiber.Unidirectional_Carbon_Fiber + +
+ + + + +

+Public Member Functions

def __defaults__ (self)
 
+ + + + + + + + + + + + + + + + + +

+Public Attributes

ultimate_tensile_strength
 
ultimate_shear_strength
 
ultimate_bearing_strength
 
yield_tensile_strength
 
yield_shear_strength
 
yield_bearing_strength
 
minimum_gage_thickness
 
density
 
+

Detailed Description

+
Default Template for Solid Attribute Classes
+
+    Assumptions:
+    None
+    
+    Source:
+    N/A
+    
+    Inputs:
+    N/A
+    
+    Outputs:
+    N/A
+    
+    Properties Used:
+    None

Member Function Documentation

+ +

◆ __defaults__()

+ + +
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Attributes/Solids/Solid.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Solid_1_1Solid.js b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Solid_1_1Solid.js new file mode 100644 index 00000000..f1f26e35 --- /dev/null +++ b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Solid_1_1Solid.js @@ -0,0 +1,12 @@ +var classSUAVE_1_1Attributes_1_1Solids_1_1Solid_1_1Solid = +[ + [ "__defaults__", "classSUAVE_1_1Attributes_1_1Solids_1_1Solid_1_1Solid.html#a049c4e20b4566da07bf97a0d1f07c9aa", null ], + [ "density", "classSUAVE_1_1Attributes_1_1Solids_1_1Solid_1_1Solid.html#a4f49cda53b0a9ee5f0af859981a88f28", null ], + [ "minimum_gage_thickness", "classSUAVE_1_1Attributes_1_1Solids_1_1Solid_1_1Solid.html#aee6f1df414ff04b8dbb1bb09800849b7", null ], + [ "ultimate_bearing_strength", "classSUAVE_1_1Attributes_1_1Solids_1_1Solid_1_1Solid.html#a41490f1c431b6b1729f4ca17015bd4cf", null ], + [ "ultimate_shear_strength", "classSUAVE_1_1Attributes_1_1Solids_1_1Solid_1_1Solid.html#a443e7cca7507499247710b4c47d24c41", null ], + [ "ultimate_tensile_strength", "classSUAVE_1_1Attributes_1_1Solids_1_1Solid_1_1Solid.html#a2aeadd0b354bcf074c277768ecfccb89", null ], + [ "yield_bearing_strength", "classSUAVE_1_1Attributes_1_1Solids_1_1Solid_1_1Solid.html#adafd8acab74a6d032da19773c182e608", null ], + [ "yield_shear_strength", "classSUAVE_1_1Attributes_1_1Solids_1_1Solid_1_1Solid.html#a2ec2b129bf860f749b8dd5acaa46ab67", null ], + [ "yield_tensile_strength", "classSUAVE_1_1Attributes_1_1Solids_1_1Solid_1_1Solid.html#a15270eaa0b7fbdcc684994b051f89de4", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Solid_1_1Solid.png b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Solid_1_1Solid.png new file mode 100644 index 00000000..311b632c Binary files /dev/null and b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Solid_1_1Solid.png differ diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Steel_1_1Steel-members.html b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Steel_1_1Steel-members.html new file mode 100644 index 00000000..95e6648a --- /dev/null +++ b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Steel_1_1Steel-members.html @@ -0,0 +1,128 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
SUAVE.Attributes.Solids.Steel.Steel Member List
+
+ +
+ + + + diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Steel_1_1Steel.html b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Steel_1_1Steel.html new file mode 100644 index 00000000..e08c3408 --- /dev/null +++ b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Steel_1_1Steel.html @@ -0,0 +1,245 @@ + + + + + + + +SUAVE: SUAVE.Attributes.Solids.Steel.Steel Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Attributes.Solids.Steel.Steel Class Reference
+
+
+
+Inheritance diagram for SUAVE.Attributes.Solids.Steel.Steel:
+
+
+ + +SUAVE.Attributes.Solids.Solid.Solid + +
+ + + + +

+Public Member Functions

def __defaults__ (self)
 
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Attributes

ultimate_tensile_strength
 
ultimate_shear_strength
 
ultimate_bearing_strength
 
yield_tensile_strength
 
yield_shear_strength
 
yield_bearing_strength
 
minimum_gage_thickness
 
density
 
- Public Attributes inherited from SUAVE.Attributes.Solids.Solid.Solid
ultimate_tensile_strength
 
ultimate_shear_strength
 
ultimate_bearing_strength
 
yield_tensile_strength
 
yield_shear_strength
 
yield_bearing_strength
 
minimum_gage_thickness
 
density
 
+

Detailed Description

+
Physical Constants Specific to AISI 4340 Steel
+
+Assumptions:
+None
+
+Source:
+MatWeb (Median of Mfg. Reported Values)
+
+Inputs:
+N/A
+
+Outputs:
+N/A
+
+Properties Used:
+None
+

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Attributes.Solids.Steel.Steel.__defaults__ ( self)
+
+
Sets material properties at instantiation.
+
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+N/A
+
+Outputs:
+N/A
+
+Properties Used:
+None
+
+

Reimplemented from SUAVE.Attributes.Solids.Solid.Solid.

+ +
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Attributes/Solids/Steel.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Steel_1_1Steel.js b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Steel_1_1Steel.js new file mode 100644 index 00000000..7e8230cf --- /dev/null +++ b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Steel_1_1Steel.js @@ -0,0 +1,12 @@ +var classSUAVE_1_1Attributes_1_1Solids_1_1Steel_1_1Steel = +[ + [ "__defaults__", "classSUAVE_1_1Attributes_1_1Solids_1_1Steel_1_1Steel.html#acfb1646d03438d752214648a79c71982", null ], + [ "density", "classSUAVE_1_1Attributes_1_1Solids_1_1Steel_1_1Steel.html#af8c06920d2ec8a435b7754470a937481", null ], + [ "minimum_gage_thickness", "classSUAVE_1_1Attributes_1_1Solids_1_1Steel_1_1Steel.html#a1514180b34c80cea84214c68b8138a13", null ], + [ "ultimate_bearing_strength", "classSUAVE_1_1Attributes_1_1Solids_1_1Steel_1_1Steel.html#a1d64fc39c6af8b402ec76d9f5b536815", null ], + [ "ultimate_shear_strength", "classSUAVE_1_1Attributes_1_1Solids_1_1Steel_1_1Steel.html#a0c779977a334ebd733cd6a0cbe103264", null ], + [ "ultimate_tensile_strength", "classSUAVE_1_1Attributes_1_1Solids_1_1Steel_1_1Steel.html#aa461bb61687f8d28136bc804f86c928c", null ], + [ "yield_bearing_strength", "classSUAVE_1_1Attributes_1_1Solids_1_1Steel_1_1Steel.html#aee2f73f0316dc75a9c67d74c97bc684e", null ], + [ "yield_shear_strength", "classSUAVE_1_1Attributes_1_1Solids_1_1Steel_1_1Steel.html#aa7803db5febd7c65a9cf42367a775d2d", null ], + [ "yield_tensile_strength", "classSUAVE_1_1Attributes_1_1Solids_1_1Steel_1_1Steel.html#a33d0cecd7d34d5ad1bb68af07c2ffdc4", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Steel_1_1Steel.png b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Steel_1_1Steel.png new file mode 100644 index 00000000..bd6b8f75 Binary files /dev/null and b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Steel_1_1Steel.png differ diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Unidirectional__Carbon__Fiber_1_1Unidirectional__Carbon__Fiber-members.html b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Unidirectional__Carbon__Fiber_1_1Unidirectional__Carbon__Fiber-members.html new file mode 100644 index 00000000..7b1518a4 --- /dev/null +++ b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Unidirectional__Carbon__Fiber_1_1Unidirectional__Carbon__Fiber-members.html @@ -0,0 +1,128 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
SUAVE.Attributes.Solids.Unidirectional_Carbon_Fiber.Unidirectional_Carbon_Fiber Member List
+
+
+ +

This is the complete list of members for SUAVE.Attributes.Solids.Unidirectional_Carbon_Fiber.Unidirectional_Carbon_Fiber, including all inherited members.

+ + + + + + + + + + +
__defaults__(self)SUAVE.Attributes.Solids.Unidirectional_Carbon_Fiber.Unidirectional_Carbon_Fiber
density (defined in SUAVE.Attributes.Solids.Unidirectional_Carbon_Fiber.Unidirectional_Carbon_Fiber)SUAVE.Attributes.Solids.Unidirectional_Carbon_Fiber.Unidirectional_Carbon_Fiber
minimum_gage_thickness (defined in SUAVE.Attributes.Solids.Unidirectional_Carbon_Fiber.Unidirectional_Carbon_Fiber)SUAVE.Attributes.Solids.Unidirectional_Carbon_Fiber.Unidirectional_Carbon_Fiber
ultimate_bearing_strength (defined in SUAVE.Attributes.Solids.Unidirectional_Carbon_Fiber.Unidirectional_Carbon_Fiber)SUAVE.Attributes.Solids.Unidirectional_Carbon_Fiber.Unidirectional_Carbon_Fiber
ultimate_shear_strength (defined in SUAVE.Attributes.Solids.Unidirectional_Carbon_Fiber.Unidirectional_Carbon_Fiber)SUAVE.Attributes.Solids.Unidirectional_Carbon_Fiber.Unidirectional_Carbon_Fiber
ultimate_tensile_strength (defined in SUAVE.Attributes.Solids.Unidirectional_Carbon_Fiber.Unidirectional_Carbon_Fiber)SUAVE.Attributes.Solids.Unidirectional_Carbon_Fiber.Unidirectional_Carbon_Fiber
yield_bearing_strength (defined in SUAVE.Attributes.Solids.Unidirectional_Carbon_Fiber.Unidirectional_Carbon_Fiber)SUAVE.Attributes.Solids.Unidirectional_Carbon_Fiber.Unidirectional_Carbon_Fiber
yield_shear_strength (defined in SUAVE.Attributes.Solids.Unidirectional_Carbon_Fiber.Unidirectional_Carbon_Fiber)SUAVE.Attributes.Solids.Unidirectional_Carbon_Fiber.Unidirectional_Carbon_Fiber
yield_tensile_strength (defined in SUAVE.Attributes.Solids.Unidirectional_Carbon_Fiber.Unidirectional_Carbon_Fiber)SUAVE.Attributes.Solids.Unidirectional_Carbon_Fiber.Unidirectional_Carbon_Fiber
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Unidirectional__Carbon__Fiber_1_1Unidirectional__Carbon__Fiber.html b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Unidirectional__Carbon__Fiber_1_1Unidirectional__Carbon__Fiber.html new file mode 100644 index 00000000..770029b6 --- /dev/null +++ b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Unidirectional__Carbon__Fiber_1_1Unidirectional__Carbon__Fiber.html @@ -0,0 +1,245 @@ + + + + + + + +SUAVE: SUAVE.Attributes.Solids.Unidirectional_Carbon_Fiber.Unidirectional_Carbon_Fiber Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Attributes.Solids.Unidirectional_Carbon_Fiber.Unidirectional_Carbon_Fiber Class Reference
+
+
+
+Inheritance diagram for SUAVE.Attributes.Solids.Unidirectional_Carbon_Fiber.Unidirectional_Carbon_Fiber:
+
+
+ + +SUAVE.Attributes.Solids.Solid.Solid + +
+ + + + +

+Public Member Functions

def __defaults__ (self)
 
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Attributes

ultimate_tensile_strength
 
ultimate_shear_strength
 
ultimate_bearing_strength
 
yield_tensile_strength
 
yield_shear_strength
 
yield_bearing_strength
 
minimum_gage_thickness
 
density
 
- Public Attributes inherited from SUAVE.Attributes.Solids.Solid.Solid
ultimate_tensile_strength
 
ultimate_shear_strength
 
ultimate_bearing_strength
 
yield_tensile_strength
 
yield_shear_strength
 
yield_bearing_strength
 
minimum_gage_thickness
 
density
 
+

Detailed Description

+
Physical Constants Specific to Unidirectional Carbon Fiber
+
+Assumptions:
+None
+
+Source:
+MatWeb (Median of Mfg. Reported Values)
+
+Inputs:
+N/A
+
+Outputs:
+N/A
+
+Properties Used:
+None
+

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Attributes.Solids.Unidirectional_Carbon_Fiber.Unidirectional_Carbon_Fiber.__defaults__ ( self)
+
+
Sets material properties at instantiation.
+
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+N/A
+
+Outputs:
+N/A
+
+Properties Used:
+None
+
+

Reimplemented from SUAVE.Attributes.Solids.Solid.Solid.

+ +
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Attributes/Solids/Unidirectional_Carbon_Fiber.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Unidirectional__Carbon__Fiber_1_1Unidirectional__Carbon__Fiber.js b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Unidirectional__Carbon__Fiber_1_1Unidirectional__Carbon__Fiber.js new file mode 100644 index 00000000..4f49ca95 --- /dev/null +++ b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Unidirectional__Carbon__Fiber_1_1Unidirectional__Carbon__Fiber.js @@ -0,0 +1,12 @@ +var classSUAVE_1_1Attributes_1_1Solids_1_1Unidirectional__Carbon__Fiber_1_1Unidirectional__Carbon__Fiber = +[ + [ "__defaults__", "classSUAVE_1_1Attributes_1_1Solids_1_1Unidirectional__Carbon__Fiber_1_1Unidirectional__Carbon__Fiber.html#a31876879b88d8a6a094c3c1da88756af", null ], + [ "density", "classSUAVE_1_1Attributes_1_1Solids_1_1Unidirectional__Carbon__Fiber_1_1Unidirectional__Carbon__Fiber.html#a62dc2f5b53132b593b7b399a85cf8317", null ], + [ "minimum_gage_thickness", "classSUAVE_1_1Attributes_1_1Solids_1_1Unidirectional__Carbon__Fiber_1_1Unidirectional__Carbon__Fiber.html#a3f47b1ece804a6709a18ab5472cb1f9d", null ], + [ "ultimate_bearing_strength", "classSUAVE_1_1Attributes_1_1Solids_1_1Unidirectional__Carbon__Fiber_1_1Unidirectional__Carbon__Fiber.html#abdc64b2d4199256722ef54ccac2c1872", null ], + [ "ultimate_shear_strength", "classSUAVE_1_1Attributes_1_1Solids_1_1Unidirectional__Carbon__Fiber_1_1Unidirectional__Carbon__Fiber.html#a573784f1693b738609da73ddbdd8d204", null ], + [ "ultimate_tensile_strength", "classSUAVE_1_1Attributes_1_1Solids_1_1Unidirectional__Carbon__Fiber_1_1Unidirectional__Carbon__Fiber.html#a4dd615365d37c108a1ecd673b080d0ad", null ], + [ "yield_bearing_strength", "classSUAVE_1_1Attributes_1_1Solids_1_1Unidirectional__Carbon__Fiber_1_1Unidirectional__Carbon__Fiber.html#ad4558d56e95415584b8c4bcd834c2221", null ], + [ "yield_shear_strength", "classSUAVE_1_1Attributes_1_1Solids_1_1Unidirectional__Carbon__Fiber_1_1Unidirectional__Carbon__Fiber.html#a9258f24e081797527ea1cb0cb83c19dc", null ], + [ "yield_tensile_strength", "classSUAVE_1_1Attributes_1_1Solids_1_1Unidirectional__Carbon__Fiber_1_1Unidirectional__Carbon__Fiber.html#a4e515c1baea71e8b831d4cb39736beba", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Unidirectional__Carbon__Fiber_1_1Unidirectional__Carbon__Fiber.png b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Unidirectional__Carbon__Fiber_1_1Unidirectional__Carbon__Fiber.png new file mode 100644 index 00000000..6f45f982 Binary files /dev/null and b/doxygen/classSUAVE_1_1Attributes_1_1Solids_1_1Unidirectional__Carbon__Fiber_1_1Unidirectional__Carbon__Fiber.png differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Airfoils_1_1Airfoil_1_1Airfoil-members.html b/doxygen/classSUAVE_1_1Components_1_1Airfoils_1_1Airfoil_1_1Airfoil-members.html new file mode 100644 index 00000000..6b2c1120 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Airfoils_1_1Airfoil_1_1Airfoil-members.html @@ -0,0 +1,131 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ + + + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Airfoils_1_1Airfoil_1_1Airfoil.html b/doxygen/classSUAVE_1_1Components_1_1Airfoils_1_1Airfoil_1_1Airfoil.html new file mode 100644 index 00000000..4fb54efb --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Airfoils_1_1Airfoil_1_1Airfoil.html @@ -0,0 +1,221 @@ + + + + + + + +SUAVE: SUAVE.Components.Airfoils.Airfoil.Airfoil Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Components.Airfoils.Airfoil.Airfoil Class Reference
+
+
+
+Inheritance diagram for SUAVE.Components.Airfoils.Airfoil.Airfoil:
+
+
+ + +SUAVE.Components.Lofted_Body.Section +SUAVE.Components.Component.Component + +
+ + + + +

+Public Member Functions

def __defaults__ (self)
 
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Attributes

tag
 
thickness_to_chord
 
naca_4_series_airfoil
 
coordinate_file
 
points
 
- Public Attributes inherited from SUAVE.Components.Lofted_Body.Section
tag
 
prev
 
next
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 
+

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Components.Airfoils.Airfoil.Airfoil.__defaults__ ( self)
+
+
This sets the default values of a airfoil defined in SUAVE.
+
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+None
+
+Outputs:
+None
+
+Properties Used:
+N/A
+
+

Reimplemented from SUAVE.Components.Lofted_Body.Section.

+ +
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Airfoils/Airfoil.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Airfoils_1_1Airfoil_1_1Airfoil.js b/doxygen/classSUAVE_1_1Components_1_1Airfoils_1_1Airfoil_1_1Airfoil.js new file mode 100644 index 00000000..777277d7 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Airfoils_1_1Airfoil_1_1Airfoil.js @@ -0,0 +1,9 @@ +var classSUAVE_1_1Components_1_1Airfoils_1_1Airfoil_1_1Airfoil = +[ + [ "__defaults__", "classSUAVE_1_1Components_1_1Airfoils_1_1Airfoil_1_1Airfoil.html#a99c8fb72187cf75c949120c0bda56da7", null ], + [ "coordinate_file", "classSUAVE_1_1Components_1_1Airfoils_1_1Airfoil_1_1Airfoil.html#a8f361107e12e0d17b945176c76d0a291", null ], + [ "naca_4_series_airfoil", "classSUAVE_1_1Components_1_1Airfoils_1_1Airfoil_1_1Airfoil.html#a093a730dc8d697bd410f3872f122ca27", null ], + [ "points", "classSUAVE_1_1Components_1_1Airfoils_1_1Airfoil_1_1Airfoil.html#adb24bbb3f131149cfcf7af8a7345c8c2", null ], + [ "tag", "classSUAVE_1_1Components_1_1Airfoils_1_1Airfoil_1_1Airfoil.html#a1d5e04a8bd3064f0631d5ada5e483f39", null ], + [ "thickness_to_chord", "classSUAVE_1_1Components_1_1Airfoils_1_1Airfoil_1_1Airfoil.html#a5d2963e60ebb338047c0bca2242eea1a", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Airfoils_1_1Airfoil_1_1Airfoil.png b/doxygen/classSUAVE_1_1Components_1_1Airfoils_1_1Airfoil_1_1Airfoil.png new file mode 100644 index 00000000..5a338dde Binary files /dev/null and b/doxygen/classSUAVE_1_1Components_1_1Airfoils_1_1Airfoil_1_1Airfoil.png differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Component_1_1Component-members.html b/doxygen/classSUAVE_1_1Components_1_1Component_1_1Component-members.html index 523cb114..4e35f932 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Component_1_1Component-members.html +++ b/doxygen/classSUAVE_1_1Components_1_1Component_1_1Component-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -108,7 +118,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Components_1_1Component_1_1Component.html b/doxygen/classSUAVE_1_1Components_1_1Component_1_1Component.html index a013162c..41587d50 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Component_1_1Component.html +++ b/doxygen/classSUAVE_1_1Components_1_1Component_1_1Component.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Components.Component.Component Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -105,24 +112,22 @@
-SUAVE.Components.Envelope.Envelope -SUAVE.Components.Lofted_Body.Curve -SUAVE.Components.Lofted_Body.Section -SUAVE.Components.Lofted_Body.Segment -SUAVE.Components.Physical_Component.Physical_Component -SUAVE.Components.Systems.System.System -SUAVE.Components.Wings.Control_Surface.Control_Surface -SUAVE.Components.Wings.Airfoils.Airfoil.Airfoil -SUAVE.Components.Wings.Control_Surface.Control_Surface_Section -SUAVE.Components.Wings.Segment.Segment -SUAVE.Components.Energy.Energy.Energy -SUAVE.Components.Energy.Energy_Component.Energy_Component -SUAVE.Components.Landing_Gear.Landing_Gear.Landing_Gear -SUAVE.Components.Lofted_Body.Lofted_Body -SUAVE.Components.Payloads.Payload.Payload -SUAVE.Components.Propulsors.Propulsor.Propulsor - -
+SUAVE.Components.Envelope.Envelope +SUAVE.Components.Lofted_Body.Section +SUAVE.Components.Lofted_Body.Segment +SUAVE.Components.Physical_Component.Physical_Component +SUAVE.Components.Airfoils.Airfoil.Airfoil +SUAVE.Components.Lofted_Body_Segment.Segment.Segment +SUAVE.Components.Wings.Segment.Segment +SUAVE.Components.Energy.Energy_Component.Energy_Component +SUAVE.Components.Energy.Networks.Network.Network +SUAVE.Components.Landing_Gear.Landing_Gear.Landing_Gear +SUAVE.Components.Lofted_Body.Lofted_Body +SUAVE.Components.Payloads.Payload.Payload +SUAVE.Components.Systems.System.System +SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface + + @@ -137,6 +142,15 @@ + + + + + +

Public Member Functions

 origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 

Detailed Description

the base component class
@@ -177,6 +191,8 @@ 

SUAVE.Components.Lofted_Body.Section, SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion_LiNiMnCoO2_18650.Lithium_Ion_LiNiMnCoO2_18650, SUAVE.Components.Lofted_Body.Segment, SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion_LiFePO4_18650.Lithium_Ion_LiFePO4_18650, SUAVE.Components.Energy.Networks.Lift_Cruise.Lift_Cruise, SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller, SUAVE.Components.Wings.Wing.Wing, SUAVE.Components.Wings.All_Moving_Surface.All_Moving_Surface, SUAVE.Components.Energy.Converters.Rotor.Rotor, SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle, SUAVE.Components.Energy.Converters.Supersonic_Nozzle.Supersonic_Nozzle, SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion, SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate, SUAVE.Components.Wings.Main_Wing.Main_Wing, SUAVE.Components.Wings.Vertical_Tail.Vertical_Tail, SUAVE.Components.Energy.Converters.Compression_Nozzle.Compression_Nozzle, SUAVE.Components.Energy.Converters.de_Laval_Nozzle.de_Laval_Nozzle, SUAVE.Components.Wings.Stabilator.Stabilator, SUAVE.Components.Wings.Vertical_Tail_All_Moving.Vertical_Tail_All_Moving, SUAVE.Components.Energy.Networks.Solar.Solar, SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_One.Rotor_Wake_Fidelity_One, SUAVE.Components.Energy.Converters.Combustor.Combustor, SUAVE.Components.Energy.Networks.Turbofan.Turbofan, SUAVE.Components.Fuselages.Fuselage.Fuselage, SUAVE.Components.Wings.Horizontal_Tail.Horizontal_Tail, SUAVE.Components.Energy.Converters.Compressor.Compressor, SUAVE.Components.Energy.Converters.Fan.Fan, SUAVE.Components.Energy.Converters.Ram.Ram, SUAVE.Components.Energy.Converters.Turbine.Turbine, SUAVE.Components.Energy.Networks.Network.Network, SUAVE.Components.Energy.Networks.PyCycle.PyCycle, SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity, SUAVE.Components.Energy.Distributors.Solar_Logic.Solar_Logic, SUAVE.Components.Energy.Networks.Turboelectric_HTS_Ducted_Fan.Turboelectric_HTS_Ducted_Fan, SUAVE.Components.Wings.Control_Surfaces.Aileron.Aileron, SUAVE.Components.Energy.Networks.Battery_Cell_Cycler.Battery_Cell_Cycler, SUAVE.Components.Energy.Networks.Ducted_Fan.Ducted_Fan, SUAVE.Components.Energy.Processes.Thrust.Thrust, SUAVE.Components.Wings.Control_Surfaces.Elevator.Elevator, SUAVE.Components.Wings.Control_Surfaces.Flap.Flap, SUAVE.Components.Wings.Control_Surfaces.Rudder.Rudder, SUAVE.Components.Wings.Control_Surfaces.Slat.Slat, SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_Zero.Rotor_Wake_Fidelity_Zero, SUAVE.Components.Energy.Converters.Fuel_Cell.Fuel_Cell, SUAVE.Components.Energy.Converters.Motor.Motor, SUAVE.Components.Energy.Converters.Motor_HTS_Rotor.Motor_HTS_Rotor, SUAVE.Components.Energy.Converters.Motor_Lo_Fid.Motor_Lo_Fid, SUAVE.Components.Energy.Converters.Rocket_Combustor.Rocket_Combustor, SUAVE.Components.Energy.Networks.Internal_Combustion_Propeller.Internal_Combustion_Propeller, SUAVE.Components.Energy.Networks.Scramjet.Scramjet, SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super, SUAVE.Components.Energy.Converters.Gearbox.Gearbox, SUAVE.Components.Energy.Cooling.Cryogenic_Heat_Exchanger.Cryogenic_Heat_Exchanger, SUAVE.Components.Energy.Networks.Internal_Combustion_Propeller_Constant_Speed.Internal_Combustion_Propeller_Constant_Speed, SUAVE.Components.Energy.Converters.Internal_Combustion_Engine.Internal_Combustion_Engine, SUAVE.Components.Energy.Converters.Propeller_Lo_Fid.Propeller_Lo_Fid, SUAVE.Components.Energy.Networks.Battery_Ducted_Fan.Battery_Ducted_Fan, SUAVE.Components.Energy.Networks.Serial_Hybrid_Ducted_Fan.Serial_Hybrid_Ducted_Fan, SUAVE.Components.Energy.Storages.Batteries.Battery.Battery, SUAVE.Components.Landing_Gear.Landing_Gear.Landing_Gear, SUAVE.Components.Physical_Component.Physical_Component, SUAVE.Components.Energy.Converters.Generator_Zero_Fid.Generator_Zero_Fid, SUAVE.Components.Energy.Converters.Turboelectric.Turboelectric, SUAVE.Components.Energy.Networks.Liquid_Rocket.Liquid_Rocket, SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Aluminum_Air.Aluminum_Air, SUAVE.Components.Systems.System.System, SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Lithium_Air.Lithium_Air, SUAVE.Components.Envelope.Envelope, SUAVE.Components.Landing_Gear.Main_Landing_Gear.Main_Landing_Gear, SUAVE.Components.Nacelles.Nacelle.Nacelle, SUAVE.Components.Energy.Converters.Shaft_Power_Off_Take.Shaft_Power_Off_Take, SUAVE.Components.Energy.Cooling.Cryocooler.Cryocooler, SUAVE.Components.Energy.Networks.Ramjet.Ramjet, SUAVE.Components.Landing_Gear.Nose_Landing_Gear.Nose_Landing_Gear, SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_Two.Rotor_Wake_Fidelity_Two, SUAVE.Components.Energy.Converters.Solar_Panel.Solar_Panel, SUAVE.Components.Energy.Peripherals.Avionics.Avionics, SUAVE.Components.Energy.Peripherals.Payload.Payload, SUAVE.Components.Energy.Storages.Fuel_Tanks.Fuel_Tank.Fuel_Tank, SUAVE.Components.Payloads.Payload.Payload, SUAVE.Components.Energy.Charging.Charging.Charging, SUAVE.Components.Energy.Distributors.Cryogenic_Lead.Cryogenic_Lead, SUAVE.Components.Energy.Energy_Component.Energy_Component, SUAVE.Components.Energy.Processes.Rocket_Thrust.Rocket_Thrust, SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Sulfur.Lithium_Sulfur, SUAVE.Components.Energy.Converters.Lift_Rotor.Lift_Rotor, SUAVE.Components.Energy.Converters.Propeller.Propeller, SUAVE.Components.Lofted_Body.Lofted_Body, SUAVE.Components.Lofted_Body_Segment.Segment.Segment, SUAVE.Components.Energy.Distributors.Electronic_Speed_Controller.Electronic_Speed_Controller, SUAVE.Components.Energy.Distributors.HTS_DC_Supply.HTS_DC_Supply, SUAVE.Components.Wings.Segment.Segment, SUAVE.Components.Airfoils.Airfoil.Airfoil, and SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface.

+


The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Components_1_1Component_1_1Component.js b/doxygen/classSUAVE_1_1Components_1_1Component_1_1Component.js index 9e83bea7..ff40ec74 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Component_1_1Component.js +++ b/doxygen/classSUAVE_1_1Components_1_1Component_1_1Component.js @@ -1,6 +1,9 @@ var classSUAVE_1_1Components_1_1Component_1_1Component = [ [ "__defaults__", "classSUAVE_1_1Components_1_1Component_1_1Component.html#a2d9252624c70b5d919bc9ec4809aaeff", null ], + [ "generative_design_characteristics", "classSUAVE_1_1Components_1_1Component_1_1Component.html#a9b0142ce837eb8fd7f11b0581acee372", null ], + [ "generative_design_max_per_vehicle", "classSUAVE_1_1Components_1_1Component_1_1Component.html#ae7305ad76eff4eb0eeb3ef2eaa198cbb", null ], + [ "generative_design_special_parent", "classSUAVE_1_1Components_1_1Component_1_1Component.html#aa6dedec164a94dbb1d776aeb42589475", null ], [ "origin", "classSUAVE_1_1Components_1_1Component_1_1Component.html#a73f01c28d509653b176d616ddf5774d6", null ], [ "tag", "classSUAVE_1_1Components_1_1Component_1_1Component.html#a03eb542a5d248132cad459e2b1da0712", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Component_1_1Component.png b/doxygen/classSUAVE_1_1Components_1_1Component_1_1Component.png index b321207e..58910f4b 100644 Binary files a/doxygen/classSUAVE_1_1Components_1_1Component_1_1Component.png and b/doxygen/classSUAVE_1_1Components_1_1Component_1_1Component.png differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Component_1_1Container-members.html b/doxygen/classSUAVE_1_1Components_1_1Component_1_1Container-members.html index ff8555c6..04f297f5 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Component_1_1Container-members.html +++ b/doxygen/classSUAVE_1_1Components_1_1Component_1_1Container-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -106,7 +113,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Components_1_1Component_1_1Container.html b/doxygen/classSUAVE_1_1Components_1_1Component_1_1Container.html index 6d154d14..89c6584e 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Component_1_1Container.html +++ b/doxygen/classSUAVE_1_1Components_1_1Component_1_1Container.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Components.Component.Container Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -104,14 +111,15 @@
-SUAVE.Components.Lofted_Body.CurveContainer -SUAVE.Components.Lofted_Body.SectionContainer -SUAVE.Components.Physical_Component.Container -SUAVE.Components.Fuselages.Fuselage.Container -SUAVE.Components.Payloads.Payload.Container -SUAVE.Components.Propulsors.Propulsor.Container - -
+SUAVE.Components.Lofted_Body.Section_Container +SUAVE.Components.Physical_Component.Container +SUAVE.Components.Energy.Networks.Network.Container +SUAVE.Components.Fuselages.Fuselage.Container +SUAVE.Components.Payloads.Payload.Container +SUAVE.Components.Wings.Wing.Container +SUAVE.Vehicle.Vehicle_Mass_Container + + @@ -138,7 +146,7 @@ + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Components_1_1Component_1_1Container.png b/doxygen/classSUAVE_1_1Components_1_1Component_1_1Container.png index 348806a8..62b621d5 100644 Binary files a/doxygen/classSUAVE_1_1Components_1_1Component_1_1Container.png and b/doxygen/classSUAVE_1_1Components_1_1Component_1_1Container.png differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Configs_1_1Config_1_1Config-members.html b/doxygen/classSUAVE_1_1Components_1_1Configs_1_1Config_1_1Config-members.html index 6f7e6a08..72eb1ee8 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Configs_1_1Config_1_1Config-members.html +++ b/doxygen/classSUAVE_1_1Components_1_1Configs_1_1Config_1_1Config-members.html @@ -1,9 +1,9 @@ - + - +SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ @@ -57,9 +60,11 @@

Static Public Attributes

SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -99,7 +106,44 @@

This is the complete list of members for SUAVE.Components.Configs.Config.Config, including all inherited members.

+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
__defaults__(self)SUAVE.Components.Configs.Config.Config
__delattr__(self, k)SUAVE.Core.Data.Data
__getattribute__(self, k)SUAVE.Core.Data.Data
__init__(self, *args, **kwarg)SUAVE.Vehicle.Vehicle
__iter__(self)SUAVE.Core.Data.Data
__new__(cls, *args, **kwarg)SUAVE.Core.Data.Data
__setattr__(self, k, v)SUAVE.Core.Data.Data
__str__(self, indent='')SUAVE.Core.Data.Data
append(self, value, key=None)SUAVE.Core.Data.Data
append_component(self, component)SUAVE.Vehicle.Vehicle
append_or_update(self, other)SUAVE.Core.Data.Data
center_of_gravity(self)SUAVE.Vehicle.Vehicle
costs (defined in SUAVE.Vehicle.Vehicle)SUAVE.Vehicle.Vehicle
dataname(self)SUAVE.Core.Data.Data
deep_get(self, keys)SUAVE.Core.Data.Data
deep_set(self, keys, val)SUAVE.Core.Data.Data
do_recursive(self, method, other=None, default=None)SUAVE.Core.Data.Data
envelope (defined in SUAVE.Vehicle.Vehicle)SUAVE.Vehicle.Vehicle
find_component_root(self, component)SUAVE.Vehicle.Vehicle
fuselages (defined in SUAVE.Vehicle.Vehicle)SUAVE.Vehicle.Vehicle
get_bases(self)SUAVE.Core.Data.Data
itervalues(self)SUAVE.Core.Data.Data
landing_gear (defined in SUAVE.Vehicle.Vehicle)SUAVE.Vehicle.Vehicle
mass_properties (defined in SUAVE.Vehicle.Vehicle)SUAVE.Vehicle.Vehicle
nacelles (defined in SUAVE.Vehicle.Vehicle)SUAVE.Vehicle.Vehicle
networks (defined in SUAVE.Vehicle.Vehicle)SUAVE.Vehicle.Vehicle
pack_array(self, output='vector')SUAVE.Core.Data.Data
passengers (defined in SUAVE.Vehicle.Vehicle)SUAVE.Vehicle.Vehicle
payload (defined in SUAVE.Vehicle.Vehicle)SUAVE.Vehicle.Vehicle
performance (defined in SUAVE.Vehicle.Vehicle)SUAVE.Vehicle.Vehicle
reference_area (defined in SUAVE.Vehicle.Vehicle)SUAVE.Vehicle.Vehicle
sum_mass(self)SUAVE.Vehicle.Vehicle
systems (defined in SUAVE.Vehicle.Vehicle)SUAVE.Vehicle.Vehicle
tag (defined in SUAVE.Components.Configs.Config.Config)SUAVE.Components.Configs.Config.Config
typestring(self)SUAVE.Core.Data.Data
unpack_array(self, M)SUAVE.Core.Data.Data
update(self, other)SUAVE.Core.Data.Data
values(self)SUAVE.Core.Data.Data
wings (defined in SUAVE.Vehicle.Vehicle)SUAVE.Vehicle.Vehicle
@@ -107,7 +151,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Components_1_1Configs_1_1Config_1_1Config.html b/doxygen/classSUAVE_1_1Components_1_1Configs_1_1Config_1_1Config.html index a2a00570..2d1c4290 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Configs_1_1Config_1_1Config.html +++ b/doxygen/classSUAVE_1_1Components_1_1Configs_1_1Config_1_1Config.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Components.Configs.Config.Config Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -105,19 +112,114 @@
- -
+SUAVE.Vehicle.Vehicle +SUAVE.Core.Data.Data + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Vehicle.Vehicle
def __init__ (self, *args, **kwarg)
 
def find_component_root (self, component)
 
def append_component (self, component)
 
def sum_mass (self)
 
def center_of_gravity (self)
 
- Public Member Functions inherited from SUAVE.Core.Data.Data
def __getattribute__ (self, k)
 
def __setattr__ (self, k, v)
 
def __delattr__ (self, k)
 
def __new__ (cls, *args, **kwarg)
 
def typestring (self)
 
def dataname (self)
 
def __str__ (self, indent='')
 
def __iter__ (self)
 
def itervalues (self)
 
def values (self)
 
def update (self, other)
 
def append_or_update (self, other)
 
def get_bases (self)
 
def append (self, value, key=None)
 
def deep_set (self, keys, val)
 
def deep_get (self, keys)
 
def pack_array (self, output='vector')
 
def unpack_array (self, M)
 
def do_recursive (self, method, other=None, default=None)
 
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + +

Public Attributes

 tag
 
- Public Attributes inherited from SUAVE.Vehicle.Vehicle
tag
 
fuselages
 
wings
 
networks
 
nacelles
 
systems
 
mass_properties
 
payload
 
costs
 
envelope
 
landing_gear
 
reference_area
 
passengers
 
performance
 

Detailed Description

SUAVE.Components.Config()
@@ -162,6 +264,8 @@ 

SUAVE.Vehicle.Vehicle.

+


The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Components_1_1Configs_1_1Config_1_1Config.png b/doxygen/classSUAVE_1_1Components_1_1Configs_1_1Config_1_1Config.png index 7887e3d1..9e49db23 100644 Binary files a/doxygen/classSUAVE_1_1Components_1_1Configs_1_1Config_1_1Config.png and b/doxygen/classSUAVE_1_1Components_1_1Configs_1_1Config_1_1Config.png differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Costs_1_1Costs_1_1Industrial__Costs-members.html b/doxygen/classSUAVE_1_1Components_1_1Costs_1_1Costs_1_1Industrial__Costs-members.html index e0070e85..ba069fac 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Costs_1_1Costs_1_1Industrial__Costs-members.html +++ b/doxygen/classSUAVE_1_1Components_1_1Costs_1_1Costs_1_1Industrial__Costs-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -122,7 +129,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Components_1_1Costs_1_1Costs_1_1Industrial__Costs.html b/doxygen/classSUAVE_1_1Components_1_1Costs_1_1Costs_1_1Industrial__Costs.html index 0cf4be17..5b3518be 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Costs_1_1Costs_1_1Industrial__Costs.html +++ b/doxygen/classSUAVE_1_1Components_1_1Costs_1_1Costs_1_1Industrial__Costs.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Components.Costs.Costs.Industrial_Costs Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -103,9 +110,7 @@ Inheritance diagram for SUAVE.Components.Costs.Costs.Industrial_Costs:
- - - +
@@ -57,9 +60,11 @@

@@ -218,7 +223,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Components_1_1Costs_1_1Costs_1_1Operating__Costs-members.html b/doxygen/classSUAVE_1_1Components_1_1Costs_1_1Costs_1_1Operating__Costs-members.html index a9f25edb..1477d289 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Costs_1_1Costs_1_1Operating__Costs-members.html +++ b/doxygen/classSUAVE_1_1Components_1_1Costs_1_1Costs_1_1Operating__Costs-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -116,7 +123,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Components_1_1Costs_1_1Costs_1_1Operating__Costs.html b/doxygen/classSUAVE_1_1Components_1_1Costs_1_1Costs_1_1Operating__Costs.html index 7f07073f..ea9ad836 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Costs_1_1Costs_1_1Operating__Costs.html +++ b/doxygen/classSUAVE_1_1Components_1_1Costs_1_1Costs_1_1Operating__Costs.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Components.Costs.Costs.Operating_Costs Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -103,9 +110,7 @@ Inheritance diagram for SUAVE.Components.Costs.Costs.Operating_Costs:
- - - +
@@ -57,9 +60,11 @@

@@ -200,7 +205,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Charging_1_1Charging_1_1Charging-members.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Charging_1_1Charging_1_1Charging-members.html new file mode 100644 index 00000000..350403b3 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Charging_1_1Charging_1_1Charging-members.html @@ -0,0 +1,131 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
SUAVE.Components.Energy.Charging.Charging.Charging Member List
+
+
+ +

This is the complete list of members for SUAVE.Components.Energy.Charging.Charging.Charging, including all inherited members.

+ + + + + + + + + + + + + +
__defaults__(self)SUAVE.Components.Energy.Charging.Charging.Charging
C_rate (defined in SUAVE.Components.Energy.Charging.Charging.Charging)SUAVE.Components.Energy.Charging.Charging.Charging
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
SOC_cutoff (defined in SUAVE.Components.Energy.Charging.Charging.Charging)SUAVE.Components.Energy.Charging.Charging.Charging
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Charging_1_1Charging_1_1Charging.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Charging_1_1Charging_1_1Charging.html new file mode 100644 index 00000000..dc2f385a --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Charging_1_1Charging_1_1Charging.html @@ -0,0 +1,231 @@ + + + + + + + +SUAVE: SUAVE.Components.Energy.Charging.Charging.Charging Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Components.Energy.Charging.Charging.Charging Class Reference
+
+
+
+Inheritance diagram for SUAVE.Components.Energy.Charging.Charging.Charging:
+
+
+ + +SUAVE.Components.Energy.Energy_Component.Energy_Component +SUAVE.Components.Physical_Component.Physical_Component +SUAVE.Components.Component.Component + +
+ + + + +

+Public Member Functions

def __defaults__ (self)
 
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Attributes

C_rate
 
SOC_cutoff
 
- Public Attributes inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
inputs
 
outputs
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 
+

Detailed Description

+
A class representing Charging.
+
+Assumptions:
+None
+
+Source:
+N/A
+

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Components.Energy.Charging.Charging.Charging.__defaults__ ( self)
+
+
This sets the default charging C rate and SOC cutoff when battery is fully charged.
+
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+None
+
+Outputs:
+None
+
+Properties Used:
+N/A
+
+

Reimplemented from SUAVE.Components.Energy.Energy_Component.Energy_Component.

+ +
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Energy/Charging/Charging.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Charging_1_1Charging_1_1Charging.js b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Charging_1_1Charging_1_1Charging.js new file mode 100644 index 00000000..96d0f35d --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Charging_1_1Charging_1_1Charging.js @@ -0,0 +1,6 @@ +var classSUAVE_1_1Components_1_1Energy_1_1Charging_1_1Charging_1_1Charging = +[ + [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Charging_1_1Charging_1_1Charging.html#a0b21dc5aa5f4c1618dff7a2269d9256f", null ], + [ "C_rate", "classSUAVE_1_1Components_1_1Energy_1_1Charging_1_1Charging_1_1Charging.html#aab57eaee1dd67d50d4f84e0146836104", null ], + [ "SOC_cutoff", "classSUAVE_1_1Components_1_1Energy_1_1Charging_1_1Charging_1_1Charging.html#a808e76e8a2e6de2a1329d3423bb2c291", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Charging_1_1Charging_1_1Charging.png b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Charging_1_1Charging_1_1Charging.png new file mode 100644 index 00000000..24d2fc5e Binary files /dev/null and b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Charging_1_1Charging_1_1Charging.png differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Combustor_1_1Combustor-members.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Combustor_1_1Combustor-members.html index 59da1856..ac0e49e6 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Combustor_1_1Combustor-members.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Combustor_1_1Combustor-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -99,18 +106,27 @@

This is the complete list of members for SUAVE.Components.Energy.Converters.Combustor.Combustor, including all inherited members.

- - - - + + + + + + + + - - - - - - - + + + + + + + + + + + +
__defaults__(self)SUAVE.Components.Energy.Converters.Combustor.Combustor
alphac (defined in SUAVE.Components.Energy.Converters.Combustor.Combustor)SUAVE.Components.Energy.Converters.Combustor.Combustor
area_ratio (defined in SUAVE.Components.Energy.Converters.Combustor.Combustor)SUAVE.Components.Energy.Converters.Combustor.Combustor
compute(self, conditions)SUAVE.Components.Energy.Converters.Combustor.Combustor
compute_rayleigh(self, conditions)SUAVE.Components.Energy.Converters.Combustor.Combustor
absolute_sensible_enthalpy (defined in SUAVE.Components.Energy.Converters.Combustor.Combustor)SUAVE.Components.Energy.Converters.Combustor.Combustor
alphac (defined in SUAVE.Components.Energy.Converters.Combustor.Combustor)SUAVE.Components.Energy.Converters.Combustor.Combustor
area_ratio (defined in SUAVE.Components.Energy.Converters.Combustor.Combustor)SUAVE.Components.Energy.Converters.Combustor.Combustor
axial_fuel_velocity_ratio (defined in SUAVE.Components.Energy.Converters.Combustor.Combustor)SUAVE.Components.Energy.Converters.Combustor.Combustor
burner_drag_coefficient (defined in SUAVE.Components.Energy.Converters.Combustor.Combustor)SUAVE.Components.Energy.Converters.Combustor.Combustor
compute(self, conditions)SUAVE.Components.Energy.Converters.Combustor.Combustor
compute_rayleigh(self, conditions)SUAVE.Components.Energy.Converters.Combustor.Combustor
compute_supersonic_combustion(self, conditions)SUAVE.Components.Energy.Converters.Combustor.Combustor
fuel_data (defined in SUAVE.Components.Energy.Converters.Combustor.Combustor)SUAVE.Components.Energy.Converters.Combustor.Combustor
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Energy.Converters.Combustor.Combustor)SUAVE.Components.Energy.Converters.Combustor.Combustor
turbine_inlet_temperature (defined in SUAVE.Components.Energy.Converters.Combustor.Combustor)SUAVE.Components.Energy.Converters.Combustor.Combustor
fuel_equivalency_ratio (defined in SUAVE.Components.Energy.Converters.Combustor.Combustor)SUAVE.Components.Energy.Converters.Combustor.Combustor
fuel_velocity_ratio (defined in SUAVE.Components.Energy.Converters.Combustor.Combustor)SUAVE.Components.Energy.Converters.Combustor.Combustor
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Energy.Converters.Combustor.Combustor)SUAVE.Components.Energy.Converters.Combustor.Combustor
turbine_inlet_temperature (defined in SUAVE.Components.Energy.Converters.Combustor.Combustor)SUAVE.Components.Energy.Converters.Combustor.Combustor
@@ -118,7 +134,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Combustor_1_1Combustor.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Combustor_1_1Combustor.html index c6d993c0..be19f93e 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Combustor_1_1Combustor.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Combustor_1_1Combustor.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Components.Energy.Converters.Combustor.Combustor Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -108,8 +115,8 @@ SUAVE.Components.Energy.Energy_Component.Energy_Component SUAVE.Components.Physical_Component.Physical_Component SUAVE.Components.Component.Component - -
+ + @@ -119,15 +126,8 @@ - - - - - - - - - + +

Public Member Functions

 
def compute_rayleigh (self, conditions)
 
- Public Member Functions inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
def compute_supersonic_combustion (self, conditions)
 
@@ -146,6 +146,21 @@ + + + + + + + + + + @@ -173,6 +188,15 @@ + + + + + +

Public Attributes

 area_ratio
 
axial_fuel_velocity_ratio
 
fuel_velocity_ratio
 
burner_drag_coefficient
 
absolute_sensible_enthalpy
 
fuel_equivalency_ratio
 
- Public Attributes inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
 inputs
 origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 

Detailed Description

This provides output values for a combustor
@@ -216,6 +240,8 @@ 

SUAVE.Components.Energy.Energy_Component.Energy_Component.

+

@@ -261,6 +287,7 @@

+

◆ compute_supersonic_combustion()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Components.Energy.Converters.Combustor.Combustor.compute_supersonic_combustion ( self,
 conditions 
)
+
+
This function computes the output values for supersonic  
+combustion (Scramjet).  This will be done using stream thrust 
+analysis. 
+
+Assumptions: 
+Constant Pressure Combustion      
+Flow is in axial direction at all times 
+Flow properities at exit are 1-Da averages 
+
+Source: 
+Heiser, William H., Pratt, D. T., Daley, D. H., and Unmeel, B. M., 
+"Hypersonic Airbreathing Propulsion", 1994 
+Chapter 4 - pgs. 175-180
+
+Inputs: 
+conditions.freestream. 
+   isentropic_expansion_factor          [-] 
+   specific_heat_at_constant_pressure   [J/(kg K)] 
+   temperature                          [K] 
+   stagnation_temperature               [K]
+   universal_gas_constant               [J/(kg K)]  
+self.inputs. 
+   stagnation_temperature               [K] 
+   stagnation_pressure                  [Pa] 
+   inlet_nozzle                         [-] 
+  
+Outputs: 
+self.outputs. 
+   stagnation_temperature               [K] 
+   stagnation_pressure                  [Pa] 
+   stagnation_enthalpy                  [J/kg] 
+   fuel_to_air_ratio                    [-] 
+   static_temperature                   [K] 
+   static_pressure                      [Pa] 
+   velocity                             [m/s] 
+   mach_number                          [-]          
+
+       Properties Used: 
+  self.fuel_data.specific_energy       [J/kg] 
+  self.efficiency                      [-]
+  self.axial_fuel_velocity_ratio       [-] 
+  self.fuel_velocity_ratio             [-] 
+  self.burner_drag_coefficient         [-] 
+  self.temperature_reference           [K] 
+  self.absolute_sensible_enthalpy      [J/kg] 
+  self.specific_heat_constant_pressure [J/(kg K)] 
+
+

The documentation for this class was generated from the following file:
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Energy/Converters/Combustor.py
@@ -351,7 +451,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Combustor_1_1Combustor.js b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Combustor_1_1Combustor.js index 342beffb..f8c2b820 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Combustor_1_1Combustor.js +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Combustor_1_1Combustor.js @@ -3,9 +3,15 @@ var classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Combustor_1_1Combustor = [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Combustor_1_1Combustor.html#a2a0f7c8f68137486dd2fec4e90f64ad2", null ], [ "compute", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Combustor_1_1Combustor.html#ab7ff2679c7aa46e60388a448b7d44120", null ], [ "compute_rayleigh", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Combustor_1_1Combustor.html#a8aa11c99e7ed4fa7baa65c351d14a546", null ], + [ "compute_supersonic_combustion", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Combustor_1_1Combustor.html#a980b35df47fb691992c7adc4ef39ef69", null ], + [ "absolute_sensible_enthalpy", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Combustor_1_1Combustor.html#af247bc90f49f5d9c26d0406e431ae069", null ], [ "alphac", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Combustor_1_1Combustor.html#abad75b1005d3585a7a56d4848997b5f9", null ], [ "area_ratio", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Combustor_1_1Combustor.html#aa467ad467292f60503afd8880a30ae23", null ], + [ "axial_fuel_velocity_ratio", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Combustor_1_1Combustor.html#a19e23e79e1d10eb0f199ce7bae16a278", null ], + [ "burner_drag_coefficient", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Combustor_1_1Combustor.html#a532e44801b264c7e3df4566dc81b925d", null ], [ "fuel_data", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Combustor_1_1Combustor.html#a167de0d8770cf94173f256e36921e3ed", null ], + [ "fuel_equivalency_ratio", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Combustor_1_1Combustor.html#a7a9feff6489f8f9b1701bb47a52d9bfb", null ], + [ "fuel_velocity_ratio", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Combustor_1_1Combustor.html#a2914e60c6996b7112ae0958dfd959888", null ], [ "tag", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Combustor_1_1Combustor.html#ab3a4977f8218e87a868b4693c7d06873", null ], [ "turbine_inlet_temperature", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Combustor_1_1Combustor.html#a42bc5e129081949bec715e938e3a7536", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Compression__Nozzle_1_1Compression__Nozzle-members.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Compression__Nozzle_1_1Compression__Nozzle-members.html index 211fd141..71ef429a 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Compression__Nozzle_1_1Compression__Nozzle-members.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Compression__Nozzle_1_1Compression__Nozzle-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -100,15 +107,22 @@ - - - - - - - + + + + + + + + + + + + + +
__defaults__(self)SUAVE.Components.Energy.Converters.Compression_Nozzle.Compression_Nozzle
compressibility_effects (defined in SUAVE.Components.Energy.Converters.Compression_Nozzle.Compression_Nozzle)SUAVE.Components.Energy.Converters.Compression_Nozzle.Compression_Nozzle
compute(self, conditions)SUAVE.Components.Energy.Converters.Compression_Nozzle.Compression_Nozzle
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
polytropic_efficiency (defined in SUAVE.Components.Energy.Converters.Compression_Nozzle.Compression_Nozzle)SUAVE.Components.Energy.Converters.Compression_Nozzle.Compression_Nozzle
pressure_ratio (defined in SUAVE.Components.Energy.Converters.Compression_Nozzle.Compression_Nozzle)SUAVE.Components.Energy.Converters.Compression_Nozzle.Compression_Nozzle
compression_levels (defined in SUAVE.Components.Energy.Converters.Compression_Nozzle.Compression_Nozzle)SUAVE.Components.Energy.Converters.Compression_Nozzle.Compression_Nozzle
compute(self, conditions)SUAVE.Components.Energy.Converters.Compression_Nozzle.Compression_Nozzle
compute_scramjet(self, conditions)SUAVE.Components.Energy.Converters.Compression_Nozzle.Compression_Nozzle
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
polytropic_efficiency (defined in SUAVE.Components.Energy.Converters.Compression_Nozzle.Compression_Nozzle)SUAVE.Components.Energy.Converters.Compression_Nozzle.Compression_Nozzle
pressure_ratio (defined in SUAVE.Components.Energy.Converters.Compression_Nozzle.Compression_Nozzle)SUAVE.Components.Energy.Converters.Compression_Nozzle.Compression_Nozzle
pressure_recovery (defined in SUAVE.Components.Energy.Converters.Compression_Nozzle.Compression_Nozzle)SUAVE.Components.Energy.Converters.Compression_Nozzle.Compression_Nozzle
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Energy.Converters.Compression_Nozzle.Compression_Nozzle)SUAVE.Components.Energy.Converters.Compression_Nozzle.Compression_Nozzle
theta (defined in SUAVE.Components.Energy.Converters.Compression_Nozzle.Compression_Nozzle)SUAVE.Components.Energy.Converters.Compression_Nozzle.Compression_Nozzle
@@ -116,7 +130,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Compression__Nozzle_1_1Compression__Nozzle.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Compression__Nozzle_1_1Compression__Nozzle.html index bdd10516..7e6292d0 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Compression__Nozzle_1_1Compression__Nozzle.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Compression__Nozzle_1_1Compression__Nozzle.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Components.Energy.Converters.Compression_Nozzle.Compression_Nozzle Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -108,8 +115,8 @@ SUAVE.Components.Energy.Energy_Component.Energy_Component SUAVE.Components.Physical_Component.Physical_Component SUAVE.Components.Component.Component - -
+ + @@ -117,15 +124,8 @@ - - - - - - - - - + +

Public Member Functions

 
def compute (self, conditions)
 
- Public Member Functions inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
def compute_scramjet (self, conditions)
 
@@ -138,9 +138,18 @@ + + + + + + @@ -168,6 +177,15 @@ + + + + + +

Public Attributes

 pressure_ratio
 
pressure_recovery
 
 compressibility_effects
 
compression_levels
 
theta
 
- Public Attributes inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
 inputs
 origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 

Detailed Description

This is a nozzle component intended for use in compression.
@@ -212,6 +230,8 @@ 

SUAVE.Components.Energy.Energy_Component.Energy_Component.

+

@@ -273,6 +293,75 @@

+

◆ compute_scramjet()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Components.Energy.Converters.Compression_Nozzle.Compression_Nozzle.compute_scramjet ( self,
 conditions 
)
+
+
This function computes the compression of a scramjet 
+using shock trains.  
+    
+Assumptions: 
+    
+Source: 
+Heiser, William H., Pratt, D. T., Daley, D. H., and Unmeel, B. M.,  
+"Hypersonic Airbreathing Propulsion", 1994  
+Chapter 4 - pgs. 175-180
+
+Inputs: 
+   conditions.freestream. 
+   isentropic_expansion_factor        [-] 
+   specific_heat_at_constant_pressure [J/(kg K)] 
+   pressure                           [Pa] 
+   gas_specific_constant              [J/(kg K)] 
+   temperature                        [K] 
+   mach_number                        [-] 
+   velocity                           [m/s] 
+    
+self.inputs. 
+   stagnation_temperature             [K] 
+   stagnation_pressure                [Pa] 
+    
+Outputs: 
+self.outputs. 
+   stagnation_temperature             [K] 
+   stagnation_pressure                [Pa] 
+   stagnation_enthalpy                [J/kg] 
+   mach_number                        [-] 
+   static_temperature                 [K] 
+   static_enthalpy                    [J/kg] 
+   velocity                           [m/s] 
+   specific_heat_at_constant_pressure [J/(kg K)] 
+    
+Properties Used: 
+self. 
+   efficiency                         [-] 
+   shock_count                        [-] 
+   theta                              [Rad] 
 
@@ -287,7 +376,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Compression__Nozzle_1_1Compression__Nozzle.js b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Compression__Nozzle_1_1Compression__Nozzle.js index 2aa790a5..19b746c7 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Compression__Nozzle_1_1Compression__Nozzle.js +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Compression__Nozzle_1_1Compression__Nozzle.js @@ -2,8 +2,12 @@ var classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Compression__Nozzle_1_1C [ [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Compression__Nozzle_1_1Compression__Nozzle.html#aac9c90445bd9c7d1bdfd4fad2f668b1e", null ], [ "compute", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Compression__Nozzle_1_1Compression__Nozzle.html#acdaf2c6eec5fbe7f8f56b2254b6461a0", null ], + [ "compute_scramjet", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Compression__Nozzle_1_1Compression__Nozzle.html#aee5079c83a80b3552f25b8b27119d8f8", null ], [ "compressibility_effects", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Compression__Nozzle_1_1Compression__Nozzle.html#a20017416230653893b8558056ad4115b", null ], + [ "compression_levels", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Compression__Nozzle_1_1Compression__Nozzle.html#a790ea83993df7aac9e1e61a4901bfcc8", null ], [ "polytropic_efficiency", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Compression__Nozzle_1_1Compression__Nozzle.html#a189581236c66eaa42b59787a0a21fab6", null ], [ "pressure_ratio", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Compression__Nozzle_1_1Compression__Nozzle.html#a001dd3301c2cefa6421b41c417338534", null ], - [ "tag", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Compression__Nozzle_1_1Compression__Nozzle.html#adc44bf1576cef3fbefa090fd7468bbe5", null ] + [ "pressure_recovery", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Compression__Nozzle_1_1Compression__Nozzle.html#a3f5af1ddd3aebecd86874597bd739cb7", null ], + [ "tag", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Compression__Nozzle_1_1Compression__Nozzle.html#adc44bf1576cef3fbefa090fd7468bbe5", null ], + [ "theta", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Compression__Nozzle_1_1Compression__Nozzle.html#aae418abf3c701dea76208a0ab46ea73f", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Compressor_1_1Compressor-members.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Compressor_1_1Compressor-members.html index dc1e05e9..7d5aa03f 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Compressor_1_1Compressor-members.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Compressor_1_1Compressor-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -100,14 +107,17 @@ - - - - - - - - + + + + + + + + + + +
__defaults__(self)SUAVE.Components.Energy.Converters.Compressor.Compressor
compute(self, conditions)SUAVE.Components.Energy.Converters.Compressor.Compressor
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
polytropic_efficiency (defined in SUAVE.Components.Energy.Converters.Compressor.Compressor)SUAVE.Components.Energy.Converters.Compressor.Compressor
pressure_ratio (defined in SUAVE.Components.Energy.Converters.Compressor.Compressor)SUAVE.Components.Energy.Converters.Compressor.Compressor
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Energy.Converters.Compressor.Compressor)SUAVE.Components.Energy.Converters.Compressor.Compressor
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
polytropic_efficiency (defined in SUAVE.Components.Energy.Converters.Compressor.Compressor)SUAVE.Components.Energy.Converters.Compressor.Compressor
pressure_ratio (defined in SUAVE.Components.Energy.Converters.Compressor.Compressor)SUAVE.Components.Energy.Converters.Compressor.Compressor
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Energy.Converters.Compressor.Compressor)SUAVE.Components.Energy.Converters.Compressor.Compressor
@@ -115,7 +125,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Compressor_1_1Compressor.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Compressor_1_1Compressor.html index dde830c0..ec8cd42d 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Compressor_1_1Compressor.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Compressor_1_1Compressor.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Components.Energy.Converters.Compressor.Compressor Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -108,8 +115,8 @@ SUAVE.Components.Energy.Energy_Component.Energy_Component SUAVE.Components.Physical_Component.Physical_Component SUAVE.Components.Component.Component - -
+ + @@ -117,15 +124,6 @@ - - - - - - - - -

Public Member Functions

 
def compute (self, conditions)
 
- Public Member Functions inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
@@ -165,6 +163,15 @@ + + + + + +

Public Attributes

 origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 

Detailed Description

This is a compressor component typically used in a turbofan.
@@ -208,6 +215,8 @@ 

SUAVE.Components.Energy.Energy_Component.Energy_Component.

+

@@ -277,7 +286,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Expansion__Nozzle_1_1Expansion__Nozzle-members.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Expansion__Nozzle_1_1Expansion__Nozzle-members.html index 7f0f263e..bf597fa6 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Expansion__Nozzle_1_1Expansion__Nozzle-members.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Expansion__Nozzle_1_1Expansion__Nozzle-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -106,41 +113,44 @@ density (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic etapold (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic gamma (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic - h_out (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic - ht_out (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic - i_high (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic - i_low (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic - inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component - Mach (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic - mach_number (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic - mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component - Mo (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic - origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component - outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component - P_out (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic - pid (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic - Po (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic - polytropic_efficiency (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle - pressure_ratio (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle - Pt_in (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic - Pt_out (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic - Pto (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic - R (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic - rho_out (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic - stagnation_enthalpy (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic - stagnation_pressure (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic - stagnation_temperature (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic - static_enthalpy (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic - static_pressure (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic - static_temperature (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic - symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component - T_out (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic - tag (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle - Tt_in (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic - Tt_out (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic - Tto (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic - u_out (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic - velocity (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic + generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component + generative_design_max_per_vehicle (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component + generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component + h_out (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic + ht_out (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic + i_high (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic + i_low (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic + inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component + Mach (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic + mach_number (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic + mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component + Mo (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic + origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component + outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component + P_out (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic + pid (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic + Po (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic + polytropic_efficiency (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle + pressure_ratio (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle + Pt_in (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic + Pt_out (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic + Pto (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic + R (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic + rho_out (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic + stagnation_enthalpy (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic + stagnation_pressure (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic + stagnation_temperature (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic + static_enthalpy (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic + static_pressure (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic + static_temperature (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic + symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component + T_out (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic + tag (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle + Tt_in (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic + Tt_out (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic + Tto (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic + u_out (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic + velocity (defined in SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle)SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzlestatic
@@ -148,7 +158,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Expansion__Nozzle_1_1Expansion__Nozzle.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Expansion__Nozzle_1_1Expansion__Nozzle.html index ef68edaf..4ee3a165 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Expansion__Nozzle_1_1Expansion__Nozzle.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Expansion__Nozzle_1_1Expansion__Nozzle.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -109,8 +116,8 @@ SUAVE.Components.Energy.Energy_Component.Energy_Component SUAVE.Components.Physical_Component.Physical_Component SUAVE.Components.Component.Component - -
+ + @@ -118,15 +125,6 @@ - - - - - - - - -

Public Member Functions

 
def compute (self, conditions)
 
- Public Member Functions inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
@@ -166,6 +164,15 @@ + + + + + +

Public Attributes

 origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 
@@ -312,6 +319,8 @@

SUAVE.Components.Energy.Energy_Component.Energy_Component.

+ @@ -344,6 +353,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Fan_1_1Fan-members.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Fan_1_1Fan-members.html index 4716f821..b9cf8c0e 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Fan_1_1Fan-members.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Fan_1_1Fan-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Static Public Attributes

SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -100,14 +107,17 @@ - - - - - - - - + + + + + + + + + + +
__defaults__(self)SUAVE.Components.Energy.Converters.Fan.Fan
compute(self, conditions)SUAVE.Components.Energy.Converters.Fan.Fan
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
polytropic_efficiency (defined in SUAVE.Components.Energy.Converters.Fan.Fan)SUAVE.Components.Energy.Converters.Fan.Fan
pressure_ratio (defined in SUAVE.Components.Energy.Converters.Fan.Fan)SUAVE.Components.Energy.Converters.Fan.Fan
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Energy.Converters.Fan.Fan)SUAVE.Components.Energy.Converters.Fan.Fan
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
polytropic_efficiency (defined in SUAVE.Components.Energy.Converters.Fan.Fan)SUAVE.Components.Energy.Converters.Fan.Fan
pressure_ratio (defined in SUAVE.Components.Energy.Converters.Fan.Fan)SUAVE.Components.Energy.Converters.Fan.Fan
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Energy.Converters.Fan.Fan)SUAVE.Components.Energy.Converters.Fan.Fan
@@ -115,7 +125,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Fan_1_1Fan.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Fan_1_1Fan.html index 52bb9f52..8ee47da1 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Fan_1_1Fan.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Fan_1_1Fan.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Components.Energy.Converters.Fan.Fan Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -108,8 +115,8 @@ SUAVE.Components.Energy.Energy_Component.Energy_Component SUAVE.Components.Physical_Component.Physical_Component SUAVE.Components.Component.Component - -
+ + @@ -117,15 +124,6 @@ - - - - - - - - -

Public Member Functions

 
def compute (self, conditions)
 
- Public Member Functions inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
@@ -165,6 +163,15 @@ + + + + + +

Public Attributes

 origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 

Detailed Description

This is a fan component typically used in a turbofan.
@@ -208,6 +215,8 @@ 

SUAVE.Components.Energy.Energy_Component.Energy_Component.

+

@@ -277,7 +286,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Fuel__Cell_1_1Fuel__Cell-members.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Fuel__Cell_1_1Fuel__Cell-members.html index 491f675c..1b3fab08 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Fuel__Cell_1_1Fuel__Cell-members.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Fuel__Cell_1_1Fuel__Cell-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -102,18 +109,21 @@ discharge_model (defined in SUAVE.Components.Energy.Converters.Fuel_Cell.Fuel_Cell)SUAVE.Components.Energy.Converters.Fuel_Cell.Fuel_Cell efficiency (defined in SUAVE.Components.Energy.Converters.Fuel_Cell.Fuel_Cell)SUAVE.Components.Energy.Converters.Fuel_Cell.Fuel_Cell energy_calc(self, conditions, numerics)SUAVE.Components.Energy.Converters.Fuel_Cell.Fuel_Cell - inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component - mass_density (defined in SUAVE.Components.Energy.Converters.Fuel_Cell.Fuel_Cell)SUAVE.Components.Energy.Converters.Fuel_Cell.Fuel_Cell - mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component - max_power (defined in SUAVE.Components.Energy.Converters.Fuel_Cell.Fuel_Cell)SUAVE.Components.Energy.Converters.Fuel_Cell.Fuel_Cell - origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component - outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component - oxidizer (defined in SUAVE.Components.Energy.Converters.Fuel_Cell.Fuel_Cell)SUAVE.Components.Energy.Converters.Fuel_Cell.Fuel_Cell - propellant (defined in SUAVE.Components.Energy.Converters.Fuel_Cell.Fuel_Cell)SUAVE.Components.Energy.Converters.Fuel_Cell.Fuel_Cell - specific_power (defined in SUAVE.Components.Energy.Converters.Fuel_Cell.Fuel_Cell)SUAVE.Components.Energy.Converters.Fuel_Cell.Fuel_Cell - symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component - tag (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component - volume (defined in SUAVE.Components.Energy.Converters.Fuel_Cell.Fuel_Cell)SUAVE.Components.Energy.Converters.Fuel_Cell.Fuel_Cell + generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component + generative_design_max_per_vehicle (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component + generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component + inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component + mass_density (defined in SUAVE.Components.Energy.Converters.Fuel_Cell.Fuel_Cell)SUAVE.Components.Energy.Converters.Fuel_Cell.Fuel_Cell + mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component + max_power (defined in SUAVE.Components.Energy.Converters.Fuel_Cell.Fuel_Cell)SUAVE.Components.Energy.Converters.Fuel_Cell.Fuel_Cell + origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component + outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component + oxidizer (defined in SUAVE.Components.Energy.Converters.Fuel_Cell.Fuel_Cell)SUAVE.Components.Energy.Converters.Fuel_Cell.Fuel_Cell + propellant (defined in SUAVE.Components.Energy.Converters.Fuel_Cell.Fuel_Cell)SUAVE.Components.Energy.Converters.Fuel_Cell.Fuel_Cell + specific_power (defined in SUAVE.Components.Energy.Converters.Fuel_Cell.Fuel_Cell)SUAVE.Components.Energy.Converters.Fuel_Cell.Fuel_Cell + symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component + tag (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component + volume (defined in SUAVE.Components.Energy.Converters.Fuel_Cell.Fuel_Cell)SUAVE.Components.Energy.Converters.Fuel_Cell.Fuel_Cell
@@ -121,7 +131,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Fuel__Cell_1_1Fuel__Cell.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Fuel__Cell_1_1Fuel__Cell.html index 1ff48875..079e9844 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Fuel__Cell_1_1Fuel__Cell.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Fuel__Cell_1_1Fuel__Cell.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Components.Energy.Converters.Fuel_Cell.Fuel_Cell Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -108,8 +115,8 @@ SUAVE.Components.Energy.Energy_Component.Energy_Component SUAVE.Components.Physical_Component.Physical_Component SUAVE.Components.Component.Component - -
+ + @@ -117,15 +124,6 @@ - - - - - - - - -

Public Member Functions

 
def energy_calc (self, conditions, numerics)
 
- Public Member Functions inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
@@ -180,6 +178,15 @@ + + + + + +

Public Attributes

 origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 

Detailed Description

This is a fuel cell component.
@@ -222,6 +229,8 @@ 

SUAVE.Components.Energy.Energy_Component.Energy_Component.

+

@@ -285,7 +294,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Gearbox_1_1Gearbox-members.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Gearbox_1_1Gearbox-members.html index 25c01ebf..6c94f7e8 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Gearbox_1_1Gearbox-members.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Gearbox_1_1Gearbox-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -101,19 +108,17 @@ __defaults__(self)SUAVE.Components.Energy.Converters.Gearbox.Gearbox compute(self)SUAVE.Components.Energy.Converters.Gearbox.Gearbox efficiency (defined in SUAVE.Components.Energy.Converters.Gearbox.Gearbox)SUAVE.Components.Energy.Converters.Gearbox.Gearbox - gearwhell_radius1 (defined in SUAVE.Components.Energy.Converters.Gearbox.Gearbox)SUAVE.Components.Energy.Converters.Gearbox.Gearbox - gearwhell_radius2 (defined in SUAVE.Components.Energy.Converters.Gearbox.Gearbox)SUAVE.Components.Energy.Converters.Gearbox.Gearbox - inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component - mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component - mass_weight (defined in SUAVE.Components.Energy.Converters.Gearbox.Gearbox)SUAVE.Components.Energy.Converters.Gearbox.Gearbox + gearwheel_radius1 (defined in SUAVE.Components.Energy.Converters.Gearbox.Gearbox)SUAVE.Components.Energy.Converters.Gearbox.Gearbox + gearwheel_radius2 (defined in SUAVE.Components.Energy.Converters.Gearbox.Gearbox)SUAVE.Components.Energy.Converters.Gearbox.Gearbox + generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component + generative_design_max_per_vehicle (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component + generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component + inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component + mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component - speed_1 (defined in SUAVE.Components.Energy.Converters.Gearbox.Gearbox)SUAVE.Components.Energy.Converters.Gearbox.Gearbox - speed_2 (defined in SUAVE.Components.Energy.Converters.Gearbox.Gearbox)SUAVE.Components.Energy.Converters.Gearbox.Gearbox symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component tag (defined in SUAVE.Components.Energy.Converters.Gearbox.Gearbox)SUAVE.Components.Energy.Converters.Gearbox.Gearbox - torque_1 (defined in SUAVE.Components.Energy.Converters.Gearbox.Gearbox)SUAVE.Components.Energy.Converters.Gearbox.Gearbox - torque_2 (defined in SUAVE.Components.Energy.Converters.Gearbox.Gearbox)SUAVE.Components.Energy.Converters.Gearbox.Gearbox
@@ -121,7 +126,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Gearbox_1_1Gearbox.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Gearbox_1_1Gearbox.html index 994c59a4..53c01c29 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Gearbox_1_1Gearbox.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Gearbox_1_1Gearbox.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Components.Energy.Converters.Gearbox.Gearbox Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -108,8 +115,8 @@ SUAVE.Components.Energy.Energy_Component.Energy_Component SUAVE.Components.Physical_Component.Physical_Component SUAVE.Components.Component.Component - -
+ + @@ -117,45 +124,21 @@ - - - - - - - - -

Public Member Functions

 
def compute (self)
 
- Public Member Functions inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
- - - - - - - - - - - - + + + + - - @@ -183,6 +166,15 @@ + + + + + +

Public Attributes

 tag
 
gearwhell_radius1
 
gearwhell_radius2
 
torque_1
 
torque_2
 
speed_1
 
speed_2
 
gearwheel_radius1
 
gearwheel_radius2
 
 efficiency
 
mass_weight
 
- Public Attributes inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
 inputs
 origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 

Detailed Description

This is a gear box component.
@@ -225,6 +217,8 @@ 

SUAVE.Components.Energy.Energy_Component.Energy_Component.

+

@@ -280,7 +274,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Gearbox_1_1Gearbox.js b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Gearbox_1_1Gearbox.js index 5aa34890..b5231fce 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Gearbox_1_1Gearbox.js +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Gearbox_1_1Gearbox.js @@ -3,12 +3,7 @@ var classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Gearbox_1_1Gearbox = [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Gearbox_1_1Gearbox.html#aae942d6c125bcaf5be47aaf69f290fce", null ], [ "compute", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Gearbox_1_1Gearbox.html#aad8e3af09759982461dd014ce41b6dea", null ], [ "efficiency", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Gearbox_1_1Gearbox.html#a67d43cd1ee31af6aed137acaf266a400", null ], - [ "gearwhell_radius1", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Gearbox_1_1Gearbox.html#a07f3413bb27609d129bb15f0c7e029a2", null ], - [ "gearwhell_radius2", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Gearbox_1_1Gearbox.html#ab206d384c80a8004e3811a7ba7c74759", null ], - [ "mass_weight", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Gearbox_1_1Gearbox.html#a96816790fe81237581ef24cea5734aec", null ], - [ "speed_1", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Gearbox_1_1Gearbox.html#a25846e8c0f2b69438d3d0666177c6b57", null ], - [ "speed_2", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Gearbox_1_1Gearbox.html#ae4f4e5cbade217b0d81fd2f509095e13", null ], - [ "tag", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Gearbox_1_1Gearbox.html#ab95ab2b40d1e96c58aaab46ee1e532a1", null ], - [ "torque_1", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Gearbox_1_1Gearbox.html#ad3011a75aa077e352379d8d45bf2e5b2", null ], - [ "torque_2", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Gearbox_1_1Gearbox.html#a9e46ec723c2948f8514290edd4294d03", null ] + [ "gearwheel_radius1", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Gearbox_1_1Gearbox.html#a3f8a607077164f6082fa0ba1e28ea58e", null ], + [ "gearwheel_radius2", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Gearbox_1_1Gearbox.html#a4667117fe16c5cfca080f75ac8dde3e6", null ], + [ "tag", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Gearbox_1_1Gearbox.html#ab95ab2b40d1e96c58aaab46ee1e532a1", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Generator__Zero__Fid_1_1Generator__Zero__Fid-members.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Generator__Zero__Fid_1_1Generator__Zero__Fid-members.html new file mode 100644 index 00000000..ccd9ffc3 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Generator__Zero__Fid_1_1Generator__Zero__Fid-members.html @@ -0,0 +1,132 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
SUAVE.Components.Energy.Converters.Generator_Zero_Fid.Generator_Zero_Fid Member List
+
+
+ +

This is the complete list of members for SUAVE.Components.Energy.Converters.Generator_Zero_Fid.Generator_Zero_Fid, including all inherited members.

+ + + + + + + + + + + + + + +
__defaults__(self)SUAVE.Components.Energy.Converters.Generator_Zero_Fid.Generator_Zero_Fid
calculate_power(self, conditions)SUAVE.Components.Energy.Converters.Generator_Zero_Fid.Generator_Zero_Fid
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
max_power (defined in SUAVE.Components.Energy.Converters.Generator_Zero_Fid.Generator_Zero_Fid)SUAVE.Components.Energy.Converters.Generator_Zero_Fid.Generator_Zero_Fid
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
sfc (defined in SUAVE.Components.Energy.Converters.Generator_Zero_Fid.Generator_Zero_Fid)SUAVE.Components.Energy.Converters.Generator_Zero_Fid.Generator_Zero_Fid
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Generator__Zero__Fid_1_1Generator__Zero__Fid.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Generator__Zero__Fid_1_1Generator__Zero__Fid.html new file mode 100644 index 00000000..b4cd0cb3 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Generator__Zero__Fid_1_1Generator__Zero__Fid.html @@ -0,0 +1,282 @@ + + + + + + + +SUAVE: SUAVE.Components.Energy.Converters.Generator_Zero_Fid.Generator_Zero_Fid Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Components.Energy.Converters.Generator_Zero_Fid.Generator_Zero_Fid Class Reference
+
+
+
+Inheritance diagram for SUAVE.Components.Energy.Converters.Generator_Zero_Fid.Generator_Zero_Fid:
+
+
+ + +SUAVE.Components.Energy.Energy_Component.Energy_Component +SUAVE.Components.Physical_Component.Physical_Component +SUAVE.Components.Component.Component + +
+ + + + + + +

+Public Member Functions

def __defaults__ (self)
 
def calculate_power (self, conditions)
 
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Attributes

sfc
 
max_power
 
- Public Attributes inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
inputs
 
outputs
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 
+

Detailed Description

+
This is a zero-fidelity generator component.
+
+Assumptions:
+None
+
+Source:
+None
+

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Components.Energy.Converters.Generator_Zero_Fid.Generator_Zero_Fid.__defaults__ ( self)
+
+
This sets the default values for the component to function.
+
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+None
+
+Outputs:
+None
+
+Properties Used:
+None
+
+

Reimplemented from SUAVE.Components.Energy.Energy_Component.Energy_Component.

+ +
+
+ +

◆ calculate_power()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Components.Energy.Converters.Generator_Zero_Fid.Generator_Zero_Fid.calculate_power ( self,
 conditions 
)
+
+
Calculates power 
+    
+Assumptions:
+Specific Fuel Consumption (SFC) is constant
+Generator always operates at max power which is constant
+conditions.propulsion.throttle exists
+    
+Source:
+N/A
+    
+Inputs:
+N/A
+    
+Outputs:
+self.outputs.
+    power_generated    [W]
+    mdot               [kg/s]
+    
+Properties Used:
+self.
+    sfc                [kg/(W*s)]
+    max_power          [W]
+
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Energy/Converters/Generator_Zero_Fid.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Generator__Zero__Fid_1_1Generator__Zero__Fid.js b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Generator__Zero__Fid_1_1Generator__Zero__Fid.js new file mode 100644 index 00000000..1cc9f37e --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Generator__Zero__Fid_1_1Generator__Zero__Fid.js @@ -0,0 +1,7 @@ +var classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Generator__Zero__Fid_1_1Generator__Zero__Fid = +[ + [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Generator__Zero__Fid_1_1Generator__Zero__Fid.html#af2aa34618affd115b144a4c185f73716", null ], + [ "calculate_power", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Generator__Zero__Fid_1_1Generator__Zero__Fid.html#a0e4ec1949824115c13e6ba0606b53d47", null ], + [ "max_power", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Generator__Zero__Fid_1_1Generator__Zero__Fid.html#a314e1f2b3ec39884547a7c8b9d29d44b", null ], + [ "sfc", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Generator__Zero__Fid_1_1Generator__Zero__Fid.html#aa1925738cb429aead6632212cd2f1640", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Generator__Zero__Fid_1_1Generator__Zero__Fid.png b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Generator__Zero__Fid_1_1Generator__Zero__Fid.png new file mode 100644 index 00000000..a94c0ec0 Binary files /dev/null and b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Generator__Zero__Fid_1_1Generator__Zero__Fid.png differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Internal__Combustion__Engine_1_1Internal__Combustion__Engine-members.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Internal__Combustion__Engine_1_1Internal__Combustion__Engine-members.html new file mode 100644 index 00000000..3726a4c0 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Internal__Combustion__Engine_1_1Internal__Combustion__Engine-members.html @@ -0,0 +1,135 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
SUAVE.Components.Energy.Converters.Internal_Combustion_Engine.Internal_Combustion_Engine Member List
+
+
+ +

This is the complete list of members for SUAVE.Components.Energy.Converters.Internal_Combustion_Engine.Internal_Combustion_Engine, including all inherited members.

+ + + + + + + + + + + + + + + + + +
__defaults__(self)SUAVE.Components.Energy.Converters.Internal_Combustion_Engine.Internal_Combustion_Engine
calculate_throttle(self, conditions)SUAVE.Components.Energy.Converters.Internal_Combustion_Engine.Internal_Combustion_Engine
flat_rate_altitude (defined in SUAVE.Components.Energy.Converters.Internal_Combustion_Engine.Internal_Combustion_Engine)SUAVE.Components.Energy.Converters.Internal_Combustion_Engine.Internal_Combustion_Engine
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
power(self, conditions)SUAVE.Components.Energy.Converters.Internal_Combustion_Engine.Internal_Combustion_Engine
power_specific_fuel_consumption (defined in SUAVE.Components.Energy.Converters.Internal_Combustion_Engine.Internal_Combustion_Engine)SUAVE.Components.Energy.Converters.Internal_Combustion_Engine.Internal_Combustion_Engine
rated_speed (defined in SUAVE.Components.Energy.Converters.Internal_Combustion_Engine.Internal_Combustion_Engine)SUAVE.Components.Energy.Converters.Internal_Combustion_Engine.Internal_Combustion_Engine
sea_level_power (defined in SUAVE.Components.Energy.Converters.Internal_Combustion_Engine.Internal_Combustion_Engine)SUAVE.Components.Energy.Converters.Internal_Combustion_Engine.Internal_Combustion_Engine
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Internal__Combustion__Engine_1_1Internal__Combustion__Engine.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Internal__Combustion__Engine_1_1Internal__Combustion__Engine.html new file mode 100644 index 00000000..fb1ee2a3 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Internal__Combustion__Engine_1_1Internal__Combustion__Engine.html @@ -0,0 +1,333 @@ + + + + + + + +SUAVE: SUAVE.Components.Energy.Converters.Internal_Combustion_Engine.Internal_Combustion_Engine Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Components.Energy.Converters.Internal_Combustion_Engine.Internal_Combustion_Engine Class Reference
+
+
+
+Inheritance diagram for SUAVE.Components.Energy.Converters.Internal_Combustion_Engine.Internal_Combustion_Engine:
+
+
+ + +SUAVE.Components.Energy.Energy_Component.Energy_Component +SUAVE.Components.Physical_Component.Physical_Component +SUAVE.Components.Component.Component + +
+ + + + + + + + +

+Public Member Functions

def __defaults__ (self)
 
def power (self, conditions)
 
def calculate_throttle (self, conditions)
 
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Attributes

sea_level_power
 
flat_rate_altitude
 
rated_speed
 
power_specific_fuel_consumption
 
- Public Attributes inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
inputs
 
outputs
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 
+

Detailed Description

+
This is an internal combustion engine component.
+
+Assumptions:
+None
+
+Source:
+None
+

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Components.Energy.Converters.Internal_Combustion_Engine.Internal_Combustion_Engine.__defaults__ ( self)
+
+
This sets the default inputs and outputs data structure.
+
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+None
+
+Outputs:
+None
+
+Properties Used:
+N/A
+
+

Reimplemented from SUAVE.Components.Energy.Energy_Component.Energy_Component.

+ +
+
+ +

◆ calculate_throttle()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Components.Energy.Converters.Internal_Combustion_Engine.Internal_Combustion_Engine.calculate_throttle ( self,
 conditions 
)
+
+
The internal combustion engine output power and specific power consumption
+
+source: 
+
+Inputs:
+    Engine:
+sea-level power
+flat rate altitude
+rated_speed (RPM)
+throttle setting
+inputs.power
+    Freestream conditions:
+altitude
+delta_isa
+Outputs:
+    Brake power (or Shaft power)
+    Power (brake) specific fuel consumption
+    Fuel flow
+    Torque
+    throttle setting
+
+
+
+ +

◆ power()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Components.Energy.Converters.Internal_Combustion_Engine.Internal_Combustion_Engine.power ( self,
 conditions 
)
+
+
The internal combustion engine output power and specific power consumption
+Inputs:
+    Engine:
+sea-level power
+flat rate altitude
+rated_speed (RPM)
+throttle setting
+inputs.speed (RPM)
+    Freestream conditions:
+altitude
+delta_isa
+Outputs:
+    Brake power (or Shaft power)
+    Power (brake) specific fuel consumption
+    Fuel flow
+    Torque
+
+
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Energy/Converters/Internal_Combustion_Engine.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Internal__Combustion__Engine_1_1Internal__Combustion__Engine.js b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Internal__Combustion__Engine_1_1Internal__Combustion__Engine.js new file mode 100644 index 00000000..00596ec9 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Internal__Combustion__Engine_1_1Internal__Combustion__Engine.js @@ -0,0 +1,10 @@ +var classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Internal__Combustion__Engine_1_1Internal__Combustion__Engine = +[ + [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Internal__Combustion__Engine_1_1Internal__Combustion__Engine.html#a5d31fb2f945861d75fbaa9bd8513476c", null ], + [ "calculate_throttle", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Internal__Combustion__Engine_1_1Internal__Combustion__Engine.html#a818e3b25ab8e4270180ba1c21cc43a15", null ], + [ "power", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Internal__Combustion__Engine_1_1Internal__Combustion__Engine.html#a94db95474312b1191020a2238ae8ba99", null ], + [ "flat_rate_altitude", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Internal__Combustion__Engine_1_1Internal__Combustion__Engine.html#af3d22be14ee81f4d17820b5ac5ae187d", null ], + [ "power_specific_fuel_consumption", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Internal__Combustion__Engine_1_1Internal__Combustion__Engine.html#adf1dcf6195a11907bcf848bcfe5ed37a", null ], + [ "rated_speed", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Internal__Combustion__Engine_1_1Internal__Combustion__Engine.html#a3bf36efe72b5a047122c6155338b2964", null ], + [ "sea_level_power", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Internal__Combustion__Engine_1_1Internal__Combustion__Engine.html#a7cb99429f9741330fb49ed3d58b9947d", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Internal__Combustion__Engine_1_1Internal__Combustion__Engine.png b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Internal__Combustion__Engine_1_1Internal__Combustion__Engine.png new file mode 100644 index 00000000..817fb20f Binary files /dev/null and b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Internal__Combustion__Engine_1_1Internal__Combustion__Engine.png differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Lift__Rotor_1_1Lift__Rotor-members.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Lift__Rotor_1_1Lift__Rotor-members.html new file mode 100644 index 00000000..85d62be2 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Lift__Rotor_1_1Lift__Rotor-members.html @@ -0,0 +1,164 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
SUAVE.Components.Energy.Converters.Lift_Rotor.Lift_Rotor Member List
+
+
+ +

This is the complete list of members for SUAVE.Components.Energy.Converters.Lift_Rotor.Lift_Rotor, including all inherited members.

+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
__defaults__(self)SUAVE.Components.Energy.Converters.Lift_Rotor.Lift_Rotor
airfoil_geometry (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
airfoil_polar_stations (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
airfoil_polars (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
axial_velocities_2d (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
azimuthal_distribution (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
blade_solidity (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
body_to_prop_vel(self)SUAVE.Components.Energy.Converters.Rotor.Rotor
chord_distribution (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
design_power (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
design_thrust (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
ducted (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
hub_radius (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
induced_power_factor (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
nonuniform_freestream (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
number_azimuthal_stations (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
number_of_blades (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
orientation_euler_angles (defined in SUAVE.Components.Energy.Converters.Lift_Rotor.Lift_Rotor)SUAVE.Components.Energy.Converters.Lift_Rotor.Lift_Rotor
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
profile_drag_coefficient (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
prop_vel_to_body(self)SUAVE.Components.Energy.Converters.Rotor.Rotor
radial_velocities_2d (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
radius_distribution (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
rotation (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
spin(self, conditions)SUAVE.Components.Energy.Converters.Rotor.Rotor
start_angle (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
sweep_distribution (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Energy.Converters.Lift_Rotor.Lift_Rotor)SUAVE.Components.Energy.Converters.Lift_Rotor.Lift_Rotor
tangential_velocities_2d (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
thickness_to_chord (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
tip_radius (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
twist_distribution (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
use_2d_analysis (defined in SUAVE.Components.Energy.Converters.Lift_Rotor.Lift_Rotor)SUAVE.Components.Energy.Converters.Lift_Rotor.Lift_Rotor
variable_pitch (defined in SUAVE.Components.Energy.Converters.Lift_Rotor.Lift_Rotor)SUAVE.Components.Energy.Converters.Lift_Rotor.Lift_Rotor
vec_to_prop_body(self) (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
vec_to_vel(self)SUAVE.Components.Energy.Converters.Rotor.Rotor
vtk_airfoil_points (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
Wake (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Lift__Rotor_1_1Lift__Rotor.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Lift__Rotor_1_1Lift__Rotor.html new file mode 100644 index 00000000..454a2aa5 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Lift__Rotor_1_1Lift__Rotor.html @@ -0,0 +1,347 @@ + + + + + + + +SUAVE: SUAVE.Components.Energy.Converters.Lift_Rotor.Lift_Rotor Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Components.Energy.Converters.Lift_Rotor.Lift_Rotor Class Reference
+
+
+
+Inheritance diagram for SUAVE.Components.Energy.Converters.Lift_Rotor.Lift_Rotor:
+
+
+ + +SUAVE.Components.Energy.Converters.Rotor.Rotor +SUAVE.Components.Energy.Energy_Component.Energy_Component +SUAVE.Components.Physical_Component.Physical_Component +SUAVE.Components.Component.Component + +
+ + + + + + + + + + + + + + + +

+Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Energy.Converters.Rotor.Rotor
def spin (self, conditions)
 
def vec_to_vel (self)
 
def body_to_prop_vel (self)
 
def prop_vel_to_body (self)
 
+def vec_to_prop_body (self)
 
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Attributes

tag
 
orientation_euler_angles
 
use_2d_analysis
 
variable_pitch
 
- Public Attributes inherited from SUAVE.Components.Energy.Converters.Rotor.Rotor
tag
 
number_of_blades
 
tip_radius
 
hub_radius
 
twist_distribution
 
sweep_distribution
 
chord_distribution
 
thickness_to_chord
 
blade_solidity
 
design_power
 
design_thrust
 
airfoil_geometry
 
airfoil_polars
 
airfoil_polar_stations
 
radius_distribution
 
rotation
 
orientation_euler_angles
 
ducted
 
number_azimuthal_stations
 
vtk_airfoil_points
 
induced_power_factor
 
profile_drag_coefficient
 
use_2d_analysis
 
nonuniform_freestream
 
axial_velocities_2d
 
tangential_velocities_2d
 
radial_velocities_2d
 
start_angle
 
variable_pitch
 
Wake
 
azimuthal_distribution
 
outputs
 
- Public Attributes inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
inputs
 
outputs
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 
+

Detailed Description

+
This is a lift rotor component, and is a sub-class of rotor.
+
+Assumptions:
+None
+
+Source:
+None
+

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Components.Energy.Converters.Lift_Rotor.Lift_Rotor.__defaults__ ( self)
+
+
This sets the default values for the component to function.
+
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+None
+
+Outputs:
+None
+
+Properties Used:
+None
+
+

Reimplemented from SUAVE.Components.Energy.Converters.Rotor.Rotor.

+ +
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Energy/Converters/Lift_Rotor.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Lift__Rotor_1_1Lift__Rotor.js b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Lift__Rotor_1_1Lift__Rotor.js new file mode 100644 index 00000000..ce3f52c4 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Lift__Rotor_1_1Lift__Rotor.js @@ -0,0 +1,8 @@ +var classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Lift__Rotor_1_1Lift__Rotor = +[ + [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Lift__Rotor_1_1Lift__Rotor.html#aec1dc297a6af4d6d47addaa30b748f66", null ], + [ "orientation_euler_angles", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Lift__Rotor_1_1Lift__Rotor.html#a1f24143bad5516745f6ca75d7235ed8b", null ], + [ "tag", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Lift__Rotor_1_1Lift__Rotor.html#a17bd1b8524267567e2b4cf7b9b758f7c", null ], + [ "use_2d_analysis", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Lift__Rotor_1_1Lift__Rotor.html#a657c6070c288457b87d5ddd0cce4ec3f", null ], + [ "variable_pitch", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Lift__Rotor_1_1Lift__Rotor.html#a603add3c2a62cbbae6eae2e733f3cf6c", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Lift__Rotor_1_1Lift__Rotor.png b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Lift__Rotor_1_1Lift__Rotor.png new file mode 100644 index 00000000..6c5aee3d Binary files /dev/null and b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Lift__Rotor_1_1Lift__Rotor.png differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor_1_1Motor-members.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor_1_1Motor-members.html index 82d6bbb6..2b77777a 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor_1_1Motor-members.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor_1_1Motor-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -100,21 +107,28 @@ - - - + + + + + + + - - - - - - - - - - - + + + + + + + + + + + + + +
__defaults__(self)SUAVE.Components.Energy.Converters.Motor.Motor
current(self, conditions)SUAVE.Components.Energy.Converters.Motor.Motor
expected_current (defined in SUAVE.Components.Energy.Converters.Motor.Motor)SUAVE.Components.Energy.Converters.Motor.Motor
gear_ratio (defined in SUAVE.Components.Energy.Converters.Motor.Motor)SUAVE.Components.Energy.Converters.Motor.Motor
gearbox_efficiency (defined in SUAVE.Components.Energy.Converters.Motor.Motor)SUAVE.Components.Energy.Converters.Motor.Motor
efficiency (defined in SUAVE.Components.Energy.Converters.Motor.Motor)SUAVE.Components.Energy.Converters.Motor.Motor
expected_current (defined in SUAVE.Components.Energy.Converters.Motor.Motor)SUAVE.Components.Energy.Converters.Motor.Motor
gear_ratio (defined in SUAVE.Components.Energy.Converters.Motor.Motor)SUAVE.Components.Energy.Converters.Motor.Motor
gearbox_efficiency (defined in SUAVE.Components.Energy.Converters.Motor.Motor)SUAVE.Components.Energy.Converters.Motor.Motor
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
no_load_current (defined in SUAVE.Components.Energy.Converters.Motor.Motor)SUAVE.Components.Energy.Converters.Motor.Motor
omega(self, conditions)SUAVE.Components.Energy.Converters.Motor.Motor
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
propeller_Cp (defined in SUAVE.Components.Energy.Converters.Motor.Motor)SUAVE.Components.Energy.Converters.Motor.Motor
propeller_radius (defined in SUAVE.Components.Energy.Converters.Motor.Motor)SUAVE.Components.Energy.Converters.Motor.Motor
resistance (defined in SUAVE.Components.Energy.Converters.Motor.Motor)SUAVE.Components.Energy.Converters.Motor.Motor
speed_constant (defined in SUAVE.Components.Energy.Converters.Motor.Motor)SUAVE.Components.Energy.Converters.Motor.Motor
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
interpolated_func (defined in SUAVE.Components.Energy.Converters.Motor.Motor)SUAVE.Components.Energy.Converters.Motor.Motor
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
no_load_current (defined in SUAVE.Components.Energy.Converters.Motor.Motor)SUAVE.Components.Energy.Converters.Motor.Motor
omega(self, conditions)SUAVE.Components.Energy.Converters.Motor.Motor
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
propeller_Cp (defined in SUAVE.Components.Energy.Converters.Motor.Motor)SUAVE.Components.Energy.Converters.Motor.Motor
propeller_radius (defined in SUAVE.Components.Energy.Converters.Motor.Motor)SUAVE.Components.Energy.Converters.Motor.Motor
resistance (defined in SUAVE.Components.Energy.Converters.Motor.Motor)SUAVE.Components.Energy.Converters.Motor.Motor
speed_constant (defined in SUAVE.Components.Energy.Converters.Motor.Motor)SUAVE.Components.Energy.Converters.Motor.Motor
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Energy.Converters.Motor.Motor)SUAVE.Components.Energy.Converters.Motor.Motor
torque(self, conditions)SUAVE.Components.Energy.Converters.Motor.Motor
voltage_current(self, conditions)SUAVE.Components.Energy.Converters.Motor.Motor
@@ -122,7 +136,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor_1_1Motor.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor_1_1Motor.html index d1f7332b..ca36c47d 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor_1_1Motor.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor_1_1Motor.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Components.Energy.Converters.Motor.Motor Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -108,8 +115,8 @@ SUAVE.Components.Energy.Energy_Component.Energy_Component SUAVE.Components.Physical_Component.Physical_Component SUAVE.Components.Component.Component - -
+ + @@ -117,20 +124,18 @@ + + + + - - - - - - - - -

Public Member Functions

 
def omega (self, conditions)
 
def torque (self, conditions)
 
def voltage_current (self, conditions)
 
def current (self, conditions)
 
- Public Member Functions inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
+ + @@ -146,6 +151,9 @@ + + @@ -155,6 +163,9 @@ + + @@ -182,6 +193,15 @@ + + + + + +

Public Attributes

tag
 
 resistance
 
 propeller_Cp
 
efficiency
 
 gear_ratio
 
 expected_current
 
interpolated_func
 
- Public Attributes inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
 inputs
 origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 

Detailed Description

This is a motor component.
@@ -224,6 +244,8 @@ 

SUAVE.Components.Energy.Energy_Component.Energy_Component.

+

@@ -254,7 +276,6 @@

Calculates the motor's current Assumptions: -Cp (power coefficient) is constant Source: N/A @@ -265,8 +286,7 @@

+

◆ torque()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Components.Energy.Converters.Motor.Motor.torque ( self,
 conditions 
)
+
+
Calculates the motor's torque
+
+Assumptions:
+
+Source:
+N/A
+
+Inputs:
+
+Outputs:
+self.outputs.torque    [N-m] 
+
+Properties Used:
+self.
+  gear_ratio           [-]
+  speed_constant       [radian/s/V]
+  resistance           [ohm]
+  outputs.omega        [radian/s]
+  gearbox_efficiency   [-]
+  expected_current     [A]
+  no_load_current      [A]
+  inputs.volage        [V]
+
+
+
+ +

◆ voltage_current()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Components.Energy.Converters.Motor.Motor.voltage_current ( self,
 conditions 
)
+
+
Calculates the motor's voltage and current
+
+Assumptions:
+
+Source:
+N/A
+
+Inputs:
+
+Outputs:
+self.outputs.current   [A]
+conditions.
+  propulsion.volage    [V]
+conditions.
+  propulsion.etam      [-] 
+
+Properties Used:
+self.
+  gear_ratio           [-]
+  speed_constant       [radian/s/V]
+  resistance           [ohm]
+  outputs.omega        [radian/s]
+  gearbox_efficiency   [-]
+  expected_current     [A]
+  no_load_current      [A]
+
+
+

The documentation for this class was generated from the following file:
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Energy/Converters/Motor.py
@@ -348,7 +471,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor_1_1Motor.js b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor_1_1Motor.js index c1dc914e..40d05a30 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor_1_1Motor.js +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor_1_1Motor.js @@ -3,12 +3,17 @@ var classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor_1_1Motor = [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor_1_1Motor.html#af941ec8976ff2b39156a3e3ceb25f1fc", null ], [ "current", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor_1_1Motor.html#a4f50c2270b78bede450b3e9db6c195f3", null ], [ "omega", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor_1_1Motor.html#ad9ab86d7bab611ffdc596a6c65dc86c2", null ], + [ "torque", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor_1_1Motor.html#a1e9aefb10ee059b66793dff9bb6a5712", null ], + [ "voltage_current", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor_1_1Motor.html#a8c1e0e7b0011c6a14ac0897820fc4cb8", null ], + [ "efficiency", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor_1_1Motor.html#a864c24ffa4c02e3cc66bd83e2f94b6d6", null ], [ "expected_current", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor_1_1Motor.html#a4f7b6aa5b6e6bb31cfec03cbcf5aad35", null ], [ "gear_ratio", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor_1_1Motor.html#a79e6c4ee71fb685fbd9bba825ec65b0d", null ], [ "gearbox_efficiency", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor_1_1Motor.html#a3dcd5ec5090f588d31f63965299cd825", null ], + [ "interpolated_func", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor_1_1Motor.html#a3e905af25b21f3134d10fc7e925913b3", null ], [ "no_load_current", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor_1_1Motor.html#a1f0b94313d59a16a6eea49a3d4e1311e", null ], [ "propeller_Cp", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor_1_1Motor.html#a16cb7590afcba652e316f45f8a761a31", null ], [ "propeller_radius", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor_1_1Motor.html#a683409fa2bccf383f2f54484848021d2", null ], [ "resistance", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor_1_1Motor.html#a13e5285d973e90a3b4caea45ed2d9d55", null ], - [ "speed_constant", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor_1_1Motor.html#adea69680702442a7a3d8489722c208d6", null ] + [ "speed_constant", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor_1_1Motor.html#adea69680702442a7a3d8489722c208d6", null ], + [ "tag", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor_1_1Motor.html#a6e2d5041adfcd056e5589e90a2baa3d5", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__HTS__Rotor_1_1Motor__HTS__Rotor-members.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__HTS__Rotor_1_1Motor__HTS__Rotor-members.html new file mode 100644 index 00000000..8788c2f2 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__HTS__Rotor_1_1Motor__HTS__Rotor-members.html @@ -0,0 +1,139 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
SUAVE.Components.Energy.Converters.Motor_HTS_Rotor.Motor_HTS_Rotor Member List
+
+
+ +

This is the complete list of members for SUAVE.Components.Energy.Converters.Motor_HTS_Rotor.Motor_HTS_Rotor, including all inherited members.

+ + + + + + + + + + + + + + + + + + + + + +
__defaults__(self)SUAVE.Components.Energy.Converters.Motor_HTS_Rotor.Motor_HTS_Rotor
current (defined in SUAVE.Components.Energy.Converters.Motor_HTS_Rotor.Motor_HTS_Rotor)SUAVE.Components.Energy.Converters.Motor_HTS_Rotor.Motor_HTS_Rotor
diameter (defined in SUAVE.Components.Energy.Converters.Motor_HTS_Rotor.Motor_HTS_Rotor)SUAVE.Components.Energy.Converters.Motor_HTS_Rotor.Motor_HTS_Rotor
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
length (defined in SUAVE.Components.Energy.Converters.Motor_HTS_Rotor.Motor_HTS_Rotor)SUAVE.Components.Energy.Converters.Motor_HTS_Rotor.Motor_HTS_Rotor
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
number_of_engines (defined in SUAVE.Components.Energy.Converters.Motor_HTS_Rotor.Motor_HTS_Rotor)SUAVE.Components.Energy.Converters.Motor_HTS_Rotor.Motor_HTS_Rotor
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
power(self, current, ambient_temp)SUAVE.Components.Energy.Converters.Motor_HTS_Rotor.Motor_HTS_Rotor
R_value (defined in SUAVE.Components.Energy.Converters.Motor_HTS_Rotor.Motor_HTS_Rotor)SUAVE.Components.Energy.Converters.Motor_HTS_Rotor.Motor_HTS_Rotor
resistance (defined in SUAVE.Components.Energy.Converters.Motor_HTS_Rotor.Motor_HTS_Rotor)SUAVE.Components.Energy.Converters.Motor_HTS_Rotor.Motor_HTS_Rotor
skin_temp (defined in SUAVE.Components.Energy.Converters.Motor_HTS_Rotor.Motor_HTS_Rotor)SUAVE.Components.Energy.Converters.Motor_HTS_Rotor.Motor_HTS_Rotor
surface_area (defined in SUAVE.Components.Energy.Converters.Motor_HTS_Rotor.Motor_HTS_Rotor)SUAVE.Components.Energy.Converters.Motor_HTS_Rotor.Motor_HTS_Rotor
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
temperature (defined in SUAVE.Components.Energy.Converters.Motor_HTS_Rotor.Motor_HTS_Rotor)SUAVE.Components.Energy.Converters.Motor_HTS_Rotor.Motor_HTS_Rotor
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__HTS__Rotor_1_1Motor__HTS__Rotor.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__HTS__Rotor_1_1Motor__HTS__Rotor.html new file mode 100644 index 00000000..34937bd5 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__HTS__Rotor_1_1Motor__HTS__Rotor.html @@ -0,0 +1,316 @@ + + + + + + + +SUAVE: SUAVE.Components.Energy.Converters.Motor_HTS_Rotor.Motor_HTS_Rotor Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Components.Energy.Converters.Motor_HTS_Rotor.Motor_HTS_Rotor Class Reference
+
+
+
+Inheritance diagram for SUAVE.Components.Energy.Converters.Motor_HTS_Rotor.Motor_HTS_Rotor:
+
+
+ + +SUAVE.Components.Energy.Energy_Component.Energy_Component +SUAVE.Components.Physical_Component.Physical_Component +SUAVE.Components.Component.Component + +
+ + + + + + +

+Public Member Functions

def __defaults__ (self)
 
def power (self, current, ambient_temp)
 
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Attributes

temperature
 
skin_temp
 
current
 
resistance
 
length
 
diameter
 
surface_area
 
R_value
 
number_of_engines
 
- Public Attributes inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
inputs
 
outputs
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 
+

Detailed Description

+
This represents just the rotor of a HTS motor, i.e. the superconducting components.
+This is used to estimate the power and cooling required for the HTS components.
+The power used here could be considered the same as that used by the motor as inefficiency, however many publications consider the overall motor efficiency, i.e. including cryocooler and/or motor drive electronics.
+
+Assumptions:
+No ACLoss in the HTS,
+HTS is operated within the Ic and Tc limits.
+i.e the power used by the coil is only due to solder resistances only, and is not affected by the motor output power or speed.
+
+Source:
+None
+

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Components.Energy.Converters.Motor_HTS_Rotor.Motor_HTS_Rotor.__defaults__ ( self)
+
+
This sets the default values for the component to function.
+
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+None
+
+Outputs:
+None
+
+Properties Used:
+None
+
+

Reimplemented from SUAVE.Components.Energy.Energy_Component.Energy_Component.

+ +
+
+ +

◆ power()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Components.Energy.Converters.Motor_HTS_Rotor.Motor_HTS_Rotor.power ( self,
 current,
 ambient_temp 
)
+
+
Calculates the electrical power draw from the HTS coils, and the total heating load on the HTS rotor cryostat.
+
+Assumptions:
+No ACLoss in the HTS,
+HTS is operated within the Ic and Tc limits.
+i.e the power used by the coil is only due to solder resistances only.
+
+Source:
+N/A
+
+Inputs:
+current             [A]
+ambient_temp        [K]
+
+Outputs:
+input_power         [W]
+cryogenic_load      [W]
+
+Properties Used:
+self.
+    temperature     [K]
+    resistance      [ohm]
+    surface_area    [m2]
+    R_value         [K.m2/W]
+
+
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Energy/Converters/Motor_HTS_Rotor.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__HTS__Rotor_1_1Motor__HTS__Rotor.js b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__HTS__Rotor_1_1Motor__HTS__Rotor.js new file mode 100644 index 00000000..b91e257b --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__HTS__Rotor_1_1Motor__HTS__Rotor.js @@ -0,0 +1,14 @@ +var classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__HTS__Rotor_1_1Motor__HTS__Rotor = +[ + [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__HTS__Rotor_1_1Motor__HTS__Rotor.html#a8c1d226e62c5353683229f63512a32c2", null ], + [ "power", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__HTS__Rotor_1_1Motor__HTS__Rotor.html#ab274712a99a4514602a43eb904f2f529", null ], + [ "current", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__HTS__Rotor_1_1Motor__HTS__Rotor.html#a1f22cd0a1883acbea06eed4e086519a7", null ], + [ "diameter", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__HTS__Rotor_1_1Motor__HTS__Rotor.html#a7058be3207193927b1004b44888582f3", null ], + [ "length", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__HTS__Rotor_1_1Motor__HTS__Rotor.html#abc7b8c0166281be0d9a3b3bfe819d92a", null ], + [ "number_of_engines", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__HTS__Rotor_1_1Motor__HTS__Rotor.html#ab4637a093f22d0c088c7a7149b65d4a2", null ], + [ "R_value", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__HTS__Rotor_1_1Motor__HTS__Rotor.html#a17bc30f101708ae01d93b7223efff63c", null ], + [ "resistance", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__HTS__Rotor_1_1Motor__HTS__Rotor.html#a7c81f76881c5c64f439ae781800a75c2", null ], + [ "skin_temp", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__HTS__Rotor_1_1Motor__HTS__Rotor.html#a9abcff850151e2d428d76656f07802e2", null ], + [ "surface_area", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__HTS__Rotor_1_1Motor__HTS__Rotor.html#a619b6c2d47b287a04041bfd6ec95b108", null ], + [ "temperature", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__HTS__Rotor_1_1Motor__HTS__Rotor.html#a355ae1a43d8a38ce23dd2e0f0ffed461", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__HTS__Rotor_1_1Motor__HTS__Rotor.png b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__HTS__Rotor_1_1Motor__HTS__Rotor.png new file mode 100644 index 00000000..74b909ea Binary files /dev/null and b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__HTS__Rotor_1_1Motor__HTS__Rotor.png differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__Lo__Fid_1_1Motor__Lo__Fid-members.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__Lo__Fid_1_1Motor__Lo__Fid-members.html index 4e437fae..051f1666 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__Lo__Fid_1_1Motor__Lo__Fid-members.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__Lo__Fid_1_1Motor__Lo__Fid-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -103,13 +110,19 @@ expected_current (defined in SUAVE.Components.Energy.Converters.Motor_Lo_Fid.Motor_Lo_Fid)SUAVE.Components.Energy.Converters.Motor_Lo_Fid.Motor_Lo_Fid gear_ratio (defined in SUAVE.Components.Energy.Converters.Motor_Lo_Fid.Motor_Lo_Fid)SUAVE.Components.Energy.Converters.Motor_Lo_Fid.Motor_Lo_Fid gearbox_efficiency (defined in SUAVE.Components.Energy.Converters.Motor_Lo_Fid.Motor_Lo_Fid)SUAVE.Components.Energy.Converters.Motor_Lo_Fid.Motor_Lo_Fid - inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component - mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component - motor_efficiency (defined in SUAVE.Components.Energy.Converters.Motor_Lo_Fid.Motor_Lo_Fid)SUAVE.Components.Energy.Converters.Motor_Lo_Fid.Motor_Lo_Fid - no_load_current (defined in SUAVE.Components.Energy.Converters.Motor_Lo_Fid.Motor_Lo_Fid)SUAVE.Components.Energy.Converters.Motor_Lo_Fid.Motor_Lo_Fid - omega(self, conditions)SUAVE.Components.Energy.Converters.Motor_Lo_Fid.Motor_Lo_Fid - origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component - outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component + generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component + generative_design_max_per_vehicle (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component + generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component + inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component + mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component + motor_efficiency (defined in SUAVE.Components.Energy.Converters.Motor_Lo_Fid.Motor_Lo_Fid)SUAVE.Components.Energy.Converters.Motor_Lo_Fid.Motor_Lo_Fid + no_load_current (defined in SUAVE.Components.Energy.Converters.Motor_Lo_Fid.Motor_Lo_Fid)SUAVE.Components.Energy.Converters.Motor_Lo_Fid.Motor_Lo_Fid + omega(self, conditions)SUAVE.Components.Energy.Converters.Motor_Lo_Fid.Motor_Lo_Fid + origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component + outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component + power_lo(self, conditions)SUAVE.Components.Energy.Converters.Motor_Lo_Fid.Motor_Lo_Fid + rated_power (defined in SUAVE.Components.Energy.Converters.Motor_Lo_Fid.Motor_Lo_Fid)SUAVE.Components.Energy.Converters.Motor_Lo_Fid.Motor_Lo_Fid + rated_voltage (defined in SUAVE.Components.Energy.Converters.Motor_Lo_Fid.Motor_Lo_Fid)SUAVE.Components.Energy.Converters.Motor_Lo_Fid.Motor_Lo_Fid resistance (defined in SUAVE.Components.Energy.Converters.Motor_Lo_Fid.Motor_Lo_Fid)SUAVE.Components.Energy.Converters.Motor_Lo_Fid.Motor_Lo_Fid speed_constant (defined in SUAVE.Components.Energy.Converters.Motor_Lo_Fid.Motor_Lo_Fid)SUAVE.Components.Energy.Converters.Motor_Lo_Fid.Motor_Lo_Fid symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component @@ -121,7 +134,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__Lo__Fid_1_1Motor__Lo__Fid.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__Lo__Fid_1_1Motor__Lo__Fid.html index b682adc1..adce08ac 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__Lo__Fid_1_1Motor__Lo__Fid.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__Lo__Fid_1_1Motor__Lo__Fid.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Components.Energy.Converters.Motor_Lo_Fid.Motor_Lo_Fid Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -108,8 +115,8 @@ SUAVE.Components.Energy.Energy_Component.Energy_Component SUAVE.Components.Physical_Component.Physical_Component SUAVE.Components.Component.Component - -
+ + @@ -119,15 +126,8 @@ - - - - - - - - - + +

Public Member Functions

 
def current (self, conditions)
 
- Public Member Functions inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
def power_lo (self, conditions)
 
@@ -152,6 +152,12 @@ + + + + @@ -179,6 +185,15 @@ + + + + + +

Public Attributes

 motor_efficiency
 
rated_power
 
rated_voltage
 
- Public Attributes inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
 inputs
 origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 

Detailed Description

This is a low-fidelity motor component.
@@ -221,6 +236,8 @@ 

SUAVE.Components.Energy.Energy_Component.Energy_Component.

+

@@ -332,6 +349,56 @@

+

◆ power_lo()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Components.Energy.Converters.Motor_Lo_Fid.Motor_Lo_Fid.power_lo ( self,
 conditions 
)
+
+
Calculates the motor's power output
+    
+Assumptions: 
+    
+Source:
+N/A
+    
+Inputs: 
+self.
+   inputs.voltage         [V] 
+    
+Outputs:
+self.outputs.
+   outputs.power          [W]
+   outputs.current        [A]
+   
+Properties Used:
+self.
+
+  motor_efficiency        [-] 
+  rated_power             [W] 
+  rated_voltage           [V] 
+
+
+

The documentation for this class was generated from the following file:
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Energy/Converters/Motor_Lo_Fid.py
@@ -343,7 +410,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__Lo__Fid_1_1Motor__Lo__Fid.js b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__Lo__Fid_1_1Motor__Lo__Fid.js index a8da841a..988508ae 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__Lo__Fid_1_1Motor__Lo__Fid.js +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__Lo__Fid_1_1Motor__Lo__Fid.js @@ -3,11 +3,14 @@ var classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__Lo__Fid_1_1Motor_ [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__Lo__Fid_1_1Motor__Lo__Fid.html#a1b9bb23be0478adab9351cf9c715f123", null ], [ "current", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__Lo__Fid_1_1Motor__Lo__Fid.html#a55ff976700d1e5f089b06bb788c7cbd1", null ], [ "omega", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__Lo__Fid_1_1Motor__Lo__Fid.html#a0e3d5a3b41ca71612ed130bfc64fc132", null ], + [ "power_lo", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__Lo__Fid_1_1Motor__Lo__Fid.html#a484e0b1906135ed2b6a7e24917cf6c38", null ], [ "expected_current", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__Lo__Fid_1_1Motor__Lo__Fid.html#a8ee1e69ab8ae5631b88055efc3929f03", null ], [ "gear_ratio", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__Lo__Fid_1_1Motor__Lo__Fid.html#a1a51a431aa3c7a764c4425df5ed6b2e8", null ], [ "gearbox_efficiency", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__Lo__Fid_1_1Motor__Lo__Fid.html#a7cc17da0e703afd6ee2014f56b8852bd", null ], [ "motor_efficiency", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__Lo__Fid_1_1Motor__Lo__Fid.html#aa153f6a56e0ac6c9fad72d00cb29e479", null ], [ "no_load_current", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__Lo__Fid_1_1Motor__Lo__Fid.html#abc0ef203bdc48a1df5a063a2fdef0ba8", null ], + [ "rated_power", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__Lo__Fid_1_1Motor__Lo__Fid.html#ac1d1722911d2c8f1e8bb7838afce54a1", null ], + [ "rated_voltage", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__Lo__Fid_1_1Motor__Lo__Fid.html#a109ea2576133b76ef826aa6beb09eeb9", null ], [ "resistance", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__Lo__Fid_1_1Motor__Lo__Fid.html#aafd9b227ddd7d6da1e0e6ee2edeea5db", null ], [ "speed_constant", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Motor__Lo__Fid_1_1Motor__Lo__Fid.html#a67aeabb364e970ae2009652abd33738d", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Propeller_1_1Propeller-members.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Propeller_1_1Propeller-members.html index 69717411..f7db26df 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Propeller_1_1Propeller-members.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Propeller_1_1Propeller-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -99,15 +106,50 @@

This is the complete list of members for SUAVE.Components.Energy.Converters.Propeller.Propeller, including all inherited members.

+ + + + + + + + + + + + + + + + + + + + - - - + + + + + + + + + - - + + + + + + + + + + +
__defaults__(self)SUAVE.Components.Energy.Converters.Propeller.Propeller
airfoil_geometry (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
airfoil_polar_stations (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
airfoil_polars (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
axial_velocities_2d (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
azimuthal_distribution (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
blade_solidity (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
body_to_prop_vel(self)SUAVE.Components.Energy.Converters.Rotor.Rotor
chord_distribution (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
design_power (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
design_thrust (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
ducted (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
hub_radius (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
induced_power_factor (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
nonuniform_freestream (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
number_azimuthal_stations (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
number_of_blades (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
orientation_euler_angles (defined in SUAVE.Components.Energy.Converters.Propeller.Propeller)SUAVE.Components.Energy.Converters.Propeller.Propeller
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
prop_attributes (defined in SUAVE.Components.Energy.Converters.Propeller.Propeller)SUAVE.Components.Energy.Converters.Propeller.Propeller
spin(self, conditions)SUAVE.Components.Energy.Converters.Propeller.Propeller
outputs (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
profile_drag_coefficient (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
prop_vel_to_body(self)SUAVE.Components.Energy.Converters.Rotor.Rotor
radial_velocities_2d (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
radius_distribution (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
rotation (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
spin(self, conditions)SUAVE.Components.Energy.Converters.Rotor.Rotor
start_angle (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
sweep_distribution (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
thrust_angle (defined in SUAVE.Components.Energy.Converters.Propeller.Propeller)SUAVE.Components.Energy.Converters.Propeller.Propeller
tag (defined in SUAVE.Components.Energy.Converters.Propeller.Propeller)SUAVE.Components.Energy.Converters.Propeller.Propeller
tangential_velocities_2d (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
thickness_to_chord (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
tip_radius (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
twist_distribution (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
use_2d_analysis (defined in SUAVE.Components.Energy.Converters.Propeller.Propeller)SUAVE.Components.Energy.Converters.Propeller.Propeller
variable_pitch (defined in SUAVE.Components.Energy.Converters.Propeller.Propeller)SUAVE.Components.Energy.Converters.Propeller.Propeller
vec_to_prop_body(self) (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
vec_to_vel(self)SUAVE.Components.Energy.Converters.Rotor.Rotor
vtk_airfoil_points (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
Wake (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
@@ -115,7 +157,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Propeller_1_1Propeller.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Propeller_1_1Propeller.html index 26a9e314..4e763578 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Propeller_1_1Propeller.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Propeller_1_1Propeller.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Components.Energy.Converters.Propeller.Propeller Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -105,36 +112,141 @@
+SUAVE.Components.Energy.Converters.Rotor.Rotor SUAVE.Components.Energy.Energy_Component.Energy_Component SUAVE.Components.Physical_Component.Physical_Component SUAVE.Components.Component.Component - -
+ + - - - - - - - - - - - + + + + + + + + + + +

Public Member Functions

def __defaults__ (self)
 
def spin (self, conditions)
 
- Public Member Functions inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Energy.Converters.Rotor.Rotor
def spin (self, conditions)
 
def vec_to_vel (self)
 
def body_to_prop_vel (self)
 
def prop_vel_to_body (self)
 
+def vec_to_prop_body (self)
 
- - - - + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + @@ -162,9 +274,18 @@ + + + + + +

Public Attributes

prop_attributes
 
thrust_angle
 
tag
 
orientation_euler_angles
 
use_2d_analysis
 
variable_pitch
 
- Public Attributes inherited from SUAVE.Components.Energy.Converters.Rotor.Rotor
tag
 
number_of_blades
 
tip_radius
 
hub_radius
 
twist_distribution
 
sweep_distribution
 
chord_distribution
 
thickness_to_chord
 
blade_solidity
 
design_power
 
design_thrust
 
airfoil_geometry
 
airfoil_polars
 
airfoil_polar_stations
 
radius_distribution
 
rotation
 
orientation_euler_angles
 
ducted
 
number_azimuthal_stations
 
vtk_airfoil_points
 
induced_power_factor
 
profile_drag_coefficient
 
use_2d_analysis
 
nonuniform_freestream
 
axial_velocities_2d
 
tangential_velocities_2d
 
radial_velocities_2d
 
start_angle
 
variable_pitch
 
Wake
 
azimuthal_distribution
 
outputs
 
- Public Attributes inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
 inputs
 origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 

Detailed Description

-
This is a propeller component.
+
This is a propeller component, and is a sub-class of rotor.
 
 Assumptions:
 None
@@ -204,84 +325,8 @@ 

-

◆ spin()

+

Reimplemented from SUAVE.Components.Energy.Converters.Rotor.Rotor.

-
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Components.Energy.Converters.Propeller.Propeller.spin ( self,
 conditions 
)
-
-
Analyzes a propeller given geometry and operating conditions.
-
-Assumptions:
-per source
-
-Source:
-Qprop theory document
-
-Inputs:
-self.inputs.omega            [radian/s]
-conditions.freestream.
-  density                    [kg/m^3]
-  dynamic_viscosity          [kg/(m-s)]
-  speed_of_sound             [m/s]
-  temperature                [K]
-conditions.frames.
-  body.transform_to_inertial (rotation matrix)
-  inertial.velocity_vector   [m/s]
-conditions.propulsion.
-  throttle                   [-]
-
-Outputs:
-conditions.propulsion.acoustic_outputs.
-  number_sections            [-]
-  r0                         [m]
-  airfoil_chord              [m]
-  blades_number              [-]
-  propeller_diameter         [m]
-  drag_coefficient           [-]
-  lift_coefficient           [-]
-  omega                      [radian/s]
-  velocity                   [m/s]
-  thrust                     [N]
-  power                      [W]
-  mid_chord_aligment         [m] (distance from the mid chord to the line axis out of the center of the blade)
-conditions.propulsion.etap   [-]
-thrust                       [N]
-torque                       [Nm]
-power                        [W]
-Cp                           [-] (coefficient of power)
-
-Properties Used:
-self.prop_attributes.
-  number_blades              [-]
-  tip_radius                 [m]
-  hub_radius                 [m]
-  twist_distribution         [radians]
-  chord_distribution         [m]
-  mid_chord_aligment         [m] (distance from the mid chord to the line axis out of the center of the blade)
-self.thrust_angle            [radians]
-

The documentation for this class was generated from the following file:

diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Propeller_1_1Propeller.js b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Propeller_1_1Propeller.js index c69a1727..7efcd4ea 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Propeller_1_1Propeller.js +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Propeller_1_1Propeller.js @@ -1,7 +1,8 @@ var classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Propeller_1_1Propeller = [ [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Propeller_1_1Propeller.html#aad1f23ecbcb98693cc81e258edd4a783", null ], - [ "spin", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Propeller_1_1Propeller.html#a7a6c4f4d97b3c18c3f7ef5878803aa4e", null ], - [ "prop_attributes", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Propeller_1_1Propeller.html#a5b098880963977153526442dc3f3ebe1", null ], - [ "thrust_angle", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Propeller_1_1Propeller.html#acd508103c9560b9c36a71f9c99028827", null ] + [ "orientation_euler_angles", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Propeller_1_1Propeller.html#a8c5692cb42babbbb88bad1348a936471", null ], + [ "tag", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Propeller_1_1Propeller.html#a6ce5409c63d254968557890c47d27a21", null ], + [ "use_2d_analysis", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Propeller_1_1Propeller.html#ae0e300aedff7aea4e9b10a91a5cf6136", null ], + [ "variable_pitch", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Propeller_1_1Propeller.html#a4d3ab97f41595426d02d6ad730065078", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Propeller_1_1Propeller.png b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Propeller_1_1Propeller.png index 9272932f..205aee30 100644 Binary files a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Propeller_1_1Propeller.png and b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Propeller_1_1Propeller.png differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Propeller__Lo__Fid_1_1Propeller__Lo__Fid-members.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Propeller__Lo__Fid_1_1Propeller__Lo__Fid-members.html index 6e3c9908..a51f3007 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Propeller__Lo__Fid_1_1Propeller__Lo__Fid-members.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Propeller__Lo__Fid_1_1Propeller__Lo__Fid-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@
- +
@@ -73,7 +78,9 @@
@@ -99,15 +106,18 @@

This is the complete list of members for SUAVE.Components.Energy.Converters.Propeller_Lo_Fid.Propeller_Lo_Fid, including all inherited members.

- - - - - - - - - + + + + + + + + + + + +
__defaults__(self)SUAVE.Components.Energy.Converters.Propeller_Lo_Fid.Propeller_Lo_Fid
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
propulsive_efficiency (defined in SUAVE.Components.Energy.Converters.Propeller_Lo_Fid.Propeller_Lo_Fid)SUAVE.Components.Energy.Converters.Propeller_Lo_Fid.Propeller_Lo_Fid
spin(self, conditions)SUAVE.Components.Energy.Converters.Propeller_Lo_Fid.Propeller_Lo_Fid
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tip_radius (defined in SUAVE.Components.Energy.Converters.Propeller_Lo_Fid.Propeller_Lo_Fid)SUAVE.Components.Energy.Converters.Propeller_Lo_Fid.Propeller_Lo_Fid
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
propulsive_efficiency (defined in SUAVE.Components.Energy.Converters.Propeller_Lo_Fid.Propeller_Lo_Fid)SUAVE.Components.Energy.Converters.Propeller_Lo_Fid.Propeller_Lo_Fid
spin(self, conditions)SUAVE.Components.Energy.Converters.Propeller_Lo_Fid.Propeller_Lo_Fid
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tip_radius (defined in SUAVE.Components.Energy.Converters.Propeller_Lo_Fid.Propeller_Lo_Fid)SUAVE.Components.Energy.Converters.Propeller_Lo_Fid.Propeller_Lo_Fid
@@ -115,7 +125,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Propeller__Lo__Fid_1_1Propeller__Lo__Fid.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Propeller__Lo__Fid_1_1Propeller__Lo__Fid.html index a1eaecfd..3b2ed52a 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Propeller__Lo__Fid_1_1Propeller__Lo__Fid.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Propeller__Lo__Fid_1_1Propeller__Lo__Fid.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Components.Energy.Converters.Propeller_Lo_Fid.Propeller_Lo_Fid Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -108,8 +115,8 @@ SUAVE.Components.Energy.Energy_Component.Energy_Component SUAVE.Components.Physical_Component.Physical_Component SUAVE.Components.Component.Component - -
+ + @@ -117,15 +124,6 @@ - - - - - - - - -

Public Member Functions

 
def spin (self, conditions)
 
- Public Member Functions inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
@@ -162,6 +160,15 @@ + + + + + +

Public Attributes

 origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 

Detailed Description

This is a low-fidelity propeller component.
@@ -204,6 +211,8 @@ 

SUAVE.Components.Energy.Energy_Component.Energy_Component.

+

@@ -273,7 +282,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Ram_1_1Ram-members.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Ram_1_1Ram-members.html index 27623f3c..879539a0 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Ram_1_1Ram-members.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Ram_1_1Ram-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -100,12 +107,15 @@ - - - - - - + + + + + + + + +
__defaults__(self)SUAVE.Components.Energy.Converters.Ram.Ram
compute(self, conditions)SUAVE.Components.Energy.Converters.Ram.Ram
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Energy.Converters.Ram.Ram)SUAVE.Components.Energy.Converters.Ram.Ram
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Energy.Converters.Ram.Ram)SUAVE.Components.Energy.Converters.Ram.Ram
@@ -113,7 +123,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Ram_1_1Ram.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Ram_1_1Ram.html index 09d12543..d32135a9 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Ram_1_1Ram.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Ram_1_1Ram.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Components.Energy.Converters.Ram.Ram Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -108,8 +115,8 @@ SUAVE.Components.Energy.Energy_Component.Energy_Component SUAVE.Components.Physical_Component.Physical_Component SUAVE.Components.Component.Component - -
+ + @@ -117,15 +124,6 @@ - - - - - - - - -

Public Member Functions

 
def compute (self, conditions)
 
- Public Member Functions inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
@@ -159,6 +157,15 @@ + + + + + +

Public Attributes

 origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 

Detailed Description

This represent the compression of incoming air flow.
@@ -202,6 +209,8 @@ 

SUAVE.Components.Energy.Energy_Component.Energy_Component.

+

@@ -276,7 +285,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Rocket__Combustor_1_1Rocket__Combustor-members.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Rocket__Combustor_1_1Rocket__Combustor-members.html new file mode 100644 index 00000000..8c00966f --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Rocket__Combustor_1_1Rocket__Combustor-members.html @@ -0,0 +1,132 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
SUAVE.Components.Energy.Converters.Rocket_Combustor.Rocket_Combustor Member List
+
+
+ +

This is the complete list of members for SUAVE.Components.Energy.Converters.Rocket_Combustor.Rocket_Combustor, including all inherited members.

+ + + + + + + + + + + + + + +
__defaults__(self)SUAVE.Components.Energy.Converters.Rocket_Combustor.Rocket_Combustor
compute(self, conditions)SUAVE.Components.Energy.Converters.Rocket_Combustor.Rocket_Combustor
efficiency (defined in SUAVE.Components.Energy.Converters.Rocket_Combustor.Rocket_Combustor)SUAVE.Components.Energy.Converters.Rocket_Combustor.Rocket_Combustor
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
propellant_data (defined in SUAVE.Components.Energy.Converters.Rocket_Combustor.Rocket_Combustor)SUAVE.Components.Energy.Converters.Rocket_Combustor.Rocket_Combustor
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Energy.Converters.Rocket_Combustor.Rocket_Combustor)SUAVE.Components.Energy.Converters.Rocket_Combustor.Rocket_Combustor
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Rocket__Combustor_1_1Rocket__Combustor.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Rocket__Combustor_1_1Rocket__Combustor.html new file mode 100644 index 00000000..c3a84ea9 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Rocket__Combustor_1_1Rocket__Combustor.html @@ -0,0 +1,290 @@ + + + + + + + +SUAVE: SUAVE.Components.Energy.Converters.Rocket_Combustor.Rocket_Combustor Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Components.Energy.Converters.Rocket_Combustor.Rocket_Combustor Class Reference
+
+
+
+Inheritance diagram for SUAVE.Components.Energy.Converters.Rocket_Combustor.Rocket_Combustor:
+
+
+ + +SUAVE.Components.Energy.Energy_Component.Energy_Component +SUAVE.Components.Physical_Component.Physical_Component +SUAVE.Components.Component.Component + +
+ + + + + + +

+Public Member Functions

def __defaults__ (self)
 
def compute (self, conditions)
 
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Attributes

tag
 
propellant_data
 
efficiency
 
- Public Attributes inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
inputs
 
outputs
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 
+

Detailed Description

+
This provides output values for a rocket combustion chamber.
+Calling this class calls the compute function.
+
+Assumptions:
+None
+
+Source:
+Chapter 7
+https://web.stanford.edu/~cantwell/AA283_Course_Material/AA283_Course_Notes/
+

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Components.Energy.Converters.Rocket_Combustor.Rocket_Combustor.__defaults__ ( self)
+
+
This sets the default values for the component to function.
+
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+None
+
+Outputs:
+None
+
+Properties Used:
+None
+
+

Reimplemented from SUAVE.Components.Energy.Energy_Component.Energy_Component.

+ +
+
+ +

◆ compute()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Components.Energy.Converters.Rocket_Combustor.Rocket_Combustor.compute ( self,
 conditions 
)
+
+
This computes the output values from the input values according to
+equations from the source. This function is currently a shell until 
+CEA surrogate is include. This functions similiarly to RAM.py at the
+moment.
+
+Assumptions:
+Combustion happens as M<<<1, assumed to be Mach = 0.
+Combustion needs CEA surrogate.
+
+Source:
+Chapter 7
+https://web.stanford.edu/~cantwell/AA283_Course_Material/AA283_Course_Notes/
+
+Inputs:
+self.inputs.
+  combustion_pressure           [Pa]
+
+Outputs:
+self.outputs.
+  combustion_temperature        [K]  
+  combustion_pressure           [Pa]
+  isentropic_expansion_factor   [-]
+  gas_specific_constant         [J/(Kg-K)]
+
+Properties Used:
+
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Energy/Converters/Rocket_Combustor.py
  • +
+
+
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+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
SUAVE.Components.Energy.Converters.Rotor.Rotor Member List
+
+
+ +

This is the complete list of members for SUAVE.Components.Energy.Converters.Rotor.Rotor, including all inherited members.

+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
__defaults__(self)SUAVE.Components.Energy.Converters.Rotor.Rotor
airfoil_geometry (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
airfoil_polar_stations (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
airfoil_polars (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
axial_velocities_2d (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
azimuthal_distribution (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
blade_solidity (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
body_to_prop_vel(self)SUAVE.Components.Energy.Converters.Rotor.Rotor
chord_distribution (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
design_power (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
design_thrust (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
ducted (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
hub_radius (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
induced_power_factor (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
nonuniform_freestream (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
number_azimuthal_stations (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
number_of_blades (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
orientation_euler_angles (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
profile_drag_coefficient (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
prop_vel_to_body(self)SUAVE.Components.Energy.Converters.Rotor.Rotor
radial_velocities_2d (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
radius_distribution (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
rotation (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
spin(self, conditions)SUAVE.Components.Energy.Converters.Rotor.Rotor
start_angle (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
sweep_distribution (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
tangential_velocities_2d (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
thickness_to_chord (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
tip_radius (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
twist_distribution (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
use_2d_analysis (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
variable_pitch (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
vec_to_prop_body(self) (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
vec_to_vel(self)SUAVE.Components.Energy.Converters.Rotor.Rotor
vtk_airfoil_points (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
Wake (defined in SUAVE.Components.Energy.Converters.Rotor.Rotor)SUAVE.Components.Energy.Converters.Rotor.Rotor
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Rotor_1_1Rotor.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Rotor_1_1Rotor.html new file mode 100644 index 00000000..c7bf4892 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Rotor_1_1Rotor.html @@ -0,0 +1,537 @@ + + + + + + + +SUAVE: SUAVE.Components.Energy.Converters.Rotor.Rotor Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Components.Energy.Converters.Rotor.Rotor Class Reference
+
+
+
+Inheritance diagram for SUAVE.Components.Energy.Converters.Rotor.Rotor:
+
+
+ + +SUAVE.Components.Energy.Energy_Component.Energy_Component +SUAVE.Components.Physical_Component.Physical_Component +SUAVE.Components.Component.Component +SUAVE.Components.Energy.Converters.Lift_Rotor.Lift_Rotor +SUAVE.Components.Energy.Converters.Propeller.Propeller + +
+ + + + + + + + + + + + + + +

+Public Member Functions

def __defaults__ (self)
 
def spin (self, conditions)
 
def vec_to_vel (self)
 
def body_to_prop_vel (self)
 
def prop_vel_to_body (self)
 
+def vec_to_prop_body (self)
 
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Attributes

tag
 
number_of_blades
 
tip_radius
 
hub_radius
 
twist_distribution
 
sweep_distribution
 
chord_distribution
 
thickness_to_chord
 
blade_solidity
 
design_power
 
design_thrust
 
airfoil_geometry
 
airfoil_polars
 
airfoil_polar_stations
 
radius_distribution
 
rotation
 
orientation_euler_angles
 
ducted
 
number_azimuthal_stations
 
vtk_airfoil_points
 
induced_power_factor
 
profile_drag_coefficient
 
use_2d_analysis
 
nonuniform_freestream
 
axial_velocities_2d
 
tangential_velocities_2d
 
radial_velocities_2d
 
start_angle
 
variable_pitch
 
Wake
 
azimuthal_distribution
 
outputs
 
- Public Attributes inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
inputs
 
outputs
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 
+

Detailed Description

+
This is a general rotor component.
+
+Assumptions:
+None
+
+Source:
+None
+

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Components.Energy.Converters.Rotor.Rotor.__defaults__ ( self)
+
+
This sets the default values for the component to function.
+
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+None
+
+Outputs:
+None
+
+Properties Used:
+None
+
+

Reimplemented from SUAVE.Components.Energy.Energy_Component.Energy_Component.

+ +

Reimplemented in SUAVE.Components.Energy.Converters.Lift_Rotor.Lift_Rotor, and SUAVE.Components.Energy.Converters.Propeller.Propeller.

+ +
+
+ +

◆ body_to_prop_vel()

+ +
+
+ + + + + + + + +
def SUAVE.Components.Energy.Converters.Rotor.Rotor.body_to_prop_vel ( self)
+
+
This rotates from the systems body frame to the propellers velocity frame
+
+Assumptions:
+There are two propeller frames, the vehicle frame describing the location and the propeller velocity frame
+velocity frame is X out the nose, Z towards the ground, and Y out the right wing
+vehicle frame is X towards the tail, Z towards the ceiling, and Y out the right wing
+
+Source:
+N/A
+
+Inputs:
+None
+
+Outputs:
+None
+
+Properties Used:
+None
+
+
+
+ +

◆ prop_vel_to_body()

+ +
+
+ + + + + + + + +
def SUAVE.Components.Energy.Converters.Rotor.Rotor.prop_vel_to_body ( self)
+
+
This rotates from the propeller's velocity frame to the system's body frame
+
+Assumptions:
+There are two propeller frames, the vehicle frame describing the location and the propeller velocity frame
+velocity frame is X out the nose, Z towards the ground, and Y out the right wing
+vehicle frame is X towards the tail, Z towards the ceiling, and Y out the right wing
+
+Source:
+N/A
+
+Inputs:
+None
+
+Outputs:
+None
+
+Properties Used:
+None
+
+
+
+ +

◆ spin()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Components.Energy.Converters.Rotor.Rotor.spin ( self,
 conditions 
)
+
+
Analyzes a general rotor given geometry and operating conditions.
+
+Assumptions:
+per source
+
+Source:
+Drela, M. "Qprop Formulation", MIT AeroAstro, June 2006
+http://web.mit.edu/drela/Public/web/qprop/qprop_theory.pdf
+
+Leishman, Gordon J. Principles of helicopter aerodynamics
+Cambridge university press, 2006.
+
+Inputs:
+self.inputs.omega                    [radian/s]
+conditions.freestream.
+  density                            [kg/m^3]
+  dynamic_viscosity                  [kg/(m-s)]
+  speed_of_sound                     [m/s]
+  temperature                        [K]
+conditions.frames.
+  body.transform_to_inertial         (rotation matrix)
+  inertial.velocity_vector           [m/s]
+conditions.propulsion.
+  throttle                           [-]
+
+Outputs:
+conditions.propulsion.outputs.
+   number_radial_stations            [-]
+   number_azimuthal_stations         [-]
+   disc_radial_distribution          [m]
+   speed_of_sound                    [m/s]
+   density                           [kg/m-3]
+   velocity                          [m/s]
+   disc_tangential_induced_velocity  [m/s]
+   disc_axial_induced_velocity       [m/s]
+   disc_tangential_velocity          [m/s]
+   disc_axial_velocity               [m/s]
+   drag_coefficient                  [-]
+   lift_coefficient                  [-]
+   omega                             [rad/s]
+   disc_circulation                  [-]
+   blade_dQ_dR                       [N/m]
+   blade_dT_dr                       [N]
+   blade_thrust_distribution         [N]
+   disc_thrust_distribution          [N]
+   thrust_per_blade                  [N]
+   thrust_coefficient                [-]
+   azimuthal_distribution            [rad]
+   disc_azimuthal_distribution       [rad]
+   blade_dQ_dR                       [N]
+   blade_dQ_dr                       [Nm]
+   blade_torque_distribution         [Nm]
+   disc_torque_distribution          [Nm]
+   torque_per_blade                  [Nm]
+   torque_coefficient                [-]
+   power                             [W]
+   power_coefficient                 [-]
+
+Properties Used:
+self.
+  number_of_blades                   [-]
+  tip_radius                         [m]
+  twist_distribution                 [radians]
+  chord_distribution                 [m]
+  orientation_euler_angles           [rad, rad, rad]
+
+
+
+ +

◆ vec_to_vel()

+ +
+
+ + + + + + + + +
def SUAVE.Components.Energy.Converters.Rotor.Rotor.vec_to_vel ( self)
+
+
This rotates from the propellers vehicle frame to the propellers velocity frame
+
+Assumptions:
+There are two propeller frames, the vehicle frame describing the location and the propeller velocity frame
+velocity frame is X out the nose, Z towards the ground, and Y out the right wing
+vehicle frame is X towards the tail, Z towards the ceiling, and Y out the right wing
+
+Source:
+N/A
+
+Inputs:
+None
+
+Outputs:
+None
+
+Properties Used:
+None
+
+
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Energy/Converters/Rotor.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Rotor_1_1Rotor.js b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Rotor_1_1Rotor.js new file mode 100644 index 00000000..8fbdb974 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Rotor_1_1Rotor.js @@ -0,0 +1,41 @@ +var classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Rotor_1_1Rotor = +[ + [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Rotor_1_1Rotor.html#ab833e90e7d5e2cb7c17bee2b80992675", null ], + [ "body_to_prop_vel", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Rotor_1_1Rotor.html#ac163bb5e35e09957e6b2087755472988", null ], + [ "prop_vel_to_body", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Rotor_1_1Rotor.html#ad3c38eab14def6849ff00209ee087e01", null ], + [ "spin", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Rotor_1_1Rotor.html#acff541e7c6cf5860866bb4ecf785657b", null ], + [ "vec_to_prop_body", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Rotor_1_1Rotor.html#a9bb145a01aee6777b39d161c1219de76", null ], + [ "vec_to_vel", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Rotor_1_1Rotor.html#ab888f8c8473aded29f6768ac6f2ca39c", null ], + [ "airfoil_geometry", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Rotor_1_1Rotor.html#ad3e7fd29793aebf2e0030ca39191da54", null ], + [ "airfoil_polar_stations", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Rotor_1_1Rotor.html#ace1d4a9042bd1bb3abad66dbca318b64", null ], + [ "airfoil_polars", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Rotor_1_1Rotor.html#a99c9544c74ccb880ef7889c186a02942", null ], + [ "axial_velocities_2d", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Rotor_1_1Rotor.html#a0578a83ff843f3101ce93a1cda5926e8", null ], + [ "azimuthal_distribution", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Rotor_1_1Rotor.html#a53cd0718cff8304123ae6e9aaddf4b2f", null ], + [ "blade_solidity", 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b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Rotor_1_1Rotor.png new file mode 100644 index 00000000..a6c4daf3 Binary files /dev/null and b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Rotor_1_1Rotor.png differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Shaft__Power__Off__Take_1_1Shaft__Power__Off__Take-members.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Shaft__Power__Off__Take_1_1Shaft__Power__Off__Take-members.html index 0c88f2df..55e3144c 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Shaft__Power__Off__Take_1_1Shaft__Power__Off__Take-members.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Shaft__Power__Off__Take_1_1Shaft__Power__Off__Take-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -100,15 +107,18 @@ - - - - - - - - - + + + + + + + + + + + +
__defaults__(self)SUAVE.Components.Energy.Converters.Shaft_Power_Off_Take.Shaft_Power_Off_Take
compute(self, state)SUAVE.Components.Energy.Converters.Shaft_Power_Off_Take.Shaft_Power_Off_Take
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
power_draw (defined in SUAVE.Components.Energy.Converters.Shaft_Power_Off_Take.Shaft_Power_Off_Take)SUAVE.Components.Energy.Converters.Shaft_Power_Off_Take.Shaft_Power_Off_Take
reference_pressure (defined in SUAVE.Components.Energy.Converters.Shaft_Power_Off_Take.Shaft_Power_Off_Take)SUAVE.Components.Energy.Converters.Shaft_Power_Off_Take.Shaft_Power_Off_Take
reference_temperature (defined in SUAVE.Components.Energy.Converters.Shaft_Power_Off_Take.Shaft_Power_Off_Take)SUAVE.Components.Energy.Converters.Shaft_Power_Off_Take.Shaft_Power_Off_Take
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
power_draw (defined in SUAVE.Components.Energy.Converters.Shaft_Power_Off_Take.Shaft_Power_Off_Take)SUAVE.Components.Energy.Converters.Shaft_Power_Off_Take.Shaft_Power_Off_Take
reference_pressure (defined in SUAVE.Components.Energy.Converters.Shaft_Power_Off_Take.Shaft_Power_Off_Take)SUAVE.Components.Energy.Converters.Shaft_Power_Off_Take.Shaft_Power_Off_Take
reference_temperature (defined in SUAVE.Components.Energy.Converters.Shaft_Power_Off_Take.Shaft_Power_Off_Take)SUAVE.Components.Energy.Converters.Shaft_Power_Off_Take.Shaft_Power_Off_Take
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
@@ -116,7 +126,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Shaft__Power__Off__Take_1_1Shaft__Power__Off__Take.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Shaft__Power__Off__Take_1_1Shaft__Power__Off__Take.html index eb9bbb32..31a0dae8 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Shaft__Power__Off__Take_1_1Shaft__Power__Off__Take.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Shaft__Power__Off__Take_1_1Shaft__Power__Off__Take.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Components.Energy.Converters.Shaft_Power_Off_Take.Shaft_Power_Off_Take Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -108,8 +115,8 @@ SUAVE.Components.Energy.Energy_Component.Energy_Component SUAVE.Components.Physical_Component.Physical_Component SUAVE.Components.Component.Component - -
+ + @@ -117,15 +124,6 @@ - - - - - - - - -

Public Member Functions

 
def compute (self, state)
 
- Public Member Functions inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
@@ -165,6 +163,15 @@ + + + + + +

Public Attributes

 origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 

Detailed Description

This is a component representing the power draw from the shaft.
@@ -207,6 +214,8 @@ 

SUAVE.Components.Energy.Energy_Component.Energy_Component.

+

@@ -269,7 +278,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Solar__Panel_1_1Solar__Panel-members.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Solar__Panel_1_1Solar__Panel-members.html index 0c48bae9..4ebc59b3 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Solar__Panel_1_1Solar__Panel-members.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Solar__Panel_1_1Solar__Panel-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -101,13 +108,16 @@ __defaults__(self)SUAVE.Components.Energy.Converters.Solar_Panel.Solar_Panel area (defined in SUAVE.Components.Energy.Converters.Solar_Panel.Solar_Panel)SUAVE.Components.Energy.Converters.Solar_Panel.Solar_Panel efficiency (defined in SUAVE.Components.Energy.Converters.Solar_Panel.Solar_Panel)SUAVE.Components.Energy.Converters.Solar_Panel.Solar_Panel - inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component - mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component - origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component - outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component - power(self)SUAVE.Components.Energy.Converters.Solar_Panel.Solar_Panel - symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component - tag (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component + generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component + generative_design_max_per_vehicle (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component + generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component + inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component + mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component + origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component + outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component + power(self)SUAVE.Components.Energy.Converters.Solar_Panel.Solar_Panel + symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component + tag (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
@@ -115,7 +125,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Solar__Panel_1_1Solar__Panel.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Solar__Panel_1_1Solar__Panel.html index 19d05793..827718dd 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Solar__Panel_1_1Solar__Panel.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Solar__Panel_1_1Solar__Panel.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Components.Energy.Converters.Solar_Panel.Solar_Panel Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -99,11 +106,6 @@
SUAVE.Components.Energy.Converters.Solar_Panel.Solar_Panel Class Reference
- -


-

Solar_Panel Class

- - More...

Inheritance diagram for SUAVE.Components.Energy.Converters.Solar_Panel.Solar_Panel:
@@ -113,8 +115,8 @@

SUAVE.Components.Physical_Component.Physical_Component SUAVE.Components.Component.Component - -

+ + @@ -122,15 +124,6 @@

- - - - - - - - -

Public Member Functions

 
def power (self)
 
- Public Member Functions inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
@@ -167,10 +160,19 @@

+ + + + + +

Public Attributes

 origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 

Detailed Description

-

-

Solar_Panel Class

+

+

Solar_Panel Class

This is a solar cell component.
 
 Assumptions:
@@ -211,6 +213,8 @@ 

SUAVE.Components.Energy.Energy_Component.Energy_Component.

+

@@ -260,7 +264,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Supersonic__Nozzle_1_1Supersonic__Nozzle-members.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Supersonic__Nozzle_1_1Supersonic__Nozzle-members.html index 0dbe7529..0a836186 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Supersonic__Nozzle_1_1Supersonic__Nozzle-members.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Supersonic__Nozzle_1_1Supersonic__Nozzle-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -101,6 +108,10 @@ __defaults__(self)SUAVE.Components.Energy.Converters.Supersonic_Nozzle.Supersonic_Nozzle compute(self, conditions)SUAVE.Components.Energy.Converters.Supersonic_Nozzle.Supersonic_Nozzle compute_limited_geometry(self, conditions)SUAVE.Components.Energy.Converters.Supersonic_Nozzle.Supersonic_Nozzle + compute_scramjet(self, conditions)SUAVE.Components.Energy.Converters.Supersonic_Nozzle.Supersonic_Nozzle + generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component + generative_design_max_per_vehicle (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component + generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component max_area_ratio (defined in SUAVE.Components.Energy.Converters.Supersonic_Nozzle.Supersonic_Nozzle)SUAVE.Components.Energy.Converters.Supersonic_Nozzle.Supersonic_Nozzle @@ -109,8 +120,9 @@ outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component polytropic_efficiency (defined in SUAVE.Components.Energy.Converters.Supersonic_Nozzle.Supersonic_Nozzle)SUAVE.Components.Energy.Converters.Supersonic_Nozzle.Supersonic_Nozzle pressure_ratio (defined in SUAVE.Components.Energy.Converters.Supersonic_Nozzle.Supersonic_Nozzle)SUAVE.Components.Energy.Converters.Supersonic_Nozzle.Supersonic_Nozzle - symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component - tag (defined in SUAVE.Components.Energy.Converters.Supersonic_Nozzle.Supersonic_Nozzle)SUAVE.Components.Energy.Converters.Supersonic_Nozzle.Supersonic_Nozzle + pressure_recovery (defined in SUAVE.Components.Energy.Converters.Supersonic_Nozzle.Supersonic_Nozzle)SUAVE.Components.Energy.Converters.Supersonic_Nozzle.Supersonic_Nozzle + symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component + tag (defined in SUAVE.Components.Energy.Converters.Supersonic_Nozzle.Supersonic_Nozzle)SUAVE.Components.Energy.Converters.Supersonic_Nozzle.Supersonic_Nozzle
@@ -118,7 +130,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Supersonic__Nozzle_1_1Supersonic__Nozzle.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Supersonic__Nozzle_1_1Supersonic__Nozzle.html index f9329560..ab76a5b4 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Supersonic__Nozzle_1_1Supersonic__Nozzle.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Supersonic__Nozzle_1_1Supersonic__Nozzle.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Components.Energy.Converters.Supersonic_Nozzle.Supersonic_Nozzle Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -108,8 +115,8 @@ SUAVE.Components.Energy.Energy_Component.Energy_Component SUAVE.Components.Physical_Component.Physical_Component SUAVE.Components.Component.Component - -
+ + @@ -119,15 +126,8 @@ - - - - - - - - - + +

Public Member Functions

 
def compute_limited_geometry (self, conditions)
 
- Public Member Functions inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
def compute_scramjet (self, conditions)
 
@@ -140,6 +140,9 @@ + + @@ -173,6 +176,15 @@ + + + + + +

Public Attributes

 pressure_ratio
 
pressure_recovery
 
 max_area_ratio
 
 origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 

Detailed Description

This is a nozzle component that allows for supersonic outflow.
@@ -216,6 +228,8 @@ 

SUAVE.Components.Energy.Energy_Component.Energy_Component.

+

@@ -281,6 +295,7 @@

+

◆ compute_scramjet()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Components.Energy.Converters.Supersonic_Nozzle.Supersonic_Nozzle.compute_scramjet ( self,
 conditions 
)
+
+
This computes exit conditions of a scramjet. 
+
+Assumptions: 
+Fixed output Cp and Gamma 
+
+Source: 
+Heiser, William H., Pratt, D. T., Daley, D. H., and Unmeel, B. M.,  
+"Hypersonic Airbreathing Propulsion", 1994  
+Chapter 4 - pgs. 175-180
+
+Inputs:  
+conditions.freestream.  
+   isentropic_expansion_factor         [-]  
+   specific_heat_at_constant_pressure  [J/(kg K)]  
+   pressure                            [Pa]  
+   stagnation_pressure                 [Pa]  
+   stagnation_temperature              [K]  
+   gas_specific_constant               [J/(kg K)]  
+   mach_number                         [-]  
+
+self.inputs.  
+   stagnation_temperature              [K]  
+   stagnation_pressure                 [Pa]  
+
+Outputs:  
+self.outputs.  
+   stagnation_temperature              [K]    
+   stagnation_pressure                 [Pa]  
+   stagnation_enthalpy                 [J/kg]  
+   mach_number                         [-]  
+   static_temperature                  [K]  
+   static_enthalpy                     [J/kg]  
+   velocity                            [m/s]  
+   static_pressure                     [Pa]  
+   area_ratio                          [-]  
+
+Properties Used:  
+self.  
+   polytropic_efficiency               [-]  
+   pressure_expansion_ratio            [-]                    
+
+
+

The documentation for this class was generated from the following file:
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Energy/Converters/Supersonic_Nozzle.py
@@ -364,7 +447,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Supersonic__Nozzle_1_1Supersonic__Nozzle.js b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Supersonic__Nozzle_1_1Supersonic__Nozzle.js index 17a7098c..56da2753 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Supersonic__Nozzle_1_1Supersonic__Nozzle.js +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Supersonic__Nozzle_1_1Supersonic__Nozzle.js @@ -3,9 +3,11 @@ var classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Supersonic__Nozzle_1_1Su [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Supersonic__Nozzle_1_1Supersonic__Nozzle.html#a861ed50883715716b13cf3d2e21e8ede", null ], [ "compute", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Supersonic__Nozzle_1_1Supersonic__Nozzle.html#a2356fafa6315dd101857f0d18b95098e", null ], [ "compute_limited_geometry", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Supersonic__Nozzle_1_1Supersonic__Nozzle.html#a6423b5f273dc7fba4eb077fe141d88fe", null ], + [ "compute_scramjet", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Supersonic__Nozzle_1_1Supersonic__Nozzle.html#a92920f8278a9b764945c514cfda6f6dd", null ], [ "max_area_ratio", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Supersonic__Nozzle_1_1Supersonic__Nozzle.html#ad79c8e2283d71ee9d50ad9f79b3ed974", null ], [ "min_area_ratio", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Supersonic__Nozzle_1_1Supersonic__Nozzle.html#acb06406357c68df0c4f8cab2e5a267b7", null ], [ "polytropic_efficiency", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Supersonic__Nozzle_1_1Supersonic__Nozzle.html#af9f1fbb06060df1c3b0af8f339c2ab9f", null ], [ "pressure_ratio", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Supersonic__Nozzle_1_1Supersonic__Nozzle.html#a781262fe820e701c453715717494bbb9", null ], + [ "pressure_recovery", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Supersonic__Nozzle_1_1Supersonic__Nozzle.html#ab0aa5a960f61a170e874ce77a4261659", null ], [ "tag", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Supersonic__Nozzle_1_1Supersonic__Nozzle.html#a7bf619594c30ca8ea126f5e0b5177d0a", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Turbine_1_1Turbine-members.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Turbine_1_1Turbine-members.html index d86b62d6..08d846f4 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Turbine_1_1Turbine-members.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Turbine_1_1Turbine-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -100,14 +107,17 @@ - - - - - - - - + + + + + + + + + + +
__defaults__(self)SUAVE.Components.Energy.Converters.Turbine.Turbine
compute(self, conditions)SUAVE.Components.Energy.Converters.Turbine.Turbine
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
mechanical_efficiency (defined in SUAVE.Components.Energy.Converters.Turbine.Turbine)SUAVE.Components.Energy.Converters.Turbine.Turbine
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
polytropic_efficiency (defined in SUAVE.Components.Energy.Converters.Turbine.Turbine)SUAVE.Components.Energy.Converters.Turbine.Turbine
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Energy.Converters.Turbine.Turbine)SUAVE.Components.Energy.Converters.Turbine.Turbine
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
mechanical_efficiency (defined in SUAVE.Components.Energy.Converters.Turbine.Turbine)SUAVE.Components.Energy.Converters.Turbine.Turbine
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
polytropic_efficiency (defined in SUAVE.Components.Energy.Converters.Turbine.Turbine)SUAVE.Components.Energy.Converters.Turbine.Turbine
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Energy.Converters.Turbine.Turbine)SUAVE.Components.Energy.Converters.Turbine.Turbine
@@ -115,7 +125,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Turbine_1_1Turbine.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Turbine_1_1Turbine.html index 9326784f..e14c6f9c 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Turbine_1_1Turbine.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Turbine_1_1Turbine.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Components.Energy.Converters.Turbine.Turbine Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -108,8 +115,8 @@ SUAVE.Components.Energy.Energy_Component.Energy_Component SUAVE.Components.Physical_Component.Physical_Component SUAVE.Components.Component.Component - -
+ + @@ -117,15 +124,6 @@ - - - - - - - - -

Public Member Functions

 
def compute (self, conditions)
 
- Public Member Functions inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
@@ -165,6 +163,15 @@ + + + + + +

Public Attributes

 origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 

Detailed Description

This is a turbine component typically used in a turbofan.
@@ -208,6 +215,8 @@ 

SUAVE.Components.Energy.Energy_Component.Energy_Component.

+

@@ -281,7 +290,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Turboelectric_1_1Turboelectric-members.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Turboelectric_1_1Turboelectric-members.html new file mode 100644 index 00000000..2bcae31e --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Turboelectric_1_1Turboelectric-members.html @@ -0,0 +1,139 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
SUAVE.Components.Energy.Converters.Turboelectric.Turboelectric Member List
+
+
+ +

This is the complete list of members for SUAVE.Components.Energy.Converters.Turboelectric.Turboelectric, including all inherited members.

+ + + + + + + + + + + + + + + + + + + + + +
__defaults__(self)SUAVE.Components.Energy.Converters.Turboelectric.Turboelectric
discharge_model (defined in SUAVE.Components.Energy.Converters.Turboelectric.Turboelectric)SUAVE.Components.Energy.Converters.Turboelectric.Turboelectric
efficiency (defined in SUAVE.Components.Energy.Converters.Turboelectric.Turboelectric)SUAVE.Components.Energy.Converters.Turboelectric.Turboelectric
energy_calc(self, conditions, numerics)SUAVE.Components.Energy.Converters.Turboelectric.Turboelectric
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
mass_density (defined in SUAVE.Components.Energy.Converters.Turboelectric.Turboelectric)SUAVE.Components.Energy.Converters.Turboelectric.Turboelectric
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
number_of_engines (defined in SUAVE.Components.Energy.Converters.Turboelectric.Turboelectric)SUAVE.Components.Energy.Converters.Turboelectric.Turboelectric
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
oxidizer (defined in SUAVE.Components.Energy.Converters.Turboelectric.Turboelectric)SUAVE.Components.Energy.Converters.Turboelectric.Turboelectric
propellant (defined in SUAVE.Components.Energy.Converters.Turboelectric.Turboelectric)SUAVE.Components.Energy.Converters.Turboelectric.Turboelectric
rated_power (defined in SUAVE.Components.Energy.Converters.Turboelectric.Turboelectric)SUAVE.Components.Energy.Converters.Turboelectric.Turboelectric
specific_power (defined in SUAVE.Components.Energy.Converters.Turboelectric.Turboelectric)SUAVE.Components.Energy.Converters.Turboelectric.Turboelectric
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
volume (defined in SUAVE.Components.Energy.Converters.Turboelectric.Turboelectric)SUAVE.Components.Energy.Converters.Turboelectric.Turboelectric
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Turboelectric_1_1Turboelectric.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Turboelectric_1_1Turboelectric.html new file mode 100644 index 00000000..707b809f --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Turboelectric_1_1Turboelectric.html @@ -0,0 +1,304 @@ + + + + + + + +SUAVE: SUAVE.Components.Energy.Converters.Turboelectric.Turboelectric Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Components.Energy.Converters.Turboelectric.Turboelectric Class Reference
+
+
+
+Inheritance diagram for SUAVE.Components.Energy.Converters.Turboelectric.Turboelectric:
+
+
+ + +SUAVE.Components.Energy.Energy_Component.Energy_Component +SUAVE.Components.Physical_Component.Physical_Component +SUAVE.Components.Component.Component + +
+ + + + + + +

+Public Member Functions

def __defaults__ (self)
 
def energy_calc (self, conditions, numerics)
 
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Attributes

propellant
 
oxidizer
 
number_of_engines
 
efficiency
 
volume
 
rated_power
 
specific_power
 
mass_density
 
discharge_model
 
- Public Attributes inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
inputs
 
outputs
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 
+

Detailed Description

+
This is a turboelectic component.
+
+Assumptions:
+None
+
+Source:
+None
+

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Components.Energy.Converters.Turboelectric.Turboelectric.__defaults__ ( self)
+
+
This sets the default values for the component to function.
+
+Assumptions:
+None
+
+Source:
+https://new.siemens.com/global/en/products/energy/power-generation/gas-turbines/sgt-a30-a35-rb.html
+
+Inputs:
+None
+
+Outputs:
+None
+
+Properties Used:
+None
+
+

Reimplemented from SUAVE.Components.Energy.Energy_Component.Energy_Component.

+ +
+
+ +

◆ energy_calc()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Components.Energy.Converters.Turboelectric.Turboelectric.energy_calc ( self,
 conditions,
 numerics 
)
+
+
This calls the assigned discharge method.
+
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+see properties used
+
+Outputs:
+mdot     [kg/s] (units may change depending on selected model)
+
+Properties Used:
+self.discharge_model(self, conditions, numerics)
+
+
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Energy/Converters/Turboelectric.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Turboelectric_1_1Turboelectric.js b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Turboelectric_1_1Turboelectric.js new file mode 100644 index 00000000..35c00665 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Turboelectric_1_1Turboelectric.js @@ -0,0 +1,14 @@ +var classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Turboelectric_1_1Turboelectric = +[ + [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Turboelectric_1_1Turboelectric.html#aa7d48c0f2549de382dbf1190f659c9fc", null ], + [ "energy_calc", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Turboelectric_1_1Turboelectric.html#a3dc70dad9e189aeb00d426753c349bd9", null ], + [ "discharge_model", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Turboelectric_1_1Turboelectric.html#a35f2e81e970b0272824f6756f861bb64", null ], + [ "efficiency", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Turboelectric_1_1Turboelectric.html#aa8371a74d04ffc4a172a13baee11f547", null ], + [ "mass_density", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Turboelectric_1_1Turboelectric.html#aae97320c57d787fe924fdc5f66c882b2", null ], + [ "number_of_engines", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Turboelectric_1_1Turboelectric.html#a6c66152961c666557e748174b19596c4", null ], + [ "oxidizer", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Turboelectric_1_1Turboelectric.html#a0984077678c3b036b2cb0bfa1e7e3a5d", null ], + [ "propellant", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Turboelectric_1_1Turboelectric.html#a85a16a218033c86facab95ab463de288", null ], + [ "rated_power", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Turboelectric_1_1Turboelectric.html#a48c3c6eb918e2629228f884018729473", null ], + [ "specific_power", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Turboelectric_1_1Turboelectric.html#a8049a87803a6e510ec1309a72c0ec954", null ], + [ "volume", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Turboelectric_1_1Turboelectric.html#a8b760c3cd83078ea1c004553acf6fe23", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Turboelectric_1_1Turboelectric.png b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Turboelectric_1_1Turboelectric.png new file mode 100644 index 00000000..924cd55f Binary files /dev/null and b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1Turboelectric_1_1Turboelectric.png differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1de__Laval__Nozzle_1_1de__Laval__Nozzle-members.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1de__Laval__Nozzle_1_1de__Laval__Nozzle-members.html new file mode 100644 index 00000000..fc457ddc --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1de__Laval__Nozzle_1_1de__Laval__Nozzle-members.html @@ -0,0 +1,135 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
SUAVE.Components.Energy.Converters.de_Laval_Nozzle.de_Laval_Nozzle Member List
+
+
+ +

This is the complete list of members for SUAVE.Components.Energy.Converters.de_Laval_Nozzle.de_Laval_Nozzle, including all inherited members.

+ + + + + + + + + + + + + + + + + +
__defaults__(self)SUAVE.Components.Energy.Converters.de_Laval_Nozzle.de_Laval_Nozzle
area_throat (defined in SUAVE.Components.Energy.Converters.de_Laval_Nozzle.de_Laval_Nozzle)SUAVE.Components.Energy.Converters.de_Laval_Nozzle.de_Laval_Nozzle
compute(self, conditions)SUAVE.Components.Energy.Converters.de_Laval_Nozzle.de_Laval_Nozzle
expansion_ratio (defined in SUAVE.Components.Energy.Converters.de_Laval_Nozzle.de_Laval_Nozzle)SUAVE.Components.Energy.Converters.de_Laval_Nozzle.de_Laval_Nozzle
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
polytropic_efficiency (defined in SUAVE.Components.Energy.Converters.de_Laval_Nozzle.de_Laval_Nozzle)SUAVE.Components.Energy.Converters.de_Laval_Nozzle.de_Laval_Nozzle
pressure_ratio_converge (defined in SUAVE.Components.Energy.Converters.de_Laval_Nozzle.de_Laval_Nozzle)SUAVE.Components.Energy.Converters.de_Laval_Nozzle.de_Laval_Nozzle
pressure_ratio_diverge (defined in SUAVE.Components.Energy.Converters.de_Laval_Nozzle.de_Laval_Nozzle)SUAVE.Components.Energy.Converters.de_Laval_Nozzle.de_Laval_Nozzle
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Energy.Converters.de_Laval_Nozzle.de_Laval_Nozzle)SUAVE.Components.Energy.Converters.de_Laval_Nozzle.de_Laval_Nozzle
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1de__Laval__Nozzle_1_1de__Laval__Nozzle.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1de__Laval__Nozzle_1_1de__Laval__Nozzle.html new file mode 100644 index 00000000..408e5dec --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1de__Laval__Nozzle_1_1de__Laval__Nozzle.html @@ -0,0 +1,310 @@ + + + + + + + +SUAVE: SUAVE.Components.Energy.Converters.de_Laval_Nozzle.de_Laval_Nozzle Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Components.Energy.Converters.de_Laval_Nozzle.de_Laval_Nozzle Class Reference
+
+
+
+Inheritance diagram for SUAVE.Components.Energy.Converters.de_Laval_Nozzle.de_Laval_Nozzle:
+
+
+ + +SUAVE.Components.Energy.Energy_Component.Energy_Component +SUAVE.Components.Physical_Component.Physical_Component +SUAVE.Components.Component.Component + +
+ + + + + + +

+Public Member Functions

def __defaults__ (self)
 
def compute (self, conditions)
 
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Attributes

tag
 
polytropic_efficiency
 
pressure_ratio_converge
 
pressure_ratio_diverge
 
expansion_ratio
 
area_throat
 
- Public Attributes inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
inputs
 
outputs
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 
+

Detailed Description

+
This is a nozzle component that allows for supersonic outflow. 
+This is a converging-diverging nozzle used primarilty in rockets.
+Calling this class calls the compute function.
+
+Assumptions:
+Pressure ratio and efficiency do not change with varying conditions.
+
+Source:
+
+https://web.stanford.edu/~cantwell/AA283_Course_Material/AA283_Course_Notes/
+

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Components.Energy.Converters.de_Laval_Nozzle.de_Laval_Nozzle.__defaults__ ( self)
+
+
This sets the default values for the component to function.
+
+Assumptions:
+None
+    
+Source:
+N/A
+    
+Inputs:
+None
+    
+Outputs:
+None
+    
+Properties Used:
+None
+
+

Reimplemented from SUAVE.Components.Energy.Energy_Component.Energy_Component.

+ +
+
+ +

◆ compute()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Components.Energy.Converters.de_Laval_Nozzle.de_Laval_Nozzle.compute ( self,
 conditions 
)
+
+
This computes the output values from the input values according to
+equations from the source.
+
+Assumptions:
+Constant polytropic efficiency and pressure ratio
+Isentropic Process from chamber to throat (Pt_throat = Pt2)
+Supersonic/Throat is Choked
+
+Source:
+Chapter 7
+https://web.stanford.edu/~cantwell/AA283_Course_Material/AA283_Course_Notes/
+
+Inputs:
+self.inputs.
+  combustion_temperature              [k]
+  combustion_pressure                 [Pa]
+  isentropic_expansion_factor         [-]
+  gas_specific_constant               [J/(kg-K)]
+             
+Outputs:
+self.outputs.
+  stagnation_pressure                 [Pa]
+  stagnation_temperature              [K]  
+  static_temperature                  [K]
+  static_pressure                     [Pa]
+  mach_number                         [-]
+  velocity                            [m/s]
+
+Properties Used:
+self.
+  pressure_ratio                      [-]
+  polytropic_efficiency               [-]
+  area_throat                         [m^2]
+  expansion_ratio                     [-]
+
+
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Energy/Converters/de_Laval_Nozzle.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1de__Laval__Nozzle_1_1de__Laval__Nozzle.js b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1de__Laval__Nozzle_1_1de__Laval__Nozzle.js new file mode 100644 index 00000000..381956b7 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1de__Laval__Nozzle_1_1de__Laval__Nozzle.js @@ -0,0 +1,11 @@ +var classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1de__Laval__Nozzle_1_1de__Laval__Nozzle = +[ + [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1de__Laval__Nozzle_1_1de__Laval__Nozzle.html#a1a44a5cfbba9d83ae09d1b69a02fddb7", null ], + [ "compute", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1de__Laval__Nozzle_1_1de__Laval__Nozzle.html#a8fe149bbabee596b6b5b038205af48ea", null ], + [ "area_throat", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1de__Laval__Nozzle_1_1de__Laval__Nozzle.html#a9bada391c12cd2ebc70234fc5314453b", null ], + [ "expansion_ratio", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1de__Laval__Nozzle_1_1de__Laval__Nozzle.html#a24167b2ab6e843f6463175784196c4be", null ], + [ "polytropic_efficiency", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1de__Laval__Nozzle_1_1de__Laval__Nozzle.html#a602ee01e5c88b5d74480889413a88328", null ], + [ "pressure_ratio_converge", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1de__Laval__Nozzle_1_1de__Laval__Nozzle.html#a2077609f727d9165fe7fdba2b7e23ee7", null ], + [ "pressure_ratio_diverge", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1de__Laval__Nozzle_1_1de__Laval__Nozzle.html#a73cf442b827b95031637c392d2b0591f", null ], + [ "tag", "classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1de__Laval__Nozzle_1_1de__Laval__Nozzle.html#ae970258310f84a253d0e11a8a8a262f1", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1de__Laval__Nozzle_1_1de__Laval__Nozzle.png b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1de__Laval__Nozzle_1_1de__Laval__Nozzle.png new file mode 100644 index 00000000..7f247e04 Binary files /dev/null and b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Converters_1_1de__Laval__Nozzle_1_1de__Laval__Nozzle.png differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Cooling_1_1Cryocooler_1_1Cryocooler-members.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Cooling_1_1Cryocooler_1_1Cryocooler-members.html new file mode 100644 index 00000000..34501c1a --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Cooling_1_1Cryocooler_1_1Cryocooler-members.html @@ -0,0 +1,134 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
SUAVE.Components.Energy.Cooling.Cryocooler.Cryocooler Member List
+
+
+ +

This is the complete list of members for SUAVE.Components.Energy.Cooling.Cryocooler.Cryocooler, including all inherited members.

+ + + + + + + + + + + + + + + + +
__defaults__(self)SUAVE.Components.Energy.Cooling.Cryocooler.Cryocooler
ambient_temp (defined in SUAVE.Components.Energy.Cooling.Cryocooler.Cryocooler)SUAVE.Components.Energy.Cooling.Cryocooler.Cryocooler
cooler_type (defined in SUAVE.Components.Energy.Cooling.Cryocooler.Cryocooler)SUAVE.Components.Energy.Cooling.Cryocooler.Cryocooler
energy_calc(self, cooling_power, cryo_temp, amb_temp)SUAVE.Components.Energy.Cooling.Cryocooler.Cryocooler
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
min_cryo_temp (defined in SUAVE.Components.Energy.Cooling.Cryocooler.Cryocooler)SUAVE.Components.Energy.Cooling.Cryocooler.Cryocooler
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
rated_power (defined in SUAVE.Components.Energy.Cooling.Cryocooler.Cryocooler)SUAVE.Components.Energy.Cooling.Cryocooler.Cryocooler
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Cooling_1_1Cryocooler_1_1Cryocooler.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Cooling_1_1Cryocooler_1_1Cryocooler.html new file mode 100644 index 00000000..e34d4808 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Cooling_1_1Cryocooler_1_1Cryocooler.html @@ -0,0 +1,299 @@ + + + + + + + +SUAVE: SUAVE.Components.Energy.Cooling.Cryocooler.Cryocooler Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Components.Energy.Cooling.Cryocooler.Cryocooler Class Reference
+
+
+
+Inheritance diagram for SUAVE.Components.Energy.Cooling.Cryocooler.Cryocooler:
+
+
+ + +SUAVE.Components.Energy.Energy_Component.Energy_Component +SUAVE.Components.Physical_Component.Physical_Component +SUAVE.Components.Component.Component + +
+ + + + + + +

+Public Member Functions

def __defaults__ (self)
 
def energy_calc (self, cooling_power, cryo_temp, amb_temp)
 
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Attributes

cooler_type
 
rated_power
 
min_cryo_temp
 
ambient_temp
 
- Public Attributes inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
inputs
 
outputs
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 
+

Detailed Description

+
Cryocooler provides cooling power to cryogenic components.
+Energy is used by this component to provide the cooling, despite the cooling power provided also being an energy inflow.
+

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Components.Energy.Cooling.Cryocooler.Cryocooler.__defaults__ ( self)
+
+
This sets the default inputs and outputs data structure.
+
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+None
+
+Outputs:
+None
+
+Properties Used:
+N/A
+
+

Reimplemented from SUAVE.Components.Energy.Energy_Component.Energy_Component.

+ +
+
+ +

◆ energy_calc()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Components.Energy.Cooling.Cryocooler.Cryocooler.energy_calc ( self,
 cooling_power,
 cryo_temp,
 amb_temp 
)
+
+
Calculate the power required by the cryocooler based on the cryocooler type, the required cooling power, and the temperature conditions.
+    
+    Assumptions:
+Based on mass data for Cryomech cryocoolers as per the datasheets for ground based non-massreduced coolers available via the cryomech website: https://www.cryomech.com/cryocoolers/.
+The mass is calculated for the requested power level, the cryocooler should be sized for the maximum power level required as its mass will not change during the flight.
+The efficiency scales with required cooling power and temperature only.
+The temperature difference and efficiency are taken not to scale with ambient temperature. This should not matter in the narrow range of temperatures in which aircraft operate, i.e. for ambient temperatures between -50 and 50 C.
+
+    Source: 
+https://www.cryomech.com/cryocoolers/
+
+    Inputs:
+
+    cooling_power -     cooling power required of the cryocooler                                [watts]
+    cryo_temp -         cryogenic output temperature required                                   [kelvin]
+    amb_temp -          ambient temperature the cooler will reject heat to, defaults to 19C     [kelvin]
+    cooler_type -       cryocooler type used
+ 
+    
+    Outputs:
+
+    input_power -   electrical input power required by the cryocooler         [watts]
+    mass -          mass of the cryocooler and supporting components          [kilogram]
+
+    Properties Used:
+N/A
+
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Energy/Cooling/Cryocooler.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Cooling_1_1Cryocooler_1_1Cryocooler.js b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Cooling_1_1Cryocooler_1_1Cryocooler.js new file mode 100644 index 00000000..5c4c05f3 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Cooling_1_1Cryocooler_1_1Cryocooler.js @@ -0,0 +1,9 @@ +var classSUAVE_1_1Components_1_1Energy_1_1Cooling_1_1Cryocooler_1_1Cryocooler = +[ + [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Cooling_1_1Cryocooler_1_1Cryocooler.html#a1e9c64afd3e9f64e595624f908b2b84e", null ], + [ "energy_calc", "classSUAVE_1_1Components_1_1Energy_1_1Cooling_1_1Cryocooler_1_1Cryocooler.html#acbdcf38e86787b420e7020204cedf511", null ], + [ "ambient_temp", "classSUAVE_1_1Components_1_1Energy_1_1Cooling_1_1Cryocooler_1_1Cryocooler.html#aa6d834d69173a7e40b2c0c5c14acc892", null ], + [ "cooler_type", "classSUAVE_1_1Components_1_1Energy_1_1Cooling_1_1Cryocooler_1_1Cryocooler.html#a8ce7d573bb71da82683c8012c77ffb8e", null ], + [ "min_cryo_temp", "classSUAVE_1_1Components_1_1Energy_1_1Cooling_1_1Cryocooler_1_1Cryocooler.html#a1ba35e3e5e3d902e4041de3fcabb0154", null ], + [ "rated_power", "classSUAVE_1_1Components_1_1Energy_1_1Cooling_1_1Cryocooler_1_1Cryocooler.html#a110a6be2d39cf9032438fafe09270011", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Cooling_1_1Cryocooler_1_1Cryocooler.png b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Cooling_1_1Cryocooler_1_1Cryocooler.png new file mode 100644 index 00000000..f0dcd1df Binary files /dev/null and b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Cooling_1_1Cryocooler_1_1Cryocooler.png differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Cooling_1_1Cryogenic__Heat__Exchanger_1_1Cryogenic__Heat__Exchanger-members.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Cooling_1_1Cryogenic__Heat__Exchanger_1_1Cryogenic__Heat__Exchanger-members.html new file mode 100644 index 00000000..bf0475f2 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Cooling_1_1Cryogenic__Heat__Exchanger_1_1Cryogenic__Heat__Exchanger-members.html @@ -0,0 +1,135 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
SUAVE.Components.Energy.Cooling.Cryogenic_Heat_Exchanger.Cryogenic_Heat_Exchanger Member List
+
+
+ +

This is the complete list of members for SUAVE.Components.Energy.Cooling.Cryogenic_Heat_Exchanger.Cryogenic_Heat_Exchanger, including all inherited members.

+ + + + + + + + + + + + + + + + + +
__defaults__(self)SUAVE.Components.Energy.Cooling.Cryogenic_Heat_Exchanger.Cryogenic_Heat_Exchanger
cryogen (defined in SUAVE.Components.Energy.Cooling.Cryogenic_Heat_Exchanger.Cryogenic_Heat_Exchanger)SUAVE.Components.Energy.Cooling.Cryogenic_Heat_Exchanger.Cryogenic_Heat_Exchanger
cryogen_inlet_temperature (defined in SUAVE.Components.Energy.Cooling.Cryogenic_Heat_Exchanger.Cryogenic_Heat_Exchanger)SUAVE.Components.Energy.Cooling.Cryogenic_Heat_Exchanger.Cryogenic_Heat_Exchanger
cryogen_is_fuel (defined in SUAVE.Components.Energy.Cooling.Cryogenic_Heat_Exchanger.Cryogenic_Heat_Exchanger)SUAVE.Components.Energy.Cooling.Cryogenic_Heat_Exchanger.Cryogenic_Heat_Exchanger
cryogen_outlet_temperature (defined in SUAVE.Components.Energy.Cooling.Cryogenic_Heat_Exchanger.Cryogenic_Heat_Exchanger)SUAVE.Components.Energy.Cooling.Cryogenic_Heat_Exchanger.Cryogenic_Heat_Exchanger
cryogen_pressure (defined in SUAVE.Components.Energy.Cooling.Cryogenic_Heat_Exchanger.Cryogenic_Heat_Exchanger)SUAVE.Components.Energy.Cooling.Cryogenic_Heat_Exchanger.Cryogenic_Heat_Exchanger
energy_calc(self, cooling_power, conditions)SUAVE.Components.Energy.Cooling.Cryogenic_Heat_Exchanger.Cryogenic_Heat_Exchanger
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Energy.Cooling.Cryogenic_Heat_Exchanger.Cryogenic_Heat_Exchanger)SUAVE.Components.Energy.Cooling.Cryogenic_Heat_Exchanger.Cryogenic_Heat_Exchanger
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Cooling_1_1Cryogenic__Heat__Exchanger_1_1Cryogenic__Heat__Exchanger.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Cooling_1_1Cryogenic__Heat__Exchanger_1_1Cryogenic__Heat__Exchanger.html new file mode 100644 index 00000000..66175949 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Cooling_1_1Cryogenic__Heat__Exchanger_1_1Cryogenic__Heat__Exchanger.html @@ -0,0 +1,296 @@ + + + + + + + +SUAVE: SUAVE.Components.Energy.Cooling.Cryogenic_Heat_Exchanger.Cryogenic_Heat_Exchanger Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Components.Energy.Cooling.Cryogenic_Heat_Exchanger.Cryogenic_Heat_Exchanger Class Reference
+
+
+
+Inheritance diagram for SUAVE.Components.Energy.Cooling.Cryogenic_Heat_Exchanger.Cryogenic_Heat_Exchanger:
+
+
+ + +SUAVE.Components.Energy.Energy_Component.Energy_Component +SUAVE.Components.Physical_Component.Physical_Component +SUAVE.Components.Component.Component + +
+ + + + + + +

+Public Member Functions

def __defaults__ (self)
 
def energy_calc (self, cooling_power, conditions)
 
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Attributes

tag
 
cryogen
 
cryogen_inlet_temperature
 
cryogen_outlet_temperature
 
cryogen_pressure
 
cryogen_is_fuel
 
- Public Attributes inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
inputs
 
outputs
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 
+

Detailed Description

+
This provides output values for a heat exchanger used to cool cryogenic components
+
+Assumptions:
+None
+
+Source:
+N/A
+

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Components.Energy.Cooling.Cryogenic_Heat_Exchanger.Cryogenic_Heat_Exchanger.__defaults__ ( self)
+
+
This sets the default values for the component to function.
+
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+None
+
+Outputs:
+None
+
+Properties Used:
+None
+
+

Reimplemented from SUAVE.Components.Energy.Energy_Component.Energy_Component.

+ +
+
+ +

◆ energy_calc()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Components.Energy.Cooling.Cryogenic_Heat_Exchanger.Cryogenic_Heat_Exchanger.energy_calc ( self,
 cooling_power,
 conditions 
)
+
+
This calculates the mass of cryogen required to achieve the desired cooling power given the temperature of the cryogen supplied, and the desired temperature of the cryogenic equipment.
+
+Assumptions:
+Perfect thermal conduction of the cryogen to the cooled equipment.
+
+Source:
+N/A
+
+Inputs:
+cryogenic_heat_exchanger.
+    cryogen_inlet_temperature       [K]
+    cryogen_outlet_temperature      [K]
+    cryogen_pressure                [Pa]
+
+Outputs:
+cryogen_mass_flow                   [kg/s]
+
+Properties Used:
+
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Energy/Cooling/Cryogenic_Heat_Exchanger.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Cooling_1_1Cryogenic__Heat__Exchanger_1_1Cryogenic__Heat__Exchanger.js b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Cooling_1_1Cryogenic__Heat__Exchanger_1_1Cryogenic__Heat__Exchanger.js new file mode 100644 index 00000000..982164b8 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Cooling_1_1Cryogenic__Heat__Exchanger_1_1Cryogenic__Heat__Exchanger.js @@ -0,0 +1,11 @@ +var classSUAVE_1_1Components_1_1Energy_1_1Cooling_1_1Cryogenic__Heat__Exchanger_1_1Cryogenic__Heat__Exchanger = +[ + [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Cooling_1_1Cryogenic__Heat__Exchanger_1_1Cryogenic__Heat__Exchanger.html#ad8e6eb394110cac1a8c5fb6d487fe876", null ], + [ "energy_calc", "classSUAVE_1_1Components_1_1Energy_1_1Cooling_1_1Cryogenic__Heat__Exchanger_1_1Cryogenic__Heat__Exchanger.html#aa2d2569d9695b40f072195ff7699aecb", null ], + [ "cryogen", "classSUAVE_1_1Components_1_1Energy_1_1Cooling_1_1Cryogenic__Heat__Exchanger_1_1Cryogenic__Heat__Exchanger.html#ae0b9ae828a7012fb8d0b2951b1e8f624", null ], + [ "cryogen_inlet_temperature", "classSUAVE_1_1Components_1_1Energy_1_1Cooling_1_1Cryogenic__Heat__Exchanger_1_1Cryogenic__Heat__Exchanger.html#a3b281b11b25b930ec097e7f4ae8acd83", null ], + [ "cryogen_is_fuel", "classSUAVE_1_1Components_1_1Energy_1_1Cooling_1_1Cryogenic__Heat__Exchanger_1_1Cryogenic__Heat__Exchanger.html#a501f4f90b51e8b39160c438cf6425bad", null ], + [ "cryogen_outlet_temperature", "classSUAVE_1_1Components_1_1Energy_1_1Cooling_1_1Cryogenic__Heat__Exchanger_1_1Cryogenic__Heat__Exchanger.html#a301aa7079efd4cdf85944e3f99774174", null ], + [ "cryogen_pressure", "classSUAVE_1_1Components_1_1Energy_1_1Cooling_1_1Cryogenic__Heat__Exchanger_1_1Cryogenic__Heat__Exchanger.html#a5ccc502e6582ba60dc2e261d6d49cd6e", null ], + [ "tag", "classSUAVE_1_1Components_1_1Energy_1_1Cooling_1_1Cryogenic__Heat__Exchanger_1_1Cryogenic__Heat__Exchanger.html#a85d743cb7df00c40f0d44c9abc9a5be6", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Cooling_1_1Cryogenic__Heat__Exchanger_1_1Cryogenic__Heat__Exchanger.png b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Cooling_1_1Cryogenic__Heat__Exchanger_1_1Cryogenic__Heat__Exchanger.png new file mode 100644 index 00000000..17acdcbd Binary files /dev/null and b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Cooling_1_1Cryogenic__Heat__Exchanger_1_1Cryogenic__Heat__Exchanger.png differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Cryogenic__Lead_1_1Cryogenic__Lead-members.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Cryogenic__Lead_1_1Cryogenic__Lead-members.html new file mode 100644 index 00000000..438d8b00 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Cryogenic__Lead_1_1Cryogenic__Lead-members.html @@ -0,0 +1,144 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
SUAVE.Components.Energy.Distributors.Cryogenic_Lead.Cryogenic_Lead Member List
+
+
+ +

This is the complete list of members for SUAVE.Components.Energy.Distributors.Cryogenic_Lead.Cryogenic_Lead, including all inherited members.

+ + + + + + + + + + + + + + + + + + + + + + + + + + +
__defaults__(self)SUAVE.Components.Energy.Distributors.Cryogenic_Lead.Cryogenic_Lead
calc_current(self, current) (defined in SUAVE.Components.Energy.Distributors.Cryogenic_Lead.Cryogenic_Lead)SUAVE.Components.Energy.Distributors.Cryogenic_Lead.Cryogenic_Lead
cold_temp (defined in SUAVE.Components.Energy.Distributors.Cryogenic_Lead.Cryogenic_Lead)SUAVE.Components.Energy.Distributors.Cryogenic_Lead.Cryogenic_Lead
cross_section (defined in SUAVE.Components.Energy.Distributors.Cryogenic_Lead.Cryogenic_Lead)SUAVE.Components.Energy.Distributors.Cryogenic_Lead.Cryogenic_Lead
current (defined in SUAVE.Components.Energy.Distributors.Cryogenic_Lead.Cryogenic_Lead)SUAVE.Components.Energy.Distributors.Cryogenic_Lead.Cryogenic_Lead
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
hot_temp (defined in SUAVE.Components.Energy.Distributors.Cryogenic_Lead.Cryogenic_Lead)SUAVE.Components.Energy.Distributors.Cryogenic_Lead.Cryogenic_Lead
initialize_material_lead(self)SUAVE.Components.Energy.Distributors.Cryogenic_Lead.Cryogenic_Lead
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
LARatio(self, material, cold_temp, hot_temp, current, minimum_Q) (defined in SUAVE.Components.Energy.Distributors.Cryogenic_Lead.Cryogenic_Lead)SUAVE.Components.Energy.Distributors.Cryogenic_Lead.Cryogenic_Lead
length (defined in SUAVE.Components.Energy.Distributors.Cryogenic_Lead.Cryogenic_Lead)SUAVE.Components.Energy.Distributors.Cryogenic_Lead.Cryogenic_Lead
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
material (defined in SUAVE.Components.Energy.Distributors.Cryogenic_Lead.Cryogenic_Lead)SUAVE.Components.Energy.Distributors.Cryogenic_Lead.Cryogenic_Lead
minimum_Q (defined in SUAVE.Components.Energy.Distributors.Cryogenic_Lead.Cryogenic_Lead)SUAVE.Components.Energy.Distributors.Cryogenic_Lead.Cryogenic_Lead
optimum_current (defined in SUAVE.Components.Energy.Distributors.Cryogenic_Lead.Cryogenic_Lead)SUAVE.Components.Energy.Distributors.Cryogenic_Lead.Cryogenic_Lead
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
Q_min(self, material, cold_temp, hot_temp, current) (defined in SUAVE.Components.Energy.Distributors.Cryogenic_Lead.Cryogenic_Lead)SUAVE.Components.Energy.Distributors.Cryogenic_Lead.Cryogenic_Lead
Q_offdesign(self, current) (defined in SUAVE.Components.Energy.Distributors.Cryogenic_Lead.Cryogenic_Lead)SUAVE.Components.Energy.Distributors.Cryogenic_Lead.Cryogenic_Lead
Q_unpowered(self) (defined in SUAVE.Components.Energy.Distributors.Cryogenic_Lead.Cryogenic_Lead)SUAVE.Components.Energy.Distributors.Cryogenic_Lead.Cryogenic_Lead
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
unpowered_Q (defined in SUAVE.Components.Energy.Distributors.Cryogenic_Lead.Cryogenic_Lead)SUAVE.Components.Energy.Distributors.Cryogenic_Lead.Cryogenic_Lead
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Cryogenic__Lead_1_1Cryogenic__Lead.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Cryogenic__Lead_1_1Cryogenic__Lead.html new file mode 100644 index 00000000..78c6fa91 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Cryogenic__Lead_1_1Cryogenic__Lead.html @@ -0,0 +1,296 @@ + + + + + + + +SUAVE: SUAVE.Components.Energy.Distributors.Cryogenic_Lead.Cryogenic_Lead Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Components.Energy.Distributors.Cryogenic_Lead.Cryogenic_Lead Class Reference
+
+
+
+Inheritance diagram for SUAVE.Components.Energy.Distributors.Cryogenic_Lead.Cryogenic_Lead:
+
+
+ + +SUAVE.Components.Energy.Energy_Component.Energy_Component +SUAVE.Components.Physical_Component.Physical_Component +SUAVE.Components.Component.Component + +
+ + + + + + + + + + + + + + + + +

+Public Member Functions

def __defaults__ (self)
 
+def Q_min (self, material, cold_temp, hot_temp, current)
 
+def LARatio (self, material, cold_temp, hot_temp, current, minimum_Q)
 
def initialize_material_lead (self)
 
+def Q_unpowered (self)
 
+def Q_offdesign (self, current)
 
+def calc_current (self, current)
 
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Attributes

cold_temp
 
hot_temp
 
current
 
length
 
material
 
cross_section
 
optimum_current
 
minimum_Q
 
unpowered_Q
 
- Public Attributes inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
inputs
 
outputs
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 
+

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Components.Energy.Distributors.Cryogenic_Lead.Cryogenic_Lead.__defaults__ ( self)
+
+
This sets the default values.
+    
+    Assumptions:
+    Cryogenic Leads only operate at their optimum current, or at zero current.
+    
+    Source:
+    Current Lead Optimization for Cryogenic Operation at Intermediate Temperatures - Broomberg
+    
+    Inputs:
+    None
+    
+    Outputs:
+    None
+    
+    Properties Used:
+    None
+

Reimplemented from SUAVE.Components.Energy.Energy_Component.Energy_Component.

+ +
+
+ +

◆ initialize_material_lead()

+ +
+
+ + + + + + + + +
def SUAVE.Components.Energy.Distributors.Cryogenic_Lead.Cryogenic_Lead.initialize_material_lead ( self)
+
+
Defines an optimum material lead for supplying current to a cryogenic environment given the operating conditions and material properties.
+
+Assumptions:
+None
+
+Inputs:
+    lead.
+cold_temp           [K]
+hot_temp            [K]
+current             [A]
+length              [m]
+
+Outputs:      
+    lead.     
+mass                [kg]
+cross_section       [m]
+optimum_current     [A]
+minimum_Q           [W]
+
+
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Energy/Distributors/Cryogenic_Lead.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Cryogenic__Lead_1_1Cryogenic__Lead.js b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Cryogenic__Lead_1_1Cryogenic__Lead.js new file mode 100644 index 00000000..6efc96b6 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Cryogenic__Lead_1_1Cryogenic__Lead.js @@ -0,0 +1,19 @@ +var classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Cryogenic__Lead_1_1Cryogenic__Lead = +[ + [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Cryogenic__Lead_1_1Cryogenic__Lead.html#a0ed67d57dddce6fb74a85e81d9bf7108", null ], + [ "calc_current", "classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Cryogenic__Lead_1_1Cryogenic__Lead.html#a45714a7246fa3fcd5f624e145518bbca", null ], + [ "initialize_material_lead", "classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Cryogenic__Lead_1_1Cryogenic__Lead.html#a7c575925b26d2b53f92f783a8f5fb391", null ], + [ "LARatio", "classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Cryogenic__Lead_1_1Cryogenic__Lead.html#aa4687f410e3408a76e1ce09380a28417", null ], + [ "Q_min", "classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Cryogenic__Lead_1_1Cryogenic__Lead.html#aba6567110f7d7bc3ff2ab3fd8e0c77eb", null ], + [ "Q_offdesign", "classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Cryogenic__Lead_1_1Cryogenic__Lead.html#a9af6f5a86aeb52e3ac520a089cb6fcbf", null ], + [ "Q_unpowered", "classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Cryogenic__Lead_1_1Cryogenic__Lead.html#ace082ae811edde38350c4e7f7cd6c5b3", null ], + [ "cold_temp", "classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Cryogenic__Lead_1_1Cryogenic__Lead.html#a0cb08a512bb95203ebb008210d0a33f0", null ], + [ "cross_section", "classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Cryogenic__Lead_1_1Cryogenic__Lead.html#a2b2bef493f79ff0bb7fa68f35a213656", null ], + [ "current", "classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Cryogenic__Lead_1_1Cryogenic__Lead.html#ad32d083bfaf9a4ae0fd9930d607d8ed6", null ], + [ "hot_temp", "classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Cryogenic__Lead_1_1Cryogenic__Lead.html#ad4aef827431a376d0c8fad5e3c3f5590", null ], + [ "length", "classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Cryogenic__Lead_1_1Cryogenic__Lead.html#a084db5aae5bc6bce5d71090fc80e3216", null ], + [ "material", "classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Cryogenic__Lead_1_1Cryogenic__Lead.html#a7fa6a82a5fd2464b0c81287e550b54c7", null ], + [ "minimum_Q", "classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Cryogenic__Lead_1_1Cryogenic__Lead.html#aa7ab8168691a5f2ac17a694bfb15126d", null ], + [ "optimum_current", "classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Cryogenic__Lead_1_1Cryogenic__Lead.html#a299f9167fe69cb22fb04dcec243648c4", null ], + [ "unpowered_Q", "classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Cryogenic__Lead_1_1Cryogenic__Lead.html#adfd579aad157662c5533969163541b2d", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Cryogenic__Lead_1_1Cryogenic__Lead.png b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Cryogenic__Lead_1_1Cryogenic__Lead.png new file mode 100644 index 00000000..7244eb97 Binary files /dev/null and b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Cryogenic__Lead_1_1Cryogenic__Lead.png differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Electronic__Speed__Controller_1_1Electronic__Speed__Controller-members.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Electronic__Speed__Controller_1_1Electronic__Speed__Controller-members.html index 15cef5bf..d4377e6f 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Electronic__Speed__Controller_1_1Electronic__Speed__Controller-members.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Electronic__Speed__Controller_1_1Electronic__Speed__Controller-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -99,15 +106,18 @@

This is the complete list of members for SUAVE.Components.Energy.Distributors.Electronic_Speed_Controller.Electronic_Speed_Controller, including all inherited members.

- + - - - - - - - + + + + + + + + + +
__defaults__(self)SUAVE.Components.Energy.Distributors.Electronic_Speed_Controller.Electronic_Speed_Controller
currentin(self)SUAVE.Components.Energy.Distributors.Electronic_Speed_Controller.Electronic_Speed_Controller
currentin(self, conditions)SUAVE.Components.Energy.Distributors.Electronic_Speed_Controller.Electronic_Speed_Controller
efficiency (defined in SUAVE.Components.Energy.Distributors.Electronic_Speed_Controller.Electronic_Speed_Controller)SUAVE.Components.Energy.Distributors.Electronic_Speed_Controller.Electronic_Speed_Controller
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
voltageout(self, conditions)SUAVE.Components.Energy.Distributors.Electronic_Speed_Controller.Electronic_Speed_Controller
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
voltageout(self, conditions)SUAVE.Components.Energy.Distributors.Electronic_Speed_Controller.Electronic_Speed_Controller
@@ -115,7 +125,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Electronic__Speed__Controller_1_1Electronic__Speed__Controller.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Electronic__Speed__Controller_1_1Electronic__Speed__Controller.html index 9fef7d98..173c1931 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Electronic__Speed__Controller_1_1Electronic__Speed__Controller.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Electronic__Speed__Controller_1_1Electronic__Speed__Controller.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Components.Energy.Distributors.Electronic_Speed_Controller.Electronic_Speed_Controller Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -108,8 +115,8 @@ SUAVE.Components.Energy.Energy_Component.Energy_Component SUAVE.Components.Physical_Component.Physical_Component SUAVE.Components.Component.Component - -
+ + @@ -117,17 +124,8 @@ - - - - - - - - - - - + +

Public Member Functions

 
def voltageout (self, conditions)
 
def currentin (self)
 
- Public Member Functions inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
def currentin (self, conditions)
 
@@ -161,6 +159,15 @@ + + + + + +

Public Attributes

 origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 

Member Function Documentation

@@ -194,10 +201,12 @@

SUAVE.Components.Energy.Energy_Component.Energy_Component.

+ - -

◆ currentin()

+ +

◆ currentin()

diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Electronic__Speed__Controller_1_1Electronic__Speed__Controller.js b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Electronic__Speed__Controller_1_1Electronic__Speed__Controller.js index 0528f68e..d60d4ec1 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Electronic__Speed__Controller_1_1Electronic__Speed__Controller.js +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Electronic__Speed__Controller_1_1Electronic__Speed__Controller.js @@ -1,7 +1,7 @@ var classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Electronic__Speed__Controller_1_1Electronic__Speed__Controller = [ [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Electronic__Speed__Controller_1_1Electronic__Speed__Controller.html#ade7b4c9066bfdee04532a683a20849b7", null ], - [ "currentin", "classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Electronic__Speed__Controller_1_1Electronic__Speed__Controller.html#ad8605cbf070de0139fee6ece5116580f", null ], + [ "currentin", "classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Electronic__Speed__Controller_1_1Electronic__Speed__Controller.html#a07846d752fbd6202138fcdacf69719a0", null ], [ "voltageout", "classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Electronic__Speed__Controller_1_1Electronic__Speed__Controller.html#a59e19c06939c4420d52a3f645e9b0c20", null ], [ "efficiency", "classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Electronic__Speed__Controller_1_1Electronic__Speed__Controller.html#af2049585ddd8e6ba97dc13591526b273", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1HTS__DC__Supply_1_1HTS__DC__Supply-members.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1HTS__DC__Supply_1_1HTS__DC__Supply-members.html new file mode 100644 index 00000000..553d0dcf --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1HTS__DC__Supply_1_1HTS__DC__Supply-members.html @@ -0,0 +1,133 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
SUAVE.Components.Energy.Distributors.HTS_DC_Supply.HTS_DC_Supply Member List
+
+
+ +

This is the complete list of members for SUAVE.Components.Energy.Distributors.HTS_DC_Supply.HTS_DC_Supply, including all inherited members.

+ + + + + + + + + + + + + + + +
__defaults__(self)SUAVE.Components.Energy.Distributors.HTS_DC_Supply.HTS_DC_Supply
efficiency (defined in SUAVE.Components.Energy.Distributors.HTS_DC_Supply.HTS_DC_Supply)SUAVE.Components.Energy.Distributors.HTS_DC_Supply.HTS_DC_Supply
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
power(self, current, power_out)SUAVE.Components.Energy.Distributors.HTS_DC_Supply.HTS_DC_Supply
rated_current (defined in SUAVE.Components.Energy.Distributors.HTS_DC_Supply.HTS_DC_Supply)SUAVE.Components.Energy.Distributors.HTS_DC_Supply.HTS_DC_Supply
rated_power (defined in SUAVE.Components.Energy.Distributors.HTS_DC_Supply.HTS_DC_Supply)SUAVE.Components.Energy.Distributors.HTS_DC_Supply.HTS_DC_Supply
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1HTS__DC__Supply_1_1HTS__DC__Supply.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1HTS__DC__Supply_1_1HTS__DC__Supply.html new file mode 100644 index 00000000..cc386e42 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1HTS__DC__Supply_1_1HTS__DC__Supply.html @@ -0,0 +1,277 @@ + + + + + + + +SUAVE: SUAVE.Components.Energy.Distributors.HTS_DC_Supply.HTS_DC_Supply Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Components.Energy.Distributors.HTS_DC_Supply.HTS_DC_Supply Class Reference
+
+
+
+Inheritance diagram for SUAVE.Components.Energy.Distributors.HTS_DC_Supply.HTS_DC_Supply:
+
+
+ + +SUAVE.Components.Energy.Energy_Component.Energy_Component +SUAVE.Components.Physical_Component.Physical_Component +SUAVE.Components.Component.Component + +
+ + + + + + +

+Public Member Functions

def __defaults__ (self)
 
def power (self, current, power_out)
 
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Attributes

efficiency
 
rated_current
 
rated_power
 
- Public Attributes inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
inputs
 
outputs
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 
+

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Components.Energy.Distributors.HTS_DC_Supply.HTS_DC_Supply.__defaults__ ( self)
+
+
This sets the default values.
+    
+    Assumptions:
+    None
+    
+    Source:
+    N/A
+    
+    Inputs:
+    None
+    
+    Outputs:
+    None
+    
+    Properties Used:
+    None
+

Reimplemented from SUAVE.Components.Energy.Energy_Component.Energy_Component.

+ +
+
+ +

◆ power()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Components.Energy.Distributors.HTS_DC_Supply.HTS_DC_Supply.power ( self,
 current,
 power_out 
)
+
+
The power that must be supplied to the DC supply to power the HTS coils.
+
+    Assumptions:
+    Supply cable is solid copper, i.e. not a rotating joint.
+    Power supply has static efficiency across current output range.
+    Power supply performance is not affected by altitude or other environmental factors. This is not generally true (Ametek SGe datasheet should be derated by 10% per 1000 feet) for current supplies designed for ground use however a supply specifically designed for airborne use can be expected to have a more appropriate cooling design that would allow high altitude use.
+
+    Source:
+    N/A
+
+    Inputs:
+    current             [A]
+    power_out           [W]
+    self.efficiency
+
+    Outputs:
+    power_in            [W]
+
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Energy/Distributors/HTS_DC_Supply.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1HTS__DC__Supply_1_1HTS__DC__Supply.js b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1HTS__DC__Supply_1_1HTS__DC__Supply.js new file mode 100644 index 00000000..4d30db86 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1HTS__DC__Supply_1_1HTS__DC__Supply.js @@ -0,0 +1,8 @@ +var classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1HTS__DC__Supply_1_1HTS__DC__Supply = +[ + [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1HTS__DC__Supply_1_1HTS__DC__Supply.html#ad680e5af2d9f107de99f0e7ce095440c", null ], + [ "power", "classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1HTS__DC__Supply_1_1HTS__DC__Supply.html#a81293f8eda0449e6da3d0d4d681337e8", null ], + [ "efficiency", "classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1HTS__DC__Supply_1_1HTS__DC__Supply.html#a78f3c854b949576450dd0850d9c2445d", null ], + [ "rated_current", "classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1HTS__DC__Supply_1_1HTS__DC__Supply.html#ace07e5ae8df4772f7d0a1afe9744731f", null ], + [ "rated_power", "classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1HTS__DC__Supply_1_1HTS__DC__Supply.html#a61df3a5d0ad2f430e150af42ae52ef71", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1HTS__DC__Supply_1_1HTS__DC__Supply.png b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1HTS__DC__Supply_1_1HTS__DC__Supply.png new file mode 100644 index 00000000..da765157 Binary files /dev/null and b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1HTS__DC__Supply_1_1HTS__DC__Supply.png differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Solar__Logic_1_1Solar__Logic-members.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Solar__Logic_1_1Solar__Logic-members.html index cd58f991..caa2f771 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Solar__Logic_1_1Solar__Logic-members.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Solar__Logic_1_1Solar__Logic-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@
- +
@@ -73,7 +78,9 @@
@@ -99,16 +106,19 @@

This is the complete list of members for SUAVE.Components.Energy.Distributors.Solar_Logic.Solar_Logic, including all inherited members.

- - - - - - - - - - + + + + + + + + + + + + +
__defaults__(self)SUAVE.Components.Energy.Distributors.Solar_Logic.Solar_Logic
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
logic(self, conditions, numerics)SUAVE.Components.Energy.Distributors.Solar_Logic.Solar_Logic
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
MPPT_efficiency (defined in SUAVE.Components.Energy.Distributors.Solar_Logic.Solar_Logic)SUAVE.Components.Energy.Distributors.Solar_Logic.Solar_Logic
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
system_voltage (defined in SUAVE.Components.Energy.Distributors.Solar_Logic.Solar_Logic)SUAVE.Components.Energy.Distributors.Solar_Logic.Solar_Logic
tag (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
voltage(self)SUAVE.Components.Energy.Distributors.Solar_Logic.Solar_Logic
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
logic(self, conditions, numerics)SUAVE.Components.Energy.Distributors.Solar_Logic.Solar_Logic
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
MPPT_efficiency (defined in SUAVE.Components.Energy.Distributors.Solar_Logic.Solar_Logic)SUAVE.Components.Energy.Distributors.Solar_Logic.Solar_Logic
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
system_voltage (defined in SUAVE.Components.Energy.Distributors.Solar_Logic.Solar_Logic)SUAVE.Components.Energy.Distributors.Solar_Logic.Solar_Logic
tag (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
voltage(self)SUAVE.Components.Energy.Distributors.Solar_Logic.Solar_Logic
@@ -116,7 +126,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Solar__Logic_1_1Solar__Logic.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Solar__Logic_1_1Solar__Logic.html index 1aa677df..8ec4c385 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Solar__Logic_1_1Solar__Logic.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Distributors_1_1Solar__Logic_1_1Solar__Logic.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Components.Energy.Distributors.Solar_Logic.Solar_Logic Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -108,8 +115,8 @@ SUAVE.Components.Energy.Energy_Component.Energy_Component SUAVE.Components.Physical_Component.Physical_Component SUAVE.Components.Component.Component - -
+ + @@ -119,15 +126,6 @@ - - - - - - - - -

Public Member Functions

 
def logic (self, conditions, numerics)
 
- Public Member Functions inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
@@ -164,6 +162,15 @@ + + + + + +

Public Attributes

 origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 

Detailed Description

The distributor is a component unique to a solar aircraft. This controls the flow of energy in to and from the battery.
@@ -208,6 +215,8 @@ 

SUAVE.Components.Energy.Energy_Component.Energy_Component.

+

@@ -255,7 +264,6 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Energy_1_1Energy-members.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Energy_1_1Energy-members.html index eba71ce3..24651c7f 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Energy_1_1Energy-members.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Energy_1_1Energy-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -13,14 +13,13 @@ - @@ -33,13 +32,13 @@ Logo
SUAVE -  1.1.0 +  2.4.0
An Aerospace Vehicle Environment for Designing Future Aircraft
- @@ -48,7 +47,7 @@ onblur="searchBox.OnSearchFieldFocus(false)" onkeyup="searchBox.OnSearchFieldChange(event)"/> - +
@@ -57,9 +56,11 @@ - +
@@ -73,7 +74,9 @@
@@ -99,18 +102,19 @@

This is the complete list of members for SUAVE.Components.Energy.Energy.Energy, including all inherited members.

- - - - + + + + + + +
__defaults__(self)SUAVE.Components.Energy.Energy.Energy
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Energy_1_1Energy.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Energy_1_1Energy.html index 9a4ae992..cf557d87 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Energy_1_1Energy.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Energy_1_1Energy.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Components.Energy.Energy.Energy Class Reference @@ -13,14 +13,13 @@ - @@ -33,13 +32,13 @@ Logo
SUAVE -  1.1.0 +  2.4.0
An Aerospace Vehicle Environment for Designing Future Aircraft
- @@ -48,7 +47,7 @@ onblur="searchBox.OnSearchFieldFocus(false)" onkeyup="searchBox.OnSearchFieldChange(event)"/> - +
@@ -57,9 +56,11 @@ - +
@@ -73,7 +74,9 @@
@@ -106,19 +109,13 @@ SUAVE.Components.Physical_Component.Physical_Component SUAVE.Components.Component.Component - -
+ + - - - - - -

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
@@ -142,6 +139,15 @@ + + + + + +

Additional Inherited Members

 origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 

Detailed Description

A class representing an energy component.
@@ -184,10 +190,12 @@ 

SUAVE.Components.Physical_Component.Physical_Component.

+


The documentation for this class was generated from the following file:
    -
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Energy/Energy.py
  • +
  • /Users/matthewclarke/Documents/SUAVE/SUAVE/trunk/SUAVE/Components/Energy/Energy.py
@@ -195,9 +203,7 @@

diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Energy__Component_1_1Energy__Component-members.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Energy__Component_1_1Energy__Component-members.html index 8ffc402a..786c35cf 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Energy__Component_1_1Energy__Component-members.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Energy__Component_1_1Energy__Component-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -99,12 +106,15 @@

This is the complete list of members for SUAVE.Components.Energy.Energy_Component.Energy_Component, including all inherited members.

- - - - - - + + + + + + + + +
__defaults__(self)SUAVE.Components.Energy.Energy_Component.Energy_Component
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
@@ -112,7 +122,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Energy__Component_1_1Energy__Component.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Energy__Component_1_1Energy__Component.html index f6ebbad8..17fe8bdb 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Energy__Component_1_1Energy__Component.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Energy__Component_1_1Energy__Component.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Components.Energy.Energy_Component.Energy_Component Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -107,42 +114,52 @@ SUAVE.Components.Physical_Component.Physical_Component SUAVE.Components.Component.Component -SUAVE.Components.Energy.Converters.Combustor.Combustor -SUAVE.Components.Energy.Converters.Compression_Nozzle.Compression_Nozzle -SUAVE.Components.Energy.Converters.Compressor.Compressor -SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle -SUAVE.Components.Energy.Converters.Fan.Fan -SUAVE.Components.Energy.Converters.Fuel_Cell.Fuel_Cell -SUAVE.Components.Energy.Converters.Gearbox.Gearbox -SUAVE.Components.Energy.Converters.Motor.Motor -SUAVE.Components.Energy.Converters.Motor_Lo_Fid.Motor_Lo_Fid -SUAVE.Components.Energy.Converters.Propeller.Propeller -SUAVE.Components.Energy.Converters.Propeller_Lo_Fid.Propeller_Lo_Fid -SUAVE.Components.Energy.Converters.Ram.Ram -SUAVE.Components.Energy.Converters.Shaft_Power_Off_Take.Shaft_Power_Off_Take -SUAVE.Components.Energy.Converters.Solar_Panel.Solar_Panel -SUAVE.Components.Energy.Converters.Supersonic_Nozzle.Supersonic_Nozzle -SUAVE.Components.Energy.Converters.Turbine.Turbine -SUAVE.Components.Energy.Distributors.Electronic_Speed_Controller.Electronic_Speed_Controller -SUAVE.Components.Energy.Distributors.Solar_Logic.Solar_Logic -SUAVE.Components.Energy.Peripherals.Avionics.Avionics -SUAVE.Components.Energy.Peripherals.Payload.Payload -SUAVE.Components.Energy.Processes.Solar_Radiation.Solar_Radiation -SUAVE.Components.Energy.Processes.Thrust.Thrust -SUAVE.Components.Energy.Storages.Batteries.Battery.Battery - -
+SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_One.Rotor_Wake_Fidelity_One +SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_Two.Rotor_Wake_Fidelity_Two +SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_Zero.Rotor_Wake_Fidelity_Zero +SUAVE.Components.Energy.Charging.Charging.Charging +SUAVE.Components.Energy.Converters.Combustor.Combustor +SUAVE.Components.Energy.Converters.Compression_Nozzle.Compression_Nozzle +SUAVE.Components.Energy.Converters.Compressor.Compressor +SUAVE.Components.Energy.Converters.de_Laval_Nozzle.de_Laval_Nozzle +SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle +SUAVE.Components.Energy.Converters.Fan.Fan +SUAVE.Components.Energy.Converters.Fuel_Cell.Fuel_Cell +SUAVE.Components.Energy.Converters.Gearbox.Gearbox +SUAVE.Components.Energy.Converters.Generator_Zero_Fid.Generator_Zero_Fid +SUAVE.Components.Energy.Converters.Internal_Combustion_Engine.Internal_Combustion_Engine +SUAVE.Components.Energy.Converters.Motor.Motor +SUAVE.Components.Energy.Converters.Motor_HTS_Rotor.Motor_HTS_Rotor +SUAVE.Components.Energy.Converters.Motor_Lo_Fid.Motor_Lo_Fid +SUAVE.Components.Energy.Converters.Propeller_Lo_Fid.Propeller_Lo_Fid +SUAVE.Components.Energy.Converters.Ram.Ram +SUAVE.Components.Energy.Converters.Rocket_Combustor.Rocket_Combustor +SUAVE.Components.Energy.Converters.Rotor.Rotor +SUAVE.Components.Energy.Converters.Shaft_Power_Off_Take.Shaft_Power_Off_Take +SUAVE.Components.Energy.Converters.Solar_Panel.Solar_Panel +SUAVE.Components.Energy.Converters.Supersonic_Nozzle.Supersonic_Nozzle +SUAVE.Components.Energy.Converters.Turbine.Turbine +SUAVE.Components.Energy.Converters.Turboelectric.Turboelectric +SUAVE.Components.Energy.Cooling.Cryocooler.Cryocooler +SUAVE.Components.Energy.Cooling.Cryogenic_Heat_Exchanger.Cryogenic_Heat_Exchanger +SUAVE.Components.Energy.Distributors.Cryogenic_Lead.Cryogenic_Lead +SUAVE.Components.Energy.Distributors.Electronic_Speed_Controller.Electronic_Speed_Controller +SUAVE.Components.Energy.Distributors.HTS_DC_Supply.HTS_DC_Supply +SUAVE.Components.Energy.Distributors.Solar_Logic.Solar_Logic +SUAVE.Components.Energy.Peripherals.Avionics.Avionics +SUAVE.Components.Energy.Peripherals.Payload.Payload +SUAVE.Components.Energy.Processes.Rocket_Thrust.Rocket_Thrust +SUAVE.Components.Energy.Processes.Solar_Radiation.Solar_Radiation +SUAVE.Components.Energy.Processes.Thrust.Thrust +SUAVE.Components.Energy.Storages.Batteries.Battery.Battery +SUAVE.Components.Energy.Storages.Fuel_Tanks.Fuel_Tank.Fuel_Tank + + - - - - - -

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
@@ -172,6 +189,15 @@ + + + + + +

Public Attributes

 origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 

Detailed Description

A class representing an energy component.
@@ -214,6 +240,10 @@ 

SUAVE.Components.Physical_Component.Physical_Component.

+ +

Reimplemented in SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion_LiNiMnCoO2_18650.Lithium_Ion_LiNiMnCoO2_18650, SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion_LiFePO4_18650.Lithium_Ion_LiFePO4_18650, SUAVE.Components.Energy.Converters.Rotor.Rotor, SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle, SUAVE.Components.Energy.Converters.Supersonic_Nozzle.Supersonic_Nozzle, SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion, SUAVE.Components.Energy.Converters.Compression_Nozzle.Compression_Nozzle, SUAVE.Components.Energy.Converters.de_Laval_Nozzle.de_Laval_Nozzle, SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_One.Rotor_Wake_Fidelity_One, SUAVE.Components.Energy.Converters.Combustor.Combustor, SUAVE.Components.Energy.Converters.Compressor.Compressor, SUAVE.Components.Energy.Converters.Fan.Fan, SUAVE.Components.Energy.Converters.Ram.Ram, SUAVE.Components.Energy.Converters.Turbine.Turbine, SUAVE.Components.Energy.Distributors.Solar_Logic.Solar_Logic, SUAVE.Components.Energy.Processes.Thrust.Thrust, SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_Zero.Rotor_Wake_Fidelity_Zero, SUAVE.Components.Energy.Converters.Fuel_Cell.Fuel_Cell, SUAVE.Components.Energy.Converters.Motor.Motor, SUAVE.Components.Energy.Converters.Motor_HTS_Rotor.Motor_HTS_Rotor, SUAVE.Components.Energy.Converters.Motor_Lo_Fid.Motor_Lo_Fid, SUAVE.Components.Energy.Converters.Rocket_Combustor.Rocket_Combustor, SUAVE.Components.Energy.Converters.Gearbox.Gearbox, SUAVE.Components.Energy.Cooling.Cryogenic_Heat_Exchanger.Cryogenic_Heat_Exchanger, SUAVE.Components.Energy.Converters.Internal_Combustion_Engine.Internal_Combustion_Engine, SUAVE.Components.Energy.Converters.Propeller_Lo_Fid.Propeller_Lo_Fid, SUAVE.Components.Energy.Storages.Batteries.Battery.Battery, SUAVE.Components.Energy.Converters.Generator_Zero_Fid.Generator_Zero_Fid, SUAVE.Components.Energy.Converters.Turboelectric.Turboelectric, SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Aluminum_Air.Aluminum_Air, SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Lithium_Air.Lithium_Air, SUAVE.Components.Energy.Converters.Shaft_Power_Off_Take.Shaft_Power_Off_Take, SUAVE.Components.Energy.Cooling.Cryocooler.Cryocooler, SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_Two.Rotor_Wake_Fidelity_Two, SUAVE.Components.Energy.Converters.Solar_Panel.Solar_Panel, SUAVE.Components.Energy.Peripherals.Avionics.Avionics, SUAVE.Components.Energy.Peripherals.Payload.Payload, SUAVE.Components.Energy.Storages.Fuel_Tanks.Fuel_Tank.Fuel_Tank, SUAVE.Components.Energy.Charging.Charging.Charging, SUAVE.Components.Energy.Distributors.Cryogenic_Lead.Cryogenic_Lead, SUAVE.Components.Energy.Processes.Rocket_Thrust.Rocket_Thrust, SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Sulfur.Lithium_Sulfur, SUAVE.Components.Energy.Converters.Lift_Rotor.Lift_Rotor, SUAVE.Components.Energy.Converters.Propeller.Propeller, SUAVE.Components.Energy.Distributors.Electronic_Speed_Controller.Electronic_Speed_Controller, and SUAVE.Components.Energy.Distributors.HTS_DC_Supply.HTS_DC_Supply.

+


The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Energy__Component_1_1Energy__Component.png b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Energy__Component_1_1Energy__Component.png index 28b35d32..fc7abf57 100644 Binary files a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Energy__Component_1_1Energy__Component.png and b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Energy__Component_1_1Energy__Component.png differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Cell__Cycler_1_1Battery__Cell__Cycler-members.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Cell__Cycler_1_1Battery__Cell__Cycler-members.html new file mode 100644 index 00000000..5df043bc --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Cell__Cycler_1_1Battery__Cell__Cycler-members.html @@ -0,0 +1,138 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
SUAVE.Components.Energy.Networks.Battery_Cell_Cycler.Battery_Cell_Cycler Member List
+
+
+ +

This is the complete list of members for SUAVE.Components.Energy.Networks.Battery_Cell_Cycler.Battery_Cell_Cycler, including all inherited members.

+ + + + + + + + + + + + + + + + + + + + +
__defaults__(self)SUAVE.Components.Energy.Networks.Battery_Cell_Cycler.Battery_Cell_Cycler
add_unknowns_and_residuals_to_segment(self, segment, initial_voltage=None, initial_battery_cell_temperature=300, initial_battery_state_of_charge=0.5, initial_battery_cell_current=5.)SUAVE.Components.Energy.Networks.Battery_Cell_Cycler.Battery_Cell_Cycler
areas (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
avionics (defined in SUAVE.Components.Energy.Networks.Battery_Cell_Cycler.Battery_Cell_Cycler)SUAVE.Components.Energy.Networks.Battery_Cell_Cycler.Battery_Cell_Cycler
engine_length (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
evaluate_thrust(self, state)SUAVE.Components.Energy.Networks.Battery_Cell_Cycler.Battery_Cell_Cycler
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
non_dimensional_origin (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
number_of_engines (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
residuals(self, segment)SUAVE.Components.Energy.Networks.Battery_Cell_Cycler.Battery_Cell_Cycler
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
unpack_unknowns(self, segment)SUAVE.Components.Energy.Networks.Battery_Cell_Cycler.Battery_Cell_Cycler
voltage (defined in SUAVE.Components.Energy.Networks.Battery_Cell_Cycler.Battery_Cell_Cycler)SUAVE.Components.Energy.Networks.Battery_Cell_Cycler.Battery_Cell_Cycler
wing_mounted (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Cell__Cycler_1_1Battery__Cell__Cycler.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Cell__Cycler_1_1Battery__Cell__Cycler.html new file mode 100644 index 00000000..4978858d --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Cell__Cycler_1_1Battery__Cell__Cycler.html @@ -0,0 +1,463 @@ + + + + + + + +SUAVE: SUAVE.Components.Energy.Networks.Battery_Cell_Cycler.Battery_Cell_Cycler Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Components.Energy.Networks.Battery_Cell_Cycler.Battery_Cell_Cycler Class Reference
+
+
+
+Inheritance diagram for SUAVE.Components.Energy.Networks.Battery_Cell_Cycler.Battery_Cell_Cycler:
+
+
+ + +SUAVE.Components.Energy.Networks.Network.Network +SUAVE.Components.Physical_Component.Physical_Component +SUAVE.Components.Component.Component + +
+ + + + + + + + + + + + +

+Public Member Functions

def __defaults__ (self)
 
def evaluate_thrust (self, state)
 
def unpack_unknowns (self, segment)
 
def residuals (self, segment)
 
def add_unknowns_and_residuals_to_segment (self, segment, initial_voltage=None, initial_battery_cell_temperature=300, initial_battery_state_of_charge=0.5, initial_battery_cell_current=5.)
 
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Attributes

avionics
 
voltage
 
- Public Attributes inherited from SUAVE.Components.Energy.Networks.Network.Network
tag
 
generative_design_max_per_vehicle
 
non_dimensional_origin
 
number_of_engines
 
engine_length
 
wing_mounted
 
areas
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 
+

Detailed Description

+
This is a test bench to analyze the discharge and charge profile 
+    of a battery cell.
+
+    Assumptions:
+    None
+    
+    Source:
+    None
+

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Components.Energy.Networks.Battery_Cell_Cycler.Battery_Cell_Cycler.__defaults__ ( self)
+
+
This sets the default values for the network to function.
+    
+    Assumptions:
+    None
+    
+    Source:
+    N/A
+    
+    Inputs:
+    None
+    
+    Outputs:
+    None
+    
+    Properties Used:
+    N/A
+
+

Reimplemented from SUAVE.Components.Energy.Networks.Network.Network.

+ +
+
+ +

◆ add_unknowns_and_residuals_to_segment()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Components.Energy.Networks.Battery_Cell_Cycler.Battery_Cell_Cycler.add_unknowns_and_residuals_to_segment ( self,
 segment,
 initial_voltage = None,
 initial_battery_cell_temperature = 300,
 initial_battery_state_of_charge = 0.5,
 initial_battery_cell_current = 5. 
)
+
+
This function sets up the information that the mission needs to run a mission segment using this network
+    
+    Assumptions:
+    None
+    
+    Source:
+    N/A
+    
+    Inputs:  
+    initial_voltage                       [volts]
+    initial_battery_cell_temperature      [Kelvin]
+    initial_battery_state_of_charge       [unitless]
+    initial_battery_cell_current          [Amperes]
+    
+    Outputs
+    None
+    
+    Properties Used:
+    N/A
+
+
+
+ +

◆ evaluate_thrust()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Components.Energy.Networks.Battery_Cell_Cycler.Battery_Cell_Cycler.evaluate_thrust ( self,
 state 
)
+
+
Evaluate the state variables of a cycled cell
+    
+    Assumptions: 
+    None
+    
+    Source:
+    N/A
+    
+    Inputs:
+    state [state()]
+    
+    Outputs: 
+    conditions.propulsion: 
+current                       [amps]
+battery_power_draw            [watts]
+battery_energy                [joules]
+battery_voltage_open_circuit  [volts]
+battery_voltage_under_load    [volts]  
+    
+    Properties Used:
+    Defaulted values
+
+
+
+ +

◆ residuals()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Components.Energy.Networks.Battery_Cell_Cycler.Battery_Cell_Cycler.residuals ( self,
 segment 
)
+
+
This packs the residuals to be sent to the mission solver.
+    
+    Assumptions:
+    None
+    
+    Source:
+    N/A
+    
+    Inputs:
+    unknowns specific to the battery cell 
+    
+    Outputs:
+    residuals specific to the battery cell
+    
+    Properties Used: 
+    N/A
+
+
+
+ +

◆ unpack_unknowns()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Components.Energy.Networks.Battery_Cell_Cycler.Battery_Cell_Cycler.unpack_unknowns ( self,
 segment 
)
+
+
This is an extra set of unknowns which are unpacked from the mission solver and send to the network.
+    
+    Assumptions:
+    None
+    
+    Source:
+    N/A
+    
+    Inputs:
+    unknowns specific to the battery cell 
+    
+    Outputs: 
+    conditions specific to the battery cell
+     
+    Properties Used:
+    N/A
+
+
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Energy/Networks/Battery_Cell_Cycler.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Cell__Cycler_1_1Battery__Cell__Cycler.js b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Cell__Cycler_1_1Battery__Cell__Cycler.js new file mode 100644 index 00000000..cbffa441 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Cell__Cycler_1_1Battery__Cell__Cycler.js @@ -0,0 +1,10 @@ +var classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Cell__Cycler_1_1Battery__Cell__Cycler = +[ + [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Cell__Cycler_1_1Battery__Cell__Cycler.html#a7c9c3b7f0fcf15f87f2e42e73893c8bf", null ], + [ "add_unknowns_and_residuals_to_segment", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Cell__Cycler_1_1Battery__Cell__Cycler.html#a7043137f2891614c3f8c72d1f2882b9d", null ], + [ "evaluate_thrust", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Cell__Cycler_1_1Battery__Cell__Cycler.html#ad8fd3edb6f264a7c2c69c44552c9e802", null ], + [ "residuals", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Cell__Cycler_1_1Battery__Cell__Cycler.html#a4e54c83e0afb869fe8b7096bc529e3c1", null ], + [ "unpack_unknowns", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Cell__Cycler_1_1Battery__Cell__Cycler.html#ae7512d6bcc2f54591569907d2e89f51b", null ], + [ "avionics", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Cell__Cycler_1_1Battery__Cell__Cycler.html#a19f7c2dd218ea9a4980628afb0229ba3", null ], + [ "voltage", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Cell__Cycler_1_1Battery__Cell__Cycler.html#ab800f4126b911222c9197fabd877b49f", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Cell__Cycler_1_1Battery__Cell__Cycler.png b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Cell__Cycler_1_1Battery__Cell__Cycler.png new file mode 100644 index 00000000..a1808c00 Binary files /dev/null and b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Cell__Cycler_1_1Battery__Cell__Cycler.png differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Ducted__Fan_1_1Battery__Ducted__Fan-members.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Ducted__Fan_1_1Battery__Ducted__Fan-members.html index 5c541e1e..ed92cdbb 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Ducted__Fan_1_1Battery__Ducted__Fan-members.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Ducted__Fan_1_1Battery__Ducted__Fan-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -99,14 +106,27 @@

This is the complete list of members for SUAVE.Components.Energy.Networks.Battery_Ducted_Fan.Battery_Ducted_Fan, including all inherited members.

+ + + + + + + + + + - - - + + + + + +
__defaults__(self)SUAVE.Components.Energy.Networks.Battery_Ducted_Fan.Battery_Ducted_Fan
areas (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
avionics (defined in SUAVE.Components.Energy.Networks.Battery_Ducted_Fan.Battery_Ducted_Fan)SUAVE.Components.Energy.Networks.Battery_Ducted_Fan.Battery_Ducted_Fan
battery (defined in SUAVE.Components.Energy.Networks.Battery_Ducted_Fan.Battery_Ducted_Fan)SUAVE.Components.Energy.Networks.Battery_Ducted_Fan.Battery_Ducted_Fan
engine_length (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
esc (defined in SUAVE.Components.Energy.Networks.Battery_Ducted_Fan.Battery_Ducted_Fan)SUAVE.Components.Energy.Networks.Battery_Ducted_Fan.Battery_Ducted_Fan
evaluate_thrust(self, state)SUAVE.Components.Energy.Networks.Battery_Ducted_Fan.Battery_Ducted_Fan
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
generative_design_minimum (defined in SUAVE.Components.Energy.Networks.Battery_Ducted_Fan.Battery_Ducted_Fan)SUAVE.Components.Energy.Networks.Battery_Ducted_Fan.Battery_Ducted_Fan
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
motor_efficiency (defined in SUAVE.Components.Energy.Networks.Battery_Ducted_Fan.Battery_Ducted_Fan)SUAVE.Components.Energy.Networks.Battery_Ducted_Fan.Battery_Ducted_Fan
non_dimensional_origin (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
number_of_engines (defined in SUAVE.Components.Energy.Networks.Battery_Ducted_Fan.Battery_Ducted_Fan)SUAVE.Components.Energy.Networks.Battery_Ducted_Fan.Battery_Ducted_Fan
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
propulsor (defined in SUAVE.Components.Energy.Networks.Battery_Ducted_Fan.Battery_Ducted_Fan)SUAVE.Components.Energy.Networks.Battery_Ducted_Fan.Battery_Ducted_Fan
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Energy.Networks.Battery_Ducted_Fan.Battery_Ducted_Fan)SUAVE.Components.Energy.Networks.Battery_Ducted_Fan.Battery_Ducted_Fan
payload (defined in SUAVE.Components.Energy.Networks.Battery_Ducted_Fan.Battery_Ducted_Fan)SUAVE.Components.Energy.Networks.Battery_Ducted_Fan.Battery_Ducted_Fan
propulsor (defined in SUAVE.Components.Energy.Networks.Battery_Ducted_Fan.Battery_Ducted_Fan)SUAVE.Components.Energy.Networks.Battery_Ducted_Fan.Battery_Ducted_Fan
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Energy.Networks.Battery_Ducted_Fan.Battery_Ducted_Fan)SUAVE.Components.Energy.Networks.Battery_Ducted_Fan.Battery_Ducted_Fan
voltage (defined in SUAVE.Components.Energy.Networks.Battery_Ducted_Fan.Battery_Ducted_Fan)SUAVE.Components.Energy.Networks.Battery_Ducted_Fan.Battery_Ducted_Fan
wing_mounted (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
@@ -114,7 +134,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Ducted__Fan_1_1Battery__Ducted__Fan.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Ducted__Fan_1_1Battery__Ducted__Fan.html index 76cfb2a4..17242d8a 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Ducted__Fan_1_1Battery__Ducted__Fan.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Ducted__Fan_1_1Battery__Ducted__Fan.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Components.Energy.Networks.Battery_Ducted_Fan.Battery_Ducted_Fan Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -105,11 +112,11 @@
-SUAVE.Components.Propulsors.Propulsor.Propulsor +SUAVE.Components.Energy.Networks.Network.Network SUAVE.Components.Physical_Component.Physical_Component SUAVE.Components.Component.Component - -
+ + @@ -117,15 +124,6 @@ - - - - - - - - -

Public Member Functions

 
def evaluate_thrust (self, state)
 
- Public Member Functions inherited from SUAVE.Components.Propulsors.Propulsor.Propulsor
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
@@ -141,10 +139,46 @@ - - + + + + + + + + + + + + + - + + + + + + + + + + + + + @@ -165,6 +199,15 @@ + + + + + +

Public Attributes

 tag
 
- Public Attributes inherited from SUAVE.Components.Propulsors.Propulsor.Propulsor
+
number_of_engines
 
esc
 
avionics
 
payload
 
voltage
 
generative_design_minimum
 
- Public Attributes inherited from SUAVE.Components.Energy.Networks.Network.Network
 tag
 
 
generative_design_max_per_vehicle
 
non_dimensional_origin
 
number_of_engines
 
engine_length
 
wing_mounted
 
areas
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
 tag
 origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 

Detailed Description

Simply connects a battery to a ducted fan, with an assumed motor efficiency
@@ -194,7 +237,7 @@ 

SUAVE.Components.Energy.Networks.Network.Network.

+

@@ -238,7 +283,9 @@

Calculate thrust given the current state of the vehicle Assumptions: - None + Constant mass batteries + ESC input voltage is constant at max battery voltage + Source: N/A @@ -266,7 +313,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Ducted__Fan_1_1Battery__Ducted__Fan.js b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Ducted__Fan_1_1Battery__Ducted__Fan.js index bdd45ca3..f6d99cce 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Ducted__Fan_1_1Battery__Ducted__Fan.js +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Ducted__Fan_1_1Battery__Ducted__Fan.js @@ -2,8 +2,14 @@ var classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Ducted__Fan_1_1Ba [ [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Ducted__Fan_1_1Battery__Ducted__Fan.html#a25ca87a711e6e06670a7d5c5a24aefd3", null ], [ "evaluate_thrust", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Ducted__Fan_1_1Battery__Ducted__Fan.html#a3c59ba5cb308705cc000fd5e28f60037", null ], + [ "avionics", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Ducted__Fan_1_1Battery__Ducted__Fan.html#a487dc42a6fc2491e18e4a6af02ddf5e3", null ], [ "battery", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Ducted__Fan_1_1Battery__Ducted__Fan.html#aa221541e0cf9cdeb125438cb052a0814", null ], + [ "esc", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Ducted__Fan_1_1Battery__Ducted__Fan.html#a6bc6d43e375bf1544c75f7d35b95af7d", null ], + [ "generative_design_minimum", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Ducted__Fan_1_1Battery__Ducted__Fan.html#ae95a033488f877f84c48a2eaaaaa04fc", null ], [ "motor_efficiency", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Ducted__Fan_1_1Battery__Ducted__Fan.html#a66b405209d8c43afa01255f145b427df", null ], + [ "number_of_engines", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Ducted__Fan_1_1Battery__Ducted__Fan.html#ad6209973f62e6f50204d12089106fa99", null ], + [ "payload", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Ducted__Fan_1_1Battery__Ducted__Fan.html#af329fb2a3193c818435d915991142a3f", null ], [ "propulsor", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Ducted__Fan_1_1Battery__Ducted__Fan.html#a122cf7faaa300ac90724b4bad1be7c98", null ], - [ "tag", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Ducted__Fan_1_1Battery__Ducted__Fan.html#ac60dafe42beba94bd1f313c2a329ad3d", null ] + [ "tag", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Ducted__Fan_1_1Battery__Ducted__Fan.html#ac60dafe42beba94bd1f313c2a329ad3d", null ], + [ "voltage", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Ducted__Fan_1_1Battery__Ducted__Fan.html#a07b78e5f04f05ad9b16704fdf6acd0b2", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Ducted__Fan_1_1Battery__Ducted__Fan.png b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Ducted__Fan_1_1Battery__Ducted__Fan.png index b5ad1180..97418c54 100644 Binary files a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Ducted__Fan_1_1Battery__Ducted__Fan.png and b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Ducted__Fan_1_1Battery__Ducted__Fan.png differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Propeller_1_1Battery__Propeller-members.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Propeller_1_1Battery__Propeller-members.html index da61be9d..0d7ff0b1 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Propeller_1_1Battery__Propeller-members.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Propeller_1_1Battery__Propeller-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -99,24 +106,38 @@

This is the complete list of members for SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller, including all inherited members.

+ + + + + + + + + + - - - + + + + + - - - - - - - + + + + + + + + +
__defaults__(self)SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller
add_unknowns_and_residuals_to_segment(self, segment, initial_voltage=None, initial_power_coefficient=0.02, initial_battery_cell_temperature=283., initial_battery_state_of_charge=0.5, initial_battery_cell_current=5.)SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller
areas (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
avionics (defined in SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller)SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller
battery (defined in SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller)SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller
engine_length (defined in SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller)SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller
esc (defined in SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller)SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller
evaluate_thrust(self, state)SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
generative_design_minimum (defined in SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller)SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
identical_lift_rotors (defined in SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller)SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller
identical_propellers (defined in SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller)SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller
lift_rotor_motors (defined in SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller)SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller
lift_rotors (defined in SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller)SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
motor (defined in SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller)SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller
nacelle_diameter (defined in SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller)SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller
number_of_engines (defined in SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller)SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller
nacelle_diameter (defined in SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller)SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller
non_dimensional_origin (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
number_of_engines (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
number_of_lift_rotor_engines (defined in SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller)SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller
number_of_propeller_engines (defined in SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller)SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
payload (defined in SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller)SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller
propeller (defined in SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller)SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller
residuals(self, segment, state)SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller)SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller
thrust_angle (defined in SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller)SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller
unpack_unknowns(self, segment, state)SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller
voltage (defined in SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller)SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller
propeller_motors (defined in SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller)SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller
propellers (defined in SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller)SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller
residuals(self, segment)SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller)SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller
unpack_unknowns(self, segment)SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller
use_surrogate (defined in SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller)SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller
voltage (defined in SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller)SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller
wing_mounted (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
@@ -124,7 +145,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Propeller_1_1Battery__Propeller.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Propeller_1_1Battery__Propeller.html index 2be8b25b..2befd089 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Propeller_1_1Battery__Propeller.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Battery__Propeller_1_1Battery__Propeller.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -105,11 +112,11 @@
-SUAVE.Components.Propulsors.Propulsor.Propulsor +SUAVE.Components.Energy.Networks.Network.Network SUAVE.Components.Physical_Component.Physical_Component SUAVE.Components.Component.Component - -
+ + @@ -117,28 +124,27 @@ - - - - - - - - - - - - - + + + + + +

Public Member Functions

 
def evaluate_thrust (self, state)
 
def unpack_unknowns (self, segment, state)
 
def residuals (self, segment, state)
 
- Public Member Functions inherited from SUAVE.Components.Propulsors.Propulsor.Propulsor
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
def unpack_unknowns (self, segment)
 
def residuals (self, segment)
 
def add_unknowns_and_residuals_to_segment (self, segment, initial_voltage=None, initial_power_coefficient=0.02, initial_battery_cell_temperature=283., initial_battery_state_of_charge=0.5, initial_battery_cell_current=5.)
 
- - - - + + + + + + + + @@ -157,22 +163,52 @@ - - + + + + - - - - + + + + + + + + + - + + + + + + + + + + + + + @@ -193,6 +229,15 @@ + + + + + +

Public Attributes

motor
 
propeller
 
propeller_motors
 
lift_rotor_motors
 
propellers
 
lift_rotors
 
 esc
 
 engine_length
 
number_of_engines
 
number_of_propeller_engines
 
number_of_lift_rotor_engines
 
 voltage
 
thrust_angle
 
 tag
 
- Public Attributes inherited from SUAVE.Components.Propulsors.Propulsor.Propulsor
+
use_surrogate
 
generative_design_minimum
 
identical_propellers
 
identical_lift_rotors
 
- Public Attributes inherited from SUAVE.Components.Energy.Networks.Network.Network
 tag
 
 
generative_design_max_per_vehicle
 
non_dimensional_origin
 
number_of_engines
 
engine_length
 
wing_mounted
 
areas
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
 tag
 origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 

Detailed Description

This is a simple network with a battery powering a propeller through
@@ -203,7 +248,7 @@
     The second is torque matching between motor and propeller.
 
     Assumptions:
-    None
+    The y axis rotation is used for rotating the propeller about the Y-axis for tilt rotors and tiltwings
     
     Source:
     None
@@ -240,16 +285,18 @@ 

SUAVE.Components.Energy.Networks.Network.Network.

+

- -

◆ evaluate_thrust()

+ +

◆ add_unknowns_and_residuals_to_segment()

- + @@ -258,7 +305,37 @@

- + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + @@ -267,53 +344,42 @@

-
Calculate thrust given the current state of the vehicle
+
This function sets up the information that the mission needs to run a mission segment using this network
     
     Assumptions:
-    Caps the throttle at 110% and linearly interpolates thrust off that
+    None
     
     Source:
     N/A
     
     Inputs:
-    state [state()]
+    segment
+    initial_voltage                   [v]
+    initial_power_coefficient         [float]s
     
     Outputs:
-    results.thrust_force_vector [newtons]
-    results.vehicle_mass_rate   [kg/s]
-    conditions.propulsion:
-rpm                  [radians/sec]
-current              [amps]
-battery_draw         [watts]
-battery_energy       [joules]
-voltage_open_circuit [volts]
-voltage_under_load   [volts]
-motor_torque         [N-M]
-propeller_torque     [N-M]
+    segment.state.unknowns.battery_voltage_under_load
+    segment.state.unknowns.propeller_power_coefficient
+    segment.state.conditions.propulsion.propeller_motor_torque
+    segment.state.conditions.propulsion.propeller_torque   
     
     Properties Used:
-    Defaulted values
+    N/A
 
-
-

◆ residuals()

+ +

◆ evaluate_thrust()

def SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller.evaluate_thrust def SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller.add_unknowns_and_residuals_to_segment (   self,  state segment,
 initial_voltage = None,
 initial_power_coefficient = 0.02,
 initial_battery_cell_temperature = 283.,
 initial_battery_state_of_charge = 0.5,
 initial_battery_cell_current = 5. 
- + - - - - - - @@ -327,37 +393,43 @@

-
This packs the residuals to be send to the mission solver.
+
Calculate thrust given the current state of the vehicle
     
     Assumptions:
-    None
+    Caps the throttle at 110% and linearly interpolates thrust off that
     
     Source:
     N/A
     
     Inputs:
-    state.conditions.propulsion:
-motor_torque                          [N-m]
-propeller_torque                      [N-m]
-voltage_under_load                    [volts]
-    state.unknowns.battery_voltage_under_load [volts]
+    state [state()]
     
     Outputs:
-    None
+    results.thrust_force_vector [newtons]
+    results.vehicle_mass_rate   [kg/s]
+    conditions.propulsion:
+rpm                          [radians/sec]
+current                      [amps]
+battery_power_draw           [watts]
+battery_energy               [joules]
+battery_voltage_open_circuit [V]
+battery_voltage_under_load   [V]
+motor_torque                 [N-M]
+propeller_torque             [N-M]
     
     Properties Used:
-    self.voltage                              [volts]
+    Defaulted values
 
-
-

◆ unpack_unknowns()

+ +

◆ residuals()

def SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller.residuals def SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller.evaluate_thrust (   self,
 segment,
- + @@ -366,13 +438,53 @@

- + + + + + + + +
def SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller.unpack_unknowns def SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller.residuals (   self,  segment, segment 
)
+
+
+ +

◆ unpack_unknowns()

+ +
+
+ + + + + + - + @@ -390,12 +502,12 @@

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- - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
-

def SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller.unpack_unknowns ( self,
 state segment 
- - - - - - - -
-
SUAVE -  1.1.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Energy.Networks.Dual_Battery_Ducted_Fan.Dual_Battery_Ducted_Fan Member List
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- -

This is the complete list of members for SUAVE.Components.Energy.Networks.Dual_Battery_Ducted_Fan.Dual_Battery_Ducted_Fan, including all inherited members.

- - - - - - - - - - - -
__defaults__(self)SUAVE.Components.Energy.Networks.Dual_Battery_Ducted_Fan.Dual_Battery_Ducted_Fan
auxiliary_battery (defined in SUAVE.Components.Energy.Networks.Dual_Battery_Ducted_Fan.Dual_Battery_Ducted_Fan)SUAVE.Components.Energy.Networks.Dual_Battery_Ducted_Fan.Dual_Battery_Ducted_Fan
evaluate_thrust(self, state)SUAVE.Components.Energy.Networks.Dual_Battery_Ducted_Fan.Dual_Battery_Ducted_Fan
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
motor_efficiency (defined in SUAVE.Components.Energy.Networks.Dual_Battery_Ducted_Fan.Dual_Battery_Ducted_Fan)SUAVE.Components.Energy.Networks.Dual_Battery_Ducted_Fan.Dual_Battery_Ducted_Fan
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
primary_battery (defined in SUAVE.Components.Energy.Networks.Dual_Battery_Ducted_Fan.Dual_Battery_Ducted_Fan)SUAVE.Components.Energy.Networks.Dual_Battery_Ducted_Fan.Dual_Battery_Ducted_Fan
propulsor (defined in SUAVE.Components.Energy.Networks.Dual_Battery_Ducted_Fan.Dual_Battery_Ducted_Fan)SUAVE.Components.Energy.Networks.Dual_Battery_Ducted_Fan.Dual_Battery_Ducted_Fan
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Energy.Networks.Dual_Battery_Ducted_Fan.Dual_Battery_Ducted_Fan)SUAVE.Components.Energy.Networks.Dual_Battery_Ducted_Fan.Dual_Battery_Ducted_Fan
-
- - - - diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Dual__Battery__Ducted__Fan_1_1Dual__Battery__Ducted__Fan.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Dual__Battery__Ducted__Fan_1_1Dual__Battery__Ducted__Fan.html deleted file mode 100644 index 31efedfa..00000000 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Dual__Battery__Ducted__Fan_1_1Dual__Battery__Ducted__Fan.html +++ /dev/null @@ -1,279 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Components.Energy.Networks.Dual_Battery_Ducted_Fan.Dual_Battery_Ducted_Fan Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.1.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Energy.Networks.Dual_Battery_Ducted_Fan.Dual_Battery_Ducted_Fan Class Reference
-
-
-
-Inheritance diagram for SUAVE.Components.Energy.Networks.Dual_Battery_Ducted_Fan.Dual_Battery_Ducted_Fan:
-
-
- - -SUAVE.Components.Propulsors.Propulsor.Propulsor -SUAVE.Components.Physical_Component.Physical_Component -SUAVE.Components.Component.Component - -
- - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def evaluate_thrust (self, state)
 
- Public Member Functions inherited from SUAVE.Components.Propulsors.Propulsor.Propulsor
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

propulsor
 
primary_battery
 
auxiliary_battery
 
motor_efficiency
 
tag
 
- Public Attributes inherited from SUAVE.Components.Propulsors.Propulsor.Propulsor
tag
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
-

Detailed Description

-
Uses two batteries to run a motor connected to a ducted fan; 
-    
-    Assumptions:
-    The primary_battery always runs, while the auxiliary_battery meets additional power needs
-    
-    Source:
-    None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Components.Energy.Networks.Dual_Battery_Ducted_Fan.Dual_Battery_Ducted_Fan.__defaults__ ( self)
-
-
This sets the default values for the network to function.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    N/A
-
-
-
- -

◆ evaluate_thrust()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Components.Energy.Networks.Dual_Battery_Ducted_Fan.Dual_Battery_Ducted_Fan.evaluate_thrust ( self,
 state 
)
-
-
Calculate thrust given the current state of the vehicle
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    state [state()]
-    
-    Outputs:
-    results.thrust_force_vector [newtons]
-    results.vehicle_mass_rate   [kg/s]
-    conditions.propulsion.primary_battery_draw     [watts]
-    conditions.propulsion.primary_battery_energy   [joules]
-    conditions.propulsion.auxiliary_battery_draw   [watts]
-    conditions.propulsion.auxiliary_battery_energy [joules]
-    
-    Properties Used:
-    Defaulted values
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Energy/Networks/Dual_Battery_Ducted_Fan.py
  • -
-
-
- - - - diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Dual__Battery__Ducted__Fan_1_1Dual__Battery__Ducted__Fan.js b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Dual__Battery__Ducted__Fan_1_1Dual__Battery__Ducted__Fan.js deleted file mode 100644 index ef19e9f3..00000000 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Dual__Battery__Ducted__Fan_1_1Dual__Battery__Ducted__Fan.js +++ /dev/null @@ -1,10 +0,0 @@ -var classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Dual__Battery__Ducted__Fan_1_1Dual__Battery__Ducted__Fan = -[ - [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Dual__Battery__Ducted__Fan_1_1Dual__Battery__Ducted__Fan.html#a5dc648add76242495190b22734c71bf3", null ], - [ "evaluate_thrust", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Dual__Battery__Ducted__Fan_1_1Dual__Battery__Ducted__Fan.html#a59f813bcd082fc977fb78b763900d879", null ], - [ "auxiliary_battery", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Dual__Battery__Ducted__Fan_1_1Dual__Battery__Ducted__Fan.html#a56345ec136a6f3101e9db068808c4a9e", null ], - [ "motor_efficiency", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Dual__Battery__Ducted__Fan_1_1Dual__Battery__Ducted__Fan.html#a5a55a6d5baf29750c2895d02467c70bf", null ], - [ "primary_battery", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Dual__Battery__Ducted__Fan_1_1Dual__Battery__Ducted__Fan.html#ac6cd6c3aa3b891ada7427eb13651290c", null ], - [ "propulsor", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Dual__Battery__Ducted__Fan_1_1Dual__Battery__Ducted__Fan.html#ad93c950b7882159dc4b0222af2a74d9e", null ], - [ "tag", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Dual__Battery__Ducted__Fan_1_1Dual__Battery__Ducted__Fan.html#a8eed85d5755d8c8f16a8a13609bad30d", null ] -]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Dual__Battery__Ducted__Fan_1_1Dual__Battery__Ducted__Fan.png b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Dual__Battery__Ducted__Fan_1_1Dual__Battery__Ducted__Fan.png deleted file mode 100644 index 0a1dd42b..00000000 Binary files a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Dual__Battery__Ducted__Fan_1_1Dual__Battery__Ducted__Fan.png and /dev/null differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ducted__Fan_1_1Ducted__Fan-members.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ducted__Fan_1_1Ducted__Fan-members.html index 1452ff11..35d58058 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ducted__Fan_1_1Ducted__Fan-members.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ducted__Fan_1_1Ducted__Fan-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -103,13 +110,17 @@ bypass_ratio (defined in SUAVE.Components.Energy.Networks.Ducted_Fan.Ducted_Fan)SUAVE.Components.Energy.Networks.Ducted_Fan.Ducted_Fan engine_length (defined in SUAVE.Components.Energy.Networks.Ducted_Fan.Ducted_Fan)SUAVE.Components.Energy.Networks.Ducted_Fan.Ducted_Fan evaluate_thrust(self, state)SUAVE.Components.Energy.Networks.Ducted_Fan.Ducted_Fan - mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component - nacelle_diameter (defined in SUAVE.Components.Energy.Networks.Ducted_Fan.Ducted_Fan)SUAVE.Components.Energy.Networks.Ducted_Fan.Ducted_Fan - number_of_engines (defined in SUAVE.Components.Energy.Networks.Ducted_Fan.Ducted_Fan)SUAVE.Components.Energy.Networks.Ducted_Fan.Ducted_Fan - origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component - size(self, state)SUAVE.Components.Energy.Networks.Ducted_Fan.Ducted_Fan - symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component - tag (defined in SUAVE.Components.Energy.Networks.Ducted_Fan.Ducted_Fan)SUAVE.Components.Energy.Networks.Ducted_Fan.Ducted_Fan + generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component + generative_design_max_per_vehicle (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network + generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component + mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component + non_dimensional_origin (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network + number_of_engines (defined in SUAVE.Components.Energy.Networks.Ducted_Fan.Ducted_Fan)SUAVE.Components.Energy.Networks.Ducted_Fan.Ducted_Fan + origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component + size(self, state)SUAVE.Components.Energy.Networks.Ducted_Fan.Ducted_Fan + symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component + tag (defined in SUAVE.Components.Energy.Networks.Ducted_Fan.Ducted_Fan)SUAVE.Components.Energy.Networks.Ducted_Fan.Ducted_Fan + wing_mounted (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
@@ -117,7 +128,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ducted__Fan_1_1Ducted__Fan.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ducted__Fan_1_1Ducted__Fan.html index 6b16e15f..cbe9b65c 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ducted__Fan_1_1Ducted__Fan.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ducted__Fan_1_1Ducted__Fan.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Components.Energy.Networks.Ducted_Fan.Ducted_Fan Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -105,11 +112,11 @@
-SUAVE.Components.Propulsors.Propulsor.Propulsor +SUAVE.Components.Energy.Networks.Network.Network SUAVE.Components.Physical_Component.Physical_Component SUAVE.Components.Component.Component - -
+ + @@ -119,15 +126,6 @@ - - - - - - - - -

Public Member Functions

 
def size (self, state)
 
- Public Member Functions inherited from SUAVE.Components.Propulsors.Propulsor.Propulsor
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
@@ -137,9 +135,6 @@ - - @@ -149,10 +144,28 @@ - - + - + + + + + + + + + + + + + @@ -173,6 +186,15 @@ + + + + + +

Public Attributes

 number_of_engines
 
nacelle_diameter
 
 engine_length
 
 areas
 
- Public Attributes inherited from SUAVE.Components.Propulsors.Propulsor.Propulsor
+
- Public Attributes inherited from SUAVE.Components.Energy.Networks.Network.Network
 tag
 
 
generative_design_max_per_vehicle
 
non_dimensional_origin
 
number_of_engines
 
engine_length
 
wing_mounted
 
areas
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
 tag
 origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 

Detailed Description

A ducted fan 
@@ -216,6 +238,8 @@ 

SUAVE.Components.Energy.Networks.Network.Network.

+

@@ -258,7 +282,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ducted__Fan_1_1Ducted__Fan.js b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ducted__Fan_1_1Ducted__Fan.js index 149b89d5..3e4a0623 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ducted__Fan_1_1Ducted__Fan.js +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ducted__Fan_1_1Ducted__Fan.js @@ -6,7 +6,6 @@ var classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ducted__Fan_1_1Ducted__Fan [ "areas", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ducted__Fan_1_1Ducted__Fan.html#ae22f76d8cb6aeb04454643964a43aae6", null ], [ "bypass_ratio", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ducted__Fan_1_1Ducted__Fan.html#aefa45fa7b6e4d57183e3b5788bf01d2f", null ], [ "engine_length", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ducted__Fan_1_1Ducted__Fan.html#ae557071255a5f36a43e0db676e4f3ba2", null ], - [ "nacelle_diameter", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ducted__Fan_1_1Ducted__Fan.html#a6e44da438a79f93ae981a68895043e74", null ], [ "number_of_engines", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ducted__Fan_1_1Ducted__Fan.html#ae845b8ec30319de8b8ced55dfa4694e8", null ], [ "tag", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ducted__Fan_1_1Ducted__Fan.html#a8909a2f8395ae333ce6080a57c69d3d0", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ducted__Fan_1_1Ducted__Fan.png b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ducted__Fan_1_1Ducted__Fan.png index 87bc30c3..c5aa7948 100644 Binary files a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ducted__Fan_1_1Ducted__Fan.png and b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ducted__Fan_1_1Ducted__Fan.png differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Internal__Combustion__Propeller_1_1Internal__Combustion__Propeller-members.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Internal__Combustion__Propeller_1_1Internal__Combustion__Propeller-members.html new file mode 100644 index 00000000..509e257e --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Internal__Combustion__Propeller_1_1Internal__Combustion__Propeller-members.html @@ -0,0 +1,139 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
SUAVE.Components.Energy.Networks.Internal_Combustion_Propeller.Internal_Combustion_Propeller Member List
+
+
+ +

This is the complete list of members for SUAVE.Components.Energy.Networks.Internal_Combustion_Propeller.Internal_Combustion_Propeller, including all inherited members.

+ + + + + + + + + + + + + + + + + + + + + +
__defaults__(self)SUAVE.Components.Energy.Networks.Internal_Combustion_Propeller.Internal_Combustion_Propeller
add_unknowns_and_residuals_to_segment(self, segment, rpm=2500)SUAVE.Components.Energy.Networks.Internal_Combustion_Propeller.Internal_Combustion_Propeller
areas (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
engine_length (defined in SUAVE.Components.Energy.Networks.Internal_Combustion_Propeller.Internal_Combustion_Propeller)SUAVE.Components.Energy.Networks.Internal_Combustion_Propeller.Internal_Combustion_Propeller
engines (defined in SUAVE.Components.Energy.Networks.Internal_Combustion_Propeller.Internal_Combustion_Propeller)SUAVE.Components.Energy.Networks.Internal_Combustion_Propeller.Internal_Combustion_Propeller
evaluate_thrust(self, state)SUAVE.Components.Energy.Networks.Internal_Combustion_Propeller.Internal_Combustion_Propeller
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
identical_propellers (defined in SUAVE.Components.Energy.Networks.Internal_Combustion_Propeller.Internal_Combustion_Propeller)SUAVE.Components.Energy.Networks.Internal_Combustion_Propeller.Internal_Combustion_Propeller
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
non_dimensional_origin (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
number_of_engines (defined in SUAVE.Components.Energy.Networks.Internal_Combustion_Propeller.Internal_Combustion_Propeller)SUAVE.Components.Energy.Networks.Internal_Combustion_Propeller.Internal_Combustion_Propeller
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
propellers (defined in SUAVE.Components.Energy.Networks.Internal_Combustion_Propeller.Internal_Combustion_Propeller)SUAVE.Components.Energy.Networks.Internal_Combustion_Propeller.Internal_Combustion_Propeller
residuals(self, segment)SUAVE.Components.Energy.Networks.Internal_Combustion_Propeller.Internal_Combustion_Propeller
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
unpack_unknowns(self, segment)SUAVE.Components.Energy.Networks.Internal_Combustion_Propeller.Internal_Combustion_Propeller
wing_mounted (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Internal__Combustion__Propeller_1_1Internal__Combustion__Propeller.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Internal__Combustion__Propeller_1_1Internal__Combustion__Propeller.html new file mode 100644 index 00000000..6300cb59 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Internal__Combustion__Propeller_1_1Internal__Combustion__Propeller.html @@ -0,0 +1,453 @@ + + + + + + + +SUAVE: SUAVE.Components.Energy.Networks.Internal_Combustion_Propeller.Internal_Combustion_Propeller Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Components.Energy.Networks.Internal_Combustion_Propeller.Internal_Combustion_Propeller Class Reference
+
+
+
+Inheritance diagram for SUAVE.Components.Energy.Networks.Internal_Combustion_Propeller.Internal_Combustion_Propeller:
+
+
+ + +SUAVE.Components.Energy.Networks.Network.Network +SUAVE.Components.Physical_Component.Physical_Component +SUAVE.Components.Component.Component + +
+ + + + + + + + + + + + +

+Public Member Functions

def __defaults__ (self)
 
def evaluate_thrust (self, state)
 
def unpack_unknowns (self, segment)
 
def residuals (self, segment)
 
def add_unknowns_and_residuals_to_segment (self, segment, rpm=2500)
 
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Attributes

engines
 
propellers
 
engine_length
 
number_of_engines
 
identical_propellers
 
- Public Attributes inherited from SUAVE.Components.Energy.Networks.Network.Network
tag
 
generative_design_max_per_vehicle
 
non_dimensional_origin
 
number_of_engines
 
engine_length
 
wing_mounted
 
areas
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 
+

Detailed Description

+
A simple mock up of an internal combustion propeller engine. Tis network adds an extra
+    unknowns to the mission, the torque matching between motor and propeller.
+
+    Assumptions:
+    None
+    
+    Source:
+    None
+

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Components.Energy.Networks.Internal_Combustion_Propeller.Internal_Combustion_Propeller.__defaults__ ( self)
+
+
This sets the default values for the network to function.
+    
+    Assumptions:
+    None
+    
+    Source:
+    N/A
+    
+    Inputs:
+    None
+    
+    Outputs:
+    None
+    
+    Properties Used:
+    N/A
+
+

Reimplemented from SUAVE.Components.Energy.Networks.Network.Network.

+ +
+
+ +

◆ add_unknowns_and_residuals_to_segment()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Components.Energy.Networks.Internal_Combustion_Propeller.Internal_Combustion_Propeller.add_unknowns_and_residuals_to_segment ( self,
 segment,
 rpm = 2500 
)
+
+
This function sets up the information that the mission needs to run a mission segment using this network
+    
+    Assumptions:
+    None
+    
+    Source:
+    N/A
+    
+    Inputs:
+    segment
+    rpm                      [rpm]
+    
+    Outputs:
+    segment.state.unknowns.battery_voltage_under_load
+    segment.state.unknowns.propeller_power_coefficient
+    segment.state.conditions.propulsion.propeller_motor_torque
+    segment.state.conditions.propulsion.propeller_torque   
+    
+    Properties Used:
+    N/A
+
+
+
+ +

◆ evaluate_thrust()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Components.Energy.Networks.Internal_Combustion_Propeller.Internal_Combustion_Propeller.evaluate_thrust ( self,
 state 
)
+
+
Calculate thrust given the current state of the vehicle
+    
+    Assumptions:
+    
+    Source:
+    N/A
+    
+    Inputs:
+    state [state()]
+    
+    Outputs:
+    results.thrust_force_vector [newtons]
+    results.vehicle_mass_rate   [kg/s]
+    conditions.propulsion:
+rpm                  [radians/sec]
+propeller_torque     [N-M]
+power                [W]
+    
+    Properties Used:
+    Defaulted values
+
+
+
+ +

◆ residuals()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Components.Energy.Networks.Internal_Combustion_Propeller.Internal_Combustion_Propeller.residuals ( self,
 segment 
)
+
+
Calculates a residual based on torques 
+
+Assumptions:
+
+Inputs:
+    segment.state.conditions.propulsion.
+motor_torque                       [newtom-meters]                 
+propeller_torque                   [newtom-meters] 
+
+Outputs:
+    segment.state:
+residuals.network                  [newtom-meters] 
+
+Properties Used:
+    N/A
+
+
+ +

◆ unpack_unknowns()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Components.Energy.Networks.Internal_Combustion_Propeller.Internal_Combustion_Propeller.unpack_unknowns ( self,
 segment 
)
+
+
Unpacks the unknowns set in the mission to be available for the mission.
+
+Assumptions:
+N/A
+
+Source:
+N/A
+
+Inputs:
+state.unknowns.rpm                 [RPM] 
+
+Outputs:
+state.conditions.propulsion.rpm    [RPM] 
+
+
+Properties Used:
+N/A
+
+
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Energy/Networks/Internal_Combustion_Propeller.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Internal__Combustion__Propeller_1_1Internal__Combustion__Propeller.js b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Internal__Combustion__Propeller_1_1Internal__Combustion__Propeller.js new file mode 100644 index 00000000..6d2a9b98 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Internal__Combustion__Propeller_1_1Internal__Combustion__Propeller.js @@ -0,0 +1,13 @@ +var classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Internal__Combustion__Propeller_1_1Internal__Combustion__Propeller = +[ + [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Internal__Combustion__Propeller_1_1Internal__Combustion__Propeller.html#ade379170c477b81a99faffc1a1dbce59", null ], + [ "add_unknowns_and_residuals_to_segment", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Internal__Combustion__Propeller_1_1Internal__Combustion__Propeller.html#a80a5c9069041ddb70309e5195c6bcbab", null ], + [ "evaluate_thrust", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Internal__Combustion__Propeller_1_1Internal__Combustion__Propeller.html#a5010124396c91a7bb51c6ac459ac9db7", null ], + [ "residuals", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Internal__Combustion__Propeller_1_1Internal__Combustion__Propeller.html#af0b1e5952a405e685ad8695efc33fea8", null ], + [ "unpack_unknowns", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Internal__Combustion__Propeller_1_1Internal__Combustion__Propeller.html#a060356683a1346134968da0202d1f7e9", null ], + [ "engine_length", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Internal__Combustion__Propeller_1_1Internal__Combustion__Propeller.html#ac17eb87b9a463383d1eb52b56be04658", null ], + [ "engines", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Internal__Combustion__Propeller_1_1Internal__Combustion__Propeller.html#ac2c3ddd888c9de91ba94695ea5444116", null ], + [ "identical_propellers", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Internal__Combustion__Propeller_1_1Internal__Combustion__Propeller.html#aeaa16dea888cc292e5143acce82f1e9f", null ], + [ "number_of_engines", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Internal__Combustion__Propeller_1_1Internal__Combustion__Propeller.html#ac707b3cfada31c18345c7fc741d2f8ae", null ], + [ "propellers", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Internal__Combustion__Propeller_1_1Internal__Combustion__Propeller.html#a1e9eaadf3b7f368f2882095a01bad379", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Internal__Combustion__Propeller_1_1Internal__Combustion__Propeller.png b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Internal__Combustion__Propeller_1_1Internal__Combustion__Propeller.png new file mode 100644 index 00000000..458b0e27 Binary files /dev/null and b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Internal__Combustion__Propeller_1_1Internal__Combustion__Propeller.png differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Internal__Combustion__Propeller__Constant__Specd61538c6e79cec95abc532ade107e43.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Internal__Combustion__Propeller__Constant__Specd61538c6e79cec95abc532ade107e43.html new file mode 100644 index 00000000..913531aa --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Internal__Combustion__Propeller__Constant__Specd61538c6e79cec95abc532ade107e43.html @@ -0,0 +1,137 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
SUAVE.Components.Energy.Networks.Internal_Combustion_Propeller_Constant_Speed.Internal_Combustion_Propeller_Constant_Speed Member List
+
+
+ +

This is the complete list of members for SUAVE.Components.Energy.Networks.Internal_Combustion_Propeller_Constant_Speed.Internal_Combustion_Propeller_Constant_Speed, including all inherited members.

+ + + + + + + + + + + + + + + + + + + +
__defaults__(self)SUAVE.Components.Energy.Networks.Internal_Combustion_Propeller_Constant_Speed.Internal_Combustion_Propeller_Constant_Speed
areas (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
engine_length (defined in SUAVE.Components.Energy.Networks.Internal_Combustion_Propeller_Constant_Speed.Internal_Combustion_Propeller_Constant_Speed)SUAVE.Components.Energy.Networks.Internal_Combustion_Propeller_Constant_Speed.Internal_Combustion_Propeller_Constant_Speed
engines (defined in SUAVE.Components.Energy.Networks.Internal_Combustion_Propeller_Constant_Speed.Internal_Combustion_Propeller_Constant_Speed)SUAVE.Components.Energy.Networks.Internal_Combustion_Propeller_Constant_Speed.Internal_Combustion_Propeller_Constant_Speed
evaluate_thrust(self, state)SUAVE.Components.Energy.Networks.Internal_Combustion_Propeller_Constant_Speed.Internal_Combustion_Propeller_Constant_Speed
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
identical_propellers (defined in SUAVE.Components.Energy.Networks.Internal_Combustion_Propeller_Constant_Speed.Internal_Combustion_Propeller_Constant_Speed)SUAVE.Components.Energy.Networks.Internal_Combustion_Propeller_Constant_Speed.Internal_Combustion_Propeller_Constant_Speed
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
non_dimensional_origin (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
number_of_engines (defined in SUAVE.Components.Energy.Networks.Internal_Combustion_Propeller_Constant_Speed.Internal_Combustion_Propeller_Constant_Speed)SUAVE.Components.Energy.Networks.Internal_Combustion_Propeller_Constant_Speed.Internal_Combustion_Propeller_Constant_Speed
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
propellers (defined in SUAVE.Components.Energy.Networks.Internal_Combustion_Propeller_Constant_Speed.Internal_Combustion_Propeller_Constant_Speed)SUAVE.Components.Energy.Networks.Internal_Combustion_Propeller_Constant_Speed.Internal_Combustion_Propeller_Constant_Speed
rated_speed (defined in SUAVE.Components.Energy.Networks.Internal_Combustion_Propeller_Constant_Speed.Internal_Combustion_Propeller_Constant_Speed)SUAVE.Components.Energy.Networks.Internal_Combustion_Propeller_Constant_Speed.Internal_Combustion_Propeller_Constant_Speed
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
wing_mounted (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Internal__Combustion__Propeller__Constant__Spefd0f47b019fa78b7cc3bc47b5f2c3d76.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Internal__Combustion__Propeller__Constant__Spefd0f47b019fa78b7cc3bc47b5f2c3d76.html new file mode 100644 index 00000000..a1e18944 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Internal__Combustion__Propeller__Constant__Spefd0f47b019fa78b7cc3bc47b5f2c3d76.html @@ -0,0 +1,308 @@ + + + + + + + +SUAVE: SUAVE.Components.Energy.Networks.Internal_Combustion_Propeller_Constant_Speed.Internal_Combustion_Propeller_Constant_Speed Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Components.Energy.Networks.Internal_Combustion_Propeller_Constant_Speed.Internal_Combustion_Propeller_Constant_Speed Class Reference
+
+
+
+Inheritance diagram for SUAVE.Components.Energy.Networks.Internal_Combustion_Propeller_Constant_Speed.Internal_Combustion_Propeller_Constant_Speed:
+
+
+ + +SUAVE.Components.Energy.Networks.Network.Network +SUAVE.Components.Physical_Component.Physical_Component +SUAVE.Components.Component.Component + +
+ + + + + + +

+Public Member Functions

def __defaults__ (self)
 
def evaluate_thrust (self, state)
 
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Attributes

engines
 
propellers
 
engine_length
 
number_of_engines
 
rated_speed
 
identical_propellers
 
- Public Attributes inherited from SUAVE.Components.Energy.Networks.Network.Network
tag
 
generative_design_max_per_vehicle
 
non_dimensional_origin
 
number_of_engines
 
engine_length
 
wing_mounted
 
areas
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 
+

Detailed Description

+
An internal combustion engine with a constant speed propeller.
+
+    Assumptions:
+    0.5 Throttle corresponds to 0 rotor pitch. Less than 0.5 throttle implies negative rotor pitch.
+    
+    Source:
+    None
+

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Components.Energy.Networks.Internal_Combustion_Propeller_Constant_Speed.Internal_Combustion_Propeller_Constant_Speed.__defaults__ ( self)
+
+
This sets the default values for the network to function.
+    
+    Assumptions:
+    None
+    
+    Source:
+    N/A
+    
+    Inputs:
+    None
+    
+    Outputs:
+    None
+    
+    Properties Used:
+    N/A
+
+

Reimplemented from SUAVE.Components.Energy.Networks.Network.Network.

+ +
+
+ +

◆ evaluate_thrust()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Components.Energy.Networks.Internal_Combustion_Propeller_Constant_Speed.Internal_Combustion_Propeller_Constant_Speed.evaluate_thrust ( self,
 state 
)
+
+
Calculate thrust given the current state of the vehicle
+    
+    Assumptions:
+    
+    Source:
+    N/A
+    
+    Inputs:
+    state [state()]
+    
+    Outputs:
+    results.thrust_force_vector [newtons]
+    results.vehicle_mass_rate   [kg/s]
+    conditions.propulsion:
+rpm                  [radians/sec]
+propeller_torque     [N-M]
+power                [W]
+    
+    Properties Used:
+    Defaulted values
+
+
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Energy/Networks/Internal_Combustion_Propeller_Constant_Speed.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Internal__Combustion__Propeller__Constant__Spefd0f47b019fa78b7cc3bc47b5f2c3d76.js b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Internal__Combustion__Propeller__Constant__Spefd0f47b019fa78b7cc3bc47b5f2c3d76.js new file mode 100644 index 00000000..6ffe68b8 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Internal__Combustion__Propeller__Constant__Spefd0f47b019fa78b7cc3bc47b5f2c3d76.js @@ -0,0 +1,11 @@ +var classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Internal__Combustion__Propeller__Constant__Spefd0f47b019fa78b7cc3bc47b5f2c3d76 = +[ + [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Internal__Combustion__Propeller__Constant__Spefd0f47b019fa78b7cc3bc47b5f2c3d76.html#a2a2b2213ef2a6209d93bfdd303ee0ec3", null ], + [ "evaluate_thrust", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Internal__Combustion__Propeller__Constant__Spefd0f47b019fa78b7cc3bc47b5f2c3d76.html#a8a99a0cb8a0b1b011245c26ef3141ce9", null ], + [ "engine_length", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Internal__Combustion__Propeller__Constant__Spefd0f47b019fa78b7cc3bc47b5f2c3d76.html#a6e93fea4e8629a4a86bc543ae68d51c5", null ], + [ "engines", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Internal__Combustion__Propeller__Constant__Spefd0f47b019fa78b7cc3bc47b5f2c3d76.html#adae0397484bf7f9acd5c81eba8cbb9b5", null ], + [ "identical_propellers", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Internal__Combustion__Propeller__Constant__Spefd0f47b019fa78b7cc3bc47b5f2c3d76.html#a48a37e77bd287c745f6f619cdd6f3f7f", null ], + [ "number_of_engines", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Internal__Combustion__Propeller__Constant__Spefd0f47b019fa78b7cc3bc47b5f2c3d76.html#a059983294b8be3d2f8e7067828ade149", null ], + [ "propellers", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Internal__Combustion__Propeller__Constant__Spefd0f47b019fa78b7cc3bc47b5f2c3d76.html#a264d51095123251c370ec27e46301b0d", null ], + [ "rated_speed", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Internal__Combustion__Propeller__Constant__Spefd0f47b019fa78b7cc3bc47b5f2c3d76.html#a3bb91d6b3b6c0fa3a1cfbb30f8dd8167", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Internal__Combustion__Propeller__Constant__Spefd0f47b019fa78b7cc3bc47b5f2c3d76.png b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Internal__Combustion__Propeller__Constant__Spefd0f47b019fa78b7cc3bc47b5f2c3d76.png new file mode 100644 index 00000000..19c54670 Binary files /dev/null and b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Internal__Combustion__Propeller__Constant__Spefd0f47b019fa78b7cc3bc47b5f2c3d76.png differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Lift__Cruise_1_1Lift__Cruise-members.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Lift__Cruise_1_1Lift__Cruise-members.html new file mode 100644 index 00000000..f3c381cd --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Lift__Cruise_1_1Lift__Cruise-members.html @@ -0,0 +1,159 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
SUAVE.Components.Energy.Networks.Lift_Cruise.Lift_Cruise Member List
+
+
+ +

This is the complete list of members for SUAVE.Components.Energy.Networks.Lift_Cruise.Lift_Cruise, including all inherited members.

+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
__defaults__(self)SUAVE.Components.Energy.Networks.Lift_Cruise.Lift_Cruise
add_cruise_unknowns_and_residuals_to_segment(self, segment, initial_voltage=None, initial_prop_power_coefficient=0.005, initial_battery_cell_temperature=283., initial_battery_state_of_charge=0.5, initial_battery_cell_current=5.)SUAVE.Components.Energy.Networks.Lift_Cruise.Lift_Cruise
add_lift_unknowns_and_residuals_to_segment(self, segment, initial_voltage=None, initial_lift_rotor_power_coefficient=0.005, initial_throttle_lift=0.9, initial_battery_cell_temperature=283., initial_battery_state_of_charge=0.5, initial_battery_cell_current=5.)SUAVE.Components.Energy.Networks.Lift_Cruise.Lift_Cruise
add_transition_unknowns_and_residuals_to_segment(self, segment, initial_voltage=None, initial_prop_power_coefficient=0.005, initial_lift_rotor_power_coefficient=0.005, initial_throttle_lift=0.9, initial_battery_cell_temperature=283., initial_battery_state_of_charge=0.5, initial_battery_cell_current=5.)SUAVE.Components.Energy.Networks.Lift_Cruise.Lift_Cruise
areas (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
avionics (defined in SUAVE.Components.Energy.Networks.Lift_Cruise.Lift_Cruise)SUAVE.Components.Energy.Networks.Lift_Cruise.Lift_Cruise
battery (defined in SUAVE.Components.Energy.Networks.Lift_Cruise.Lift_Cruise)SUAVE.Components.Energy.Networks.Lift_Cruise.Lift_Cruise
engine_length (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
evaluate_thrust(self, state)SUAVE.Components.Energy.Networks.Lift_Cruise.Lift_Cruise
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
generative_design_minimum (defined in SUAVE.Components.Energy.Networks.Lift_Cruise.Lift_Cruise)SUAVE.Components.Energy.Networks.Lift_Cruise.Lift_Cruise
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
identical_lift_rotors (defined in SUAVE.Components.Energy.Networks.Lift_Cruise.Lift_Cruise)SUAVE.Components.Energy.Networks.Lift_Cruise.Lift_Cruise
identical_propellers (defined in SUAVE.Components.Energy.Networks.Lift_Cruise.Lift_Cruise)SUAVE.Components.Energy.Networks.Lift_Cruise.Lift_Cruise
lift_rotor_engine_length (defined in SUAVE.Components.Energy.Networks.Lift_Cruise.Lift_Cruise)SUAVE.Components.Energy.Networks.Lift_Cruise.Lift_Cruise
lift_rotor_esc (defined in SUAVE.Components.Energy.Networks.Lift_Cruise.Lift_Cruise)SUAVE.Components.Energy.Networks.Lift_Cruise.Lift_Cruise
lift_rotor_motors (defined in SUAVE.Components.Energy.Networks.Lift_Cruise.Lift_Cruise)SUAVE.Components.Energy.Networks.Lift_Cruise.Lift_Cruise
lift_rotors (defined in SUAVE.Components.Energy.Networks.Lift_Cruise.Lift_Cruise)SUAVE.Components.Energy.Networks.Lift_Cruise.Lift_Cruise
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
non_dimensional_origin (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
number_of_engines (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
number_of_lift_rotor_engines (defined in SUAVE.Components.Energy.Networks.Lift_Cruise.Lift_Cruise)SUAVE.Components.Energy.Networks.Lift_Cruise.Lift_Cruise
number_of_propeller_engines (defined in SUAVE.Components.Energy.Networks.Lift_Cruise.Lift_Cruise)SUAVE.Components.Energy.Networks.Lift_Cruise.Lift_Cruise
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
payload (defined in SUAVE.Components.Energy.Networks.Lift_Cruise.Lift_Cruise)SUAVE.Components.Energy.Networks.Lift_Cruise.Lift_Cruise
propeller_engine_length (defined in SUAVE.Components.Energy.Networks.Lift_Cruise.Lift_Cruise)SUAVE.Components.Energy.Networks.Lift_Cruise.Lift_Cruise
propeller_esc (defined in SUAVE.Components.Energy.Networks.Lift_Cruise.Lift_Cruise)SUAVE.Components.Energy.Networks.Lift_Cruise.Lift_Cruise
propeller_motors (defined in SUAVE.Components.Energy.Networks.Lift_Cruise.Lift_Cruise)SUAVE.Components.Energy.Networks.Lift_Cruise.Lift_Cruise
propellers (defined in SUAVE.Components.Energy.Networks.Lift_Cruise.Lift_Cruise)SUAVE.Components.Energy.Networks.Lift_Cruise.Lift_Cruise
residuals_cruise(self, segment)SUAVE.Components.Energy.Networks.Lift_Cruise.Lift_Cruise
residuals_lift(self, segment)SUAVE.Components.Energy.Networks.Lift_Cruise.Lift_Cruise
residuals_transition(self, segment)SUAVE.Components.Energy.Networks.Lift_Cruise.Lift_Cruise
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Energy.Networks.Lift_Cruise.Lift_Cruise)SUAVE.Components.Energy.Networks.Lift_Cruise.Lift_Cruise
unpack_unknowns_cruise(self, segment)SUAVE.Components.Energy.Networks.Lift_Cruise.Lift_Cruise
unpack_unknowns_lift(self, segment)SUAVE.Components.Energy.Networks.Lift_Cruise.Lift_Cruise
unpack_unknowns_transition(self, segment)SUAVE.Components.Energy.Networks.Lift_Cruise.Lift_Cruise
voltage (defined in SUAVE.Components.Energy.Networks.Lift_Cruise.Lift_Cruise)SUAVE.Components.Energy.Networks.Lift_Cruise.Lift_Cruise
wing_mounted (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Lift__Cruise_1_1Lift__Cruise.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Lift__Cruise_1_1Lift__Cruise.html new file mode 100644 index 00000000..e43cc0ad --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Lift__Cruise_1_1Lift__Cruise.html @@ -0,0 +1,947 @@ + + + + + + + +SUAVE: SUAVE.Components.Energy.Networks.Lift_Cruise.Lift_Cruise Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Components.Energy.Networks.Lift_Cruise.Lift_Cruise Class Reference
+
+
+
+Inheritance diagram for SUAVE.Components.Energy.Networks.Lift_Cruise.Lift_Cruise:
+
+
+ + +SUAVE.Components.Energy.Networks.Network.Network +SUAVE.Components.Physical_Component.Physical_Component +SUAVE.Components.Component.Component + +
+ + + + + + + + + + + + + + + + + + + + + + + + +

+Public Member Functions

def __defaults__ (self)
 
def evaluate_thrust (self, state)
 
def unpack_unknowns_transition (self, segment)
 
def unpack_unknowns_cruise (self, segment)
 
def unpack_unknowns_lift (self, segment)
 
def residuals_transition (self, segment)
 
def residuals_cruise (self, segment)
 
def residuals_lift (self, segment)
 
def add_transition_unknowns_and_residuals_to_segment (self, segment, initial_voltage=None, initial_prop_power_coefficient=0.005, initial_lift_rotor_power_coefficient=0.005, initial_throttle_lift=0.9, initial_battery_cell_temperature=283., initial_battery_state_of_charge=0.5, initial_battery_cell_current=5.)
 
def add_cruise_unknowns_and_residuals_to_segment (self, segment, initial_voltage=None, initial_prop_power_coefficient=0.005, initial_battery_cell_temperature=283., initial_battery_state_of_charge=0.5, initial_battery_cell_current=5.)
 
def add_lift_unknowns_and_residuals_to_segment (self, segment, initial_voltage=None, initial_lift_rotor_power_coefficient=0.005, initial_throttle_lift=0.9, initial_battery_cell_temperature=283., initial_battery_state_of_charge=0.5, initial_battery_cell_current=5.)
 
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Attributes

lift_rotor_motors
 
propeller_motors
 
lift_rotors
 
propellers
 
lift_rotor_esc
 
propeller_esc
 
avionics
 
payload
 
battery
 
lift_rotor_engine_length
 
propeller_engine_length
 
number_of_lift_rotor_engines
 
number_of_propeller_engines
 
voltage
 
tag
 
generative_design_minimum
 
identical_propellers
 
identical_lift_rotors
 
- Public Attributes inherited from SUAVE.Components.Energy.Networks.Network.Network
tag
 
generative_design_max_per_vehicle
 
non_dimensional_origin
 
number_of_engines
 
engine_length
 
wing_mounted
 
areas
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 
+

Detailed Description

+
This is a complex version of battery_propeller with a battery powering propellers through
+    electric motors. In this case we have 2 sets of motors at different motors that can be controlled seperately
+    
+    This network adds 2 extra unknowns to the mission. The first is
+    a voltage, to calculate the thevenin voltage drop in the pack.
+    The second is torque matching between motor and propeller.
+    
+    We have two inputs, the forward throttle and the lift throttle setting
+    Since this is an airplane first and foremost, the "throttle" will be for forward thrust
+    The new unknown will be for lift throttle, because of the assumption on throttle something needs to be done...
+    Want only 1 residual on voltage
+
+    Assumptions:
+    For any segment using this, body angle can't be an unknown.
+    
+    Source:
+    None
+

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Components.Energy.Networks.Lift_Cruise.Lift_Cruise.__defaults__ ( self)
+
+
This sets the default values for the network to function.
+    
+    Assumptions:
+    None
+    
+    Source:
+    N/A
+    
+    Inputs:
+    None
+    
+    Outputs:
+    None
+    
+    Properties Used:
+    N/A
+
+

Reimplemented from SUAVE.Components.Energy.Networks.Network.Network.

+ +
+
+ +

◆ add_cruise_unknowns_and_residuals_to_segment()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Components.Energy.Networks.Lift_Cruise.Lift_Cruise.add_cruise_unknowns_and_residuals_to_segment ( self,
 segment,
 initial_voltage = None,
 initial_prop_power_coefficient = 0.005,
 initial_battery_cell_temperature = 283.,
 initial_battery_state_of_charge = 0.5,
 initial_battery_cell_current = 5. 
)
+
+
This function sets up the information that the mission needs to run a mission segment using this network
+    
+    Assumptions:
+    None
+    
+    Source:
+    N/A
+    
+    Inputs:
+    segment
+    initial_voltage                   [v]
+    initial_power_coefficient         [float]s
+    
+    Outputs:
+    segment.state.unknowns.battery_voltage_under_load
+    segment.state.unknowns.propeller_power_coefficient
+    segment.state.conditions.propulsion.propeller_motor_torque
+    segment.state.conditions.propulsion.propeller_torque   
+    
+    Properties Used:
+    N/A
+
+
+
+ +

◆ add_lift_unknowns_and_residuals_to_segment()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Components.Energy.Networks.Lift_Cruise.Lift_Cruise.add_lift_unknowns_and_residuals_to_segment ( self,
 segment,
 initial_voltage = None,
 initial_lift_rotor_power_coefficient = 0.005,
 initial_throttle_lift = 0.9,
 initial_battery_cell_temperature = 283.,
 initial_battery_state_of_charge = 0.5,
 initial_battery_cell_current = 5. 
)
+
+
This function sets up the information that the mission needs to run a mission segment using this network
+
+    Assumptions:
+    None
+
+    Source:
+    N/A
+
+    Inputs:
+    segment
+    initial_voltage                   [v]
+    initial_power_coefficient         [float]s
+
+    Outputs:
+    segment.state.unknowns.battery_voltage_under_load
+    segment.state.unknowns.propeller_power_coefficient
+    segment.state.conditions.propulsion.propeller_motor_torque
+    segment.state.conditions.propulsion.propeller_torque   
+
+    Properties Used:
+    N/A
+
+
+
+ +

◆ add_transition_unknowns_and_residuals_to_segment()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Components.Energy.Networks.Lift_Cruise.Lift_Cruise.add_transition_unknowns_and_residuals_to_segment ( self,
 segment,
 initial_voltage = None,
 initial_prop_power_coefficient = 0.005,
 initial_lift_rotor_power_coefficient = 0.005,
 initial_throttle_lift = 0.9,
 initial_battery_cell_temperature = 283.,
 initial_battery_state_of_charge = 0.5,
 initial_battery_cell_current = 5. 
)
+
+
This function sets up the information that the mission needs to run a mission segment using this network
+    
+    Assumptions:
+    None
+    
+    Source:
+    N/A
+    
+    Inputs:
+    segment
+    initial_voltage                   [v]
+    initial_power_coefficient         [float]s
+    
+    Outputs:
+    segment.state.unknowns.battery_voltage_under_load
+    segment.state.unknowns.propeller_power_coefficient
+    segment.state.conditions.propulsion.propeller_motor_torque
+    segment.state.conditions.propulsion.propeller_torque   
+    
+    Properties Used:
+    N/A
+
+
+
+ +

◆ evaluate_thrust()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Components.Energy.Networks.Lift_Cruise.Lift_Cruise.evaluate_thrust ( self,
 state 
)
+
+
Calculate thrust given the current state of the vehicle
+    
+    Assumptions:
+    Caps the throttle at 110% and linearly interpolates thrust off that
+    
+    Source:
+    N/A
+    
+    Inputs:
+    state [state()]
+    
+    Outputs:
+    results.thrust_force_vector       [Newtons]
+    results.vehicle_mass_rate         [kg/s]
+    conditions.propulsion:
+lift_rotor_rpm                [radians/sec]
+rpm _forward                  [radians/sec]
+lift_rotor_current_draw       [amps]
+propeller_current_draw        [amps]
+battery_power_draw            [watts]
+battery_energy                [joules]
+voltage_open_circuit          [volts]
+voltage_under_load            [volts]
+lift_rotor_motor_torque       [N-M]
+propeller_motor_torque        [N-M]
+lift_rotor_thrust             [N]
+propeller_thrust              [N]
+lift_rotor_torque             [N-M]
+propeller_torque              [N-M]
+    
+    Properties Used:
+    Defaulted values
+
+
+
+ +

◆ residuals_cruise()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Components.Energy.Networks.Lift_Cruise.Lift_Cruise.residuals_cruise ( self,
 segment 
)
+
+
This packs the residuals to be sent to the mission solver.
+    Use this if only the forward motors are operational
+    
+    Assumptions:
+    Only the forward motors are operational
+    
+    Source:
+    N/A
+    
+    Inputs:
+    state.conditions.propulsion:
+propeller_motor_torque                [N-m]
+lift_rotor_motor_torque               [N-m]
+propeller_torque                      [N-m]
+lift_rotor_torque                     [N-m]
+voltage_under_load                    [volts]
+    state.unknowns.battery_voltage_under_load [volts]
+    
+    Outputs:
+    None
+    
+    Properties Used:
+    self.voltage                              [volts]
+
+
+
+ +

◆ residuals_lift()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Components.Energy.Networks.Lift_Cruise.Lift_Cruise.residuals_lift ( self,
 segment 
)
+
+
This packs the residuals to be sent to the mission solver.
+    Only the lift motors are operational
+    
+    Assumptions:
+    The lift motors are operational
+    
+    Source:
+    N/A
+    
+    Inputs:
+    state.conditions.propulsion:
+propeller_motor_torque                [N-m]
+lift_rotor_motor_torque               [N-m]
+propeller_torque                      [N-m]
+lift_rotor_torque                     [N-m]
+voltage_under_load                    [volts]
+    state.unknowns.battery_voltage_under_load [volts]
+    
+    Outputs:
+    None
+    
+    Properties Used:
+    self.voltage                              [volts]
+
+
+
+ +

◆ residuals_transition()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Components.Energy.Networks.Lift_Cruise.Lift_Cruise.residuals_transition ( self,
 segment 
)
+
+
This packs the residuals to be sent to the mission solver.
+    Use this if all motors are operational
+    
+    Assumptions:
+    All motors are operational
+    
+    Source:
+    N/A
+    
+    Inputs:
+    state.conditions.propulsion:
+propeller_motor_torque                [N-m]
+lift_rotor_motor_torque               [N-m]
+propeller_torque                      [N-m]
+lift_rotor_torque                     [N-m]
+voltage_under_load                    [volts]
+    state.unknowns.battery_voltage_under_load [volts]
+    
+    Outputs:
+    None
+    
+    Properties Used:
+    self.voltage                              [volts]
+
+
+
+ +

◆ unpack_unknowns_cruise()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Components.Energy.Networks.Lift_Cruise.Lift_Cruise.unpack_unknowns_cruise ( self,
 segment 
)
+
+
This is an extra set of unknowns which are unpacked from the mission solver and send to the network.
+    This uses only the forward motors and turns the rest off.
+    
+    Assumptions:
+    Only the forward motors and turns the rest off.
+    
+    Source:
+    N/A
+    
+    Inputs:
+    state.unknowns.propeller_power_coefficient [None]
+    state.unknowns.battery_voltage_under_load  [volts]
+    state.unknowns.throttle_lift               [0-1]
+    state.unknowns.throttle                    [0-1]
+    
+    Outputs:
+    state.conditions.propulsion.propeller_power_coefficient [None]
+    state.conditions.propulsion.battery_voltage_under_load  [volts]
+    state.conditions.propulsion.throttle_lift               [0-1]
+    state.conditions.propulsion.throttle                    [0-1]
+    
+    Properties Used:
+    N/A
+
+
+
+ +

◆ unpack_unknowns_lift()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Components.Energy.Networks.Lift_Cruise.Lift_Cruise.unpack_unknowns_lift ( self,
 segment 
)
+
+
This is an extra set of unknowns which are unpacked from the mission solver and send to the network.
+    This uses only the lift motors.
+    
+    Assumptions:
+    Only the lift motors.
+    
+    Source:
+    N/A
+    
+    Inputs:
+    state.unknowns.propeller_power_coefficient [None]
+    state.unknowns.battery_voltage_under_load  [volts]
+    state.unknowns.throttle_lift               [0-1]
+    state.unknowns.throttle                    [0-1]
+    
+    Outputs:
+    state.conditions.propulsion.propeller_power_coefficient [None]
+    state.conditions.propulsion.battery_voltage_under_load  [volts]
+    state.conditions.propulsion.throttle_lift               [0-1]
+    state.conditions.propulsion.throttle                    [0-1]
+    
+    Properties Used:
+    N/A
+
+
+
+ +

◆ unpack_unknowns_transition()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Components.Energy.Networks.Lift_Cruise.Lift_Cruise.unpack_unknowns_transition ( self,
 segment 
)
+
+
This is an extra set of unknowns which are unpacked from the mission solver and sent to the network.
+    This uses all the motors.
+    
+    Assumptions:
+    None
+    
+    Source:
+    N/A
+    
+    Inputs:
+    state.unknowns.lift_rotor_power_coefficient [None]
+    state.unknowns.propeller_power_coefficient  [None]
+    state.unknowns.battery_voltage_under_load   [volts]
+    state.unknowns.throttle_lift                [0-1]
+    state.unknowns.throttle                     [0-1]
+    
+    Outputs:
+    state.conditions.propulsion.lift_rotor_power_coefficient [None]
+    state.conditions.propulsion.propeller_power_coefficient  [None]
+    state.conditions.propulsion.battery_voltage_under_load   [volts]
+    state.conditions.propulsion.throttle_lift                [0-1]
+    state.conditions.propulsion.throttle                     [0-1]
+    
+    Properties Used:
+    N/A
+
+
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Energy/Networks/Lift_Cruise.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Lift__Cruise_1_1Lift__Cruise.js b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Lift__Cruise_1_1Lift__Cruise.js new file mode 100644 index 00000000..c2bbd758 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Lift__Cruise_1_1Lift__Cruise.js @@ -0,0 +1,32 @@ +var classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Lift__Cruise_1_1Lift__Cruise = +[ + [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Lift__Cruise_1_1Lift__Cruise.html#a41965401948b59792f0e7485497279b7", null ], + [ "add_cruise_unknowns_and_residuals_to_segment", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Lift__Cruise_1_1Lift__Cruise.html#a63c461cf2dbc6ac456d1f7531145090d", null ], + [ "add_lift_unknowns_and_residuals_to_segment", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Lift__Cruise_1_1Lift__Cruise.html#ad8142b81db8e46b318cdf38eccac710d", null ], + [ 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a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Lift__Forward__Propulsor_1_1Lift__Forward__Propulsor-members.html +++ /dev/null @@ -1,142 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.1.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
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-
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-
-
- -
- -
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- - -
- -
- -
-
-
SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward_Propulsor Member List
-
-
- -

This is the complete list of members for SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward_Propulsor, including all inherited members.

- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
__defaults__(self)SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward_Propulsor
avionics (defined in SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward_Propulsor)SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward_Propulsor
battery (defined in SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward_Propulsor)SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward_Propulsor
engine_length_forward (defined in SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward_Propulsor)SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward_Propulsor
engine_length_lift (defined in SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward_Propulsor)SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward_Propulsor
esc_forward (defined in SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward_Propulsor)SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward_Propulsor
esc_lift (defined in SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward_Propulsor)SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward_Propulsor
evaluate_thrust(self, state)SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward_Propulsor
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
motor_forward (defined in SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward_Propulsor)SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward_Propulsor
motor_lift (defined in SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward_Propulsor)SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward_Propulsor
nacelle_diameter_forward (defined in SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward_Propulsor)SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward_Propulsor
nacelle_diameter_lift (defined in SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward_Propulsor)SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward_Propulsor
number_of_engines_forward (defined in SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward_Propulsor)SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward_Propulsor
number_of_engines_lift (defined in SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward_Propulsor)SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward_Propulsor
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
payload (defined in SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward_Propulsor)SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward_Propulsor
propeller_forward (defined in SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward_Propulsor)SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward_Propulsor
propeller_lift (defined in SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward_Propulsor)SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward_Propulsor
residuals(self, segment, state)SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward_Propulsor
residuals_no_forward(self, segment, state)SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward_Propulsor
residuals_no_lift(self, segment, state)SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward_Propulsor
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Propulsors.Propulsor.Propulsor)SUAVE.Components.Propulsors.Propulsor.Propulsor
thrust_angle_forward (defined in SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward_Propulsor)SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward_Propulsor
thrust_angle_lift (defined in SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward_Propulsor)SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward_Propulsor
unpack_unknowns(self, segment, state)SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward_Propulsor
unpack_unknowns_no_forward(self, segment, state)SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward_Propulsor
unpack_unknowns_no_lift(self, segment, state)SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward_Propulsor
voltage (defined in SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward_Propulsor)SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward_Propulsor
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- - - - diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Lift__Forward__Propulsor_1_1Lift__Forward__Propulsor.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Lift__Forward__Propulsor_1_1Lift__Forward__Propulsor.html deleted file mode 100644 index de1e3a24..00000000 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Lift__Forward__Propulsor_1_1Lift__Forward__Propulsor.html +++ /dev/null @@ -1,693 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward_Propulsor Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.1.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward_Propulsor Class Reference
-
-
-
-Inheritance diagram for SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward_Propulsor:
-
-
- - -SUAVE.Components.Propulsors.Propulsor.Propulsor -SUAVE.Components.Physical_Component.Physical_Component -SUAVE.Components.Component.Component - -
- - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
def evaluate_thrust (self, state)
 
def unpack_unknowns (self, segment, state)
 
def unpack_unknowns_no_lift (self, segment, state)
 
def unpack_unknowns_no_forward (self, segment, state)
 
def residuals (self, segment, state)
 
def residuals_no_lift (self, segment, state)
 
def residuals_no_forward (self, segment, state)
 
- Public Member Functions inherited from SUAVE.Components.Propulsors.Propulsor.Propulsor
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

motor_lift
 
motor_forward
 
propeller_lift
 
propeller_forward
 
esc_lift
 
esc_forward
 
avionics
 
payload
 
battery
 
nacelle_diameter_lift
 
nacelle_diameter_forward
 
engine_length_lift
 
engine_length_forward
 
number_of_engines_lift
 
number_of_engines_forward
 
voltage
 
thrust_angle_lift
 
thrust_angle_forward
 
- Public Attributes inherited from SUAVE.Components.Propulsors.Propulsor.Propulsor
tag
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
-

Detailed Description

-
This is a complex version of battery_propeller with a battery powering propellers through
-    electric motors. In this case we have 2 sets of motors at different motors that can be controlled seperately
-    
-    This network adds 2 extra unknowns to the mission. The first is
-    a voltage, to calculate the thevenin voltage drop in the pack.
-    The second is torque matching between motor and propeller.
-    
-    We have two inputs, the forward throttle and the lift throttle setting
-
-    Since this is an airplane first and foremost, the "throttle" will be for forward thrust
-    The new unknown will be for lift throttle, because of the assumption on throttle something needs to be done...
-
-    Want only 1 residual on voltage
-
-    Assumptions:
-    For any segment using this, body angle can't be an unknown.
-    
-    Source:
-    None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward_Propulsor.__defaults__ ( self)
-
-
This sets the default values for the network to function.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    N/A
-
-
-
- -

◆ evaluate_thrust()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward_Propulsor.evaluate_thrust ( self,
 state 
)
-
-
Calculate thrust given the current state of the vehicle
-    
-    Assumptions:
-    Caps the throttle at 110% and linearly interpolates thrust off that
-    
-    Source:
-    N/A
-    
-    Inputs:
-    state [state()]
-    
-    Outputs:
-    results.thrust_force_vector [Newtons]
-    results.vehicle_mass_rate   [kg/s]
-    conditions.propulsion:
-rpm_lift                 [radians/sec]
-rpm _forward             [radians/sec]
-current_lift             [amps]
-current_forward          [amps]
-battery_draw             [watts]
-battery_energy           [joules]
-voltage_open_circuit     [volts]
-voltage_under_load       [volts]
-motor_torque_lift        [N-M]
-motor_torque_forward     [N-M]
-propeller_torque_lift    [N-M]
-propeller_torque_forward [N-M]
-    
-    Properties Used:
-    Defaulted values
-
-
-
- -

◆ residuals()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward_Propulsor.residuals ( self,
 segment,
 state 
)
-
-
This packs the residuals to be send to the mission solver.
-    Use this if all motors are operational
-    
-    Assumptions:
-    All motors are operational
-    
-    Source:
-    N/A
-    
-    Inputs:
-    state.conditions.propulsion:
-motor_torque_forward                  [N-m]
-motor_torque_lift                     [N-m]
-propeller_torque_forward              [N-m]
-propeller_torque_lift                 [N-m]
-voltage_under_load                    [volts]
-    state.unknowns.battery_voltage_under_load [volts]
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    self.voltage                              [volts]
-
-
-
- -

◆ residuals_no_forward()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward_Propulsor.residuals_no_forward ( self,
 segment,
 state 
)
-
-
This packs the residuals to be send to the mission solver.
-    Only the lift motors are operational
-    
-    Assumptions:
-    The lift motors are operational
-    
-    Source:
-    N/A
-    
-    Inputs:
-    state.conditions.propulsion:
-motor_torque_forward                  [N-m]
-motor_torque_lift                     [N-m]
-propeller_torque_forward              [N-m]
-propeller_torque_lift                 [N-m]
-voltage_under_load                    [volts]
-    state.unknowns.battery_voltage_under_load [volts]
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    self.voltage                              [volts]
-
-
-
- -

◆ residuals_no_lift()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward_Propulsor.residuals_no_lift ( self,
 segment,
 state 
)
-
-
This packs the residuals to be send to the mission solver.
-    Use this if only the forward motors are operational
-    
-    Assumptions:
-    Only the forward motors are operational
-    
-    Source:
-    N/A
-    
-    Inputs:
-    state.conditions.propulsion:
-motor_torque_forward                  [N-m]
-motor_torque_lift                     [N-m]
-propeller_torque_forward              [N-m]
-propeller_torque_lift                 [N-m]
-voltage_under_load                    [volts]
-    state.unknowns.battery_voltage_under_load [volts]
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    self.voltage                              [volts]
-
-
-
- -

◆ unpack_unknowns()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward_Propulsor.unpack_unknowns ( self,
 segment,
 state 
)
-
-
This is an extra set of unknowns which are unpacked from the mission solver and send to the network.
-    This uses all the motors.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    state.unknowns.propeller_power_coefficient [None]
-    state.unknowns.battery_voltage_under_load  [volts]
-    state.unknowns.lift_throttle               [0-1]
-    state.unknowns.throttle                    [0-1]
-    
-    Outputs:
-    state.conditions.propulsion.propeller_power_coefficient [None]
-    state.conditions.propulsion.battery_voltage_under_load  [volts]
-    state.conditions.propulsion.lift_throttle               [0-1]
-    state.conditions.propulsion.throttle                    [0-1]
-    
-    Properties Used:
-    N/A
-
-
-
- -

◆ unpack_unknowns_no_forward()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward_Propulsor.unpack_unknowns_no_forward ( self,
 segment,
 state 
)
-
-
This is an extra set of unknowns which are unpacked from the mission solver and send to the network.
-    This uses only the lift motors.
-    
-    Assumptions:
-    Only the lift motors.
-    
-    Source:
-    N/A
-    
-    Inputs:
-    state.unknowns.propeller_power_coefficient [None]
-    state.unknowns.battery_voltage_under_load  [volts]
-    state.unknowns.lift_throttle               [0-1]
-    state.unknowns.throttle                    [0-1]
-    
-    Outputs:
-    state.conditions.propulsion.propeller_power_coefficient [None]
-    state.conditions.propulsion.battery_voltage_under_load  [volts]
-    state.conditions.propulsion.lift_throttle               [0-1]
-    state.conditions.propulsion.throttle                    [0-1]
-    
-    Properties Used:
-    N/A
-
-
-
- -

◆ unpack_unknowns_no_lift()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward_Propulsor.unpack_unknowns_no_lift ( self,
 segment,
 state 
)
-
-
This is an extra set of unknowns which are unpacked from the mission solver and send to the network.
-    This uses only the forward motors and turns the rest off.
-    
-    Assumptions:
-    Only the forward motors and turns the rest off.
-    
-    Source:
-    N/A
-    
-    Inputs:
-    state.unknowns.propeller_power_coefficient [None]
-    state.unknowns.battery_voltage_under_load  [volts]
-    state.unknowns.lift_throttle               [0-1]
-    state.unknowns.throttle                    [0-1]
-    
-    Outputs:
-    state.conditions.propulsion.propeller_power_coefficient [None]
-    state.conditions.propulsion.battery_voltage_under_load  [volts]
-    state.conditions.propulsion.lift_throttle               [0-1]
-    state.conditions.propulsion.throttle                    [0-1]
-    
-    Properties Used:
-    N/A
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Energy/Networks/Lift_Forward_Propulsor.py
  • -
-
-
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+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
SUAVE.Components.Energy.Networks.Liquid_Rocket.Liquid_Rocket Member List
+
+
+ +

This is the complete list of members for SUAVE.Components.Energy.Networks.Liquid_Rocket.Liquid_Rocket, including all inherited members.

+ + + + + + + + + + + + + + + + + +
__defaults__(self)SUAVE.Components.Energy.Networks.Liquid_Rocket.Liquid_Rocket
areas (defined in SUAVE.Components.Energy.Networks.Liquid_Rocket.Liquid_Rocket)SUAVE.Components.Energy.Networks.Liquid_Rocket.Liquid_Rocket
engine_length (defined in SUAVE.Components.Energy.Networks.Liquid_Rocket.Liquid_Rocket)SUAVE.Components.Energy.Networks.Liquid_Rocket.Liquid_Rocket
evaluate_thrust(self, state)SUAVE.Components.Energy.Networks.Liquid_Rocket.Liquid_Rocket
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
internal (defined in SUAVE.Components.Energy.Networks.Liquid_Rocket.Liquid_Rocket)SUAVE.Components.Energy.Networks.Liquid_Rocket.Liquid_Rocket
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
non_dimensional_origin (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
number_of_engines (defined in SUAVE.Components.Energy.Networks.Liquid_Rocket.Liquid_Rocket)SUAVE.Components.Energy.Networks.Liquid_Rocket.Liquid_Rocket
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
size(self, state)SUAVE.Components.Energy.Networks.Liquid_Rocket.Liquid_Rocket
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Energy.Networks.Liquid_Rocket.Liquid_Rocket)SUAVE.Components.Energy.Networks.Liquid_Rocket.Liquid_Rocket
wing_mounted (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Liquid__Rocket_1_1Liquid__Rocket.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Liquid__Rocket_1_1Liquid__Rocket.html new file mode 100644 index 00000000..4299be39 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Liquid__Rocket_1_1Liquid__Rocket.html @@ -0,0 +1,358 @@ + + + + + + + +SUAVE: SUAVE.Components.Energy.Networks.Liquid_Rocket.Liquid_Rocket Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Components.Energy.Networks.Liquid_Rocket.Liquid_Rocket Class Reference
+
+
+
+Inheritance diagram for SUAVE.Components.Energy.Networks.Liquid_Rocket.Liquid_Rocket:
+
+
+ + +SUAVE.Components.Energy.Networks.Network.Network +SUAVE.Components.Physical_Component.Physical_Component +SUAVE.Components.Component.Component + +
+ + + + + + + + +

+Public Member Functions

def __defaults__ (self)
 
def evaluate_thrust (self, state)
 
def size (self, state)
 
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Attributes

tag
 
number_of_engines
 
engine_length
 
areas
 
internal
 
- Public Attributes inherited from SUAVE.Components.Energy.Networks.Network.Network
tag
 
generative_design_max_per_vehicle
 
non_dimensional_origin
 
number_of_engines
 
engine_length
 
wing_mounted
 
areas
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 
+

Detailed Description

+
This sets up the equations for a liquid rocket.
+
+    Assumptions:
+    Quasi 1-D flow
+    Adiabatic Nozzles
+    Throat Always Choked
+
+    Source:
+    Chapter 7
+    https://web.stanford.edu/~cantwell/AA283_Course_Material/AA283_Course_Notes/
+

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Components.Energy.Networks.Liquid_Rocket.Liquid_Rocket.__defaults__ ( self)
+
+
This sets the default values for the network to function.
+
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+None
+
+Outputs:
+None
+
+Properties Used:
+N/A
+
+

Reimplemented from SUAVE.Components.Energy.Networks.Network.Network.

+ +
+
+ +

◆ evaluate_thrust()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Components.Energy.Networks.Liquid_Rocket.Liquid_Rocket.evaluate_thrust ( self,
 state 
)
+
+
Calculate thrust given the current state of the vehicle
+
+    Assumptions:
+    None
+
+    Source:
+    N/A
+
+    Inputs:
+    state [state()]
+
+    Outputs:
+    results.thrust_force_vector                      [newtons]
+    results.vehicle_mass_rate                        [kg/s]
+    results.specific_impulse                         [s]
+    conditions.noise.sources.liquid_rocket:
+core:
+exit_static_temperature                  [K]
+exit_static_pressure                     [K]
+exit_stagnation_temperature              [K]
+exit_stagnation_pressure                 [Pa]
+exit_velocity                            [m/s]
+
+    Properties Used:
+    Defaulted values
+
+
+ +

◆ size()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Components.Energy.Networks.Liquid_Rocket.Liquid_Rocket.size ( self,
 state 
)
+
+
Size the ramjet
+
+    Assumptions:
+    None
+
+    Source:
+    N/A
+
+    Inputs:
+    State [state()]
+
+    Outputs:
+    None
+
+    Properties Used:
+    N/A
+
+
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Energy/Networks/Liquid_Rocket.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Liquid__Rocket_1_1Liquid__Rocket.js b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Liquid__Rocket_1_1Liquid__Rocket.js new file mode 100644 index 00000000..c3c705dd --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Liquid__Rocket_1_1Liquid__Rocket.js @@ -0,0 +1,11 @@ +var classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Liquid__Rocket_1_1Liquid__Rocket = +[ + [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Liquid__Rocket_1_1Liquid__Rocket.html#a6346a4609154bee391c196c35c6a42c7", null ], + [ "evaluate_thrust", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Liquid__Rocket_1_1Liquid__Rocket.html#a757d64d2aa39d22579a51e3beb181d3a", null ], + [ "size", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Liquid__Rocket_1_1Liquid__Rocket.html#a52467435a573f00ef77e69400a7fe8c7", null ], + [ "areas", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Liquid__Rocket_1_1Liquid__Rocket.html#a93d2fac67e083b85c52a7c9f9fdb2a32", null ], + [ "engine_length", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Liquid__Rocket_1_1Liquid__Rocket.html#a53fdefdb12b469c50e9ec9d01c96dd7b", null ], + [ "internal", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Liquid__Rocket_1_1Liquid__Rocket.html#ae6d29f84ddebfc60613bdbed1e514bcf", null ], + [ "number_of_engines", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Liquid__Rocket_1_1Liquid__Rocket.html#a3570b5d84da944998fa00a23e7d29aaf", null ], + [ "tag", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Liquid__Rocket_1_1Liquid__Rocket.html#addeecd5a5ae5ec3e2528536f9cdad583", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Liquid__Rocket_1_1Liquid__Rocket.png b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Liquid__Rocket_1_1Liquid__Rocket.png new file mode 100644 index 00000000..c804599d Binary files /dev/null and b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Liquid__Rocket_1_1Liquid__Rocket.png differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Network_1_1Container-members.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Network_1_1Container-members.html new file mode 100644 index 00000000..67d61e96 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Network_1_1Container-members.html @@ -0,0 +1,124 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
SUAVE.Components.Energy.Networks.Network.Container Member List
+
+ +
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Network_1_1Container.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Network_1_1Container.html new file mode 100644 index 00000000..72a26281 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Network_1_1Container.html @@ -0,0 +1,242 @@ + + + + + + + +SUAVE: SUAVE.Components.Energy.Networks.Network.Container Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Components.Energy.Networks.Network.Container Class Reference
+
+
+
+Inheritance diagram for SUAVE.Components.Energy.Networks.Network.Container:
+
+
+ + +SUAVE.Components.Physical_Component.Container +SUAVE.Components.Component.Container + +
+ + + + + + + + + + + +

+Public Member Functions

def get_children (self)
 
def evaluate_thrust (self, state)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Container
def sum_mass (self)
 
def total_moment (self)
 
+ + + + +

+Additional Inherited Members

- Static Public Attributes inherited from SUAVE.Components.Component.Container
Container
 
+

Detailed Description

+
SUAVE.Components.Energy.Networks.Network.Container()
+    
+    The Network Container Class
+
+        Assumptions:
+        None
+        
+        Source:
+        N/A

Member Function Documentation

+ +

◆ evaluate_thrust()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Components.Energy.Networks.Network.Container.evaluate_thrust ( self,
 state 
)
+
+
This is used to evaluate the thrust produced by the network.
+
+Assumptions:
+Network has "evaluate_thrust" method
+If multiple networks are attached their masses will be summed
+
+Source:
+N/A
+
+Inputs:
+State variables
+
+Outputs:
+Results of the "evaluate_thrust" method
+
+Properties Used:
+N/A
+
+
+
+ +

◆ get_children()

+ +
+
+ + + + + + + + +
def SUAVE.Components.Energy.Networks.Network.Container.get_children ( self)
+
+
Returns the components that can go inside
+
+Assumptions:
+None
+    
+Source:
+N/A
+    
+Inputs:
+None
+    
+Outputs:
+None
+    
+Properties Used:
+N/A
+
+
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Energy/Networks/Network.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Network_1_1Container.js b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Network_1_1Container.js new file mode 100644 index 00000000..f4c4cc21 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Network_1_1Container.js @@ -0,0 +1,5 @@ +var classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Network_1_1Container = +[ + [ "evaluate_thrust", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Network_1_1Container.html#a4846e6abc24e477648186a94eef2017a", null ], + [ "get_children", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Network_1_1Container.html#a8aed9c51d77937df972d1a888169dc99", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Network_1_1Container.png b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Network_1_1Container.png new file mode 100644 index 00000000..9c6e5bd9 Binary files /dev/null and b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Network_1_1Container.png differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Network_1_1Network-members.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Network_1_1Network-members.html new file mode 100644 index 00000000..3dcd47f5 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Network_1_1Network-members.html @@ -0,0 +1,132 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
SUAVE.Components.Energy.Networks.Network.Network Member List
+
+
+ +

This is the complete list of members for SUAVE.Components.Energy.Networks.Network.Network, including all inherited members.

+ + + + + + + + + + + + + + +
__defaults__(self)SUAVE.Components.Energy.Networks.Network.Network
areas (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
engine_length (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
non_dimensional_origin (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
number_of_engines (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
wing_mounted (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Network_1_1Network.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Network_1_1Network.html new file mode 100644 index 00000000..82aa14ac --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Network_1_1Network.html @@ -0,0 +1,258 @@ + + + + + + + +SUAVE: SUAVE.Components.Energy.Networks.Network.Network Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Components.Energy.Networks.Network.Network Class Reference
+
+
+
+Inheritance diagram for SUAVE.Components.Energy.Networks.Network.Network:
+
+
+ + +SUAVE.Components.Physical_Component.Physical_Component +SUAVE.Components.Component.Component +SUAVE.Components.Energy.Networks.Battery_Cell_Cycler.Battery_Cell_Cycler +SUAVE.Components.Energy.Networks.Battery_Ducted_Fan.Battery_Ducted_Fan +SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller +SUAVE.Components.Energy.Networks.Ducted_Fan.Ducted_Fan +SUAVE.Components.Energy.Networks.Internal_Combustion_Propeller.Internal_Combustion_Propeller +SUAVE.Components.Energy.Networks.Internal_Combustion_Propeller_Constant_Speed.Internal_Combustion_Propeller_Constant_Speed +SUAVE.Components.Energy.Networks.Lift_Cruise.Lift_Cruise +SUAVE.Components.Energy.Networks.Liquid_Rocket.Liquid_Rocket +SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate +SUAVE.Components.Energy.Networks.Ramjet.Ramjet +SUAVE.Components.Energy.Networks.Scramjet.Scramjet +SUAVE.Components.Energy.Networks.Serial_Hybrid_Ducted_Fan.Serial_Hybrid_Ducted_Fan +SUAVE.Components.Energy.Networks.Solar.Solar +SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity +SUAVE.Components.Energy.Networks.Turboelectric_HTS_Ducted_Fan.Turboelectric_HTS_Ducted_Fan +SUAVE.Components.Energy.Networks.Turbofan.Turbofan +SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super + +
+ + + + +

+Public Member Functions

def __defaults__ (self)
 
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Attributes

tag
 
generative_design_max_per_vehicle
 
non_dimensional_origin
 
number_of_engines
 
engine_length
 
wing_mounted
 
areas
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 
+

Detailed Description

+
SUAVE.Components.Energy.Networks.Network()
+
+    The Top Level Network Class
+        
+        Assumptions:
+        None
+        
+        Source:
+        N/As

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Components.Energy.Networks.Network.Network.__defaults__ ( self)
+
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Energy/Networks/Network.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Network_1_1Network.js b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Network_1_1Network.js new file mode 100644 index 00000000..404700c3 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Network_1_1Network.js @@ -0,0 +1,11 @@ +var classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Network_1_1Network = +[ + [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Network_1_1Network.html#a7a5d3bb11ab9901d11036359becf7e64", null ], + [ "areas", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Network_1_1Network.html#a78e3ed07ad6da7d1e53fc69a9536658b", null ], + [ "engine_length", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Network_1_1Network.html#a4d8a80583415b9e10f8e9b3bb26f2554", null ], + [ "generative_design_max_per_vehicle", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Network_1_1Network.html#a6ef65f7aed62f7d025dada76295e3e19", null ], + [ "non_dimensional_origin", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Network_1_1Network.html#a7f79f7aebbd97d4ff0db8aea58016deb", null ], + [ "number_of_engines", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Network_1_1Network.html#a61559d62ccda762c56dcbda7490b03a4", null ], + [ "tag", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Network_1_1Network.html#a69987988f32ccc4d9e71780b3406ecd4", null ], + [ "wing_mounted", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Network_1_1Network.html#a2d62dacd764a6e5d0aa44e171864a8d3", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Network_1_1Network.png b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Network_1_1Network.png new file mode 100644 index 00000000..d75a78a2 Binary files /dev/null and b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Network_1_1Network.png differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Propulsor__Surrogate_1_1Propulsor__Surrogate-members.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Propulsor__Surrogate_1_1Propulsor__Surrogate-members.html index 9c55513f..9fa684eb 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Propulsor__Surrogate_1_1Propulsor__Surrogate-members.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Propulsor__Surrogate_1_1Propulsor__Surrogate-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -99,21 +106,40 @@

This is the complete list of members for SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate, including all inherited members.

- - - - + + + + + + + + + + - - + + + + + + + + + + - - + + + + + + +
__defaults__(self)SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate
areas (defined in SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate)SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate
build_surrogate(self)SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate
engine_length (defined in SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate)SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate
evaluate_thrust(self, state)SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate
altitude_input_scale (defined in SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate)SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate
areas (defined in SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate)SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate
build_surrogate(self)SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate
engine_length (defined in SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate)SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate
evaluate_thrust(self, state)SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate
extended_sfc_surrogate(self, sfc_surrogate, cond, lo_blender, hi_blender)SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate
extended_thrust_surrogate(self, thr_surrogate, cond, lo_blender, hi_blender)SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
input_file (defined in SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate)SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
nacelle_diameter (defined in SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate)SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate
number_of_engines (defined in SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate)SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate
negative_throttle_values (defined in SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate)SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate
non_dimensional_origin (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
number_of_engines (defined in SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate)SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate
orientation_euler_angles (defined in SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate)SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
sealevel_static_thrust (defined in SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate)SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate
sfc_anchor (defined in SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate)SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate
sfc_anchor_conditions (defined in SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate)SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate
sfc_anchor_scale (defined in SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate)SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate
sfc_input_scale (defined in SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate)SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate
sfc_rubber_scale (defined in SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate)SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate
sfc_surrogate (defined in SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate)SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate
surrogate_type (defined in SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate)SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate)SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate
thrust_angle (defined in SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate)SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate
thrust_surrogate (defined in SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate)SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate
thrust_anchor (defined in SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate)SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate
thrust_anchor_conditions (defined in SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate)SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate
thrust_anchor_scale (defined in SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate)SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate
thrust_input_scale (defined in SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate)SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate
thrust_surrogate (defined in SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate)SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate
use_extended_surrogate (defined in SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate)SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate
wing_mounted (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
@@ -121,7 +147,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Propulsor__Surrogate_1_1Propulsor__Surrogate.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Propulsor__Surrogate_1_1Propulsor__Surrogate.html index b8e2340c..4897c9e6 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Propulsor__Surrogate_1_1Propulsor__Surrogate.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Propulsor__Surrogate_1_1Propulsor__Surrogate.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -105,11 +112,12 @@
-SUAVE.Components.Propulsors.Propulsor.Propulsor +SUAVE.Components.Energy.Networks.Network.Network SUAVE.Components.Physical_Component.Physical_Component SUAVE.Components.Component.Component - -
+SUAVE.Components.Energy.Networks.PyCycle.PyCycle + + @@ -119,21 +127,13 @@ - - - - - - - - - + + + +

Public Member Functions

 
def build_surrogate (self)
 
- Public Member Functions inherited from SUAVE.Components.Propulsors.Propulsor.Propulsor
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
def extended_thrust_surrogate (self, thr_surrogate, cond, lo_blender, hi_blender)
 
def extended_sfc_surrogate (self, sfc_surrogate, cond, lo_blender, hi_blender)
 
- - @@ -152,19 +152,76 @@ - - + + - - + + + + + + + + + + + + + + + + + + + + + + + + + + + - + + + + + + + + + + + + + @@ -185,13 +242,22 @@ + + + + + +

Public Attributes

nacelle_diameter
 
 engine_length
 
 thrust_surrogate
 
thrust_angle
 
orientation_euler_angles
 
 areas
 
 surrogate_type
 
- Public Attributes inherited from SUAVE.Components.Propulsors.Propulsor.Propulsor
+
altitude_input_scale
 
thrust_input_scale
 
sfc_anchor
 
sfc_anchor_scale
 
sfc_anchor_conditions
 
thrust_anchor
 
thrust_anchor_scale
 
thrust_anchor_conditions
 
sfc_rubber_scale
 
use_extended_surrogate
 
sealevel_static_thrust
 
negative_throttle_values
 
sfc_input_scale
 
- Public Attributes inherited from SUAVE.Components.Energy.Networks.Network.Network
 tag
 
 
generative_design_max_per_vehicle
 
non_dimensional_origin
 
number_of_engines
 
engine_length
 
wing_mounted
 
areas
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
 tag
 origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 

Detailed Description

This is a way for you to load engine data from a source.
     A .csv file is read in, a surrogate made, that surrogate is used during the mission analysis.
     
     You need to use build surrogate first when setting up the vehicle to make this work.
-
+    
     Assumptions:
     The input format for this should be Altitude, Mach, Throttle, Thrust, SFC
     
@@ -213,8 +279,8 @@ 

-
This sets the default values for the network to function.
-    
+
This sets the default values for the network to function
+
     Assumptions:
     None
     
@@ -230,6 +296,10 @@ 

SUAVE.Components.Energy.Networks.Network.Network.

+ +

Reimplemented in SUAVE.Components.Energy.Networks.PyCycle.PyCycle.

+

@@ -268,6 +338,8 @@

SUAVE.Components.Energy.Networks.PyCycle.PyCycle.

+ @@ -296,7 +368,7 @@

Calculate thrust given the current state of the vehicle
-    
+
     Assumptions:
     None
     
@@ -315,6 +387,138 @@ 

+

◆ extended_sfc_surrogate()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate.extended_sfc_surrogate ( self,
 sfc_surrogate,
 cond,
 lo_blender,
 hi_blender 
)
+
+
Fixes sfc values outside of the standard throttle range in order to provide
+    reasonable values outside of the typical surrogate coverage area. 
+    
+    Assumptions:
+    None
+    
+    Source:
+    N/A
+    
+    Inputs:
+    sfc_surrogate     - Trained sklearn surrogate that outputs a scaled sfc value
+    cond              - nx3 numpy array with input conditions for the surrogate
+    lo_blender        - Cubic spline blending class that is used at the low throttle cutoff
+    hi_blender        - Cubic spline blending class that is used at the high throttle cutoff
+    
+    Outputs:
+    sfcs              [nondim]
+    
+    Properties Used:
+    None
+
+
+
+ +

◆ extended_thrust_surrogate()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate.extended_thrust_surrogate ( self,
 thr_surrogate,
 cond,
 lo_blender,
 hi_blender 
)
+
+
Fixes thrust values outside of the standard throttle range in order to provide
+    reasonable values outside of the typical surrogate coverage area. 
+    
+    Assumptions:
+    None
+    
+    Source:
+    N/A
+    
+    Inputs:
+    thr_surrogate     - Trained sklearn surrogate that outputs a scaled thrust value
+    cond              - nx3 numpy array with input conditions for the surrogate
+    lo_blender        - Cubic spline blending class that is used at the low throttle cutoff
+    hi_blender        - Cubic spline blending class that is used at the high throttle cutoff
+    
+    Outputs:
+    T                 [nondim]
+    
+    Properties Used:
+    None
+
+
+

The documentation for this class was generated from the following file:
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Energy/Networks/Propulsor_Surrogate.py
@@ -326,7 +530,7 @@

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+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
SUAVE.Components.Energy.Networks.PyCycle.PyCycle Member List
+
+
+ +

This is the complete list of members for SUAVE.Components.Energy.Networks.PyCycle.PyCycle, including all inherited members.

+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
__defaults__(self)SUAVE.Components.Energy.Networks.PyCycle.PyCycle
altitude_input_scale (defined in SUAVE.Components.Energy.Networks.PyCycle.PyCycle)SUAVE.Components.Energy.Networks.PyCycle.PyCycle
areas (defined in SUAVE.Components.Energy.Networks.PyCycle.PyCycle)SUAVE.Components.Energy.Networks.PyCycle.PyCycle
build_surrogate(self)SUAVE.Components.Energy.Networks.PyCycle.PyCycle
engine_length (defined in SUAVE.Components.Energy.Networks.PyCycle.PyCycle)SUAVE.Components.Energy.Networks.PyCycle.PyCycle
evaluate_thrust(self, state)SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate
evaluation_mach_alt (defined in SUAVE.Components.Energy.Networks.PyCycle.PyCycle)SUAVE.Components.Energy.Networks.PyCycle.PyCycle
evaluation_throttles (defined in SUAVE.Components.Energy.Networks.PyCycle.PyCycle)SUAVE.Components.Energy.Networks.PyCycle.PyCycle
extended_sfc_surrogate(self, sfc_surrogate, cond, lo_blender, hi_blender)SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate
extended_thrust_surrogate(self, thr_surrogate, cond, lo_blender, hi_blender)SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
input_file (defined in SUAVE.Components.Energy.Networks.PyCycle.PyCycle)SUAVE.Components.Energy.Networks.PyCycle.PyCycle
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
negative_throttle_values (defined in SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate)SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate
non_dimensional_origin (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
number_of_engines (defined in SUAVE.Components.Energy.Networks.PyCycle.PyCycle)SUAVE.Components.Energy.Networks.PyCycle.PyCycle
orientation_euler_angles (defined in SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate)SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
save_deck (defined in SUAVE.Components.Energy.Networks.PyCycle.PyCycle)SUAVE.Components.Energy.Networks.PyCycle.PyCycle
sealevel_static_thrust (defined in SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate)SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate
sfc_anchor (defined in SUAVE.Components.Energy.Networks.PyCycle.PyCycle)SUAVE.Components.Energy.Networks.PyCycle.PyCycle
sfc_anchor_conditions (defined in SUAVE.Components.Energy.Networks.PyCycle.PyCycle)SUAVE.Components.Energy.Networks.PyCycle.PyCycle
sfc_anchor_scale (defined in SUAVE.Components.Energy.Networks.PyCycle.PyCycle)SUAVE.Components.Energy.Networks.PyCycle.PyCycle
sfc_input_scale (defined in SUAVE.Components.Energy.Networks.PyCycle.PyCycle)SUAVE.Components.Energy.Networks.PyCycle.PyCycle
sfc_rubber_scale (defined in SUAVE.Components.Energy.Networks.PyCycle.PyCycle)SUAVE.Components.Energy.Networks.PyCycle.PyCycle
sfc_surrogate (defined in SUAVE.Components.Energy.Networks.PyCycle.PyCycle)SUAVE.Components.Energy.Networks.PyCycle.PyCycle
surrogate_type (defined in SUAVE.Components.Energy.Networks.PyCycle.PyCycle)SUAVE.Components.Energy.Networks.PyCycle.PyCycle
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Energy.Networks.PyCycle.PyCycle)SUAVE.Components.Energy.Networks.PyCycle.PyCycle
thrust_anchor (defined in SUAVE.Components.Energy.Networks.PyCycle.PyCycle)SUAVE.Components.Energy.Networks.PyCycle.PyCycle
thrust_anchor_conditions (defined in SUAVE.Components.Energy.Networks.PyCycle.PyCycle)SUAVE.Components.Energy.Networks.PyCycle.PyCycle
thrust_anchor_scale (defined in SUAVE.Components.Energy.Networks.PyCycle.PyCycle)SUAVE.Components.Energy.Networks.PyCycle.PyCycle
thrust_input_scale (defined in SUAVE.Components.Energy.Networks.PyCycle.PyCycle)SUAVE.Components.Energy.Networks.PyCycle.PyCycle
thrust_surrogate (defined in SUAVE.Components.Energy.Networks.PyCycle.PyCycle)SUAVE.Components.Energy.Networks.PyCycle.PyCycle
use_extended_surrogate (defined in SUAVE.Components.Energy.Networks.PyCycle.PyCycle)SUAVE.Components.Energy.Networks.PyCycle.PyCycle
wing_mounted (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1PyCycle_1_1PyCycle.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1PyCycle_1_1PyCycle.html new file mode 100644 index 00000000..2e6f3d2c --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1PyCycle_1_1PyCycle.html @@ -0,0 +1,423 @@ + + + + + + + +SUAVE: SUAVE.Components.Energy.Networks.PyCycle.PyCycle Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Components.Energy.Networks.PyCycle.PyCycle Class Reference
+
+
+
+Inheritance diagram for SUAVE.Components.Energy.Networks.PyCycle.PyCycle:
+
+
+ + +SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate +SUAVE.Components.Energy.Networks.Network.Network +SUAVE.Components.Physical_Component.Physical_Component +SUAVE.Components.Component.Component + +
+ + + + + + + + + + + + + +

+Public Member Functions

def __defaults__ (self)
 
def build_surrogate (self)
 
- Public Member Functions inherited from SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate
def evaluate_thrust (self, state)
 
def extended_thrust_surrogate (self, thr_surrogate, cond, lo_blender, hi_blender)
 
def extended_sfc_surrogate (self, sfc_surrogate, cond, lo_blender, hi_blender)
 
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Attributes

engine_length
 
number_of_engines
 
tag
 
input_file
 
sfc_surrogate
 
thrust_surrogate
 
areas
 
surrogate_type
 
altitude_input_scale
 
thrust_input_scale
 
sfc_anchor
 
sfc_anchor_scale
 
sfc_anchor_conditions
 
thrust_anchor
 
thrust_anchor_scale
 
thrust_anchor_conditions
 
sfc_rubber_scale
 
use_extended_surrogate
 
save_deck
 
evaluation_mach_alt
 
evaluation_throttles
 
sfc_input_scale
 
- Public Attributes inherited from SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate
engine_length
 
number_of_engines
 
tag
 
input_file
 
sfc_surrogate
 
thrust_surrogate
 
orientation_euler_angles
 
areas
 
surrogate_type
 
altitude_input_scale
 
thrust_input_scale
 
sfc_anchor
 
sfc_anchor_scale
 
sfc_anchor_conditions
 
thrust_anchor
 
thrust_anchor_scale
 
thrust_anchor_conditions
 
sfc_rubber_scale
 
use_extended_surrogate
 
sealevel_static_thrust
 
negative_throttle_values
 
sfc_input_scale
 
- Public Attributes inherited from SUAVE.Components.Energy.Networks.Network.Network
tag
 
generative_design_max_per_vehicle
 
non_dimensional_origin
 
number_of_engines
 
engine_length
 
wing_mounted
 
areas
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 
+

Detailed Description

+
This is a way for you to run PyCycle, create a deck, and load the deck into a SUAVE surrogate
+    
+    Assumptions:
+    The input format for this should be Altitude, Mach, Throttle, Thrust, SFC
+    
+    Source:
+    None
+

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Components.Energy.Networks.PyCycle.PyCycle.__defaults__ ( self)
+
+
This sets the default values for the network to function
+
+    Assumptions:
+    None
+    
+    Source:
+    N/A
+    
+    Inputs:
+    None
+    
+    Outputs:
+    None
+    
+    Properties Used:
+    N/A
+
+

Reimplemented from SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate.

+ +
+
+ +

◆ build_surrogate()

+ +
+
+ + + + + + + + +
def SUAVE.Components.Energy.Networks.PyCycle.PyCycle.build_surrogate ( self)
+
+
Build a surrogate. Multiple options for models are available including:
+    -Gaussian Processes
+    -KNN
+    -SVR
+    
+    Assumptions:
+    None
+    
+    Source:
+    N/A
+    
+    Inputs:
+    state [state()]
+    
+    Outputs:
+    self.sfc_surrogate    [fun()]
+    self.thrust_surrogate [fun()]
+    
+    Properties Used:
+    Defaulted values
+
+

Reimplemented from SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate.

+ +
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Energy/Networks/PyCycle.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1PyCycle_1_1PyCycle.js b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1PyCycle_1_1PyCycle.js new file mode 100644 index 00000000..f2109ae6 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1PyCycle_1_1PyCycle.js @@ -0,0 +1,27 @@ +var classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1PyCycle_1_1PyCycle = +[ + [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1PyCycle_1_1PyCycle.html#a07c50927f7831a2bc742ba960140ee25", null ], + [ "build_surrogate", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1PyCycle_1_1PyCycle.html#a4f49aee1af6f1a8663414abec4a8553d", null ], + [ "altitude_input_scale", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1PyCycle_1_1PyCycle.html#aa4881d1adc9bcd1d9874e9ffee5f8bce", null ], + [ "areas", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1PyCycle_1_1PyCycle.html#aea18b84b5f6ac96db4aca974e432b99f", null ], + [ "engine_length", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1PyCycle_1_1PyCycle.html#a7ca406ecfc6a0378336c6f86d558ee98", null ], + [ "evaluation_mach_alt", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1PyCycle_1_1PyCycle.html#a9b458518eb0ff7aafb6a995d74ed2f34", null ], + [ "evaluation_throttles", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1PyCycle_1_1PyCycle.html#ae423f0d95c870abde894925012141f7c", null ], + [ "input_file", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1PyCycle_1_1PyCycle.html#a2b87646d410df21857f3f66bf8f03abd", null ], + [ "number_of_engines", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1PyCycle_1_1PyCycle.html#aadf59b826fd42735bf67ff390bf6113b", null ], + [ "save_deck", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1PyCycle_1_1PyCycle.html#add43c2d818748d0ef0c5eca051dc7765", null ], + [ "sfc_anchor", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1PyCycle_1_1PyCycle.html#abd577dd0c97be86592d2ea35af36cd80", null ], + [ "sfc_anchor_conditions", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1PyCycle_1_1PyCycle.html#a3f6cedd6db5d7dc3e87b491de0ea361f", null ], + [ "sfc_anchor_scale", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1PyCycle_1_1PyCycle.html#a78a49a2980d9c1fafa52f014bd2efa32", null ], + [ "sfc_input_scale", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1PyCycle_1_1PyCycle.html#ac20a963a95db93d66d7839426f20d0dc", null ], + [ "sfc_rubber_scale", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1PyCycle_1_1PyCycle.html#a2a02ef81b882c6d6664e842f3844ad9c", null ], + [ "sfc_surrogate", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1PyCycle_1_1PyCycle.html#ac12291bf1cd7bd6390b0f317a8949113", null ], + [ "surrogate_type", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1PyCycle_1_1PyCycle.html#a34f8a5b4f94164390f13ef55f9ef164a", null ], + [ "tag", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1PyCycle_1_1PyCycle.html#acccb120b145c3dc2d4d7da3d2ea32cb5", null ], + [ "thrust_anchor", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1PyCycle_1_1PyCycle.html#a2bb0145f8091ced5d5aa8e7568a3ffba", null ], + [ "thrust_anchor_conditions", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1PyCycle_1_1PyCycle.html#a696146a17b3580999c23ecab1adcaa4f", null ], + [ "thrust_anchor_scale", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1PyCycle_1_1PyCycle.html#a1067889138e26236bdebe755a1807e4d", null ], + [ "thrust_input_scale", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1PyCycle_1_1PyCycle.html#a2a7080250d43425ac5aa1020bfa8164e", null ], + [ "thrust_surrogate", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1PyCycle_1_1PyCycle.html#ae3e83d6ed231cab191daf52f1ce470f5", null ], + [ "use_extended_surrogate", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1PyCycle_1_1PyCycle.html#a3486696470154cb5ea31c67360b01639", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1PyCycle_1_1PyCycle.png b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1PyCycle_1_1PyCycle.png new file mode 100644 index 00000000..97678cae Binary files /dev/null and b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1PyCycle_1_1PyCycle.png differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ramjet_1_1Ramjet-members.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ramjet_1_1Ramjet-members.html index a49a6602..e9812085 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ramjet_1_1Ramjet-members.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ramjet_1_1Ramjet-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -98,39 +105,21 @@

This is the complete list of members for SUAVE.Components.Energy.Networks.Ramjet.Ramjet, including all inherited members.

- - - - - - - - - - - - - - - - - - - + + + + + + + + + + + - - - - - - - - - - - - - + + +
__defaults__(self) (defined in SUAVE.Components.Energy.Networks.Ramjet.Ramjet)SUAVE.Components.Energy.Networks.Ramjet.Ramjet
combustor (defined in SUAVE.Components.Energy.Networks.Ramjet.Ramjet)SUAVE.Components.Energy.Networks.Ramjet.Ramjetstatic
conditionsSUAVE.Components.Energy.Networks.Ramjet.Ramjetstatic
core_nozzle (defined in SUAVE.Components.Energy.Networks.Ramjet.Ramjet)SUAVE.Components.Energy.Networks.Ramjet.Ramjetstatic
engine_length (defined in SUAVE.Components.Energy.Networks.Ramjet.Ramjet)SUAVE.Components.Energy.Networks.Ramjet.Ramjetstatic
evaluate_thrust(self, state) (defined in SUAVE.Components.Energy.Networks.Ramjet.Ramjet)SUAVE.Components.Energy.Networks.Ramjet.Ramjet
F (defined in SUAVE.Components.Energy.Networks.Ramjet.Ramjet)SUAVE.Components.Energy.Networks.Ramjet.Ramjetstatic
F (defined in SUAVE.Components.Energy.Networks.Ramjet.Ramjet)SUAVE.Components.Energy.Networks.Ramjet.Ramjetstatic
F_vec (defined in SUAVE.Components.Energy.Networks.Ramjet.Ramjet)SUAVE.Components.Energy.Networks.Ramjet.Ramjetstatic
flow_through_core (defined in SUAVE.Components.Energy.Networks.Ramjet.Ramjet)SUAVE.Components.Energy.Networks.Ramjet.Ramjetstatic
flow_through_fan (defined in SUAVE.Components.Energy.Networks.Ramjet.Ramjet)SUAVE.Components.Energy.Networks.Ramjet.Ramjetstatic
fuel_to_air_ratio (defined in SUAVE.Components.Energy.Networks.Ramjet.Ramjet)SUAVE.Components.Energy.Networks.Ramjet.Ramjetstatic
inlet_nozzle (defined in SUAVE.Components.Energy.Networks.Ramjet.Ramjet)SUAVE.Components.Energy.Networks.Ramjet.Ramjetstatic
inputs (defined in SUAVE.Components.Energy.Networks.Ramjet.Ramjet)SUAVE.Components.Energy.Networks.Ramjet.Ramjetstatic
Isp (defined in SUAVE.Components.Energy.Networks.Ramjet.Ramjet)SUAVE.Components.Energy.Networks.Ramjet.Ramjetstatic
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
mdot (defined in SUAVE.Components.Energy.Networks.Ramjet.Ramjet)SUAVE.Components.Energy.Networks.Ramjet.Ramjetstatic
nacelle_diameter (defined in SUAVE.Components.Energy.Networks.Ramjet.Ramjet)SUAVE.Components.Energy.Networks.Ramjet.Ramjetstatic
number_of_engines (defined in SUAVE.Components.Energy.Networks.Ramjet.Ramjet)SUAVE.Components.Energy.Networks.Ramjet.Ramjetstatic
__defaults__(self)SUAVE.Components.Energy.Networks.Ramjet.Ramjet
areas (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
engine_length (defined in SUAVE.Components.Energy.Networks.Ramjet.Ramjet)SUAVE.Components.Energy.Networks.Ramjet.Ramjet
evaluate_thrust(self, state)SUAVE.Components.Energy.Networks.Ramjet.Ramjet
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
generative_design_minimum (defined in SUAVE.Components.Energy.Networks.Ramjet.Ramjet)SUAVE.Components.Energy.Networks.Ramjet.Ramjet
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
non_dimensional_origin (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
number_of_engines (defined in SUAVE.Components.Energy.Networks.Ramjet.Ramjet)SUAVE.Components.Energy.Networks.Ramjet.Ramjet
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
output_power (defined in SUAVE.Components.Energy.Networks.Ramjet.Ramjet)SUAVE.Components.Energy.Networks.Ramjet.Ramjetstatic
ram (defined in SUAVE.Components.Energy.Networks.Ramjet.Ramjet)SUAVE.Components.Energy.Networks.Ramjet.Ramjetstatic
results (defined in SUAVE.Components.Energy.Networks.Ramjet.Ramjet)SUAVE.Components.Energy.Networks.Ramjet.Ramjetstatic
size(self, state)SUAVE.Components.Energy.Networks.Ramjet.Ramjet
specific_impulse (defined in SUAVE.Components.Energy.Networks.Ramjet.Ramjet)SUAVE.Components.Energy.Networks.Ramjet.Ramjetstatic
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tagSUAVE.Components.Energy.Networks.Ramjet.Ramjetstatic
thrust (defined in SUAVE.Components.Energy.Networks.Ramjet.Ramjet)SUAVE.Components.Energy.Networks.Ramjet.Ramjetstatic
thrust_force_vector (defined in SUAVE.Components.Energy.Networks.Ramjet.Ramjet)SUAVE.Components.Energy.Networks.Ramjet.Ramjetstatic
total_pressure_reference (defined in SUAVE.Components.Energy.Networks.Ramjet.Ramjet)SUAVE.Components.Energy.Networks.Ramjet.Ramjetstatic
total_temperature_reference (defined in SUAVE.Components.Energy.Networks.Ramjet.Ramjet)SUAVE.Components.Energy.Networks.Ramjet.Ramjetstatic
vehicle_mass_rate (defined in SUAVE.Components.Energy.Networks.Ramjet.Ramjet)SUAVE.Components.Energy.Networks.Ramjet.Ramjetstatic
working_fluid (defined in SUAVE.Components.Energy.Networks.Ramjet.Ramjet)SUAVE.Components.Energy.Networks.Ramjet.Ramjetstatic
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Energy.Networks.Ramjet.Ramjet)SUAVE.Components.Energy.Networks.Ramjet.Ramjet
wing_mounted (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
@@ -138,7 +127,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ramjet_1_1Ramjet.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ramjet_1_1Ramjet.html index 6a21ccb3..45879335 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ramjet_1_1Ramjet.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ramjet_1_1Ramjet.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Components.Energy.Networks.Ramjet.Ramjet Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -93,7 +100,7 @@
SUAVE.Components.Energy.Networks.Ramjet.Ramjet Class Reference
@@ -105,120 +112,55 @@
-SUAVE.Components.Propulsors.Propulsor.Propulsor +SUAVE.Components.Energy.Networks.Network.Network SUAVE.Components.Physical_Component.Physical_Component SUAVE.Components.Component.Component - -
+ +
- + - + - - - - - - - - - - -

Public Member Functions

-def __defaults__ (self)
def __defaults__ (self)
 
-def evaluate_thrust (self, state)
def evaluate_thrust (self, state)
 
def size (self, state)
 
- Public Member Functions inherited from SUAVE.Components.Propulsors.Propulsor.Propulsor
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
- - + + +  - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Static Public Attributes

 tag

+Public Attributes

tag
 
number_of_engines = self.number_of_engines
number_of_engines
 
nacelle_diameter
 
 engine_length
 
 conditions = state.conditions
 
ram = self.ram
 
inlet_nozzle = self.inlet_nozzle
 
combustor = self.combustor
 
core_nozzle = self.core_nozzle
 
thrust = self.thrust
 
working_fluid
 
inputs
 
total_temperature_reference
 
total_pressure_reference
 
fuel_to_air_ratio
 
flow_through_core
 
flow_through_fan
 
F = thrust.outputs.thrust*[1,0,0]
 
mdot = thrust.outputs.fuel_flow_rate
 
Isp = thrust.outputs.specific_impulse
 
output_power = thrust.outputs.power
 
-float F_vec = conditions.ones_row(3) * 0.0
 
-float F = F_vec
 
results = Data()
 
thrust_force_vector
 
vehicle_mass_rate
 
specific_impulse
 
- - - + + + - + + + + + + + + + + + + + @@ -239,6 +181,15 @@ + + + + + +

-Additional Inherited Members

- Public Attributes inherited from SUAVE.Components.Propulsors.Propulsor.Propulsor
+
generative_design_minimum
 
- Public Attributes inherited from SUAVE.Components.Energy.Networks.Network.Network
 tag
 
 
generative_design_max_per_vehicle
 
non_dimensional_origin
 
number_of_engines
 
engine_length
 
wing_mounted
 
areas
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
 tag
 origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 

Detailed Description

This is a ramjet for supersonic flight.
@@ -250,71 +201,22 @@
     Most of the componentes come from this book:
     https://web.stanford.edu/~cantwell/AA283_Course_Material/AA283_Course_Notes/
 

Member Function Documentation

- -

◆ size()

+ +

◆ __defaults__()

- + - - - - - - - - - + - -
def SUAVE.Components.Energy.Networks.Ramjet.Ramjet.size def SUAVE.Components.Energy.Networks.Ramjet.Ramjet.__defaults__ (  self,
 state 
self) )
-
Size the ramjet
-
-    Assumptions:
-    None
-
-    Source:
-    N/A
-
-    Inputs:
-    State [state()]
-
-    Outputs:
-    None
-
-    Properties Used:
-    N/A
-
-
-
-

Member Data Documentation

- -

◆ conditions

- -
-
- - - - - -
- - - - -
SUAVE.Components.Energy.Networks.Ramjet.Ramjet.conditions = state.conditions
-
-static
-
-
Calculate thrust given the current state of the vehicle
+
This sets the default values for the network to function.
 
 Assumptions:
 None
@@ -323,45 +225,44 @@ 

SUAVE.Components.Energy.Networks.Network.Network.

+

- -

◆ tag

+ +

◆ evaluate_thrust()

- - - - - -
- + + + + + + + + + + + + + + +
SUAVE.Components.Energy.Networks.Ramjet.Ramjet.tagdef SUAVE.Components.Energy.Networks.Ramjet.Ramjet.evaluate_thrust ( self,
 state 
)
-
-static
-
This sets the default values for the network to function.
+
Calculate thrust given the current state of the vehicle
 
     Assumptions:
     None
@@ -370,14 +271,22 @@ 

SUAVE + doxygen 1.8.15

diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ramjet_1_1Ramjet.js b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ramjet_1_1Ramjet.js index 880b278b..fb11e669 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ramjet_1_1Ramjet.js +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ramjet_1_1Ramjet.js @@ -2,5 +2,8 @@ var classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ramjet_1_1Ramjet = [ [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ramjet_1_1Ramjet.html#a6a768c023b410be59f9b8fb017d56fa0", null ], [ "evaluate_thrust", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ramjet_1_1Ramjet.html#a38173d1141d4e1e6f53f44c812cb8bc5", null ], - [ "size", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ramjet_1_1Ramjet.html#aa4932e67dca52aaad7e8cb37d651029f", null ] + [ "engine_length", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ramjet_1_1Ramjet.html#abe9a20679a2d34fe28d856e7a7c89bdc", null ], + [ "generative_design_minimum", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ramjet_1_1Ramjet.html#aae835ef5f84eb1a1d1945aa69e0cbe7c", null ], + [ "number_of_engines", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ramjet_1_1Ramjet.html#adf0d1e626acac3fb0e4277a4b94cf3a0", null ], + [ "tag", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ramjet_1_1Ramjet.html#a7777970b206874a28129f9ad109a3ea1", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ramjet_1_1Ramjet.png b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ramjet_1_1Ramjet.png index 3e17ff12..83b3829d 100644 Binary files a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ramjet_1_1Ramjet.png and b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Ramjet_1_1Ramjet.png differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Scramjet_1_1Scramjet-members.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Scramjet_1_1Scramjet-members.html new file mode 100644 index 00000000..5e7e6c46 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Scramjet_1_1Scramjet-members.html @@ -0,0 +1,134 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
SUAVE.Components.Energy.Networks.Scramjet.Scramjet Member List
+
+
+ +

This is the complete list of members for SUAVE.Components.Energy.Networks.Scramjet.Scramjet, including all inherited members.

+ + + + + + + + + + + + + + + + +
__defaults__(self)SUAVE.Components.Energy.Networks.Scramjet.Scramjet
areas (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
engine_length (defined in SUAVE.Components.Energy.Networks.Scramjet.Scramjet)SUAVE.Components.Energy.Networks.Scramjet.Scramjet
evaluate_thrust(self, state)SUAVE.Components.Energy.Networks.Scramjet.Scramjet
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
generative_design_minimum (defined in SUAVE.Components.Energy.Networks.Scramjet.Scramjet)SUAVE.Components.Energy.Networks.Scramjet.Scramjet
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
non_dimensional_origin (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
number_of_engines (defined in SUAVE.Components.Energy.Networks.Scramjet.Scramjet)SUAVE.Components.Energy.Networks.Scramjet.Scramjet
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Energy.Networks.Scramjet.Scramjet)SUAVE.Components.Energy.Networks.Scramjet.Scramjet
wing_mounted (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Scramjet_1_1Scramjet.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Scramjet_1_1Scramjet.html new file mode 100644 index 00000000..a3c63060 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Scramjet_1_1Scramjet.html @@ -0,0 +1,319 @@ + + + + + + + +SUAVE: SUAVE.Components.Energy.Networks.Scramjet.Scramjet Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Components.Energy.Networks.Scramjet.Scramjet Class Reference
+
+
+
+Inheritance diagram for SUAVE.Components.Energy.Networks.Scramjet.Scramjet:
+
+
+ + +SUAVE.Components.Energy.Networks.Network.Network +SUAVE.Components.Physical_Component.Physical_Component +SUAVE.Components.Component.Component + +
+ + + + + + +

+Public Member Functions

def __defaults__ (self)
 
def evaluate_thrust (self, state)
 
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Attributes

tag
 
number_of_engines
 
engine_length
 
generative_design_minimum
 
- Public Attributes inherited from SUAVE.Components.Energy.Networks.Network.Network
tag
 
generative_design_max_per_vehicle
 
non_dimensional_origin
 
number_of_engines
 
engine_length
 
wing_mounted
 
areas
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 
+

Detailed Description

+
This is a scramjet for hypersonic flight. 
+
+    Assumptions: 
+    Currently implements Stream Function Method
+    Combustion, Thermochemical Properties are estimated (HAP in below reference unavailable)
+    Assumes no spillage drag at the momement
+    Shock-BL Interaction negected
+    
+    Source: 
+    Most of the componentes come from this book: 
+    Heiser, William H., Pratt, D. T., Daley, D. H., and Unmeel, B. M., 
+    "Hypersonic Airbreathing Propulsion", 1994 
+    Chapter 4 - pgs. 175-180
+

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Components.Energy.Networks.Scramjet.Scramjet.__defaults__ ( self)
+
+
This sets the default values for the network to function. 
+
+    Assumptions: 
+    None 
+
+    Source: 
+    N/A 
+
+    Inputs: 
+    None 
+
+    Outputs: 
+    None 
+
+    Properties Used: 
+    N/A 
+
+

Reimplemented from SUAVE.Components.Energy.Networks.Network.Network.

+ +
+
+ +

◆ evaluate_thrust()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Components.Energy.Networks.Scramjet.Scramjet.evaluate_thrust ( self,
 state 
)
+
+
Calculate thrust given the current state of the vehicle 
+
+Assumptions: 
+None 
+
+Source: 
+N/A 
+
+Inputs: 
+state [state()] 
+
+Outputs: 
+results.thrust_force_vector                   [N] 
+results.vehicle_mass_rate                     [kg/s] 
+
+conditions.noise.sources.scramjets:
+core: 
+exit_static_temperature                  [K]  
+exit_static_pressure                     [K]  
+exit_stagnation_temperature              [K]  
+exit_stagnation_pressure                 [Pa]  
+exit_velocity                            [m/s]  
+fan: 
+exit_static_temperature                  [K]   
+exit_static_pressure                     [K]  
+exit_stagnation_temperature              [K]  
+exit_stagnation_pressure                 [Pa]  
+exit_velocity                            [m/s]  
+
+Properties Used: 
+Defaulted values 
+
+
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Energy/Networks/Scramjet.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Scramjet_1_1Scramjet.js b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Scramjet_1_1Scramjet.js new file mode 100644 index 00000000..6e384c21 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Scramjet_1_1Scramjet.js @@ -0,0 +1,9 @@ +var classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Scramjet_1_1Scramjet = +[ + [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Scramjet_1_1Scramjet.html#a947650c48aa553bbde16cb6dfb2f8b13", null ], + [ "evaluate_thrust", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Scramjet_1_1Scramjet.html#ab529a210b3acae885a9c63afc07e8d36", null ], + [ "engine_length", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Scramjet_1_1Scramjet.html#a29aaf2ac4ea65d6247b01d5bb4b00b34", null ], + [ "generative_design_minimum", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Scramjet_1_1Scramjet.html#ae9c91ec74f2bd202fd2c19b375b30ce4", null ], + [ "number_of_engines", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Scramjet_1_1Scramjet.html#a10ac6137b9e8a9af01398661c1f2c5b7", null ], + [ "tag", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Scramjet_1_1Scramjet.html#a49756d7506e802ba0b68872da75189cb", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Scramjet_1_1Scramjet.png b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Scramjet_1_1Scramjet.png new file mode 100644 index 00000000..be8208be Binary files /dev/null and b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Scramjet_1_1Scramjet.png differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Serial__Hybrid__Ducted__Fan_1_1Serial__Hybrid__Ducted__Fan-members.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Serial__Hybrid__Ducted__Fan_1_1Serial__Hybrid__Ducted__Fan-members.html new file mode 100644 index 00000000..fe1357dc --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Serial__Hybrid__Ducted__Fan_1_1Serial__Hybrid__Ducted__Fan-members.html @@ -0,0 +1,142 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
SUAVE.Components.Energy.Networks.Serial_Hybrid_Ducted_Fan.Serial_Hybrid_Ducted_Fan Member List
+
+
+ +

This is the complete list of members for SUAVE.Components.Energy.Networks.Serial_Hybrid_Ducted_Fan.Serial_Hybrid_Ducted_Fan, including all inherited members.

+ + + + + + + + + + + + + + + + + + + + + + + + +
__defaults__(self)SUAVE.Components.Energy.Networks.Serial_Hybrid_Ducted_Fan.Serial_Hybrid_Ducted_Fan
areas (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
avionics (defined in SUAVE.Components.Energy.Networks.Serial_Hybrid_Ducted_Fan.Serial_Hybrid_Ducted_Fan)SUAVE.Components.Energy.Networks.Serial_Hybrid_Ducted_Fan.Serial_Hybrid_Ducted_Fan
battery (defined in SUAVE.Components.Energy.Networks.Serial_Hybrid_Ducted_Fan.Serial_Hybrid_Ducted_Fan)SUAVE.Components.Energy.Networks.Serial_Hybrid_Ducted_Fan.Serial_Hybrid_Ducted_Fan
engine_length (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
esc (defined in SUAVE.Components.Energy.Networks.Serial_Hybrid_Ducted_Fan.Serial_Hybrid_Ducted_Fan)SUAVE.Components.Energy.Networks.Serial_Hybrid_Ducted_Fan.Serial_Hybrid_Ducted_Fan
evaluate_thrust(self, state)SUAVE.Components.Energy.Networks.Serial_Hybrid_Ducted_Fan.Serial_Hybrid_Ducted_Fan
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generator (defined in SUAVE.Components.Energy.Networks.Serial_Hybrid_Ducted_Fan.Serial_Hybrid_Ducted_Fan)SUAVE.Components.Energy.Networks.Serial_Hybrid_Ducted_Fan.Serial_Hybrid_Ducted_Fan
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
motor_efficiency (defined in SUAVE.Components.Energy.Networks.Serial_Hybrid_Ducted_Fan.Serial_Hybrid_Ducted_Fan)SUAVE.Components.Energy.Networks.Serial_Hybrid_Ducted_Fan.Serial_Hybrid_Ducted_Fan
non_dimensional_origin (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
number_of_engines (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
OpenVSP_flow_through (defined in SUAVE.Components.Energy.Networks.Serial_Hybrid_Ducted_Fan.Serial_Hybrid_Ducted_Fan)SUAVE.Components.Energy.Networks.Serial_Hybrid_Ducted_Fan.Serial_Hybrid_Ducted_Fan
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
payload (defined in SUAVE.Components.Energy.Networks.Serial_Hybrid_Ducted_Fan.Serial_Hybrid_Ducted_Fan)SUAVE.Components.Energy.Networks.Serial_Hybrid_Ducted_Fan.Serial_Hybrid_Ducted_Fan
propulsor (defined in SUAVE.Components.Energy.Networks.Serial_Hybrid_Ducted_Fan.Serial_Hybrid_Ducted_Fan)SUAVE.Components.Energy.Networks.Serial_Hybrid_Ducted_Fan.Serial_Hybrid_Ducted_Fan
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Energy.Networks.Serial_Hybrid_Ducted_Fan.Serial_Hybrid_Ducted_Fan)SUAVE.Components.Energy.Networks.Serial_Hybrid_Ducted_Fan.Serial_Hybrid_Ducted_Fan
voltage (defined in SUAVE.Components.Energy.Networks.Serial_Hybrid_Ducted_Fan.Serial_Hybrid_Ducted_Fan)SUAVE.Components.Energy.Networks.Serial_Hybrid_Ducted_Fan.Serial_Hybrid_Ducted_Fan
wing_mounted (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Serial__Hybrid__Ducted__Fan_1_1Serial__Hybrid__Ducted__Fan.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Serial__Hybrid__Ducted__Fan_1_1Serial__Hybrid__Ducted__Fan.html new file mode 100644 index 00000000..674703ef --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Serial__Hybrid__Ducted__Fan_1_1Serial__Hybrid__Ducted__Fan.html @@ -0,0 +1,321 @@ + + + + + + + +SUAVE: SUAVE.Components.Energy.Networks.Serial_Hybrid_Ducted_Fan.Serial_Hybrid_Ducted_Fan Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Components.Energy.Networks.Serial_Hybrid_Ducted_Fan.Serial_Hybrid_Ducted_Fan Class Reference
+
+
+
+Inheritance diagram for SUAVE.Components.Energy.Networks.Serial_Hybrid_Ducted_Fan.Serial_Hybrid_Ducted_Fan:
+
+
+ + +SUAVE.Components.Energy.Networks.Network.Network +SUAVE.Components.Physical_Component.Physical_Component +SUAVE.Components.Component.Component + +
+ + + + + + +

+Public Member Functions

def __defaults__ (self)
 
def evaluate_thrust (self, state)
 
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Attributes

propulsor
 
battery
 
motor_efficiency
 
esc
 
avionics
 
payload
 
voltage
 
generator
 
tag
 
OpenVSP_flow_through
 
- Public Attributes inherited from SUAVE.Components.Energy.Networks.Network.Network
tag
 
generative_design_max_per_vehicle
 
non_dimensional_origin
 
number_of_engines
 
engine_length
 
wing_mounted
 
areas
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 
+

Detailed Description

+
Connects a generator to a battery to a ducted fan, with assumed motor & generator efficiencies
+
+    Assumptions:
+    None
+    
+    Source:
+    None
+

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Components.Energy.Networks.Serial_Hybrid_Ducted_Fan.Serial_Hybrid_Ducted_Fan.__defaults__ ( self)
+
+
This sets the default values for the network to function.
+    This network operates slightly different than most as it attaches a propulsor to the net.
+    
+    Assumptions:
+    None
+
+    Source:
+    N/A
+    
+    Inputs:
+    None
+    
+    Outputs:
+    None
+    
+    Properties Used:
+    N/A
+
+

Reimplemented from SUAVE.Components.Energy.Networks.Network.Network.

+ +
+
+ +

◆ evaluate_thrust()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Components.Energy.Networks.Serial_Hybrid_Ducted_Fan.Serial_Hybrid_Ducted_Fan.evaluate_thrust ( self,
 state 
)
+
+
Calculate thrust given the current state of the vehicle
+    
+    Assumptions:
+    Constant mass batteries
+    A DC distribution architecture  with no bus loses
+    DC motor
+    ESC input voltage is constant at max battery voltage
+    
+    Source:
+    N/A
+    
+    Inputs:
+    state [state()]
+    
+    Outputs:
+    results.thrust_force_vector [newtons]
+    results.vehicle_mass_rate   [kg/s]
+    
+    Properties Used:
+    Defaulted values
+
+
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Energy/Networks/Serial_Hybrid_Ducted_Fan.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Serial__Hybrid__Ducted__Fan_1_1Serial__Hybrid__Ducted__Fan.js b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Serial__Hybrid__Ducted__Fan_1_1Serial__Hybrid__Ducted__Fan.js new file mode 100644 index 00000000..fcc98f11 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Serial__Hybrid__Ducted__Fan_1_1Serial__Hybrid__Ducted__Fan.js @@ -0,0 +1,15 @@ +var classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Serial__Hybrid__Ducted__Fan_1_1Serial__Hybrid__Ducted__Fan = +[ + [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Serial__Hybrid__Ducted__Fan_1_1Serial__Hybrid__Ducted__Fan.html#a6e07671b349bb7d3ccfe35636dda737d", null ], + [ "evaluate_thrust", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Serial__Hybrid__Ducted__Fan_1_1Serial__Hybrid__Ducted__Fan.html#add8f44a207a51b58b16de44e6715d5d9", null ], + [ "avionics", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Serial__Hybrid__Ducted__Fan_1_1Serial__Hybrid__Ducted__Fan.html#a97b6e47655f29f15e4c438443d91d4fa", null ], + [ "battery", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Serial__Hybrid__Ducted__Fan_1_1Serial__Hybrid__Ducted__Fan.html#ab06af99cb1f399d4e15e9887549f021c", null ], + [ "esc", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Serial__Hybrid__Ducted__Fan_1_1Serial__Hybrid__Ducted__Fan.html#a816815c22c01fbe2962440c76abdf3fe", null ], + [ "generator", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Serial__Hybrid__Ducted__Fan_1_1Serial__Hybrid__Ducted__Fan.html#a78bd91f7ddf77a434f06c13ebfa2a155", null ], + [ "motor_efficiency", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Serial__Hybrid__Ducted__Fan_1_1Serial__Hybrid__Ducted__Fan.html#af4516330c5806e007c9748e2a409348b", null ], + [ "OpenVSP_flow_through", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Serial__Hybrid__Ducted__Fan_1_1Serial__Hybrid__Ducted__Fan.html#a522b007ad6eaadf47722021aa3bdf4e8", null ], + [ "payload", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Serial__Hybrid__Ducted__Fan_1_1Serial__Hybrid__Ducted__Fan.html#a36dabf8b33efc61430d786d3f52cf26a", null ], + [ "propulsor", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Serial__Hybrid__Ducted__Fan_1_1Serial__Hybrid__Ducted__Fan.html#a93b5a69f989d1e2601466ac8f8f2bd3c", null ], + [ "tag", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Serial__Hybrid__Ducted__Fan_1_1Serial__Hybrid__Ducted__Fan.html#a5109418807eaf4e2328f59ce1777287e", null ], + [ "voltage", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Serial__Hybrid__Ducted__Fan_1_1Serial__Hybrid__Ducted__Fan.html#ae5624593405f97c5c60bf414b8fac44e", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Serial__Hybrid__Ducted__Fan_1_1Serial__Hybrid__Ducted__Fan.png b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Serial__Hybrid__Ducted__Fan_1_1Serial__Hybrid__Ducted__Fan.png new file mode 100644 index 00000000..cdc30133 Binary files /dev/null and b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Serial__Hybrid__Ducted__Fan_1_1Serial__Hybrid__Ducted__Fan.png differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar-members.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar-members.html index bbf0a8c7..f6668f26 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar-members.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@
- +
@@ -73,7 +78,9 @@
@@ -99,25 +106,34 @@

This is the complete list of members for SUAVE.Components.Energy.Networks.Solar.Solar, including all inherited members.

+ + - - - - - - - - - - - - - - + + + + + + + + + + + + + + + + + + + + +
__defaults__(self)SUAVE.Components.Energy.Networks.Solar.Solar
add_unknowns_and_residuals_to_segment(self, segment, initial_power_coefficient=0.005)SUAVE.Components.Energy.Networks.Solar.Solar
areas (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
avionics (defined in SUAVE.Components.Energy.Networks.Solar.Solar)SUAVE.Components.Energy.Networks.Solar.Solar
battery (defined in SUAVE.Components.Energy.Networks.Solar.Solar)SUAVE.Components.Energy.Networks.Solar.Solar
engine_length (defined in SUAVE.Components.Energy.Networks.Solar.Solar)SUAVE.Components.Energy.Networks.Solar.Solar
esc (defined in SUAVE.Components.Energy.Networks.Solar.Solar)SUAVE.Components.Energy.Networks.Solar.Solar
evaluate_thrust(self, state)SUAVE.Components.Energy.Networks.Solar.Solar
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
motor (defined in SUAVE.Components.Energy.Networks.Solar.Solar)SUAVE.Components.Energy.Networks.Solar.Solar
nacelle_diameter (defined in SUAVE.Components.Energy.Networks.Solar.Solar)SUAVE.Components.Energy.Networks.Solar.Solar
number_of_engines (defined in SUAVE.Components.Energy.Networks.Solar.Solar)SUAVE.Components.Energy.Networks.Solar.Solar
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
payload (defined in SUAVE.Components.Energy.Networks.Solar.Solar)SUAVE.Components.Energy.Networks.Solar.Solar
propeller (defined in SUAVE.Components.Energy.Networks.Solar.Solar)SUAVE.Components.Energy.Networks.Solar.Solar
residuals(self, segment, state)SUAVE.Components.Energy.Networks.Solar.Solar
solar_flux (defined in SUAVE.Components.Energy.Networks.Solar.Solar)SUAVE.Components.Energy.Networks.Solar.Solar
solar_logic (defined in SUAVE.Components.Energy.Networks.Solar.Solar)SUAVE.Components.Energy.Networks.Solar.Solar
solar_panel (defined in SUAVE.Components.Energy.Networks.Solar.Solar)SUAVE.Components.Energy.Networks.Solar.Solar
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Energy.Networks.Solar.Solar)SUAVE.Components.Energy.Networks.Solar.Solar
unpack_unknowns(self, segment, state)SUAVE.Components.Energy.Networks.Solar.Solar
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
generative_design_minimum (defined in SUAVE.Components.Energy.Networks.Solar.Solar)SUAVE.Components.Energy.Networks.Solar.Solar
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
identical_propellers (defined in SUAVE.Components.Energy.Networks.Solar.Solar)SUAVE.Components.Energy.Networks.Solar.Solar
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
motors (defined in SUAVE.Components.Energy.Networks.Solar.Solar)SUAVE.Components.Energy.Networks.Solar.Solar
non_dimensional_origin (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
number_of_engines (defined in SUAVE.Components.Energy.Networks.Solar.Solar)SUAVE.Components.Energy.Networks.Solar.Solar
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
payload (defined in SUAVE.Components.Energy.Networks.Solar.Solar)SUAVE.Components.Energy.Networks.Solar.Solar
propellers (defined in SUAVE.Components.Energy.Networks.Solar.Solar)SUAVE.Components.Energy.Networks.Solar.Solar
residuals(self, segment)SUAVE.Components.Energy.Networks.Solar.Solar
solar_flux (defined in SUAVE.Components.Energy.Networks.Solar.Solar)SUAVE.Components.Energy.Networks.Solar.Solar
solar_logic (defined in SUAVE.Components.Energy.Networks.Solar.Solar)SUAVE.Components.Energy.Networks.Solar.Solar
solar_panel (defined in SUAVE.Components.Energy.Networks.Solar.Solar)SUAVE.Components.Energy.Networks.Solar.Solar
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Energy.Networks.Solar.Solar)SUAVE.Components.Energy.Networks.Solar.Solar
unpack_unknowns(self, segment)SUAVE.Components.Energy.Networks.Solar.Solar
use_surrogate (defined in SUAVE.Components.Energy.Networks.Solar.Solar)SUAVE.Components.Energy.Networks.Solar.Solar
wing_mounted (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
@@ -125,7 +141,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar.html index 89838893..1620ae35 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Components.Energy.Networks.Solar.Solar Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -105,11 +112,11 @@
-SUAVE.Components.Propulsors.Propulsor.Propulsor +SUAVE.Components.Energy.Networks.Network.Network SUAVE.Components.Physical_Component.Physical_Component SUAVE.Components.Component.Component - -
+ + @@ -117,19 +124,12 @@ - - - - - - - - - - - - - + + + + + +

Public Member Functions

 
def evaluate_thrust (self, state)
 
def unpack_unknowns (self, segment, state)
 
def residuals (self, segment, state)
 
- Public Member Functions inherited from SUAVE.Components.Propulsors.Propulsor.Propulsor
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
def unpack_unknowns (self, segment)
 
def residuals (self, segment)
 
def add_unknowns_and_residuals_to_segment (self, segment, initial_power_coefficient=0.005)
 
@@ -139,12 +139,12 @@ - - - - + + + + @@ -160,9 +160,6 @@ - - @@ -172,10 +169,37 @@ - - + + + + + + + - + + + + + + + + + + + + + @@ -196,6 +220,15 @@ + + + + + +

Public Attributes

 solar_panel
 
motor
 
propeller
 
motors
 
propellers
 
 esc
 
 battery
 
nacelle_diameter
 
 engine_length
 
 tag
 
- Public Attributes inherited from SUAVE.Components.Propulsors.Propulsor.Propulsor
+
use_surrogate
 
generative_design_minimum
 
identical_propellers
 
- Public Attributes inherited from SUAVE.Components.Energy.Networks.Network.Network
 tag
 
 
generative_design_max_per_vehicle
 
non_dimensional_origin
 
number_of_engines
 
engine_length
 
wing_mounted
 
areas
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
 tag
 origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 

Detailed Description

A solar powered system with batteries and maximum power point tracking.
@@ -240,6 +273,62 @@ 

SUAVE.Components.Energy.Networks.Network.Network.

+ +

+ + +

◆ add_unknowns_and_residuals_to_segment()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Components.Energy.Networks.Solar.Solar.add_unknowns_and_residuals_to_segment ( self,
 segment,
 initial_power_coefficient = 0.005 
)
+
+
This function sets up the information that the mission needs to run a mission segment using this network
+    
+    Assumptions:
+    None
+    
+    Source:
+    N/A
+    
+    Inputs:
+    segment
+    initial_voltage                   [v]
+    initial_power_coefficient         [float]s
+    
+    Outputs:
+    segment.state.unknowns.propeller_power_coefficient
+    segment.state.conditions.propulsion.propeller_motor_torque
+    segment.state.conditions.propulsion.propeller_torque   
+    
+    Properties Used:
+    N/A
+
@@ -285,7 +374,7 @@

-

◆ residuals()

+ +

◆ residuals()

@@ -311,13 +400,7 @@

  - segment, - - - - -   - state  + segment  @@ -347,8 +430,8 @@

-

◆ unpack_unknowns()

+ +

◆ unpack_unknowns()

diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar.js b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar.js index 9ee33118..e953c6d3 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar.js +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar.js @@ -1,20 +1,23 @@ var classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar = [ [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar.html#a1b845035b4dfa9e54c0487e6d9c1c55b", null ], + [ "add_unknowns_and_residuals_to_segment", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar.html#ada03f4553fc9422b599efdfdbd8e1bbc", null ], [ "evaluate_thrust", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar.html#a03837081f89d8b2f3e50455f44411e41", null ], - [ "residuals", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar.html#afc4852d79b60415d25511fc2a6bb1930", null ], - [ "unpack_unknowns", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar.html#a7d95eeb99fa7ca3bd14e4c5f833f09c8", null ], + [ "residuals", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar.html#aab86666a7580790e990512521b58e5da", null ], + [ "unpack_unknowns", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar.html#ad248090876d7a5f6246379b8c8b34a26", null ], [ "avionics", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar.html#a1f33f40e58f05ee58ed0669fe5302e72", null ], [ "battery", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar.html#ac16762f88873f88419a0d851b4d7c5f0", null ], [ "engine_length", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar.html#a9e7c3492cc016f11fd98c3a47317961f", null ], [ "esc", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar.html#a33cfb357ddf776d510b8501cdadfc777", null ], - [ "motor", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar.html#aaedcd0dd93c8c610bdfb6760269bf3a1", null ], - [ "nacelle_diameter", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar.html#a072998c85626b49f300270c8e4b5a8c9", null ], + [ "generative_design_minimum", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar.html#a6bceea89276535bd146105703912d348", null ], + [ "identical_propellers", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar.html#a67a5a544cf198ae0ab2cebdeeb2e184e", null ], + [ "motors", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar.html#ac87d85cf853eefe27f353fc14f2ef2bf", null ], [ "number_of_engines", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar.html#af9d3157b48236320e321b822a10427fb", null ], [ "payload", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar.html#ab2fe0fa4d19dc750a430fbd2d2c7fbd5", null ], - [ "propeller", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar.html#a9bfbd8f231fa46f7f693a7340556fb1a", null ], + [ "propellers", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar.html#a0bf2d8b2fe4123b40999de39a4b58357", null ], [ "solar_flux", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar.html#ad9c27f16e7457864328b37d4111abda0", null ], [ "solar_logic", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar.html#a70294c7d2ddd2f3b719e7777e9845d6b", null ], [ "solar_panel", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar.html#af1a064708a49ca2d7bb64912724e69b2", null ], - [ "tag", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar.html#a28f5aacd5ba78c3de21f5af4f4808f9b", null ] + [ "tag", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar.html#a28f5aacd5ba78c3de21f5af4f4808f9b", null ], + [ "use_surrogate", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar.html#ac34ffb60cd093e18d6309e402937af34", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar.png b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar.png index 63eb68b1..c9ad9dda 100644 Binary files a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar.png and b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar_1_1Solar.png differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar__Low__Fidelity_1_1Solar__Low__Fidelity-members.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar__Low__Fidelity_1_1Solar__Low__Fidelity-members.html index 98570406..17e3c6d2 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar__Low__Fidelity_1_1Solar__Low__Fidelity-members.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar__Low__Fidelity_1_1Solar__Low__Fidelity-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@
- +

@@ -73,7 +78,9 @@
@@ -99,14 +106,18 @@

This is the complete list of members for SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity, including all inherited members.

- - - - - + + + + + + + + + - + @@ -116,6 +127,7 @@ +
__defaults__(self)SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity
avionics (defined in SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity)SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity
battery (defined in SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity)SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity
engine_length (defined in SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity)SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity
esc (defined in SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity)SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity
evaluate_thrust(self, state)SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity
areas (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
avionics (defined in SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity)SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity
battery (defined in SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity)SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity
engine_length (defined in SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity)SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity
esc (defined in SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity)SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity
evaluate_thrust(self, state)SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
motor (defined in SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity)SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity
nacelle_dia (defined in SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity)SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity
non_dimensional_origin (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
number_of_engines (defined in SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity)SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
payload (defined in SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity)SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity
solar_panel (defined in SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity)SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity)SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity
wing_mounted (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
@@ -123,7 +135,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar__Low__Fidelity_1_1Solar__Low__Fidelity.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar__Low__Fidelity_1_1Solar__Low__Fidelity.html index c6c71d63..4c1ffa14 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar__Low__Fidelity_1_1Solar__Low__Fidelity.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar__Low__Fidelity_1_1Solar__Low__Fidelity.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -105,11 +112,11 @@
-SUAVE.Components.Propulsors.Propulsor.Propulsor +SUAVE.Components.Energy.Networks.Network.Network SUAVE.Components.Physical_Component.Physical_Component SUAVE.Components.Component.Component - -
+ + @@ -117,15 +124,6 @@ - - - - - - - - -

Public Member Functions

 
def evaluate_thrust (self, state)
 
- Public Member Functions inherited from SUAVE.Components.Propulsors.Propulsor.Propulsor
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
@@ -156,9 +154,6 @@ - - @@ -168,10 +163,28 @@ - - + - + + + + + + + + + + + + + @@ -192,6 +205,15 @@ + + + + + +

Public Attributes

 battery
 
nacelle_dia
 
 engine_length
 
 tag
 
- Public Attributes inherited from SUAVE.Components.Propulsors.Propulsor.Propulsor
+
- Public Attributes inherited from SUAVE.Components.Energy.Networks.Network.Network
 tag
 
 
generative_design_max_per_vehicle
 
non_dimensional_origin
 
number_of_engines
 
engine_length
 
wing_mounted
 
areas
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
 tag
 origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 

Detailed Description

A solar powered system with batteries and maximum power point tracking.
@@ -237,6 +259,8 @@ 

SUAVE.Components.Energy.Networks.Network.Network.

+

@@ -279,11 +303,11 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar__Low__Fidelity_1_1Solar__Low__Fidelity.js b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar__Low__Fidelity_1_1Solar__Low__Fidelity.js index fd41ef09..cfb3af8e 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar__Low__Fidelity_1_1Solar__Low__Fidelity.js +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar__Low__Fidelity_1_1Solar__Low__Fidelity.js @@ -7,7 +7,6 @@ var classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar__Low__Fidelity_1_1So [ "engine_length", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar__Low__Fidelity_1_1Solar__Low__Fidelity.html#ae59b65392146034a9b407394de7c336f", null ], [ "esc", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar__Low__Fidelity_1_1Solar__Low__Fidelity.html#ae7fc5861cb4a944129c9749270885b0e", null ], [ "motor", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar__Low__Fidelity_1_1Solar__Low__Fidelity.html#acae5bbd194cad986cfd52f880a22935f", null ], - [ "nacelle_dia", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar__Low__Fidelity_1_1Solar__Low__Fidelity.html#acc0224108fa8af8cf4f290ccb30c0272", null ], [ "number_of_engines", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar__Low__Fidelity_1_1Solar__Low__Fidelity.html#a4a5ad2f9600fa7bcd88310f7f972700e", null ], [ "payload", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar__Low__Fidelity_1_1Solar__Low__Fidelity.html#a233c717fad987512c42cb83c53e4c651", null ], [ "propeller", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar__Low__Fidelity_1_1Solar__Low__Fidelity.html#a8e2853156ffcf1aef68eb1108d852da4", null ], diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar__Low__Fidelity_1_1Solar__Low__Fidelity.png b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar__Low__Fidelity_1_1Solar__Low__Fidelity.png index 05054854..57635a7d 100644 Binary files a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar__Low__Fidelity_1_1Solar__Low__Fidelity.png and b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Solar__Low__Fidelity_1_1Solar__Low__Fidelity.png differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turboelectric__HTS__Ducted__Fan_1_1Turboelectric__HTS__Ducted__Fan-members.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turboelectric__HTS__Ducted__Fan_1_1Turboelectric__HTS__Ducted__Fan-members.html new file mode 100644 index 00000000..9eb06f08 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turboelectric__HTS__Ducted__Fan_1_1Turboelectric__HTS__Ducted__Fan-members.html @@ -0,0 +1,140 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
SUAVE.Components.Energy.Networks.Turboelectric_HTS_Ducted_Fan.Turboelectric_HTS_Ducted_Fan Member List
+
+
+ +

This is the complete list of members for SUAVE.Components.Energy.Networks.Turboelectric_HTS_Ducted_Fan.Turboelectric_HTS_Ducted_Fan, including all inherited members.

+ + + + + + + + + + + + + + + + + + + + + + +
__defaults__(self)SUAVE.Components.Energy.Networks.Turboelectric_HTS_Ducted_Fan.Turboelectric_HTS_Ducted_Fan
ambient_skin (defined in SUAVE.Components.Energy.Networks.Turboelectric_HTS_Ducted_Fan.Turboelectric_HTS_Ducted_Fan)SUAVE.Components.Energy.Networks.Turboelectric_HTS_Ducted_Fan.Turboelectric_HTS_Ducted_Fan
areas (defined in SUAVE.Components.Energy.Networks.Turboelectric_HTS_Ducted_Fan.Turboelectric_HTS_Ducted_Fan)SUAVE.Components.Energy.Networks.Turboelectric_HTS_Ducted_Fan.Turboelectric_HTS_Ducted_Fan
bypass_ratio (defined in SUAVE.Components.Energy.Networks.Turboelectric_HTS_Ducted_Fan.Turboelectric_HTS_Ducted_Fan)SUAVE.Components.Energy.Networks.Turboelectric_HTS_Ducted_Fan.Turboelectric_HTS_Ducted_Fan
cryogen_proportion (defined in SUAVE.Components.Energy.Networks.Turboelectric_HTS_Ducted_Fan.Turboelectric_HTS_Ducted_Fan)SUAVE.Components.Energy.Networks.Turboelectric_HTS_Ducted_Fan.Turboelectric_HTS_Ducted_Fan
engine_length (defined in SUAVE.Components.Energy.Networks.Turboelectric_HTS_Ducted_Fan.Turboelectric_HTS_Ducted_Fan)SUAVE.Components.Energy.Networks.Turboelectric_HTS_Ducted_Fan.Turboelectric_HTS_Ducted_Fan
evaluate_thrust(self, state)SUAVE.Components.Energy.Networks.Turboelectric_HTS_Ducted_Fan.Turboelectric_HTS_Ducted_Fan
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
has_additional_fuel_type (defined in SUAVE.Components.Energy.Networks.Turboelectric_HTS_Ducted_Fan.Turboelectric_HTS_Ducted_Fan)SUAVE.Components.Energy.Networks.Turboelectric_HTS_Ducted_Fan.Turboelectric_HTS_Ducted_Fan
leads (defined in SUAVE.Components.Energy.Networks.Turboelectric_HTS_Ducted_Fan.Turboelectric_HTS_Ducted_Fan)SUAVE.Components.Energy.Networks.Turboelectric_HTS_Ducted_Fan.Turboelectric_HTS_Ducted_Fan
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
non_dimensional_origin (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
number_of_engines (defined in SUAVE.Components.Energy.Networks.Turboelectric_HTS_Ducted_Fan.Turboelectric_HTS_Ducted_Fan)SUAVE.Components.Energy.Networks.Turboelectric_HTS_Ducted_Fan.Turboelectric_HTS_Ducted_Fan
number_of_powersupplies (defined in SUAVE.Components.Energy.Networks.Turboelectric_HTS_Ducted_Fan.Turboelectric_HTS_Ducted_Fan)SUAVE.Components.Energy.Networks.Turboelectric_HTS_Ducted_Fan.Turboelectric_HTS_Ducted_Fan
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
skin_temp (defined in SUAVE.Components.Energy.Networks.Turboelectric_HTS_Ducted_Fan.Turboelectric_HTS_Ducted_Fan)SUAVE.Components.Energy.Networks.Turboelectric_HTS_Ducted_Fan.Turboelectric_HTS_Ducted_Fan
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Energy.Networks.Turboelectric_HTS_Ducted_Fan.Turboelectric_HTS_Ducted_Fan)SUAVE.Components.Energy.Networks.Turboelectric_HTS_Ducted_Fan.Turboelectric_HTS_Ducted_Fan
wing_mounted (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turboelectric__HTS__Ducted__Fan_1_1Turboelectric__HTS__Ducted__Fan.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turboelectric__HTS__Ducted__Fan_1_1Turboelectric__HTS__Ducted__Fan.html new file mode 100644 index 00000000..f665fd79 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turboelectric__HTS__Ducted__Fan_1_1Turboelectric__HTS__Ducted__Fan.html @@ -0,0 +1,322 @@ + + + + + + + +SUAVE: SUAVE.Components.Energy.Networks.Turboelectric_HTS_Ducted_Fan.Turboelectric_HTS_Ducted_Fan Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Components.Energy.Networks.Turboelectric_HTS_Ducted_Fan.Turboelectric_HTS_Ducted_Fan Class Reference
+
+
+
+Inheritance diagram for SUAVE.Components.Energy.Networks.Turboelectric_HTS_Ducted_Fan.Turboelectric_HTS_Ducted_Fan:
+
+
+ + +SUAVE.Components.Energy.Networks.Network.Network +SUAVE.Components.Physical_Component.Physical_Component +SUAVE.Components.Component.Component + +
+ + + + + + +

+Public Member Functions

def __defaults__ (self)
 
def evaluate_thrust (self, state)
 
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Attributes

cryogen_proportion
 
has_additional_fuel_type
 
leads
 
number_of_engines
 
number_of_powersupplies
 
engine_length
 
bypass_ratio
 
areas
 
tag
 
ambient_skin
 
skin_temp
 
- Public Attributes inherited from SUAVE.Components.Energy.Networks.Network.Network
tag
 
generative_design_max_per_vehicle
 
non_dimensional_origin
 
number_of_engines
 
engine_length
 
wing_mounted
 
areas
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 
+

Detailed Description

+
A serial hybrid powertrain with partially superconducting propulsion motors where the superconducting field coils are energised by resistive current leads.
+
+    Assumptions:
+    None
+    
+    Source:
+    None
+

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Components.Energy.Networks.Turboelectric_HTS_Ducted_Fan.Turboelectric_HTS_Ducted_Fan.__defaults__ ( self)
+
+
This sets the default values for the network to function.
+    
+    Assumptions:
+    N/A
+    
+    Source:
+    N/A
+    
+    Inputs:
+    None
+    
+    Outputs:
+    None
+    
+    Properties Used:
+    N/A
+
+

Reimplemented from SUAVE.Components.Energy.Networks.Network.Network.

+ +
+
+ +

◆ evaluate_thrust()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Components.Energy.Networks.Turboelectric_HTS_Ducted_Fan.Turboelectric_HTS_Ducted_Fan.evaluate_thrust ( self,
 state 
)
+
+
Calculate thrust given the current state of the vehicle
+    
+    Assumptions:
+    None
+    
+    Source:
+    N/A
+    
+    Inputs:
+    state [state()]
+    
+    Outputs:
+    results.thrust_force_vector             [newtons]
+    results.vehicle_mass_rate               [kg/s]
+    results.vehicle_additional_fuel_rate    [kg/s]
+    results.vehicle_fuel_rate               [kg/s]
+    
+    Properties Used:
+    Defaulted values
+
+
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Energy/Networks/Turboelectric_HTS_Ducted_Fan.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turboelectric__HTS__Ducted__Fan_1_1Turboelectric__HTS__Ducted__Fan.js b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turboelectric__HTS__Ducted__Fan_1_1Turboelectric__HTS__Ducted__Fan.js new file mode 100644 index 00000000..999ad735 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turboelectric__HTS__Ducted__Fan_1_1Turboelectric__HTS__Ducted__Fan.js @@ -0,0 +1,16 @@ +var classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turboelectric__HTS__Ducted__Fan_1_1Turboelectric__HTS__Ducted__Fan = +[ + [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turboelectric__HTS__Ducted__Fan_1_1Turboelectric__HTS__Ducted__Fan.html#a0c60a605e062b9fea62e3369a5401772", null ], + [ "evaluate_thrust", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turboelectric__HTS__Ducted__Fan_1_1Turboelectric__HTS__Ducted__Fan.html#a8cd476e45727fc7a26ab0143a6324ab4", null ], + [ "ambient_skin", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turboelectric__HTS__Ducted__Fan_1_1Turboelectric__HTS__Ducted__Fan.html#a856d812d5835f911c1fc4c0934756550", null ], + [ "areas", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turboelectric__HTS__Ducted__Fan_1_1Turboelectric__HTS__Ducted__Fan.html#a17da6c772ea353bfd3489866ce04717c", null ], + [ "bypass_ratio", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turboelectric__HTS__Ducted__Fan_1_1Turboelectric__HTS__Ducted__Fan.html#a0bb2afa69065cbc649788ec16f714f56", null ], + [ "cryogen_proportion", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turboelectric__HTS__Ducted__Fan_1_1Turboelectric__HTS__Ducted__Fan.html#a185f7133eb47b8d0b669b9a5e5f93970", null ], + [ "engine_length", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turboelectric__HTS__Ducted__Fan_1_1Turboelectric__HTS__Ducted__Fan.html#a0853e52c3902be952f777df79bb95537", null ], + [ "has_additional_fuel_type", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turboelectric__HTS__Ducted__Fan_1_1Turboelectric__HTS__Ducted__Fan.html#a3da8b278abda6052c485a8c8dac15989", null ], + [ "leads", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turboelectric__HTS__Ducted__Fan_1_1Turboelectric__HTS__Ducted__Fan.html#ac5334c58803636077fc957f7dad316dd", null ], + [ "number_of_engines", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turboelectric__HTS__Ducted__Fan_1_1Turboelectric__HTS__Ducted__Fan.html#a3708a7aaed2ef24c421da27c53c6e9b0", null ], + [ "number_of_powersupplies", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turboelectric__HTS__Ducted__Fan_1_1Turboelectric__HTS__Ducted__Fan.html#ad513ab8b1efbbf45ee373eb11d0dda49", null ], + [ "skin_temp", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turboelectric__HTS__Ducted__Fan_1_1Turboelectric__HTS__Ducted__Fan.html#a8c7ef4eae15eb26e5980307c65e6723c", null ], + [ "tag", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turboelectric__HTS__Ducted__Fan_1_1Turboelectric__HTS__Ducted__Fan.html#a227f3987f1c9dd6dd2ff2d9ed6b980e6", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turboelectric__HTS__Ducted__Fan_1_1Turboelectric__HTS__Ducted__Fan.png b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turboelectric__HTS__Ducted__Fan_1_1Turboelectric__HTS__Ducted__Fan.png new file mode 100644 index 00000000..ce601207 Binary files /dev/null and b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turboelectric__HTS__Ducted__Fan_1_1Turboelectric__HTS__Ducted__Fan.png differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbofan_1_1Turbofan-members.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbofan_1_1Turbofan-members.html index e3aed2c4..85ec7a19 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbofan_1_1Turbofan-members.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbofan_1_1Turbofan-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -104,13 +111,22 @@ engine_length (defined in SUAVE.Components.Energy.Networks.Turbofan.Turbofan)SUAVE.Components.Energy.Networks.Turbofan.Turbofan engine_out(self, state)SUAVE.Components.Energy.Networks.Turbofan.Turbofan evaluate_thrust(self, state)SUAVE.Components.Energy.Networks.Turbofan.Turbofan + generative_design_char_max_bounds (defined in SUAVE.Components.Energy.Networks.Turbofan.Turbofan)SUAVE.Components.Energy.Networks.Turbofan.Turbofan + generative_design_char_min_bounds (defined in SUAVE.Components.Energy.Networks.Turbofan.Turbofan)SUAVE.Components.Energy.Networks.Turbofan.Turbofan + generative_design_characteristics (defined in SUAVE.Components.Energy.Networks.Turbofan.Turbofan)SUAVE.Components.Energy.Networks.Turbofan.Turbofan + generative_design_max_per_vehicle (defined in SUAVE.Components.Energy.Networks.Turbofan.Turbofan)SUAVE.Components.Energy.Networks.Turbofan.Turbofan + generative_design_minimum (defined in SUAVE.Components.Energy.Networks.Turbofan.Turbofan)SUAVE.Components.Energy.Networks.Turbofan.Turbofan + generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component - nacelle_diameter (defined in SUAVE.Components.Energy.Networks.Turbofan.Turbofan)SUAVE.Components.Energy.Networks.Turbofan.Turbofan + non_dimensional_origin (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network number_of_engines (defined in SUAVE.Components.Energy.Networks.Turbofan.Turbofan)SUAVE.Components.Energy.Networks.Turbofan.Turbofan - origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component + OpenVSP_flow_through (defined in SUAVE.Components.Energy.Networks.Turbofan.Turbofan)SUAVE.Components.Energy.Networks.Turbofan.Turbofan + origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component + SFC_adjustment (defined in SUAVE.Components.Energy.Networks.Turbofan.Turbofan)SUAVE.Components.Energy.Networks.Turbofan.Turbofan size(self, state)SUAVE.Components.Energy.Networks.Turbofan.Turbofan symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component tag (defined in SUAVE.Components.Energy.Networks.Turbofan.Turbofan)SUAVE.Components.Energy.Networks.Turbofan.Turbofan + wing_mounted (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
@@ -118,7 +134,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbofan_1_1Turbofan.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbofan_1_1Turbofan.html index 595886de..20762ae5 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbofan_1_1Turbofan.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbofan_1_1Turbofan.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Components.Energy.Networks.Turbofan.Turbofan Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -105,11 +112,11 @@
-SUAVE.Components.Propulsors.Propulsor.Propulsor +SUAVE.Components.Energy.Networks.Network.Network SUAVE.Components.Physical_Component.Physical_Component SUAVE.Components.Component.Component - -
+ + @@ -121,15 +128,6 @@ - - - - - - - - -

Public Member Functions

 
def engine_out (self, state)
 
- Public Member Functions inherited from SUAVE.Components.Propulsors.Propulsor.Propulsor
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
@@ -139,22 +137,58 @@ - - + + + + - - + + + + + + + + + + + - + + + + + + + + + + + + + @@ -175,6 +209,15 @@ + + + + + +

Public Attributes

 number_of_engines
 
nacelle_diameter
 
 engine_length
 
 bypass_ratio
 
SFC_adjustment
 
OpenVSP_flow_through
 
 areas
 
- Public Attributes inherited from SUAVE.Components.Propulsors.Propulsor.Propulsor
+
generative_design_minimum
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_char_min_bounds
 
generative_design_char_max_bounds
 
- Public Attributes inherited from SUAVE.Components.Energy.Networks.Network.Network
 tag
 
 
generative_design_max_per_vehicle
 
non_dimensional_origin
 
number_of_engines
 
engine_length
 
wing_mounted
 
areas
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
 tag
 origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 

Detailed Description

This is a turbofan. 
@@ -218,6 +261,8 @@ 

SUAVE.Components.Energy.Networks.Network.Network.

+

@@ -303,7 +348,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbofan_1_1Turbofan.js b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbofan_1_1Turbofan.js index 34fbf304..8941afa2 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbofan_1_1Turbofan.js +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbofan_1_1Turbofan.js @@ -7,7 +7,13 @@ var classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbofan_1_1Turbofan = [ "areas", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbofan_1_1Turbofan.html#a507a47908221e71e51bdb6edf7a6f4ab", null ], [ "bypass_ratio", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbofan_1_1Turbofan.html#a7da8c93851aa2763d0a38f53de203619", null ], [ "engine_length", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbofan_1_1Turbofan.html#a5985a59648a18ea778c429c5cf2ac948", null ], - [ "nacelle_diameter", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbofan_1_1Turbofan.html#a1bf3a72eac55b30fc00ddc8cdc099d26", null ], + [ "generative_design_char_max_bounds", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbofan_1_1Turbofan.html#a24235bb99cf5919d22f1b2ec03097019", null ], + [ "generative_design_char_min_bounds", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbofan_1_1Turbofan.html#a0a34894b6f30ccb63229ddeb6ec9a52a", null ], + [ "generative_design_characteristics", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbofan_1_1Turbofan.html#a508c85b29be7c6e600210bf518914bae", null ], + [ "generative_design_max_per_vehicle", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbofan_1_1Turbofan.html#a201434e46f84981c1aaaac4193bf3fa4", null ], + [ "generative_design_minimum", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbofan_1_1Turbofan.html#a021072fa2d0d835bc556164d9674d189", null ], [ "number_of_engines", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbofan_1_1Turbofan.html#ac838a4ddc129e87df7fe82977d42caad", null ], + [ "OpenVSP_flow_through", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbofan_1_1Turbofan.html#ad71e3cc0e8a88d101a605d3e52c28dc8", null ], + [ "SFC_adjustment", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbofan_1_1Turbofan.html#a03e991a7a9e667101a88861cd7f88595", null ], [ "tag", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbofan_1_1Turbofan.html#a643c70b63ac983fcf945798e9cbc1bcf", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbofan_1_1Turbofan.png b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbofan_1_1Turbofan.png index 6f15b8a1..4516bcf5 100644 Binary files a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbofan_1_1Turbofan.png and b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbofan_1_1Turbofan.png differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbojet__Super_1_1Turbojet__Super-members.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbojet__Super_1_1Turbojet__Super-members.html index 124b1229..ef275c87 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbojet__Super_1_1Turbojet__Super-members.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbojet__Super_1_1Turbojet__Super-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -98,47 +105,27 @@

This is the complete list of members for SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super, including all inherited members.

- - - - - - - - - - - - - - - - - - - - - - + + + + + + + + + + + + - - - + + + - - - - - - - - - - - - - - + + + +
__defaults__(self) (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super
bypass_ratio (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Superstatic
combustor (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Superstatic
compressor (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Superstatic
conditionsSUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Superstatic
core_area_ratio (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Superstatic
core_exit_velocity (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Superstatic
core_nozzle (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Superstatic
engine_length (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Superstatic
evaluate_thrust(self, state) (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super
F (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Superstatic
F (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Superstatic
F_vec (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Superstatic
flow_through_core (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Superstatic
flow_through_fan (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Superstatic
fuel_to_air_ratio (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Superstatic
high_pressure_compressor (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Superstatic
high_pressure_turbine (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Superstatic
inlet_nozzle (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Superstatic
Isp (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Superstatic
low_pressure_compressor (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Superstatic
low_pressure_turbine (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Superstatic
__defaults__(self)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super
afterburner_active (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super
areas (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super
engine_length (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super
engine_out(self, state)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super
evaluate_thrust(self, state)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super
generative_design_char_max_bounds (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super
generative_design_char_min_bounds (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super
generative_design_characteristics (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super
generative_design_max_per_vehicle (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super
generative_design_minimum (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
mdot (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Superstatic
nacelle_diameter (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Superstatic
number_of_engines (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Superstatic
non_dimensional_origin (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
number_of_engines (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super
OpenVSP_flow_through (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
output_power (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Superstatic
ram (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Superstatic
results (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Superstatic
size(self, state) (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super
stag_press_lpt_exit (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Superstatic
stag_temp_lpt_exit (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Superstatic
stagnation_pressure (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Superstatic
stagnation_temperature (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Superstatic
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tagSUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Superstatic
thrust (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Superstatic
thrust_force_vector (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Superstatic
vehicle_mass_rate (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Superstatic
working_fluid (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Superstatic
size(self, state)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super)SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super
wing_mounted (defined in SUAVE.Components.Energy.Networks.Network.Network)SUAVE.Components.Energy.Networks.Network.Network
@@ -146,7 +133,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbojet__Super_1_1Turbojet__Super.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbojet__Super_1_1Turbojet__Super.html index 89d94980..eec79c96 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbojet__Super_1_1Turbojet__Super.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbojet__Super_1_1Turbojet__Super.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -93,7 +100,7 @@
SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super Class Reference
@@ -105,145 +112,80 @@
-SUAVE.Components.Propulsors.Propulsor.Propulsor +SUAVE.Components.Energy.Networks.Network.Network SUAVE.Components.Physical_Component.Physical_Component SUAVE.Components.Component.Component - -
+ +
- + - + - + - - - - - - - - - + +

Public Member Functions

-def __defaults__ (self)
def __defaults__ (self)
 
-def evaluate_thrust (self, state)
def evaluate_thrust (self, state)
 
-def size (self, state)
def size (self, state)
 
- Public Member Functions inherited from SUAVE.Components.Propulsors.Propulsor.Propulsor
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
def engine_out (self, state)
 
- - + + +  - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Static Public Attributes

 tag

+Public Attributes

tag
 
number_of_engines = self.number_of_engines
number_of_engines
 
nacelle_diameter
 
 engine_length
 
 conditions = state.conditions
 
ram = self.ram
 
inlet_nozzle = self.inlet_nozzle
 
low_pressure_compressor = self.low_pressure_compressor
 
high_pressure_compressor = self.high_pressure_compressor
 
combustor = self.combustor
 
high_pressure_turbine = self.high_pressure_turbine
 
low_pressure_turbine = self.low_pressure_turbine
 
core_nozzle = self.core_nozzle
 
thrust = self.thrust
 
working_fluid
 
stagnation_temperature
 
stagnation_pressure
 
fuel_to_air_ratio
 
compressor
 
bypass_ratio
 
core_exit_velocity
 
core_area_ratio
 
stag_temp_lpt_exit
 
stag_press_lpt_exit
 
flow_through_core
 
flow_through_fan
 
F = thrust.outputs.thrust*[1,0,0]
 
mdot = thrust.outputs.fuel_flow_rate
 
Isp = thrust.outputs.specific_impulse
 
output_power = thrust.outputs.power
 
-float F_vec = conditions.ones_row(3) * 0.0
 
-float F = F_vec
 
results = Data()
 
thrust_force_vector
 
vehicle_mass_rate
 
- - - + + + + + + + + + + + + + + + + + - + + + + + + + + + + + + + @@ -264,6 +206,15 @@ + + + + + +

-Additional Inherited Members

- Public Attributes inherited from SUAVE.Components.Propulsors.Propulsor.Propulsor
+
afterburner_active
 
OpenVSP_flow_through
 
areas
 
generative_design_minimum
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_char_min_bounds
 
generative_design_char_max_bounds
 
- Public Attributes inherited from SUAVE.Components.Energy.Networks.Network.Network
 tag
 
 
generative_design_max_per_vehicle
 
non_dimensional_origin
 
number_of_engines
 
engine_length
 
wing_mounted
 
areas
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
 tag
 origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 

Detailed Description

This is a turbojet for supersonic flight.
@@ -274,27 +225,23 @@
     Source:
     Most of the componentes come from this book:
     https://web.stanford.edu/~cantwell/AA283_Course_Material/AA283_Course_Notes/
-

Member Data Documentation

- -

◆ conditions

+

Member Function Documentation

+ +

◆ __defaults__()

- - - - - -
- + + + + +
SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super.conditions = state.conditionsdef SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super.__defaults__ ( self)
-
-static
-
Calculate thrust given the current state of the vehicle
+
This sets the default values for the network to function.
 
 Assumptions:
 None
@@ -303,50 +250,88 @@ 

SUAVE.Components.Energy.Networks.Network.Network.

+

- -

◆ tag

+ +

◆ engine_out()

- - - - - -
- + + + + + + + + + + + + + + +
SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super.tagdef SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super.engine_out ( self,
 state 
)
-
-static
-
This sets the default values for the network to function.
+
Lose an engine
+    
+    Assumptions:
+    None
+    
+    Source:
+    N/A
+    
+    Inputs:
+    None
+    
+    Outputs:
+    None
+    
+    Properties Used:
+    N/A
+
+
+
+ +

◆ evaluate_thrust()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super.evaluate_thrust ( self,
 state 
)
+
+
Calculate thrust given the current state of the vehicle
 
     Assumptions:
     None
@@ -355,13 +340,70 @@ 

+

◆ size()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super.size ( self,
 state 
)
+
+
Size the turbojet
+
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+State [state()]
+
+Outputs:
+None
+
+Properties Used:
+N/A
 
@@ -376,7 +418,7 @@

SUAVE + doxygen 1.8.15

diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbojet__Super_1_1Turbojet__Super.js b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbojet__Super_1_1Turbojet__Super.js index 4bc542f8..065fc256 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbojet__Super_1_1Turbojet__Super.js +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbojet__Super_1_1Turbojet__Super.js @@ -1,6 +1,18 @@ var classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbojet__Super_1_1Turbojet__Super = [ [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbojet__Super_1_1Turbojet__Super.html#ab4871db4337784d79070b2b52f4a1287", null ], + [ "engine_out", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbojet__Super_1_1Turbojet__Super.html#a4fdeb95e3a0a35163b3e86601564f505", null ], [ "evaluate_thrust", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbojet__Super_1_1Turbojet__Super.html#ac08d01e1cb8d375476c9363d9bc05c43", null ], - [ "size", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbojet__Super_1_1Turbojet__Super.html#a2c1031116d3527670cf4a69e55d79649", null ] + [ "size", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbojet__Super_1_1Turbojet__Super.html#a2c1031116d3527670cf4a69e55d79649", null ], + [ "afterburner_active", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbojet__Super_1_1Turbojet__Super.html#a6432cda7398b6f092da5278928c3a6e9", null ], + [ "areas", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbojet__Super_1_1Turbojet__Super.html#a5c0e83653d64b4281a63d3fe164ec8ec", null ], + [ "engine_length", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbojet__Super_1_1Turbojet__Super.html#a810e8034a2eaec30ea82817c5ac1a606", null ], + [ "generative_design_char_max_bounds", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbojet__Super_1_1Turbojet__Super.html#a5102ef62aa08d9854f583bd881f42bfb", null ], + [ "generative_design_char_min_bounds", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbojet__Super_1_1Turbojet__Super.html#a62474c39c8fb77545571c163c6614d64", null ], + [ "generative_design_characteristics", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbojet__Super_1_1Turbojet__Super.html#acfb8de3adcd832869962fd4ff93e9add", null ], + [ "generative_design_max_per_vehicle", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbojet__Super_1_1Turbojet__Super.html#a163769caf5448859d08c213ce3fa89c2", null ], + [ "generative_design_minimum", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbojet__Super_1_1Turbojet__Super.html#acc973f5639f119d38b0c87f88fe47691", null ], + [ "number_of_engines", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbojet__Super_1_1Turbojet__Super.html#aae19aad195489dfe7852a1442a8cf3fa", null ], + [ "OpenVSP_flow_through", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbojet__Super_1_1Turbojet__Super.html#af43fe7111125073b050e52bd534c93ef", null ], + [ "tag", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbojet__Super_1_1Turbojet__Super.html#ad551ef45a70d71e80c6030f0af8470a3", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbojet__Super_1_1Turbojet__Super.png b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbojet__Super_1_1Turbojet__Super.png index dc4f3d62..7905eae0 100644 Binary files a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbojet__Super_1_1Turbojet__Super.png and b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Turbojet__Super_1_1Turbojet__Super.png differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Vectored__Thrust_1_1Vectored__Thrust-members.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Vectored__Thrust_1_1Vectored__Thrust-members.html new file mode 100644 index 00000000..7d90a0d0 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Vectored__Thrust_1_1Vectored__Thrust-members.html @@ -0,0 +1,141 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.4.0 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
SUAVE.Components.Energy.Networks.Vectored_Thrust.Vectored_Thrust Member List
+
+
+ +

This is the complete list of members for SUAVE.Components.Energy.Networks.Vectored_Thrust.Vectored_Thrust, including all inherited members.

+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
__defaults__(self)SUAVE.Components.Energy.Networks.Vectored_Thrust.Vectored_Thrust
areas (defined in SUAVE.Components.Propulsors.Propulsor.Propulsor)SUAVE.Components.Propulsors.Propulsor.Propulsor
avionics (defined in SUAVE.Components.Energy.Networks.Vectored_Thrust.Vectored_Thrust)SUAVE.Components.Energy.Networks.Vectored_Thrust.Vectored_Thrust
battery (defined in SUAVE.Components.Energy.Networks.Vectored_Thrust.Vectored_Thrust)SUAVE.Components.Energy.Networks.Vectored_Thrust.Vectored_Thrust
engine_length (defined in SUAVE.Components.Energy.Networks.Vectored_Thrust.Vectored_Thrust)SUAVE.Components.Energy.Networks.Vectored_Thrust.Vectored_Thrust
esc (defined in SUAVE.Components.Energy.Networks.Vectored_Thrust.Vectored_Thrust)SUAVE.Components.Energy.Networks.Vectored_Thrust.Vectored_Thrust
evaluate_thrust(self, state)SUAVE.Components.Energy.Networks.Vectored_Thrust.Vectored_Thrust
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Propulsors.Propulsor.Propulsor)SUAVE.Components.Propulsors.Propulsor.Propulsor
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
motor (defined in SUAVE.Components.Energy.Networks.Vectored_Thrust.Vectored_Thrust)SUAVE.Components.Energy.Networks.Vectored_Thrust.Vectored_Thrust
nacelle_diameter (defined in SUAVE.Components.Energy.Networks.Vectored_Thrust.Vectored_Thrust)SUAVE.Components.Energy.Networks.Vectored_Thrust.Vectored_Thrust
non_dimensional_origin (defined in SUAVE.Components.Propulsors.Propulsor.Propulsor)SUAVE.Components.Propulsors.Propulsor.Propulsor
number_of_engines (defined in SUAVE.Components.Energy.Networks.Vectored_Thrust.Vectored_Thrust)SUAVE.Components.Energy.Networks.Vectored_Thrust.Vectored_Thrust
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
payload (defined in SUAVE.Components.Energy.Networks.Vectored_Thrust.Vectored_Thrust)SUAVE.Components.Energy.Networks.Vectored_Thrust.Vectored_Thrust
pitch_command (defined in SUAVE.Components.Energy.Networks.Vectored_Thrust.Vectored_Thrust)SUAVE.Components.Energy.Networks.Vectored_Thrust.Vectored_Thrust
residuals(self, segment)SUAVE.Components.Energy.Networks.Vectored_Thrust.Vectored_Thrust
rotor (defined in SUAVE.Components.Energy.Networks.Vectored_Thrust.Vectored_Thrust)SUAVE.Components.Energy.Networks.Vectored_Thrust.Vectored_Thrust
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Energy.Networks.Vectored_Thrust.Vectored_Thrust)SUAVE.Components.Energy.Networks.Vectored_Thrust.Vectored_Thrust
thrust_angle (defined in SUAVE.Components.Energy.Networks.Vectored_Thrust.Vectored_Thrust)SUAVE.Components.Energy.Networks.Vectored_Thrust.Vectored_Thrust
thrust_angle_end (defined in SUAVE.Components.Energy.Networks.Vectored_Thrust.Vectored_Thrust)SUAVE.Components.Energy.Networks.Vectored_Thrust.Vectored_Thrust
thrust_angle_start (defined in SUAVE.Components.Energy.Networks.Vectored_Thrust.Vectored_Thrust)SUAVE.Components.Energy.Networks.Vectored_Thrust.Vectored_Thrust
unpack_unknowns(self, segment)SUAVE.Components.Energy.Networks.Vectored_Thrust.Vectored_Thrust
voltage (defined in SUAVE.Components.Energy.Networks.Vectored_Thrust.Vectored_Thrust)SUAVE.Components.Energy.Networks.Vectored_Thrust.Vectored_Thrust
wing_mounted (defined in SUAVE.Components.Propulsors.Propulsor.Propulsor)SUAVE.Components.Propulsors.Propulsor.Propulsor
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Vectored__Thrust_1_1Vectored__Thrust.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Vectored__Thrust_1_1Vectored__Thrust.html new file mode 100644 index 00000000..c7d7b3f9 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Vectored__Thrust_1_1Vectored__Thrust.html @@ -0,0 +1,437 @@ + + + + + + + +SUAVE: SUAVE.Components.Energy.Networks.Vectored_Thrust.Vectored_Thrust Class Reference + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.4.0 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Components.Energy.Networks.Vectored_Thrust.Vectored_Thrust Class Reference
+
+
+
+Inheritance diagram for SUAVE.Components.Energy.Networks.Vectored_Thrust.Vectored_Thrust:
+
+
+ + +SUAVE.Components.Propulsors.Propulsor.Propulsor +SUAVE.Components.Physical_Component.Physical_Component +SUAVE.Components.Component.Component + +
+ + + + + + + + + + +

+Public Member Functions

def __defaults__ (self)
 
def evaluate_thrust (self, state)
 
def unpack_unknowns (self, segment)
 
def residuals (self, segment)
 
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Attributes

tag
 
motor
 
rotor
 
esc
 
avionics
 
payload
 
battery
 
nacelle_diameter
 
engine_length
 
number_of_engines
 
voltage
 
thrust_angle
 
pitch_command
 
thrust_angle_start
 
thrust_angle_end
 
- Public Attributes inherited from SUAVE.Components.Propulsors.Propulsor.Propulsor
tag
 
generative_design_max_per_vehicle
 
non_dimensional_origin
 
number_of_engines
 
nacelle_diameter
 
engine_length
 
wing_mounted
 
areas
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 
+

Detailed Description

+
 This is a simple network with a battery powering a rotor through
+    an electric motor
+
+    Assumptions:
+    None
+    
+    Source:
+    None
+

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Components.Energy.Networks.Vectored_Thrust.Vectored_Thrust.__defaults__ ( self)
+
+
 This sets the default values for the network to function.
+
+    Assumptions:
+    None
+
+    Source:
+    N/A
+
+    Inputs:
+    None
+
+    Outputs:
+    None
+
+    Properties Used:
+    N/A
+
+

Reimplemented from SUAVE.Components.Propulsors.Propulsor.Propulsor.

+ +
+
+ +

◆ evaluate_thrust()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Components.Energy.Networks.Vectored_Thrust.Vectored_Thrust.evaluate_thrust ( self,
 state 
)
+
+
 Calculate thrust given the current state of the vehicle
+
+    Assumptions:
+    Caps the throttle at 110% and linearly interpolates thrust off that
+
+    Source:
+    N/A
+
+    Inputs:
+    state [state()]
+
+    Outputs:
+    results.thrust_force_vector [newtons]
+    results.vehicle_mass_rate   [kg/s]
+    conditions.propulsion:
+        rpm                  [radians/sec]
+        current              [amps]
+        battery_draw         [watts]
+        battery_energy       [joules]
+        voltage_open_circuit [volts]
+        voltage_under_load   [volts]
+        motor_torque         [N-M]
+        propeller_torque     [N-M]
+
+    Properties Used:
+    Defaulted values
+
+
+
+ +

◆ residuals()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Components.Energy.Networks.Vectored_Thrust.Vectored_Thrust.residuals ( self,
 segment 
)
+
+
 This packs the residuals to be send to the mission solver.
+
+    Assumptions:
+    None
+
+    Source:
+    N/A
+
+    Inputs:
+    state.conditions.propulsion:
+        motor_torque                          [N-m]
+        propeller_torque                      [N-m]
+        voltage_under_load                    [volts]
+    state.unknowns.battery_voltage_under_load [volts]
+    
+    Outputs:
+    None
+
+    Properties Used:
+    self.voltage                              [volts]
+
+
+
+ +

◆ unpack_unknowns()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Components.Energy.Networks.Vectored_Thrust.Vectored_Thrust.unpack_unknowns ( self,
 segment 
)
+
+
 This is an extra set of unknowns which are unpacked from the mission solver and send to the network.
+
+    Assumptions:
+    None
+
+    Source:
+    N/A
+
+    Inputs:
+    state.unknowns.propeller_power_coefficient [None]
+    state.unknowns.battery_voltage_under_load  [volts]
+
+    Outputs:
+    state.conditions.propulsion.propeller_power_coefficient [None]
+    state.conditions.propulsion.battery_voltage_under_load  [volts]
+
+    Properties Used:
+    N/A
+
+
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/matthewclarke/Documents/SUAVE/SUAVE/trunk/SUAVE/Components/Energy/Networks/Vectored_Thrust.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Vectored__Thrust_1_1Vectored__Thrust.js b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Vectored__Thrust_1_1Vectored__Thrust.js new file mode 100644 index 00000000..f8c37487 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Vectored__Thrust_1_1Vectored__Thrust.js @@ -0,0 +1,22 @@ +var classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Vectored__Thrust_1_1Vectored__Thrust = +[ + [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Vectored__Thrust_1_1Vectored__Thrust.html#a16cb483fe666addf6517affc0889bfcb", null ], + [ "evaluate_thrust", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Vectored__Thrust_1_1Vectored__Thrust.html#aade3d00e542c8a7bfd1e6a3bd26fc15b", null ], + [ "residuals", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Vectored__Thrust_1_1Vectored__Thrust.html#aeef6fb51df12a1dfb48a80b779ada3ee", null ], + [ "unpack_unknowns", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Vectored__Thrust_1_1Vectored__Thrust.html#abf5390b4e6c4fa05ebe59a22a4a6575b", null ], + [ "avionics", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Vectored__Thrust_1_1Vectored__Thrust.html#a3c23ae0be6a97abc41d57b668f6bc2f0", null ], + [ "battery", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Vectored__Thrust_1_1Vectored__Thrust.html#ace1e22413b0aa7042e6dc2ff65a05be7", null ], + [ "engine_length", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Vectored__Thrust_1_1Vectored__Thrust.html#a31b8e582d73ef03c1374eea76959086d", null ], + [ "esc", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Vectored__Thrust_1_1Vectored__Thrust.html#a7d1f2ab0d027d7c7ee03fc29efe70ab5", null ], + [ "motor", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Vectored__Thrust_1_1Vectored__Thrust.html#a55c040eef436f04d9ecfd7cc2f40cae6", null ], + [ "nacelle_diameter", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Vectored__Thrust_1_1Vectored__Thrust.html#a2e0efea543e2269ef696ba34efabbf69", null ], + [ "number_of_engines", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Vectored__Thrust_1_1Vectored__Thrust.html#ab68e658abf997c3a90dcb569abd40d86", null ], + [ "payload", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Vectored__Thrust_1_1Vectored__Thrust.html#abf758f2100621270b12dc2e22921b77a", null ], + [ "pitch_command", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Vectored__Thrust_1_1Vectored__Thrust.html#a119a847a37d1373a0101bf6e42a80497", null ], + [ "rotor", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Vectored__Thrust_1_1Vectored__Thrust.html#a440fbced6c23b7bc70a717716d329362", null ], + [ "tag", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Vectored__Thrust_1_1Vectored__Thrust.html#a0774f19e611a4b85d9bebb32215c944c", null ], + [ "thrust_angle", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Vectored__Thrust_1_1Vectored__Thrust.html#a0d1a91b88cdfc8c327bcf70cc7ab6fe5", null ], + [ "thrust_angle_end", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Vectored__Thrust_1_1Vectored__Thrust.html#aac11f6eb14d0cc5502d76163bc66ae30", null ], + [ "thrust_angle_start", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Vectored__Thrust_1_1Vectored__Thrust.html#af508f853b156917b975ecf2f44d76c80", null ], + [ "voltage", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Vectored__Thrust_1_1Vectored__Thrust.html#a404c5fd2ce129fe7f91fcede3e348f8e", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Vectored__Thrust_1_1Vectored__Thrust.png b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Vectored__Thrust_1_1Vectored__Thrust.png new file mode 100644 index 00000000..e7021d8a Binary files /dev/null and b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Vectored__Thrust_1_1Vectored__Thrust.png differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Peripherals_1_1Avionics_1_1Avionics-members.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Peripherals_1_1Avionics_1_1Avionics-members.html index 9a7cbafe..6cb99fb5 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Peripherals_1_1Avionics_1_1Avionics-members.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Peripherals_1_1Avionics_1_1Avionics-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@
- +
@@ -73,7 +78,9 @@
@@ -99,14 +106,17 @@

This is the complete list of members for SUAVE.Components.Energy.Peripherals.Avionics.Avionics, including all inherited members.

- - - - - - - - + + + + + + + + + + +
__defaults__(self)SUAVE.Components.Energy.Peripherals.Avionics.Avionics
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
power(self)SUAVE.Components.Energy.Peripherals.Avionics.Avionics
power_draw (defined in SUAVE.Components.Energy.Peripherals.Avionics.Avionics)SUAVE.Components.Energy.Peripherals.Avionics.Avionics
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
power(self)SUAVE.Components.Energy.Peripherals.Avionics.Avionics
power_draw (defined in SUAVE.Components.Energy.Peripherals.Avionics.Avionics)SUAVE.Components.Energy.Peripherals.Avionics.Avionics
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Energy.Peripherals.Avionics.Avionics)SUAVE.Components.Energy.Peripherals.Avionics.Avionics
@@ -114,7 +124,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Peripherals_1_1Avionics_1_1Avionics.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Peripherals_1_1Avionics_1_1Avionics.html index 36bcdb25..94c4e821 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Peripherals_1_1Avionics_1_1Avionics.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Peripherals_1_1Avionics_1_1Avionics.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Components.Energy.Peripherals.Avionics.Avionics Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -108,8 +115,8 @@ SUAVE.Components.Energy.Energy_Component.Energy_Component SUAVE.Components.Physical_Component.Physical_Component SUAVE.Components.Component.Component - -
+ + @@ -117,21 +124,15 @@ - - - - - - - - -

Public Member Functions

 
def power (self)
 
- Public Member Functions inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
+ + @@ -159,6 +160,15 @@ + + + + + +

Public Attributes

 power_draw
 
tag
 
- Public Attributes inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
 inputs
 origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 

Detailed Description

A class representing avionics.
@@ -201,6 +211,8 @@ 

SUAVE.Components.Energy.Energy_Component.Energy_Component.

+

@@ -248,7 +260,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Peripherals_1_1Avionics_1_1Avionics.js b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Peripherals_1_1Avionics_1_1Avionics.js index 99603b87..7c366fbe 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Peripherals_1_1Avionics_1_1Avionics.js +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Peripherals_1_1Avionics_1_1Avionics.js @@ -2,5 +2,6 @@ var classSUAVE_1_1Components_1_1Energy_1_1Peripherals_1_1Avionics_1_1Avionics = [ [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Peripherals_1_1Avionics_1_1Avionics.html#a9e84c9c15af2fee12b95f1da79a4ff79", null ], [ "power", "classSUAVE_1_1Components_1_1Energy_1_1Peripherals_1_1Avionics_1_1Avionics.html#ac9c2993263546a5f21acbf48fa637a28", null ], - [ "power_draw", "classSUAVE_1_1Components_1_1Energy_1_1Peripherals_1_1Avionics_1_1Avionics.html#a47460105eda78a3f35e8bfa9e5ae2ca2", null ] + [ "power_draw", "classSUAVE_1_1Components_1_1Energy_1_1Peripherals_1_1Avionics_1_1Avionics.html#a47460105eda78a3f35e8bfa9e5ae2ca2", null ], + [ "tag", "classSUAVE_1_1Components_1_1Energy_1_1Peripherals_1_1Avionics_1_1Avionics.html#afcb15975525021229679e223d090ab4e", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Peripherals_1_1Payload_1_1Payload-members.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Peripherals_1_1Payload_1_1Payload-members.html index 1d18292e..63071037 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Peripherals_1_1Payload_1_1Payload-members.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Peripherals_1_1Payload_1_1Payload-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -99,14 +106,17 @@

This is the complete list of members for SUAVE.Components.Energy.Peripherals.Payload.Payload, including all inherited members.

- - - - - - - - + + + + + + + + + + +
__defaults__(self)SUAVE.Components.Energy.Peripherals.Payload.Payload
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
power(self)SUAVE.Components.Energy.Peripherals.Payload.Payload
power_draw (defined in SUAVE.Components.Energy.Peripherals.Payload.Payload)SUAVE.Components.Energy.Peripherals.Payload.Payload
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
power(self)SUAVE.Components.Energy.Peripherals.Payload.Payload
power_draw (defined in SUAVE.Components.Energy.Peripherals.Payload.Payload)SUAVE.Components.Energy.Peripherals.Payload.Payload
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
@@ -114,7 +124,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Peripherals_1_1Payload_1_1Payload.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Peripherals_1_1Payload_1_1Payload.html index c7c63a09..86c6d47a 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Peripherals_1_1Payload_1_1Payload.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Peripherals_1_1Payload_1_1Payload.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Components.Energy.Peripherals.Payload.Payload Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -108,8 +115,8 @@ SUAVE.Components.Energy.Energy_Component.Energy_Component SUAVE.Components.Physical_Component.Physical_Component SUAVE.Components.Component.Component - -
+ + @@ -117,15 +124,6 @@ - - - - - - - - -

Public Member Functions

 
def power (self)
 
- Public Member Functions inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
@@ -159,6 +157,15 @@ + + + + + +

Public Attributes

 origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 

Detailed Description

A class representing a payload.
@@ -201,6 +208,8 @@ 

SUAVE.Components.Energy.Energy_Component.Energy_Component.

+

@@ -248,7 +257,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Rocket__Thrust_1_1Rocket__Thrust-members.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Rocket__Thrust_1_1Rocket__Thrust-members.html new file mode 100644 index 00000000..97f7c4f0 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Rocket__Thrust_1_1Rocket__Thrust-members.html @@ -0,0 +1,135 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
SUAVE.Components.Energy.Processes.Rocket_Thrust.Rocket_Thrust Member List
+
+
+ +

This is the complete list of members for SUAVE.Components.Energy.Processes.Rocket_Thrust.Rocket_Thrust, including all inherited members.

+ + + + + + + + + + + + + + + + + +
__defaults__(self)SUAVE.Components.Energy.Processes.Rocket_Thrust.Rocket_Thrust
compute(self, conditions)SUAVE.Components.Energy.Processes.Rocket_Thrust.Rocket_Thrust
design_thrust (defined in SUAVE.Components.Energy.Processes.Rocket_Thrust.Rocket_Thrust)SUAVE.Components.Energy.Processes.Rocket_Thrust.Rocket_Thrust
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
ISP_design (defined in SUAVE.Components.Energy.Processes.Rocket_Thrust.Rocket_Thrust)SUAVE.Components.Energy.Processes.Rocket_Thrust.Rocket_Thrust
mass_flow_rate (defined in SUAVE.Components.Energy.Processes.Rocket_Thrust.Rocket_Thrust)SUAVE.Components.Energy.Processes.Rocket_Thrust.Rocket_Thrust
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
number_of_engines (defined in SUAVE.Components.Energy.Processes.Rocket_Thrust.Rocket_Thrust)SUAVE.Components.Energy.Processes.Rocket_Thrust.Rocket_Thrust
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
size(self, conditions)SUAVE.Components.Energy.Processes.Rocket_Thrust.Rocket_Thrust
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Energy.Processes.Rocket_Thrust.Rocket_Thrust)SUAVE.Components.Energy.Processes.Rocket_Thrust.Rocket_Thrust
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Rocket__Thrust_1_1Rocket__Thrust.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Rocket__Thrust_1_1Rocket__Thrust.html new file mode 100644 index 00000000..08416a3d --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Rocket__Thrust_1_1Rocket__Thrust.html @@ -0,0 +1,355 @@ + + + + + + + +SUAVE: SUAVE.Components.Energy.Processes.Rocket_Thrust.Rocket_Thrust Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Components.Energy.Processes.Rocket_Thrust.Rocket_Thrust Class Reference
+
+
+
+Inheritance diagram for SUAVE.Components.Energy.Processes.Rocket_Thrust.Rocket_Thrust:
+
+
+ + +SUAVE.Components.Energy.Energy_Component.Energy_Component +SUAVE.Components.Physical_Component.Physical_Component +SUAVE.Components.Component.Component + +
+ + + + + + + + +

+Public Member Functions

def __defaults__ (self)
 
def compute (self, conditions)
 
def size (self, conditions)
 
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Attributes

tag
 
number_of_engines
 
mass_flow_rate
 
design_thrust
 
ISP_design
 
- Public Attributes inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
inputs
 
outputs
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 
+

Detailed Description

+
A class that handles computation of thrust and ISP for rocket engines
+
+Assumptions:
+
+Source:
+Chapter 7
+https://web.stanford.edu/~cantwell/AA283_Course_Material/AA283_Course_Notes/
+

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Components.Energy.Processes.Rocket_Thrust.Rocket_Thrust.__defaults__ ( self)
+
+
This sets the default value.
+
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+None
+
+Outputs:
+None
+
+Properties Used:
+N/A
+
+

Reimplemented from SUAVE.Components.Energy.Energy_Component.Energy_Component.

+ +
+
+ +

◆ compute()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Components.Energy.Processes.Rocket_Thrust.Rocket_Thrust.compute ( self,
 conditions 
)
+
+
Computes thrust and other properties as below.
+
+Assumptions:
+Perfect gas
+
+Source:
+https://web.stanford.edu/~cantwell/AA283_Course_Material/AA283_Course_Notes/
+
+Inputs:
+conditions.freestream.
+  pressure                           [Pa]
+  temperature                        [K]
+  gravity                            [-]
+conditions.throttle                  [-]
+self.inputs.
+  propellant_mass_rate               [kg/s]
+  combustion_pressure                [Pa]
+  expansion_ratio                    [-]
+  area_throat                        [m^2]
+  exhaust_velocity                   [m/s]
+  number_of_engines                  [-]
+
+Outputs:
+self.outputs.
+  thrust                             [N]
+  propellant_mass_flow_rate          [kg/s]
+  power                              [W]
+  specific_impulse                   [s]
+  exhuast_velocity                   [m/s]
+
+Properties Used:
+
+
+ +

◆ size()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Components.Energy.Processes.Rocket_Thrust.Rocket_Thrust.size ( self,
 conditions 
)
+
+
Sizes the engine for the design condition.
+
+Assumptions:
+Perfect gas
+
+Source:
+Chapter 7
+https://web.stanford.edu/~cantwell/AA283_Course_Material/AA283_Course_Notes/
+
+Inputs:
+conditions.freestream.speed_of_sound [m/s] (conditions is also passed to self.compute(..))
+self.inputs.
+  bypass_ratio                       [-]
+  total_temperature_reference        [K]
+  total_pressure_reference           [Pa]
+  number_of_engines                  [-]
+
+Outputs:
+self.outputs.non_dimensional_thrust  [-]
+
+Properties Used:
+self.
+  reference_temperature              [K]
+  reference_pressure                 [Pa]
+  total_design                       [N] - Design thrust
+
+
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Energy/Processes/Rocket_Thrust.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Rocket__Thrust_1_1Rocket__Thrust.js b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Rocket__Thrust_1_1Rocket__Thrust.js new file mode 100644 index 00000000..8258240e --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Rocket__Thrust_1_1Rocket__Thrust.js @@ -0,0 +1,11 @@ +var classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Rocket__Thrust_1_1Rocket__Thrust = +[ + [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Rocket__Thrust_1_1Rocket__Thrust.html#a83f46e0a05a4678a2715c99a14abd315", null ], + [ "compute", "classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Rocket__Thrust_1_1Rocket__Thrust.html#aded48da4e8bf71672758c413c7cd51a8", null ], + [ "size", "classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Rocket__Thrust_1_1Rocket__Thrust.html#a12029b6b3fd9a6b80271886e6e22c580", null ], + [ "design_thrust", "classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Rocket__Thrust_1_1Rocket__Thrust.html#a9b7661f406fd17e49f976ee12d7819c7", null ], + [ "ISP_design", "classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Rocket__Thrust_1_1Rocket__Thrust.html#af25c5d501c8353ad9aae9007a7061049", null ], + [ "mass_flow_rate", "classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Rocket__Thrust_1_1Rocket__Thrust.html#aea57541019a6a9e912ea85b890749043", null ], + [ "number_of_engines", "classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Rocket__Thrust_1_1Rocket__Thrust.html#a580c786d39c052eba70f461e8d2a96fe", null ], + [ "tag", "classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Rocket__Thrust_1_1Rocket__Thrust.html#ab82f9398b045d7cc8534bd4e35e802c6", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Rocket__Thrust_1_1Rocket__Thrust.png b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Rocket__Thrust_1_1Rocket__Thrust.png new file mode 100644 index 00000000..876f6f3a Binary files /dev/null and b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Rocket__Thrust_1_1Rocket__Thrust.png differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Solar__Radiation_1_1Solar__Radiation-members.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Solar__Radiation_1_1Solar__Radiation-members.html index c16afa16..ecfe034b 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Solar__Radiation_1_1Solar__Radiation-members.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Solar__Radiation_1_1Solar__Radiation-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -99,13 +106,16 @@

This is the complete list of members for SUAVE.Components.Energy.Processes.Solar_Radiation.Solar_Radiation, including all inherited members.

- - - - - - - + + + + + + + + + +
__defaults__(self)SUAVE.Components.Energy.Energy_Component.Energy_Component
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
solar_radiation(self, conditions)SUAVE.Components.Energy.Processes.Solar_Radiation.Solar_Radiation
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
solar_radiation(self, conditions)SUAVE.Components.Energy.Processes.Solar_Radiation.Solar_Radiation
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
@@ -113,7 +123,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Solar__Radiation_1_1Solar__Radiation.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Solar__Radiation_1_1Solar__Radiation.html index d00e0e80..3281aa45 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Solar__Radiation_1_1Solar__Radiation.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Solar__Radiation_1_1Solar__Radiation.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Components.Energy.Processes.Solar_Radiation.Solar_Radiation Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -107,8 +114,8 @@ SUAVE.Components.Energy.Energy_Component.Energy_Component SUAVE.Components.Physical_Component.Physical_Component SUAVE.Components.Component.Component - -
+ + @@ -117,12 +124,6 @@ - - - - - -

Public Member Functions

- Public Member Functions inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
@@ -153,6 +154,15 @@ + + + + + +

Additional Inherited Members

 origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 

Detailed Description

A class that handle solar radiation computation.
@@ -228,7 +238,7 @@ 

SUAVE + doxygen 1.8.15

diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Thrust_1_1Thrust-members.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Thrust_1_1Thrust-members.html index 9443462e..f669f6fa 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Thrust_1_1Thrust-members.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Thrust_1_1Thrust-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -102,7 +109,11 @@ bypass_ratio (defined in SUAVE.Components.Energy.Processes.Thrust.Thrust)SUAVE.Components.Energy.Processes.Thrust.Thrust compressor_nondimensional_massflow (defined in SUAVE.Components.Energy.Processes.Thrust.Thrust)SUAVE.Components.Energy.Processes.Thrust.Thrust compute(self, conditions)SUAVE.Components.Energy.Processes.Thrust.Thrust - design_thrust (defined in SUAVE.Components.Energy.Processes.Thrust.Thrust)SUAVE.Components.Energy.Processes.Thrust.Thrust + compute_stream_thrust(self, conditions)SUAVE.Components.Energy.Processes.Thrust.Thrust + design_thrust (defined in SUAVE.Components.Energy.Processes.Thrust.Thrust)SUAVE.Components.Energy.Processes.Thrust.Thrust + generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component + generative_design_max_per_vehicle (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component + generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component mass_flow_rate_design (defined in SUAVE.Components.Energy.Processes.Thrust.Thrust)SUAVE.Components.Energy.Processes.Thrust.Thrust mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component @@ -111,7 +122,9 @@ outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component reference_pressure (defined in SUAVE.Components.Energy.Processes.Thrust.Thrust)SUAVE.Components.Energy.Processes.Thrust.Thrust reference_temperature (defined in SUAVE.Components.Energy.Processes.Thrust.Thrust)SUAVE.Components.Energy.Processes.Thrust.Thrust - size(self, conditions)SUAVE.Components.Energy.Processes.Thrust.Thrust + SFC_adjustment (defined in SUAVE.Components.Energy.Processes.Thrust.Thrust)SUAVE.Components.Energy.Processes.Thrust.Thrust + size(self, conditions)SUAVE.Components.Energy.Processes.Thrust.Thrust + size_stream_thrust(self, conditions)SUAVE.Components.Energy.Processes.Thrust.Thrust symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component tag (defined in SUAVE.Components.Energy.Processes.Thrust.Thrust)SUAVE.Components.Energy.Processes.Thrust.Thrust
@@ -121,7 +134,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Thrust_1_1Thrust.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Thrust_1_1Thrust.html index 325f94f4..5b32ff43 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Thrust_1_1Thrust.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Thrust_1_1Thrust.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Components.Energy.Processes.Thrust.Thrust Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -108,8 +115,8 @@ SUAVE.Components.Energy.Energy_Component.Energy_Component SUAVE.Components.Physical_Component.Physical_Component SUAVE.Components.Component.Component - -
+ + @@ -117,17 +124,12 @@ + + - - - - - - - - - + +

Public Member Functions

 
def compute (self, conditions)
 
def compute_stream_thrust (self, conditions)
 
def size (self, conditions)
 
- Public Member Functions inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
def size_stream_thrust (self, conditions)
 
@@ -155,6 +157,9 @@ + + @@ -182,6 +187,15 @@ + + + + + +

Public Attributes

 mass_flow_rate_design
 
SFC_adjustment
 
- Public Attributes inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
 inputs
 origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 

Detailed Description

A class that handles computation of thrust and other outputs for a gas turbine engine.
@@ -224,6 +238,8 @@ 

SUAVE.Components.Energy.Energy_Component.Energy_Component.

+

@@ -301,6 +317,88 @@

+

◆ compute_stream_thrust()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Components.Energy.Processes.Thrust.Thrust.compute_stream_thrust ( self,
 conditions 
)
+
+
Computes thrust and other properties as below. 
+
+Assumptions: 
+
+Source: 
+Heiser, William H., Pratt, D. T., Daley, D. H., and Unmeel, B. M., 
+"Hypersonic Airbreathing Propulsion", 1994 
+Chapter 4 - pgs. 175-180
+
+Inputs: 
+conditions.freestream. 
+   isentropic_expansion_factor        [-]  
+   specific_heat_at_constant_pressure [J/(kg K)] 
+   velocity                           [m/s] 
+   speed_of_sound                     [m/s] 
+   mach_number                        [-] 
+   pressure                           [Pa] 
+   gravity                            [m/s^2] 
+conditions.throttle                  [-] (.1 is 10%) 
+
+self.inputs. 
+   fuel_to_air_ratio                  [-] 
+   total_temperature_reference        [K] 
+   total_pressure_reference           [Pa] 
+
+core_nozzle. 
+    velocity                         [m/s] 
+    static_pressure                  [Pa] 
+    area_ratio                       [-] 
+
+fan_nozzle. 
+    velocity                         [m/s] 
+    static_pressure                  [Pa] 
+    area_ratio                       [-] 
+    number_of_engines                [-] 
+    bypass_ratio                     [-] 
+    flow_through_core                [-] percentage of total flow (.1 is 10%) 
+    flow_through_fan                 [-] percentage of total flow (.1 is 10%)
+
+Outputs: 
+self.outputs. 
+  thrust                             [N] 
+  thrust_specific_fuel_consumption   [N/N-s] 
+  non_dimensional_thrust             [-] 
+  core_mass_flow_rate                [kg/s] 
+  fuel_flow_rate                     [kg/s] 
+  power                              [W] 
+
+Properties Used: 
+self. 
+  reference_temperature              [K] 
+  reference_pressure                 [Pa] 
+  compressor_nondimensional_massflow [-] 
 
@@ -356,6 +454,59 @@

+

◆ size_stream_thrust()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Components.Energy.Processes.Thrust.Thrust.size_stream_thrust ( self,
 conditions 
)
+
+
Sizes the core flow for the design condition. 
+
+   Assumptions: 
+   Perfect gas 
+
+   Source: 
+   Heiser, William H., Pratt, D. T., Daley, D. H., and Unmeel, B. M., 
+   "Hypersonic Airbreathing Propulsion", 1994 
+   Chapter 4 - pgs. 175-180
+   
+   Inputs: 
+   conditions.freestream.speed_of_sound [m/s] (conditions is also passed to self.compute(..)) 
+   self.inputs. 
+      bypass_ratio                       [-] 
+      total_temperature_reference        [K] 
+      total_pressure_reference           [Pa] 
+      number_of_engines                  [-] 
+
+    Outputs: 
+      self.outputs.non_dimensional_thrust  [-] 
+
+    Properties Used: 
+    self. 
+       reference_temperature              [K] 
+       reference_pressure                 [Pa] 
+       total_design                       [N] - Design thrust 
+
+

The documentation for this class was generated from the following file:
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Energy/Processes/Thrust.py
@@ -367,7 +518,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Thrust_1_1Thrust.js b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Thrust_1_1Thrust.js index f57121e2..47e97141 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Thrust_1_1Thrust.js +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Thrust_1_1Thrust.js @@ -2,7 +2,9 @@ var classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Thrust_1_1Thrust = [ [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Thrust_1_1Thrust.html#a4a6b965d0e738d3cd7cf259b2157dfd3", null ], [ "compute", "classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Thrust_1_1Thrust.html#a65285d08cd9bf97245c4b0933e23b9d2", null ], + [ "compute_stream_thrust", "classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Thrust_1_1Thrust.html#ae83c8e3d7a39bc95c289c83c08060bee", null ], [ "size", "classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Thrust_1_1Thrust.html#ae63d108105b0578e786f51d8799eb8c2", null ], + [ "size_stream_thrust", "classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Thrust_1_1Thrust.html#acd7e80279bbc0a232b95cf4064a46aa0", null ], [ "bypass_ratio", "classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Thrust_1_1Thrust.html#a57203285c31d0d5df7fbb063ef566b29", null ], [ "compressor_nondimensional_massflow", "classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Thrust_1_1Thrust.html#a1be464918920af147d428173a68853e7", null ], [ "design_thrust", "classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Thrust_1_1Thrust.html#a0a2b78e1b59fe6be7c860c1b7972af56", null ], @@ -10,5 +12,6 @@ var classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Thrust_1_1Thrust = [ "number_of_engines", "classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Thrust_1_1Thrust.html#aa048c9f61b35a2ea1b903e53d9d43a99", null ], [ "reference_pressure", "classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Thrust_1_1Thrust.html#aa96a8f8bc7798801e719bf41f7d495d4", null ], [ "reference_temperature", "classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Thrust_1_1Thrust.html#a6d23c79620a073c073109e0dfe4d0c69", null ], + [ "SFC_adjustment", "classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Thrust_1_1Thrust.html#ab0f315d508bbe21fd04ea1a33a272998", null ], [ "tag", "classSUAVE_1_1Components_1_1Energy_1_1Processes_1_1Thrust_1_1Thrust.html#a1dd2cf24444b3f094c0fce37fc000ac9", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery-members.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery-members.html index 7ae90cc6..30c113cc 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery-members.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -98,20 +105,26 @@

This is the complete list of members for SUAVE.Components.Energy.Storages.Batteries.Battery.Battery, including all inherited members.

- + + + - - - - - - - - - - - - + + + + + + + + + + + + + + + +
__defaults__(self) (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
__defaults__(self)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
chemistry (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
current_capacitor_charge (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
current_energy (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
discharge_model (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
energy_calc(self, numerics) (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
energy_density (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
max_energy (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
max_power (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
max_voltage (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
ragone (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
resistance (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
discharge_performance_map (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
energy_density (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
initial_temperature (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
max_energy (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
max_power (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
max_voltage (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
ragone (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
resistance (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
specific_heat_capacity (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
@@ -121,7 +134,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.html index 4eed56ed..27dd5621 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Components.Energy.Storages.Batteries.Battery.Battery Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -105,45 +112,46 @@
-SUAVE.Components.Energy.Energy_Component.Energy_Component -SUAVE.Components.Physical_Component.Physical_Component -SUAVE.Components.Component.Component -SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion -SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Sulfur.Lithium_Sulfur -SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Aluminum_Air.Aluminum_Air -SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Lithium_Air.Lithium_Air - -
+SUAVE.Components.Energy.Energy_Component.Energy_Component +SUAVE.Components.Physical_Component.Physical_Component +SUAVE.Components.Component.Component +SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion +SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Sulfur.Lithium_Sulfur +SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Aluminum_Air.Aluminum_Air +SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Lithium_Air.Lithium_Air +SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion_LiFePO4_18650.Lithium_Ion_LiFePO4_18650 +SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion_LiNiMnCoO2_18650.Lithium_Ion_LiNiMnCoO2_18650 + + - + - - - - - - - - - - -

Public Member Functions

-def __defaults__ (self)
def __defaults__ (self)
 
-def energy_calc (self, numerics)
 
- Public Member Functions inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
+ + + + + + + + @@ -153,9 +161,9 @@ - - + + @@ -186,12 +194,60 @@ + + + + + +

Public Attributes

chemistry
 
 energy_density
 
 current_energy
 
initial_temperature
 
current_capacitor_charge
 
 resistance
 
specific_heat_capacity
 
 max_energy
 
 max_voltage
 
discharge_model
 
discharge_performance_map
 
 ragone
 
 origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 

Detailed Description

Energy Component object that stores energy. Contains values
 used to indicate its discharge characterics, including a model
 that calculates discharge losses
-

The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.js b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.js index 90cadf61..776dcf67 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.js +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.js @@ -1,13 +1,16 @@ var classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery = [ [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.html#a529cffa04fba4664bd432349f14fe268", null ], - [ "energy_calc", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.html#aa65c7a1b8d7ff1b54685851fb8d8f2cd", null ], + [ "chemistry", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.html#a42d0b6739ed87941a1b3a463ea3058f9", null ], + [ "current_capacitor_charge", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.html#a5ddf82deeb13f9bbae7c60cbfe3a3bfb", null ], [ "current_energy", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.html#ab75d672bb965c5aec6968c38e1fec34e", null ], - [ "discharge_model", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.html#ac1e376177175252082d5b465a7915f7a", null ], + [ "discharge_performance_map", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.html#a9930464c6ac27fbf2c1e5986451e1bdb", null ], [ "energy_density", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.html#af6ab54f2a19d11ce4b6362a21610c96c", null ], + [ "initial_temperature", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.html#a443530ab6d7d61e4a9c962a1060d6175", null ], [ "max_energy", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.html#a26fea5041ae1d5bb54a6a816420191a8", null ], [ "max_power", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.html#a216ae6ac99fb528716599d14c64a1888", null ], [ "max_voltage", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.html#af34d6af1003c3d903a9eef49f1a7f368", null ], [ "ragone", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.html#acfe3bfad30bd53b5c4608a7660606832", null ], - [ "resistance", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.html#a53d46e3ffe1570d23a4423005dd608a9", null ] + [ "resistance", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.html#a53d46e3ffe1570d23a4423005dd608a9", null ], + [ "specific_heat_capacity", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.html#a36b9efe4eec78bd29abd52176fd6033f", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.png b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.png index d7fc26c8..9d09d001 100644 Binary files a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.png and b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.png differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Constant__Mass_1_1Lithium__Ion_1_1Lithium__Ion-members.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Constant__Mass_1_1Lithium__Ion_1_1Lithium__Ion-members.html index 3112c8ce..ab9c09da 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Constant__Mass_1_1Lithium__Ion_1_1Lithium__Ion-members.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Constant__Mass_1_1Lithium__Ion_1_1Lithium__Ion-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -98,24 +105,44 @@

This is the complete list of members for SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion, including all inherited members.

- + + + + + + + + + + + - - + + - - - - - - - + + + + + + + + + + + + + + + - - - + + + + +
__defaults__(self) (defined in SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion
__defaults__(self)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion
age (defined in SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion
append_battery_residuals(self, segment, network)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion
append_battery_unknowns(self, segment)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion
append_battery_unknowns_and_residuals_to_segment(self, segment, initial_voltage, initial_battery_cell_temperature, initial_battery_state_of_charge, initial_battery_cell_current)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion
cell (defined in SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion
chemistry (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
compute_voltage(self, state)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion
convective_heat_transfer_coefficient (defined in SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion
cooling_fluid (defined in SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion
current_capacitor_charge (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
current_energy (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
discharge_model (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
energy_calc(self, numerics) (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
discharge_performance_map (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
energy_calc(self, numerics, battery_discharge_flag=True)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion
energy_density (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
max_energy (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
max_power (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
max_voltage (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
heat_transfer_efficiency (defined in SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion
initial_temperature (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
max_energy (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
max_power (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
max_voltage (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
module (defined in SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion
module_config (defined in SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
pack_config (defined in SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion
ragone (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
resistance (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
specific_energy (defined in SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion
specific_power (defined in SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
specific_heat_capacity (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
specific_power (defined in SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion
update_battery_state_of_health(self, segment, increment_battery_cycle_day=False) (defined in SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion
@@ -123,7 +150,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Constant__Mass_1_1Lithium__Ion_1_1Lithium__Ion.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Constant__Mass_1_1Lithium__Ion_1_1Lithium__Ion.html index fca3ab29..913d679d 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Constant__Mass_1_1Lithium__Ion_1_1Lithium__Ion.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Constant__Mass_1_1Lithium__Ion_1_1Lithium__Ion.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -105,37 +112,62 @@
-SUAVE.Components.Energy.Storages.Batteries.Battery.Battery -SUAVE.Components.Energy.Energy_Component.Energy_Component -SUAVE.Components.Physical_Component.Physical_Component -SUAVE.Components.Component.Component - -
+SUAVE.Components.Energy.Storages.Batteries.Battery.Battery +SUAVE.Components.Energy.Energy_Component.Energy_Component +SUAVE.Components.Physical_Component.Physical_Component +SUAVE.Components.Component.Component +SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion_LiFePO4_18650.Lithium_Ion_LiFePO4_18650 +SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion_LiNiMnCoO2_18650.Lithium_Ion_LiNiMnCoO2_18650 + + - + - - - - - - - - - - - - - - + + + + + + + + + + + +

Public Member Functions

-def __defaults__ (self)
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
-def __defaults__ (self)
 
-def energy_calc (self, numerics)
 
- Public Member Functions inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
def energy_calc (self, numerics, battery_discharge_flag=True)
 
def append_battery_unknowns (self, segment)
 
def append_battery_residuals (self, segment, network)
 
def append_battery_unknowns_and_residuals_to_segment (self, segment, initial_voltage, initial_battery_cell_temperature, initial_battery_state_of_charge, initial_battery_cell_current)
 
def compute_voltage (self, state)
 
+def update_battery_state_of_health (self, segment, increment_battery_cycle_day=False)
 
+ + + + + + + + + + + + + + + + + + @@ -143,15 +175,27 @@   + + + + + + + + @@ -161,9 +205,9 @@ - - + + @@ -194,11 +238,378 @@ + + + + + +

Public Attributes

tag
 
cell
 
module
 
pack_config
 
module_config
 
age
 
convective_heat_transfer_coefficient
 
heat_transfer_efficiency
 
cooling_fluid
 
 specific_energy
 
specific_power
 
- Public Attributes inherited from SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
chemistry
 
 energy_density
 
 current_energy
 
initial_temperature
 
current_capacitor_charge
 
 resistance
 
specific_heat_capacity
 
 max_energy
 
 max_voltage
 
discharge_model
 
discharge_performance_map
 
 ragone
 
 origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 

Detailed Description

-
Specifies discharge/specific energy characteristics specific tobytes
-lithium-ion batteries
-

The documentation for this class was generated from the following file:
    +
    Generic lithium ion battery that specifies discharge/specific energy 
    +characteristics. 
    +
    +Assumptions
    +1) Default discharge curves correspond to lithium-iron-phosphate cells
    +
    +2) Convective Thermal Conductivity Coefficient corresponds to forced
    +air cooling in 35 m/s air 
    +
    +Inputs:
    +None
    +
    +Outputs:
    +None
    +
    +Properties Used:
    +N/A
    +

    Member Function Documentation

    + +

    ◆ __defaults__()

    + +
    +
    + + + + + + + + +
    def SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion.__defaults__ ( self)
    +
    +
    This sets the default inputs and outputs data structure.
    +
    +Assumptions:
    +None
    +
    +Source:
    +N/A
    +
    +Inputs:
    +None
    +
    +Outputs:
    +None
    +
    +Properties Used:
    +N/A
    +
    +

    Reimplemented from SUAVE.Components.Energy.Storages.Batteries.Battery.Battery.

    + +

    Reimplemented in SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion_LiNiMnCoO2_18650.Lithium_Ion_LiNiMnCoO2_18650, and SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion_LiFePO4_18650.Lithium_Ion_LiFePO4_18650.

    + +
    +
    + +

    ◆ append_battery_residuals()

    + +
    +
    + + + + + + + + + + + + + + + + + + + + + + + + +
    def SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion.append_battery_residuals ( self,
     segment,
     network 
    )
    +
    +
    Packs the residuals specific to LFP cells to be sent to the mission solver.
    +    
    +    Assumptions:
    +    None
    +    
    +    Source:
    +    N/A
    +    
    +    Inputs:
    +    state.conditions.propulsion:
    +motor_torque                          [N-m]
    +propeller_torque                      [N-m]
    +voltage_under_load                    [volts]
    +    state.unknowns.battery_voltage_under_load [volts]
    +    
    +    Outputs:
    +    None
    +    
    +    Properties Used:
    +    network.voltage                           [volts]
    +
    +

    Reimplemented in SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion_LiNiMnCoO2_18650.Lithium_Ion_LiNiMnCoO2_18650.

    + +
    +
    + +

    ◆ append_battery_unknowns()

    + +
    +
    + + + + + + + + + + + + + + + + + + +
    def SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion.append_battery_unknowns ( self,
     segment 
    )
    +
    +
    Appends unknowns specific to LFP cells which are unpacked from the mission solver and send to the network.
    +    
    +    Assumptions:
    +    None
    +    
    +    Source:
    +    N/A
    +    
    +    Inputs:
    +    state.unknowns.battery_voltage_under_load               [volts]
    +    
    +    Outputs: 
    +    state.conditions.propulsion.battery_voltage_under_load  [volts]
    +    
    +    Properties Used:
    +    N/A
    +
    +

    Reimplemented in SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion_LiNiMnCoO2_18650.Lithium_Ion_LiNiMnCoO2_18650.

    + +
    +
    + +

    ◆ append_battery_unknowns_and_residuals_to_segment()

    + +
    +
    + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
    def SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion.append_battery_unknowns_and_residuals_to_segment ( self,
     segment,
     initial_voltage,
     initial_battery_cell_temperature,
     initial_battery_state_of_charge,
     initial_battery_cell_current 
    )
    +
    +
    Sets up the information that the mission needs to run a mission segment using this network
    +    
    +    Assumptions:
    +    None
    +    
    +    Source:
    +    N/A
    +    
    +    Inputs:  
    +    initial_voltage                       [volts]
    +    initial_battery_cell_temperature      [Kelvin]
    +    initial_battery_state_of_charge       [unitless]
    +    initial_battery_cell_current          [Amperes]
    +    
    +    Outputs
    +    None
    +    
    +    Properties Used:
    +    N/A
    +
    +

    Reimplemented in SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion_LiNiMnCoO2_18650.Lithium_Ion_LiNiMnCoO2_18650.

    + +
    +
    + +

    ◆ compute_voltage()

    + +
    +
    + + + + + + + + + + + + + + + + + + +
    def SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion.compute_voltage ( self,
     state 
    )
    +
    +
    Computes the voltage of a single LFP cell or a battery pack of LFP cells   
    +    
    +    Assumptions:
    +    None
    +    
    +    Source:
    +    N/A
    +    
    +    Inputs:  
    +state   - segment unknowns to define voltage [unitless]
    +    
    +    Outputs
    +V_ul    - under-load voltage                 [volts]
    +     
    +    Properties Used:
    +    N/A
    +
    +

    Reimplemented in SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion_LiNiMnCoO2_18650.Lithium_Ion_LiNiMnCoO2_18650.

    + +
    +
    + +

    ◆ energy_calc()

    + +
    +
    + + + + + + + + + + + + + + + + + + + + + + + + +
    def SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion.energy_calc ( self,
     numerics,
     battery_discharge_flag = True 
    )
    +
    +
    This is an electric cycle model for 18650 lithium-iron_phosphate battery cells. It
    +   models losses based on an empirical correlation Based on method taken 
    +   from Datta and Johnson.
    +   
    +   Assumptions: 
    +   1) Constant Peukart coefficient
    +   2) All battery modules exhibit the same themal behaviour.
    +   
    +   Source:
    +   Internal Resistance:
    +   Nikolian, Alexandros, et al. "Complete cell-level lithium-ion electrical ECM model 
    +   for different chemistries (NMC, LFP, LTO) and temperatures (− 5° C to 45° C)–
    +   Optimized modelling techniques." International Journal of Electrical Power &
    +   Energy Systems 98 (2018): 133-146.
    +  
    +   Voltage:
    +   Chen, M. and Rincon-Mora, G. A., "Accurate Electrical
    +   Battery Model Capable of Predicting Runtime and I - V Performance" IEEE
    +   Transactions on Energy Conversion, Vol. 21, No. 2, June 2006, pp. 504-511
    +   
    +   Inputs:
    +     battery. 
    +   I_bat             (max_energy)                          [Joules]
    +   cell_mass         (battery cell mass)                   [kilograms]
    +   Cp                (battery cell specific heat capacity) [J/(K kg)] 
    +   E_max             (max energy)                          [Joules]
    +   E_current         (current energy)                      [Joules]
    +   Q_prior           (charge throughput)                   [Amp-hrs]
    +   R_growth_factor   (internal resistance growth factor)   [unitless]
    +   E_growth_factor   (capactance (energy) growth factor)   [unitless] 
    +       
    +     inputs.
    +   I_bat             (current)                             [amps]
    +   P_bat             (power)                               [Watts]
    +   
    +   Outputs:
    +     battery.          
    +  current_energy                                           [Joules]
    +  cell_temperature                                         [Kelvin]
    +  resistive_losses                                         [Watts] 
    +  load_power                                               [Watts]
    +  current                                                  [Amps]
    +  battery_voltage_open_circuit                             [Volts]
    +  cell_charge_throughput                                   [Amp-hrs]
    +  internal_resistance                                      [Ohms]
    +  battery_state_of_charge                                  [unitless]
    +  depth_of_discharge                                       [unitless]
    +  battery_voltage_under_load                               [Volts]   
    +

    Reimplemented in SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion_LiNiMnCoO2_18650.Lithium_Ion_LiNiMnCoO2_18650.

    + +
    +
    +
    The documentation for this class was generated from the following file:
    • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Energy/Storages/Batteries/Constant_Mass/Lithium_Ion.py
    @@ -209,7 +620,7 @@ + doxygen 1.8.15
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+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion_LiFePO4_18650.Lithium_Ion_LiFePO4_18650 Member List
+
+
+ +

This is the complete list of members for SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion_LiFePO4_18650.Lithium_Ion_LiFePO4_18650, including all inherited members.

+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
__defaults__(self)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion_LiFePO4_18650.Lithium_Ion_LiFePO4_18650
age (defined in SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion
append_battery_residuals(self, segment, network)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion
append_battery_unknowns(self, segment)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion
append_battery_unknowns_and_residuals_to_segment(self, segment, initial_voltage, initial_battery_cell_temperature, initial_battery_state_of_charge, initial_battery_cell_current)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion
cell (defined in SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion
chemistry (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
compute_voltage(self, state)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion
convective_heat_transfer_coefficient (defined in SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion
cooling_fluid (defined in SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion
current_capacitor_charge (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
current_energy (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
discharge_performance_map (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
energy_calc(self, numerics, battery_discharge_flag=True)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion
energy_density (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
heat_transfer_efficiency (defined in SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion
initial_temperature (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
max_energy (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
max_power (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
max_voltage (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
module (defined in SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion
module_config (defined in SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
pack_config (defined in SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion
ragone (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
resistance (defined in SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion_LiFePO4_18650.Lithium_Ion_LiFePO4_18650)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion_LiFePO4_18650.Lithium_Ion_LiFePO4_18650
specific_energy (defined in SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion_LiFePO4_18650.Lithium_Ion_LiFePO4_18650)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion_LiFePO4_18650.Lithium_Ion_LiFePO4_18650
specific_heat_capacity (defined in SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion_LiFePO4_18650.Lithium_Ion_LiFePO4_18650)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion_LiFePO4_18650.Lithium_Ion_LiFePO4_18650
specific_power (defined in SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion_LiFePO4_18650.Lithium_Ion_LiFePO4_18650)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion_LiFePO4_18650.Lithium_Ion_LiFePO4_18650
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion_LiFePO4_18650.Lithium_Ion_LiFePO4_18650)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion_LiFePO4_18650.Lithium_Ion_LiFePO4_18650
update_battery_state_of_health(self, segment, increment_battery_cycle_day=False) (defined in SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion
watt_hour_rating (defined in SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion_LiFePO4_18650.Lithium_Ion_LiFePO4_18650)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion_LiFePO4_18650.Lithium_Ion_LiFePO4_18650
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Constant__Mass_1_1Lithium__Ion__Lb658a67ca689f30f162c48dfa2560f8c.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Constant__Mass_1_1Lithium__Ion__Lb658a67ca689f30f162c48dfa2560f8c.html new file mode 100644 index 00000000..e83a6c65 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Constant__Mass_1_1Lithium__Ion__Lb658a67ca689f30f162c48dfa2560f8c.html @@ -0,0 +1,158 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion_LiNiMnCoO2_18650.Lithium_Ion_LiNiMnCoO2_18650 Member List
+
+
+ +

This is the complete list of members for SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion_LiNiMnCoO2_18650.Lithium_Ion_LiNiMnCoO2_18650, including all inherited members.

+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
__defaults__(self)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion_LiNiMnCoO2_18650.Lithium_Ion_LiNiMnCoO2_18650
age (defined in SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion
append_battery_residuals(self, segment, network)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion_LiNiMnCoO2_18650.Lithium_Ion_LiNiMnCoO2_18650
append_battery_unknowns(self, segment)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion_LiNiMnCoO2_18650.Lithium_Ion_LiNiMnCoO2_18650
append_battery_unknowns_and_residuals_to_segment(self, segment, initial_voltage, initial_battery_cell_temperature, initial_battery_state_of_charge, initial_battery_cell_current)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion_LiNiMnCoO2_18650.Lithium_Ion_LiNiMnCoO2_18650
cell (defined in SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion
chemistry (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
compute_voltage(self, state)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion_LiNiMnCoO2_18650.Lithium_Ion_LiNiMnCoO2_18650
convective_heat_transfer_coefficient (defined in SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion
cooling_fluid (defined in SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion
current_capacitor_charge (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
current_energy (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
discharge_performance_map (defined in SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion_LiNiMnCoO2_18650.Lithium_Ion_LiNiMnCoO2_18650)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion_LiNiMnCoO2_18650.Lithium_Ion_LiNiMnCoO2_18650
energy_calc(self, numerics, battery_discharge_flag=True)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion_LiNiMnCoO2_18650.Lithium_Ion_LiNiMnCoO2_18650
energy_density (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
heat_transfer_efficiency (defined in SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion
initial_temperature (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
max_energy (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
max_power (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
max_voltage (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
module (defined in SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion
module_config (defined in SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
pack_config (defined in SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion
ragone (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
resistance (defined in SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion_LiNiMnCoO2_18650.Lithium_Ion_LiNiMnCoO2_18650)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion_LiNiMnCoO2_18650.Lithium_Ion_LiNiMnCoO2_18650
specific_energy (defined in SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion_LiNiMnCoO2_18650.Lithium_Ion_LiNiMnCoO2_18650)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion_LiNiMnCoO2_18650.Lithium_Ion_LiNiMnCoO2_18650
specific_heat_capacity (defined in SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion_LiNiMnCoO2_18650.Lithium_Ion_LiNiMnCoO2_18650)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion_LiNiMnCoO2_18650.Lithium_Ion_LiNiMnCoO2_18650
specific_power (defined in SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion_LiNiMnCoO2_18650.Lithium_Ion_LiNiMnCoO2_18650)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion_LiNiMnCoO2_18650.Lithium_Ion_LiNiMnCoO2_18650
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion_LiNiMnCoO2_18650.Lithium_Ion_LiNiMnCoO2_18650)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion_LiNiMnCoO2_18650.Lithium_Ion_LiNiMnCoO2_18650
update_battery_state_of_health(self, segment, increment_battery_cycle_day=False)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion_LiNiMnCoO2_18650.Lithium_Ion_LiNiMnCoO2_18650
watt_hour_rating (defined in SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion_LiNiMnCoO2_18650.Lithium_Ion_LiNiMnCoO2_18650)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion_LiNiMnCoO2_18650.Lithium_Ion_LiNiMnCoO2_18650
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Constant__Mass_1_1Lithium__Ion__Lc7c774ecc0e754e494e2e31ae8c98a5c.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Constant__Mass_1_1Lithium__Ion__Lc7c774ecc0e754e494e2e31ae8c98a5c.html new file mode 100644 index 00000000..e85ce854 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Constant__Mass_1_1Lithium__Ion__Lc7c774ecc0e754e494e2e31ae8c98a5c.html @@ -0,0 +1,358 @@ + + + + + + + +SUAVE: SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion_LiFePO4_18650.Lithium_Ion_LiFePO4_18650 Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion_LiFePO4_18650.Lithium_Ion_LiFePO4_18650 Class Reference
+
+
+
+Inheritance diagram for SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion_LiFePO4_18650.Lithium_Ion_LiFePO4_18650:
+
+
+ + +SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion +SUAVE.Components.Energy.Storages.Batteries.Battery.Battery +SUAVE.Components.Energy.Energy_Component.Energy_Component +SUAVE.Components.Physical_Component.Physical_Component +SUAVE.Components.Component.Component + +
+ + + + + + + + + + + + + + + + + +

+Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion
def energy_calc (self, numerics, battery_discharge_flag=True)
 
def append_battery_unknowns (self, segment)
 
def append_battery_residuals (self, segment, network)
 
def append_battery_unknowns_and_residuals_to_segment (self, segment, initial_voltage, initial_battery_cell_temperature, initial_battery_state_of_charge, initial_battery_cell_current)
 
def compute_voltage (self, state)
 
+def update_battery_state_of_health (self, segment, increment_battery_cycle_day=False)
 
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Attributes

tag
 
watt_hour_rating
 
specific_energy
 
specific_power
 
resistance
 
specific_heat_capacity
 
- Public Attributes inherited from SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion
tag
 
cell
 
module
 
pack_config
 
module_config
 
age
 
convective_heat_transfer_coefficient
 
heat_transfer_efficiency
 
cooling_fluid
 
specific_energy
 
specific_power
 
- Public Attributes inherited from SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
chemistry
 
energy_density
 
current_energy
 
initial_temperature
 
current_capacitor_charge
 
resistance
 
specific_heat_capacity
 
max_energy
 
max_power
 
max_voltage
 
discharge_performance_map
 
ragone
 
- Public Attributes inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
inputs
 
outputs
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 
+

Detailed Description

+
Specifies discharge/specific energy characteristics specific 
+    18650 lithium-iron-phosphate-oxide battery cells.     
+    
+    Assumptions: 
+    N/A 
+    
+    Source:
+    # Cell Information 
+    Saw, L. H., Yonghuang Ye, and A. A. O. Tay. "Electrochemical–thermal analysis of 
+    18650 Lithium Iron Phosphate cell." Energy Conversion and Management 75 (2013): 
+    162-174.
+    
+    # Electrode Area
+    Muenzel, Valentin, et al. "A comparative testing study of commercial
+    18650-format lithium-ion battery cells." Journal of The Electrochemical
+    Society 162.8 (2015): A1592.
+    
+    # Cell Thermal Conductivities 
+    (radial)
+    Murashko, Kirill A., Juha Pyrhönen, and Jorma Jokiniemi. "Determination of the 
+    through-plane thermal conductivity and specific heat capacity of a Li-ion cylindrical 
+    cell." International Journal of Heat and Mass Transfer 162 (2020): 120330.
+    
+    (axial)
+    Saw, L. H., Yonghuang Ye, and A. A. O. Tay. "Electrochemical–thermal analysis of 
+    18650 Lithium Iron Phosphate cell." Energy Conversion and Management 75 (2013): 
+    162-174.
+    
+    Inputs:
+    None
+    
+    Outputs:
+    None
+    
+    Properties Used:
+    N/A

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion_LiFePO4_18650.Lithium_Ion_LiFePO4_18650.__defaults__ ( self)
+
+
This sets the default inputs and outputs data structure.
+
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+None
+
+Outputs:
+None
+
+Properties Used:
+N/A
+
+

Reimplemented from SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion.

+ +
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Energy/Storages/Batteries/Constant_Mass/Lithium_Ion_LiFePO4_18650.py
  • +
+
+
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+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion_LiNiMnCoO2_18650.Lithium_Ion_LiNiMnCoO2_18650 Class Reference
+
+
+
+Inheritance diagram for SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion_LiNiMnCoO2_18650.Lithium_Ion_LiNiMnCoO2_18650:
+
+
+ + +SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion +SUAVE.Components.Energy.Storages.Batteries.Battery.Battery +SUAVE.Components.Energy.Energy_Component.Energy_Component +SUAVE.Components.Physical_Component.Physical_Component +SUAVE.Components.Component.Component + +
+ + + + + + + + + + + + + + + + +

+Public Member Functions

def __defaults__ (self)
 
def energy_calc (self, numerics, battery_discharge_flag=True)
 
def append_battery_unknowns (self, segment)
 
def append_battery_residuals (self, segment, network)
 
def append_battery_unknowns_and_residuals_to_segment (self, segment, initial_voltage, initial_battery_cell_temperature, initial_battery_state_of_charge, initial_battery_cell_current)
 
def compute_voltage (self, state)
 
def update_battery_state_of_health (self, segment, increment_battery_cycle_day=False)
 
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Attributes

tag
 
watt_hour_rating
 
specific_energy
 
specific_power
 
resistance
 
specific_heat_capacity
 
discharge_performance_map
 
- Public Attributes inherited from SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion
tag
 
cell
 
module
 
pack_config
 
module_config
 
age
 
convective_heat_transfer_coefficient
 
heat_transfer_efficiency
 
cooling_fluid
 
specific_energy
 
specific_power
 
- Public Attributes inherited from SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
chemistry
 
energy_density
 
current_energy
 
initial_temperature
 
current_capacitor_charge
 
resistance
 
specific_heat_capacity
 
max_energy
 
max_power
 
max_voltage
 
discharge_performance_map
 
ragone
 
- Public Attributes inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
inputs
 
outputs
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 
+

Detailed Description

+
Specifies discharge/specific energy characteristics specific 
+    18650 lithium-nickel-manganese-cobalt-oxide battery cells     
+    
+    Assumptions:
+    Convective Thermal Conductivity Coefficient corresponds to forced
+    air cooling in 35 m/s air 
+    
+    Source:
+    Automotive Industrial Systems Company of Panasonic Group, Technical Information of 
+    NCR18650G, URL https://www.imrbatteries.com/content/panasonic_ncr18650g.pdf
+    
+    convective  heat transfer coefficient, h 
+    Jeon, Dong Hyup, and Seung Man Baek. "Thermal modeling of cylindrical 
+    lithium ion battery during discharge cycle." Energy Conversion and Management
+    52.8-9 (2011): 2973-2981.
+    
+    thermal conductivity, k 
+    Yang, Shuting, et al. "A Review of Lithium-Ion Battery Thermal Management 
+    System Strategies and the Evaluate Criteria." Int. J. Electrochem. Sci 14
+    (2019): 6077-6107.
+    
+    specific heat capacity, Cp
+    (axial and radial)
+    Yang, Shuting, et al. "A Review of Lithium-Ion Battery Thermal Management 
+    System Strategies and the Evaluate Criteria." Int. J. Electrochem. Sci 14
+    (2019): 6077-6107.
+    
+    # Electrode Area
+    Muenzel, Valentin, et al. "A comparative testing study of commercial
+    18650-format lithium-ion battery cells." Journal of The Electrochemical
+    Society 162.8 (2015): A1592.
+    
+    Inputs:
+    None
+    
+    Outputs:
+    None
+    
+    Properties Used:
+    N/A
+

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion_LiNiMnCoO2_18650.Lithium_Ion_LiNiMnCoO2_18650.__defaults__ ( self)
+
+
This sets the default inputs and outputs data structure.
+
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+None
+
+Outputs:
+None
+
+Properties Used:
+N/A
+
+

Reimplemented from SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion.

+ +
+
+ +

◆ append_battery_residuals()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion_LiNiMnCoO2_18650.Lithium_Ion_LiNiMnCoO2_18650.append_battery_residuals ( self,
 segment,
 network 
)
+
+
Packs the residuals specific to NMC cells to be sent to the mission solver.
+    
+    Assumptions:
+    None
+    
+    Source:
+    N/A
+    
+    Inputs:
+    segment.state.conditions.propulsion:
+battery_state_of_charge      [unitless] 
+battery_cell_temperature     [Kelvin]        
+battery_current              [Amperes]
+    segment.state.unknowns.
+battery_state_of_charge      [unitless]
+battery_cell_temperature     [Kelvin]  
+battery_current              [Amperes]
+    Outputs:
+    None
+    
+    Properties Used:
+    None
+
+

Reimplemented from SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion.

+ +
+
+ +

◆ append_battery_unknowns()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion_LiNiMnCoO2_18650.Lithium_Ion_LiNiMnCoO2_18650.append_battery_unknowns ( self,
 segment 
)
+
+
Appends unknowns specific to NMC cells which are unpacked from the mission solver and send to the network.
+    
+    Assumptions:
+    None
+    
+    Source:
+    N/A
+    
+    Inputs:
+    segment.state.unknowns.battery_cell_temperature   [Kelvin]
+    segment.state.unknowns.battery_state_of_charge    [unitless]
+    segment.state.unknowns.battery_current            [Amperes]
+    
+    Outputs: 
+    segment.state.conditions.propulsion.battery_cell_temperature  [Kelvin]  
+    segment.state.conditions.propulsion.battery_state_of_charge   [unitless]
+    segment.state.conditions.propulsion.battery_current           [Amperes]
+    
+    Properties Used:
+    N/A
+
+

Reimplemented from SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion.

+ +
+
+ +

◆ append_battery_unknowns_and_residuals_to_segment()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion_LiNiMnCoO2_18650.Lithium_Ion_LiNiMnCoO2_18650.append_battery_unknowns_and_residuals_to_segment ( self,
 segment,
 initial_voltage,
 initial_battery_cell_temperature,
 initial_battery_state_of_charge,
 initial_battery_cell_current 
)
+
+
Sets up the information that the mission needs to run a mission segment using this network
+    
+    Assumptions:
+    None
+    
+    Source:
+    N/A
+    
+    Inputs:  
+    initial_voltage                       [volts] 
+    initial_battery_cell_temperature      [Kelvin]
+    initial_battery_state_of_charge       [unitless]
+    initial_battery_cell_current          [Amperes]
+    
+    Outputs
+    None
+    
+    Properties Used:
+    N/A
+
+

Reimplemented from SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion.

+ +
+
+ +

◆ compute_voltage()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion_LiNiMnCoO2_18650.Lithium_Ion_LiNiMnCoO2_18650.compute_voltage ( self,
 state 
)
+
+
Computes the voltage of a single NMC cell or a battery pack of NMC cells  
+    
+    Assumptions:
+    None
+    
+    Source:
+    N/A
+    
+    Inputs:  
+self    - battery data structure             [unitless]
+state   - segment unknowns to define voltage [unitless]
+    
+    Outputs
+V_ul    - under-load voltage                 [volts]
+     
+    Properties Used:
+    N/A
+
+

Reimplemented from SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion.

+ +
+
+ +

◆ energy_calc()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion_LiNiMnCoO2_18650.Lithium_Ion_LiNiMnCoO2_18650.energy_calc ( self,
 numerics,
 battery_discharge_flag = True 
)
+
+
This is an electric cycle model for 18650 lithium-nickel-manganese-cobalt-oxide
+   battery cells. The model uses experimental data performed
+   by the Automotive Industrial Systems Company of Panasonic Group 
+      
+   Sources:  
+   Internal Resistance Model:
+   Zou, Y., Hu, X., Ma, H., and Li, S. E., "Combined State of Charge and State of
+   Health estimation over lithium-ion battery cellcycle lifespan for electric 
+   vehicles,"Journal of Power Sources, Vol. 273, 2015, pp. 793-803.
+   doi:10.1016/j.jpowsour.2014.09.146,URLhttp://dx.doi.org/10.1016/j.jpowsour.2014.09.146. 
+    
+   Battery Heat Generation Model and  Entropy Model:
+   Jeon, Dong Hyup, and Seung Man Baek. "Thermal modeling of cylindrical lithium ion 
+   battery during discharge cycle." Energy Conversion and Management 52.8-9 (2011): 
+   2973-2981. 
+   
+   Assumtions:
+   1) All battery modules exhibit the same themal behaviour. 
+   
+   Inputs:
+     battery.
+   I_bat             (max_energy)                          [Joules]
+   cell_mass         (battery cell mass)                   [kilograms]
+   Cp                (battery cell specific heat capacity) [J/(K kg)] 
+   t                 (battery age in days)                 [days] 
+   T_ambient         (ambient temperature)                 [Kelvin]
+   T_current         (pack temperature)                    [Kelvin]
+   T_cell            (battery cell temperature)            [Kelvin]
+   E_max             (max energy)                          [Joules]
+   E_current         (current energy)                      [Joules]
+   Q_prior           (charge throughput)                   [Amp-hrs]
+   R_growth_factor   (internal resistance growth factor)   [unitless]
+   
+     inputs.
+   I_bat             (current)                             [amps]
+   P_bat             (power)                               [Watts]
+   
+   Outputs:
+     battery.
+  current_energy                                           [Joules]
+  cell_temperature                                         [Kelvin]
+  resistive_losses                                         [Watts]
+  load_power                                               [Watts]
+  current                                                  [Amps]
+  battery_voltage_open_circuit                             [Volts]
+  cell_charge_throughput                                   [Amp-hrs]
+  internal_resistance                                      [Ohms]
+  battery_state_of_charge                                  [unitless]
+  depth_of_discharge                                       [unitless]
+  battery_voltage_under_load                               [Volts]
+

Reimplemented from SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion.

+ +
+
+ +

◆ update_battery_state_of_health()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion_LiNiMnCoO2_18650.Lithium_Ion_LiNiMnCoO2_18650.update_battery_state_of_health ( self,
 segment,
 increment_battery_cycle_day = False 
)
+
+
This is an aging model for 18650 lithium-nickel-manganese-cobalt-oxide batteries. 
+       
+Source: 
+Schmalstieg, Johannes, et al. "A holistic aging model for Li (NiMnCo) O2
+based 18650 lithium-ion batteries." Journal of Power Sources 257 (2014): 325-334.
+  
+Assumptions:
+None
+    
+Inputs:
+  segment.conditions.propulsion. 
+     battery_cycle_day                                                      [unitless]
+     battery_cell_temperature                                               [Kelvin] 
+     battery_voltage_open_circuit                                           [Volts] 
+     battery_charge_throughput                                              [Amp-hrs] 
+     battery_state_of_charge                                                [unitless] 
+
+Outputs:
+   segment.conditions.propulsion.
+     battery_capacity_fade_factor     (internal resistance growth factor)   [unitless]
+     battery_resistance_growth_factor (capactance (energy) growth factor)   [unitless]  
+     
+Properties Used:
+N/A 
+
+

Reimplemented from SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion.

+ +
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Energy/Storages/Batteries/Constant_Mass/Lithium_Ion_LiNiMnCoO2_18650.py
  • +
+
+
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SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -98,21 +105,27 @@

This is the complete list of members for SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Sulfur.Lithium_Sulfur, including all inherited members.

- + + + - - - - - - - - - - - - - + + + + + + + + + + + + + + + + + @@ -123,7 +136,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Constant__Mass_1_1Lithium__Sulfur_1_1Lithium__Sulfur.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Constant__Mass_1_1Lithium__Sulfur_1_1Lithium__Sulfur.html index ad5d112e..5140a0e6 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Constant__Mass_1_1Lithium__Sulfur_1_1Lithium__Sulfur.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Constant__Mass_1_1Lithium__Sulfur_1_1Lithium__Sulfur.html @@ -1,9 +1,9 @@ - + - +SUAVE: SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Sulfur.Lithium_Sulfur Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ @@ -57,9 +60,11 @@
__defaults__(self) (defined in SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Sulfur.Lithium_Sulfur)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Sulfur.Lithium_Sulfur
__defaults__(self)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Sulfur.Lithium_Sulfur
chemistry (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
current_capacitor_charge (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
current_energy (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
discharge_model (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
energy_calc(self, numerics) (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
energy_density (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
max_energy (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
max_power (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
max_voltage (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
ragone (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
resistance (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
specific_energy (defined in SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Sulfur.Lithium_Sulfur)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Sulfur.Lithium_Sulfur
discharge_performance_map (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
energy_density (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
initial_temperature (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
max_energy (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
max_power (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
max_voltage (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
ragone (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
resistance (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
specific_energy (defined in SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Sulfur.Lithium_Sulfur)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Sulfur.Lithium_Sulfur
specific_heat_capacity (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
specific_power (defined in SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Sulfur.Lithium_Sulfur)SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Sulfur.Lithium_Sulfur
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -109,30 +116,13 @@ SUAVE.Components.Energy.Energy_Component.Energy_Component SUAVE.Components.Physical_Component.Physical_Component SUAVE.Components.Component.Component - -
+ + - + - - - - - - - - - - - - - -

Public Member Functions

-def __defaults__ (self)
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
-def __defaults__ (self)
 
-def energy_calc (self, numerics)
 
- Public Member Functions inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
@@ -143,15 +133,27 @@   + + + + + + + + @@ -161,9 +163,9 @@ - - + + @@ -194,11 +196,57 @@ + + + + + +

Public Attributes

specific_power
 
- Public Attributes inherited from SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
chemistry
 
 energy_density
 
 current_energy
 
initial_temperature
 
current_capacitor_charge
 
 resistance
 
specific_heat_capacity
 
 max_energy
 
 max_voltage
 
discharge_model
 
discharge_performance_map
 
 ragone
 
 origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 

Detailed Description

Specifies discharge/specific energy characteristics specific to
 lithium-ion batteries
-

The documentation for this class was generated from the following file:
    +

    Member Function Documentation

    + +

    ◆ __defaults__()

    + +
    +
    + + + + + + + + +
    def SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Sulfur.Lithium_Sulfur.__defaults__ ( self)
    +
    +
    This sets the default inputs and outputs data structure.
    +
    +Assumptions:
    +None
    +
    +Source:
    +N/A
    +
    +Inputs:
    +None
    +
    +Outputs:
    +None
    +
    +Properties Used:
    +N/A
    +
    +

    Reimplemented from SUAVE.Components.Energy.Storages.Batteries.Battery.Battery.

    + +
    +
    +
    The documentation for this class was generated from the following file:
    • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Energy/Storages/Batteries/Constant_Mass/Lithium_Sulfur.py
    @@ -209,7 +257,7 @@ + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Variable__Mass_1_1Aluminum__Air_1_1Aluminum__Air-members.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Variable__Mass_1_1Aluminum__Air_1_1Aluminum__Air-members.html index 9c15e79e..e18c3605 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Variable__Mass_1_1Aluminum__Air_1_1Aluminum__Air-members.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Variable__Mass_1_1Aluminum__Air_1_1Aluminum__Air-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -98,25 +105,31 @@

This is the complete list of members for SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Aluminum_Air.Aluminum_Air, including all inherited members.

- + + + - - - - - - - - - - - - - - - - + + + + + + + + + + + + + + + + + + + + @@ -128,7 +141,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Variable__Mass_1_1Aluminum__Air_1_1Aluminum__Air.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Variable__Mass_1_1Aluminum__Air_1_1Aluminum__Air.html index 0bdb5eb3..757132ac 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Variable__Mass_1_1Aluminum__Air_1_1Aluminum__Air.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Variable__Mass_1_1Aluminum__Air_1_1Aluminum__Air.html @@ -1,9 +1,9 @@ - + - +SUAVE: SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Aluminum_Air.Aluminum_Air Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ @@ -57,9 +60,11 @@
__defaults__(self) (defined in SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Aluminum_Air.Aluminum_Air)SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Aluminum_Air.Aluminum_Air
__defaults__(self)SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Aluminum_Air.Aluminum_Air
aluminum_mass_factor (defined in SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Aluminum_Air.Aluminum_Air)SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Aluminum_Air.Aluminum_Air
chemistry (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
current_capacitor_charge (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
current_energy (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
discharge_model (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
energy_calc(self, numerics) (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
energy_density (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
find_aluminum_mass(self, energy) (defined in SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Aluminum_Air.Aluminum_Air)SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Aluminum_Air.Aluminum_Air
find_water_mass(self, energy) (defined in SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Aluminum_Air.Aluminum_Air)SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Aluminum_Air.Aluminum_Air
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
mass_gain_factor (defined in SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Aluminum_Air.Aluminum_Air)SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Aluminum_Air.Aluminum_Air
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
max_energy (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
max_power (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
max_voltage (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
ragone (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
resistance (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
specific_energy (defined in SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Aluminum_Air.Aluminum_Air)SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Aluminum_Air.Aluminum_Air
discharge_performance_map (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
energy_density (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
find_aluminum_mass(self, energy) (defined in SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Aluminum_Air.Aluminum_Air)SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Aluminum_Air.Aluminum_Air
find_water_mass(self, energy) (defined in SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Aluminum_Air.Aluminum_Air)SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Aluminum_Air.Aluminum_Air
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
initial_temperature (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
mass_gain_factor (defined in SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Aluminum_Air.Aluminum_Air)SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Aluminum_Air.Aluminum_Air
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
max_energy (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
max_power (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
max_voltage (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
ragone (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
resistance (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
specific_energy (defined in SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Aluminum_Air.Aluminum_Air)SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Aluminum_Air.Aluminum_Air
specific_heat_capacity (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
specific_power (defined in SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Aluminum_Air.Aluminum_Air)SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Aluminum_Air.Aluminum_Air
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -109,13 +116,12 @@ SUAVE.Components.Energy.Energy_Component.Energy_Component SUAVE.Components.Physical_Component.Physical_Component SUAVE.Components.Component.Component - -
+ + - + @@ -123,22 +129,6 @@ - - - - - - - - - - - - - -

Public Member Functions

-def __defaults__ (self)
def __defaults__ (self)
 
def find_water_mass (self, energy)
def find_aluminum_mass (self, energy)
 
- Public Member Functions inherited from SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
-def __defaults__ (self)
 
-def energy_calc (self, numerics)
 
- Public Member Functions inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
@@ -158,15 +148,27 @@   + + + + + + + + @@ -176,9 +178,9 @@ - - + + @@ -209,12 +211,58 @@ + + + + + +

Public Attributes

aluminum_mass_factor
 
- Public Attributes inherited from SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
chemistry
 
 energy_density
 
 current_energy
 
initial_temperature
 
current_capacitor_charge
 
 resistance
 
specific_heat_capacity
 
 max_energy
 
 max_voltage
 
discharge_model
 
discharge_performance_map
 
 ragone
 
 origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 

Detailed Description

Specifies discharge/specific energy characteristics specific to
 aluminum-air batteries. Also includes parameters related to 
 consumption of aluminum, oxygen, and water
-

The documentation for this class was generated from the following file:
    +

    Member Function Documentation

    + +

    ◆ __defaults__()

    + +
    +
    + + + + + + + + +
    def SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Aluminum_Air.Aluminum_Air.__defaults__ ( self)
    +
    +
    This sets the default inputs and outputs data structure.
    +
    +Assumptions:
    +None
    +
    +Source:
    +N/A
    +
    +Inputs:
    +None
    +
    +Outputs:
    +None
    +
    +Properties Used:
    +N/A
    +
    +

    Reimplemented from SUAVE.Components.Energy.Storages.Batteries.Battery.Battery.

    + +
    +
    +
    The documentation for this class was generated from the following file:
    • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Energy/Storages/Batteries/Variable_Mass/Aluminum_Air.py
    @@ -225,7 +273,7 @@ + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Variable__Mass_1_1Lithium__Air_1_1Lithium__Air-members.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Variable__Mass_1_1Lithium__Air_1_1Lithium__Air-members.html index 32c53267..1ee41e20 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Variable__Mass_1_1Lithium__Air_1_1Lithium__Air-members.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Variable__Mass_1_1Lithium__Air_1_1Lithium__Air-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -98,22 +105,28 @@

This is the complete list of members for SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Lithium_Air.Lithium_Air, including all inherited members.

- + + + - - - - - - - - - - - - - - + + + + + + + + + + + + + + + + + + @@ -124,7 +137,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Variable__Mass_1_1Lithium__Air_1_1Lithium__Air.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Variable__Mass_1_1Lithium__Air_1_1Lithium__Air.html index 9f07d588..93aae315 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Variable__Mass_1_1Lithium__Air_1_1Lithium__Air.html +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Variable__Mass_1_1Lithium__Air_1_1Lithium__Air.html @@ -1,9 +1,9 @@ - + - +SUAVE: SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Lithium_Air.Lithium_Air Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ @@ -57,9 +60,11 @@
__defaults__(self) (defined in SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Lithium_Air.Lithium_Air)SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Lithium_Air.Lithium_Air
__defaults__(self)SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Lithium_Air.Lithium_Air
chemistry (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
current_capacitor_charge (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
current_energy (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
discharge_model (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
energy_calc(self, numerics) (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
energy_density (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
mass_gain_factor (defined in SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Lithium_Air.Lithium_Air)SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Lithium_Air.Lithium_Air
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
max_energy (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
max_power (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
max_voltage (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
ragone (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
resistance (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
specific_energy (defined in SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Lithium_Air.Lithium_Air)SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Lithium_Air.Lithium_Air
discharge_performance_map (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
energy_density (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
initial_temperature (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
mass_gain_factor (defined in SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Lithium_Air.Lithium_Air)SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Lithium_Air.Lithium_Air
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
max_energy (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
max_power (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
max_voltage (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
ragone (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
resistance (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
specific_energy (defined in SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Lithium_Air.Lithium_Air)SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Lithium_Air.Lithium_Air
specific_heat_capacity (defined in SUAVE.Components.Energy.Storages.Batteries.Battery.Battery)SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
specific_power (defined in SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Lithium_Air.Lithium_Air)SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Lithium_Air.Lithium_Air
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -109,30 +116,13 @@ SUAVE.Components.Energy.Energy_Component.Energy_Component SUAVE.Components.Physical_Component.Physical_Component SUAVE.Components.Component.Component - -
+ + - + - - - - - - - - - - - - - -

Public Member Functions

-def __defaults__ (self)
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
-def __defaults__ (self)
 
-def energy_calc (self, numerics)
 
- Public Member Functions inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
@@ -146,15 +136,27 @@   + + + + + + + + @@ -164,9 +166,9 @@ - - + + @@ -197,12 +199,58 @@ + + + + + +

Public Attributes

mass_gain_factor
 
- Public Attributes inherited from SUAVE.Components.Energy.Storages.Batteries.Battery.Battery
chemistry
 
 energy_density
 
 current_energy
 
initial_temperature
 
current_capacitor_charge
 
 resistance
 
specific_heat_capacity
 
 max_energy
 
 max_voltage
 
discharge_model
 
discharge_performance_map
 
 ragone
 
 origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 

Detailed Description

Specifies specific energy characteristics specific to
 lithium-air batteries. Also includes parameters related to 
 consumption of oxygen
-

The documentation for this class was generated from the following file:
    +

    Member Function Documentation

    + +

    ◆ __defaults__()

    + +
    +
    + + + + + + + + +
    def SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Lithium_Air.Lithium_Air.__defaults__ ( self)
    +
    +
    This sets the default inputs and outputs data structure.
    +
    +Assumptions:
    +None
    +
    +Source:
    +N/A
    +
    +Inputs:
    +None
    +
    +Outputs:
    +None
    +
    +Properties Used:
    +N/A
    +
    +

    Reimplemented from SUAVE.Components.Energy.Storages.Batteries.Battery.Battery.

    + +
    +
    +
    The documentation for this class was generated from the following file:
    • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Energy/Storages/Batteries/Variable_Mass/Lithium_Air.py
    @@ -213,7 +261,7 @@ + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Fuel__Tanks_1_1Fuel__Tank_1_1Fuel__Tank-members.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Fuel__Tanks_1_1Fuel__Tank_1_1Fuel__Tank-members.html new file mode 100644 index 00000000..9b7d19e6 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Fuel__Tanks_1_1Fuel__Tank_1_1Fuel__Tank-members.html @@ -0,0 +1,130 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
SUAVE.Components.Energy.Storages.Fuel_Tanks.Fuel_Tank.Fuel_Tank Member List
+
+
+ +

This is the complete list of members for SUAVE.Components.Energy.Storages.Fuel_Tanks.Fuel_Tank.Fuel_Tank, including all inherited members.

+ + + + + + + + + + + + +
__defaults__(self)SUAVE.Components.Energy.Storages.Fuel_Tanks.Fuel_Tank.Fuel_Tank
fuel_type (defined in SUAVE.Components.Energy.Storages.Fuel_Tanks.Fuel_Tank.Fuel_Tank)SUAVE.Components.Energy.Storages.Fuel_Tanks.Fuel_Tank.Fuel_Tank
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
inputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
outputs (defined in SUAVE.Components.Energy.Energy_Component.Energy_Component)SUAVE.Components.Energy.Energy_Component.Energy_Component
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Fuel__Tanks_1_1Fuel__Tank_1_1Fuel__Tank.html b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Fuel__Tanks_1_1Fuel__Tank_1_1Fuel__Tank.html new file mode 100644 index 00000000..59bcd65a --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Fuel__Tanks_1_1Fuel__Tank_1_1Fuel__Tank.html @@ -0,0 +1,223 @@ + + + + + + + +SUAVE: SUAVE.Components.Energy.Storages.Fuel_Tanks.Fuel_Tank.Fuel_Tank Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Components.Energy.Storages.Fuel_Tanks.Fuel_Tank.Fuel_Tank Class Reference
+
+
+
+Inheritance diagram for SUAVE.Components.Energy.Storages.Fuel_Tanks.Fuel_Tank.Fuel_Tank:
+
+
+ + +SUAVE.Components.Energy.Energy_Component.Energy_Component +SUAVE.Components.Physical_Component.Physical_Component +SUAVE.Components.Component.Component + +
+ + + + +

+Public Member Functions

def __defaults__ (self)
 
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Attributes

fuel_type
 
- Public Attributes inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
inputs
 
outputs
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 
+

Detailed Description

+
Energy Component object that stores fuel. Contains values
+used to indicate its fuel type.
+

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Components.Energy.Storages.Fuel_Tanks.Fuel_Tank.Fuel_Tank.__defaults__ ( self)
+
+
This sets the default inputs and outputs data structure.
+
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+None
+
+Outputs:
+None
+
+Properties Used:
+N/A
+
+

Reimplemented from SUAVE.Components.Energy.Energy_Component.Energy_Component.

+ +
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Energy/Storages/Fuel_Tanks/Fuel_Tank.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Fuel__Tanks_1_1Fuel__Tank_1_1Fuel__Tank.js b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Fuel__Tanks_1_1Fuel__Tank_1_1Fuel__Tank.js new file mode 100644 index 00000000..8083c6cb --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Fuel__Tanks_1_1Fuel__Tank_1_1Fuel__Tank.js @@ -0,0 +1,5 @@ +var classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Fuel__Tanks_1_1Fuel__Tank_1_1Fuel__Tank = +[ + [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Fuel__Tanks_1_1Fuel__Tank_1_1Fuel__Tank.html#a0fae30e144620337fe56cb161153de00", null ], + [ "fuel_type", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Fuel__Tanks_1_1Fuel__Tank_1_1Fuel__Tank.html#ac9a394b940b40d6f3f7742b37822b38d", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Fuel__Tanks_1_1Fuel__Tank_1_1Fuel__Tank.png b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Fuel__Tanks_1_1Fuel__Tank_1_1Fuel__Tank.png new file mode 100644 index 00000000..46e9454f Binary files /dev/null and b/doxygen/classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Fuel__Tanks_1_1Fuel__Tank_1_1Fuel__Tank.png differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Envelope_1_1Envelope-members.html b/doxygen/classSUAVE_1_1Components_1_1Envelope_1_1Envelope-members.html index bcb70736..d7d14225 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Envelope_1_1Envelope-members.html +++ b/doxygen/classSUAVE_1_1Components_1_1Envelope_1_1Envelope-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
diff --git a/doxygen/classSUAVE_1_1Components_1_1Envelope_1_1Envelope.html b/doxygen/classSUAVE_1_1Components_1_1Envelope_1_1Envelope.html index 46f23e3b..b7d9ad32 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Envelope_1_1Envelope.html +++ b/doxygen/classSUAVE_1_1Components_1_1Envelope_1_1Envelope.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Components.Envelope.Envelope Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -106,16 +113,13 @@ SUAVE.Components.Component.Component - -
+ + - - -

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
@@ -128,6 +132,9 @@ + + @@ -159,6 +166,15 @@ + + + + + +

Public Attributes

 limit_load
 
limit_loads
 
 alpha_maximum
 
 origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 

Detailed Description

Flight envelope for a vehicle
@@ -201,6 +217,8 @@ 

SUAVE.Components.Component.Component.

+


The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Components_1_1Envelope_1_1Envelope.js b/doxygen/classSUAVE_1_1Components_1_1Envelope_1_1Envelope.js index d4fac5c9..87a35af9 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Envelope_1_1Envelope.js +++ b/doxygen/classSUAVE_1_1Components_1_1Envelope_1_1Envelope.js @@ -6,6 +6,7 @@ var classSUAVE_1_1Components_1_1Envelope_1_1Envelope = [ "alt_vc", "classSUAVE_1_1Components_1_1Envelope_1_1Envelope.html#a9fa1d524f7072f9d99a79b7a4960e59f", null ], [ "gust", "classSUAVE_1_1Components_1_1Envelope_1_1Envelope.html#a817cbf39aeec6758432ee3eab3f4b882", null ], [ "limit_load", "classSUAVE_1_1Components_1_1Envelope_1_1Envelope.html#ad9653f50cbbd9323878da353fe49e6fe", null ], + [ "limit_loads", "classSUAVE_1_1Components_1_1Envelope_1_1Envelope.html#a112b162587abd43e313aede02cfcf9c9", null ], [ "maneuver", "classSUAVE_1_1Components_1_1Envelope_1_1Envelope.html#a49d434a90895935ad7a89d77db9f763e", null ], [ "max_ceiling", "classSUAVE_1_1Components_1_1Envelope_1_1Envelope.html#a3d0278765533a69d81e74c9da73d6677", null ], [ "maximum_dynamic_pressure", "classSUAVE_1_1Components_1_1Envelope_1_1Envelope.html#a510c802653d940134add99ab206a186c", null ], diff --git a/doxygen/classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Container-members.html b/doxygen/classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Container-members.html index 1eea1e49..12df3686 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Container-members.html +++ b/doxygen/classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Container-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -107,7 +116,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Container.html b/doxygen/classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Container.html index e9a8fbb6..c0f1c9d6 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Container.html +++ b/doxygen/classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Container.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Components.Fuselages.Fuselage.Container Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -92,7 +99,7 @@
SUAVE.Components.Fuselages.Fuselage.Container Class Reference
@@ -106,25 +113,61 @@ SUAVE.Components.Physical_Component.Container SUAVE.Components.Component.Container - -
+ + - - - + + + + + + + + +

-Static Public Attributes

Container
 

+Public Member Functions

def get_children (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Container
def sum_mass (self)
 
def total_moment (self)
 
+ -

+Additional Inherited Members

- Static Public Attributes inherited from SUAVE.Components.Component.Container
 Container
 
- - - -

-Additional Inherited Members

- Public Member Functions inherited from SUAVE.Components.Physical_Component.Container
def sum_mass (self)
 
+

Member Function Documentation

+ +

◆ get_children()

+ +
+
+ + + + + + + + +
def SUAVE.Components.Fuselages.Fuselage.Container.get_children ( self)
+
+
Returns the components that can go inside
+
+Assumptions:
+None
+    
+Source:
+N/A
+    
+Inputs:
+None
+    
+Outputs:
+None
+    
+Properties Used:
+N/A
+
+
+

The documentation for this class was generated from the following file:
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Fuselages/Fuselage.py
@@ -136,7 +179,7 @@ + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Container.js b/doxygen/classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Container.js new file mode 100644 index 00000000..28d17b11 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Container.js @@ -0,0 +1,4 @@ +var classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Container = +[ + [ "get_children", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Container.html#a8b77d3fdeab54fe378ba134252f9a424", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage-members.html b/doxygen/classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage-members.html index 65f991d4..e5ffe99a 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage-members.html +++ b/doxygen/classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -102,23 +109,39 @@ aerodynamic_center (defined in SUAVE.Components.Fuselages.Fuselage.Fuselage)SUAVE.Components.Fuselages.Fuselage.Fuselage aft_centerbody_area (defined in SUAVE.Components.Fuselages.Fuselage.Fuselage)SUAVE.Components.Fuselages.Fuselage.Fuselage aft_centerbody_taper (defined in SUAVE.Components.Fuselages.Fuselage.Fuselage)SUAVE.Components.Fuselages.Fuselage.Fuselage + append_fuel_tank(self, fuel_tank)SUAVE.Components.Fuselages.Fuselage.Fuselage + append_segment(self, segment)SUAVE.Components.Fuselages.Fuselage.Fuselage areas (defined in SUAVE.Components.Fuselages.Fuselage.Fuselage)SUAVE.Components.Fuselages.Fuselage.Fuselage cabin_area (defined in SUAVE.Components.Fuselages.Fuselage.Fuselage)SUAVE.Components.Fuselages.Fuselage.Fuselage differential_pressure (defined in SUAVE.Components.Fuselages.Fuselage.Fuselage)SUAVE.Components.Fuselages.Fuselage.Fuselage effective_diameter (defined in SUAVE.Components.Fuselages.Fuselage.Fuselage)SUAVE.Components.Fuselages.Fuselage.Fuselage fineness (defined in SUAVE.Components.Fuselages.Fuselage.Fuselage)SUAVE.Components.Fuselages.Fuselage.Fuselage - heights (defined in SUAVE.Components.Fuselages.Fuselage.Fuselage)SUAVE.Components.Fuselages.Fuselage.Fuselage - lengths (defined in SUAVE.Components.Fuselages.Fuselage.Fuselage)SUAVE.Components.Fuselages.Fuselage.Fuselage - mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component + Fuel_Tanks (defined in SUAVE.Components.Fuselages.Fuselage.Fuselage)SUAVE.Components.Fuselages.Fuselage.Fuselage + generative_design_char_max_bounds (defined in SUAVE.Components.Fuselages.Fuselage.Fuselage)SUAVE.Components.Fuselages.Fuselage.Fuselage + generative_design_char_min_bounds (defined in SUAVE.Components.Fuselages.Fuselage.Fuselage)SUAVE.Components.Fuselages.Fuselage.Fuselage + generative_design_characteristics (defined in SUAVE.Components.Fuselages.Fuselage.Fuselage)SUAVE.Components.Fuselages.Fuselage.Fuselage + generative_design_max_per_vehicle (defined in SUAVE.Components.Fuselages.Fuselage.Fuselage)SUAVE.Components.Fuselages.Fuselage.Fuselage + generative_design_minimum (defined in SUAVE.Components.Fuselages.Fuselage.Fuselage)SUAVE.Components.Fuselages.Fuselage.Fuselage + generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component + heights (defined in SUAVE.Components.Fuselages.Fuselage.Fuselage)SUAVE.Components.Fuselages.Fuselage.Fuselage + lengths (defined in SUAVE.Components.Fuselages.Fuselage.Fuselage)SUAVE.Components.Fuselages.Fuselage.Fuselage + mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component + max_per_vehicle (defined in SUAVE.Components.Fuselages.Fuselage.Fuselage)SUAVE.Components.Fuselages.Fuselage.Fuselage + non_dimensional_origin (defined in SUAVE.Components.Fuselages.Fuselage.Fuselage)SUAVE.Components.Fuselages.Fuselage.Fuselage + nose_curvature (defined in SUAVE.Components.Fuselages.Fuselage.Fuselage)SUAVE.Components.Fuselages.Fuselage.Fuselage number_coach_seats (defined in SUAVE.Components.Fuselages.Fuselage.Fuselage)SUAVE.Components.Fuselages.Fuselage.Fuselage - origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component + origin (defined in SUAVE.Components.Fuselages.Fuselage.Fuselage)SUAVE.Components.Fuselages.Fuselage.Fuselage seat_pitch (defined in SUAVE.Components.Fuselages.Fuselage.Fuselage)SUAVE.Components.Fuselages.Fuselage.Fuselage seats_abreast (defined in SUAVE.Components.Fuselages.Fuselage.Fuselage)SUAVE.Components.Fuselages.Fuselage.Fuselage - Sections (defined in SUAVE.Components.Fuselages.Fuselage.Fuselage)SUAVE.Components.Fuselages.Fuselage.Fuselage - Segments (defined in SUAVE.Components.Fuselages.Fuselage.Fuselage)SUAVE.Components.Fuselages.Fuselage.Fuselage - symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component - tag (defined in SUAVE.Components.Fuselages.Fuselage.Fuselage)SUAVE.Components.Fuselages.Fuselage.Fuselage - width (defined in SUAVE.Components.Fuselages.Fuselage.Fuselage)SUAVE.Components.Fuselages.Fuselage.Fuselage + Segments (defined in SUAVE.Components.Fuselages.Fuselage.Fuselage)SUAVE.Components.Fuselages.Fuselage.Fuselage + symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component + tag (defined in SUAVE.Components.Fuselages.Fuselage.Fuselage)SUAVE.Components.Fuselages.Fuselage.Fuselage + tail_curvature (defined in SUAVE.Components.Fuselages.Fuselage.Fuselage)SUAVE.Components.Fuselages.Fuselage.Fuselage + vsp_data (defined in SUAVE.Components.Fuselages.Fuselage.Fuselage)SUAVE.Components.Fuselages.Fuselage.Fuselage + width (defined in SUAVE.Components.Fuselages.Fuselage.Fuselage)SUAVE.Components.Fuselages.Fuselage.Fuselage + x_rotation (defined in SUAVE.Components.Fuselages.Fuselage.Fuselage)SUAVE.Components.Fuselages.Fuselage.Fuselage + y_rotation (defined in SUAVE.Components.Fuselages.Fuselage.Fuselage)SUAVE.Components.Fuselages.Fuselage.Fuselage + z_rotation (defined in SUAVE.Components.Fuselages.Fuselage.Fuselage)SUAVE.Components.Fuselages.Fuselage.Fuselage
@@ -126,7 +149,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html b/doxygen/classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html index 6e870878..8b225c2d 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html +++ b/doxygen/classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Components.Fuselages.Fuselage.Fuselage Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -108,37 +115,32 @@ SUAVE.Components.Lofted_Body.Lofted_Body SUAVE.Components.Physical_Component.Physical_Component SUAVE.Components.Component.Component - -
+ + - - - - - - - - - + + + +

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Lofted_Body.Lofted_Body
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
def append_segment (self, segment)
 
def append_fuel_tank (self, fuel_tank)
 
+ + - - - - + + @@ -157,9 +159,24 @@ + + + + + + + + + + @@ -178,6 +195,33 @@ + + + + + + + + + + + + + + + + + + @@ -185,9 +229,6 @@ - - @@ -208,6 +249,15 @@ + + + + + +

Public Attributes

 tag
 
origin
 
 aerodynamic_center
 
Sections
 
Segments
 
max_per_vehicle
 
 number_coach_seats
 
 width
 
nose_curvature
 
tail_curvature
 
 heights
 
x_rotation
 
y_rotation
 
z_rotation
 
 lengths
 
 cabin_area
 
non_dimensional_origin
 
generative_design_minimum
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_char_min_bounds
 
generative_design_char_max_bounds
 
Fuel_Tanks
 
vsp_data
 
Segments
 
- Public Attributes inherited from SUAVE.Components.Lofted_Body.Lofted_Body
 tag
 Segments
 
Sections
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
 tag
 origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 

Detailed Description

This is a standard fuselage for a tube and wing aircraft.
@@ -250,6 +300,88 @@ 

SUAVE.Components.Lofted_Body.Lofted_Body.

+ +

+ + +

◆ append_fuel_tank()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Components.Fuselages.Fuselage.Fuselage.append_fuel_tank ( self,
 fuel_tank 
)
+
+
Adds a fuel tank to the fuselage 
+    
+Assumptions:
+None
+Source:
+N/A
+Inputs:
+None
+Outputs:
+None
+Properties Used:
+N/A
+
+
+
+ +

◆ append_segment()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Components.Fuselages.Fuselage.Fuselage.append_segment ( self,
 segment 
)
+
+
Adds a segment to the fuselage. 
+    
+Assumptions:
+None
+Source:
+N/A
+Inputs:
+None
+Outputs:
+None
+Properties Used:
+N/A
+

The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.js b/doxygen/classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.js index b319ebbc..83152b1d 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.js +++ b/doxygen/classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.js @@ -1,6 +1,8 @@ var classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage = [ [ "__defaults__", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#a13a4cd81f10d72cd1bbfbc756d69ca25", null ], + [ "append_fuel_tank", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#a615394f9cefa0cb72b775efa71dde7b3", null ], + [ "append_segment", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#a71849cc67e000a19806a3a134c8de503", null ], [ "aerodynamic_center", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#a804b9a97a7090359a6ba48d636714e1f", null ], [ "aft_centerbody_area", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#ae569f01643b85dfeb3da55275897144d", null ], [ "aft_centerbody_taper", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#a928c49bd07c05f4e278827f08b0a976f", null ], @@ -9,13 +11,27 @@ var classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage = [ "differential_pressure", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#a60e74147869ccd496f8c8185c5d07c09", null ], [ "effective_diameter", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#a79f6884ddd6e0ca4241194b4966d8cf1", null ], [ "fineness", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#afb50945499974ff3306d15d9715bc8f7", null ], + [ "Fuel_Tanks", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#a2b3df4dc373a45db0faa78838b5b39c9", null ], + [ "generative_design_char_max_bounds", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#a786bd2bf623a59a48b6531abcc41f93e", null ], + [ "generative_design_char_min_bounds", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#a012c0557881ba9cb1f9a62c53a77c766", null ], + [ "generative_design_characteristics", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#a8a3e4d4c290d3bd24f6e5ae920dbb72a", null ], + [ "generative_design_max_per_vehicle", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#aab41dc0f6471d0439b4743a509b618ad", null ], + [ "generative_design_minimum", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#a190c2fdb02c38a02cc6bda829401ddd4", null ], [ "heights", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#ae46d1a31c166bca78400a194d3ef3686", null ], [ "lengths", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#acc972f58e4a9f7d1632271f0ed24e1df", null ], + [ "max_per_vehicle", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#a3f3d52098dc33a3f7ce0784c8883cbf5", null ], + [ "non_dimensional_origin", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#a8b7a4f557fcb3743696dd568b15a2b1a", null ], + [ "nose_curvature", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#a2d506f5051ed8803337809e76699aef9", null ], [ "number_coach_seats", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#acc6f517eb0fdec2c551169210492af0c", null ], + [ "origin", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#a2315530edda0fe1b2e9a93f793e50c4b", null ], [ "seat_pitch", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#ab06ac6ecf14ab5ce6b3346d05d2e284d", null ], [ "seats_abreast", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#a779b05b88a125d4ea57d480112384c9f", null ], - [ "Sections", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#a6214ee66b1f87414bc095f9f2587ada7", null ], [ "Segments", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#a60d47dc740536a8703505ce95da44bb3", null ], [ "tag", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#aeb1aab02a525f21939d7b5e5b11375f3", null ], - [ "width", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#a2d18b6bcb752bfb5d39974806c0079e8", null ] + [ "tail_curvature", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#aaef82973d65dfb24addce41293e02253", null ], + [ "vsp_data", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#ac17ea88a9708643456699bf3a980c5fd", null ], + [ "width", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#a2d18b6bcb752bfb5d39974806c0079e8", null ], + [ "x_rotation", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#a9e7dfc07cbbd08d981d59eed910052a4", null ], + [ "y_rotation", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#a57bae7168626693898f7e40286b7fdc9", null ], + [ "z_rotation", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#af2c1b6de77d2a27de9a07555f29c9f39", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Fuselages_1_1Segment_1_1Segment-members.html b/doxygen/classSUAVE_1_1Components_1_1Fuselages_1_1Segment_1_1Segment-members.html new file mode 100644 index 00000000..cfc19747 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Fuselages_1_1Segment_1_1Segment-members.html @@ -0,0 +1,129 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.4.0 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
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+ + +
+ +
+ +
+
+
SUAVE.Components.Fuselages.Segment.Segment Member List
+
+
+ +

This is the complete list of members for SUAVE.Components.Fuselages.Segment.Segment, including all inherited members.

+ + + + + + + + + + + + + + + + + +
__defaults__(self)SUAVE.Components.Fuselages.Segment.Segment
effective_diameter (defined in SUAVE.Components.Fuselages.Segment.Segment)SUAVE.Components.Fuselages.Segment.Segment
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
height (defined in SUAVE.Components.Fuselages.Segment.Segment)SUAVE.Components.Fuselages.Segment.Segment
length (defined in SUAVE.Components.Fuselages.Segment.Segment)SUAVE.Components.Fuselages.Segment.Segment
next (defined in SUAVE.Components.Lofted_Body.Segment)SUAVE.Components.Lofted_Body.Segment
origin (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
percent_x_location (defined in SUAVE.Components.Fuselages.Segment.Segment)SUAVE.Components.Fuselages.Segment.Segment
percent_y_location (defined in SUAVE.Components.Fuselages.Segment.Segment)SUAVE.Components.Fuselages.Segment.Segment
percent_z_location (defined in SUAVE.Components.Fuselages.Segment.Segment)SUAVE.Components.Fuselages.Segment.Segment
prev (defined in SUAVE.Components.Lofted_Body.Segment)SUAVE.Components.Lofted_Body.Segment
tag (defined in SUAVE.Components.Fuselages.Segment.Segment)SUAVE.Components.Fuselages.Segment.Segment
vsp_data (defined in SUAVE.Components.Fuselages.Segment.Segment)SUAVE.Components.Fuselages.Segment.Segment
width (defined in SUAVE.Components.Fuselages.Segment.Segment)SUAVE.Components.Fuselages.Segment.Segment
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Fuselages_1_1Segment_1_1Segment.html b/doxygen/classSUAVE_1_1Components_1_1Fuselages_1_1Segment_1_1Segment.html new file mode 100644 index 00000000..22376bff --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Fuselages_1_1Segment_1_1Segment.html @@ -0,0 +1,227 @@ + + + + + + + +SUAVE: SUAVE.Components.Fuselages.Segment.Segment Class Reference + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.4.0 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
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+ +
+ +
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+ +
+
SUAVE.Components.Fuselages.Segment.Segment Class Reference
+
+
+
+Inheritance diagram for SUAVE.Components.Fuselages.Segment.Segment:
+
+
+ + +SUAVE.Components.Lofted_Body.Segment +SUAVE.Components.Component.Component + +
+ + + + +

+Public Member Functions

def __defaults__ (self)
 
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Attributes

tag
 
percent_x_location
 
percent_y_location
 
percent_z_location
 
height
 
width
 
length
 
effective_diameter
 
vsp_data
 
- Public Attributes inherited from SUAVE.Components.Lofted_Body.Segment
tag
 
prev
 
next
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 
+

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Components.Fuselages.Segment.Segment.__defaults__ ( self)
+
+
This sets the defaults for fuselage segments in SUAVE.
+
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+None
+
+Outputs:
+None
+
+Properties Used:
+N/A
+
+

Reimplemented from SUAVE.Components.Lofted_Body.Segment.

+ +
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/matthewclarke/Documents/SUAVE/SUAVE/trunk/SUAVE/Components/Fuselages/Segment.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Fuselages_1_1Segment_1_1Segment.js b/doxygen/classSUAVE_1_1Components_1_1Fuselages_1_1Segment_1_1Segment.js new file mode 100644 index 00000000..cceba79d --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Fuselages_1_1Segment_1_1Segment.js @@ -0,0 +1,13 @@ +var classSUAVE_1_1Components_1_1Fuselages_1_1Segment_1_1Segment = +[ + [ "__defaults__", "classSUAVE_1_1Components_1_1Fuselages_1_1Segment_1_1Segment.html#aec6bf69e78519cf29395ccb798c329f6", null ], + [ "effective_diameter", "classSUAVE_1_1Components_1_1Fuselages_1_1Segment_1_1Segment.html#afcf60c83c8ce8a802fa82fe4e019743d", null ], + [ "height", "classSUAVE_1_1Components_1_1Fuselages_1_1Segment_1_1Segment.html#a834755bde905392eee894e9414aad3e9", null ], + [ "length", "classSUAVE_1_1Components_1_1Fuselages_1_1Segment_1_1Segment.html#a38aeedd79de1ab7f741dc838a4a1f58a", null ], + [ "percent_x_location", "classSUAVE_1_1Components_1_1Fuselages_1_1Segment_1_1Segment.html#a695cf9fa65ecd350eea69b927adda2f5", null ], + [ "percent_y_location", "classSUAVE_1_1Components_1_1Fuselages_1_1Segment_1_1Segment.html#adc0e99efe47851aa64da77c5ccc6c867", null ], + [ "percent_z_location", "classSUAVE_1_1Components_1_1Fuselages_1_1Segment_1_1Segment.html#a2f90e600315f1c76c96ce0474ec5457c", null ], + [ "tag", "classSUAVE_1_1Components_1_1Fuselages_1_1Segment_1_1Segment.html#a6f43efc31a1062ccd0039b1e3da9d768", null ], + [ "vsp_data", "classSUAVE_1_1Components_1_1Fuselages_1_1Segment_1_1Segment.html#a9f3e5edfc08a825c1fcebacf212c6e4b", null ], + [ "width", "classSUAVE_1_1Components_1_1Fuselages_1_1Segment_1_1Segment.html#a8b153b5580b95829c578821866f3ec30", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Fuselages_1_1Segment_1_1Segment.png b/doxygen/classSUAVE_1_1Components_1_1Fuselages_1_1Segment_1_1Segment.png new file mode 100644 index 00000000..d76cf058 Binary files /dev/null and b/doxygen/classSUAVE_1_1Components_1_1Fuselages_1_1Segment_1_1Segment.png differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Fuselages_1_1Segment_1_1Segment__Container-members.html b/doxygen/classSUAVE_1_1Components_1_1Fuselages_1_1Segment_1_1Segment__Container-members.html new file mode 100644 index 00000000..b9e552f3 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Fuselages_1_1Segment_1_1Segment__Container-members.html @@ -0,0 +1,114 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.4.0 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
SUAVE.Components.Fuselages.Segment.Segment_Container Member List
+
+
+ +

This is the complete list of members for SUAVE.Components.Fuselages.Segment.Segment_Container, including all inherited members.

+ + +
get_children(self)SUAVE.Components.Fuselages.Segment.Segment_Container
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Fuselages_1_1Segment_1_1Segment__Container.html b/doxygen/classSUAVE_1_1Components_1_1Fuselages_1_1Segment_1_1Segment__Container.html new file mode 100644 index 00000000..84da52cd --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Fuselages_1_1Segment_1_1Segment__Container.html @@ -0,0 +1,181 @@ + + + + + + + +SUAVE: SUAVE.Components.Fuselages.Segment.Segment_Container Class Reference + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.4.0 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Components.Fuselages.Segment.Segment_Container Class Reference
+
+
+
+Inheritance diagram for SUAVE.Components.Fuselages.Segment.Segment_Container:
+
+
+ +
+ + + + +

+Public Member Functions

def get_children (self)
 
+

Detailed Description

+
 Container for wing segment
+
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+None
+
+Outputs:
+None
+
+Properties Used:
+N/A
+

Member Function Documentation

+ +

◆ get_children()

+ +
+
+ + + + + + + + +
def SUAVE.Components.Fuselages.Segment.Segment_Container.get_children ( self)
+
+
 Returns the components that can go inside
+
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+None
+
+Outputs:
+None
+
+Properties Used:
+N/A
+
+
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/matthewclarke/Documents/SUAVE/SUAVE/trunk/SUAVE/Components/Fuselages/Segment.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Fuselages_1_1Segment_1_1Segment__Container.js b/doxygen/classSUAVE_1_1Components_1_1Fuselages_1_1Segment_1_1Segment__Container.js new file mode 100644 index 00000000..54e38ab7 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Fuselages_1_1Segment_1_1Segment__Container.js @@ -0,0 +1,4 @@ +var classSUAVE_1_1Components_1_1Fuselages_1_1Segment_1_1Segment__Container = +[ + [ "get_children", "classSUAVE_1_1Components_1_1Fuselages_1_1Segment_1_1Segment__Container.html#a48accd677d8fafff1c03827d061c11cf", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Fuselages_1_1Segment_1_1Segment__Container.png b/doxygen/classSUAVE_1_1Components_1_1Fuselages_1_1Segment_1_1Segment__Container.png new file mode 100644 index 00000000..978f0f27 Binary files /dev/null and b/doxygen/classSUAVE_1_1Components_1_1Fuselages_1_1Segment_1_1Segment__Container.png differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Landing__Gear_1_1Landing__Gear_1_1Landing__Gear-members.html b/doxygen/classSUAVE_1_1Components_1_1Landing__Gear_1_1Landing__Gear_1_1Landing__Gear-members.html index 1c4e8b5b..91a4158f 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Landing__Gear_1_1Landing__Gear_1_1Landing__Gear-members.html +++ b/doxygen/classSUAVE_1_1Components_1_1Landing__Gear_1_1Landing__Gear_1_1Landing__Gear-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -99,10 +106,13 @@

This is the complete list of members for SUAVE.Components.Landing_Gear.Landing_Gear.Landing_Gear, including all inherited members.

- - - - + + + + + + +
__defaults__(self)SUAVE.Components.Landing_Gear.Landing_Gear.Landing_Gear
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Landing_Gear.Landing_Gear.Landing_Gear)SUAVE.Components.Landing_Gear.Landing_Gear.Landing_Gear
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Landing_Gear.Landing_Gear.Landing_Gear)SUAVE.Components.Landing_Gear.Landing_Gear.Landing_Gear
@@ -110,7 +120,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Components_1_1Landing__Gear_1_1Landing__Gear_1_1Landing__Gear.html b/doxygen/classSUAVE_1_1Components_1_1Landing__Gear_1_1Landing__Gear_1_1Landing__Gear.html index 9f24bc3b..41ae88d0 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Landing__Gear_1_1Landing__Gear_1_1Landing__Gear.html +++ b/doxygen/classSUAVE_1_1Components_1_1Landing__Gear_1_1Landing__Gear_1_1Landing__Gear.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Components.Landing_Gear.Landing_Gear.Landing_Gear Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -96,7 +103,7 @@ Public Attributes | List of all members
-
SUAVE.Components.Landing_Gear.Landing_Gear.Landing_Gear Class Reference
+
SUAVE.Components.Landing_Gear.Landing_Gear.Landing_Gear Class Reference
@@ -109,19 +116,13 @@ SUAVE.Components.Component.Component SUAVE.Components.Landing_Gear.Main_Landing_Gear.Main_Landing_Gear SUAVE.Components.Landing_Gear.Nose_Landing_Gear.Nose_Landing_Gear - -
+ + - - - - - -

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
@@ -148,6 +149,15 @@ + + + + + +

Public Attributes

 origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 

Detailed Description


The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Components_1_1Landing__Gear_1_1Main__Landing__Gear_1_1Main__Landing__Gear-members.html b/doxygen/classSUAVE_1_1Components_1_1Landing__Gear_1_1Main__Landing__Gear_1_1Main__Landing__Gear-members.html index ec446f6e..e0de21f1 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Landing__Gear_1_1Main__Landing__Gear_1_1Main__Landing__Gear-members.html +++ b/doxygen/classSUAVE_1_1Components_1_1Landing__Gear_1_1Main__Landing__Gear_1_1Main__Landing__Gear-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -99,14 +106,17 @@

This is the complete list of members for SUAVE.Components.Landing_Gear.Main_Landing_Gear.Main_Landing_Gear, including all inherited members.

- - - - - - - - + + + + + + + + + + +
__defaults__(self)SUAVE.Components.Landing_Gear.Main_Landing_Gear.Main_Landing_Gear
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
strut_length (defined in SUAVE.Components.Landing_Gear.Main_Landing_Gear.Main_Landing_Gear)SUAVE.Components.Landing_Gear.Main_Landing_Gear.Main_Landing_Gear
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Landing_Gear.Landing_Gear.Landing_Gear)SUAVE.Components.Landing_Gear.Landing_Gear.Landing_Gear
tire_diameter (defined in SUAVE.Components.Landing_Gear.Main_Landing_Gear.Main_Landing_Gear)SUAVE.Components.Landing_Gear.Main_Landing_Gear.Main_Landing_Gear
units (defined in SUAVE.Components.Landing_Gear.Main_Landing_Gear.Main_Landing_Gear)SUAVE.Components.Landing_Gear.Main_Landing_Gear.Main_Landing_Gear
wheels (defined in SUAVE.Components.Landing_Gear.Main_Landing_Gear.Main_Landing_Gear)SUAVE.Components.Landing_Gear.Main_Landing_Gear.Main_Landing_Gear
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
strut_length (defined in SUAVE.Components.Landing_Gear.Main_Landing_Gear.Main_Landing_Gear)SUAVE.Components.Landing_Gear.Main_Landing_Gear.Main_Landing_Gear
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Landing_Gear.Main_Landing_Gear.Main_Landing_Gear)SUAVE.Components.Landing_Gear.Main_Landing_Gear.Main_Landing_Gear
tire_diameter (defined in SUAVE.Components.Landing_Gear.Main_Landing_Gear.Main_Landing_Gear)SUAVE.Components.Landing_Gear.Main_Landing_Gear.Main_Landing_Gear
units (defined in SUAVE.Components.Landing_Gear.Main_Landing_Gear.Main_Landing_Gear)SUAVE.Components.Landing_Gear.Main_Landing_Gear.Main_Landing_Gear
wheels (defined in SUAVE.Components.Landing_Gear.Main_Landing_Gear.Main_Landing_Gear)SUAVE.Components.Landing_Gear.Main_Landing_Gear.Main_Landing_Gear
@@ -114,7 +124,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Components_1_1Landing__Gear_1_1Main__Landing__Gear_1_1Main__Landing__Gear.html b/doxygen/classSUAVE_1_1Components_1_1Landing__Gear_1_1Main__Landing__Gear_1_1Main__Landing__Gear.html index 43d3285b..d0fdb0fb 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Landing__Gear_1_1Main__Landing__Gear_1_1Main__Landing__Gear.html +++ b/doxygen/classSUAVE_1_1Components_1_1Landing__Gear_1_1Main__Landing__Gear_1_1Main__Landing__Gear.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Components.Landing_Gear.Main_Landing_Gear.Main_Landing_Gear Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -96,7 +103,7 @@ Public Attributes | List of all members
-
SUAVE.Components.Landing_Gear.Main_Landing_Gear.Main_Landing_Gear Class Reference
+
SUAVE.Components.Landing_Gear.Main_Landing_Gear.Main_Landing_Gear Class Reference
@@ -108,25 +115,19 @@ SUAVE.Components.Landing_Gear.Landing_Gear.Landing_Gear SUAVE.Components.Physical_Component.Physical_Component SUAVE.Components.Component.Component - -
+ + - - - - - - - - -

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Landing_Gear.Landing_Gear.Landing_Gear
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
+ + @@ -163,6 +164,15 @@ + + + + + +

Public Attributes

tag
 
 units
 
 origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 

Detailed Description

SUAVE.Components.Landing_Gear.Main_Landing_Gear()
@@ -206,6 +216,8 @@ 

SUAVE.Components.Landing_Gear.Landing_Gear.Landing_Gear.

+


The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Components_1_1Landing__Gear_1_1Main__Landing__Gear_1_1Main__Landing__Gear.js b/doxygen/classSUAVE_1_1Components_1_1Landing__Gear_1_1Main__Landing__Gear_1_1Main__Landing__Gear.js index 08ae7c96..6e3f1dbd 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Landing__Gear_1_1Main__Landing__Gear_1_1Main__Landing__Gear.js +++ b/doxygen/classSUAVE_1_1Components_1_1Landing__Gear_1_1Main__Landing__Gear_1_1Main__Landing__Gear.js @@ -2,6 +2,7 @@ var classSUAVE_1_1Components_1_1Landing__Gear_1_1Main__Landing__Gear_1_1Main__La [ [ "__defaults__", "classSUAVE_1_1Components_1_1Landing__Gear_1_1Main__Landing__Gear_1_1Main__Landing__Gear.html#a49f8c147fcead8400fbf06ba5607257c", null ], [ "strut_length", "classSUAVE_1_1Components_1_1Landing__Gear_1_1Main__Landing__Gear_1_1Main__Landing__Gear.html#a0746446ff4e556f4bfaa8e8133269cf8", null ], + [ "tag", "classSUAVE_1_1Components_1_1Landing__Gear_1_1Main__Landing__Gear_1_1Main__Landing__Gear.html#afef7bd4ee2b5f3df712b783c14ab7efc", null ], [ "tire_diameter", "classSUAVE_1_1Components_1_1Landing__Gear_1_1Main__Landing__Gear_1_1Main__Landing__Gear.html#a3fdc93cc5f4a391eeff8ce20588a422d", null ], [ "units", "classSUAVE_1_1Components_1_1Landing__Gear_1_1Main__Landing__Gear_1_1Main__Landing__Gear.html#adf90062bd324cc58d3fa5c4165412f50", null ], [ "wheels", "classSUAVE_1_1Components_1_1Landing__Gear_1_1Main__Landing__Gear_1_1Main__Landing__Gear.html#abcfe6aac23f12d46d7c1eaa686982d41", null ] diff --git a/doxygen/classSUAVE_1_1Components_1_1Landing__Gear_1_1Nose__Landing__Gear_1_1Nose__Landing__Gear-members.html b/doxygen/classSUAVE_1_1Components_1_1Landing__Gear_1_1Nose__Landing__Gear_1_1Nose__Landing__Gear-members.html index c02e1167..10ce1953 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Landing__Gear_1_1Nose__Landing__Gear_1_1Nose__Landing__Gear-members.html +++ b/doxygen/classSUAVE_1_1Components_1_1Landing__Gear_1_1Nose__Landing__Gear_1_1Nose__Landing__Gear-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -99,14 +106,17 @@

This is the complete list of members for SUAVE.Components.Landing_Gear.Nose_Landing_Gear.Nose_Landing_Gear, including all inherited members.

- - - - - - - - + + + + + + + + + + +
__defaults__(self)SUAVE.Components.Landing_Gear.Nose_Landing_Gear.Nose_Landing_Gear
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
strut_length (defined in SUAVE.Components.Landing_Gear.Nose_Landing_Gear.Nose_Landing_Gear)SUAVE.Components.Landing_Gear.Nose_Landing_Gear.Nose_Landing_Gear
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Landing_Gear.Landing_Gear.Landing_Gear)SUAVE.Components.Landing_Gear.Landing_Gear.Landing_Gear
tire_diameter (defined in SUAVE.Components.Landing_Gear.Nose_Landing_Gear.Nose_Landing_Gear)SUAVE.Components.Landing_Gear.Nose_Landing_Gear.Nose_Landing_Gear
units (defined in SUAVE.Components.Landing_Gear.Nose_Landing_Gear.Nose_Landing_Gear)SUAVE.Components.Landing_Gear.Nose_Landing_Gear.Nose_Landing_Gear
wheels (defined in SUAVE.Components.Landing_Gear.Nose_Landing_Gear.Nose_Landing_Gear)SUAVE.Components.Landing_Gear.Nose_Landing_Gear.Nose_Landing_Gear
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
strut_length (defined in SUAVE.Components.Landing_Gear.Nose_Landing_Gear.Nose_Landing_Gear)SUAVE.Components.Landing_Gear.Nose_Landing_Gear.Nose_Landing_Gear
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Landing_Gear.Nose_Landing_Gear.Nose_Landing_Gear)SUAVE.Components.Landing_Gear.Nose_Landing_Gear.Nose_Landing_Gear
tire_diameter (defined in SUAVE.Components.Landing_Gear.Nose_Landing_Gear.Nose_Landing_Gear)SUAVE.Components.Landing_Gear.Nose_Landing_Gear.Nose_Landing_Gear
units (defined in SUAVE.Components.Landing_Gear.Nose_Landing_Gear.Nose_Landing_Gear)SUAVE.Components.Landing_Gear.Nose_Landing_Gear.Nose_Landing_Gear
wheels (defined in SUAVE.Components.Landing_Gear.Nose_Landing_Gear.Nose_Landing_Gear)SUAVE.Components.Landing_Gear.Nose_Landing_Gear.Nose_Landing_Gear
@@ -114,7 +124,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Components_1_1Landing__Gear_1_1Nose__Landing__Gear_1_1Nose__Landing__Gear.html b/doxygen/classSUAVE_1_1Components_1_1Landing__Gear_1_1Nose__Landing__Gear_1_1Nose__Landing__Gear.html index 69c9243f..4193912d 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Landing__Gear_1_1Nose__Landing__Gear_1_1Nose__Landing__Gear.html +++ b/doxygen/classSUAVE_1_1Components_1_1Landing__Gear_1_1Nose__Landing__Gear_1_1Nose__Landing__Gear.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Components.Landing_Gear.Nose_Landing_Gear.Nose_Landing_Gear Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -96,7 +103,7 @@ Public Attributes | List of all members
-
SUAVE.Components.Landing_Gear.Nose_Landing_Gear.Nose_Landing_Gear Class Reference
+
SUAVE.Components.Landing_Gear.Nose_Landing_Gear.Nose_Landing_Gear Class Reference
@@ -108,25 +115,19 @@ SUAVE.Components.Landing_Gear.Landing_Gear.Landing_Gear SUAVE.Components.Physical_Component.Physical_Component SUAVE.Components.Component.Component - -
+ + - - - - - - - - -

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Landing_Gear.Landing_Gear.Landing_Gear
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
+ + @@ -163,6 +164,15 @@ + + + + + +

Public Attributes

tag
 
 tire_diameter
 
 origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 

Detailed Description

SUAVE.Components.Landing_Gear.Nose_Landing_Gear()
@@ -207,6 +217,8 @@ 

SUAVE.Components.Landing_Gear.Landing_Gear.Landing_Gear.

+


The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Components_1_1Landing__Gear_1_1Nose__Landing__Gear_1_1Nose__Landing__Gear.js b/doxygen/classSUAVE_1_1Components_1_1Landing__Gear_1_1Nose__Landing__Gear_1_1Nose__Landing__Gear.js index 24071e69..2c140dac 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Landing__Gear_1_1Nose__Landing__Gear_1_1Nose__Landing__Gear.js +++ b/doxygen/classSUAVE_1_1Components_1_1Landing__Gear_1_1Nose__Landing__Gear_1_1Nose__Landing__Gear.js @@ -2,6 +2,7 @@ var classSUAVE_1_1Components_1_1Landing__Gear_1_1Nose__Landing__Gear_1_1Nose__La [ [ "__defaults__", "classSUAVE_1_1Components_1_1Landing__Gear_1_1Nose__Landing__Gear_1_1Nose__Landing__Gear.html#ac5ad8f513c8037bdcafe89490ae9b771", null ], [ "strut_length", "classSUAVE_1_1Components_1_1Landing__Gear_1_1Nose__Landing__Gear_1_1Nose__Landing__Gear.html#ab9bd2221e3bc7debc15df18403b3d039", null ], + [ "tag", "classSUAVE_1_1Components_1_1Landing__Gear_1_1Nose__Landing__Gear_1_1Nose__Landing__Gear.html#aa1d302486ac5d47da8154f0b52470a39", null ], [ "tire_diameter", "classSUAVE_1_1Components_1_1Landing__Gear_1_1Nose__Landing__Gear_1_1Nose__Landing__Gear.html#ab0f697c45997ba5b6de8021eef2850be", null ], [ "units", "classSUAVE_1_1Components_1_1Landing__Gear_1_1Nose__Landing__Gear_1_1Nose__Landing__Gear.html#a4d7fc084dfa42ced1729cd0949e5db24", null ], [ "wheels", "classSUAVE_1_1Components_1_1Landing__Gear_1_1Nose__Landing__Gear_1_1Nose__Landing__Gear.html#a6ba38038577df2b45650d9452cb87cda", null ] diff --git a/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Curve-members.html b/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Curve-members.html deleted file mode 100644 index f5833396..00000000 --- a/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Curve-members.html +++ /dev/null @@ -1,116 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.1.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
-
- - - -
-
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- -
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SUAVE.Components.Lofted_Body.Curve Member List
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- -
- - - - diff --git a/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Curve.html b/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Curve.html deleted file mode 100644 index 94876b1c..00000000 --- a/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Curve.html +++ /dev/null @@ -1,194 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Components.Lofted_Body.Curve Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.1.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
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- - - -
-
- -
-
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- -
- -
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- -
- -
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SUAVE.Components.Lofted_Body.Curve Class Reference
-
-
-
-Inheritance diagram for SUAVE.Components.Lofted_Body.Curve:
-
-
- - -SUAVE.Components.Component.Component - -
- - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
- - - - - - - - - - -

-Public Attributes

tag
 
points
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
-

Detailed Description

-
A class that stubs out what a curve is
-
-Assumptions:
-None
-
-Source:
-None
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Components.Lofted_Body.Curve.__defaults__ ( self)
-
-
This sets the default values.
-    
-    Assumptions:
-    None
-    
-    Source:
-    N/A
-    
-    Inputs:
-    None
-    
-    Outputs:
-    None
-    
-    Properties Used:
-    None
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Lofted_Body.py
  • -
-
-
- - - - diff --git a/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Curve.js b/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Curve.js deleted file mode 100644 index 124b4bd2..00000000 --- a/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Curve.js +++ /dev/null @@ -1,6 +0,0 @@ -var classSUAVE_1_1Components_1_1Lofted__Body_1_1Curve = -[ - [ "__defaults__", "classSUAVE_1_1Components_1_1Lofted__Body_1_1Curve.html#a843aec6fd606521a8c2336e992438158", null ], - [ "points", "classSUAVE_1_1Components_1_1Lofted__Body_1_1Curve.html#a3f471917d7e9ebdab3b61771389ddd21", null ], - [ "tag", "classSUAVE_1_1Components_1_1Lofted__Body_1_1Curve.html#aa3d06b7633c0175e5b5020576d767c89", null ] -]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Curve.png b/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Curve.png deleted file mode 100644 index 8eb5fdb1..00000000 Binary files a/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Curve.png and /dev/null differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1CurveContainer-members.html b/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1CurveContainer-members.html deleted file mode 100644 index 6b8f8851..00000000 --- a/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1CurveContainer-members.html +++ /dev/null @@ -1,116 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.1.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
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-
-
- - - -
-
- -
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- -
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SUAVE.Components.Lofted_Body.CurveContainer Member List
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- - - - diff --git a/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1CurveContainer.html b/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1CurveContainer.html deleted file mode 100644 index e30654fa..00000000 --- a/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1CurveContainer.html +++ /dev/null @@ -1,153 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Components.Lofted_Body.CurveContainer Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.1.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
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-
-
- - - -
-
- -
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- -
- -
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SUAVE.Components.Lofted_Body.CurveContainer Class Reference
-
-
-
-Inheritance diagram for SUAVE.Components.Lofted_Body.CurveContainer:
-
-
- - -SUAVE.Components.Component.Container - -
- - - - - - - - - - - - - -

-Static Public Attributes

Curve
 
Container
 
Section
 
Segment
 
- Static Public Attributes inherited from SUAVE.Components.Component.Container
Container
 
-

Detailed Description

-
This does nothing
-
-Assumptions:
-None
-
-Source:
-None
-

The documentation for this class was generated from the following file:
    -
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Lofted_Body.py
  • -
-
-
- - - - diff --git a/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1CurveContainer.png b/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1CurveContainer.png deleted file mode 100644 index e23cea6c..00000000 Binary files a/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1CurveContainer.png and /dev/null differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Lofted__Body-members.html b/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Lofted__Body-members.html index aa43db02..c4409a30 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Lofted__Body-members.html +++ b/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Lofted__Body-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -99,9 +106,11 @@

This is the complete list of members for SUAVE.Components.Lofted_Body.Lofted_Body, including all inherited members.

- - - + + + + + @@ -112,7 +121,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Lofted__Body.html b/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Lofted__Body.html index cf9717b6..1a8e93f3 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Lofted__Body.html +++ b/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Lofted__Body.html @@ -1,9 +1,9 @@ - + - +SUAVE: SUAVE.Components.Lofted_Body.Lofted_Body Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ @@ -57,9 +60,11 @@
__defaults__(self)SUAVE.Components.Lofted_Body.Lofted_Body
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
Sections (defined in SUAVE.Components.Lofted_Body.Lofted_Body)SUAVE.Components.Lofted_Body.Lofted_Body
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
Segments (defined in SUAVE.Components.Lofted_Body.Lofted_Body)SUAVE.Components.Lofted_Body.Lofted_Body
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Lofted_Body.Lofted_Body)SUAVE.Components.Lofted_Body.Lofted_Body
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -105,26 +112,26 @@
-SUAVE.Components.Physical_Component.Physical_Component -SUAVE.Components.Component.Component -SUAVE.Components.Fuselages.Fuselage.Fuselage -SUAVE.Components.Wings.Wing.Wing -SUAVE.Components.Wings.Horizontal_Tail.Horizontal_Tail -SUAVE.Components.Wings.Main_Wing.Main_Wing -SUAVE.Components.Wings.Vertical_Tail.Vertical_Tail - -
+SUAVE.Components.Physical_Component.Physical_Component +SUAVE.Components.Component.Component +SUAVE.Components.Fuselages.Fuselage.Fuselage +SUAVE.Components.Nacelles.Nacelle.Nacelle +SUAVE.Components.Wings.All_Moving_Surface.All_Moving_Surface +SUAVE.Components.Wings.Wing.Wing +SUAVE.Components.Wings.Stabilator.Stabilator +SUAVE.Components.Wings.Vertical_Tail_All_Moving.Vertical_Tail_All_Moving +SUAVE.Components.Wings.Horizontal_Tail.Horizontal_Tail +SUAVE.Components.Wings.Main_Wing.Main_Wing +SUAVE.Components.Wings.Vertical_Tail.Vertical_Tail +SUAVE.Components.Wings.Stabilator.Stabilator +SUAVE.Components.Wings.Vertical_Tail_All_Moving.Vertical_Tail_All_Moving + + - - - - - -

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
@@ -134,9 +141,6 @@ - - @@ -157,6 +161,15 @@ + + + + + +

Public Attributes

 Segments
 
Sections
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
 tag
 origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 

Member Function Documentation

@@ -191,6 +204,10 @@

SUAVE.Components.Physical_Component.Physical_Component.

+ +

Reimplemented in SUAVE.Components.Wings.Wing.Wing, SUAVE.Components.Wings.All_Moving_Surface.All_Moving_Surface, SUAVE.Components.Wings.Main_Wing.Main_Wing, SUAVE.Components.Wings.Vertical_Tail.Vertical_Tail, SUAVE.Components.Wings.Stabilator.Stabilator, SUAVE.Components.Wings.Vertical_Tail_All_Moving.Vertical_Tail_All_Moving, SUAVE.Components.Fuselages.Fuselage.Fuselage, SUAVE.Components.Wings.Horizontal_Tail.Horizontal_Tail, and SUAVE.Components.Nacelles.Nacelle.Nacelle.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Lofted__Body.js b/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Lofted__Body.js index 07cc6449..4d4abc37 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Lofted__Body.js +++ b/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Lofted__Body.js @@ -1,7 +1,6 @@ var classSUAVE_1_1Components_1_1Lofted__Body_1_1Lofted__Body = [ [ "__defaults__", "classSUAVE_1_1Components_1_1Lofted__Body_1_1Lofted__Body.html#a9a41b92aeca26b01f43527677f0f715a", null ], - [ "Sections", "classSUAVE_1_1Components_1_1Lofted__Body_1_1Lofted__Body.html#a436ac8f3ad1b562b09051693377b70df", null ], [ "Segments", "classSUAVE_1_1Components_1_1Lofted__Body_1_1Lofted__Body.html#ad997a3fd0531a8c08fe66cd427b27391", null ], [ "tag", "classSUAVE_1_1Components_1_1Lofted__Body_1_1Lofted__Body.html#a9be10450331f26faa3e4f6e222e12ee1", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Lofted__Body.png b/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Lofted__Body.png index 5ad6393b..0a812255 100644 Binary files a/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Lofted__Body.png and b/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Lofted__Body.png differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Section-members.html b/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Section-members.html index 6674d614..737088bc 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Section-members.html +++ b/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Section-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -99,7 +106,9 @@

This is the complete list of members for SUAVE.Components.Lofted_Body.Section, including all inherited members.

- + + + @@ -111,7 +120,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Section.html b/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Section.html index d81d4cdc..b09753ad 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Section.html +++ b/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Section.html @@ -1,9 +1,9 @@ - + - +SUAVE: SUAVE.Components.Lofted_Body.Section Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ @@ -57,9 +60,11 @@
__defaults__(self)SUAVE.Components.Lofted_Body.Section
Curves (defined in SUAVE.Components.Lofted_Body.Section)SUAVE.Components.Lofted_Body.Section
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
next (defined in SUAVE.Components.Lofted_Body.Section)SUAVE.Components.Lofted_Body.Section
origin (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
prev (defined in SUAVE.Components.Lofted_Body.Section)SUAVE.Components.Lofted_Body.Section
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -105,28 +112,21 @@
-SUAVE.Components.Component.Component -SUAVE.Components.Wings.Airfoils.Airfoil.Airfoil -SUAVE.Components.Wings.Control_Surface.Control_Surface_Section - -
+SUAVE.Components.Component.Component +SUAVE.Components.Airfoils.Airfoil.Airfoil + + - - -

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
- - @@ -140,6 +140,15 @@ + + + + + +

Public Attributes

 tag
 
Curves
 
 prev
 
 origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 

Detailed Description

A class that stubs out what a section is
@@ -182,6 +191,10 @@ 

SUAVE.Components.Component.Component.

+ +

Reimplemented in SUAVE.Components.Airfoils.Airfoil.Airfoil.

+


The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Section.js b/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Section.js index 02aaa64c..428d2303 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Section.js +++ b/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Section.js @@ -1,7 +1,6 @@ var classSUAVE_1_1Components_1_1Lofted__Body_1_1Section = [ [ "__defaults__", "classSUAVE_1_1Components_1_1Lofted__Body_1_1Section.html#a18e362879f7fe5a3c64d9320eff94a07", null ], - [ "Curves", "classSUAVE_1_1Components_1_1Lofted__Body_1_1Section.html#a5fea20dce1b6cebb2ea0bde9f41d7393", null ], [ "next", "classSUAVE_1_1Components_1_1Lofted__Body_1_1Section.html#afc04bc14b1deba0e6a9a3b7e2a7f1973", null ], [ "prev", "classSUAVE_1_1Components_1_1Lofted__Body_1_1Section.html#a4a00ad1e29432ac6ff0a0b7a30f8e3eb", null ], [ "tag", "classSUAVE_1_1Components_1_1Lofted__Body_1_1Section.html#adcd5d2ed1bb07f1fe5cd326c10341d85", null ] diff --git a/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Section.png b/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Section.png index 2d5246ad..0d53e1c2 100644 Binary files a/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Section.png and b/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Section.png differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1SectionContainer-members.html b/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1SectionContainer-members.html deleted file mode 100644 index 21c66000..00000000 --- a/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1SectionContainer-members.html +++ /dev/null @@ -1,113 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.1.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
-
- - - -
-
- -
-
-
- -
- -
-
- - -
- -
- -
-
-
SUAVE.Components.Lofted_Body.SectionContainer Member List
-
-
- -

This is the complete list of members for SUAVE.Components.Lofted_Body.SectionContainer, including all inherited members.

- - -
Container (defined in SUAVE.Components.Component.Container)SUAVE.Components.Component.Containerstatic
-
- - - - diff --git a/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1SectionContainer.html b/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1SectionContainer.html deleted file mode 100644 index 9540aa02..00000000 --- a/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1SectionContainer.html +++ /dev/null @@ -1,140 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Components.Lofted_Body.SectionContainer Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.1.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
-
- - - -
-
- -
-
-
- -
- -
-
- - -
- -
- -
- -
-
SUAVE.Components.Lofted_Body.SectionContainer Class Reference
-
-
-
-Inheritance diagram for SUAVE.Components.Lofted_Body.SectionContainer:
-
-
- - -SUAVE.Components.Component.Container - -
- - - - - -

-Additional Inherited Members

- Static Public Attributes inherited from SUAVE.Components.Component.Container
Container
 
-

Detailed Description

-
This does nothing
-
-Assumptions:
-None
-
-Source:
-None
-

The documentation for this class was generated from the following file:
    -
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Lofted_Body.py
  • -
-
-
- - - - diff --git a/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1SectionContainer.png b/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1SectionContainer.png deleted file mode 100644 index 60e0d669..00000000 Binary files a/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1SectionContainer.png and /dev/null differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Section__Container-members.html b/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Section__Container-members.html new file mode 100644 index 00000000..047ca6a4 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Section__Container-members.html @@ -0,0 +1,121 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
SUAVE.Components.Lofted_Body.Section_Container Member List
+
+
+ +

This is the complete list of members for SUAVE.Components.Lofted_Body.Section_Container, including all inherited members.

+ + + +
Container (defined in SUAVE.Components.Component.Container)SUAVE.Components.Component.Containerstatic
get_children(self)SUAVE.Components.Lofted_Body.Section_Container
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Section__Container.html b/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Section__Container.html new file mode 100644 index 00000000..948e3180 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Section__Container.html @@ -0,0 +1,188 @@ + + + + + + + +SUAVE: SUAVE.Components.Lofted_Body.Section_Container Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Components.Lofted_Body.Section_Container Class Reference
+
+
+
+Inheritance diagram for SUAVE.Components.Lofted_Body.Section_Container:
+
+
+ + +SUAVE.Components.Component.Container + +
+ + + + +

+Public Member Functions

def get_children (self)
 
+ + + + +

+Additional Inherited Members

- Static Public Attributes inherited from SUAVE.Components.Component.Container
Container
 
+

Detailed Description

+
This does nothing
+
+Assumptions:
+None
+
+Source:
+None
+

Member Function Documentation

+ +

◆ get_children()

+ +
+
+ + + + + + + + +
def SUAVE.Components.Lofted_Body.Section_Container.get_children ( self)
+
+
Returns the components that can go inside
+
+Assumptions:
+None
+    
+Source:
+N/A
+    
+Inputs:
+None
+    
+Outputs:
+None
+    
+Properties Used:
+N/A
+
+
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Lofted_Body.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Section__Container.js b/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Section__Container.js new file mode 100644 index 00000000..f290e33b --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Section__Container.js @@ -0,0 +1,4 @@ +var classSUAVE_1_1Components_1_1Lofted__Body_1_1Section__Container = +[ + [ "get_children", "classSUAVE_1_1Components_1_1Lofted__Body_1_1Section__Container.html#a345540bcc35295bf4ac162292381fa8c", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Section__Container.png b/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Section__Container.png new file mode 100644 index 00000000..5de78886 Binary files /dev/null and b/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Section__Container.png differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Segment-members.html b/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Segment-members.html index b10201bc..7f2f6cc7 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Segment-members.html +++ b/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Segment-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -110,7 +120,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Segment.html b/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Segment.html index cdde0925..2bc3a8a6 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Segment.html +++ b/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Segment.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Components.Lofted_Body.Segment Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -105,18 +112,16 @@
-SUAVE.Components.Component.Component -SUAVE.Components.Wings.Segment.Segment - -
+SUAVE.Components.Component.Component +SUAVE.Components.Lofted_Body_Segment.Segment.Segment +SUAVE.Components.Wings.Segment.Segment + + - - -

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
@@ -136,6 +141,15 @@ + + + + + +

Public Attributes

 origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 

Detailed Description

A class that stubs out what a segment is
@@ -178,6 +192,10 @@ 

SUAVE.Components.Component.Component.

+ +

Reimplemented in SUAVE.Components.Lofted_Body_Segment.Segment.Segment, and SUAVE.Components.Wings.Segment.Segment.

+


The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Segment.png b/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Segment.png index eec13d3e..50e3290c 100644 Binary files a/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Segment.png and b/doxygen/classSUAVE_1_1Components_1_1Lofted__Body_1_1Segment.png differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Lofted__Body__Segment_1_1Segment_1_1Segment-members.html b/doxygen/classSUAVE_1_1Components_1_1Lofted__Body__Segment_1_1Segment_1_1Segment-members.html new file mode 100644 index 00000000..6db36937 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Lofted__Body__Segment_1_1Segment_1_1Segment-members.html @@ -0,0 +1,135 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
SUAVE.Components.Lofted_Body_Segment.Segment.Segment Member List
+
+
+ +

This is the complete list of members for SUAVE.Components.Lofted_Body_Segment.Segment.Segment, including all inherited members.

+ + + + + + + + + + + + + + + + + +
__defaults__(self)SUAVE.Components.Lofted_Body_Segment.Segment.Segment
effective_diameter (defined in SUAVE.Components.Lofted_Body_Segment.Segment.Segment)SUAVE.Components.Lofted_Body_Segment.Segment.Segment
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
height (defined in SUAVE.Components.Lofted_Body_Segment.Segment.Segment)SUAVE.Components.Lofted_Body_Segment.Segment.Segment
length (defined in SUAVE.Components.Lofted_Body_Segment.Segment.Segment)SUAVE.Components.Lofted_Body_Segment.Segment.Segment
next (defined in SUAVE.Components.Lofted_Body.Segment)SUAVE.Components.Lofted_Body.Segment
origin (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
percent_x_location (defined in SUAVE.Components.Lofted_Body_Segment.Segment.Segment)SUAVE.Components.Lofted_Body_Segment.Segment.Segment
percent_y_location (defined in SUAVE.Components.Lofted_Body_Segment.Segment.Segment)SUAVE.Components.Lofted_Body_Segment.Segment.Segment
percent_z_location (defined in SUAVE.Components.Lofted_Body_Segment.Segment.Segment)SUAVE.Components.Lofted_Body_Segment.Segment.Segment
prev (defined in SUAVE.Components.Lofted_Body.Segment)SUAVE.Components.Lofted_Body.Segment
tag (defined in SUAVE.Components.Lofted_Body_Segment.Segment.Segment)SUAVE.Components.Lofted_Body_Segment.Segment.Segment
vsp_data (defined in SUAVE.Components.Lofted_Body_Segment.Segment.Segment)SUAVE.Components.Lofted_Body_Segment.Segment.Segment
width (defined in SUAVE.Components.Lofted_Body_Segment.Segment.Segment)SUAVE.Components.Lofted_Body_Segment.Segment.Segment
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Lofted__Body__Segment_1_1Segment_1_1Segment.html b/doxygen/classSUAVE_1_1Components_1_1Lofted__Body__Segment_1_1Segment_1_1Segment.html new file mode 100644 index 00000000..4785b0bf --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Lofted__Body__Segment_1_1Segment_1_1Segment.html @@ -0,0 +1,233 @@ + + + + + + + +SUAVE: SUAVE.Components.Lofted_Body_Segment.Segment.Segment Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Components.Lofted_Body_Segment.Segment.Segment Class Reference
+
+
+
+Inheritance diagram for SUAVE.Components.Lofted_Body_Segment.Segment.Segment:
+
+
+ + +SUAVE.Components.Lofted_Body.Segment +SUAVE.Components.Component.Component + +
+ + + + +

+Public Member Functions

def __defaults__ (self)
 
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Attributes

tag
 
percent_x_location
 
percent_y_location
 
percent_z_location
 
height
 
width
 
length
 
effective_diameter
 
vsp_data
 
- Public Attributes inherited from SUAVE.Components.Lofted_Body.Segment
tag
 
prev
 
next
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 
+

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Components.Lofted_Body_Segment.Segment.Segment.__defaults__ ( self)
+
+
This sets the defaults for fuselage segments in SUAVE.
+
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+None
+
+Outputs:
+None
+
+Properties Used:
+N/A
+
+

Reimplemented from SUAVE.Components.Lofted_Body.Segment.

+ +
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Lofted_Body_Segment/Segment.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Lofted__Body__Segment_1_1Segment_1_1Segment.js b/doxygen/classSUAVE_1_1Components_1_1Lofted__Body__Segment_1_1Segment_1_1Segment.js new file mode 100644 index 00000000..60e23649 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Lofted__Body__Segment_1_1Segment_1_1Segment.js @@ -0,0 +1,13 @@ +var classSUAVE_1_1Components_1_1Lofted__Body__Segment_1_1Segment_1_1Segment = +[ + [ "__defaults__", "classSUAVE_1_1Components_1_1Lofted__Body__Segment_1_1Segment_1_1Segment.html#a58e897a3daaf36a662e702db8b6322ab", null ], + [ "effective_diameter", "classSUAVE_1_1Components_1_1Lofted__Body__Segment_1_1Segment_1_1Segment.html#abe03029a4aa6fbffe66f11c6e685d608", null ], + [ "height", "classSUAVE_1_1Components_1_1Lofted__Body__Segment_1_1Segment_1_1Segment.html#ad34fed3c80edf72c300e9a1ffb7771c4", null ], + [ "length", "classSUAVE_1_1Components_1_1Lofted__Body__Segment_1_1Segment_1_1Segment.html#aa18249d4913b1369ccd66e87fd3bf850", null ], + [ "percent_x_location", "classSUAVE_1_1Components_1_1Lofted__Body__Segment_1_1Segment_1_1Segment.html#a2778d32d0229ecbd488d6707c88b2587", null ], + [ "percent_y_location", "classSUAVE_1_1Components_1_1Lofted__Body__Segment_1_1Segment_1_1Segment.html#afa608b0027609aef1a9dcd1aed5639dd", null ], + [ "percent_z_location", "classSUAVE_1_1Components_1_1Lofted__Body__Segment_1_1Segment_1_1Segment.html#a102b0dfcdf09609752ddf1c7e5eb27d1", null ], + [ "tag", "classSUAVE_1_1Components_1_1Lofted__Body__Segment_1_1Segment_1_1Segment.html#a59485cd539d5be672f22563dc2bfeb9e", null ], + [ "vsp_data", "classSUAVE_1_1Components_1_1Lofted__Body__Segment_1_1Segment_1_1Segment.html#a3d783325b1b9303b828fe66351389522", null ], + [ "width", "classSUAVE_1_1Components_1_1Lofted__Body__Segment_1_1Segment_1_1Segment.html#a9ec584532efc8665753395fe18b6abd6", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Lofted__Body__Segment_1_1Segment_1_1Segment.png b/doxygen/classSUAVE_1_1Components_1_1Lofted__Body__Segment_1_1Segment_1_1Segment.png new file mode 100644 index 00000000..ed4d315f Binary files /dev/null and b/doxygen/classSUAVE_1_1Components_1_1Lofted__Body__Segment_1_1Segment_1_1Segment.png differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Lofted__Body__Segment_1_1Segment_1_1Segment__Container-members.html b/doxygen/classSUAVE_1_1Components_1_1Lofted__Body__Segment_1_1Segment_1_1Segment__Container-members.html new file mode 100644 index 00000000..9b3c3134 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Lofted__Body__Segment_1_1Segment_1_1Segment__Container-members.html @@ -0,0 +1,120 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
SUAVE.Components.Lofted_Body_Segment.Segment.Segment_Container Member List
+
+
+ +

This is the complete list of members for SUAVE.Components.Lofted_Body_Segment.Segment.Segment_Container, including all inherited members.

+ + +
get_children(self)SUAVE.Components.Lofted_Body_Segment.Segment.Segment_Container
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Lofted__Body__Segment_1_1Segment_1_1Segment__Container.html b/doxygen/classSUAVE_1_1Components_1_1Lofted__Body__Segment_1_1Segment_1_1Segment__Container.html new file mode 100644 index 00000000..a0536c06 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Lofted__Body__Segment_1_1Segment_1_1Segment__Container.html @@ -0,0 +1,187 @@ + + + + + + + +SUAVE: SUAVE.Components.Lofted_Body_Segment.Segment.Segment_Container Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Components.Lofted_Body_Segment.Segment.Segment_Container Class Reference
+
+
+
+Inheritance diagram for SUAVE.Components.Lofted_Body_Segment.Segment.Segment_Container:
+
+
+ +
+ + + + +

+Public Member Functions

def get_children (self)
 
+

Detailed Description

+
Container for wing segment
+
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+None
+
+Outputs:
+None
+
+Properties Used:
+N/A
+

Member Function Documentation

+ +

◆ get_children()

+ +
+
+ + + + + + + + +
def SUAVE.Components.Lofted_Body_Segment.Segment.Segment_Container.get_children ( self)
+
+
Returns the components that can go inside
+
+Assumptions:
+None
+    
+Source:
+N/A
+    
+Inputs:
+None
+    
+Outputs:
+None
+    
+Properties Used:
+N/A
+
+
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Lofted_Body_Segment/Segment.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Lofted__Body__Segment_1_1Segment_1_1Segment__Container.js b/doxygen/classSUAVE_1_1Components_1_1Lofted__Body__Segment_1_1Segment_1_1Segment__Container.js new file mode 100644 index 00000000..4faa3750 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Lofted__Body__Segment_1_1Segment_1_1Segment__Container.js @@ -0,0 +1,4 @@ +var classSUAVE_1_1Components_1_1Lofted__Body__Segment_1_1Segment_1_1Segment__Container = +[ + [ "get_children", "classSUAVE_1_1Components_1_1Lofted__Body__Segment_1_1Segment_1_1Segment__Container.html#ad286fe85b5f22aa51c309832f5e0bd96", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Lofted__Body__Segment_1_1Segment_1_1Segment__Container.png b/doxygen/classSUAVE_1_1Components_1_1Lofted__Body__Segment_1_1Segment_1_1Segment__Container.png new file mode 100644 index 00000000..5db8fd67 Binary files /dev/null and b/doxygen/classSUAVE_1_1Components_1_1Lofted__Body__Segment_1_1Segment_1_1Segment__Container.png differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Mass__Properties_1_1Mass__Properties-members.html b/doxygen/classSUAVE_1_1Components_1_1Mass__Properties_1_1Mass__Properties-members.html index 6d67c3e2..b2661cea 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Mass__Properties_1_1Mass__Properties-members.html +++ b/doxygen/classSUAVE_1_1Components_1_1Mass__Properties_1_1Mass__Properties-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -110,7 +117,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Components_1_1Mass__Properties_1_1Mass__Properties.html b/doxygen/classSUAVE_1_1Components_1_1Mass__Properties_1_1Mass__Properties.html index 7c070979..d0139742 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Mass__Properties_1_1Mass__Properties.html +++ b/doxygen/classSUAVE_1_1Components_1_1Mass__Properties_1_1Mass__Properties.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Components.Mass_Properties.Mass_Properties Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -106,8 +113,9 @@ SUAVE.Vehicle.Vehicle_Mass_Properties - -
+SUAVE.Vehicle.Vehicle_Mass_Container + + @@ -170,6 +178,8 @@

SUAVE.Vehicle.Vehicle_Mass_Properties.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Components_1_1Mass__Properties_1_1Mass__Properties.png b/doxygen/classSUAVE_1_1Components_1_1Mass__Properties_1_1Mass__Properties.png index b734ddea..f8099760 100644 Binary files a/doxygen/classSUAVE_1_1Components_1_1Mass__Properties_1_1Mass__Properties.png and b/doxygen/classSUAVE_1_1Components_1_1Mass__Properties_1_1Mass__Properties.png differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Nacelles_1_1Nacelle_1_1Nacelle-members.html b/doxygen/classSUAVE_1_1Components_1_1Nacelles_1_1Nacelle_1_1Nacelle-members.html new file mode 100644 index 00000000..86948640 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Nacelles_1_1Nacelle_1_1Nacelle-members.html @@ -0,0 +1,143 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+

Public Member Functions

+ + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+ + + + + +
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
SUAVE.Components.Nacelles.Nacelle.Nacelle Member List
+
+
+ +

This is the complete list of members for SUAVE.Components.Nacelles.Nacelle.Nacelle, including all inherited members.

+ + + + + + + + + + + + + + + + + + + + + + + + + +
__defaults__(self)SUAVE.Components.Nacelles.Nacelle.Nacelle
aerodynamic_center (defined in SUAVE.Components.Nacelles.Nacelle.Nacelle)SUAVE.Components.Nacelles.Nacelle.Nacelle
Airfoil (defined in SUAVE.Components.Nacelles.Nacelle.Nacelle)SUAVE.Components.Nacelles.Nacelle.Nacelle
append_airfoil(self, airfoil)SUAVE.Components.Nacelles.Nacelle.Nacelle
append_segment(self, segment)SUAVE.Components.Nacelles.Nacelle.Nacelle
areas (defined in SUAVE.Components.Nacelles.Nacelle.Nacelle)SUAVE.Components.Nacelles.Nacelle.Nacelle
body_to_nac_vel(self)SUAVE.Components.Nacelles.Nacelle.Nacelle
cowling_airfoil_angle (defined in SUAVE.Components.Nacelles.Nacelle.Nacelle)SUAVE.Components.Nacelles.Nacelle.Nacelle
diameter (defined in SUAVE.Components.Nacelles.Nacelle.Nacelle)SUAVE.Components.Nacelles.Nacelle.Nacelle
differential_pressure (defined in SUAVE.Components.Nacelles.Nacelle.Nacelle)SUAVE.Components.Nacelles.Nacelle.Nacelle
flow_through (defined in SUAVE.Components.Nacelles.Nacelle.Nacelle)SUAVE.Components.Nacelles.Nacelle.Nacelle
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
inlet_diameter (defined in SUAVE.Components.Nacelles.Nacelle.Nacelle)SUAVE.Components.Nacelles.Nacelle.Nacelle
length (defined in SUAVE.Components.Nacelles.Nacelle.Nacelle)SUAVE.Components.Nacelles.Nacelle.Nacelle
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
nac_vel_to_body(self)SUAVE.Components.Nacelles.Nacelle.Nacelle
orientation_euler_angles (defined in SUAVE.Components.Nacelles.Nacelle.Nacelle)SUAVE.Components.Nacelles.Nacelle.Nacelle
origin (defined in SUAVE.Components.Nacelles.Nacelle.Nacelle)SUAVE.Components.Nacelles.Nacelle.Nacelle
Segments (defined in SUAVE.Components.Nacelles.Nacelle.Nacelle)SUAVE.Components.Nacelles.Nacelle.Nacelle
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Nacelles.Nacelle.Nacelle)SUAVE.Components.Nacelles.Nacelle.Nacelle
vec_to_vel(self)SUAVE.Components.Nacelles.Nacelle.Nacelle
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Nacelles_1_1Nacelle_1_1Nacelle.html b/doxygen/classSUAVE_1_1Components_1_1Nacelles_1_1Nacelle_1_1Nacelle.html new file mode 100644 index 00000000..cc269739 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Nacelles_1_1Nacelle_1_1Nacelle.html @@ -0,0 +1,466 @@ + + + + + + + +SUAVE: SUAVE.Components.Nacelles.Nacelle.Nacelle Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Components.Nacelles.Nacelle.Nacelle Class Reference
+
+
+
+Inheritance diagram for SUAVE.Components.Nacelles.Nacelle.Nacelle:
+
+
+ + +SUAVE.Components.Lofted_Body.Lofted_Body +SUAVE.Components.Physical_Component.Physical_Component +SUAVE.Components.Component.Component + +
+ + + + + + + + + + + + + + +

+Public Member Functions

def __defaults__ (self)
 
def append_segment (self, segment)
 
def append_airfoil (self, airfoil)
 
def nac_vel_to_body (self)
 
def body_to_nac_vel (self)
 
def vec_to_vel (self)
 
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Attributes

tag
 
origin
 
aerodynamic_center
 
areas
 
diameter
 
inlet_diameter
 
length
 
orientation_euler_angles
 
flow_through
 
differential_pressure
 
Airfoil
 
cowling_airfoil_angle
 
Segments
 
- Public Attributes inherited from SUAVE.Components.Lofted_Body.Lofted_Body
tag
 
Segments
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 
+

Detailed Description

+
This is a nacelle for a generic aircraft.
+
+Assumptions:
+None
+
+Source:
+N/A
+

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Components.Nacelles.Nacelle.Nacelle.__defaults__ ( self)
+
+
This sets the default values for the component to function.
+
+Assumptions:
+None
+    
+Source:
+N/A
+    
+Inputs:
+None
+    
+Outputs:
+None
+    
+Properties Used:
+None
+
+

Reimplemented from SUAVE.Components.Lofted_Body.Lofted_Body.

+ +
+
+ +

◆ append_airfoil()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Components.Nacelles.Nacelle.Nacelle.append_airfoil ( self,
 airfoil 
)
+
+
Adds an airfoil to the segment 
+    
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+None
+
+Outputs:
+None
+
+Properties Used:
+N/A
+
+
+
+ +

◆ append_segment()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Components.Nacelles.Nacelle.Nacelle.append_segment ( self,
 segment 
)
+
+
Adds a segment to the nacelle. 
+    
+Assumptions:
+None
+Source:
+N/A
+Inputs:
+None
+Outputs:
+None
+Properties Used:
+N/A
+
+
+
+ +

◆ body_to_nac_vel()

+ +
+
+ + + + + + + + +
def SUAVE.Components.Nacelles.Nacelle.Nacelle.body_to_nac_vel ( self)
+
+
This rotates from the systems body frame to the nacelles velocity frame
+
+Assumptions:
+There are two nacelle frames, the vehicle frame describing the location and the nacelle velocity frame
+velocity frame is X out the nose, Z towards the ground, and Y out the right wing
+vehicle frame is X towards the tail, Z towards the ceiling, and Y out the right wing
+
+Source:
+N/A
+
+Inputs:
+None
+
+Outputs:
+None
+
+Properties Used:
+None
+
+
+
+ +

◆ nac_vel_to_body()

+ +
+
+ + + + + + + + +
def SUAVE.Components.Nacelles.Nacelle.Nacelle.nac_vel_to_body ( self)
+
+
This rotates from the systems body frame to the nacelles velocity frame
+
+Assumptions:
+There are two nacelle frames, the vehicle frame describing the location and the nacelle velocity frame
+velocity frame is X out the nose, Z towards the ground, and Y out the right wing
+vehicle frame is X towards the tail, Z towards the ceiling, and Y out the right wing
+
+Source:
+N/A
+
+Inputs:
+None
+
+Outputs:
+None
+
+Properties Used:
+None
+
+
+
+ +

◆ vec_to_vel()

+ +
+
+ + + + + + + + +
def SUAVE.Components.Nacelles.Nacelle.Nacelle.vec_to_vel ( self)
+
+
This rotates from the nacelles vehicle frame to the nacelles velocity frame
+
+Assumptions:
+There are two nacelle frames, the vehicle frame describing the location and the nacelle velocity frame
+velocity frame is X out the nose, Z towards the ground, and Y out the right wing
+vehicle frame is X towards the tail, Z towards the ceiling, and Y out the right wing
+
+Source:
+N/A
+
+Inputs:
+None
+
+Outputs:
+None
+
+Properties Used:
+None
+
+
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Nacelles/Nacelle.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Nacelles_1_1Nacelle_1_1Nacelle.js b/doxygen/classSUAVE_1_1Components_1_1Nacelles_1_1Nacelle_1_1Nacelle.js new file mode 100644 index 00000000..f3cb7408 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Nacelles_1_1Nacelle_1_1Nacelle.js @@ -0,0 +1,22 @@ +var classSUAVE_1_1Components_1_1Nacelles_1_1Nacelle_1_1Nacelle = +[ + [ "__defaults__", "classSUAVE_1_1Components_1_1Nacelles_1_1Nacelle_1_1Nacelle.html#ae5ddc3db6efb431b82fb2bbf5b824ca2", null ], + [ "append_airfoil", "classSUAVE_1_1Components_1_1Nacelles_1_1Nacelle_1_1Nacelle.html#a2530f804f8e38063f63333349e33a5a4", null ], + [ "append_segment", "classSUAVE_1_1Components_1_1Nacelles_1_1Nacelle_1_1Nacelle.html#aa8629381a1b7492ed80554788a99e6a6", null ], + [ "body_to_nac_vel", "classSUAVE_1_1Components_1_1Nacelles_1_1Nacelle_1_1Nacelle.html#a5621a1639a60c0d0449be4b9c6fe614e", null ], + [ "nac_vel_to_body", "classSUAVE_1_1Components_1_1Nacelles_1_1Nacelle_1_1Nacelle.html#a5ffbb24f270eb3aa06a5db2ac4f4e260", null ], + [ "vec_to_vel", "classSUAVE_1_1Components_1_1Nacelles_1_1Nacelle_1_1Nacelle.html#a72d645271916069fd62b434dc576e410", null ], + [ "aerodynamic_center", "classSUAVE_1_1Components_1_1Nacelles_1_1Nacelle_1_1Nacelle.html#a4e5c12076105f48ff5b93b3cb0934679", null ], + [ "Airfoil", "classSUAVE_1_1Components_1_1Nacelles_1_1Nacelle_1_1Nacelle.html#a715f3490c583270191a11198f1a2640e", null ], + [ "areas", "classSUAVE_1_1Components_1_1Nacelles_1_1Nacelle_1_1Nacelle.html#ac6cd1e9d61a9b251a7bf5de1f28ae41c", null ], + [ "cowling_airfoil_angle", "classSUAVE_1_1Components_1_1Nacelles_1_1Nacelle_1_1Nacelle.html#acbbad4e6b16b36dbe1ceee15433abed8", null ], + [ "diameter", "classSUAVE_1_1Components_1_1Nacelles_1_1Nacelle_1_1Nacelle.html#aa5f1ac06d95f975c10fd19337110c137", null ], + [ "differential_pressure", "classSUAVE_1_1Components_1_1Nacelles_1_1Nacelle_1_1Nacelle.html#ad765cc9ec62046f2d4452828bf16cfd9", null ], + [ "flow_through", "classSUAVE_1_1Components_1_1Nacelles_1_1Nacelle_1_1Nacelle.html#ae9bda35371563e3eb6c464f06c797e47", null ], + [ "inlet_diameter", "classSUAVE_1_1Components_1_1Nacelles_1_1Nacelle_1_1Nacelle.html#a41935580f02f87271c3fc17d85034820", null ], + [ "length", "classSUAVE_1_1Components_1_1Nacelles_1_1Nacelle_1_1Nacelle.html#aceda1593b44746cc2b5c9aa2cbeccf1e", null ], + [ "orientation_euler_angles", "classSUAVE_1_1Components_1_1Nacelles_1_1Nacelle_1_1Nacelle.html#ab8e853f87560d4fc26cd0a816b16f77f", null ], + [ "origin", "classSUAVE_1_1Components_1_1Nacelles_1_1Nacelle_1_1Nacelle.html#a745ce2dc66c1914eb4c2513f3b222fff", null ], + [ "Segments", "classSUAVE_1_1Components_1_1Nacelles_1_1Nacelle_1_1Nacelle.html#a6d9ae942479fe9a052fe4df862280dd6", null ], + [ "tag", "classSUAVE_1_1Components_1_1Nacelles_1_1Nacelle_1_1Nacelle.html#ac5fe3503dfd989dfd9ce58f6552e8b8b", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Nacelles_1_1Nacelle_1_1Nacelle.png b/doxygen/classSUAVE_1_1Components_1_1Nacelles_1_1Nacelle_1_1Nacelle.png new file mode 100644 index 00000000..637db5eb Binary files /dev/null and b/doxygen/classSUAVE_1_1Components_1_1Nacelles_1_1Nacelle_1_1Nacelle.png differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Cargo_1_1Cargo-members.html b/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Cargo_1_1Cargo-members.html deleted file mode 100644 index d63a958e..00000000 --- a/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Cargo_1_1Cargo-members.html +++ /dev/null @@ -1,117 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.1.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
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- - - - - - diff --git a/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Cargo_1_1Cargo.html b/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Cargo_1_1Cargo.html deleted file mode 100644 index e144b818..00000000 --- a/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Cargo_1_1Cargo.html +++ /dev/null @@ -1,216 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Components.Payloads.Cargo.Cargo Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
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SUAVE -  1.1.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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- -
-
SUAVE.Components.Payloads.Cargo.Cargo Class Reference
-
-
-
-Inheritance diagram for SUAVE.Components.Payloads.Cargo.Cargo:
-
-
- - -SUAVE.Components.Payloads.Payload.Payload -SUAVE.Components.Physical_Component.Physical_Component -SUAVE.Components.Component.Component - -
- - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Payloads.Payload.Payload
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
- - - - - - - - - - - - - - - - - - - - -

-Public Attributes

tag
 
- Public Attributes inherited from SUAVE.Components.Payloads.Payload.Payload
tag
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
-

Detailed Description

-
A class representing cargo.
-
-Assumptions:
-None
-
-Source:
-N/A
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Components.Payloads.Cargo.Cargo.__defaults__ ( self)
-
-
This sets the default tag for cargo.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Payloads/Cargo.py
  • -
-
-
- - - - diff --git a/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Cargo_1_1Cargo.js b/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Cargo_1_1Cargo.js deleted file mode 100644 index 4c2661cb..00000000 --- a/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Cargo_1_1Cargo.js +++ /dev/null @@ -1,5 +0,0 @@ -var classSUAVE_1_1Components_1_1Payloads_1_1Cargo_1_1Cargo = -[ - [ "__defaults__", "classSUAVE_1_1Components_1_1Payloads_1_1Cargo_1_1Cargo.html#a4f97de17ea1ae1c4e6e68e3a6307952e", null ], - [ "tag", "classSUAVE_1_1Components_1_1Payloads_1_1Cargo_1_1Cargo.html#a0113edcfd4ad704eed565e3201d5a5fb", null ] -]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Cargo_1_1Cargo.png b/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Cargo_1_1Cargo.png deleted file mode 100644 index 0e20a305..00000000 Binary files a/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Cargo_1_1Cargo.png and /dev/null differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Payload_1_1Container-members.html b/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Payload_1_1Container-members.html index c7f0a290..7d9a07b6 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Payload_1_1Container-members.html +++ b/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Payload_1_1Container-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -107,7 +115,7 @@
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diff --git a/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Payload_1_1Container.html b/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Payload_1_1Container.html index aaf1f43a..f241672b 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Payload_1_1Container.html +++ b/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Payload_1_1Container.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Components.Payloads.Payload.Container Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -106,8 +113,8 @@ SUAVE.Components.Physical_Component.Container SUAVE.Components.Component.Container - -
+ + @@ -124,6 +131,8 @@ + +

Static Public Attributes

- Public Member Functions inherited from SUAVE.Components.Physical_Component.Container
def sum_mass (self)
 
def total_moment (self)
 

Detailed Description

The container used for payloads. No additional functionality.
@@ -144,7 +153,7 @@
     
     
+    doxygen 1.8.15 
   
 
diff --git a/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Payload_1_1Payload-members.html b/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Payload_1_1Payload-members.html index 6422e358..56858a97 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Payload_1_1Payload-members.html +++ b/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Payload_1_1Payload-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -99,10 +106,13 @@

This is the complete list of members for SUAVE.Components.Payloads.Payload.Payload, including all inherited members.

- - - - + + + + + + +
__defaults__(self)SUAVE.Components.Payloads.Payload.Payload
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Payloads.Payload.Payload)SUAVE.Components.Payloads.Payload.Payload
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Payloads.Payload.Payload)SUAVE.Components.Payloads.Payload.Payload
@@ -110,7 +120,7 @@
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diff --git a/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Payload_1_1Payload.html b/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Payload_1_1Payload.html index 34fb15d0..d86a5268 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Payload_1_1Payload.html +++ b/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Payload_1_1Payload.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Components.Payloads.Payload.Payload Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -105,24 +112,15 @@
-SUAVE.Components.Physical_Component.Physical_Component -SUAVE.Components.Component.Component -SUAVE.Components.Payloads.Cargo.Cargo -SUAVE.Components.Payloads.Person.Person -SUAVE.Components.Payloads.Satellite.Satellite - -
+SUAVE.Components.Physical_Component.Physical_Component +SUAVE.Components.Component.Component + + - - - - - -

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
@@ -149,6 +147,15 @@ + + + + + +

Public Attributes

 origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 

Detailed Description

A class representing a payload.
@@ -191,6 +198,8 @@ 

SUAVE.Components.Physical_Component.Physical_Component.

+


The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Payload_1_1Payload.png b/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Payload_1_1Payload.png index 92f742d8..da7d4351 100644 Binary files a/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Payload_1_1Payload.png and b/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Payload_1_1Payload.png differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Person_1_1Person-members.html b/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Person_1_1Person-members.html deleted file mode 100644 index 1a1477ed..00000000 --- a/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Person_1_1Person-members.html +++ /dev/null @@ -1,117 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
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SUAVE -  1.1.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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- - - - - - diff --git a/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Person_1_1Person.html b/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Person_1_1Person.html deleted file mode 100644 index fcf7ff65..00000000 --- a/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Person_1_1Person.html +++ /dev/null @@ -1,216 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Components.Payloads.Person.Person Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.1.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Payloads.Person.Person Class Reference
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-Inheritance diagram for SUAVE.Components.Payloads.Person.Person:
-
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- - -SUAVE.Components.Payloads.Payload.Payload -SUAVE.Components.Physical_Component.Physical_Component -SUAVE.Components.Component.Component - -
- - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Payloads.Payload.Payload
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
- - - - - - - - - - - - - - - - - - - - -

-Public Attributes

tag
 
- Public Attributes inherited from SUAVE.Components.Payloads.Payload.Payload
tag
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
-

Detailed Description

-
A class representing a person.
-
-Assumptions:
-None
-
-Source:
-N/A
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Components.Payloads.Person.Person.__defaults__ ( self)
-
-
This sets the default values for a person.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Payloads/Person.py
  • -
-
-
- - - - diff --git a/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Person_1_1Person.js b/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Person_1_1Person.js deleted file mode 100644 index 1ff52699..00000000 --- a/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Person_1_1Person.js +++ /dev/null @@ -1,5 +0,0 @@ -var classSUAVE_1_1Components_1_1Payloads_1_1Person_1_1Person = -[ - [ "__defaults__", "classSUAVE_1_1Components_1_1Payloads_1_1Person_1_1Person.html#a057b4069cf1182ae815f9ac23828a483", null ], - [ "tag", "classSUAVE_1_1Components_1_1Payloads_1_1Person_1_1Person.html#a8a256ceea2c9695987a0760609a2fd3a", null ] -]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Person_1_1Person.png b/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Person_1_1Person.png deleted file mode 100644 index dae4c78c..00000000 Binary files a/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Person_1_1Person.png and /dev/null differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Satellite_1_1Satellite-members.html b/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Satellite_1_1Satellite-members.html deleted file mode 100644 index 478f20d5..00000000 --- a/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Satellite_1_1Satellite-members.html +++ /dev/null @@ -1,117 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
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SUAVE -  1.1.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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- - - - - - diff --git a/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Satellite_1_1Satellite.html b/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Satellite_1_1Satellite.html deleted file mode 100644 index fcb6200e..00000000 --- a/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Satellite_1_1Satellite.html +++ /dev/null @@ -1,216 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Components.Payloads.Satellite.Satellite Class Reference - - - - - - - - - - - - - - - -
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SUAVE -  1.1.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Payloads.Satellite.Satellite Class Reference
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-Inheritance diagram for SUAVE.Components.Payloads.Satellite.Satellite:
-
-
- - -SUAVE.Components.Payloads.Payload.Payload -SUAVE.Components.Physical_Component.Physical_Component -SUAVE.Components.Component.Component - -
- - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Payloads.Payload.Payload
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
- - - - - - - - - - - - - - - - - - - - -

-Public Attributes

tag
 
- Public Attributes inherited from SUAVE.Components.Payloads.Payload.Payload
tag
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
-

Detailed Description

-
A class representing a satellite.
-
-Assumptions:
-None
-
-Source:
-N/A
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Components.Payloads.Satellite.Satellite.__defaults__ ( self)
-
-
This sets the default tag for a satellite.
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Payloads/Satellite.py
  • -
-
-
- - - - diff --git a/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Satellite_1_1Satellite.js b/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Satellite_1_1Satellite.js deleted file mode 100644 index 98406b48..00000000 --- a/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Satellite_1_1Satellite.js +++ /dev/null @@ -1,5 +0,0 @@ -var classSUAVE_1_1Components_1_1Payloads_1_1Satellite_1_1Satellite = -[ - [ "__defaults__", "classSUAVE_1_1Components_1_1Payloads_1_1Satellite_1_1Satellite.html#a0dd0be04f50f34e19e8c5130a4d38956", null ], - [ "tag", "classSUAVE_1_1Components_1_1Payloads_1_1Satellite_1_1Satellite.html#a11c080c0b8112d73fe2eb41668bf5809", null ] -]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Satellite_1_1Satellite.png b/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Satellite_1_1Satellite.png deleted file mode 100644 index 5d3a5456..00000000 Binary files a/doxygen/classSUAVE_1_1Components_1_1Payloads_1_1Satellite_1_1Satellite.png and /dev/null differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Physical__Component_1_1Container-members.html b/doxygen/classSUAVE_1_1Components_1_1Physical__Component_1_1Container-members.html index 3fbc99e4..53a70eba 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Physical__Component_1_1Container-members.html +++ b/doxygen/classSUAVE_1_1Components_1_1Physical__Component_1_1Container-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -107,7 +115,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Components_1_1Physical__Component_1_1Container.html b/doxygen/classSUAVE_1_1Components_1_1Physical__Component_1_1Container.html index 586533b7..4bf96c03 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Physical__Component_1_1Container.html +++ b/doxygen/classSUAVE_1_1Components_1_1Physical__Component_1_1Container.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Components.Physical_Component.Container Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -104,17 +111,21 @@
-SUAVE.Components.Component.Container -SUAVE.Components.Fuselages.Fuselage.Container -SUAVE.Components.Payloads.Payload.Container -SUAVE.Components.Propulsors.Propulsor.Container - -
+SUAVE.Components.Component.Container +SUAVE.Components.Energy.Networks.Network.Container +SUAVE.Components.Fuselages.Fuselage.Container +SUAVE.Components.Payloads.Payload.Container +SUAVE.Components.Wings.Wing.Container +SUAVE.Vehicle.Vehicle_Mass_Container + + + +

Public Member Functions

def sum_mass (self)
 
def total_moment (self)
 
@@ -160,8 +171,43 @@

+

◆ total_moment()

+ +
+
+

Additional Inherited Members

+ + + + + + + +
def SUAVE.Components.Physical_Component.Container.total_moment ( self)
+
+
will recursively search the data tree and sum
+    any Comp.Mass_Properties.mass, and return the total sum of moments
+    
+    Assumptions:
     None
     
+    Source:
+    N/A
+    
+    Inputs:
+    None
+    
+    Outputs:
+    total moment [kg*m]
+    
     Properties Used:
     None
 
@@ -178,7 +224,7 @@

SUAVE + doxygen 1.8.15

diff --git a/doxygen/classSUAVE_1_1Components_1_1Physical__Component_1_1Container.js b/doxygen/classSUAVE_1_1Components_1_1Physical__Component_1_1Container.js index 0d9c75f7..8e52a97d 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Physical__Component_1_1Container.js +++ b/doxygen/classSUAVE_1_1Components_1_1Physical__Component_1_1Container.js @@ -1,4 +1,5 @@ var classSUAVE_1_1Components_1_1Physical__Component_1_1Container = [ - [ "sum_mass", "classSUAVE_1_1Components_1_1Physical__Component_1_1Container.html#ae51f620275537cac1c60ba136c68735e", null ] + [ "sum_mass", "classSUAVE_1_1Components_1_1Physical__Component_1_1Container.html#ae51f620275537cac1c60ba136c68735e", null ], + [ "total_moment", "classSUAVE_1_1Components_1_1Physical__Component_1_1Container.html#a7c5629c0cc965bad4c8799fd7616f3e4", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Physical__Component_1_1Container.png b/doxygen/classSUAVE_1_1Components_1_1Physical__Component_1_1Container.png index d75a8578..0490b60b 100644 Binary files a/doxygen/classSUAVE_1_1Components_1_1Physical__Component_1_1Container.png and b/doxygen/classSUAVE_1_1Components_1_1Physical__Component_1_1Container.png differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Physical__Component_1_1Physical__Component-members.html b/doxygen/classSUAVE_1_1Components_1_1Physical__Component_1_1Physical__Component-members.html index 34535b22..c3115f63 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Physical__Component_1_1Physical__Component-members.html +++ b/doxygen/classSUAVE_1_1Components_1_1Physical__Component_1_1Physical__Component-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -99,10 +106,13 @@

This is the complete list of members for SUAVE.Components.Physical_Component.Physical_Component, including all inherited members.

- - - - + + + + + + +
__defaults__(self)SUAVE.Components.Physical_Component.Physical_Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
@@ -110,7 +120,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Components_1_1Physical__Component_1_1Physical__Component.html b/doxygen/classSUAVE_1_1Components_1_1Physical__Component_1_1Physical__Component.html index 0d7c8633..83122669 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Physical__Component_1_1Physical__Component.html +++ b/doxygen/classSUAVE_1_1Components_1_1Physical__Component_1_1Physical__Component.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Components.Physical_Component.Physical_Component Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -105,64 +112,88 @@
-SUAVE.Components.Component.Component -SUAVE.Components.Energy.Energy.Energy -SUAVE.Components.Energy.Energy_Component.Energy_Component -SUAVE.Components.Landing_Gear.Landing_Gear.Landing_Gear -SUAVE.Components.Lofted_Body.Lofted_Body -SUAVE.Components.Payloads.Payload.Payload -SUAVE.Components.Propulsors.Propulsor.Propulsor -SUAVE.Components.Energy.Converters.Combustor.Combustor -SUAVE.Components.Energy.Converters.Compression_Nozzle.Compression_Nozzle -SUAVE.Components.Energy.Converters.Compressor.Compressor -SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle -SUAVE.Components.Energy.Converters.Fan.Fan -SUAVE.Components.Energy.Converters.Fuel_Cell.Fuel_Cell -SUAVE.Components.Energy.Converters.Gearbox.Gearbox -SUAVE.Components.Energy.Converters.Motor.Motor -SUAVE.Components.Energy.Converters.Motor_Lo_Fid.Motor_Lo_Fid -SUAVE.Components.Energy.Converters.Propeller.Propeller -SUAVE.Components.Energy.Converters.Propeller_Lo_Fid.Propeller_Lo_Fid -SUAVE.Components.Energy.Converters.Ram.Ram -SUAVE.Components.Energy.Converters.Shaft_Power_Off_Take.Shaft_Power_Off_Take -SUAVE.Components.Energy.Converters.Solar_Panel.Solar_Panel -SUAVE.Components.Energy.Converters.Supersonic_Nozzle.Supersonic_Nozzle -SUAVE.Components.Energy.Converters.Turbine.Turbine -SUAVE.Components.Energy.Distributors.Electronic_Speed_Controller.Electronic_Speed_Controller -SUAVE.Components.Energy.Distributors.Solar_Logic.Solar_Logic -SUAVE.Components.Energy.Peripherals.Avionics.Avionics -SUAVE.Components.Energy.Peripherals.Payload.Payload -SUAVE.Components.Energy.Processes.Solar_Radiation.Solar_Radiation -SUAVE.Components.Energy.Processes.Thrust.Thrust -SUAVE.Components.Energy.Storages.Batteries.Battery.Battery -SUAVE.Components.Landing_Gear.Main_Landing_Gear.Main_Landing_Gear -SUAVE.Components.Landing_Gear.Nose_Landing_Gear.Nose_Landing_Gear -SUAVE.Components.Fuselages.Fuselage.Fuselage -SUAVE.Components.Wings.Wing.Wing -SUAVE.Components.Payloads.Cargo.Cargo -SUAVE.Components.Payloads.Person.Person -SUAVE.Components.Payloads.Satellite.Satellite -SUAVE.Components.Energy.Networks.Battery_Ducted_Fan.Battery_Ducted_Fan -SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller -SUAVE.Components.Energy.Networks.Dual_Battery_Ducted_Fan.Dual_Battery_Ducted_Fan -SUAVE.Components.Energy.Networks.Ducted_Fan.Ducted_Fan -SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward_Propulsor -SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate -SUAVE.Components.Energy.Networks.Ramjet.Ramjet -SUAVE.Components.Energy.Networks.Solar.Solar -SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity -SUAVE.Components.Energy.Networks.Turbofan.Turbofan -SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super - -
+SUAVE.Components.Component.Component +SUAVE.Components.Energy.Energy_Component.Energy_Component +SUAVE.Components.Energy.Networks.Network.Network +SUAVE.Components.Landing_Gear.Landing_Gear.Landing_Gear +SUAVE.Components.Lofted_Body.Lofted_Body +SUAVE.Components.Payloads.Payload.Payload +SUAVE.Components.Systems.System.System +SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface +SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_One.Rotor_Wake_Fidelity_One +SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_Two.Rotor_Wake_Fidelity_Two +SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_Zero.Rotor_Wake_Fidelity_Zero +SUAVE.Components.Energy.Charging.Charging.Charging +SUAVE.Components.Energy.Converters.Combustor.Combustor +SUAVE.Components.Energy.Converters.Compression_Nozzle.Compression_Nozzle +SUAVE.Components.Energy.Converters.Compressor.Compressor +SUAVE.Components.Energy.Converters.de_Laval_Nozzle.de_Laval_Nozzle +SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle +SUAVE.Components.Energy.Converters.Fan.Fan +SUAVE.Components.Energy.Converters.Fuel_Cell.Fuel_Cell +SUAVE.Components.Energy.Converters.Gearbox.Gearbox +SUAVE.Components.Energy.Converters.Generator_Zero_Fid.Generator_Zero_Fid +SUAVE.Components.Energy.Converters.Internal_Combustion_Engine.Internal_Combustion_Engine +SUAVE.Components.Energy.Converters.Motor.Motor +SUAVE.Components.Energy.Converters.Motor_HTS_Rotor.Motor_HTS_Rotor +SUAVE.Components.Energy.Converters.Motor_Lo_Fid.Motor_Lo_Fid +SUAVE.Components.Energy.Converters.Propeller_Lo_Fid.Propeller_Lo_Fid +SUAVE.Components.Energy.Converters.Ram.Ram +SUAVE.Components.Energy.Converters.Rocket_Combustor.Rocket_Combustor +SUAVE.Components.Energy.Converters.Rotor.Rotor +SUAVE.Components.Energy.Converters.Shaft_Power_Off_Take.Shaft_Power_Off_Take +SUAVE.Components.Energy.Converters.Solar_Panel.Solar_Panel +SUAVE.Components.Energy.Converters.Supersonic_Nozzle.Supersonic_Nozzle +SUAVE.Components.Energy.Converters.Turbine.Turbine +SUAVE.Components.Energy.Converters.Turboelectric.Turboelectric +SUAVE.Components.Energy.Cooling.Cryocooler.Cryocooler +SUAVE.Components.Energy.Cooling.Cryogenic_Heat_Exchanger.Cryogenic_Heat_Exchanger +SUAVE.Components.Energy.Distributors.Cryogenic_Lead.Cryogenic_Lead +SUAVE.Components.Energy.Distributors.Electronic_Speed_Controller.Electronic_Speed_Controller +SUAVE.Components.Energy.Distributors.HTS_DC_Supply.HTS_DC_Supply +SUAVE.Components.Energy.Distributors.Solar_Logic.Solar_Logic +SUAVE.Components.Energy.Peripherals.Avionics.Avionics +SUAVE.Components.Energy.Peripherals.Payload.Payload +SUAVE.Components.Energy.Processes.Rocket_Thrust.Rocket_Thrust +SUAVE.Components.Energy.Processes.Solar_Radiation.Solar_Radiation +SUAVE.Components.Energy.Processes.Thrust.Thrust +SUAVE.Components.Energy.Storages.Batteries.Battery.Battery +SUAVE.Components.Energy.Storages.Fuel_Tanks.Fuel_Tank.Fuel_Tank +SUAVE.Components.Energy.Networks.Battery_Cell_Cycler.Battery_Cell_Cycler +SUAVE.Components.Energy.Networks.Battery_Ducted_Fan.Battery_Ducted_Fan +SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller +SUAVE.Components.Energy.Networks.Ducted_Fan.Ducted_Fan +SUAVE.Components.Energy.Networks.Internal_Combustion_Propeller.Internal_Combustion_Propeller +SUAVE.Components.Energy.Networks.Internal_Combustion_Propeller_Constant_Speed.Internal_Combustion_Propeller_Constant_Speed +SUAVE.Components.Energy.Networks.Lift_Cruise.Lift_Cruise +SUAVE.Components.Energy.Networks.Liquid_Rocket.Liquid_Rocket +SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate +SUAVE.Components.Energy.Networks.Ramjet.Ramjet +SUAVE.Components.Energy.Networks.Scramjet.Scramjet +SUAVE.Components.Energy.Networks.Serial_Hybrid_Ducted_Fan.Serial_Hybrid_Ducted_Fan +SUAVE.Components.Energy.Networks.Solar.Solar +SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity +SUAVE.Components.Energy.Networks.Turboelectric_HTS_Ducted_Fan.Turboelectric_HTS_Ducted_Fan +SUAVE.Components.Energy.Networks.Turbofan.Turbofan +SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super +SUAVE.Components.Landing_Gear.Main_Landing_Gear.Main_Landing_Gear +SUAVE.Components.Landing_Gear.Nose_Landing_Gear.Nose_Landing_Gear +SUAVE.Components.Fuselages.Fuselage.Fuselage +SUAVE.Components.Nacelles.Nacelle.Nacelle +SUAVE.Components.Wings.All_Moving_Surface.All_Moving_Surface +SUAVE.Components.Wings.Wing.Wing +SUAVE.Components.Wings.Control_Surfaces.Aileron.Aileron +SUAVE.Components.Wings.Control_Surfaces.Elevator.Elevator +SUAVE.Components.Wings.Control_Surfaces.Flap.Flap +SUAVE.Components.Wings.Control_Surfaces.Rudder.Rudder +SUAVE.Components.Wings.Control_Surfaces.Slat.Slat + + - - -

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
@@ -185,6 +216,15 @@ + + + + + +

Public Attributes

 origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 

Detailed Description

A component that has a Mass_Properties Data
@@ -227,6 +267,10 @@ 

SUAVE.Components.Component.Component.

+ +

Reimplemented in SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion_LiNiMnCoO2_18650.Lithium_Ion_LiNiMnCoO2_18650, SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion_LiFePO4_18650.Lithium_Ion_LiFePO4_18650, SUAVE.Components.Energy.Networks.Lift_Cruise.Lift_Cruise, SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller, SUAVE.Components.Wings.Wing.Wing, SUAVE.Components.Wings.All_Moving_Surface.All_Moving_Surface, SUAVE.Components.Energy.Converters.Rotor.Rotor, SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle, SUAVE.Components.Energy.Converters.Supersonic_Nozzle.Supersonic_Nozzle, SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion, SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate, SUAVE.Components.Wings.Main_Wing.Main_Wing, SUAVE.Components.Wings.Vertical_Tail.Vertical_Tail, SUAVE.Components.Energy.Converters.Compression_Nozzle.Compression_Nozzle, SUAVE.Components.Energy.Converters.de_Laval_Nozzle.de_Laval_Nozzle, SUAVE.Components.Wings.Stabilator.Stabilator, SUAVE.Components.Wings.Vertical_Tail_All_Moving.Vertical_Tail_All_Moving, SUAVE.Components.Energy.Networks.Solar.Solar, SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_One.Rotor_Wake_Fidelity_One, SUAVE.Components.Energy.Converters.Combustor.Combustor, SUAVE.Components.Energy.Networks.Turbofan.Turbofan, SUAVE.Components.Fuselages.Fuselage.Fuselage, SUAVE.Components.Wings.Horizontal_Tail.Horizontal_Tail, SUAVE.Components.Energy.Converters.Compressor.Compressor, SUAVE.Components.Energy.Converters.Fan.Fan, SUAVE.Components.Energy.Converters.Ram.Ram, SUAVE.Components.Energy.Converters.Turbine.Turbine, SUAVE.Components.Energy.Networks.Network.Network, SUAVE.Components.Energy.Networks.PyCycle.PyCycle, SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity, SUAVE.Components.Energy.Distributors.Solar_Logic.Solar_Logic, SUAVE.Components.Energy.Networks.Turboelectric_HTS_Ducted_Fan.Turboelectric_HTS_Ducted_Fan, SUAVE.Components.Wings.Control_Surfaces.Aileron.Aileron, SUAVE.Components.Energy.Networks.Battery_Cell_Cycler.Battery_Cell_Cycler, SUAVE.Components.Energy.Networks.Ducted_Fan.Ducted_Fan, SUAVE.Components.Energy.Processes.Thrust.Thrust, SUAVE.Components.Wings.Control_Surfaces.Elevator.Elevator, SUAVE.Components.Wings.Control_Surfaces.Flap.Flap, SUAVE.Components.Wings.Control_Surfaces.Rudder.Rudder, SUAVE.Components.Wings.Control_Surfaces.Slat.Slat, SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_Zero.Rotor_Wake_Fidelity_Zero, SUAVE.Components.Energy.Converters.Fuel_Cell.Fuel_Cell, SUAVE.Components.Energy.Converters.Motor.Motor, SUAVE.Components.Energy.Converters.Motor_HTS_Rotor.Motor_HTS_Rotor, SUAVE.Components.Energy.Converters.Motor_Lo_Fid.Motor_Lo_Fid, SUAVE.Components.Energy.Converters.Rocket_Combustor.Rocket_Combustor, SUAVE.Components.Energy.Networks.Internal_Combustion_Propeller.Internal_Combustion_Propeller, SUAVE.Components.Energy.Networks.Scramjet.Scramjet, SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super, SUAVE.Components.Energy.Converters.Gearbox.Gearbox, SUAVE.Components.Energy.Cooling.Cryogenic_Heat_Exchanger.Cryogenic_Heat_Exchanger, SUAVE.Components.Energy.Networks.Internal_Combustion_Propeller_Constant_Speed.Internal_Combustion_Propeller_Constant_Speed, SUAVE.Components.Energy.Converters.Internal_Combustion_Engine.Internal_Combustion_Engine, SUAVE.Components.Energy.Converters.Propeller_Lo_Fid.Propeller_Lo_Fid, SUAVE.Components.Energy.Networks.Battery_Ducted_Fan.Battery_Ducted_Fan, SUAVE.Components.Energy.Networks.Serial_Hybrid_Ducted_Fan.Serial_Hybrid_Ducted_Fan, SUAVE.Components.Energy.Storages.Batteries.Battery.Battery, SUAVE.Components.Landing_Gear.Landing_Gear.Landing_Gear, SUAVE.Components.Energy.Converters.Generator_Zero_Fid.Generator_Zero_Fid, SUAVE.Components.Energy.Converters.Turboelectric.Turboelectric, SUAVE.Components.Energy.Networks.Liquid_Rocket.Liquid_Rocket, SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Aluminum_Air.Aluminum_Air, SUAVE.Components.Systems.System.System, SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Lithium_Air.Lithium_Air, SUAVE.Components.Landing_Gear.Main_Landing_Gear.Main_Landing_Gear, SUAVE.Components.Nacelles.Nacelle.Nacelle, SUAVE.Components.Energy.Converters.Shaft_Power_Off_Take.Shaft_Power_Off_Take, SUAVE.Components.Energy.Cooling.Cryocooler.Cryocooler, SUAVE.Components.Energy.Networks.Ramjet.Ramjet, SUAVE.Components.Landing_Gear.Nose_Landing_Gear.Nose_Landing_Gear, SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_Two.Rotor_Wake_Fidelity_Two, SUAVE.Components.Energy.Converters.Solar_Panel.Solar_Panel, SUAVE.Components.Energy.Peripherals.Avionics.Avionics, SUAVE.Components.Energy.Peripherals.Payload.Payload, SUAVE.Components.Energy.Storages.Fuel_Tanks.Fuel_Tank.Fuel_Tank, SUAVE.Components.Payloads.Payload.Payload, SUAVE.Components.Energy.Charging.Charging.Charging, SUAVE.Components.Energy.Distributors.Cryogenic_Lead.Cryogenic_Lead, SUAVE.Components.Energy.Energy_Component.Energy_Component, SUAVE.Components.Energy.Processes.Rocket_Thrust.Rocket_Thrust, SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Sulfur.Lithium_Sulfur, SUAVE.Components.Energy.Converters.Lift_Rotor.Lift_Rotor, SUAVE.Components.Energy.Converters.Propeller.Propeller, SUAVE.Components.Lofted_Body.Lofted_Body, SUAVE.Components.Energy.Distributors.Electronic_Speed_Controller.Electronic_Speed_Controller, SUAVE.Components.Energy.Distributors.HTS_DC_Supply.HTS_DC_Supply, and SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface.

+


The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Components_1_1Physical__Component_1_1Physical__Component.png b/doxygen/classSUAVE_1_1Components_1_1Physical__Component_1_1Physical__Component.png index 6449b8a1..a01fad68 100644 Binary files a/doxygen/classSUAVE_1_1Components_1_1Physical__Component_1_1Physical__Component.png and b/doxygen/classSUAVE_1_1Components_1_1Physical__Component_1_1Physical__Component.png differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Container-members.html b/doxygen/classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Container-members.html index cebc2acd..f785750f 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Container-members.html +++ b/doxygen/classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Container-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -13,14 +13,13 @@ - @@ -33,13 +32,13 @@ Logo
SUAVE -  1.1.0 +  2.4.0
An Aerospace Vehicle Environment for Designing Future Aircraft
- @@ -48,7 +47,7 @@ onblur="searchBox.OnSearchFieldFocus(false)" onkeyup="searchBox.OnSearchFieldChange(event)"/> - +
@@ -57,9 +56,11 @@ - +
@@ -73,7 +74,9 @@
diff --git a/doxygen/classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Container.html b/doxygen/classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Container.html index e57daf07..66a70092 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Container.html +++ b/doxygen/classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Container.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Components.Propulsors.Propulsor.Container Class Reference @@ -13,14 +13,13 @@ - @@ -33,13 +32,13 @@ Logo
SUAVE -  1.1.0 +  2.4.0
An Aerospace Vehicle Environment for Designing Future Aircraft
- @@ -48,7 +47,7 @@ onblur="searchBox.OnSearchFieldFocus(false)" onkeyup="searchBox.OnSearchFieldChange(event)"/> - +
@@ -57,9 +56,11 @@ - +
@@ -73,7 +74,9 @@
@@ -104,28 +107,25 @@
-SUAVE.Components.Physical_Component.Container +SUAVE.Components.Physical_Component.Container SUAVE.Components.Component.Container - -
+ + + + -

Public Member Functions

def get_children (self)
 
def evaluate_thrust (self, state)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Container
def sum_mass (self)
 
- - - - + +

-Additional Inherited Members

- Static Public Attributes inherited from SUAVE.Components.Component.Container
Container
 
def total_moment (self)
 

Detailed Description

- + +

◆ get_children()

+ +
+
+ + + + + + + + +
def SUAVE.Components.Propulsors.Propulsor.Container.get_children ( self)
+
+
 Returns the components that can go inside
 
 Assumptions:
-Propulsor has "evaluate_thrust" method
+None
 
 Source:
 N/A
 
 Inputs:
-State variables
+None
 
 Outputs:
-Results of the "evaluate_thrust" method
+None
 
 Properties Used:
 N/A
@@ -179,7 +214,7 @@ 

diff --git a/doxygen/classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Container.js b/doxygen/classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Container.js index 5fb1f3ec..b2e522b5 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Container.js +++ b/doxygen/classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Container.js @@ -1,4 +1,5 @@ var classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Container = [ - [ "evaluate_thrust", "classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Container.html#a42e24eef8ee7108c8f99379060824724", null ] + [ "evaluate_thrust", "classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Container.html#a42e24eef8ee7108c8f99379060824724", null ], + [ "get_children", "classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Container.html#a36a16c1656b07b2be4ac4e2e9bde3b2e", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Propulsor-members.html b/doxygen/classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Propulsor-members.html index 1ad9a914..98e0af32 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Propulsor-members.html +++ b/doxygen/classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Propulsor-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -13,14 +13,13 @@ - @@ -33,13 +32,13 @@ Logo
SUAVE -  1.1.0 +  2.4.0
An Aerospace Vehicle Environment for Designing Future Aircraft
- @@ -48,7 +47,7 @@ onblur="searchBox.OnSearchFieldFocus(false)" onkeyup="searchBox.OnSearchFieldChange(event)"/> - +
@@ -57,9 +56,11 @@
- +
@@ -73,7 +74,9 @@
@@ -99,18 +102,25 @@

This is the complete list of members for SUAVE.Components.Propulsors.Propulsor.Propulsor, including all inherited members.

- + + + + + + + + + +
__defaults__(self)SUAVE.Components.Propulsors.Propulsor.Propulsor
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
areas (defined in SUAVE.Components.Propulsors.Propulsor.Propulsor)SUAVE.Components.Propulsors.Propulsor.Propulsor
engine_length (defined in SUAVE.Components.Propulsors.Propulsor.Propulsor)SUAVE.Components.Propulsors.Propulsor.Propulsor
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Propulsors.Propulsor.Propulsor)SUAVE.Components.Propulsors.Propulsor.Propulsor
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
nacelle_diameter (defined in SUAVE.Components.Propulsors.Propulsor.Propulsor)SUAVE.Components.Propulsors.Propulsor.Propulsor
non_dimensional_origin (defined in SUAVE.Components.Propulsors.Propulsor.Propulsor)SUAVE.Components.Propulsors.Propulsor.Propulsor
number_of_engines (defined in SUAVE.Components.Propulsors.Propulsor.Propulsor)SUAVE.Components.Propulsors.Propulsor.Propulsor
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Propulsors.Propulsor.Propulsor)SUAVE.Components.Propulsors.Propulsor.Propulsor
wing_mounted (defined in SUAVE.Components.Propulsors.Propulsor.Propulsor)SUAVE.Components.Propulsors.Propulsor.Propulsor
diff --git a/doxygen/classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Propulsor.html b/doxygen/classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Propulsor.html index f6567755..20731009 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Propulsor.html +++ b/doxygen/classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Propulsor.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Components.Propulsors.Propulsor.Propulsor Class Reference @@ -13,14 +13,13 @@ - @@ -33,13 +32,13 @@ Logo
SUAVE -  1.1.0 +  2.4.0
An Aerospace Vehicle Environment for Designing Future Aircraft
- @@ -48,7 +47,7 @@ onblur="searchBox.OnSearchFieldFocus(false)" onkeyup="searchBox.OnSearchFieldChange(event)"/> - +
@@ -57,9 +56,11 @@ - +
@@ -73,7 +74,9 @@
@@ -105,38 +108,58 @@
-SUAVE.Components.Physical_Component.Physical_Component -SUAVE.Components.Component.Component -SUAVE.Components.Energy.Networks.Battery_Ducted_Fan.Battery_Ducted_Fan -SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller -SUAVE.Components.Energy.Networks.Dual_Battery_Ducted_Fan.Dual_Battery_Ducted_Fan -SUAVE.Components.Energy.Networks.Ducted_Fan.Ducted_Fan -SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward_Propulsor -SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate -SUAVE.Components.Energy.Networks.Ramjet.Ramjet -SUAVE.Components.Energy.Networks.Solar.Solar -SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity -SUAVE.Components.Energy.Networks.Turbofan.Turbofan -SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super - -
+SUAVE.Components.Physical_Component.Physical_Component +SUAVE.Components.Component.Component +SUAVE.Components.Energy.Networks.Battery_Ducted_Fan.Battery_Ducted_Fan +SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller +SUAVE.Components.Energy.Networks.Ducted_Fan.Ducted_Fan +SUAVE.Components.Energy.Networks.Internal_Combustion_Propeller.Internal_Combustion_Propeller +SUAVE.Components.Energy.Networks.Internal_Combustion_Propeller_Constant_Speed.Internal_Combustion_Propeller_Constant_Speed +SUAVE.Components.Energy.Networks.Lift_Cruise.Lift_Cruise +SUAVE.Components.Energy.Networks.Liquid_Rocket.Liquid_Rocket +SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate +SUAVE.Components.Energy.Networks.Ramjet.Ramjet +SUAVE.Components.Energy.Networks.Scramjet.Scramjet +SUAVE.Components.Energy.Networks.Serial_Hybrid_Ducted_Fan.Serial_Hybrid_Ducted_Fan +SUAVE.Components.Energy.Networks.Solar.Solar +SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity +SUAVE.Components.Energy.Networks.Turbofan.Turbofan +SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super +SUAVE.Components.Energy.Networks.Vectored_Thrust.Vectored_Thrust + + - - - - - -

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
+ + + + + + + + + + + + + + @@ -157,9 +180,18 @@ + + + + + +

Public Attributes

 tag
 
generative_design_max_per_vehicle
 
non_dimensional_origin
 
number_of_engines
 
nacelle_diameter
 
engine_length
 
wing_mounted
 
areas
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
 tag
 origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 

Detailed Description

-
SUAVE.Components.Propulsor()
+
 SUAVE.Components.Propulsor()
 
     The Top Level Propulsor Class
         
@@ -183,27 +215,31 @@ 

-
This sets the default attributes for the propulsor.
-
-Assumptions:
-None
-
-Source:
-N/A
+
 This sets the default attributes for the propulsor.
 
-Inputs:
-None
+        Assumptions:
+        None
+        
+        Source:
+        N/A
+        
+        Inputs:
+        None
+        
+        Outputs:
+        None
+        
+        Properties Used:
+        N/A
+
+

Reimplemented from SUAVE.Components.Physical_Component.Physical_Component.

-Outputs: -None +

Reimplemented in SUAVE.Components.Energy.Networks.Vectored_Thrust.Vectored_Thrust, SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super, SUAVE.Components.Energy.Networks.Turbofan.Turbofan, SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity, SUAVE.Components.Energy.Networks.Solar.Solar, SUAVE.Components.Energy.Networks.Serial_Hybrid_Ducted_Fan.Serial_Hybrid_Ducted_Fan, SUAVE.Components.Energy.Networks.Scramjet.Scramjet, SUAVE.Components.Energy.Networks.Ramjet.Ramjet, SUAVE.Components.Energy.Networks.PyCycle.PyCycle, SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate, SUAVE.Components.Energy.Networks.Liquid_Rocket.Liquid_Rocket, SUAVE.Components.Energy.Networks.Lift_Cruise.Lift_Cruise, SUAVE.Components.Energy.Networks.Internal_Combustion_Propeller_Constant_Speed.Internal_Combustion_Propeller_Constant_Speed, SUAVE.Components.Energy.Networks.Internal_Combustion_Propeller.Internal_Combustion_Propeller, SUAVE.Components.Energy.Networks.Ducted_Fan.Ducted_Fan, SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller, and SUAVE.Components.Energy.Networks.Battery_Ducted_Fan.Battery_Ducted_Fan.

-Properties Used: -N/A -


The documentation for this class was generated from the following file:
    -
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Propulsors/Propulsor.py
  • +
  • /Users/matthewclarke/Documents/SUAVE/SUAVE/trunk/SUAVE/Components/Propulsors/Propulsor.py
@@ -211,9 +247,7 @@

diff --git a/doxygen/classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Propulsor.js b/doxygen/classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Propulsor.js index b46c5843..690336c8 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Propulsor.js +++ b/doxygen/classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Propulsor.js @@ -1,5 +1,12 @@ var classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Propulsor = [ [ "__defaults__", "classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Propulsor.html#a1a13b12fb63990dcd51c6ecc46c83f21", null ], - [ "tag", "classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Propulsor.html#a297d16d03533b9da160be9d970073588", null ] + [ "areas", "classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Propulsor.html#a7a272c60a24251274736178759b23670", null ], + [ "engine_length", "classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Propulsor.html#ace561d0f1785a664db4b0819bbd52ac1", null ], + [ "generative_design_max_per_vehicle", "classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Propulsor.html#a227b12da3c263476f6590fc0b20ae168", null ], + [ "nacelle_diameter", "classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Propulsor.html#afb86b97c48b3de4244e5b0b1a6eb1596", null ], + [ "non_dimensional_origin", "classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Propulsor.html#a5de38c53079018f365142c9a53284def", null ], + [ "number_of_engines", "classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Propulsor.html#a858187796822a9a4c783cd74aab0d717", null ], + [ "tag", "classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Propulsor.html#a297d16d03533b9da160be9d970073588", null ], + [ "wing_mounted", "classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Propulsor.html#ab4bb759ed381dabbe1f40027aa20230a", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Propulsor.png b/doxygen/classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Propulsor.png index b4f235c3..1f816322 100644 Binary files a/doxygen/classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Propulsor.png and b/doxygen/classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Propulsor.png differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Systems_1_1System_1_1System-members.html b/doxygen/classSUAVE_1_1Components_1_1Systems_1_1System_1_1System-members.html index 1cc7c8f3..4eabf2c8 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Systems_1_1System_1_1System-members.html +++ b/doxygen/classSUAVE_1_1Components_1_1Systems_1_1System_1_1System-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -101,10 +108,13 @@ __defaults__(self)SUAVE.Components.Systems.System.System accessories (defined in SUAVE.Components.Systems.System.System)SUAVE.Components.Systems.System.System control (defined in SUAVE.Components.Systems.System.System)SUAVE.Components.Systems.System.System - mass_properties (defined in SUAVE.Components.Systems.System.System)SUAVE.Components.Systems.System.System - origin (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component - position (defined in SUAVE.Components.Systems.System.System)SUAVE.Components.Systems.System.System - tag (defined in SUAVE.Components.Systems.System.System)SUAVE.Components.Systems.System.System + generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component + generative_design_max_per_vehicle (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component + generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component + mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component + origin (defined in SUAVE.Components.Systems.System.System)SUAVE.Components.Systems.System.System + symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component + tag (defined in SUAVE.Components.Systems.System.System)SUAVE.Components.Systems.System.System
@@ -112,7 +122,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Components_1_1Systems_1_1System_1_1System.html b/doxygen/classSUAVE_1_1Components_1_1Systems_1_1System_1_1System.html index 1813ce1f..0c2fe9db 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Systems_1_1System_1_1System.html +++ b/doxygen/classSUAVE_1_1Components_1_1Systems_1_1System_1_1System.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Components.Systems.System.System Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -105,35 +112,43 @@
-SUAVE.Components.Component.Component - -
+SUAVE.Components.Physical_Component.Physical_Component +SUAVE.Components.Component.Component + + - - -

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
- - - - + + + + + + + + + + + @@ -141,17 +156,24 @@ + + + + + +

Public Attributes

 tag
 
mass_properties
 
position
 
origin
 
 control
 
 accessories
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
 tag
 origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 

Detailed Description

-
SUAVE.Components.Systems.System()
+
A class representing an aircraft system/systems.
 
-    The Top Level System Class
-    
-        Assumptions:
-        None
-        
-        Source:
-        N/A
+Assumptions:
+None
+
+Source:
+N/A
 

Member Function Documentation

◆ __defaults__()

@@ -185,6 +207,8 @@

SUAVE.Components.Physical_Component.Physical_Component.

+


The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Components_1_1Systems_1_1System_1_1System.js b/doxygen/classSUAVE_1_1Components_1_1Systems_1_1System_1_1System.js index ee63ae2c..175879cd 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Systems_1_1System_1_1System.js +++ b/doxygen/classSUAVE_1_1Components_1_1Systems_1_1System_1_1System.js @@ -3,7 +3,6 @@ var classSUAVE_1_1Components_1_1Systems_1_1System_1_1System = [ "__defaults__", "classSUAVE_1_1Components_1_1Systems_1_1System_1_1System.html#afc1811095781c3b874ab279c8449b53a", null ], [ "accessories", "classSUAVE_1_1Components_1_1Systems_1_1System_1_1System.html#a22ad3a5dc4d33c9c53a2d01897173e99", null ], [ "control", "classSUAVE_1_1Components_1_1Systems_1_1System_1_1System.html#adb487ae49fd4892c42ef0cd2ffdd9530", null ], - [ "mass_properties", "classSUAVE_1_1Components_1_1Systems_1_1System_1_1System.html#ac257d2d78c0da7c92ddd9cf16256bfe5", null ], - [ "position", "classSUAVE_1_1Components_1_1Systems_1_1System_1_1System.html#ae3836f93b6ac5c6bab29ec4074b8ff38", null ], + [ "origin", "classSUAVE_1_1Components_1_1Systems_1_1System_1_1System.html#a552a352294cfe4dbd1b6869e2a7851c5", null ], [ "tag", "classSUAVE_1_1Components_1_1Systems_1_1System_1_1System.html#a4fa86faee2bbe57bbd444c14417e1e76", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Systems_1_1System_1_1System.png b/doxygen/classSUAVE_1_1Components_1_1Systems_1_1System_1_1System.png index b7e8e600..7a6dc7b1 100644 Binary files a/doxygen/classSUAVE_1_1Components_1_1Systems_1_1System_1_1System.png and b/doxygen/classSUAVE_1_1Components_1_1Systems_1_1System_1_1System.png differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Airfoils_1_1Airfoil_1_1Airfoil-members.html b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Airfoils_1_1Airfoil_1_1Airfoil-members.html index b8cd2bc6..61a13fc2 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Airfoils_1_1Airfoil_1_1Airfoil-members.html +++ b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Airfoils_1_1Airfoil_1_1Airfoil-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -13,14 +13,13 @@ - @@ -33,13 +32,13 @@ Logo
SUAVE -  1.1.0 +  2.4.0
An Aerospace Vehicle Environment for Designing Future Aircraft
- @@ -48,7 +47,7 @@ onblur="searchBox.OnSearchFieldFocus(false)" onkeyup="searchBox.OnSearchFieldChange(event)"/> - +
@@ -57,9 +56,11 @@ - +
@@ -73,7 +74,9 @@
@@ -100,22 +103,21 @@ - - - - - - - - + + + + + + + + +
__defaults__(self)SUAVE.Components.Wings.Airfoils.Airfoil.Airfoil
coordinate_file (defined in SUAVE.Components.Wings.Airfoils.Airfoil.Airfoil)SUAVE.Components.Wings.Airfoils.Airfoil.Airfoil
Curves (defined in SUAVE.Components.Lofted_Body.Section)SUAVE.Components.Lofted_Body.Section
import_airfoil_dat(self)SUAVE.Components.Wings.Airfoils.Airfoil.Airfoil
next (defined in SUAVE.Components.Lofted_Body.Section)SUAVE.Components.Lofted_Body.Section
origin (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
points (defined in SUAVE.Components.Wings.Airfoils.Airfoil.Airfoil)SUAVE.Components.Wings.Airfoils.Airfoil.Airfoil
prev (defined in SUAVE.Components.Lofted_Body.Section)SUAVE.Components.Lofted_Body.Section
tag (defined in SUAVE.Components.Wings.Airfoils.Airfoil.Airfoil)SUAVE.Components.Wings.Airfoils.Airfoil.Airfoil
thickness_to_chord (defined in SUAVE.Components.Wings.Airfoils.Airfoil.Airfoil)SUAVE.Components.Wings.Airfoils.Airfoil.Airfoil
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
next (defined in SUAVE.Components.Lofted_Body.Section)SUAVE.Components.Lofted_Body.Section
origin (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
points (defined in SUAVE.Components.Wings.Airfoils.Airfoil.Airfoil)SUAVE.Components.Wings.Airfoils.Airfoil.Airfoil
prev (defined in SUAVE.Components.Lofted_Body.Section)SUAVE.Components.Lofted_Body.Section
tag (defined in SUAVE.Components.Wings.Airfoils.Airfoil.Airfoil)SUAVE.Components.Wings.Airfoils.Airfoil.Airfoil
thickness_to_chord (defined in SUAVE.Components.Wings.Airfoils.Airfoil.Airfoil)SUAVE.Components.Wings.Airfoils.Airfoil.Airfoil
diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Airfoils_1_1Airfoil_1_1Airfoil.html b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Airfoils_1_1Airfoil_1_1Airfoil.html index 72536e54..c8834fea 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Airfoils_1_1Airfoil_1_1Airfoil.html +++ b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Airfoils_1_1Airfoil_1_1Airfoil.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Components.Wings.Airfoils.Airfoil.Airfoil Class Reference @@ -13,14 +13,13 @@ - @@ -33,13 +32,13 @@ Logo
SUAVE -  1.1.0 +  2.4.0
An Aerospace Vehicle Environment for Designing Future Aircraft
- @@ -48,7 +47,7 @@ onblur="searchBox.OnSearchFieldFocus(false)" onkeyup="searchBox.OnSearchFieldChange(event)"/> - +
@@ -57,9 +56,11 @@ - +
@@ -73,7 +74,9 @@
@@ -107,21 +110,13 @@ SUAVE.Components.Lofted_Body.Section SUAVE.Components.Component.Component - -
+ + - - - - - - - -

Public Member Functions

def __defaults__ (self)
 
def import_airfoil_dat (self)
 
- Public Member Functions inherited from SUAVE.Components.Lofted_Body.Section
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
@@ -141,9 +136,6 @@ - - @@ -157,6 +149,15 @@ + + + + + +

Public Attributes

 tag
 
Curves
 
 prev
 
 origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 

Member Function Documentation

@@ -191,44 +192,12 @@

-

◆ import_airfoil_dat()

- -
-
- - - - - - - - -
def SUAVE.Components.Wings.Airfoils.Airfoil.Airfoil.import_airfoil_dat ( self)
-
-
Imports airfoil data
+

Reimplemented from SUAVE.Components.Lofted_Body.Section.

-Assumptions: -None - -Source: -N/A - -Inputs: -None - -Outputs: -None - -Properties Used: -N/A -

The documentation for this class was generated from the following file:
    -
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Wings/Airfoils/Airfoil.py
  • +
  • /Users/matthewclarke/Documents/SUAVE/SUAVE/trunk/SUAVE/Components/Wings/Airfoils/Airfoil.py
@@ -236,9 +205,7 @@

diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Airfoils_1_1Airfoil_1_1Airfoil.js b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Airfoils_1_1Airfoil_1_1Airfoil.js index 49ca67b5..84442f09 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Airfoils_1_1Airfoil_1_1Airfoil.js +++ b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Airfoils_1_1Airfoil_1_1Airfoil.js @@ -1,7 +1,6 @@ var classSUAVE_1_1Components_1_1Wings_1_1Airfoils_1_1Airfoil_1_1Airfoil = [ [ "__defaults__", "classSUAVE_1_1Components_1_1Wings_1_1Airfoils_1_1Airfoil_1_1Airfoil.html#aebc33642fbd2cee33d7238535c4ed955", null ], - [ "import_airfoil_dat", "classSUAVE_1_1Components_1_1Wings_1_1Airfoils_1_1Airfoil_1_1Airfoil.html#a2fa4f8f73f27a56e42ae3ea2df7584a8", null ], [ "coordinate_file", "classSUAVE_1_1Components_1_1Wings_1_1Airfoils_1_1Airfoil_1_1Airfoil.html#ad622a4ec18682cda7a5392a9a190f1e3", null ], [ "points", "classSUAVE_1_1Components_1_1Wings_1_1Airfoils_1_1Airfoil_1_1Airfoil.html#a17ef2e1e3e857a5397db8b47044092d3", null ], [ "tag", "classSUAVE_1_1Components_1_1Wings_1_1Airfoils_1_1Airfoil_1_1Airfoil.html#ab960bdfdc567919896007568600ce750", null ], diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1All__Moving__Surface_1_1All__Moving__Surface-members.html b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1All__Moving__Surface_1_1All__Moving__Surface-members.html new file mode 100644 index 00000000..b8688995 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1All__Moving__Surface_1_1All__Moving__Surface-members.html @@ -0,0 +1,133 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
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+ + + + + + +
+
+
+ + + +
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+
+
SUAVE.Components.Wings.All_Moving_Surface.All_Moving_Surface Member List
+
+
+ +

This is the complete list of members for SUAVE.Components.Wings.All_Moving_Surface.All_Moving_Surface, including all inherited members.

+ + + + + + + + + + + + + + + +
__defaults__(self)SUAVE.Components.Wings.All_Moving_Surface.All_Moving_Surface
deflection (defined in SUAVE.Components.Wings.All_Moving_Surface.All_Moving_Surface)SUAVE.Components.Wings.All_Moving_Surface.All_Moving_Surface
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
hinge_fraction (defined in SUAVE.Components.Wings.All_Moving_Surface.All_Moving_Surface)SUAVE.Components.Wings.All_Moving_Surface.All_Moving_Surface
hinge_vector (defined in SUAVE.Components.Wings.All_Moving_Surface.All_Moving_Surface)SUAVE.Components.Wings.All_Moving_Surface.All_Moving_Surface
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
Segments (defined in SUAVE.Components.Lofted_Body.Lofted_Body)SUAVE.Components.Lofted_Body.Lofted_Body
sign_duplicate (defined in SUAVE.Components.Wings.All_Moving_Surface.All_Moving_Surface)SUAVE.Components.Wings.All_Moving_Surface.All_Moving_Surface
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Wings.All_Moving_Surface.All_Moving_Surface)SUAVE.Components.Wings.All_Moving_Surface.All_Moving_Surface
use_constant_hinge_fraction (defined in SUAVE.Components.Wings.All_Moving_Surface.All_Moving_Surface)SUAVE.Components.Wings.All_Moving_Surface.All_Moving_Surface
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1All__Moving__Surface_1_1All__Moving__Surface.html b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1All__Moving__Surface_1_1All__Moving__Surface.html new file mode 100644 index 00000000..a9e521f7 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1All__Moving__Surface_1_1All__Moving__Surface.html @@ -0,0 +1,279 @@ + + + + + + + +SUAVE: SUAVE.Components.Wings.All_Moving_Surface.All_Moving_Surface Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
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+
+
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+
+ +
+
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+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Components.Wings.All_Moving_Surface.All_Moving_Surface Class Reference
+
+
+
+Inheritance diagram for SUAVE.Components.Wings.All_Moving_Surface.All_Moving_Surface:
+
+
+ + +SUAVE.Components.Lofted_Body.Lofted_Body +SUAVE.Components.Physical_Component.Physical_Component +SUAVE.Components.Component.Component +SUAVE.Components.Wings.Stabilator.Stabilator +SUAVE.Components.Wings.Vertical_Tail_All_Moving.Vertical_Tail_All_Moving + +
+ + + + +

+Public Member Functions

def __defaults__ (self)
 
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Attributes

tag
 
sign_duplicate
 
hinge_fraction
 
deflection
 
use_constant_hinge_fraction
 
hinge_vector
 
- Public Attributes inherited from SUAVE.Components.Lofted_Body.Lofted_Body
tag
 
Segments
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 
+

Detailed Description

+
This class is used to allow every all-moving control surface class
+(e.g. Stabilator) to inherit from both a type of Wing (Horizontal_Tail
+in the case of a Stabilator) and this class. This, way All_Moving_Surface
+subclasses can inherit necessary functionality without code bloat or 
+lengthy type checking if-statements.
+
+In general, this class should not be used directly, and should only exist
+as one of the parents of another class that also inherits from Wing  
+
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+None
+
+Outputs:
+None
+
+Properties Used:
+N/A
+

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Components.Wings.All_Moving_Surface.All_Moving_Surface.__defaults__ ( self)
+
+
This sets the default for All_Moving_Surface objects in SUAVE.
+
+Attributes also found in Control_Surface:
+    see Control_Surface().__defaults__ for an explanation of attributes. Any
+    attributes used by this class that are shared with Control_Surface should 
+    always adhere to the convention established in Control_Surface.py
+    
+Attributes unique to All_Moving_Surface:
+- use_constant_hinge_fraction: false by default. If this is true, the hinge vector 
+    will follow a constant chord_fraction allong the wing, regardless of what is set
+    for hinge_vector. Note that constant hinge fractions are how hinges are handled for 
+    Control_Surfaces. If this attribute is false, the hinge vector is described by
+    the hinge_vector attribute
+- hinge_vector: The vector in body-frame that the hingeline points along. By default, 
+    it is [0,0,0], and this is taken to mean that the hinge line is normal to the root
+    chord, in-plane with the wing. This attribute does nothing if use_constant_hinge_fraction
+    is set to True.
+
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+None
+
+Outputs:
+None
+
+Properties Used:
+N/A
+
+

Reimplemented from SUAVE.Components.Lofted_Body.Lofted_Body.

+ +

Reimplemented in SUAVE.Components.Wings.Stabilator.Stabilator, and SUAVE.Components.Wings.Vertical_Tail_All_Moving.Vertical_Tail_All_Moving.

+ +
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Wings/All_Moving_Surface.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1All__Moving__Surface_1_1All__Moving__Surface.js b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1All__Moving__Surface_1_1All__Moving__Surface.js new file mode 100644 index 00000000..81d172d3 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1All__Moving__Surface_1_1All__Moving__Surface.js @@ -0,0 +1,10 @@ +var classSUAVE_1_1Components_1_1Wings_1_1All__Moving__Surface_1_1All__Moving__Surface = +[ + [ "__defaults__", "classSUAVE_1_1Components_1_1Wings_1_1All__Moving__Surface_1_1All__Moving__Surface.html#a9e8c83a908f45487b6e809154f11ce5e", null ], + [ "deflection", "classSUAVE_1_1Components_1_1Wings_1_1All__Moving__Surface_1_1All__Moving__Surface.html#ad2c06cfe7fe8d969f24ab10f40e0c3ed", null ], + [ "hinge_fraction", "classSUAVE_1_1Components_1_1Wings_1_1All__Moving__Surface_1_1All__Moving__Surface.html#afc889b952ed9179374acbdbcc6f7e119", null ], + [ "hinge_vector", "classSUAVE_1_1Components_1_1Wings_1_1All__Moving__Surface_1_1All__Moving__Surface.html#aef372fef97f71e9592a260f0f9f5ff4f", null ], + [ "sign_duplicate", "classSUAVE_1_1Components_1_1Wings_1_1All__Moving__Surface_1_1All__Moving__Surface.html#a3d6aabd20aedb6ccb0706209e1bc1fc6", null ], + [ "tag", "classSUAVE_1_1Components_1_1Wings_1_1All__Moving__Surface_1_1All__Moving__Surface.html#ac4f515556bbfc151a272c20870ed3c78", null ], + [ "use_constant_hinge_fraction", "classSUAVE_1_1Components_1_1Wings_1_1All__Moving__Surface_1_1All__Moving__Surface.html#a60d0c3419c3460fbeedc517ce7688404", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1All__Moving__Surface_1_1All__Moving__Surface.png b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1All__Moving__Surface_1_1All__Moving__Surface.png new file mode 100644 index 00000000..cd857d9b Binary files /dev/null and b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1All__Moving__Surface_1_1All__Moving__Surface.png differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surface_1_1Control__Surface-members.html b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surface_1_1Control__Surface-members.html deleted file mode 100644 index 55fb2f42..00000000 --- a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surface_1_1Control__Surface-members.html +++ /dev/null @@ -1,125 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.1.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
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-
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-
-
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- - -
- -
- -
-
-
SUAVE.Components.Wings.Control_Surface.Control_Surface Member List
-
-
- -

This is the complete list of members for SUAVE.Components.Wings.Control_Surface.Control_Surface, including all inherited members.

- - - - - - - - - - - - - - -
__defaults__(self)SUAVE.Components.Wings.Control_Surface.Control_Surface
append_section(self, section) (defined in SUAVE.Components.Wings.Control_Surface.Control_Surface)SUAVE.Components.Wings.Control_Surface.Control_Surface
chord_fraction (defined in SUAVE.Components.Wings.Control_Surface.Control_Surface)SUAVE.Components.Wings.Control_Surface.Control_Surfacestatic
deflection_gain (defined in SUAVE.Components.Wings.Control_Surface.Control_Surface)SUAVE.Components.Wings.Control_Surface.Control_Surfacestatic
deflection_symmetry (defined in SUAVE.Components.Wings.Control_Surface.Control_Surface)SUAVE.Components.Wings.Control_Surface.Control_Surfacestatic
next (defined in SUAVE.Components.Wings.Control_Surface.Control_Surface)SUAVE.Components.Wings.Control_Surface.Control_Surfacestatic
origin (defined in SUAVE.Components.Wings.Control_Surface.Control_Surface)SUAVE.Components.Wings.Control_Surface.Control_Surfacestatic
prev (defined in SUAVE.Components.Wings.Control_Surface.Control_Surface)SUAVE.Components.Wings.Control_Surface.Control_Surfacestatic
sections (defined in SUAVE.Components.Wings.Control_Surface.Control_Surface)SUAVE.Components.Wings.Control_Surface.Control_Surfacestatic
span (defined in SUAVE.Components.Wings.Control_Surface.Control_Surface)SUAVE.Components.Wings.Control_Surface.Control_Surfacestatic
span_fraction (defined in SUAVE.Components.Wings.Control_Surface.Control_Surface)SUAVE.Components.Wings.Control_Surface.Control_Surfacestatic
tag (defined in SUAVE.Components.Wings.Control_Surface.Control_Surface)SUAVE.Components.Wings.Control_Surface.Control_Surfacestatic
transformation_matrix (defined in SUAVE.Components.Wings.Control_Surface.Control_Surface)SUAVE.Components.Wings.Control_Surface.Control_Surfacestatic
-
- - - - diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surface_1_1Control__Surface.html b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surface_1_1Control__Surface.html deleted file mode 100644 index 6bb82a84..00000000 --- a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surface_1_1Control__Surface.html +++ /dev/null @@ -1,223 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Components.Wings.Control_Surface.Control_Surface Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.1.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
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SUAVE.Components.Wings.Control_Surface.Control_Surface Class Reference
-
-
-
-Inheritance diagram for SUAVE.Components.Wings.Control_Surface.Control_Surface:
-
-
- - -SUAVE.Components.Component.Component - -
- - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
-def append_section (self, section)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
- - - - - - - - - - - - - - - - - - - - - - - -

-Static Public Attributes

tag
 
span
 
span_fraction
 
chord_fraction
 
deflection_gain
 
origin
 
transformation_matrix
 
deflection_symmetry
 
sections
 
prev
 
next
 
- - - - - - -

-Additional Inherited Members

- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Components.Wings.Control_Surface.Control_Surface.__defaults__ ( self)
-
-
This sets the default values of control surfaces defined in SUAVE. 
-    sign_duplicate: 1.0 or -1.0 - the sign of the duplicate control on the mirror wing.
-    Use 1.0 for a mirrored control surface, like an elevator. Use -1.0 for an aileron.
-The span fraction is given by the array shown below:  
-    [abs. % span location at beginning of crtl surf, abs. % span location at end  of crtl surf]
-    
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Wings/Control_Surface.py
  • -
-
-
- - - - diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surface_1_1Control__Surface.js b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surface_1_1Control__Surface.js deleted file mode 100644 index da212585..00000000 --- a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surface_1_1Control__Surface.js +++ /dev/null @@ -1,5 +0,0 @@ -var classSUAVE_1_1Components_1_1Wings_1_1Control__Surface_1_1Control__Surface = -[ - [ "__defaults__", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surface_1_1Control__Surface.html#a3a781f5847d12f2774321c3ef8b2247c", null ], - [ "append_section", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surface_1_1Control__Surface.html#ac0a1c6961466410eaa6bd591ad1fca87", null ] -]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surface_1_1Control__Surface.png b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surface_1_1Control__Surface.png deleted file mode 100644 index b2557445..00000000 Binary files a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surface_1_1Control__Surface.png and /dev/null differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surface_1_1Control__Surface__Section-members.html b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surface_1_1Control__Surface__Section-members.html deleted file mode 100644 index 58b17080..00000000 --- a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surface_1_1Control__Surface__Section-members.html +++ /dev/null @@ -1,127 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.1.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
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-
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-
-
- -
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- - -
- -
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-
SUAVE.Components.Wings.Control_Surface.Control_Surface_Section Member List
-
-
- -

This is the complete list of members for SUAVE.Components.Wings.Control_Surface.Control_Surface_Section, including all inherited members.

- - - - - - - - - - - - - - - - -
__defaults__(self) (defined in SUAVE.Components.Wings.Control_Surface.Control_Surface_Section)SUAVE.Components.Wings.Control_Surface.Control_Surface_Section
chord (defined in SUAVE.Components.Wings.Control_Surface.Control_Surface_Section)SUAVE.Components.Wings.Control_Surface.Control_Surface_Sectionstatic
chord_fraction (defined in SUAVE.Components.Wings.Control_Surface.Control_Surface_Section)SUAVE.Components.Wings.Control_Surface.Control_Surface_Sectionstatic
Curves (defined in SUAVE.Components.Lofted_Body.Section)SUAVE.Components.Lofted_Body.Section
dimensional (defined in SUAVE.Components.Wings.Control_Surface.Control_Surface_Section)SUAVE.Components.Wings.Control_Surface.Control_Surface_Sectionstatic
leading_edge (defined in SUAVE.Components.Wings.Control_Surface.Control_Surface_Section)SUAVE.Components.Wings.Control_Surface.Control_Surface_Sectionstatic
next (defined in SUAVE.Components.Lofted_Body.Section)SUAVE.Components.Lofted_Body.Section
origin (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
origins (defined in SUAVE.Components.Wings.Control_Surface.Control_Surface_Section)SUAVE.Components.Wings.Control_Surface.Control_Surface_Sectionstatic
points (defined in SUAVE.Components.Wings.Control_Surface.Control_Surface_Section)SUAVE.Components.Wings.Control_Surface.Control_Surface_Sectionstatic
prev (defined in SUAVE.Components.Lofted_Body.Section)SUAVE.Components.Lofted_Body.Section
span_fraction (defined in SUAVE.Components.Wings.Control_Surface.Control_Surface_Section)SUAVE.Components.Wings.Control_Surface.Control_Surface_Sectionstatic
tagSUAVE.Components.Wings.Control_Surface.Control_Surface_Sectionstatic
trailing_edge (defined in SUAVE.Components.Wings.Control_Surface.Control_Surface_Section)SUAVE.Components.Wings.Control_Surface.Control_Surface_Sectionstatic
twist (defined in SUAVE.Components.Wings.Control_Surface.Control_Surface_Section)SUAVE.Components.Wings.Control_Surface.Control_Surface_Sectionstatic
-
- - - - diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surface_1_1Control__Surface__Section.html b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surface_1_1Control__Surface__Section.html deleted file mode 100644 index 8607907c..00000000 --- a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surface_1_1Control__Surface__Section.html +++ /dev/null @@ -1,234 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Components.Wings.Control_Surface.Control_Surface_Section Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.1.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
-
- - - -
-
- -
-
-
- -
- -
-
- - -
- -
- -
- -
-
SUAVE.Components.Wings.Control_Surface.Control_Surface_Section Class Reference
-
-
-
-Inheritance diagram for SUAVE.Components.Wings.Control_Surface.Control_Surface_Section:
-
-
- - -SUAVE.Components.Lofted_Body.Section -SUAVE.Components.Component.Component - -
- - - - - - - - - - -

-Public Member Functions

-def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Lofted_Body.Section
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
- - - - - - - - - - - - - - - - - - - - - -

-Static Public Attributes

 tag
 
chord
 
chord_fraction
 
twist
 
origins
 
dimensional
 
span_fraction
 
points
 
leading_edge
 
trailing_edge
 
- - - - - - - - - - - - - - - -

-Additional Inherited Members

- Public Attributes inherited from SUAVE.Components.Lofted_Body.Section
tag
 
Curves
 
prev
 
next
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
-

Member Data Documentation

- -

◆ tag

- -
-
- - - - - -
- - - - -
SUAVE.Components.Wings.Control_Surface.Control_Surface_Section.tag
-
-static
-
-
This sets the default values control surface sections defined in SUAVE.   
-
-Assumptions:    
-None    
-
-Source: 
-N/A 
-
-Inputs: 
-None    
-
-Outputs:    
-None    
-
-Properties Used:    
-N/A 
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Wings/Control_Surface.py
  • -
-
-
- - - - diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surface_1_1Control__Surface__Section.js b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surface_1_1Control__Surface__Section.js deleted file mode 100644 index 2e0e48bc..00000000 --- a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surface_1_1Control__Surface__Section.js +++ /dev/null @@ -1,4 +0,0 @@ -var classSUAVE_1_1Components_1_1Wings_1_1Control__Surface_1_1Control__Surface__Section = -[ - [ "__defaults__", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surface_1_1Control__Surface__Section.html#a855cf0fac5ec39dd04d67cd0f438687b", null ] -]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surface_1_1Control__Surface__Section.png b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surface_1_1Control__Surface__Section.png deleted file mode 100644 index 1c3f0698..00000000 Binary files a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surface_1_1Control__Surface__Section.png and /dev/null differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Aileron_1_1Aileron-members.html b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Aileron_1_1Aileron-members.html new file mode 100644 index 00000000..90915dab --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Aileron_1_1Aileron-members.html @@ -0,0 +1,136 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
SUAVE.Components.Wings.Control_Surfaces.Aileron.Aileron Member List
+
+
+ +

This is the complete list of members for SUAVE.Components.Wings.Control_Surfaces.Aileron.Aileron, including all inherited members.

+ + + + + + + + + + + + + + + + + + +
__defaults__(self)SUAVE.Components.Wings.Control_Surfaces.Aileron.Aileron
chord_fraction (defined in SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface)SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface
configuration_type (defined in SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface)SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface
deflection (defined in SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface)SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface
gain (defined in SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface)SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
hinge_fraction (defined in SUAVE.Components.Wings.Control_Surfaces.Aileron.Aileron)SUAVE.Components.Wings.Control_Surfaces.Aileron.Aileron
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
sign_duplicate (defined in SUAVE.Components.Wings.Control_Surfaces.Aileron.Aileron)SUAVE.Components.Wings.Control_Surfaces.Aileron.Aileron
span (defined in SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface)SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface
span_fraction_end (defined in SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface)SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface
span_fraction_start (defined in SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface)SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Wings.Control_Surfaces.Aileron.Aileron)SUAVE.Components.Wings.Control_Surfaces.Aileron.Aileron
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Aileron_1_1Aileron.html b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Aileron_1_1Aileron.html new file mode 100644 index 00000000..42190001 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Aileron_1_1Aileron.html @@ -0,0 +1,269 @@ + + + + + + + +SUAVE: SUAVE.Components.Wings.Control_Surfaces.Aileron.Aileron Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Components.Wings.Control_Surfaces.Aileron.Aileron Class Reference
+
+
+
+Inheritance diagram for SUAVE.Components.Wings.Control_Surfaces.Aileron.Aileron:
+
+
+ + +SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface +SUAVE.Components.Physical_Component.Physical_Component +SUAVE.Components.Component.Component + +
+ + + + +

+Public Member Functions

def __defaults__ (self)
 
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Attributes

tag
 
hinge_fraction
 
sign_duplicate
 
- Public Attributes inherited from SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface
tag
 
span
 
span_fraction_start
 
span_fraction_end
 
hinge_fraction
 
chord_fraction
 
sign_duplicate
 
deflection
 
configuration_type
 
gain
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 
+

Detailed Description

+
This class is used to define slats in SUAVE
+
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+None
+
+Outputs:
+None
+
+Properties Used:
+N/A
+

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Components.Wings.Control_Surfaces.Aileron.Aileron.__defaults__ ( self)
+
+
This sets the default for slats in SUAVE.
+
+see Control_Surface().__defaults__ for an explanation of attributes
+    
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+None
+
+Outputs:
+None
+
+Properties Used:
+N/A
+
+

Reimplemented from SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface.

+ +
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Wings/Control_Surfaces/Aileron.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Aileron_1_1Aileron.js b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Aileron_1_1Aileron.js new file mode 100644 index 00000000..fa385cd8 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Aileron_1_1Aileron.js @@ -0,0 +1,7 @@ +var classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Aileron_1_1Aileron = +[ + [ "__defaults__", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Aileron_1_1Aileron.html#a1aef6c2fff4e4610f8c3957e970eba1b", null ], + [ "hinge_fraction", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Aileron_1_1Aileron.html#a0335292c5a97375a2bddc0983b813d44", null ], + [ "sign_duplicate", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Aileron_1_1Aileron.html#ac25dc134f708135060c5cb2b266054b6", null ], + [ "tag", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Aileron_1_1Aileron.html#afc38a662433e229cb08f4861a4ad43e6", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Aileron_1_1Aileron.png b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Aileron_1_1Aileron.png new file mode 100644 index 00000000..cf1601c1 Binary files /dev/null and b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Aileron_1_1Aileron.png differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Control__Surface_1_1Control__Surface-members.html b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Control__Surface_1_1Control__Surface-members.html new file mode 100644 index 00000000..74afbc99 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Control__Surface_1_1Control__Surface-members.html @@ -0,0 +1,136 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
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+
+
+ + + +
+
+ +
+
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+ +
+ +
+
+ + +
+ +
+ +
+
+
SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface Member List
+
+
+ +

This is the complete list of members for SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface, including all inherited members.

+ + + + + + + + + + + + + + + + + + +
__defaults__(self)SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface
chord_fraction (defined in SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface)SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface
configuration_type (defined in SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface)SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface
deflection (defined in SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface)SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface
gain (defined in SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface)SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
hinge_fraction (defined in SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface)SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
sign_duplicate (defined in SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface)SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface
span (defined in SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface)SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface
span_fraction_end (defined in SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface)SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface
span_fraction_start (defined in SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface)SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface)SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Control__Surface_1_1Control__Surface.html b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Control__Surface_1_1Control__Surface.html new file mode 100644 index 00000000..a47936ce --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Control__Surface_1_1Control__Surface.html @@ -0,0 +1,262 @@ + + + + + + + +SUAVE: SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface Class Reference
+
+
+
+Inheritance diagram for SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface:
+
+
+ + +SUAVE.Components.Physical_Component.Physical_Component +SUAVE.Components.Component.Component +SUAVE.Components.Wings.Control_Surfaces.Aileron.Aileron +SUAVE.Components.Wings.Control_Surfaces.Elevator.Elevator +SUAVE.Components.Wings.Control_Surfaces.Flap.Flap +SUAVE.Components.Wings.Control_Surfaces.Rudder.Rudder +SUAVE.Components.Wings.Control_Surfaces.Slat.Slat + +
+ + + + +

+Public Member Functions

def __defaults__ (self)
 
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Attributes

tag
 
span
 
span_fraction_start
 
span_fraction_end
 
hinge_fraction
 
chord_fraction
 
sign_duplicate
 
deflection
 
configuration_type
 
gain
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 
+

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface.__defaults__ ( self)
+
+
This sets the default values of control surfaces defined in SUAVE. 
+
+- span: the span of the control surface in meters        
+- span_fraction_start: % span of the wing where the control surface starts        
+- span_fraction_start: % span of the wing where the control surface starts
+
+- hinge_fraction: number between 0.0 and 1.0. This corresponds to the location of the 
+    hingeline, where 0 and 1 correspond to the leading and trailing edges, respectively, 
+    of the CONTROL SURFACE (NOT the wing).
+- chord_fraction: number between 0.0 and 1.0 describing the fraction of the wing's chord
+    that is 'cut' out by the control surface
+
+- sign_duplicate: 1.0 or -1.0 - the sign of the duplicate control on the mirror wing.        
+    Use 1.0 for a mirrored control surface, like an elevator. Use -1.0 for an aileron.
+- deflection: the angle the control surface is deflected. 
+- configuration_type: the kind of control surface (e.g. single_slotted)
+
+Assumptions:
+- for chord_fraction, Slats are always cut out from the leading edge and everything else
+    os cut out from the trailing edge.
+
+Source:
+N/A
+
+Inputs:
+None
+
+Outputs:
+None
+
+Properties Used:
+N/A
+
+

Reimplemented from SUAVE.Components.Physical_Component.Physical_Component.

+ +

Reimplemented in SUAVE.Components.Wings.Control_Surfaces.Aileron.Aileron, SUAVE.Components.Wings.Control_Surfaces.Elevator.Elevator, SUAVE.Components.Wings.Control_Surfaces.Flap.Flap, SUAVE.Components.Wings.Control_Surfaces.Rudder.Rudder, and SUAVE.Components.Wings.Control_Surfaces.Slat.Slat.

+ +
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Wings/Control_Surfaces/Control_Surface.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Control__Surface_1_1Control__Surface.js b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Control__Surface_1_1Control__Surface.js new file mode 100644 index 00000000..e51baa51 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Control__Surface_1_1Control__Surface.js @@ -0,0 +1,14 @@ +var classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Control__Surface_1_1Control__Surface = +[ + [ "__defaults__", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Control__Surface_1_1Control__Surface.html#a266272aaf7c761a92f0d4263d08ec6f6", null ], + [ "chord_fraction", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Control__Surface_1_1Control__Surface.html#ad310ffe2632c5f8aafc423137a8e7790", null ], + [ "configuration_type", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Control__Surface_1_1Control__Surface.html#abe8c19fab542263392f677464859fd5b", null ], + [ "deflection", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Control__Surface_1_1Control__Surface.html#ab384c96474818b75e512327dac1a124c", null ], + [ "gain", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Control__Surface_1_1Control__Surface.html#a068ded7bfe62fcd99af1546b09e7f413", null ], + [ "hinge_fraction", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Control__Surface_1_1Control__Surface.html#a107e91da9b6a9de5e54ea935466dfc1a", null ], + [ "sign_duplicate", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Control__Surface_1_1Control__Surface.html#a87b559559bd66b520f6ed249248891e1", null ], + [ "span", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Control__Surface_1_1Control__Surface.html#aa494855dfe72d9fd9e794d242c612d5a", null ], + [ "span_fraction_end", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Control__Surface_1_1Control__Surface.html#a61ea28b90ef5f20680789b261146b9d9", null ], + [ "span_fraction_start", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Control__Surface_1_1Control__Surface.html#a84befa5459c4e7bb0ed4aaa5785d61c4", null ], + [ "tag", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Control__Surface_1_1Control__Surface.html#a79d658a9ea81b367ce91633d1a8f0272", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Control__Surface_1_1Control__Surface.png b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Control__Surface_1_1Control__Surface.png new file mode 100644 index 00000000..ced33acd Binary files /dev/null and b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Control__Surface_1_1Control__Surface.png differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Elevator_1_1Elevator-members.html b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Elevator_1_1Elevator-members.html new file mode 100644 index 00000000..c2a55fee --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Elevator_1_1Elevator-members.html @@ -0,0 +1,136 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
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+ +
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+
+
SUAVE.Components.Wings.Control_Surfaces.Elevator.Elevator Member List
+
+
+ +

This is the complete list of members for SUAVE.Components.Wings.Control_Surfaces.Elevator.Elevator, including all inherited members.

+ + + + + + + + + + + + + + + + + + +
__defaults__(self)SUAVE.Components.Wings.Control_Surfaces.Elevator.Elevator
chord_fraction (defined in SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface)SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface
configuration_type (defined in SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface)SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface
deflection (defined in SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface)SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface
gain (defined in SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface)SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
hinge_fraction (defined in SUAVE.Components.Wings.Control_Surfaces.Elevator.Elevator)SUAVE.Components.Wings.Control_Surfaces.Elevator.Elevator
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
sign_duplicate (defined in SUAVE.Components.Wings.Control_Surfaces.Elevator.Elevator)SUAVE.Components.Wings.Control_Surfaces.Elevator.Elevator
span (defined in SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface)SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface
span_fraction_end (defined in SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface)SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface
span_fraction_start (defined in SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface)SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Wings.Control_Surfaces.Elevator.Elevator)SUAVE.Components.Wings.Control_Surfaces.Elevator.Elevator
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Elevator_1_1Elevator.html b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Elevator_1_1Elevator.html new file mode 100644 index 00000000..9cf88fa9 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Elevator_1_1Elevator.html @@ -0,0 +1,269 @@ + + + + + + + +SUAVE: SUAVE.Components.Wings.Control_Surfaces.Elevator.Elevator Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Components.Wings.Control_Surfaces.Elevator.Elevator Class Reference
+
+
+
+Inheritance diagram for SUAVE.Components.Wings.Control_Surfaces.Elevator.Elevator:
+
+
+ + +SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface +SUAVE.Components.Physical_Component.Physical_Component +SUAVE.Components.Component.Component + +
+ + + + +

+Public Member Functions

def __defaults__ (self)
 
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Attributes

tag
 
hinge_fraction
 
sign_duplicate
 
- Public Attributes inherited from SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface
tag
 
span
 
span_fraction_start
 
span_fraction_end
 
hinge_fraction
 
chord_fraction
 
sign_duplicate
 
deflection
 
configuration_type
 
gain
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 
+

Detailed Description

+
This class is used to define slats in SUAVE
+
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+None
+
+Outputs:
+None
+
+Properties Used:
+N/A
+

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Components.Wings.Control_Surfaces.Elevator.Elevator.__defaults__ ( self)
+
+
This sets the default for slats in SUAVE.
+
+see Control_Surface().__defaults__ for an explanation of attributes
+    
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+None
+
+Outputs:
+None
+
+Properties Used:
+N/A
+
+

Reimplemented from SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface.

+ +
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Wings/Control_Surfaces/Elevator.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Elevator_1_1Elevator.js b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Elevator_1_1Elevator.js new file mode 100644 index 00000000..33c7ab04 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Elevator_1_1Elevator.js @@ -0,0 +1,7 @@ +var classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Elevator_1_1Elevator = +[ + [ "__defaults__", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Elevator_1_1Elevator.html#a14963fc6797c8433c15b0ae135e765c4", null ], + [ "hinge_fraction", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Elevator_1_1Elevator.html#aff3c52011ae60ea6fc8a57609f50fd7e", null ], + [ "sign_duplicate", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Elevator_1_1Elevator.html#a7820e96e94fa54a3a83014ff1e4e8530", null ], + [ "tag", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Elevator_1_1Elevator.html#afa594ff8374a2c1ad267a913ff851e9f", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Elevator_1_1Elevator.png b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Elevator_1_1Elevator.png new file mode 100644 index 00000000..74296ff6 Binary files /dev/null and b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Elevator_1_1Elevator.png differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Flap_1_1Flap-members.html b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Flap_1_1Flap-members.html new file mode 100644 index 00000000..f351d6ff --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Flap_1_1Flap-members.html @@ -0,0 +1,136 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
SUAVE.Components.Wings.Control_Surfaces.Flap.Flap Member List
+
+
+ +

This is the complete list of members for SUAVE.Components.Wings.Control_Surfaces.Flap.Flap, including all inherited members.

+ + + + + + + + + + + + + + + + + + +
__defaults__(self)SUAVE.Components.Wings.Control_Surfaces.Flap.Flap
chord_fraction (defined in SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface)SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface
configuration_type (defined in SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface)SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface
deflection (defined in SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface)SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface
gain (defined in SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface)SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
hinge_fraction (defined in SUAVE.Components.Wings.Control_Surfaces.Flap.Flap)SUAVE.Components.Wings.Control_Surfaces.Flap.Flap
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
sign_duplicate (defined in SUAVE.Components.Wings.Control_Surfaces.Flap.Flap)SUAVE.Components.Wings.Control_Surfaces.Flap.Flap
span (defined in SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface)SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface
span_fraction_end (defined in SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface)SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface
span_fraction_start (defined in SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface)SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Wings.Control_Surfaces.Flap.Flap)SUAVE.Components.Wings.Control_Surfaces.Flap.Flap
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Flap_1_1Flap.html b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Flap_1_1Flap.html new file mode 100644 index 00000000..58bf2956 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Flap_1_1Flap.html @@ -0,0 +1,269 @@ + + + + + + + +SUAVE: SUAVE.Components.Wings.Control_Surfaces.Flap.Flap Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Components.Wings.Control_Surfaces.Flap.Flap Class Reference
+
+
+
+Inheritance diagram for SUAVE.Components.Wings.Control_Surfaces.Flap.Flap:
+
+
+ + +SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface +SUAVE.Components.Physical_Component.Physical_Component +SUAVE.Components.Component.Component + +
+ + + + +

+Public Member Functions

def __defaults__ (self)
 
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Attributes

tag
 
hinge_fraction
 
sign_duplicate
 
- Public Attributes inherited from SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface
tag
 
span
 
span_fraction_start
 
span_fraction_end
 
hinge_fraction
 
chord_fraction
 
sign_duplicate
 
deflection
 
configuration_type
 
gain
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 
+

Detailed Description

+
This class is used to define slats in SUAVE
+
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+None
+
+Outputs:
+None
+
+Properties Used:
+N/A
+

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Components.Wings.Control_Surfaces.Flap.Flap.__defaults__ ( self)
+
+
This sets the default for slats in SUAVE.
+
+see Control_Surface().__defaults__ for an explanation of attributes
+    
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+None
+
+Outputs:
+None
+
+Properties Used:
+N/A
+
+

Reimplemented from SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface.

+ +
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Wings/Control_Surfaces/Flap.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Flap_1_1Flap.js b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Flap_1_1Flap.js new file mode 100644 index 00000000..f9127f15 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Flap_1_1Flap.js @@ -0,0 +1,7 @@ +var classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Flap_1_1Flap = +[ + [ "__defaults__", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Flap_1_1Flap.html#a71a66ce5826c44d8f027db149ae4430a", null ], + [ "hinge_fraction", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Flap_1_1Flap.html#a175e44b3849244a14c3a2a96146e26f4", null ], + [ "sign_duplicate", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Flap_1_1Flap.html#a96a77fb3a7879e9e33b14d60a8838057", null ], + [ "tag", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Flap_1_1Flap.html#a67d2e06146f3516abf653bd298877a91", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Flap_1_1Flap.png b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Flap_1_1Flap.png new file mode 100644 index 00000000..f3285766 Binary files /dev/null and b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Flap_1_1Flap.png differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Rudder_1_1Rudder-members.html b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Rudder_1_1Rudder-members.html new file mode 100644 index 00000000..23dbb4a4 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Rudder_1_1Rudder-members.html @@ -0,0 +1,136 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
SUAVE.Components.Wings.Control_Surfaces.Rudder.Rudder Member List
+
+
+ +

This is the complete list of members for SUAVE.Components.Wings.Control_Surfaces.Rudder.Rudder, including all inherited members.

+ + + + + + + + + + + + + + + + + + +
__defaults__(self)SUAVE.Components.Wings.Control_Surfaces.Rudder.Rudder
chord_fraction (defined in SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface)SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface
configuration_type (defined in SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface)SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface
deflection (defined in SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface)SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface
gain (defined in SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface)SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
hinge_fraction (defined in SUAVE.Components.Wings.Control_Surfaces.Rudder.Rudder)SUAVE.Components.Wings.Control_Surfaces.Rudder.Rudder
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
sign_duplicate (defined in SUAVE.Components.Wings.Control_Surfaces.Rudder.Rudder)SUAVE.Components.Wings.Control_Surfaces.Rudder.Rudder
span (defined in SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface)SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface
span_fraction_end (defined in SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface)SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface
span_fraction_start (defined in SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface)SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Wings.Control_Surfaces.Rudder.Rudder)SUAVE.Components.Wings.Control_Surfaces.Rudder.Rudder
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Rudder_1_1Rudder.html b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Rudder_1_1Rudder.html new file mode 100644 index 00000000..186d0281 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Rudder_1_1Rudder.html @@ -0,0 +1,269 @@ + + + + + + + +SUAVE: SUAVE.Components.Wings.Control_Surfaces.Rudder.Rudder Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Components.Wings.Control_Surfaces.Rudder.Rudder Class Reference
+
+
+
+Inheritance diagram for SUAVE.Components.Wings.Control_Surfaces.Rudder.Rudder:
+
+
+ + +SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface +SUAVE.Components.Physical_Component.Physical_Component +SUAVE.Components.Component.Component + +
+ + + + +

+Public Member Functions

def __defaults__ (self)
 
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Attributes

tag
 
hinge_fraction
 
sign_duplicate
 
- Public Attributes inherited from SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface
tag
 
span
 
span_fraction_start
 
span_fraction_end
 
hinge_fraction
 
chord_fraction
 
sign_duplicate
 
deflection
 
configuration_type
 
gain
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 
+

Detailed Description

+
This class is used to define slats in SUAVE
+
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+None
+
+Outputs:
+None
+
+Properties Used:
+N/A
+

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Components.Wings.Control_Surfaces.Rudder.Rudder.__defaults__ ( self)
+
+
This sets the default for slats in SUAVE.
+
+see Control_Surface().__defaults__ for an explanation of attributes
+    
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+None
+
+Outputs:
+None
+
+Properties Used:
+N/A
+
+

Reimplemented from SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface.

+ +
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Wings/Control_Surfaces/Rudder.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Rudder_1_1Rudder.js b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Rudder_1_1Rudder.js new file mode 100644 index 00000000..7a5a7b43 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Rudder_1_1Rudder.js @@ -0,0 +1,7 @@ +var classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Rudder_1_1Rudder = +[ + [ "__defaults__", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Rudder_1_1Rudder.html#ad84bc82bb1ee0d8aec7dc204495343b7", null ], + [ "hinge_fraction", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Rudder_1_1Rudder.html#acb8fec0ae31489890a36673a5b406843", null ], + [ "sign_duplicate", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Rudder_1_1Rudder.html#a23f9597375bfdf7679e5ed52780525f2", null ], + [ "tag", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Rudder_1_1Rudder.html#a9543a54cef7d6303f7c20ba29e883c24", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Rudder_1_1Rudder.png b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Rudder_1_1Rudder.png new file mode 100644 index 00000000..d1502744 Binary files /dev/null and b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Rudder_1_1Rudder.png differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Slat_1_1Slat-members.html b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Slat_1_1Slat-members.html new file mode 100644 index 00000000..8ee7f421 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Slat_1_1Slat-members.html @@ -0,0 +1,136 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
SUAVE.Components.Wings.Control_Surfaces.Slat.Slat Member List
+
+
+ +

This is the complete list of members for SUAVE.Components.Wings.Control_Surfaces.Slat.Slat, including all inherited members.

+ + + + + + + + + + + + + + + + + + +
__defaults__(self)SUAVE.Components.Wings.Control_Surfaces.Slat.Slat
chord_fraction (defined in SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface)SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface
configuration_type (defined in SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface)SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface
deflection (defined in SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface)SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface
gain (defined in SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface)SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface
generative_design_characteristics (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_max_per_vehicle (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
hinge_fraction (defined in SUAVE.Components.Wings.Control_Surfaces.Slat.Slat)SUAVE.Components.Wings.Control_Surfaces.Slat.Slat
mass_properties (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
sign_duplicate (defined in SUAVE.Components.Wings.Control_Surfaces.Slat.Slat)SUAVE.Components.Wings.Control_Surfaces.Slat.Slat
span (defined in SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface)SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface
span_fraction_end (defined in SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface)SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface
span_fraction_start (defined in SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface)SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface
symmetric (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component
tag (defined in SUAVE.Components.Wings.Control_Surfaces.Slat.Slat)SUAVE.Components.Wings.Control_Surfaces.Slat.Slat
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Slat_1_1Slat.html b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Slat_1_1Slat.html new file mode 100644 index 00000000..a9c61c52 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Slat_1_1Slat.html @@ -0,0 +1,269 @@ + + + + + + + +SUAVE: SUAVE.Components.Wings.Control_Surfaces.Slat.Slat Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Components.Wings.Control_Surfaces.Slat.Slat Class Reference
+
+
+
+Inheritance diagram for SUAVE.Components.Wings.Control_Surfaces.Slat.Slat:
+
+
+ + +SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface +SUAVE.Components.Physical_Component.Physical_Component +SUAVE.Components.Component.Component + +
+ + + + +

+Public Member Functions

def __defaults__ (self)
 
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Attributes

tag
 
hinge_fraction
 
sign_duplicate
 
- Public Attributes inherited from SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface
tag
 
span
 
span_fraction_start
 
span_fraction_end
 
hinge_fraction
 
chord_fraction
 
sign_duplicate
 
deflection
 
configuration_type
 
gain
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 
+

Detailed Description

+
This class is used to define slats in SUAVE
+
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+None
+
+Outputs:
+None
+
+Properties Used:
+N/A
+

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Components.Wings.Control_Surfaces.Slat.Slat.__defaults__ ( self)
+
+
This sets the default for slats in SUAVE.
+
+see Control_Surface().__defaults__ for an explanation of attributes
+    
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+None
+
+Outputs:
+None
+
+Properties Used:
+N/A
+
+

Reimplemented from SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface.

+ +
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Wings/Control_Surfaces/Slat.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Slat_1_1Slat.js b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Slat_1_1Slat.js new file mode 100644 index 00000000..1323b91c --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Slat_1_1Slat.js @@ -0,0 +1,7 @@ +var classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Slat_1_1Slat = +[ + [ "__defaults__", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Slat_1_1Slat.html#a1b9d0bcc5720185967deee4c82fcdd64", null ], + [ "hinge_fraction", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Slat_1_1Slat.html#aad49f95d5e0db82212ae9ac67c4bfa4a", null ], + [ "sign_duplicate", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Slat_1_1Slat.html#a49144d397031c73769845d5bac37bca3", null ], + [ "tag", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Slat_1_1Slat.html#af141c42e0810a2f107ce0d7165037573", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Slat_1_1Slat.png b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Slat_1_1Slat.png new file mode 100644 index 00000000..727e9bb3 Binary files /dev/null and b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Slat_1_1Slat.png differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Horizontal__Tail_1_1Horizontal__Tail-members.html b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Horizontal__Tail_1_1Horizontal__Tail-members.html index 4855049e..e477bc49 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Horizontal__Tail_1_1Horizontal__Tail-members.html +++ b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Horizontal__Tail_1_1Horizontal__Tail-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -103,35 +110,42 @@ Airfoil (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing append_airfoil(self, airfoil)SUAVE.Components.Wings.Wing.Wing append_control_surface(self, control_surface)SUAVE.Components.Wings.Wing.Wing - append_segment(self, segment)SUAVE.Components.Wings.Wing.Wing - areas (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing - aspect_ratio (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing - chords (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing - control_surfaces (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing - dihedral (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + append_fuel_tank(self, fuel_tank)SUAVE.Components.Wings.Wing.Wing + append_segment(self, segment)SUAVE.Components.Wings.Wing.Wing + areas (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + aspect_ratio (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + chords (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + control_surfaces (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + dihedral (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + dynamic_pressure_ratio (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing exposed_root_chord_offset (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing - flaps (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + Fuel_Tanks (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + generative_design_char_max_bounds (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + generative_design_char_min_bounds (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + generative_design_characteristics (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + generative_design_max_per_vehicle (defined in SUAVE.Components.Wings.Horizontal_Tail.Horizontal_Tail)SUAVE.Components.Wings.Horizontal_Tail.Horizontal_Tail + generative_design_minimum (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component high_lift (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing high_mach (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing mass_properties (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing - origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component - position (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing - Sections (defined in SUAVE.Components.Lofted_Body.Lofted_Body)SUAVE.Components.Lofted_Body.Lofted_Body - Segments (defined in SUAVE.Components.Lofted_Body.Lofted_Body)SUAVE.Components.Lofted_Body.Lofted_Body - slats (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing - span_efficiency (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing - spans (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing - sweeps (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + non_dimensional_origin (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + origin (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + Segments (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + spans (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + sweeps (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + symbolic (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing symmetric (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing t_tail (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing - tag (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + tag (defined in SUAVE.Components.Wings.Horizontal_Tail.Horizontal_Tail)SUAVE.Components.Wings.Horizontal_Tail.Horizontal_Tail taper (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing thickness_to_chord (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing - transition_x_lower (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing - transition_x_upper (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing - twists (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing - vertical (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing - vortex_lift (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + total_length (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + transition_x_lower (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + transition_x_upper (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + twists (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + vertical (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + vortex_lift (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
@@ -139,7 +153,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Horizontal__Tail_1_1Horizontal__Tail.html b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Horizontal__Tail_1_1Horizontal__Tail.html index 7fcc41ef..1847042d 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Horizontal__Tail_1_1Horizontal__Tail.html +++ b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Horizontal__Tail_1_1Horizontal__Tail.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Components.Wings.Horizontal_Tail.Horizontal_Tail Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -93,6 +100,7 @@
SUAVE.Components.Wings.Horizontal_Tail.Horizontal_Tail Class Reference
@@ -108,34 +116,32 @@ SUAVE.Components.Lofted_Body.Lofted_Body SUAVE.Components.Physical_Component.Physical_Component SUAVE.Components.Component.Component - -
+SUAVE.Components.Wings.Stabilator.Stabilator + + - - - - - - - - - - - + +

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Wings.Wing.Wing
def __defaults__ (self)
 
def append_segment (self, segment)
 
def append_airfoil (self, airfoil)
 
def append_control_surface (self, control_surface)
 
- Public Member Functions inherited from SUAVE.Components.Lofted_Body.Lofted_Body
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
def append_fuel_tank (self, fuel_tank)
 
- + + + + + @@ -143,9 +149,9 @@ - - + + @@ -167,15 +173,15 @@ - - + + @@ -191,18 +197,12 @@ - - - - - - + + @@ -215,9 +215,39 @@ + + + + + + + + + + + + + + + + + + + + @@ -225,9 +255,6 @@ - - @@ -248,6 +275,15 @@ + + + + + +

-Additional Inherited Members

+Public Attributes

tag
 
generative_design_max_per_vehicle
 
- Public Attributes inherited from SUAVE.Components.Wings.Wing.Wing
 tag
 mass_properties
 
position
 
origin
 
 symmetric
 
 thickness_to_chord
 
span_efficiency
 
 aerodynamic_center
 
 exposed_root_chord_offset
 
total_length
 
 spans
 
 twists
 
control_surfaces
 
flaps
 
slats
 
 high_lift
 
symbolic
 
 high_mach
 
 transition_x_lower
 
dynamic_pressure_ratio
 
 Airfoil
 
non_dimensional_origin
 
generative_design_minimum
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_char_min_bounds
 
generative_design_char_max_bounds
 
Segments
 
control_surfaces
 
Fuel_Tanks
 
- Public Attributes inherited from SUAVE.Components.Lofted_Body.Lofted_Body
 tag
 Segments
 
Sections
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
 tag
 origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 

Detailed Description

This class is used to define horiontal tails SUAVE
@@ -298,6 +334,10 @@ 

SUAVE.Components.Wings.Wing.Wing.

+ +

Reimplemented in SUAVE.Components.Wings.Stabilator.Stabilator.

+


The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Horizontal__Tail_1_1Horizontal__Tail.js b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Horizontal__Tail_1_1Horizontal__Tail.js index 36a689c5..f934121d 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Horizontal__Tail_1_1Horizontal__Tail.js +++ b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Horizontal__Tail_1_1Horizontal__Tail.js @@ -1,4 +1,6 @@ var classSUAVE_1_1Components_1_1Wings_1_1Horizontal__Tail_1_1Horizontal__Tail = [ - [ "__defaults__", "classSUAVE_1_1Components_1_1Wings_1_1Horizontal__Tail_1_1Horizontal__Tail.html#a674bb83b6f89d403ae41c506caaedc1d", null ] + [ "__defaults__", "classSUAVE_1_1Components_1_1Wings_1_1Horizontal__Tail_1_1Horizontal__Tail.html#a674bb83b6f89d403ae41c506caaedc1d", null ], + [ "generative_design_max_per_vehicle", "classSUAVE_1_1Components_1_1Wings_1_1Horizontal__Tail_1_1Horizontal__Tail.html#afaf847a03e6441af79de0a9032f2f21c", null ], + [ "tag", "classSUAVE_1_1Components_1_1Wings_1_1Horizontal__Tail_1_1Horizontal__Tail.html#aa3f910d2b56c8e38647fac287197d977", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Horizontal__Tail_1_1Horizontal__Tail.png b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Horizontal__Tail_1_1Horizontal__Tail.png index adfa3a00..b4f9647e 100644 Binary files a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Horizontal__Tail_1_1Horizontal__Tail.png and b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Horizontal__Tail_1_1Horizontal__Tail.png differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Main__Wing_1_1Main__Wing-members.html b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Main__Wing_1_1Main__Wing-members.html index 82252a34..0fd844d6 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Main__Wing_1_1Main__Wing-members.html +++ b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Main__Wing_1_1Main__Wing-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -103,35 +110,42 @@ Airfoil (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing append_airfoil(self, airfoil)SUAVE.Components.Wings.Wing.Wing append_control_surface(self, control_surface)SUAVE.Components.Wings.Wing.Wing - append_segment(self, segment)SUAVE.Components.Wings.Wing.Wing - areas (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing - aspect_ratio (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing - chords (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing - control_surfaces (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing - dihedral (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + append_fuel_tank(self, fuel_tank)SUAVE.Components.Wings.Wing.Wing + append_segment(self, segment)SUAVE.Components.Wings.Wing.Wing + areas (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + aspect_ratio (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + chords (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + control_surfaces (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + dihedral (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + dynamic_pressure_ratio (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing exposed_root_chord_offset (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing - flaps (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + Fuel_Tanks (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + generative_design_char_max_bounds (defined in SUAVE.Components.Wings.Main_Wing.Main_Wing)SUAVE.Components.Wings.Main_Wing.Main_Wing + generative_design_char_min_bounds (defined in SUAVE.Components.Wings.Main_Wing.Main_Wing)SUAVE.Components.Wings.Main_Wing.Main_Wing + generative_design_characteristics (defined in SUAVE.Components.Wings.Main_Wing.Main_Wing)SUAVE.Components.Wings.Main_Wing.Main_Wing + generative_design_max_per_vehicle (defined in SUAVE.Components.Wings.Main_Wing.Main_Wing)SUAVE.Components.Wings.Main_Wing.Main_Wing + generative_design_minimum (defined in SUAVE.Components.Wings.Main_Wing.Main_Wing)SUAVE.Components.Wings.Main_Wing.Main_Wing + generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component high_lift (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing high_mach (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing mass_properties (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing - origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component - position (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing - Sections (defined in SUAVE.Components.Lofted_Body.Lofted_Body)SUAVE.Components.Lofted_Body.Lofted_Body - Segments (defined in SUAVE.Components.Lofted_Body.Lofted_Body)SUAVE.Components.Lofted_Body.Lofted_Body - slats (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing - span_efficiency (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing - spans (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing - sweeps (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + non_dimensional_origin (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + origin (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + Segments (defined in SUAVE.Components.Wings.Main_Wing.Main_Wing)SUAVE.Components.Wings.Main_Wing.Main_Wing + spans (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + sweeps (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + symbolic (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing symmetric (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing t_tail (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing - tag (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + tag (defined in SUAVE.Components.Wings.Main_Wing.Main_Wing)SUAVE.Components.Wings.Main_Wing.Main_Wing taper (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing thickness_to_chord (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing - transition_x_lower (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing - transition_x_upper (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing - twists (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing - vertical (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing - vortex_lift (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + total_length (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + transition_x_lower (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + transition_x_upper (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + twists (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + vertical (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + vortex_lift (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
@@ -139,7 +153,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Main__Wing_1_1Main__Wing.html b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Main__Wing_1_1Main__Wing.html index bee5c52a..3de0e383 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Main__Wing_1_1Main__Wing.html +++ b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Main__Wing_1_1Main__Wing.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Components.Wings.Main_Wing.Main_Wing Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -93,6 +100,7 @@
SUAVE.Components.Wings.Main_Wing.Main_Wing Class Reference
@@ -108,34 +116,46 @@ SUAVE.Components.Lofted_Body.Lofted_Body SUAVE.Components.Physical_Component.Physical_Component SUAVE.Components.Component.Component - -
+ + - - - - - - - - - - - + +

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Wings.Wing.Wing
def __defaults__ (self)
 
def append_segment (self, segment)
 
def append_airfoil (self, airfoil)
 
def append_control_surface (self, control_surface)
 
- Public Member Functions inherited from SUAVE.Components.Lofted_Body.Lofted_Body
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
def append_fuel_tank (self, fuel_tank)
 
- + + + + + + + + + + + + + + + @@ -143,9 +163,9 @@ - - + + @@ -167,15 +187,15 @@ - - + + @@ -191,18 +211,12 @@ - - - - - - + + @@ -215,9 +229,39 @@ + + + + + + + + + + + + + + + + + + + + @@ -225,9 +269,6 @@ - - @@ -248,6 +289,15 @@ + + + + + +

-Additional Inherited Members

+Public Attributes

tag
 
Segments
 
generative_design_max_per_vehicle
 
generative_design_minimum
 
generative_design_characteristics
 
generative_design_char_min_bounds
 
generative_design_char_max_bounds
 
- Public Attributes inherited from SUAVE.Components.Wings.Wing.Wing
 tag
 mass_properties
 
position
 
origin
 
 symmetric
 
 thickness_to_chord
 
span_efficiency
 
 aerodynamic_center
 
 exposed_root_chord_offset
 
total_length
 
 spans
 
 twists
 
control_surfaces
 
flaps
 
slats
 
 high_lift
 
symbolic
 
 high_mach
 
 transition_x_lower
 
dynamic_pressure_ratio
 
 Airfoil
 
non_dimensional_origin
 
generative_design_minimum
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_char_min_bounds
 
generative_design_char_max_bounds
 
Segments
 
control_surfaces
 
Fuel_Tanks
 
- Public Attributes inherited from SUAVE.Components.Lofted_Body.Lofted_Body
 tag
 Segments
 
Sections
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
 tag
 origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 

Detailed Description

This class is used to define main wings SUAVE
@@ -299,6 +349,8 @@ 

SUAVE.Components.Wings.Wing.Wing.

+


The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Main__Wing_1_1Main__Wing.js b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Main__Wing_1_1Main__Wing.js index cc39dea4..7df641a1 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Main__Wing_1_1Main__Wing.js +++ b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Main__Wing_1_1Main__Wing.js @@ -1,4 +1,11 @@ var classSUAVE_1_1Components_1_1Wings_1_1Main__Wing_1_1Main__Wing = [ - [ "__defaults__", "classSUAVE_1_1Components_1_1Wings_1_1Main__Wing_1_1Main__Wing.html#afb04e9aa708e98fcaacd798cea14da3f", null ] + [ "__defaults__", "classSUAVE_1_1Components_1_1Wings_1_1Main__Wing_1_1Main__Wing.html#afb04e9aa708e98fcaacd798cea14da3f", null ], + [ "generative_design_char_max_bounds", "classSUAVE_1_1Components_1_1Wings_1_1Main__Wing_1_1Main__Wing.html#a102e9173b9451207b988cff4e2f0a7d7", null ], + [ "generative_design_char_min_bounds", "classSUAVE_1_1Components_1_1Wings_1_1Main__Wing_1_1Main__Wing.html#a457e36d84402bcf64afba75141155499", null ], + [ "generative_design_characteristics", "classSUAVE_1_1Components_1_1Wings_1_1Main__Wing_1_1Main__Wing.html#a11b86dbab02f565c56e66c5fab0c87d7", null ], + [ "generative_design_max_per_vehicle", "classSUAVE_1_1Components_1_1Wings_1_1Main__Wing_1_1Main__Wing.html#af23a55f74c7f85ab7ad97d99c47e9cac", null ], + [ "generative_design_minimum", "classSUAVE_1_1Components_1_1Wings_1_1Main__Wing_1_1Main__Wing.html#accfc901b0a20d3336f61ef2e987b9dbd", null ], + [ "Segments", "classSUAVE_1_1Components_1_1Wings_1_1Main__Wing_1_1Main__Wing.html#ae1ea6977cb2b23929676b33a1f938e1b", null ], + [ "tag", "classSUAVE_1_1Components_1_1Wings_1_1Main__Wing_1_1Main__Wing.html#af60a731c84888e88d3fcfc1cbba1b135", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Main__Wing_1_1Segment__Container-members.html b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Main__Wing_1_1Segment__Container-members.html new file mode 100644 index 00000000..56fd2bfa --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Main__Wing_1_1Segment__Container-members.html @@ -0,0 +1,121 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
SUAVE.Components.Wings.Main_Wing.Segment_Container Member List
+
+ +
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Main__Wing_1_1Segment__Container.html b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Main__Wing_1_1Segment__Container.html new file mode 100644 index 00000000..02315248 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Main__Wing_1_1Segment__Container.html @@ -0,0 +1,233 @@ + + + + + + + +SUAVE: SUAVE.Components.Wings.Main_Wing.Segment_Container Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Components.Wings.Main_Wing.Segment_Container Class Reference
+
+
+
+Inheritance diagram for SUAVE.Components.Wings.Main_Wing.Segment_Container:
+
+
+ +
+ + + + + + +

+Public Member Functions

def get_children (self)
 
def append (self, val)
 
+

Detailed Description

+
Container for wing segment
+
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+None
+
+Outputs:
+None
+
+Properties Used:
+N/A
+

Member Function Documentation

+ +

◆ append()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Components.Wings.Main_Wing.Segment_Container.append ( self,
 val 
)
+
+
Appends the value to the containers
+  This overrides the basic data class append
+    
+    Assumptions:
+    None
+    
+    Source:
+    N/A
+    
+    Inputs:
+    self
+    
+    Outputs:
+    N/A
+    
+    Properties Used:
+    N/A
+
+
+ +

◆ get_children()

+ +
+
+ + + + + + + + +
def SUAVE.Components.Wings.Main_Wing.Segment_Container.get_children ( self)
+
+
Returns the components that can go inside
+
+Assumptions:
+None
+    
+Source:
+N/A
+    
+Inputs:
+None
+    
+Outputs:
+None
+    
+Properties Used:
+N/A
+
+
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Wings/Main_Wing.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Main__Wing_1_1Segment__Container.js b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Main__Wing_1_1Segment__Container.js new file mode 100644 index 00000000..7007f4de --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Main__Wing_1_1Segment__Container.js @@ -0,0 +1,5 @@ +var classSUAVE_1_1Components_1_1Wings_1_1Main__Wing_1_1Segment__Container = +[ + [ "append", "classSUAVE_1_1Components_1_1Wings_1_1Main__Wing_1_1Segment__Container.html#a7a2f372812350469942ea561e0c03abd", null ], + [ "get_children", "classSUAVE_1_1Components_1_1Wings_1_1Main__Wing_1_1Segment__Container.html#ac954cb74df9e54d8fd508d9c8c201494", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Main__Wing_1_1Segment__Container.png b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Main__Wing_1_1Segment__Container.png new file mode 100644 index 00000000..162e5d08 Binary files /dev/null and b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Main__Wing_1_1Segment__Container.png differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Segment_1_1Segment-members.html b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Segment_1_1Segment-members.html index 6961e422..c8b34e2c 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Segment_1_1Segment-members.html +++ b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Segment_1_1Segment-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -101,9 +108,15 @@ __defaults__(self)SUAVE.Components.Wings.Segment.Segment Airfoil (defined in SUAVE.Components.Wings.Segment.Segment)SUAVE.Components.Wings.Segment.Segment append_airfoil(self, airfoil)SUAVE.Components.Wings.Segment.Segment - append_control_surface(self, control_surface)SUAVE.Components.Wings.Segment.Segment - control_surfaces (defined in SUAVE.Components.Wings.Segment.Segment)SUAVE.Components.Wings.Segment.Segment + areas (defined in SUAVE.Components.Wings.Segment.Segment)SUAVE.Components.Wings.Segment.Segment + chords (defined in SUAVE.Components.Wings.Segment.Segment)SUAVE.Components.Wings.Segment.Segment dihedral_outboard (defined in SUAVE.Components.Wings.Segment.Segment)SUAVE.Components.Wings.Segment.Segment + generative_design_char_max_bounds (defined in SUAVE.Components.Wings.Segment.Segment)SUAVE.Components.Wings.Segment.Segment + generative_design_char_min_bounds (defined in SUAVE.Components.Wings.Segment.Segment)SUAVE.Components.Wings.Segment.Segment + generative_design_characteristics (defined in SUAVE.Components.Wings.Segment.Segment)SUAVE.Components.Wings.Segment.Segment + generative_design_max_per_vehicle (defined in SUAVE.Components.Wings.Segment.Segment)SUAVE.Components.Wings.Segment.Segment + generative_design_minimum (defined in SUAVE.Components.Wings.Segment.Segment)SUAVE.Components.Wings.Segment.Segment + generative_design_special_parent (defined in SUAVE.Components.Wings.Segment.Segment)SUAVE.Components.Wings.Segment.Segment next (defined in SUAVE.Components.Lofted_Body.Segment)SUAVE.Components.Lofted_Body.Segment origin (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component percent_span_location (defined in SUAVE.Components.Wings.Segment.Segment)SUAVE.Components.Wings.Segment.Segment @@ -111,6 +124,8 @@ root_chord_percent (defined in SUAVE.Components.Wings.Segment.Segment)SUAVE.Components.Wings.Segment.Segment sweeps (defined in SUAVE.Components.Wings.Segment.Segment)SUAVE.Components.Wings.Segment.Segment tag (defined in SUAVE.Components.Wings.Segment.Segment)SUAVE.Components.Wings.Segment.Segment + taper (defined in SUAVE.Components.Wings.Segment.Segment)SUAVE.Components.Wings.Segment.Segment + thickness_to_chord (defined in SUAVE.Components.Wings.Segment.Segment)SUAVE.Components.Wings.Segment.Segment twist (defined in SUAVE.Components.Wings.Segment.Segment)SUAVE.Components.Wings.Segment.Segment
@@ -119,7 +134,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Segment_1_1Segment.html b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Segment_1_1Segment.html index 07e0d9de..b02e996f 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Segment_1_1Segment.html +++ b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Segment_1_1Segment.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Components.Wings.Segment.Segment Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -107,8 +114,8 @@ SUAVE.Components.Lofted_Body.Segment SUAVE.Components.Component.Component - -
+ + @@ -116,14 +123,6 @@ - - - - - - - -

Public Member Functions

 
def append_airfoil (self, airfoil)
 
def append_control_surface (self, control_surface)
 
- Public Member Functions inherited from SUAVE.Components.Lofted_Body.Segment
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
@@ -136,21 +135,48 @@ + + + + + + + + - - + + + + + + + + + + + + @@ -168,6 +194,15 @@ + + + + + +

Public Attributes

 twist
 
taper
 
 root_chord_percent
 
 dihedral_outboard
 
thickness_to_chord
 
 sweeps
 
chords
 
areas
 
 Airfoil
 
control_surfaces
 
generative_design_minimum
 
generative_design_max_per_vehicle
 
generative_design_special_parent
 
generative_design_characteristics
 
generative_design_char_min_bounds
 
generative_design_char_max_bounds
 
- Public Attributes inherited from SUAVE.Components.Lofted_Body.Segment
 tag
 origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 

Member Function Documentation

@@ -202,6 +237,8 @@

SUAVE.Components.Lofted_Body.Segment.

+ @@ -243,50 +280,6 @@

-

◆ append_control_surface()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Components.Wings.Segment.Segment.append_control_surface ( self,
 control_surface 
)
-
-
Adds an control_surface to the segment
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
 Properties Used:
 N/A
 
@@ -303,7 +296,7 @@

SUAVE + doxygen 1.8.15

diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Segment_1_1Segment.js b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Segment_1_1Segment.js index 87b5f782..30648fd1 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Segment_1_1Segment.js +++ b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Segment_1_1Segment.js @@ -2,13 +2,21 @@ var classSUAVE_1_1Components_1_1Wings_1_1Segment_1_1Segment = [ [ "__defaults__", "classSUAVE_1_1Components_1_1Wings_1_1Segment_1_1Segment.html#a61224a8134dae53d9b10a6db3a4af800", null ], [ "append_airfoil", "classSUAVE_1_1Components_1_1Wings_1_1Segment_1_1Segment.html#a47fc0861956a7eae28e13a4f5e1ee7c7", null ], - [ "append_control_surface", "classSUAVE_1_1Components_1_1Wings_1_1Segment_1_1Segment.html#aaab654b3bbb6547ca992644fc3dbd300", null ], [ "Airfoil", "classSUAVE_1_1Components_1_1Wings_1_1Segment_1_1Segment.html#afea77873575432d9f76c0216b53913b0", null ], - [ "control_surfaces", "classSUAVE_1_1Components_1_1Wings_1_1Segment_1_1Segment.html#a18d1010aa92045660148a35417f8b9bf", null ], + [ "areas", "classSUAVE_1_1Components_1_1Wings_1_1Segment_1_1Segment.html#a58c917c9cc37d7f2de79a05e1398a23d", null ], + [ "chords", "classSUAVE_1_1Components_1_1Wings_1_1Segment_1_1Segment.html#a8da90f02eb421dec5c2edcba02545053", null ], [ "dihedral_outboard", "classSUAVE_1_1Components_1_1Wings_1_1Segment_1_1Segment.html#a9f87970e346855bfdc2b7184e8a44dad", null ], + [ "generative_design_char_max_bounds", "classSUAVE_1_1Components_1_1Wings_1_1Segment_1_1Segment.html#a3384243281940903bbc4dae5893b6665", null ], + [ "generative_design_char_min_bounds", "classSUAVE_1_1Components_1_1Wings_1_1Segment_1_1Segment.html#a4ff7d31163654d471a261bb7793d1e40", null ], + [ "generative_design_characteristics", "classSUAVE_1_1Components_1_1Wings_1_1Segment_1_1Segment.html#a5f13500f6d303940711dd90a8a04dd4e", null ], + [ "generative_design_max_per_vehicle", "classSUAVE_1_1Components_1_1Wings_1_1Segment_1_1Segment.html#a86298341205e695e9253aaa30e899ccc", null ], + [ "generative_design_minimum", "classSUAVE_1_1Components_1_1Wings_1_1Segment_1_1Segment.html#a073a92f9d7b4827ce82b49574da2aa91", null ], + [ "generative_design_special_parent", "classSUAVE_1_1Components_1_1Wings_1_1Segment_1_1Segment.html#a946328b85e606eb6539450dc9473f705", null ], [ "percent_span_location", "classSUAVE_1_1Components_1_1Wings_1_1Segment_1_1Segment.html#a693876b634b417655e245b0d89e81651", null ], [ "root_chord_percent", "classSUAVE_1_1Components_1_1Wings_1_1Segment_1_1Segment.html#ada3a394de76d358909b23d1c3ad128e3", null ], [ "sweeps", "classSUAVE_1_1Components_1_1Wings_1_1Segment_1_1Segment.html#a9b3b815e75c41ec078bc0731f512aa63", null ], [ "tag", "classSUAVE_1_1Components_1_1Wings_1_1Segment_1_1Segment.html#ad9267b68b97363a777b56fac8d0712ee", null ], + [ "taper", "classSUAVE_1_1Components_1_1Wings_1_1Segment_1_1Segment.html#a182b3c789492877b842df35c01982c5e", null ], + [ "thickness_to_chord", "classSUAVE_1_1Components_1_1Wings_1_1Segment_1_1Segment.html#aecd440f8429c47d647d8b39140d49455", null ], [ "twist", "classSUAVE_1_1Components_1_1Wings_1_1Segment_1_1Segment.html#afd7bcd8236516d3e8eb7cd8e93dc90ee", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Segment_1_1SegmentContainer.html b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Segment_1_1SegmentContainer.html deleted file mode 100644 index 70f179b9..00000000 --- a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Segment_1_1SegmentContainer.html +++ /dev/null @@ -1,138 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Components.Wings.Segment.SegmentContainer Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
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SUAVE -  1.1.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Components.Wings.Segment.SegmentContainer Class Reference
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-Inheritance diagram for SUAVE.Components.Wings.Segment.SegmentContainer:
-
-
- - - -
-

Detailed Description

-
Container for wing segment
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-

The documentation for this class was generated from the following file:
    -
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Wings/Segment.py
  • -
-
-
- - - - diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Segment_1_1SegmentContainer.png b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Segment_1_1SegmentContainer.png deleted file mode 100644 index d1b5bf3d..00000000 Binary files a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Segment_1_1SegmentContainer.png and /dev/null differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Segment_1_1Segment__Container-members.html b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Segment_1_1Segment__Container-members.html new file mode 100644 index 00000000..04d47380 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Segment_1_1Segment__Container-members.html @@ -0,0 +1,120 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
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+ +
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+
SUAVE.Components.Wings.Segment.Segment_Container Member List
+
+
+ +

This is the complete list of members for SUAVE.Components.Wings.Segment.Segment_Container, including all inherited members.

+ + +
get_children(self)SUAVE.Components.Wings.Segment.Segment_Container
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Segment_1_1Segment__Container.html b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Segment_1_1Segment__Container.html new file mode 100644 index 00000000..c62cfe14 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Segment_1_1Segment__Container.html @@ -0,0 +1,187 @@ + + + + + + + +SUAVE: SUAVE.Components.Wings.Segment.Segment_Container Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
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+ + + +
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+ +
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+ +
+ +
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+ + +
+ +
+ +
+ +
+
SUAVE.Components.Wings.Segment.Segment_Container Class Reference
+
+
+
+Inheritance diagram for SUAVE.Components.Wings.Segment.Segment_Container:
+
+
+ +
+ + + + +

+Public Member Functions

def get_children (self)
 
+

Detailed Description

+
Container for wing segment
+
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+None
+
+Outputs:
+None
+
+Properties Used:
+N/A
+

Member Function Documentation

+ +

◆ get_children()

+ +
+
+ + + + + + + + +
def SUAVE.Components.Wings.Segment.Segment_Container.get_children ( self)
+
+
Returns the components that can go inside
+
+Assumptions:
+None
+    
+Source:
+N/A
+    
+Inputs:
+None
+    
+Outputs:
+None
+    
+Properties Used:
+N/A
+
+
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Wings/Segment.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Segment_1_1Segment__Container.js b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Segment_1_1Segment__Container.js new file mode 100644 index 00000000..00d20fc3 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Segment_1_1Segment__Container.js @@ -0,0 +1,4 @@ +var classSUAVE_1_1Components_1_1Wings_1_1Segment_1_1Segment__Container = +[ + [ "get_children", "classSUAVE_1_1Components_1_1Wings_1_1Segment_1_1Segment__Container.html#a36f10de9f1b090401d0295b4e13f86bf", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Segment_1_1Segment__Container.png b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Segment_1_1Segment__Container.png new file mode 100644 index 00000000..4459f1ae Binary files /dev/null and b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Segment_1_1Segment__Container.png differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Stabilator_1_1Stabilator-members.html b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Stabilator_1_1Stabilator-members.html new file mode 100644 index 00000000..c493864a --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Stabilator_1_1Stabilator-members.html @@ -0,0 +1,166 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
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+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
SUAVE.Components.Wings.Stabilator.Stabilator Member List
+
+
+ +

This is the complete list of members for SUAVE.Components.Wings.Stabilator.Stabilator, including all inherited members.

+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
__defaults__(self)SUAVE.Components.Wings.Stabilator.Stabilator
aerodynamic_center (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
Airfoil (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
append_airfoil(self, airfoil)SUAVE.Components.Wings.Wing.Wing
append_control_surface(self, control_surface)SUAVE.Components.Wings.Wing.Wing
append_fuel_tank(self, fuel_tank)SUAVE.Components.Wings.Wing.Wing
append_segment(self, segment)SUAVE.Components.Wings.Wing.Wing
areas (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
aspect_ratio (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
chords (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
control_surfaces (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
deflection (defined in SUAVE.Components.Wings.All_Moving_Surface.All_Moving_Surface)SUAVE.Components.Wings.All_Moving_Surface.All_Moving_Surface
dihedral (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
dynamic_pressure_ratio (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
exposed_root_chord_offset (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
Fuel_Tanks (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
generative_design_char_max_bounds (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
generative_design_char_min_bounds (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
generative_design_characteristics (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
generative_design_max_per_vehicle (defined in SUAVE.Components.Wings.Horizontal_Tail.Horizontal_Tail)SUAVE.Components.Wings.Horizontal_Tail.Horizontal_Tail
generative_design_minimum (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
high_lift (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
high_mach (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
hinge_fraction (defined in SUAVE.Components.Wings.All_Moving_Surface.All_Moving_Surface)SUAVE.Components.Wings.All_Moving_Surface.All_Moving_Surface
hinge_vector (defined in SUAVE.Components.Wings.All_Moving_Surface.All_Moving_Surface)SUAVE.Components.Wings.All_Moving_Surface.All_Moving_Surface
mass_properties (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
non_dimensional_origin (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
origin (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
Segments (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
sign_duplicate (defined in SUAVE.Components.Wings.Stabilator.Stabilator)SUAVE.Components.Wings.Stabilator.Stabilator
spans (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
sweeps (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
symbolic (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
symmetric (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
t_tail (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
tag (defined in SUAVE.Components.Wings.Stabilator.Stabilator)SUAVE.Components.Wings.Stabilator.Stabilator
taper (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
thickness_to_chord (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
total_length (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
transition_x_lower (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
transition_x_upper (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
twists (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
use_constant_hinge_fraction (defined in SUAVE.Components.Wings.All_Moving_Surface.All_Moving_Surface)SUAVE.Components.Wings.All_Moving_Surface.All_Moving_Surface
vertical (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
vortex_lift (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Stabilator_1_1Stabilator.html b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Stabilator_1_1Stabilator.html new file mode 100644 index 00000000..1320e577 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Stabilator_1_1Stabilator.html @@ -0,0 +1,390 @@ + + + + + + + +SUAVE: SUAVE.Components.Wings.Stabilator.Stabilator Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Components.Wings.Stabilator.Stabilator Class Reference
+
+
+
+Inheritance diagram for SUAVE.Components.Wings.Stabilator.Stabilator:
+
+
+ + +SUAVE.Components.Wings.Horizontal_Tail.Horizontal_Tail +SUAVE.Components.Wings.All_Moving_Surface.All_Moving_Surface +SUAVE.Components.Wings.Wing.Wing +SUAVE.Components.Lofted_Body.Lofted_Body +SUAVE.Components.Lofted_Body.Lofted_Body +SUAVE.Components.Physical_Component.Physical_Component +SUAVE.Components.Physical_Component.Physical_Component +SUAVE.Components.Component.Component +SUAVE.Components.Component.Component + +
+ + + + + + + + + + + + + +

+Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Wings.Wing.Wing
def append_segment (self, segment)
 
def append_airfoil (self, airfoil)
 
def append_control_surface (self, control_surface)
 
def append_fuel_tank (self, fuel_tank)
 
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Attributes

tag
 
sign_duplicate
 
- Public Attributes inherited from SUAVE.Components.Wings.Horizontal_Tail.Horizontal_Tail
tag
 
generative_design_max_per_vehicle
 
- Public Attributes inherited from SUAVE.Components.Wings.Wing.Wing
tag
 
mass_properties
 
origin
 
symmetric
 
vertical
 
t_tail
 
taper
 
dihedral
 
aspect_ratio
 
thickness_to_chord
 
aerodynamic_center
 
exposed_root_chord_offset
 
total_length
 
spans
 
areas
 
chords
 
sweeps
 
twists
 
high_lift
 
symbolic
 
high_mach
 
vortex_lift
 
transition_x_upper
 
transition_x_lower
 
dynamic_pressure_ratio
 
Airfoil
 
non_dimensional_origin
 
generative_design_minimum
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_char_min_bounds
 
generative_design_char_max_bounds
 
Segments
 
control_surfaces
 
Fuel_Tanks
 
- Public Attributes inherited from SUAVE.Components.Lofted_Body.Lofted_Body
tag
 
Segments
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 
- Public Attributes inherited from SUAVE.Components.Wings.All_Moving_Surface.All_Moving_Surface
tag
 
sign_duplicate
 
hinge_fraction
 
deflection
 
use_constant_hinge_fraction
 
hinge_vector
 
+

Detailed Description

+
This class is used to define stabilators in SUAVE. Note that it 
+inherits from both Horizontal_Tail and All_Moving_Surface
+
+    Assumptions:
+    None
+
+    Source:
+    N/A
+
+    Inputs:
+    None
+
+    Outputs:
+    None
+
+    Properties Used:
+    N/A

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Components.Wings.Stabilator.Stabilator.__defaults__ ( self)
+
+
This sets the default for stabilators in SUAVE.
+
+See All_Moving_Surface().__defaults__ and Wing().__defaults__ for 
+an explanation of attributes
+    
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+None
+
+Outputs:
+None
+
+Properties Used:
+N/A
+
+

Reimplemented from SUAVE.Components.Wings.All_Moving_Surface.All_Moving_Surface.

+ +
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Wings/Stabilator.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Stabilator_1_1Stabilator.js b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Stabilator_1_1Stabilator.js new file mode 100644 index 00000000..e8af8733 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Stabilator_1_1Stabilator.js @@ -0,0 +1,6 @@ +var classSUAVE_1_1Components_1_1Wings_1_1Stabilator_1_1Stabilator = +[ + [ "__defaults__", "classSUAVE_1_1Components_1_1Wings_1_1Stabilator_1_1Stabilator.html#a0122d3061c59cd1748857025837e7c07", null ], + [ "sign_duplicate", "classSUAVE_1_1Components_1_1Wings_1_1Stabilator_1_1Stabilator.html#a68b5c6568449beee450e5aaccdf87e27", null ], + [ "tag", "classSUAVE_1_1Components_1_1Wings_1_1Stabilator_1_1Stabilator.html#a6394903d4bee3041b13fd84e3d115a9d", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Stabilator_1_1Stabilator.png b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Stabilator_1_1Stabilator.png new file mode 100644 index 00000000..2760458d Binary files /dev/null and b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Stabilator_1_1Stabilator.png differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Vertical__Tail_1_1Vertical__Tail-members.html b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Vertical__Tail_1_1Vertical__Tail-members.html index 2b9fe146..ada43319 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Vertical__Tail_1_1Vertical__Tail-members.html +++ b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Vertical__Tail_1_1Vertical__Tail-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@
- +
@@ -73,7 +78,9 @@
@@ -103,34 +110,42 @@ Airfoil (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing append_airfoil(self, airfoil)SUAVE.Components.Wings.Wing.Wing append_control_surface(self, control_surface)SUAVE.Components.Wings.Wing.Wing - append_segment(self, segment)SUAVE.Components.Wings.Wing.Wing - areas (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing - aspect_ratio (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing - chords (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing - control_surfaces (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing - dihedral (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + append_fuel_tank(self, fuel_tank)SUAVE.Components.Wings.Wing.Wing + append_segment(self, segment)SUAVE.Components.Wings.Wing.Wing + areas (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + aspect_ratio (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + chords (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + control_surfaces (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + dihedral (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + dynamic_pressure_ratio (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing exposed_root_chord_offset (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing - flaps (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + Fuel_Tanks (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + generative_design_char_max_bounds (defined in SUAVE.Components.Wings.Vertical_Tail.Vertical_Tail)SUAVE.Components.Wings.Vertical_Tail.Vertical_Tail + generative_design_char_min_bounds (defined in SUAVE.Components.Wings.Vertical_Tail.Vertical_Tail)SUAVE.Components.Wings.Vertical_Tail.Vertical_Tail + generative_design_characteristics (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + generative_design_max_per_vehicle (defined in SUAVE.Components.Wings.Vertical_Tail.Vertical_Tail)SUAVE.Components.Wings.Vertical_Tail.Vertical_Tail + generative_design_minimum (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component high_lift (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing high_mach (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing - mass_properties (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing - origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component - position (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing - Sections (defined in SUAVE.Components.Lofted_Body.Lofted_Body)SUAVE.Components.Lofted_Body.Lofted_Body - Segments (defined in SUAVE.Components.Lofted_Body.Lofted_Body)SUAVE.Components.Lofted_Body.Lofted_Body - slats (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing - span_efficiency (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + make_x_z_reflection(self)SUAVE.Components.Wings.Vertical_Tail.Vertical_Tail + mass_properties (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + non_dimensional_origin (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + origin (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + Segments (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing spans (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing sweeps (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing - symmetric (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing - t_tail (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing - tag (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing - taper (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing - thickness_to_chord (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + symbolic (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + symmetric (defined in SUAVE.Components.Wings.Vertical_Tail.Vertical_Tail)SUAVE.Components.Wings.Vertical_Tail.Vertical_Tail + t_tail (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + tag (defined in SUAVE.Components.Wings.Vertical_Tail.Vertical_Tail)SUAVE.Components.Wings.Vertical_Tail.Vertical_Tail + taper (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + thickness_to_chord (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + total_length (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing transition_x_lower (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing transition_x_upper (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing twists (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing - vertical (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + vertical (defined in SUAVE.Components.Wings.Vertical_Tail.Vertical_Tail)SUAVE.Components.Wings.Vertical_Tail.Vertical_Tail vortex_lift (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
@@ -139,7 +154,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Vertical__Tail_1_1Vertical__Tail.html b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Vertical__Tail_1_1Vertical__Tail.html index 460ed436..2c818dee 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Vertical__Tail_1_1Vertical__Tail.html +++ b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Vertical__Tail_1_1Vertical__Tail.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Components.Wings.Vertical_Tail.Vertical_Tail Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -93,6 +100,7 @@
SUAVE.Components.Wings.Vertical_Tail.Vertical_Tail Class Reference
@@ -104,38 +112,50 @@
-SUAVE.Components.Wings.Wing.Wing -SUAVE.Components.Lofted_Body.Lofted_Body -SUAVE.Components.Physical_Component.Physical_Component -SUAVE.Components.Component.Component - -
+SUAVE.Components.Wings.Wing.Wing +SUAVE.Components.Lofted_Body.Lofted_Body +SUAVE.Components.Physical_Component.Physical_Component +SUAVE.Components.Component.Component +SUAVE.Components.Wings.Vertical_Tail_All_Moving.Vertical_Tail_All_Moving + +
+ + - - - - - - - - - - - + +

Public Member Functions

def __defaults__ (self)
 
def make_x_z_reflection (self)
 
- Public Member Functions inherited from SUAVE.Components.Wings.Wing.Wing
def __defaults__ (self)
 
def append_segment (self, segment)
 
def append_airfoil (self, airfoil)
 
def append_control_surface (self, control_surface)
 
- Public Member Functions inherited from SUAVE.Components.Lofted_Body.Lofted_Body
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
def append_fuel_tank (self, fuel_tank)
 
- + + + + + + + + + + + + + @@ -143,9 +163,9 @@ - - + + @@ -167,15 +187,15 @@ - - + + @@ -191,18 +211,12 @@ - - - - - - + + @@ -215,9 +229,39 @@ + + + + + + + + + + + + + + + + + + + + @@ -225,9 +269,6 @@ - - @@ -248,6 +289,15 @@ + + + + + +

-Additional Inherited Members

+Public Attributes

tag
 
vertical
 
symmetric
 
generative_design_max_per_vehicle
 
generative_design_char_min_bounds
 
generative_design_char_max_bounds
 
- Public Attributes inherited from SUAVE.Components.Wings.Wing.Wing
 tag
 mass_properties
 
position
 
origin
 
 symmetric
 
 thickness_to_chord
 
span_efficiency
 
 aerodynamic_center
 
 exposed_root_chord_offset
 
total_length
 
 spans
 
 twists
 
control_surfaces
 
flaps
 
slats
 
 high_lift
 
symbolic
 
 high_mach
 
 transition_x_lower
 
dynamic_pressure_ratio
 
 Airfoil
 
non_dimensional_origin
 
generative_design_minimum
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_char_min_bounds
 
generative_design_char_max_bounds
 
Segments
 
control_surfaces
 
Fuel_Tanks
 
- Public Attributes inherited from SUAVE.Components.Lofted_Body.Lofted_Body
 tag
 Segments
 
Sections
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
 tag
 origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 

Detailed Description

This class is used to define vertical tails SUAVE
@@ -299,6 +349,56 @@ 

SUAVE.Components.Wings.Wing.Wing.

+ +

Reimplemented in SUAVE.Components.Wings.Vertical_Tail_All_Moving.Vertical_Tail_All_Moving.

+ +

+ + +

◆ make_x_z_reflection()

+ +
+
+ + + + + + + + +
def SUAVE.Components.Wings.Vertical_Tail.Vertical_Tail.make_x_z_reflection ( self)
+
+
This returns a Vertical_Tail class or subclass object that is the reflection
+of this object over the x-z plane. This is useful since if Vertical_Tail's symmetric 
+attribute is True, the symmetric wing gets reflected over the x-y plane.
+
+WARNING: this uses deepcopy to achieve its purpose. If this copies too many unwanted 
+attributes, it is recommended that the user should write their own code, taking 
+after the form of this function.
+
+It is also recommended that the user call this function after they set control surface
+or all moving surface deflections. This way the deflection is also properly reflected 
+to the other side
+    
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+None
+
+Outputs:
+None
+
+Properties Used:
+N/A
+
+

Reimplemented in SUAVE.Components.Wings.Vertical_Tail_All_Moving.Vertical_Tail_All_Moving.

+

The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Vertical__Tail_1_1Vertical__Tail.js b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Vertical__Tail_1_1Vertical__Tail.js index 37eeafea..6961d3bf 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Vertical__Tail_1_1Vertical__Tail.js +++ b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Vertical__Tail_1_1Vertical__Tail.js @@ -1,4 +1,11 @@ var classSUAVE_1_1Components_1_1Wings_1_1Vertical__Tail_1_1Vertical__Tail = [ - [ "__defaults__", "classSUAVE_1_1Components_1_1Wings_1_1Vertical__Tail_1_1Vertical__Tail.html#a140e95184807806f674ada3a7f7d783a", null ] + [ "__defaults__", "classSUAVE_1_1Components_1_1Wings_1_1Vertical__Tail_1_1Vertical__Tail.html#a140e95184807806f674ada3a7f7d783a", null ], + [ "make_x_z_reflection", "classSUAVE_1_1Components_1_1Wings_1_1Vertical__Tail_1_1Vertical__Tail.html#a979d5913a2fe9409c9cecaf5974aae92", null ], + [ "generative_design_char_max_bounds", "classSUAVE_1_1Components_1_1Wings_1_1Vertical__Tail_1_1Vertical__Tail.html#a56c4d3abe1bfd26666719457a65ce03d", null ], + [ "generative_design_char_min_bounds", "classSUAVE_1_1Components_1_1Wings_1_1Vertical__Tail_1_1Vertical__Tail.html#a85e12410050b7aea67dea950eae92c79", null ], + [ "generative_design_max_per_vehicle", "classSUAVE_1_1Components_1_1Wings_1_1Vertical__Tail_1_1Vertical__Tail.html#a00a6c7ea87d6c65c68d807be5404f7ac", null ], + [ "symmetric", "classSUAVE_1_1Components_1_1Wings_1_1Vertical__Tail_1_1Vertical__Tail.html#a2728b3a1713eeeaf8d7e48950e9f1db9", null ], + [ "tag", "classSUAVE_1_1Components_1_1Wings_1_1Vertical__Tail_1_1Vertical__Tail.html#a543a87c24d439910a48097786ea9591f", null ], + [ "vertical", "classSUAVE_1_1Components_1_1Wings_1_1Vertical__Tail_1_1Vertical__Tail.html#af6d89bd61fd4d3b01fdea92cdc20dc00", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Vertical__Tail_1_1Vertical__Tail.png b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Vertical__Tail_1_1Vertical__Tail.png index a3937a4e..904d93d8 100644 Binary files a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Vertical__Tail_1_1Vertical__Tail.png and b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Vertical__Tail_1_1Vertical__Tail.png differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Vertical__Tail__All__Moving_1_1Vertical__Tail__All__Moving-members.html b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Vertical__Tail__All__Moving_1_1Vertical__Tail__All__Moving-members.html new file mode 100644 index 00000000..ccfd6f94 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Vertical__Tail__All__Moving_1_1Vertical__Tail__All__Moving-members.html @@ -0,0 +1,167 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
SUAVE.Components.Wings.Vertical_Tail_All_Moving.Vertical_Tail_All_Moving Member List
+
+
+ +

This is the complete list of members for SUAVE.Components.Wings.Vertical_Tail_All_Moving.Vertical_Tail_All_Moving, including all inherited members.

+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
__defaults__(self)SUAVE.Components.Wings.Vertical_Tail_All_Moving.Vertical_Tail_All_Moving
aerodynamic_center (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
Airfoil (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
append_airfoil(self, airfoil)SUAVE.Components.Wings.Wing.Wing
append_control_surface(self, control_surface)SUAVE.Components.Wings.Wing.Wing
append_fuel_tank(self, fuel_tank)SUAVE.Components.Wings.Wing.Wing
append_segment(self, segment)SUAVE.Components.Wings.Wing.Wing
areas (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
aspect_ratio (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
chords (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
control_surfaces (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
deflection (defined in SUAVE.Components.Wings.All_Moving_Surface.All_Moving_Surface)SUAVE.Components.Wings.All_Moving_Surface.All_Moving_Surface
dihedral (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
dynamic_pressure_ratio (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
exposed_root_chord_offset (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
Fuel_Tanks (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
generative_design_char_max_bounds (defined in SUAVE.Components.Wings.Vertical_Tail.Vertical_Tail)SUAVE.Components.Wings.Vertical_Tail.Vertical_Tail
generative_design_char_min_bounds (defined in SUAVE.Components.Wings.Vertical_Tail.Vertical_Tail)SUAVE.Components.Wings.Vertical_Tail.Vertical_Tail
generative_design_characteristics (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
generative_design_max_per_vehicle (defined in SUAVE.Components.Wings.Vertical_Tail.Vertical_Tail)SUAVE.Components.Wings.Vertical_Tail.Vertical_Tail
generative_design_minimum (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component
high_lift (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
high_mach (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
hinge_fraction (defined in SUAVE.Components.Wings.All_Moving_Surface.All_Moving_Surface)SUAVE.Components.Wings.All_Moving_Surface.All_Moving_Surface
hinge_vector (defined in SUAVE.Components.Wings.All_Moving_Surface.All_Moving_Surface)SUAVE.Components.Wings.All_Moving_Surface.All_Moving_Surface
make_x_z_reflection(self)SUAVE.Components.Wings.Vertical_Tail_All_Moving.Vertical_Tail_All_Moving
mass_properties (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
non_dimensional_origin (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
origin (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
Segments (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
sign_duplicate (defined in SUAVE.Components.Wings.Vertical_Tail_All_Moving.Vertical_Tail_All_Moving)SUAVE.Components.Wings.Vertical_Tail_All_Moving.Vertical_Tail_All_Moving
spans (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
sweeps (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
symbolic (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
symmetric (defined in SUAVE.Components.Wings.Vertical_Tail.Vertical_Tail)SUAVE.Components.Wings.Vertical_Tail.Vertical_Tail
t_tail (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
tag (defined in SUAVE.Components.Wings.Vertical_Tail_All_Moving.Vertical_Tail_All_Moving)SUAVE.Components.Wings.Vertical_Tail_All_Moving.Vertical_Tail_All_Moving
taper (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
thickness_to_chord (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
total_length (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
transition_x_lower (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
transition_x_upper (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
twists (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
use_constant_hinge_fraction (defined in SUAVE.Components.Wings.All_Moving_Surface.All_Moving_Surface)SUAVE.Components.Wings.All_Moving_Surface.All_Moving_Surface
vertical (defined in SUAVE.Components.Wings.Vertical_Tail.Vertical_Tail)SUAVE.Components.Wings.Vertical_Tail.Vertical_Tail
vortex_lift (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Vertical__Tail__All__Moving_1_1Vertical__Tail__All__Moving.html b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Vertical__Tail__All__Moving_1_1Vertical__Tail__All__Moving.html new file mode 100644 index 00000000..319e29c7 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Vertical__Tail__All__Moving_1_1Vertical__Tail__All__Moving.html @@ -0,0 +1,450 @@ + + + + + + + +SUAVE: SUAVE.Components.Wings.Vertical_Tail_All_Moving.Vertical_Tail_All_Moving Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Components.Wings.Vertical_Tail_All_Moving.Vertical_Tail_All_Moving Class Reference
+
+
+
+Inheritance diagram for SUAVE.Components.Wings.Vertical_Tail_All_Moving.Vertical_Tail_All_Moving:
+
+
+ + +SUAVE.Components.Wings.Vertical_Tail.Vertical_Tail +SUAVE.Components.Wings.All_Moving_Surface.All_Moving_Surface +SUAVE.Components.Wings.Wing.Wing +SUAVE.Components.Lofted_Body.Lofted_Body +SUAVE.Components.Lofted_Body.Lofted_Body +SUAVE.Components.Physical_Component.Physical_Component +SUAVE.Components.Physical_Component.Physical_Component +SUAVE.Components.Component.Component +SUAVE.Components.Component.Component + +
+ + + + + + + + + + + + + + + +

+Public Member Functions

def __defaults__ (self)
 
def make_x_z_reflection (self)
 
- Public Member Functions inherited from SUAVE.Components.Wings.Wing.Wing
def append_segment (self, segment)
 
def append_airfoil (self, airfoil)
 
def append_control_surface (self, control_surface)
 
def append_fuel_tank (self, fuel_tank)
 
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Attributes

tag
 
sign_duplicate
 
- Public Attributes inherited from SUAVE.Components.Wings.Vertical_Tail.Vertical_Tail
tag
 
vertical
 
symmetric
 
generative_design_max_per_vehicle
 
generative_design_char_min_bounds
 
generative_design_char_max_bounds
 
- Public Attributes inherited from SUAVE.Components.Wings.Wing.Wing
tag
 
mass_properties
 
origin
 
symmetric
 
vertical
 
t_tail
 
taper
 
dihedral
 
aspect_ratio
 
thickness_to_chord
 
aerodynamic_center
 
exposed_root_chord_offset
 
total_length
 
spans
 
areas
 
chords
 
sweeps
 
twists
 
high_lift
 
symbolic
 
high_mach
 
vortex_lift
 
transition_x_upper
 
transition_x_lower
 
dynamic_pressure_ratio
 
Airfoil
 
non_dimensional_origin
 
generative_design_minimum
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_char_min_bounds
 
generative_design_char_max_bounds
 
Segments
 
control_surfaces
 
Fuel_Tanks
 
- Public Attributes inherited from SUAVE.Components.Lofted_Body.Lofted_Body
tag
 
Segments
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
tag
 
mass_properties
 
origin
 
symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
tag
 
origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 
- Public Attributes inherited from SUAVE.Components.Wings.All_Moving_Surface.All_Moving_Surface
tag
 
sign_duplicate
 
hinge_fraction
 
deflection
 
use_constant_hinge_fraction
 
hinge_vector
 
+

Detailed Description

+
This class is used to define all-moving vertical tails in SUAVE. Note that it 
+inherits from both Horizontal_Tail and All_Moving_Surface
+
+    Assumptions:
+    None
+
+    Source:
+    N/A
+
+    Inputs:
+    None
+
+    Outputs:
+    None
+
+    Properties Used:
+    N/A

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Components.Wings.Vertical_Tail_All_Moving.Vertical_Tail_All_Moving.__defaults__ ( self)
+
+
This sets the default for all moving-vertical tails in SUAVE.
+
+See All_Moving_Surface().__defaults__ and Wing().__defaults__ for an explanation 
+of attributes
+    
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+None
+
+Outputs:
+None
+
+Properties Used:
+N/A
+
+

Reimplemented from SUAVE.Components.Wings.All_Moving_Surface.All_Moving_Surface.

+ +
+
+ +

◆ make_x_z_reflection()

+ +
+
+ + + + + + + + +
def SUAVE.Components.Wings.Vertical_Tail_All_Moving.Vertical_Tail_All_Moving.make_x_z_reflection ( self)
+
+
This returns a Vertical_Tail class or subclass object that is the reflection
+of this object over the x-z plane. This is useful since if Vertical_Tail's symmetric 
+attribute is True, the symmetric wing gets reflected over the x-y plane.
+
+This function uses deepcopy to achieve its purpose. If this copies too many unwanted 
+attributes, it is recommended that the user should write their own code, taking 
+after the form of this function.
+
+It is also recommended that the user call this function after they set control surface
+or all moving surface deflections. This way the deflection is also properly reflected 
+to the other side
+    
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+None
+
+Outputs:
+None
+
+Properties Used:
+N/A
+
+

Reimplemented from SUAVE.Components.Wings.Vertical_Tail.Vertical_Tail.

+ +
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Wings/Vertical_Tail_All_Moving.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Vertical__Tail__All__Moving_1_1Vertical__Tail__All__Moving.js b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Vertical__Tail__All__Moving_1_1Vertical__Tail__All__Moving.js new file mode 100644 index 00000000..987bf55b --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Vertical__Tail__All__Moving_1_1Vertical__Tail__All__Moving.js @@ -0,0 +1,7 @@ +var classSUAVE_1_1Components_1_1Wings_1_1Vertical__Tail__All__Moving_1_1Vertical__Tail__All__Moving = +[ + [ "__defaults__", "classSUAVE_1_1Components_1_1Wings_1_1Vertical__Tail__All__Moving_1_1Vertical__Tail__All__Moving.html#a8d78f0bdb7134d85b46ad81e996d2586", null ], + [ "make_x_z_reflection", "classSUAVE_1_1Components_1_1Wings_1_1Vertical__Tail__All__Moving_1_1Vertical__Tail__All__Moving.html#a9b99dae4a164f4935bca8f62bf7f11bb", null ], + [ "sign_duplicate", "classSUAVE_1_1Components_1_1Wings_1_1Vertical__Tail__All__Moving_1_1Vertical__Tail__All__Moving.html#a7d88c7dd8524a367a5ff74b60f47aac8", null ], + [ "tag", "classSUAVE_1_1Components_1_1Wings_1_1Vertical__Tail__All__Moving_1_1Vertical__Tail__All__Moving.html#a8d726769dc3a3b89d6cc6c42ff9b23e2", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Vertical__Tail__All__Moving_1_1Vertical__Tail__All__Moving.png b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Vertical__Tail__All__Moving_1_1Vertical__Tail__All__Moving.png new file mode 100644 index 00000000..cede9ca9 Binary files /dev/null and b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Vertical__Tail__All__Moving_1_1Vertical__Tail__All__Moving.png differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Container-members.html b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Container-members.html new file mode 100644 index 00000000..a4bd0cf5 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Container-members.html @@ -0,0 +1,123 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
SUAVE.Components.Wings.Wing.Container Member List
+
+ +
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Container.html b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Container.html new file mode 100644 index 00000000..b42fadae --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Container.html @@ -0,0 +1,186 @@ + + + + + + + +SUAVE: SUAVE.Components.Wings.Wing.Container Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Components.Wings.Wing.Container Class Reference
+
+
+
+Inheritance diagram for SUAVE.Components.Wings.Wing.Container:
+
+
+ + +SUAVE.Components.Physical_Component.Container +SUAVE.Components.Component.Container + +
+ + + + + + + + + +

+Public Member Functions

def get_children (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Container
def sum_mass (self)
 
def total_moment (self)
 
+ + + + +

+Additional Inherited Members

- Static Public Attributes inherited from SUAVE.Components.Component.Container
Container
 
+

Member Function Documentation

+ +

◆ get_children()

+ +
+
+ + + + + + + + +
def SUAVE.Components.Wings.Wing.Container.get_children ( self)
+
+
Returns the components that can go inside
+
+Assumptions:
+None
+    
+Source:
+N/A
+    
+Inputs:
+None
+    
+Outputs:
+None
+    
+Properties Used:
+N/A
+
+
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Wings/Wing.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Container.js b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Container.js new file mode 100644 index 00000000..983cccb9 --- /dev/null +++ b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Container.js @@ -0,0 +1,4 @@ +var classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Container = +[ + [ "get_children", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Container.html#a62f1a93e6661277589c105c6f231e13a", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Container.png b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Container.png new file mode 100644 index 00000000..ca4a2600 Binary files /dev/null and b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Container.png differ diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing-members.html b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing-members.html index fd53bbe4..22ff1b46 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing-members.html +++ b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -103,35 +110,42 @@ Airfoil (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing append_airfoil(self, airfoil)SUAVE.Components.Wings.Wing.Wing append_control_surface(self, control_surface)SUAVE.Components.Wings.Wing.Wing - append_segment(self, segment)SUAVE.Components.Wings.Wing.Wing - areas (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing - aspect_ratio (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing - chords (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing - control_surfaces (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing - dihedral (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + append_fuel_tank(self, fuel_tank)SUAVE.Components.Wings.Wing.Wing + append_segment(self, segment)SUAVE.Components.Wings.Wing.Wing + areas (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + aspect_ratio (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + chords (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + control_surfaces (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + dihedral (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + dynamic_pressure_ratio (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing exposed_root_chord_offset (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing - flaps (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + Fuel_Tanks (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + generative_design_char_max_bounds (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + generative_design_char_min_bounds (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + generative_design_characteristics (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + generative_design_max_per_vehicle (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + generative_design_minimum (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + generative_design_special_parent (defined in SUAVE.Components.Component.Component)SUAVE.Components.Component.Component high_lift (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing high_mach (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing mass_properties (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing - origin (defined in SUAVE.Components.Physical_Component.Physical_Component)SUAVE.Components.Physical_Component.Physical_Component - position (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing - Sections (defined in SUAVE.Components.Lofted_Body.Lofted_Body)SUAVE.Components.Lofted_Body.Lofted_Body - Segments (defined in SUAVE.Components.Lofted_Body.Lofted_Body)SUAVE.Components.Lofted_Body.Lofted_Body - slats (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing - span_efficiency (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing - spans (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing - sweeps (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + non_dimensional_origin (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + origin (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + Segments (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + spans (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + sweeps (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + symbolic (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing symmetric (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing t_tail (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing tag (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing taper (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing thickness_to_chord (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing - transition_x_lower (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing - transition_x_upper (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing - twists (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing - vertical (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing - vortex_lift (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + total_length (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + transition_x_lower (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + transition_x_upper (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + twists (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + vertical (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing + vortex_lift (defined in SUAVE.Components.Wings.Wing.Wing)SUAVE.Components.Wings.Wing.Wing
@@ -139,7 +153,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html index 88ccd0e1..eb40c060 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html +++ b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Components.Wings.Wing.Wing Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -105,14 +112,16 @@
-SUAVE.Components.Lofted_Body.Lofted_Body -SUAVE.Components.Physical_Component.Physical_Component -SUAVE.Components.Component.Component -SUAVE.Components.Wings.Horizontal_Tail.Horizontal_Tail -SUAVE.Components.Wings.Main_Wing.Main_Wing -SUAVE.Components.Wings.Vertical_Tail.Vertical_Tail - -
+SUAVE.Components.Lofted_Body.Lofted_Body +SUAVE.Components.Physical_Component.Physical_Component +SUAVE.Components.Component.Component +SUAVE.Components.Wings.Horizontal_Tail.Horizontal_Tail +SUAVE.Components.Wings.Main_Wing.Main_Wing +SUAVE.Components.Wings.Vertical_Tail.Vertical_Tail +SUAVE.Components.Wings.Stabilator.Stabilator +SUAVE.Components.Wings.Vertical_Tail_All_Moving.Vertical_Tail_All_Moving + + @@ -124,15 +133,8 @@ - - - - - - - - - + +

Public Member Functions

 
def append_control_surface (self, control_surface)
 
- Public Member Functions inherited from SUAVE.Components.Lofted_Body.Lofted_Body
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Physical_Component
def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Component.Component
def __defaults__ (self)
 
def append_fuel_tank (self, fuel_tank)
 
@@ -142,9 +144,9 @@ - - + + @@ -166,15 +168,15 @@ - - + + @@ -190,18 +192,12 @@ - - - - - - + + @@ -214,9 +210,39 @@ + + + + + + + + + + + + + + + + + + + + @@ -224,9 +250,6 @@ - - @@ -247,6 +270,15 @@ + + + + + +

Public Attributes

 mass_properties
 
position
 
origin
 
 symmetric
 
 thickness_to_chord
 
span_efficiency
 
 aerodynamic_center
 
 exposed_root_chord_offset
 
total_length
 
 spans
 
 twists
 
control_surfaces
 
flaps
 
slats
 
 high_lift
 
symbolic
 
 high_mach
 
 transition_x_lower
 
dynamic_pressure_ratio
 
 Airfoil
 
non_dimensional_origin
 
generative_design_minimum
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_char_min_bounds
 
generative_design_char_max_bounds
 
Segments
 
control_surfaces
 
Fuel_Tanks
 
- Public Attributes inherited from SUAVE.Components.Lofted_Body.Lofted_Body
 tag
 Segments
 
Sections
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
 tag
 origin
 
generative_design_max_per_vehicle
 
generative_design_characteristics
 
generative_design_special_parent
 

Detailed Description

@@ -383,6 +419,50 @@

+

◆ append_fuel_tank()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Components.Wings.Wing.Wing.append_fuel_tank ( self,
 fuel_tank 
)
+
+
Adds a fuel tank to the wing 
+    
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+None
+
+Outputs:
+None
+
 Properties Used:
 N/A
 
@@ -443,7 +523,7 @@

SUAVE + doxygen 1.8.15

diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.js b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.js index a8fa3a70..55810428 100644 --- a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.js +++ b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.js @@ -3,6 +3,7 @@ var classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing = [ "__defaults__", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html#ab53e649ccbbc13673b6aacc081dc59dc", null ], [ "append_airfoil", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html#aae7e3c4e26c570a1df378ae24e537713", null ], [ "append_control_surface", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html#aadd013ca1ee42a79fdd1c5c0a1b92506", null ], + [ "append_fuel_tank", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html#a56e06c9901a94f23c3c5d37233955c0d", null ], [ "append_segment", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html#a6af83046c14d3a0ef4d4d21fbd4be086", null ], [ "aerodynamic_center", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html#a571c1dc8eb5821ad559d01dbb4574076", null ], [ "Airfoil", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html#a4b25ac0ada709189458bd5cbf5098421", null ], @@ -11,21 +12,29 @@ var classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing = [ "chords", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html#a7eef52d56996afb3d5745eb608ee138b", null ], [ "control_surfaces", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html#aafa1c4446e778b2adf84925c96c45df0", null ], [ "dihedral", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html#a122fc4a8b8195bc82e8988eae413638c", null ], + [ "dynamic_pressure_ratio", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html#a6b31c9e3eff8f4442233b0247106e81b", null ], [ "exposed_root_chord_offset", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html#aa65cca0ac4c258e0fd48d851468ec25e", null ], - [ "flaps", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html#ade2666acf39d8ab9d0f0452380432722", null ], + [ "Fuel_Tanks", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html#a03cbb89c854a4a99d491b20987536d6f", null ], + [ "generative_design_char_max_bounds", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html#ae6a1135f4396196cd327f0f0108aeffb", null ], + [ "generative_design_char_min_bounds", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html#a1e1f7da9500136dd3f769a14c95a3d34", null ], + [ "generative_design_characteristics", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html#a1c1cd6fc0833e70a1ae9b32add0f13ce", null ], + [ "generative_design_max_per_vehicle", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html#a3fc7c0283b2f46f91e96b8f8c357dd38", null ], + [ "generative_design_minimum", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html#a3f5704be0f973113fb0c202561a97580", null ], [ "high_lift", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html#a54b2922197121a8e144c864052addbc1", null ], [ "high_mach", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html#a39814d7d0a9045ecc4b52a90602d2eb5", null ], [ "mass_properties", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html#a734345ca36c535557e19cf72afb2dec3", null ], - [ "position", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html#a9dc4902e77f1210d8ff622c9cc663d3a", null ], - [ "slats", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html#a62971f29066998a4cecd60c373a5ce47", null ], - [ "span_efficiency", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html#ab9486856c8849049ee532753f2f28d34", null ], + [ "non_dimensional_origin", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html#a1ad2d8a78c2b713c42f35d27c02a1c70", null ], + [ "origin", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html#a7b06c7368545903984412a454de68042", null ], + [ "Segments", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html#a9d72647f10ef4f7864b26cc314789bbb", null ], [ "spans", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html#a9c8581500143469644736a6a346fb574", null ], [ "sweeps", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html#a9c95d8e5232adf728ae14f240d20e37a", null ], + [ "symbolic", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html#a5a85fc2af0705f26604cbfd2ef9d0b9f", null ], [ "symmetric", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html#a868aa0c0bd1e95b99eebe899c0e68c27", null ], [ "t_tail", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html#ac02d70ef5a4c6491d94ef4ceb6bdd8a6", null ], [ "tag", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html#a82a4410a681cbee9d280a7742d3f8f21", null ], [ "taper", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html#ab95ccc5960b40df6a1c1cf23106be252", null ], [ "thickness_to_chord", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html#a13a5cf4a4553b887e2686dc253f54f80", null ], + [ "total_length", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html#ab80adca4badcb71250e64d2581d1b28c", null ], [ "transition_x_lower", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html#a7fae8d960f7f53c9c158a8b5eeacc4f0", null ], [ "transition_x_upper", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html#ab9ac0e252a2cd2a169acf061c555059d", null ], [ "twists", "classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.html#a0e4556318f06695584f96db46c226211", null ], diff --git a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.png b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.png index 252c646b..c27ae9d7 100644 Binary files a/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.png and b/doxygen/classSUAVE_1_1Components_1_1Wings_1_1Wing_1_1Wing.png differ diff --git a/doxygen/classSUAVE_1_1Core_1_1ContainerOrdered_1_1ContainerOrdered-members.html b/doxygen/classSUAVE_1_1Core_1_1ContainerOrdered_1_1ContainerOrdered-members.html index 599c13a9..de48dd3b 100644 --- a/doxygen/classSUAVE_1_1Core_1_1ContainerOrdered_1_1ContainerOrdered-members.html +++ b/doxygen/classSUAVE_1_1Core_1_1ContainerOrdered_1_1ContainerOrdered-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@
- +
@@ -73,7 +78,9 @@
@@ -102,34 +109,35 @@ __delattr__(self, key)SUAVE.Core.DataOrdered.DataOrdered __eq__(self, other)SUAVE.Core.DataOrdered.DataOrdered __getitem__(self, k)SUAVE.Core.DataOrdered.DataOrdered - __init__(self, args, kwarg)SUAVE.Core.ContainerOrdered.ContainerOrdered + __init__(self, *args, **kwarg)SUAVE.Core.ContainerOrdered.ContainerOrdered __iter__(self)SUAVE.Core.DataOrdered.DataOrdered - __iter__(self)SUAVE.Core.DataOrdered.DataOrdered + __iter_basic__(self)SUAVE.Core.DataOrdered.DataOrdered __len__(self)SUAVE.Core.DataOrdered.DataOrdered - __new__(cls, args, kwarg)SUAVE.Core.DataOrdered.DataOrdered + __new__(cls, *args, **kwarg)SUAVE.Core.DataOrdered.DataOrdered __reduce__(self)SUAVE.Core.DataOrdered.DataOrdered - __repr__(self)SUAVE.Core.DataOrdered.DataOrdered - __setattr__(self, key, value)SUAVE.Core.DataOrdered.DataOrdered - __setitem__(self, k, v)SUAVE.Core.DataOrdered.DataOrdered - __str__(self, indent='')SUAVE.Core.DataOrdered.DataOrdered - append(self, val)SUAVE.Core.ContainerOrdered.ContainerOrdered - SUAVE::Core::DataOrdered::DataOrdered.append(self, value, key=None)SUAVE.Core.DataOrdered.DataOrdered - clear(self)SUAVE.Core.DataOrdered.DataOrdered - dataname(self)SUAVE.Core.DataOrdered.DataOrdered - deep_get(self, keys)SUAVE.Core.DataOrdered.DataOrdered - deep_set(self, keys, val)SUAVE.Core.DataOrdered.DataOrdered - extend(self, vals)SUAVE.Core.ContainerOrdered.ContainerOrdered - get(self, k, d=None)SUAVE.Core.DataOrdered.DataOrdered - get_bases(self)SUAVE.Core.DataOrdered.DataOrdered + __setattr__(self, key, value)SUAVE.Core.DataOrdered.DataOrdered + __setitem__(self, k, v)SUAVE.Core.DataOrdered.DataOrdered + __str__(self, indent='')SUAVE.Core.DataOrdered.DataOrdered + append(self, val)SUAVE.Core.ContainerOrdered.ContainerOrdered + SUAVE::Core::DataOrdered::DataOrdered.append(self, value, key=None)SUAVE.Core.DataOrdered.DataOrdered + clear(self)SUAVE.Core.DataOrdered.DataOrdered + dataname(self)SUAVE.Core.DataOrdered.DataOrdered + deep_get(self, keys)SUAVE.Core.DataOrdered.DataOrdered + deep_set(self, keys, val)SUAVE.Core.DataOrdered.DataOrdered + extend(self, vals)SUAVE.Core.ContainerOrdered.ContainerOrdered + get(self, k, d=None)SUAVE.Core.DataOrdered.DataOrdered + get_bases(self)SUAVE.Core.DataOrdered.DataOrdered + get_children(self)SUAVE.Core.ContainerOrdered.ContainerOrdered has_key(self, k)SUAVE.Core.DataOrdered.DataOrdered - items(self)SUAVE.Core.DataOrdered.DataOrdered - iteritems(self)SUAVE.Core.DataOrdered.DataOrdered - iterkeys(self)SUAVE.Core.DataOrdered.DataOrdered - itervalues(self)SUAVE.Core.DataOrdered.DataOrdered - keys(self)SUAVE.Core.DataOrdered.DataOrdered - typestring(self)SUAVE.Core.DataOrdered.DataOrdered - update(self, other)SUAVE.Core.DataOrdered.DataOrdered - values(self)SUAVE.Core.DataOrdered.DataOrdered + hasattr(self, k) (defined in SUAVE.Core.DataOrdered.DataOrdered)SUAVE.Core.DataOrdered.DataOrdered + items(self)SUAVE.Core.DataOrdered.DataOrdered + iteritems(self)SUAVE.Core.DataOrdered.DataOrdered + iterkeys(self)SUAVE.Core.DataOrdered.DataOrdered + itervalues(self)SUAVE.Core.DataOrdered.DataOrdered + keys(self)SUAVE.Core.DataOrdered.DataOrdered + typestring(self)SUAVE.Core.DataOrdered.DataOrdered + update(self, other)SUAVE.Core.DataOrdered.DataOrdered + values(self)SUAVE.Core.DataOrdered.DataOrdered
@@ -137,7 +145,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Core_1_1ContainerOrdered_1_1ContainerOrdered.html b/doxygen/classSUAVE_1_1Core_1_1ContainerOrdered_1_1ContainerOrdered.html index 368efc67..4f866212 100644 --- a/doxygen/classSUAVE_1_1Core_1_1ContainerOrdered_1_1ContainerOrdered.html +++ b/doxygen/classSUAVE_1_1Core_1_1ContainerOrdered_1_1ContainerOrdered.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Core.ContainerOrdered.ContainerOrdered Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -105,36 +112,35 @@ SUAVE.Core.DataOrdered.DataOrdered - -
+ + - - + + + + - - - - - - + + + + - - @@ -153,8 +159,8 @@ - - + + @@ -189,8 +195,8 @@ Source: N/A

Constructor & Destructor Documentation

- -

◆ __init__()

+ +

◆ __init__()

@@ -204,13 +210,13 @@

- + - + @@ -236,6 +242,8 @@

SUAVE.Core.DataOrdered.DataOrdered.

+

Member Function Documentation

@@ -270,6 +278,8 @@

SUAVE.Core.DataOrdered.DataOrdered.

+ @@ -358,6 +368,40 @@

+

◆ get_children()

+ +
+
+

Public Member Functions

def __defaults__ (self)
 
def __init__ (self, args, kwarg)
 
def __init__ (self, *args, **kwarg)
 
def append (self, val)
 
def extend (self, vals)
 
def get_children (self)
 
- Public Member Functions inherited from SUAVE.Core.DataOrdered.DataOrdered
def append (self, value, key=None)
 
def __defaults__ (self)
 
def __getitem__ (self, k)
 
def __new__ (cls, args, kwarg)
 
def __init__ (self, args, kwarg)
 
def __new__ (cls, *args, **kwarg)
 
+def hasattr (self, k)
 
def __iter__ (self)
 
def __str__ (self, indent='')
 
def __repr__ (self)
 
def get_bases (self)
 
def typestring (self)
 
def __len__ (self)
 
def __iter__ (self)
 
def __iter_basic__ (self)
 
def __reduce__ (self)
 
def __setattr__ (self, key, value)
  args,
 **  kwarg 
+ + + + + + + +
def SUAVE.Core.ContainerOrdered.ContainerOrdered.get_children ( self)
+
+
Returns the components that can go inside
+
+Assumptions:
+None
+    
+Source:
+N/A
+    
+Inputs:
+None
+    
+Outputs:
+None
+    
+Properties Used:
+N/A
+
+
+
The documentation for this class was generated from the following file:
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Core/ContainerOrdered.py
@@ -369,7 +413,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Core_1_1ContainerOrdered_1_1ContainerOrdered.js b/doxygen/classSUAVE_1_1Core_1_1ContainerOrdered_1_1ContainerOrdered.js index d97c28bc..4e290dba 100644 --- a/doxygen/classSUAVE_1_1Core_1_1ContainerOrdered_1_1ContainerOrdered.js +++ b/doxygen/classSUAVE_1_1Core_1_1ContainerOrdered_1_1ContainerOrdered.js @@ -1,7 +1,8 @@ var classSUAVE_1_1Core_1_1ContainerOrdered_1_1ContainerOrdered = [ - [ "__init__", "classSUAVE_1_1Core_1_1ContainerOrdered_1_1ContainerOrdered.html#aed0a64ed7ae49700963351f337d3efa3", null ], + [ "__init__", "classSUAVE_1_1Core_1_1ContainerOrdered_1_1ContainerOrdered.html#a838faf2047087526c9e341e4b87244a5", null ], [ "__defaults__", "classSUAVE_1_1Core_1_1ContainerOrdered_1_1ContainerOrdered.html#ad4208e02ac70e846604b536c4f654c66", null ], [ "append", "classSUAVE_1_1Core_1_1ContainerOrdered_1_1ContainerOrdered.html#a7011a4af617cd2242a9dfb98e36e2a24", null ], - [ "extend", "classSUAVE_1_1Core_1_1ContainerOrdered_1_1ContainerOrdered.html#a9c2614dcd055d49735be64e500c3baaa", null ] + [ "extend", "classSUAVE_1_1Core_1_1ContainerOrdered_1_1ContainerOrdered.html#a9c2614dcd055d49735be64e500c3baaa", null ], + [ "get_children", "classSUAVE_1_1Core_1_1ContainerOrdered_1_1ContainerOrdered.html#a5a04a9f18eb08825061e74ca2932e78b", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Core_1_1Container_1_1Container-members.html b/doxygen/classSUAVE_1_1Core_1_1Container_1_1Container-members.html index 4fad6173..7bfafb95 100644 --- a/doxygen/classSUAVE_1_1Core_1_1Container_1_1Container-members.html +++ b/doxygen/classSUAVE_1_1Core_1_1Container_1_1Container-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
diff --git a/doxygen/classSUAVE_1_1Core_1_1Container_1_1Container.html b/doxygen/classSUAVE_1_1Core_1_1Container_1_1Container.html index 0515646c..7bd723d1 100644 --- a/doxygen/classSUAVE_1_1Core_1_1Container_1_1Container.html +++ b/doxygen/classSUAVE_1_1Core_1_1Container_1_1Container.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Core.Container.Container Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -105,19 +112,21 @@ SUAVE.Core.Data.Data - -
+ + - - + + + + @@ -125,18 +134,14 @@ - - - - + + - - @@ -145,6 +150,8 @@ + + @@ -169,8 +176,8 @@ Source: N/A

Constructor & Destructor Documentation

- -

◆ __init__()

+ +

◆ __init__()

@@ -184,13 +191,13 @@

- + - + @@ -217,6 +224,8 @@

SUAVE.Core.Data.Data.

+

Member Function Documentation

@@ -252,6 +261,8 @@

SUAVE.Core.Data.Data.

+ @@ -280,6 +291,8 @@

Appends the value to the containers
+    This overrides the Data class append by allowing for duplicate named components
+    The following components will get new names.
 
     Assumptions:
     None
@@ -342,6 +355,40 @@ 

+

◆ get_children()

+ +
+
+

Public Member Functions

def __defaults__ (self)
 
def __init__ (self, args, kwarg)
 
def __init__ (self, *args, **kwarg)
 
def append (self, val)
 
def extend (self, vals)
 
def get_children (self)
 
- Public Member Functions inherited from SUAVE.Core.Data.Data
def __getattribute__ (self, k)
 
 
def __delattr__ (self, k)
 
def __defaults__ (self)
 
def __new__ (cls, args, kwarg)
 
def __new__ (cls, *args, **kwarg)
 
def typestring (self)
 
def dataname (self)
 
def __str__ (self, indent='')
 
def __init__ (self, args, kwarg)
 
def __iter__ (self)
 
def itervalues (self)
 
def update (self, other)
 
def append_or_update (self, other)
 
def get_bases (self)
 
def append (self, value, key=None)
  args,
 **  kwarg 
+ + + + + + + +
def SUAVE.Core.Container.Container.get_children ( self)
+
+
Returns the components that can go inside
+
+Assumptions:
+None
+    
+Source:
+N/A
+    
+Inputs:
+None
+    
+Outputs:
+None
+    
+Properties Used:
+N/A
+
+
+
The documentation for this class was generated from the following file:
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Core/Container.py
@@ -353,7 +400,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Core_1_1Container_1_1Container.js b/doxygen/classSUAVE_1_1Core_1_1Container_1_1Container.js index d65466be..e72c9553 100644 --- a/doxygen/classSUAVE_1_1Core_1_1Container_1_1Container.js +++ b/doxygen/classSUAVE_1_1Core_1_1Container_1_1Container.js @@ -1,7 +1,8 @@ var classSUAVE_1_1Core_1_1Container_1_1Container = [ - [ "__init__", "classSUAVE_1_1Core_1_1Container_1_1Container.html#a7cbac1bbad1dd3279655f10d8315ffb2", null ], + [ "__init__", "classSUAVE_1_1Core_1_1Container_1_1Container.html#ade60f359bbe42e43d4688674fca339a4", null ], [ "__defaults__", "classSUAVE_1_1Core_1_1Container_1_1Container.html#a566ffa56d67a534512525e5212065568", null ], [ "append", "classSUAVE_1_1Core_1_1Container_1_1Container.html#a0f2652c760244b0128b854b9dce9a774", null ], - [ "extend", "classSUAVE_1_1Core_1_1Container_1_1Container.html#a6e9b7dbfa8ffa88162d698d32318b22d", null ] + [ "extend", "classSUAVE_1_1Core_1_1Container_1_1Container.html#a6e9b7dbfa8ffa88162d698d32318b22d", null ], + [ "get_children", "classSUAVE_1_1Core_1_1Container_1_1Container.html#ac8cc25ab031c7085e6b1e961ff562fcd", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Core_1_1DataOrdered_1_1DataOrdered-members.html b/doxygen/classSUAVE_1_1Core_1_1DataOrdered_1_1DataOrdered-members.html index 4c1d58f2..8254fb9b 100644 --- a/doxygen/classSUAVE_1_1Core_1_1DataOrdered_1_1DataOrdered-members.html +++ b/doxygen/classSUAVE_1_1Core_1_1DataOrdered_1_1DataOrdered-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -102,24 +109,24 @@ __delattr__(self, key)SUAVE.Core.DataOrdered.DataOrdered __eq__(self, other)SUAVE.Core.DataOrdered.DataOrdered __getitem__(self, k)SUAVE.Core.DataOrdered.DataOrdered - __init__(self, args, kwarg)SUAVE.Core.DataOrdered.DataOrdered + __init__(self, *args, **kwarg)SUAVE.Core.DataOrdered.DataOrdered __iter__(self)SUAVE.Core.DataOrdered.DataOrdered - __iter__(self)SUAVE.Core.DataOrdered.DataOrdered + __iter_basic__(self)SUAVE.Core.DataOrdered.DataOrdered __len__(self)SUAVE.Core.DataOrdered.DataOrdered - __new__(cls, args, kwarg)SUAVE.Core.DataOrdered.DataOrdered + __new__(cls, *args, **kwarg)SUAVE.Core.DataOrdered.DataOrdered __reduce__(self)SUAVE.Core.DataOrdered.DataOrdered - __repr__(self)SUAVE.Core.DataOrdered.DataOrdered - __setattr__(self, key, value)SUAVE.Core.DataOrdered.DataOrdered - __setitem__(self, k, v)SUAVE.Core.DataOrdered.DataOrdered - __str__(self, indent='')SUAVE.Core.DataOrdered.DataOrdered - append(self, value, key=None)SUAVE.Core.DataOrdered.DataOrdered - clear(self)SUAVE.Core.DataOrdered.DataOrdered - dataname(self)SUAVE.Core.DataOrdered.DataOrdered - deep_get(self, keys)SUAVE.Core.DataOrdered.DataOrdered - deep_set(self, keys, val)SUAVE.Core.DataOrdered.DataOrdered - get(self, k, d=None)SUAVE.Core.DataOrdered.DataOrdered - get_bases(self)SUAVE.Core.DataOrdered.DataOrdered - has_key(self, k)SUAVE.Core.DataOrdered.DataOrdered + __setattr__(self, key, value)SUAVE.Core.DataOrdered.DataOrdered + __setitem__(self, k, v)SUAVE.Core.DataOrdered.DataOrdered + __str__(self, indent='')SUAVE.Core.DataOrdered.DataOrdered + append(self, value, key=None)SUAVE.Core.DataOrdered.DataOrdered + clear(self)SUAVE.Core.DataOrdered.DataOrdered + dataname(self)SUAVE.Core.DataOrdered.DataOrdered + deep_get(self, keys)SUAVE.Core.DataOrdered.DataOrdered + deep_set(self, keys, val)SUAVE.Core.DataOrdered.DataOrdered + get(self, k, d=None)SUAVE.Core.DataOrdered.DataOrdered + get_bases(self)SUAVE.Core.DataOrdered.DataOrdered + has_key(self, k)SUAVE.Core.DataOrdered.DataOrdered + hasattr(self, k) (defined in SUAVE.Core.DataOrdered.DataOrdered)SUAVE.Core.DataOrdered.DataOrdered items(self)SUAVE.Core.DataOrdered.DataOrdered iteritems(self)SUAVE.Core.DataOrdered.DataOrdered iterkeys(self)SUAVE.Core.DataOrdered.DataOrdered @@ -135,7 +142,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Core_1_1DataOrdered_1_1DataOrdered.html b/doxygen/classSUAVE_1_1Core_1_1DataOrdered_1_1DataOrdered.html index 9ba5dba4..09ea7d3e 100644 --- a/doxygen/classSUAVE_1_1Core_1_1DataOrdered_1_1DataOrdered.html +++ b/doxygen/classSUAVE_1_1Core_1_1DataOrdered_1_1DataOrdered.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Core.DataOrdered.DataOrdered Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -107,8 +114,8 @@ SUAVE.Core.ContainerOrdered.ContainerOrdered SUAVE.Input_Output.D3JS.Tree_Element.Tree_Element SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Container - -
+ + @@ -118,16 +125,17 @@ - - - - + + + + + + - - @@ -146,8 +154,8 @@ - - + + @@ -175,8 +183,7 @@

Public Member Functions

 
def __getitem__ (self, k)
 
def __new__ (cls, args, kwarg)
 
def __init__ (self, args, kwarg)
 
def __new__ (cls, *args, **kwarg)
 
+def hasattr (self, k)
 
def __init__ (self, *args, **kwarg)
 
def __iter__ (self)
 
def __str__ (self, indent='')
 
def __repr__ (self)
 
def get_bases (self)
 
def typestring (self)
 
def __len__ (self)
 
def __iter__ (self)
 
def __iter_basic__ (self)
 
def __reduce__ (self)
 
def __setattr__ (self, key, value)

Detailed Description

An extension of the Python dict which allows for both tag and '.' usage.
-    This is an unordered dictionary. So indexing it will not produce deterministic results.
-    This has less overhead than ordering. If ordering is needed use DataOrdered().
+    This is an ordered dictionary. So indexing it will produce deterministic results.
    
     Assumptions:
     N/A
@@ -184,8 +191,8 @@
     Source:
     N/A
 

Constructor & Destructor Documentation

- -

◆ __init__()

+ +

◆ __init__()

Member Function Documentation

@@ -267,6 +276,8 @@

SUAVE.Core.ContainerOrdered.ContainerOrdered.

+ @@ -402,7 +413,7 @@

-

◆ __iter__() [1/2]

+

◆ __iter__()

@@ -435,14 +446,14 @@

-

◆ __iter__() [2/2]

+ +

◆ __iter_basic__()

- + @@ -503,8 +514,8 @@

-

◆ __new__()

+ +

◆ __new__()

@@ -518,13 +529,13 @@

- + - + @@ -568,41 +579,7 @@

-
Reduction function used for pickling data
-    
-    Assumptions:
-    N/A
-    
-    Source:
-    N/A
-    
-    Inputs:
-    N/A
-    
-    Outputs:
-    N/A
-    
-    Properties Used:
-    N/A    
-
- - -
-

◆ __repr__()

- -
-
-
def SUAVE.Core.DataOrdered.DataOrdered.__iter__ def SUAVE.Core.DataOrdered.DataOrdered.__iter_basic__ (   self)  args,
 **  kwarg 
- - - - - - - -
def SUAVE.Core.DataOrdered.DataOrdered.__repr__ ( self)
-
-
This function is used for printing the dataname of the class
+
Reduction function used for making configs
     
     Assumptions:
     N/A
@@ -661,8 +638,8 @@ 

SUAVE + doxygen 1.8.15

diff --git a/doxygen/classSUAVE_1_1Core_1_1DataOrdered_1_1DataOrdered.js b/doxygen/classSUAVE_1_1Core_1_1DataOrdered_1_1DataOrdered.js index 06c1a82b..dd67f28d 100644 --- a/doxygen/classSUAVE_1_1Core_1_1DataOrdered_1_1DataOrdered.js +++ b/doxygen/classSUAVE_1_1Core_1_1DataOrdered_1_1DataOrdered.js @@ -1,16 +1,15 @@ var classSUAVE_1_1Core_1_1DataOrdered_1_1DataOrdered = [ - [ "__init__", "classSUAVE_1_1Core_1_1DataOrdered_1_1DataOrdered.html#a32224efd77bc24aea74d33999e4481f2", null ], + [ "__init__", "classSUAVE_1_1Core_1_1DataOrdered_1_1DataOrdered.html#a8e20af0ef213f277078958966e6fa7c5", null ], [ "__defaults__", "classSUAVE_1_1Core_1_1DataOrdered_1_1DataOrdered.html#a45c6bab8cd0a7b4aa27464d642cd7a5e", null ], [ "__delattr__", "classSUAVE_1_1Core_1_1DataOrdered_1_1DataOrdered.html#a44eb78bf6c80590d5cb5fc726c7f3184", null ], [ "__eq__", "classSUAVE_1_1Core_1_1DataOrdered_1_1DataOrdered.html#a645e8940eb0f28f92e629b125d79e0e1", null ], [ "__getitem__", "classSUAVE_1_1Core_1_1DataOrdered_1_1DataOrdered.html#a2a4d54c5646822649f356d80ed8d5001", null ], [ "__iter__", "classSUAVE_1_1Core_1_1DataOrdered_1_1DataOrdered.html#a727a22d1550136cdd217dc06981483db", null ], - [ "__iter__", "classSUAVE_1_1Core_1_1DataOrdered_1_1DataOrdered.html#a727a22d1550136cdd217dc06981483db", null ], + [ "__iter_basic__", "classSUAVE_1_1Core_1_1DataOrdered_1_1DataOrdered.html#aa500118acb942ad788ee2694f764104e", null ], [ "__len__", "classSUAVE_1_1Core_1_1DataOrdered_1_1DataOrdered.html#a1474cad96213dedce62249375071e51c", null ], - [ "__new__", "classSUAVE_1_1Core_1_1DataOrdered_1_1DataOrdered.html#ae7f8ca82a6526fdd42b49a4d4cd5bc0e", null ], + [ "__new__", "classSUAVE_1_1Core_1_1DataOrdered_1_1DataOrdered.html#add46625ec81f96d6b591547ea41b034a", null ], [ "__reduce__", "classSUAVE_1_1Core_1_1DataOrdered_1_1DataOrdered.html#ad384e66a99054e3a8f12c83b6a84c93d", null ], - [ "__repr__", "classSUAVE_1_1Core_1_1DataOrdered_1_1DataOrdered.html#a14e6ece7703001986b937d76716150c6", null ], [ "__setattr__", "classSUAVE_1_1Core_1_1DataOrdered_1_1DataOrdered.html#afc623fdd952face9c05101a11e71baed", null ], [ "__setitem__", "classSUAVE_1_1Core_1_1DataOrdered_1_1DataOrdered.html#ad4449f7906047b8638173be32929176d", null ], [ "__str__", "classSUAVE_1_1Core_1_1DataOrdered_1_1DataOrdered.html#abce8790556fa9730b7fdbd99f85a6416", null ], @@ -22,6 +21,7 @@ var classSUAVE_1_1Core_1_1DataOrdered_1_1DataOrdered = [ "get", "classSUAVE_1_1Core_1_1DataOrdered_1_1DataOrdered.html#a0fa21939a6607e52c6ec64f0df530da6", null ], [ "get_bases", "classSUAVE_1_1Core_1_1DataOrdered_1_1DataOrdered.html#a70121d322ad7d8f87ed8a493d9a91531", null ], [ "has_key", "classSUAVE_1_1Core_1_1DataOrdered_1_1DataOrdered.html#a0b2be2982aab545624276df6126050a0", null ], + [ "hasattr", "classSUAVE_1_1Core_1_1DataOrdered_1_1DataOrdered.html#a66994af42b97fb5d3c01bf1b301ddce2", null ], [ "items", "classSUAVE_1_1Core_1_1DataOrdered_1_1DataOrdered.html#a636e98cfed893d934ebfa3802beedfb7", null ], [ "iteritems", "classSUAVE_1_1Core_1_1DataOrdered_1_1DataOrdered.html#aa217f7f5308b213b95df7ee5d5cfeda1", null ], [ "iterkeys", "classSUAVE_1_1Core_1_1DataOrdered_1_1DataOrdered.html#a2b50d5ad6676e71674d02afbbdf08bed", null ], diff --git a/doxygen/classSUAVE_1_1Core_1_1DataOrdered_1_1Property-members.html b/doxygen/classSUAVE_1_1Core_1_1DataOrdered_1_1Property-members.html index 292f89a3..91001cb6 100644 --- a/doxygen/classSUAVE_1_1Core_1_1DataOrdered_1_1Property-members.html +++ b/doxygen/classSUAVE_1_1Core_1_1DataOrdered_1_1Property-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@
- +

@@ -73,7 +78,9 @@
@@ -109,7 +116,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Core_1_1DataOrdered_1_1Property.html b/doxygen/classSUAVE_1_1Core_1_1DataOrdered_1_1Property.html index f2e99074..3174467f 100644 --- a/doxygen/classSUAVE_1_1Core_1_1DataOrdered_1_1Property.html +++ b/doxygen/classSUAVE_1_1Core_1_1DataOrdered_1_1Property.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Core.DataOrdered.Property Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -102,9 +109,7 @@ Inheritance diagram for SUAVE.Core.DataOrdered.Property:
- - - +
@@ -57,9 +60,11 @@

@@ -328,7 +333,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Core_1_1Data_1_1Data-members.html b/doxygen/classSUAVE_1_1Core_1_1Data_1_1Data-members.html index b9b68d34..a0ebf8f0 100644 --- a/doxygen/classSUAVE_1_1Core_1_1Data_1_1Data-members.html +++ b/doxygen/classSUAVE_1_1Core_1_1Data_1_1Data-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -101,23 +108,24 @@ __defaults__(self)SUAVE.Core.Data.Data __delattr__(self, k)SUAVE.Core.Data.Data __getattribute__(self, k)SUAVE.Core.Data.Data - __init__(self, args, kwarg)SUAVE.Core.Data.Data + __init__(self, *args, **kwarg)SUAVE.Core.Data.Data __iter__(self)SUAVE.Core.Data.Data - __new__(cls, args, kwarg)SUAVE.Core.Data.Data + __new__(cls, *args, **kwarg)SUAVE.Core.Data.Data __setattr__(self, k, v)SUAVE.Core.Data.Data __str__(self, indent='')SUAVE.Core.Data.Data append(self, value, key=None)SUAVE.Core.Data.Data - dataname(self)SUAVE.Core.Data.Data - deep_get(self, keys)SUAVE.Core.Data.Data - deep_set(self, keys, val)SUAVE.Core.Data.Data - do_recursive(self, method, other=None, default=None)SUAVE.Core.Data.Data - get_bases(self)SUAVE.Core.Data.Data - itervalues(self)SUAVE.Core.Data.Data - pack_array(self, output='vector')SUAVE.Core.Data.Data - typestring(self)SUAVE.Core.Data.Data - unpack_array(self, M)SUAVE.Core.Data.Data - update(self, other)SUAVE.Core.Data.Data - values(self)SUAVE.Core.Data.Data + append_or_update(self, other)SUAVE.Core.Data.Data + dataname(self)SUAVE.Core.Data.Data + deep_get(self, keys)SUAVE.Core.Data.Data + deep_set(self, keys, val)SUAVE.Core.Data.Data + do_recursive(self, method, other=None, default=None)SUAVE.Core.Data.Data + get_bases(self)SUAVE.Core.Data.Data + itervalues(self)SUAVE.Core.Data.Data + pack_array(self, output='vector')SUAVE.Core.Data.Data + typestring(self)SUAVE.Core.Data.Data + unpack_array(self, M)SUAVE.Core.Data.Data + update(self, other)SUAVE.Core.Data.Data + values(self)SUAVE.Core.Data.Data
@@ -125,7 +133,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Core_1_1Data_1_1Data.html b/doxygen/classSUAVE_1_1Core_1_1Data_1_1Data.html index e2b4233f..547828ec 100644 --- a/doxygen/classSUAVE_1_1Core_1_1Data_1_1Data.html +++ b/doxygen/classSUAVE_1_1Core_1_1Data_1_1Data.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Core.Data.Data Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -111,21 +118,21 @@ SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Run_Case SUAVE.Methods.Aerodynamics.AVL.Data.Configuration.Configuration SUAVE.Methods.Aerodynamics.AVL.Data.Inputs.Inputs -SUAVE.Methods.Aerodynamics.AVL.Data.Settings.AVL_Discretization_Settings -SUAVE.Methods.Aerodynamics.AVL.Data.Settings.Settings -SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface -SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Section -SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing -SUAVE.Optimization.Nexus.Nexus -SUAVE.Optimization.Package_Setups.TRMM.Trust_Region.Trust_Region -SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization -SUAVE.Optimization.Surrogate_Optimization.Surrogate_Optimization -SUAVE.Sizing.Sizing_Loop.Sizing_Loop +SUAVE.Methods.Aerodynamics.AVL.Data.Settings.Settings +SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface +SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface_Data +SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface_Results +SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Section +SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing +SUAVE.Optimization.Nexus.Nexus +SUAVE.Optimization.Package_Setups.TRMM.Trust_Region.Trust_Region +SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization +SUAVE.Optimization.Surrogate_Optimization.Surrogate_Optimization SUAVE.Surrogate.Surrogate_Problem.Surrogate_Problem SUAVE.Vehicle.Costs SUAVE.Vehicle.Vehicle - -
+ + @@ -137,16 +144,16 @@ - - + + - - + + @@ -155,6 +162,8 @@ + + @@ -181,8 +190,8 @@ Source: N/A

Constructor & Destructor Documentation

- -

◆ __init__()

+ +

◆ __init__()

@@ -196,13 +205,13 @@

- + - + @@ -229,6 +238,8 @@

SUAVE.Vehicle.Vehicle, and SUAVE.Core.Container.Container.

+

Member Function Documentation

@@ -264,6 +275,8 @@

SUAVE.Vehicle.Costs, SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface_Results, SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface_Data, SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface, SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Section, SUAVE.Optimization.Nexus.Nexus, SUAVE.Methods.Aerodynamics.AVL.Data.Body.Body, SUAVE.Core.Container.Container, SUAVE.Methods.Aerodynamics.AVL.Data.Aircraft.Aircraft, SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Run_Case, SUAVE.Methods.Aerodynamics.AVL.Data.Configuration.Configuration, SUAVE.Methods.Aerodynamics.AVL.Data.Settings.Settings, SUAVE.Methods.Aerodynamics.AVL.Data.Inputs.Inputs, SUAVE.Vehicle.Vehicle, SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization, SUAVE.Optimization.Surrogate_Optimization.Surrogate_Optimization, SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing, SUAVE.Core.Diffed_Data.Diffed_Data, SUAVE.Components.Configs.Config.Config, SUAVE.Optimization.Package_Setups.TRMM.Trust_Region.Trust_Region, and SUAVE.Surrogate.Surrogate_Problem.Surrogate_Problem.

+ @@ -387,8 +400,8 @@

-

◆ __new__()

+ +

◆ __new__()

@@ -402,13 +415,13 @@

- + - + @@ -530,6 +543,8 @@

SUAVE.Core.Diffed_Data.Diffed_Data.

+ @@ -583,6 +598,50 @@

+

◆ append_or_update()

+ +
+
+

Public Member Functions

 
def __defaults__ (self)
 
def __new__ (cls, args, kwarg)
 
def __new__ (cls, *args, **kwarg)
 
def typestring (self)
 
def dataname (self)
 
def __str__ (self, indent='')
 
def __init__ (self, args, kwarg)
 
def __init__ (self, *args, **kwarg)
 
def __iter__ (self)
 
def itervalues (self)
 
def update (self, other)
 
def append_or_update (self, other)
 
def get_bases (self)
 
def append (self, value, key=None)
  args,
 **  kwarg 
  args,
 **  kwarg 
+ + + + + + + + + + + + + + + + + +
def SUAVE.Core.Data.Data.append_or_update ( self,
 other 
)
+
+
Appends an array or updates the internal values of a dictionary with given data
+    
+    Assumptions:
+    N/A
+    
+    Source:
+    N/A
+    
+    Inputs:
+    other
+    
+    Outputs:
+    N/A
+    
+    Properties Used:
+    N/A    
+
+
+

◆ dataname()

@@ -1052,7 +1111,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Core_1_1Data_1_1Data.js b/doxygen/classSUAVE_1_1Core_1_1Data_1_1Data.js index fea501c5..b8c2ddb0 100644 --- a/doxygen/classSUAVE_1_1Core_1_1Data_1_1Data.js +++ b/doxygen/classSUAVE_1_1Core_1_1Data_1_1Data.js @@ -1,14 +1,15 @@ var classSUAVE_1_1Core_1_1Data_1_1Data = [ - [ "__init__", "classSUAVE_1_1Core_1_1Data_1_1Data.html#a9662296ec537f32756a3db527d76f0d8", null ], + [ "__init__", "classSUAVE_1_1Core_1_1Data_1_1Data.html#a53cdb6dff3faeb47d13b68f989012733", null ], [ "__defaults__", "classSUAVE_1_1Core_1_1Data_1_1Data.html#aaf592cb5828e2e77556cb96137be6509", null ], [ "__delattr__", "classSUAVE_1_1Core_1_1Data_1_1Data.html#a2540d3d9f85dbedb84b4a677d559a6b3", null ], [ "__getattribute__", "classSUAVE_1_1Core_1_1Data_1_1Data.html#a3a9e65571555260186c6ae54cfeeea3c", null ], [ "__iter__", "classSUAVE_1_1Core_1_1Data_1_1Data.html#a98f17bb9cd886ccc1110c3c18d1c12d3", null ], - [ "__new__", "classSUAVE_1_1Core_1_1Data_1_1Data.html#a348c73ed2549fa7ffbe432e03bbffcd8", null ], + [ "__new__", "classSUAVE_1_1Core_1_1Data_1_1Data.html#a5bf781781988c1d31bd4c2deca7fdb08", null ], [ "__setattr__", "classSUAVE_1_1Core_1_1Data_1_1Data.html#aaceda3bf72e5beb15e59bf079edba2ce", null ], [ "__str__", "classSUAVE_1_1Core_1_1Data_1_1Data.html#a7847accf45dc18262cb7ceca42f74156", null ], [ "append", "classSUAVE_1_1Core_1_1Data_1_1Data.html#a69c46e0c3a6b4e0edc62596ab0af232b", null ], + [ "append_or_update", "classSUAVE_1_1Core_1_1Data_1_1Data.html#ad78beab7014e25a1b0d11b094a8df22b", null ], [ "dataname", "classSUAVE_1_1Core_1_1Data_1_1Data.html#ad25649de315ac95f3059ee0cad6294c6", null ], [ "deep_get", "classSUAVE_1_1Core_1_1Data_1_1Data.html#a3bbf5c11c2462b89b0a3df6dcaacf501", null ], [ "deep_set", "classSUAVE_1_1Core_1_1Data_1_1Data.html#a84ba0de5ac002c9fd4fc2953f5d452d4", null ], diff --git a/doxygen/classSUAVE_1_1Core_1_1Data_1_1Data.png b/doxygen/classSUAVE_1_1Core_1_1Data_1_1Data.png index fd4826df..22749f12 100644 Binary files a/doxygen/classSUAVE_1_1Core_1_1Data_1_1Data.png and b/doxygen/classSUAVE_1_1Core_1_1Data_1_1Data.png differ diff --git a/doxygen/classSUAVE_1_1Core_1_1Diffed__Data_1_1Container-members.html b/doxygen/classSUAVE_1_1Core_1_1Diffed__Data_1_1Container-members.html index 08a8e60b..e802bc62 100644 --- a/doxygen/classSUAVE_1_1Core_1_1Diffed__Data_1_1Container-members.html +++ b/doxygen/classSUAVE_1_1Core_1_1Diffed__Data_1_1Container-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -109,7 +116,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Core_1_1Diffed__Data_1_1Container.html b/doxygen/classSUAVE_1_1Core_1_1Diffed__Data_1_1Container.html index a2760154..c41eb23f 100644 --- a/doxygen/classSUAVE_1_1Core_1_1Diffed__Data_1_1Container.html +++ b/doxygen/classSUAVE_1_1Core_1_1Diffed__Data_1_1Container.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Core.Diffed_Data.Container Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -102,9 +109,7 @@ Inheritance diagram for SUAVE.Core.Diffed_Data.Container:
- - - +
@@ -57,9 +60,11 @@

@@ -284,7 +289,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Core_1_1Diffed__Data_1_1Diffed__Data-members.html b/doxygen/classSUAVE_1_1Core_1_1Diffed__Data_1_1Diffed__Data-members.html index 4f85ac30..01d586f0 100644 --- a/doxygen/classSUAVE_1_1Core_1_1Diffed__Data_1_1Diffed__Data-members.html +++ b/doxygen/classSUAVE_1_1Core_1_1Diffed__Data_1_1Diffed__Data-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -102,27 +109,28 @@ __delattr__(self, k)SUAVE.Core.Data.Data __getattribute__(self, k)SUAVE.Core.Data.Data __init__(self, base=None)SUAVE.Core.Diffed_Data.Diffed_Data - SUAVE::Core::Data::Data.__init__(self, args, kwarg)SUAVE.Core.Data.Data + SUAVE::Core::Data::Data.__init__(self, *args, **kwarg)SUAVE.Core.Data.Data __iter__(self)SUAVE.Core.Data.Data - __new__(cls, args, kwarg)SUAVE.Core.Data.Data + __new__(cls, *args, **kwarg)SUAVE.Core.Data.Data __setattr__(self, k, v)SUAVE.Core.Data.Data __str__(self, indent='')SUAVE.Core.Diffed_Data.Diffed_Data append(self, value, key=None)SUAVE.Core.Data.Data - dataname(self)SUAVE.Core.Data.Data - deep_get(self, keys)SUAVE.Core.Data.Data - deep_set(self, keys, val)SUAVE.Core.Data.Data - do_recursive(self, method, other=None, default=None)SUAVE.Core.Data.Data - finalize(self)SUAVE.Core.Diffed_Data.Diffed_Data - get_bases(self)SUAVE.Core.Data.Data - itervalues(self)SUAVE.Core.Data.Data - pack_array(self, output='vector')SUAVE.Core.Data.Data - pull_base(self)SUAVE.Core.Diffed_Data.Diffed_Data - store_diff(self)SUAVE.Core.Diffed_Data.Diffed_Data - tag (defined in SUAVE.Core.Diffed_Data.Diffed_Data)SUAVE.Core.Diffed_Data.Diffed_Data - typestring(self)SUAVE.Core.Data.Data - unpack_array(self, M)SUAVE.Core.Data.Data - update(self, other)SUAVE.Core.Data.Data - values(self)SUAVE.Core.Data.Data + append_or_update(self, other)SUAVE.Core.Data.Data + dataname(self)SUAVE.Core.Data.Data + deep_get(self, keys)SUAVE.Core.Data.Data + deep_set(self, keys, val)SUAVE.Core.Data.Data + do_recursive(self, method, other=None, default=None)SUAVE.Core.Data.Data + finalize(self)SUAVE.Core.Diffed_Data.Diffed_Data + get_bases(self)SUAVE.Core.Data.Data + itervalues(self)SUAVE.Core.Data.Data + pack_array(self, output='vector')SUAVE.Core.Data.Data + pull_base(self)SUAVE.Core.Diffed_Data.Diffed_Data + store_diff(self)SUAVE.Core.Diffed_Data.Diffed_Data + tag (defined in SUAVE.Core.Diffed_Data.Diffed_Data)SUAVE.Core.Diffed_Data.Diffed_Data + typestring(self)SUAVE.Core.Data.Data + unpack_array(self, M)SUAVE.Core.Data.Data + update(self, other)SUAVE.Core.Data.Data + values(self)SUAVE.Core.Data.Data
@@ -130,7 +138,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Core_1_1Diffed__Data_1_1Diffed__Data.html b/doxygen/classSUAVE_1_1Core_1_1Diffed__Data_1_1Diffed__Data.html index 2ba9a319..9c339773 100644 --- a/doxygen/classSUAVE_1_1Core_1_1Diffed__Data_1_1Diffed__Data.html +++ b/doxygen/classSUAVE_1_1Core_1_1Diffed__Data_1_1Diffed__Data.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Core.Diffed_Data.Diffed_Data Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -106,8 +113,8 @@ SUAVE.Core.Data.Data - -
+ + @@ -130,18 +137,14 @@ - - - - + + - - - - + + @@ -150,6 +153,8 @@ + + @@ -258,6 +263,8 @@

SUAVE.Core.Data.Data.

+ @@ -302,6 +309,8 @@

SUAVE.Core.Data.Data.

+ @@ -417,7 +426,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Core_1_1redirect_1_1folder-members.html b/doxygen/classSUAVE_1_1Core_1_1redirect_1_1folder-members.html index 9e4fb6c3..8c98e572 100644 --- a/doxygen/classSUAVE_1_1Core_1_1redirect_1_1folder-members.html +++ b/doxygen/classSUAVE_1_1Core_1_1redirect_1_1folder-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Member Functions

 
def __delattr__ (self, k)
 
def __defaults__ (self)
 
def __new__ (cls, args, kwarg)
 
def __new__ (cls, *args, **kwarg)
 
def typestring (self)
 
def dataname (self)
 
def __str__ (self, indent='')
 
def __init__ (self, args, kwarg)
 
def __init__ (self, *args, **kwarg)
 
def __iter__ (self)
 
def itervalues (self)
 
def update (self, other)
 
def append_or_update (self, other)
 
def get_bases (self)
 
def append (self, value, key=None)
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -114,7 +121,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Core_1_1redirect_1_1folder.html b/doxygen/classSUAVE_1_1Core_1_1redirect_1_1folder.html index 16584178..b010ece2 100644 --- a/doxygen/classSUAVE_1_1Core_1_1redirect_1_1folder.html +++ b/doxygen/classSUAVE_1_1Core_1_1redirect_1_1folder.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Core.redirect.folder Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -103,9 +110,7 @@ Inheritance diagram for SUAVE.Core.redirect.folder:
- - - +
@@ -57,9 +60,11 @@

@@ -237,7 +242,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Core_1_1redirect_1_1output-members.html b/doxygen/classSUAVE_1_1Core_1_1redirect_1_1output-members.html index cf2af6ad..dacb38c2 100644 --- a/doxygen/classSUAVE_1_1Core_1_1redirect_1_1output-members.html +++ b/doxygen/classSUAVE_1_1Core_1_1redirect_1_1output-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -109,7 +116,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Core_1_1redirect_1_1output.html b/doxygen/classSUAVE_1_1Core_1_1redirect_1_1output.html index 3e97412a..9598846b 100644 --- a/doxygen/classSUAVE_1_1Core_1_1redirect_1_1output.html +++ b/doxygen/classSUAVE_1_1Core_1_1redirect_1_1output.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Core.redirect.output Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -103,9 +110,7 @@ Inheritance diagram for SUAVE.Core.redirect.output:
- - - +
@@ -57,9 +60,11 @@

@@ -204,7 +209,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Input__Output_1_1D3JS_1_1Tree__Element_1_1Tree__Element-members.html b/doxygen/classSUAVE_1_1Input__Output_1_1D3JS_1_1Tree__Element_1_1Tree__Element-members.html index ebc8b5c6..33297d7a 100644 --- a/doxygen/classSUAVE_1_1Input__Output_1_1D3JS_1_1Tree__Element_1_1Tree__Element-members.html +++ b/doxygen/classSUAVE_1_1Input__Output_1_1D3JS_1_1Tree__Element_1_1Tree__Element-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -103,26 +110,26 @@ __eq__(self, other)SUAVE.Core.DataOrdered.DataOrdered __getitem__(self, k)SUAVE.Core.DataOrdered.DataOrdered __init__(self, name)SUAVE.Input_Output.D3JS.Tree_Element.Tree_Element - SUAVE::Core::DataOrdered::DataOrdered.__init__(self, args, kwarg)SUAVE.Core.DataOrdered.DataOrdered + SUAVE::Core::DataOrdered::DataOrdered.__init__(self, *args, **kwarg)SUAVE.Core.DataOrdered.DataOrdered __iter__(self)SUAVE.Core.DataOrdered.DataOrdered - __iter__(self)SUAVE.Core.DataOrdered.DataOrdered + __iter_basic__(self)SUAVE.Core.DataOrdered.DataOrdered __len__(self)SUAVE.Core.DataOrdered.DataOrdered - __new__(cls, args, kwarg)SUAVE.Core.DataOrdered.DataOrdered + __new__(cls, *args, **kwarg)SUAVE.Core.DataOrdered.DataOrdered __reduce__(self)SUAVE.Core.DataOrdered.DataOrdered - __repr__(self)SUAVE.Core.DataOrdered.DataOrdered - __setattr__(self, key, value)SUAVE.Core.DataOrdered.DataOrdered - __setitem__(self, k, v)SUAVE.Core.DataOrdered.DataOrdered - __str__(self, indent='')SUAVE.Core.DataOrdered.DataOrdered - append(self, element)SUAVE.Input_Output.D3JS.Tree_Element.Tree_Element - SUAVE::Core::DataOrdered::DataOrdered.append(self, value, key=None)SUAVE.Core.DataOrdered.DataOrdered - children (defined in SUAVE.Input_Output.D3JS.Tree_Element.Tree_Element)SUAVE.Input_Output.D3JS.Tree_Element.Tree_Element - clear(self)SUAVE.Core.DataOrdered.DataOrdered - dataname(self)SUAVE.Core.DataOrdered.DataOrdered - deep_get(self, keys)SUAVE.Core.DataOrdered.DataOrdered - deep_set(self, keys, val)SUAVE.Core.DataOrdered.DataOrdered - get(self, k, d=None)SUAVE.Core.DataOrdered.DataOrdered - get_bases(self)SUAVE.Core.DataOrdered.DataOrdered - has_key(self, k)SUAVE.Core.DataOrdered.DataOrdered + __setattr__(self, key, value)SUAVE.Core.DataOrdered.DataOrdered + __setitem__(self, k, v)SUAVE.Core.DataOrdered.DataOrdered + __str__(self, indent='')SUAVE.Core.DataOrdered.DataOrdered + append(self, element)SUAVE.Input_Output.D3JS.Tree_Element.Tree_Element + SUAVE::Core::DataOrdered::DataOrdered.append(self, value, key=None)SUAVE.Core.DataOrdered.DataOrdered + children (defined in SUAVE.Input_Output.D3JS.Tree_Element.Tree_Element)SUAVE.Input_Output.D3JS.Tree_Element.Tree_Element + clear(self)SUAVE.Core.DataOrdered.DataOrdered + dataname(self)SUAVE.Core.DataOrdered.DataOrdered + deep_get(self, keys)SUAVE.Core.DataOrdered.DataOrdered + deep_set(self, keys, val)SUAVE.Core.DataOrdered.DataOrdered + get(self, k, d=None)SUAVE.Core.DataOrdered.DataOrdered + get_bases(self)SUAVE.Core.DataOrdered.DataOrdered + has_key(self, k)SUAVE.Core.DataOrdered.DataOrdered + hasattr(self, k) (defined in SUAVE.Core.DataOrdered.DataOrdered)SUAVE.Core.DataOrdered.DataOrdered items(self)SUAVE.Core.DataOrdered.DataOrdered iteritems(self)SUAVE.Core.DataOrdered.DataOrdered iterkeys(self)SUAVE.Core.DataOrdered.DataOrdered @@ -139,7 +146,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Input__Output_1_1D3JS_1_1Tree__Element_1_1Tree__Element.html b/doxygen/classSUAVE_1_1Input__Output_1_1D3JS_1_1Tree__Element_1_1Tree__Element.html index 40593148..f52133c4 100644 --- a/doxygen/classSUAVE_1_1Input__Output_1_1D3JS_1_1Tree__Element_1_1Tree__Element.html +++ b/doxygen/classSUAVE_1_1Input__Output_1_1D3JS_1_1Tree__Element_1_1Tree__Element.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Input_Output.D3JS.Tree_Element.Tree_Element Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -106,8 +113,8 @@ SUAVE.Core.DataOrdered.DataOrdered - -
+ + @@ -122,16 +129,17 @@ - - - - + + + + + + - - @@ -150,8 +158,8 @@ - - + + @@ -295,7 +303,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Input__Output_1_1XML_1_1Data_1_1Attributes.html b/doxygen/classSUAVE_1_1Input__Output_1_1XML_1_1Data_1_1Attributes.html index 0e9a99bb..bb3dde29 100644 --- a/doxygen/classSUAVE_1_1Input__Output_1_1XML_1_1Data_1_1Attributes.html +++ b/doxygen/classSUAVE_1_1Input__Output_1_1XML_1_1Data_1_1Attributes.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Input_Output.XML.Data.Attributes Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Member Functions

 
def __getitem__ (self, k)
 
def __new__ (cls, args, kwarg)
 
def __init__ (self, args, kwarg)
 
def __new__ (cls, *args, **kwarg)
 
+def hasattr (self, k)
 
def __init__ (self, *args, **kwarg)
 
def __iter__ (self)
 
def __str__ (self, indent='')
 
def __repr__ (self)
 
def get_bases (self)
 
def typestring (self)
 
def __len__ (self)
 
def __iter__ (self)
 
def __iter_basic__ (self)
 
def __reduce__ (self)
 
def __setattr__ (self, key, value)
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -99,9 +106,7 @@ Inheritance diagram for SUAVE.Input_Output.XML.Data.Attributes:
- - - +

Detailed Description

Placeholder class. No functionality.
@@ -122,7 +127,7 @@
     
     
+    doxygen 1.8.15 
   
 
diff --git a/doxygen/classSUAVE_1_1Input__Output_1_1XML_1_1Data_1_1Data-members.html b/doxygen/classSUAVE_1_1Input__Output_1_1XML_1_1Data_1_1Data-members.html index 6111809b..b7a3ff42 100644 --- a/doxygen/classSUAVE_1_1Input__Output_1_1XML_1_1Data_1_1Data-members.html +++ b/doxygen/classSUAVE_1_1Input__Output_1_1XML_1_1Data_1_1Data-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -114,7 +121,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Input__Output_1_1XML_1_1Data_1_1Data.html b/doxygen/classSUAVE_1_1Input__Output_1_1XML_1_1Data_1_1Data.html index e075519c..d059d250 100644 --- a/doxygen/classSUAVE_1_1Input__Output_1_1XML_1_1Data_1_1Data.html +++ b/doxygen/classSUAVE_1_1Input__Output_1_1XML_1_1Data_1_1Data.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Input_Output.XML.Data.Data Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -104,9 +111,7 @@ Inheritance diagram for SUAVE.Input_Output.XML.Data.Data:
- - - +
@@ -57,9 +60,11 @@

@@ -368,7 +373,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Input__Output_1_1XML_1_1load_1_1TreeBuilder-members.html b/doxygen/classSUAVE_1_1Input__Output_1_1XML_1_1load_1_1TreeBuilder-members.html index ab408f5f..b76f4db3 100644 --- a/doxygen/classSUAVE_1_1Input__Output_1_1XML_1_1load_1_1TreeBuilder-members.html +++ b/doxygen/classSUAVE_1_1Input__Output_1_1XML_1_1load_1_1TreeBuilder-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -113,7 +120,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Input__Output_1_1XML_1_1load_1_1TreeBuilder.html b/doxygen/classSUAVE_1_1Input__Output_1_1XML_1_1load_1_1TreeBuilder.html index afd992ea..a712c604 100644 --- a/doxygen/classSUAVE_1_1Input__Output_1_1XML_1_1load_1_1TreeBuilder.html +++ b/doxygen/classSUAVE_1_1Input__Output_1_1XML_1_1load_1_1TreeBuilder.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Input_Output.XML.load.TreeBuilder Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -103,9 +110,7 @@ Inheritance diagram for SUAVE.Input_Output.XML.load.TreeBuilder:
- - - +
@@ -57,9 +60,11 @@

@@ -338,7 +343,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Aircraft_1_1Aircraft-members.html b/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Aircraft_1_1Aircraft-members.html index 45ec29d9..3f5a4800 100644 --- a/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Aircraft_1_1Aircraft-members.html +++ b/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Aircraft_1_1Aircraft-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -101,28 +108,29 @@ __defaults__(self)SUAVE.Methods.Aerodynamics.AVL.Data.Aircraft.Aircraft __delattr__(self, k)SUAVE.Core.Data.Data __getattribute__(self, k)SUAVE.Core.Data.Data - __init__(self, args, kwarg)SUAVE.Core.Data.Data + __init__(self, *args, **kwarg)SUAVE.Core.Data.Data __iter__(self)SUAVE.Core.Data.Data - __new__(cls, args, kwarg)SUAVE.Core.Data.Data + __new__(cls, *args, **kwarg)SUAVE.Core.Data.Data __setattr__(self, k, v)SUAVE.Core.Data.Data __str__(self, indent='')SUAVE.Core.Data.Data append(self, value, key=None)SUAVE.Core.Data.Data append_body(self, body)SUAVE.Methods.Aerodynamics.AVL.Data.Aircraft.Aircraft - append_wing(self, wing)SUAVE.Methods.Aerodynamics.AVL.Data.Aircraft.Aircraft - bodies (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Aircraft.Aircraft)SUAVE.Methods.Aerodynamics.AVL.Data.Aircraft.Aircraft - dataname(self)SUAVE.Core.Data.Data - deep_get(self, keys)SUAVE.Core.Data.Data - deep_set(self, keys, val)SUAVE.Core.Data.Data - do_recursive(self, method, other=None, default=None)SUAVE.Core.Data.Data - get_bases(self)SUAVE.Core.Data.Data - itervalues(self)SUAVE.Core.Data.Data - pack_array(self, output='vector')SUAVE.Core.Data.Data - tag (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Aircraft.Aircraft)SUAVE.Methods.Aerodynamics.AVL.Data.Aircraft.Aircraft - typestring(self)SUAVE.Core.Data.Data - unpack_array(self, M)SUAVE.Core.Data.Data - update(self, other)SUAVE.Core.Data.Data - values(self)SUAVE.Core.Data.Data - wings (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Aircraft.Aircraft)SUAVE.Methods.Aerodynamics.AVL.Data.Aircraft.Aircraft + append_or_update(self, other)SUAVE.Core.Data.Data + append_wing(self, wing)SUAVE.Methods.Aerodynamics.AVL.Data.Aircraft.Aircraft + bodies (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Aircraft.Aircraft)SUAVE.Methods.Aerodynamics.AVL.Data.Aircraft.Aircraft + dataname(self)SUAVE.Core.Data.Data + deep_get(self, keys)SUAVE.Core.Data.Data + deep_set(self, keys, val)SUAVE.Core.Data.Data + do_recursive(self, method, other=None, default=None)SUAVE.Core.Data.Data + get_bases(self)SUAVE.Core.Data.Data + itervalues(self)SUAVE.Core.Data.Data + pack_array(self, output='vector')SUAVE.Core.Data.Data + tag (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Aircraft.Aircraft)SUAVE.Methods.Aerodynamics.AVL.Data.Aircraft.Aircraft + typestring(self)SUAVE.Core.Data.Data + unpack_array(self, M)SUAVE.Core.Data.Data + update(self, other)SUAVE.Core.Data.Data + values(self)SUAVE.Core.Data.Data + wings (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Aircraft.Aircraft)SUAVE.Methods.Aerodynamics.AVL.Data.Aircraft.Aircraft
@@ -130,7 +138,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Aircraft_1_1Aircraft.html b/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Aircraft_1_1Aircraft.html index d2d825b4..1b5a7972 100644 --- a/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Aircraft_1_1Aircraft.html +++ b/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Aircraft_1_1Aircraft.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Methods.Aerodynamics.AVL.Data.Aircraft.Aircraft Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -106,8 +113,8 @@ SUAVE.Core.Data.Data - -
+ + @@ -124,18 +131,16 @@ - - - - + + - - + + @@ -144,6 +149,8 @@ + + @@ -221,6 +228,8 @@

SUAVE.Core.Data.Data.

+ @@ -322,7 +331,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Body_1_1Body-members.html b/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Body_1_1Body-members.html index 91c7c46d..10a043cf 100644 --- a/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Body_1_1Body-members.html +++ b/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Body_1_1Body-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Member Functions

 
def __delattr__ (self, k)
 
def __defaults__ (self)
 
def __new__ (cls, args, kwarg)
 
def __new__ (cls, *args, **kwarg)
 
def typestring (self)
 
def dataname (self)
 
def __str__ (self, indent='')
 
def __init__ (self, args, kwarg)
 
def __init__ (self, *args, **kwarg)
 
def __iter__ (self)
 
def itervalues (self)
 
def update (self, other)
 
def append_or_update (self, other)
 
def get_bases (self)
 
def append (self, value, key=None)
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -101,32 +108,33 @@ __defaults__(self)SUAVE.Methods.Aerodynamics.AVL.Data.Body.Body __delattr__(self, k)SUAVE.Core.Data.Data __getattribute__(self, k)SUAVE.Core.Data.Data - __init__(self, args, kwarg)SUAVE.Core.Data.Data + __init__(self, *args, **kwarg)SUAVE.Core.Data.Data __iter__(self)SUAVE.Core.Data.Data - __new__(cls, args, kwarg)SUAVE.Core.Data.Data + __new__(cls, *args, **kwarg)SUAVE.Core.Data.Data __setattr__(self, k, v)SUAVE.Core.Data.Data __str__(self, indent='')SUAVE.Core.Data.Data append(self, value, key=None)SUAVE.Core.Data.Data - append_section(self, section, orientation='Horizontal')SUAVE.Methods.Aerodynamics.AVL.Data.Body.Body - configuration (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Body.Body)SUAVE.Methods.Aerodynamics.AVL.Data.Body.Body - dataname(self)SUAVE.Core.Data.Data - deep_get(self, keys)SUAVE.Core.Data.Data - deep_set(self, keys, val)SUAVE.Core.Data.Data - do_recursive(self, method, other=None, default=None)SUAVE.Core.Data.Data - get_bases(self)SUAVE.Core.Data.Data - heights (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Body.Body)SUAVE.Methods.Aerodynamics.AVL.Data.Body.Body - itervalues(self)SUAVE.Core.Data.Data - lengths (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Body.Body)SUAVE.Methods.Aerodynamics.AVL.Data.Body.Body - origin (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Body.Body)SUAVE.Methods.Aerodynamics.AVL.Data.Body.Body - pack_array(self, output='vector')SUAVE.Core.Data.Data - sections (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Body.Body)SUAVE.Methods.Aerodynamics.AVL.Data.Body.Body - symmetric (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Body.Body)SUAVE.Methods.Aerodynamics.AVL.Data.Body.Body - tag (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Body.Body)SUAVE.Methods.Aerodynamics.AVL.Data.Body.Body - typestring(self)SUAVE.Core.Data.Data - unpack_array(self, M)SUAVE.Core.Data.Data - update(self, other)SUAVE.Core.Data.Data - values(self)SUAVE.Core.Data.Data - widths (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Body.Body)SUAVE.Methods.Aerodynamics.AVL.Data.Body.Body + append_or_update(self, other)SUAVE.Core.Data.Data + append_section(self, section, orientation='Horizontal')SUAVE.Methods.Aerodynamics.AVL.Data.Body.Body + configuration (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Body.Body)SUAVE.Methods.Aerodynamics.AVL.Data.Body.Body + dataname(self)SUAVE.Core.Data.Data + deep_get(self, keys)SUAVE.Core.Data.Data + deep_set(self, keys, val)SUAVE.Core.Data.Data + do_recursive(self, method, other=None, default=None)SUAVE.Core.Data.Data + get_bases(self)SUAVE.Core.Data.Data + heights (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Body.Body)SUAVE.Methods.Aerodynamics.AVL.Data.Body.Body + itervalues(self)SUAVE.Core.Data.Data + lengths (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Body.Body)SUAVE.Methods.Aerodynamics.AVL.Data.Body.Body + origin (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Body.Body)SUAVE.Methods.Aerodynamics.AVL.Data.Body.Body + pack_array(self, output='vector')SUAVE.Core.Data.Data + sections (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Body.Body)SUAVE.Methods.Aerodynamics.AVL.Data.Body.Body + symmetric (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Body.Body)SUAVE.Methods.Aerodynamics.AVL.Data.Body.Body + tag (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Body.Body)SUAVE.Methods.Aerodynamics.AVL.Data.Body.Body + typestring(self)SUAVE.Core.Data.Data + unpack_array(self, M)SUAVE.Core.Data.Data + update(self, other)SUAVE.Core.Data.Data + values(self)SUAVE.Core.Data.Data + widths (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Body.Body)SUAVE.Methods.Aerodynamics.AVL.Data.Body.Body
@@ -134,7 +142,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Body_1_1Body.html b/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Body_1_1Body.html index afe52eaf..4cae2ab3 100644 --- a/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Body_1_1Body.html +++ b/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Body_1_1Body.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Methods.Aerodynamics.AVL.Data.Body.Body Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -106,8 +113,8 @@ SUAVE.Core.Data.Data - -
+ + @@ -122,18 +129,16 @@ - - - - + + - - + + @@ -142,6 +147,8 @@ + + @@ -236,6 +243,8 @@

SUAVE.Core.Data.Data.

+ @@ -299,7 +308,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Container-members.html b/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Container-members.html index d7150e69..29796407 100644 --- a/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Container-members.html +++ b/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Container-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Member Functions

 
def __delattr__ (self, k)
 
def __defaults__ (self)
 
def __new__ (cls, args, kwarg)
 
def __new__ (cls, *args, **kwarg)
 
def typestring (self)
 
def dataname (self)
 
def __str__ (self, indent='')
 
def __init__ (self, args, kwarg)
 
def __init__ (self, *args, **kwarg)
 
def __iter__ (self)
 
def itervalues (self)
 
def update (self, other)
 
def append_or_update (self, other)
 
def get_bases (self)
 
def append (self, value, key=None)
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -102,25 +109,25 @@ __delattr__(self, key)SUAVE.Core.DataOrdered.DataOrdered __eq__(self, other)SUAVE.Core.DataOrdered.DataOrdered __getitem__(self, k)SUAVE.Core.DataOrdered.DataOrdered - __init__(self, args, kwarg)SUAVE.Core.DataOrdered.DataOrdered + __init__(self, *args, **kwarg)SUAVE.Core.DataOrdered.DataOrdered __iter__(self)SUAVE.Core.DataOrdered.DataOrdered - __iter__(self)SUAVE.Core.DataOrdered.DataOrdered + __iter_basic__(self)SUAVE.Core.DataOrdered.DataOrdered __len__(self)SUAVE.Core.DataOrdered.DataOrdered - __new__(cls, args, kwarg)SUAVE.Core.DataOrdered.DataOrdered + __new__(cls, *args, **kwarg)SUAVE.Core.DataOrdered.DataOrdered __reduce__(self)SUAVE.Core.DataOrdered.DataOrdered - __repr__(self)SUAVE.Core.DataOrdered.DataOrdered - __setattr__(self, key, value)SUAVE.Core.DataOrdered.DataOrdered - __setitem__(self, k, v)SUAVE.Core.DataOrdered.DataOrdered - __str__(self, indent='')SUAVE.Core.DataOrdered.DataOrdered - append(self, value, key=None)SUAVE.Core.DataOrdered.DataOrdered - append_case(self, case)SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Container - clear(self)SUAVE.Core.DataOrdered.DataOrdered - dataname(self)SUAVE.Core.DataOrdered.DataOrdered - deep_get(self, keys)SUAVE.Core.DataOrdered.DataOrdered - deep_set(self, keys, val)SUAVE.Core.DataOrdered.DataOrdered - get(self, k, d=None)SUAVE.Core.DataOrdered.DataOrdered - get_bases(self)SUAVE.Core.DataOrdered.DataOrdered - has_key(self, k)SUAVE.Core.DataOrdered.DataOrdered + __setattr__(self, key, value)SUAVE.Core.DataOrdered.DataOrdered + __setitem__(self, k, v)SUAVE.Core.DataOrdered.DataOrdered + __str__(self, indent='')SUAVE.Core.DataOrdered.DataOrdered + append(self, value, key=None)SUAVE.Core.DataOrdered.DataOrdered + append_case(self, case)SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Container + clear(self)SUAVE.Core.DataOrdered.DataOrdered + dataname(self)SUAVE.Core.DataOrdered.DataOrdered + deep_get(self, keys)SUAVE.Core.DataOrdered.DataOrdered + deep_set(self, keys, val)SUAVE.Core.DataOrdered.DataOrdered + get(self, k, d=None)SUAVE.Core.DataOrdered.DataOrdered + get_bases(self)SUAVE.Core.DataOrdered.DataOrdered + has_key(self, k)SUAVE.Core.DataOrdered.DataOrdered + hasattr(self, k) (defined in SUAVE.Core.DataOrdered.DataOrdered)SUAVE.Core.DataOrdered.DataOrdered items(self)SUAVE.Core.DataOrdered.DataOrdered iteritems(self)SUAVE.Core.DataOrdered.DataOrdered iterkeys(self)SUAVE.Core.DataOrdered.DataOrdered @@ -136,7 +143,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Container.html b/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Container.html index a8003e55..fb0dc1b5 100644 --- a/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Container.html +++ b/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Container.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Container Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -105,8 +112,8 @@ SUAVE.Core.DataOrdered.DataOrdered - -
+ + @@ -119,16 +126,17 @@ - - - - + + + + + + - - @@ -147,8 +155,8 @@ - - + + @@ -175,7 +183,7 @@

Public Member Functions

 
def __getitem__ (self, k)
 
def __new__ (cls, args, kwarg)
 
def __init__ (self, args, kwarg)
 
def __new__ (cls, *args, **kwarg)
 
+def hasattr (self, k)
 
def __init__ (self, *args, **kwarg)
 
def __iter__ (self)
 
def __str__ (self, indent='')
 
def __repr__ (self)
 
def get_bases (self)
 
def typestring (self)
 
def __len__ (self)
 
def __iter__ (self)
 
def __iter_basic__ (self)
 
def __reduce__ (self)
 
def __setattr__ (self, key, value)
 

Detailed Description

-
A data class for the addition of a cases to the set of run cases
+
This is a data class for the addition of a cases to the set of run cases
 
 Assumptions:
     None
@@ -246,7 +254,7 @@ 

SUAVE + doxygen 1.8.15

diff --git a/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Run__Case-members.html b/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Run__Case-members.html index 69467d8b..c046468a 100644 --- a/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Run__Case-members.html +++ b/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Run__Case-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@
- +
@@ -73,7 +78,9 @@
@@ -101,25 +108,29 @@ __defaults__(self)SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Run_Case __delattr__(self, k)SUAVE.Core.Data.Data __getattribute__(self, k)SUAVE.Core.Data.Data - __init__(self, args, kwarg)SUAVE.Core.Data.Data + __init__(self, *args, **kwarg)SUAVE.Core.Data.Data __iter__(self)SUAVE.Core.Data.Data - __new__(cls, args, kwarg)SUAVE.Core.Data.Data + __new__(cls, *args, **kwarg)SUAVE.Core.Data.Data __setattr__(self, k, v)SUAVE.Core.Data.Data __str__(self, indent='')SUAVE.Core.Data.Data + aero_result_filename_1 (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Run_Case)SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Run_Case + aero_result_filename_2 (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Run_Case)SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Run_Case + aero_result_filename_3 (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Run_Case)SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Run_Case + aero_result_filename_4 (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Run_Case)SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Run_Case append(self, value, key=None)SUAVE.Core.Data.Data - append_control_deflection(self, control_tag, deflection)SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Run_Case + append_or_update(self, other)SUAVE.Core.Data.Data conditions (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Run_Case)SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Run_Case dataname(self)SUAVE.Core.Data.Data deep_get(self, keys)SUAVE.Core.Data.Data deep_set(self, keys, val)SUAVE.Core.Data.Data do_recursive(self, method, other=None, default=None)SUAVE.Core.Data.Data - eigen_result_filename (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Run_Case)SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Run_Case - get_bases(self)SUAVE.Core.Data.Data - index (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Run_Case)SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Run_Case - itervalues(self)SUAVE.Core.Data.Data - mass (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Run_Case)SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Run_Case - pack_array(self, output='vector')SUAVE.Core.Data.Data - result_filename (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Run_Case)SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Run_Case + eigen_result_filename_1 (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Run_Case)SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Run_Case + eigen_result_filename_2 (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Run_Case)SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Run_Case + get_bases(self)SUAVE.Core.Data.Data + index (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Run_Case)SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Run_Case + itervalues(self)SUAVE.Core.Data.Data + mass (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Run_Case)SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Run_Case + pack_array(self, output='vector')SUAVE.Core.Data.Data stability_and_control (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Run_Case)SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Run_Case tag (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Run_Case)SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Run_Case typestring(self)SUAVE.Core.Data.Data @@ -133,7 +144,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Run__Case.html b/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Run__Case.html index 0e91ad30..66d31096 100644 --- a/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Run__Case.html +++ b/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Run__Case.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Run_Case Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -106,15 +113,13 @@ SUAVE.Core.Data.Data - -
+ + - - @@ -122,18 +127,16 @@ - - - - + + - - + + @@ -142,6 +145,8 @@ + + @@ -174,15 +179,27 @@ - - - - + + + + + + + + + + + +

Public Member Functions

def __defaults__ (self)
 
def append_control_deflection (self, control_tag, deflection)
 
- Public Member Functions inherited from SUAVE.Core.Data.Data
def __getattribute__ (self, k)
 
 
def __delattr__ (self, k)
 
def __defaults__ (self)
 
def __new__ (cls, args, kwarg)
 
def __new__ (cls, *args, **kwarg)
 
def typestring (self)
 
def dataname (self)
 
def __str__ (self, indent='')
 
def __init__ (self, args, kwarg)
 
def __init__ (self, *args, **kwarg)
 
def __iter__ (self)
 
def itervalues (self)
 
def update (self, other)
 
def append_or_update (self, other)
 
def get_bases (self)
 
def append (self, value, key=None)
 stability_and_control
 
result_filename
 
eigen_result_filename
 
aero_result_filename_1
 
aero_result_filename_2
 
aero_result_filename_3
 
aero_result_filename_4
 
eigen_result_filename_1
 
eigen_result_filename_2
 

Detailed Description

-
A data class defining the parameters for the analysis cases 
+
This data class defines the parameters for the analysis cases 
 including angle of attack and mach number 
 
 Assumptions:
@@ -216,7 +233,7 @@ 

Defines the data structure and defaults of aerodynamics coefficients, 
-body derivatives and stability derivatives   
+body axis derivatives and stability axis derivatives   
 
 Assumptions:
     None
@@ -233,55 +250,8 @@ 

-

◆ append_control_deflection()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Aerodynamics.AVL.Data.Cases.Run_Case.append_control_deflection ( self,
 control_tag,
 deflection 
)
-
-
Adds a control deflection case 
+

Reimplemented from SUAVE.Core.Data.Data.

- Assumptions: -None - - Source: -None - - Inputs: -None - - Outputs: -None - - Properties Used: -N/A

The documentation for this class was generated from the following file:

diff --git a/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Run__Case.js b/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Run__Case.js index c8c72c46..6dc87fdf 100644 --- a/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Run__Case.js +++ b/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Run__Case.js @@ -1,12 +1,15 @@ var classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Run__Case = [ [ "__defaults__", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Run__Case.html#a6a9108165be8c60598d8040c1b3c5203", null ], - [ "append_control_deflection", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Run__Case.html#a0204b074d5dad2d32d5b221ad922dc2a", null ], + [ "aero_result_filename_1", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Run__Case.html#ab2020f583786f08fad116df7bd0d4fcd", null ], + [ "aero_result_filename_2", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Run__Case.html#acec5a3e0dfb52539fdc3136618caa5ea", null ], + [ "aero_result_filename_3", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Run__Case.html#a1f8d22469b8f3d78585a16babe48d570", null ], + [ "aero_result_filename_4", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Run__Case.html#a86724b57e2dcf8b5b43686e5bfcf230f", null ], [ "conditions", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Run__Case.html#a3eddb7985cac1df2f93fd4c90b5d14f2", null ], - [ "eigen_result_filename", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Run__Case.html#ae88894a124bdf653ae64543605114198", null ], + [ "eigen_result_filename_1", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Run__Case.html#a4e4049020099e3a1e9cfa6be5d7dbcc2", null ], + [ "eigen_result_filename_2", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Run__Case.html#a4f5c4e7bc7d3f75def3b7eb38f0da65f", null ], [ "index", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Run__Case.html#a5271bb99f849f5f6dca450f1f293023a", null ], [ "mass", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Run__Case.html#a92517a94d9e4bb763fceaca80c3a4b25", null ], - [ "result_filename", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Run__Case.html#a8cbb7d2798c08a5e631204180b4bd9c2", null ], [ "stability_and_control", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Run__Case.html#a5958cefee53f8e33db6a32520c7b7f91", null ], [ "tag", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Run__Case.html#a94540c93dbd0009db6b3b022c9a3fbdc", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Configuration_1_1Configuration-members.html b/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Configuration_1_1Configuration-members.html index 404cccad..e96ab9ad 100644 --- a/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Configuration_1_1Configuration-members.html +++ b/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Configuration_1_1Configuration-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@
- +
@@ -73,7 +78,9 @@
@@ -101,28 +108,29 @@ __defaults__(self)SUAVE.Methods.Aerodynamics.AVL.Data.Configuration.Configuration __delattr__(self, k)SUAVE.Core.Data.Data __getattribute__(self, k)SUAVE.Core.Data.Data - __init__(self, args, kwarg)SUAVE.Core.Data.Data + __init__(self, *args, **kwarg)SUAVE.Core.Data.Data __iter__(self)SUAVE.Core.Data.Data - __new__(cls, args, kwarg)SUAVE.Core.Data.Data + __new__(cls, *args, **kwarg)SUAVE.Core.Data.Data __setattr__(self, k, v)SUAVE.Core.Data.Data __str__(self, indent='')SUAVE.Core.Data.Data append(self, value, key=None)SUAVE.Core.Data.Data - dataname(self)SUAVE.Core.Data.Data - deep_get(self, keys)SUAVE.Core.Data.Data - deep_set(self, keys, val)SUAVE.Core.Data.Data - do_recursive(self, method, other=None, default=None)SUAVE.Core.Data.Data - get_bases(self)SUAVE.Core.Data.Data - itervalues(self)SUAVE.Core.Data.Data - mass_properties (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Configuration.Configuration)SUAVE.Methods.Aerodynamics.AVL.Data.Configuration.Configuration - pack_array(self, output='vector')SUAVE.Core.Data.Data - parasite_drag (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Configuration.Configuration)SUAVE.Methods.Aerodynamics.AVL.Data.Configuration.Configuration - reference_values (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Configuration.Configuration)SUAVE.Methods.Aerodynamics.AVL.Data.Configuration.Configuration - symmetry_settings (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Configuration.Configuration)SUAVE.Methods.Aerodynamics.AVL.Data.Configuration.Configuration - tag (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Configuration.Configuration)SUAVE.Methods.Aerodynamics.AVL.Data.Configuration.Configuration - typestring(self)SUAVE.Core.Data.Data - unpack_array(self, M)SUAVE.Core.Data.Data - update(self, other)SUAVE.Core.Data.Data - values(self)SUAVE.Core.Data.Data + append_or_update(self, other)SUAVE.Core.Data.Data + dataname(self)SUAVE.Core.Data.Data + deep_get(self, keys)SUAVE.Core.Data.Data + deep_set(self, keys, val)SUAVE.Core.Data.Data + do_recursive(self, method, other=None, default=None)SUAVE.Core.Data.Data + get_bases(self)SUAVE.Core.Data.Data + itervalues(self)SUAVE.Core.Data.Data + mass_properties (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Configuration.Configuration)SUAVE.Methods.Aerodynamics.AVL.Data.Configuration.Configuration + pack_array(self, output='vector')SUAVE.Core.Data.Data + parasite_drag (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Configuration.Configuration)SUAVE.Methods.Aerodynamics.AVL.Data.Configuration.Configuration + reference_values (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Configuration.Configuration)SUAVE.Methods.Aerodynamics.AVL.Data.Configuration.Configuration + symmetry_settings (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Configuration.Configuration)SUAVE.Methods.Aerodynamics.AVL.Data.Configuration.Configuration + tag (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Configuration.Configuration)SUAVE.Methods.Aerodynamics.AVL.Data.Configuration.Configuration + typestring(self)SUAVE.Core.Data.Data + unpack_array(self, M)SUAVE.Core.Data.Data + update(self, other)SUAVE.Core.Data.Data + values(self)SUAVE.Core.Data.Data
@@ -130,7 +138,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Configuration_1_1Configuration.html b/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Configuration_1_1Configuration.html index fb642c73..f3eac228 100644 --- a/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Configuration_1_1Configuration.html +++ b/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Configuration_1_1Configuration.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Methods.Aerodynamics.AVL.Data.Configuration.Configuration Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -106,8 +113,8 @@ SUAVE.Core.Data.Data - -
+ + @@ -120,18 +127,16 @@ - - - - + + - - + + @@ -140,6 +145,8 @@ + + @@ -174,7 +181,7 @@

Public Member Functions

 
def __delattr__ (self, k)
 
def __defaults__ (self)
 
def __new__ (cls, args, kwarg)
 
def __new__ (cls, *args, **kwarg)
 
def typestring (self)
 
def dataname (self)
 
def __str__ (self, indent='')
 
def __init__ (self, args, kwarg)
 
def __init__ (self, *args, **kwarg)
 
def __iter__ (self)
 
def itervalues (self)
 
def update (self, other)
 
def append_or_update (self, other)
 
def get_bases (self)
 
def append (self, value, key=None)
 

Detailed Description

-
A data class defining the reference parameters of the aircraft geoemtry and 
+
A data class defining the reference parameters of the aircraft geometry and 
 flight configuration 
 
 Assumptions:
@@ -225,6 +232,8 @@ 

SUAVE.Core.Data.Data.

+


The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Inputs_1_1Inputs-members.html b/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Inputs_1_1Inputs-members.html index 47d29a0a..51cc4b64 100644 --- a/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Inputs_1_1Inputs-members.html +++ b/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Inputs_1_1Inputs-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -101,28 +108,29 @@ __defaults__(self)SUAVE.Methods.Aerodynamics.AVL.Data.Inputs.Inputs __delattr__(self, k)SUAVE.Core.Data.Data __getattribute__(self, k)SUAVE.Core.Data.Data - __init__(self, args, kwarg)SUAVE.Core.Data.Data + __init__(self, *args, **kwarg)SUAVE.Core.Data.Data __iter__(self)SUAVE.Core.Data.Data - __new__(cls, args, kwarg)SUAVE.Core.Data.Data + __new__(cls, *args, **kwarg)SUAVE.Core.Data.Data __setattr__(self, k, v)SUAVE.Core.Data.Data __str__(self, indent='')SUAVE.Core.Data.Data aircraft (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Inputs.Inputs)SUAVE.Methods.Aerodynamics.AVL.Data.Inputs.Inputs append(self, value, key=None)SUAVE.Core.Data.Data - avl_bin_path (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Inputs.Inputs)SUAVE.Methods.Aerodynamics.AVL.Data.Inputs.Inputs - cases (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Inputs.Inputs)SUAVE.Methods.Aerodynamics.AVL.Data.Inputs.Inputs - configuration (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Inputs.Inputs)SUAVE.Methods.Aerodynamics.AVL.Data.Inputs.Inputs - dataname(self)SUAVE.Core.Data.Data - deep_get(self, keys)SUAVE.Core.Data.Data - deep_set(self, keys, val)SUAVE.Core.Data.Data - do_recursive(self, method, other=None, default=None)SUAVE.Core.Data.Data - get_bases(self)SUAVE.Core.Data.Data - input_files (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Inputs.Inputs)SUAVE.Methods.Aerodynamics.AVL.Data.Inputs.Inputs - itervalues(self)SUAVE.Core.Data.Data - pack_array(self, output='vector')SUAVE.Core.Data.Data - typestring(self)SUAVE.Core.Data.Data - unpack_array(self, M)SUAVE.Core.Data.Data - update(self, other)SUAVE.Core.Data.Data - values(self)SUAVE.Core.Data.Data + append_or_update(self, other)SUAVE.Core.Data.Data + avl_bin_path (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Inputs.Inputs)SUAVE.Methods.Aerodynamics.AVL.Data.Inputs.Inputs + cases (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Inputs.Inputs)SUAVE.Methods.Aerodynamics.AVL.Data.Inputs.Inputs + configuration (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Inputs.Inputs)SUAVE.Methods.Aerodynamics.AVL.Data.Inputs.Inputs + dataname(self)SUAVE.Core.Data.Data + deep_get(self, keys)SUAVE.Core.Data.Data + deep_set(self, keys, val)SUAVE.Core.Data.Data + do_recursive(self, method, other=None, default=None)SUAVE.Core.Data.Data + get_bases(self)SUAVE.Core.Data.Data + input_files (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Inputs.Inputs)SUAVE.Methods.Aerodynamics.AVL.Data.Inputs.Inputs + itervalues(self)SUAVE.Core.Data.Data + pack_array(self, output='vector')SUAVE.Core.Data.Data + typestring(self)SUAVE.Core.Data.Data + unpack_array(self, M)SUAVE.Core.Data.Data + update(self, other)SUAVE.Core.Data.Data + values(self)SUAVE.Core.Data.Data
@@ -130,7 +138,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Inputs_1_1Inputs.html b/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Inputs_1_1Inputs.html index c421254c..23456944 100644 --- a/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Inputs_1_1Inputs.html +++ b/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Inputs_1_1Inputs.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Methods.Aerodynamics.AVL.Data.Inputs.Inputs Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -106,8 +113,8 @@ SUAVE.Core.Data.Data - -
+ + @@ -120,18 +127,16 @@ - - - - + + - - + + @@ -140,6 +145,8 @@ + + @@ -223,6 +230,8 @@

SUAVE.Core.Data.Data.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Settings_1_1AVL__Discretization__Settings-members.html b/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Settings_1_1AVL__Discretization__Settings-members.html deleted file mode 100644 index eccee9d5..00000000 --- a/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Settings_1_1AVL__Discretization__Settings-members.html +++ /dev/null @@ -1,136 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
-

Public Member Functions

 
def __delattr__ (self, k)
 
def __defaults__ (self)
 
def __new__ (cls, args, kwarg)
 
def __new__ (cls, *args, **kwarg)
 
def typestring (self)
 
def dataname (self)
 
def __str__ (self, indent='')
 
def __init__ (self, args, kwarg)
 
def __init__ (self, *args, **kwarg)
 
def __iter__ (self)
 
def itervalues (self)
 
def update (self, other)
 
def append_or_update (self, other)
 
def get_bases (self)
 
def append (self, value, key=None)
- - - - - - - -
-
SUAVE -  1.1.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
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- - - - - -
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SUAVE.Methods.Aerodynamics.AVL.Data.Settings.AVL_Discretization_Settings Member List
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This is the complete list of members for SUAVE.Methods.Aerodynamics.AVL.Data.Settings.AVL_Discretization_Settings, including all inherited members.

- - - - - - - - - - - - - - - - - - - - - - - - - -
__defaults__(self)SUAVE.Methods.Aerodynamics.AVL.Data.Settings.AVL_Discretization_Settings
__delattr__(self, k)SUAVE.Core.Data.Data
__getattribute__(self, k)SUAVE.Core.Data.Data
__init__(self, args, kwarg)SUAVE.Core.Data.Data
__iter__(self)SUAVE.Core.Data.Data
__new__(cls, args, kwarg)SUAVE.Core.Data.Data
__setattr__(self, k, v)SUAVE.Core.Data.Data
__str__(self, indent='')SUAVE.Core.Data.Data
append(self, value, key=None)SUAVE.Core.Data.Data
chordwise_elements (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Settings.AVL_Discretization_Settings)SUAVE.Methods.Aerodynamics.AVL.Data.Settings.AVL_Discretization_Settings
chordwise_spacing_scheme (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Settings.AVL_Discretization_Settings)SUAVE.Methods.Aerodynamics.AVL.Data.Settings.AVL_Discretization_Settings
dataname(self)SUAVE.Core.Data.Data
deep_get(self, keys)SUAVE.Core.Data.Data
deep_set(self, keys, val)SUAVE.Core.Data.Data
do_recursive(self, method, other=None, default=None)SUAVE.Core.Data.Data
get_bases(self)SUAVE.Core.Data.Data
itervalues(self)SUAVE.Core.Data.Data
pack_array(self, output='vector')SUAVE.Core.Data.Data
spanwise_elements (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Settings.AVL_Discretization_Settings)SUAVE.Methods.Aerodynamics.AVL.Data.Settings.AVL_Discretization_Settings
spanwise_spacing_scheme (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Settings.AVL_Discretization_Settings)SUAVE.Methods.Aerodynamics.AVL.Data.Settings.AVL_Discretization_Settings
typestring(self)SUAVE.Core.Data.Data
unpack_array(self, M)SUAVE.Core.Data.Data
update(self, other)SUAVE.Core.Data.Data
values(self)SUAVE.Core.Data.Data
-
- - - - diff --git a/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Settings_1_1AVL__Discretization__Settings.html b/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Settings_1_1AVL__Discretization__Settings.html deleted file mode 100644 index eeda78e0..00000000 --- a/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Settings_1_1AVL__Discretization__Settings.html +++ /dev/null @@ -1,245 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Methods.Aerodynamics.AVL.Data.Settings.AVL_Discretization_Settings Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.1.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
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-
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-
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- -
- -
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- - -
- -
- -
- -
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SUAVE.Methods.Aerodynamics.AVL.Data.Settings.AVL_Discretization_Settings Class Reference
-
-
-
-Inheritance diagram for SUAVE.Methods.Aerodynamics.AVL.Data.Settings.AVL_Discretization_Settings:
-
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- - -SUAVE.Core.Data.Data - -
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Core.Data.Data
def __getattribute__ (self, k)
 
def __setattr__ (self, k, v)
 
def __delattr__ (self, k)
 
def __defaults__ (self)
 
def __new__ (cls, args, kwarg)
 
def typestring (self)
 
def dataname (self)
 
def __str__ (self, indent='')
 
def __init__ (self, args, kwarg)
 
def __iter__ (self)
 
def itervalues (self)
 
def values (self)
 
def update (self, other)
 
def get_bases (self)
 
def append (self, value, key=None)
 
def deep_set (self, keys, val)
 
def deep_get (self, keys)
 
def pack_array (self, output='vector')
 
def unpack_array (self, M)
 
def do_recursive (self, method, other=None, default=None)
 
- - - - - - - - - -

-Public Attributes

chordwise_elements
 
chordwise_spacing_scheme
 
spanwise_elements
 
spanwise_spacing_scheme
 
-

Detailed Description

-
A class that defines discretization of vortices on the aircraft wing
-
-Assumptions:
-    None
-    
-Source:
-    None
-    
-Inputs:
-    None
-    
-Outputs:
-    None
-    
-Properties Used:
-    N/A
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Methods.Aerodynamics.AVL.Data.Settings.AVL_Discretization_Settings.__defaults__ ( self)
-
-
Defines the spacing of vortices on lifting surface in AVL
-SPACING SCHEMES:
-    - 'cosine' : ||  |    |      |      |    |  || (bunched at both ends)
-    - '+sine'  : || |  |   |    |    |     |     | (bunched at start)
-    - 'equal'  : |   |   |   |   |   |   |   |   | (equally spaced)
-    - '-sine'  : |     |     |    |    |   |  | || (bunched at end)
-               
-Assumptions:
-    None
-
-Source:
-    None
-
-Inputs:
-    None
-
-Outputs:
-    None
-
-Properties Used:
-    N/A
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Methods/Aerodynamics/AVL/Data/Settings.py
  • -
-
-
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SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -101,28 +108,29 @@ __defaults__(self)SUAVE.Methods.Aerodynamics.AVL.Data.Settings.Settings __delattr__(self, k)SUAVE.Core.Data.Data __getattribute__(self, k)SUAVE.Core.Data.Data - __init__(self, args, kwarg)SUAVE.Core.Data.Data + __init__(self, *args, **kwarg)SUAVE.Core.Data.Data __iter__(self)SUAVE.Core.Data.Data - __new__(cls, args, kwarg)SUAVE.Core.Data.Data + __new__(cls, *args, **kwarg)SUAVE.Core.Data.Data __setattr__(self, k, v)SUAVE.Core.Data.Data __str__(self, indent='')SUAVE.Core.Data.Data append(self, value, key=None)SUAVE.Core.Data.Data - dataname(self)SUAVE.Core.Data.Data - deep_get(self, keys)SUAVE.Core.Data.Data - deep_set(self, keys, val)SUAVE.Core.Data.Data - discretization (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Settings.Settings)SUAVE.Methods.Aerodynamics.AVL.Data.Settings.Settings - do_recursive(self, method, other=None, default=None)SUAVE.Core.Data.Data - filenames (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Settings.Settings)SUAVE.Methods.Aerodynamics.AVL.Data.Settings.Settings - flow_symmetry (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Settings.Settings)SUAVE.Methods.Aerodynamics.AVL.Data.Settings.Settings - get_bases(self)SUAVE.Core.Data.Data - itervalues(self)SUAVE.Core.Data.Data - number_control_surfaces (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Settings.Settings)SUAVE.Methods.Aerodynamics.AVL.Data.Settings.Settings - pack_array(self, output='vector')SUAVE.Core.Data.Data - run_cases (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Settings.Settings)SUAVE.Methods.Aerodynamics.AVL.Data.Settings.Settings - typestring(self)SUAVE.Core.Data.Data - unpack_array(self, M)SUAVE.Core.Data.Data - update(self, other)SUAVE.Core.Data.Data - values(self)SUAVE.Core.Data.Data + append_or_update(self, other)SUAVE.Core.Data.Data + dataname(self)SUAVE.Core.Data.Data + deep_get(self, keys)SUAVE.Core.Data.Data + deep_set(self, keys, val)SUAVE.Core.Data.Data + discretization (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Settings.Settings)SUAVE.Methods.Aerodynamics.AVL.Data.Settings.Settings + do_recursive(self, method, other=None, default=None)SUAVE.Core.Data.Data + filenames (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Settings.Settings)SUAVE.Methods.Aerodynamics.AVL.Data.Settings.Settings + flow_symmetry (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Settings.Settings)SUAVE.Methods.Aerodynamics.AVL.Data.Settings.Settings + get_bases(self)SUAVE.Core.Data.Data + itervalues(self)SUAVE.Core.Data.Data + number_control_surfaces (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Settings.Settings)SUAVE.Methods.Aerodynamics.AVL.Data.Settings.Settings + pack_array(self, output='vector')SUAVE.Core.Data.Data + run_cases (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Settings.Settings)SUAVE.Methods.Aerodynamics.AVL.Data.Settings.Settings + typestring(self)SUAVE.Core.Data.Data + unpack_array(self, M)SUAVE.Core.Data.Data + update(self, other)SUAVE.Core.Data.Data + values(self)SUAVE.Core.Data.Data
@@ -130,7 +138,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Settings_1_1Settings.html b/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Settings_1_1Settings.html index d8cf23b7..17121a8b 100644 --- a/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Settings_1_1Settings.html +++ b/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Settings_1_1Settings.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Methods.Aerodynamics.AVL.Data.Settings.Settings Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -106,8 +113,8 @@ SUAVE.Core.Data.Data - -
+ + @@ -120,18 +127,16 @@ - - - - + + - - + + @@ -140,6 +145,8 @@ + + @@ -224,6 +231,8 @@

SUAVE.Core.Data.Data.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface-members.html b/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface-members.html index 542946b2..eb4d45fd 100644 --- a/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface-members.html +++ b/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Member Functions

 
def __delattr__ (self, k)
 
def __defaults__ (self)
 
def __new__ (cls, args, kwarg)
 
def __new__ (cls, *args, **kwarg)
 
def typestring (self)
 
def dataname (self)
 
def __str__ (self, indent='')
 
def __init__ (self, args, kwarg)
 
def __init__ (self, *args, **kwarg)
 
def __iter__ (self)
 
def itervalues (self)
 
def update (self, other)
 
def append_or_update (self, other)
 
def get_bases (self)
 
def append (self, value, key=None)
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -101,28 +108,31 @@ __defaults__(self)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface __delattr__(self, k)SUAVE.Core.Data.Data __getattribute__(self, k)SUAVE.Core.Data.Data - __init__(self, args, kwarg)SUAVE.Core.Data.Data + __init__(self, *args, **kwarg)SUAVE.Core.Data.Data __iter__(self)SUAVE.Core.Data.Data - __new__(cls, args, kwarg)SUAVE.Core.Data.Data + __new__(cls, *args, **kwarg)SUAVE.Core.Data.Data __setattr__(self, k, v)SUAVE.Core.Data.Data __str__(self, indent='')SUAVE.Core.Data.Data append(self, value, key=None)SUAVE.Core.Data.Data - dataname(self)SUAVE.Core.Data.Data - deep_get(self, keys)SUAVE.Core.Data.Data - deep_set(self, keys, val)SUAVE.Core.Data.Data + append_or_update(self, other)SUAVE.Core.Data.Data + dataname(self)SUAVE.Core.Data.Data + deep_get(self, keys)SUAVE.Core.Data.Data + deep_set(self, keys, val)SUAVE.Core.Data.Data + deflection (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface do_recursive(self, method, other=None, default=None)SUAVE.Core.Data.Data - gain (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface - get_bases(self)SUAVE.Core.Data.Data - hinge_vector (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface - itervalues(self)SUAVE.Core.Data.Data - pack_array(self, output='vector')SUAVE.Core.Data.Data - sign_duplicate (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface - tag (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface - typestring(self)SUAVE.Core.Data.Data - unpack_array(self, M)SUAVE.Core.Data.Data - update(self, other)SUAVE.Core.Data.Data - values(self)SUAVE.Core.Data.Data - x_hinge (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface + function (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface + gain (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface + get_bases(self)SUAVE.Core.Data.Data + hinge_vector (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface + itervalues(self)SUAVE.Core.Data.Data + pack_array(self, output='vector')SUAVE.Core.Data.Data + sign_duplicate (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface + tag (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface + typestring(self)SUAVE.Core.Data.Data + unpack_array(self, M)SUAVE.Core.Data.Data + update(self, other)SUAVE.Core.Data.Data + values(self)SUAVE.Core.Data.Data + x_hinge (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface
@@ -130,7 +140,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface.html b/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface.html index 04145b45..8716d038 100644 --- a/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface.html +++ b/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -106,8 +113,8 @@ SUAVE.Core.Data.Data - -
+ + @@ -120,18 +127,16 @@ - - - - + + - - + + @@ -140,6 +145,8 @@ + + @@ -160,12 +167,18 @@ + + + + @@ -174,7 +187,7 @@

Public Member Functions

 
def __delattr__ (self, k)
 
def __defaults__ (self)
 
def __new__ (cls, args, kwarg)
 
def __new__ (cls, *args, **kwarg)
 
def typestring (self)
 
def dataname (self)
 
def __str__ (self, indent='')
 
def __init__ (self, args, kwarg)
 
def __init__ (self, *args, **kwarg)
 
def __iter__ (self)
 
def itervalues (self)
 
def update (self, other)
 
def append_or_update (self, other)
 
def get_bases (self)
 
def append (self, value, key=None)
 tag
 
function
 
 gain
 
 x_hinge
 
deflection
 
 hinge_vector
 
 

Detailed Description

-
A class that defines the control surface geometry and deflection
+
This class defines the control surface geometry and deflection
 on the aircraft wing in AVL
 
 Assumptions:
@@ -225,6 +238,8 @@ 

SUAVE.Core.Data.Data.

+


The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface.js b/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface.js index 47e5548e..22bccc70 100644 --- a/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface.js +++ b/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface.js @@ -1,6 +1,8 @@ var classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface = [ [ "__defaults__", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface.html#ac6c75479876eeb8f1e1b0fa6427c75dd", null ], + [ "deflection", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface.html#ac59fc6184e94e446cb95d292cf9c29c4", null ], + [ "function", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface.html#a021960a9db21e857b79a877cca7a9b43", null ], [ "gain", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface.html#aa1cc6c9fc9019988b3ddbb82a95b2dd2", null ], [ "hinge_vector", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface.html#a4ffdcdedc2d6b764687c9e42940587e2", null ], [ "sign_duplicate", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface.html#a89515ef6de21cda9f08ac9dc4de0f5ba", null ], diff --git a/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface__Data-members.html b/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface__Data-members.html new file mode 100644 index 00000000..fc7b1312 --- /dev/null +++ b/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface__Data-members.html @@ -0,0 +1,143 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface_Data Member List
+
+
+ +

This is the complete list of members for SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface_Data, including all inherited members.

+ + + + + + + + + + + + + + + + + + + + + + + + + +
__defaults__(self)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface_Data
__delattr__(self, k)SUAVE.Core.Data.Data
__getattribute__(self, k)SUAVE.Core.Data.Data
__init__(self, *args, **kwarg)SUAVE.Core.Data.Data
__iter__(self)SUAVE.Core.Data.Data
__new__(cls, *args, **kwarg)SUAVE.Core.Data.Data
__setattr__(self, k, v)SUAVE.Core.Data.Data
__str__(self, indent='')SUAVE.Core.Data.Data
append(self, value, key=None)SUAVE.Core.Data.Data
append_control_surface_result(self, control_res)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface_Data
append_or_update(self, other)SUAVE.Core.Data.Data
control_surfaces (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface_Data)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface_Data
dataname(self)SUAVE.Core.Data.Data
deep_get(self, keys)SUAVE.Core.Data.Data
deep_set(self, keys, val)SUAVE.Core.Data.Data
do_recursive(self, method, other=None, default=None)SUAVE.Core.Data.Data
get_bases(self)SUAVE.Core.Data.Data
itervalues(self)SUAVE.Core.Data.Data
pack_array(self, output='vector')SUAVE.Core.Data.Data
tag (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface_Data)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface_Data
typestring(self)SUAVE.Core.Data.Data
unpack_array(self, M)SUAVE.Core.Data.Data
update(self, other)SUAVE.Core.Data.Data
values(self)SUAVE.Core.Data.Data
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface__Data.html b/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface__Data.html new file mode 100644 index 00000000..59575b40 --- /dev/null +++ b/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface__Data.html @@ -0,0 +1,259 @@ + + + + + + + +SUAVE: SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface_Data Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface_Data Class Reference
+
+
+
+Inheritance diagram for SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface_Data:
+
+
+ + +SUAVE.Core.Data.Data + +
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Member Functions

def __defaults__ (self)
 
def append_control_surface_result (self, control_res)
 
- Public Member Functions inherited from SUAVE.Core.Data.Data
def __getattribute__ (self, k)
 
def __setattr__ (self, k, v)
 
def __delattr__ (self, k)
 
def __new__ (cls, *args, **kwarg)
 
def typestring (self)
 
def dataname (self)
 
def __str__ (self, indent='')
 
def __init__ (self, *args, **kwarg)
 
def __iter__ (self)
 
def itervalues (self)
 
def values (self)
 
def update (self, other)
 
def append_or_update (self, other)
 
def get_bases (self)
 
def append (self, value, key=None)
 
def deep_set (self, keys, val)
 
def deep_get (self, keys)
 
def pack_array (self, output='vector')
 
def unpack_array (self, M)
 
def do_recursive (self, method, other=None, default=None)
 
+ + + + + +

+Public Attributes

tag
 
control_surfaces
 
+

Detailed Description

+
This class stores results from the control surfaces  
+

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface_Data.__defaults__ ( self)
+
+
A stub for all classes that come later
+    
+    Assumptions:
+    N/A
+    
+    Source:
+    N/A
+    
+    Inputs:
+    N/A
+    
+    Outputs:
+    N/A
+    
+    Properties Used:
+    N/A    
+
+

Reimplemented from SUAVE.Core.Data.Data.

+ +
+
+ +

◆ append_control_surface_result()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface_Data.append_control_surface_result ( self,
 control_res 
)
+
+
Adds a control_surface to the wing section in AVL
+
+
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Methods/Aerodynamics/AVL/Data/Wing.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface__Data.js b/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface__Data.js new file mode 100644 index 00000000..0effe954 --- /dev/null +++ b/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface__Data.js @@ -0,0 +1,7 @@ +var classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface__Data = +[ + [ "__defaults__", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface__Data.html#a58d65514f08f56cb07ea2565c6645573", null ], + [ "append_control_surface_result", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface__Data.html#a89f2b8ccce38b82a5edb73b303aae36d", null ], + [ "control_surfaces", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface__Data.html#a095d693f00dd8565641e6915d56c5293", null ], + [ "tag", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface__Data.html#ac8fed5c21954b665cf2417e4c30b5491", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface__Data.png b/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface__Data.png new file mode 100644 index 00000000..7a5746c1 Binary files /dev/null and b/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface__Data.png differ diff --git a/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface__Results-members.html b/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface__Results-members.html new file mode 100644 index 00000000..438d34ca --- /dev/null +++ b/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface__Results-members.html @@ -0,0 +1,149 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface_Results Member List
+
+
+ +

This is the complete list of members for SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface_Results, including all inherited members.

+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
__defaults__(self)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface_Results
__delattr__(self, k)SUAVE.Core.Data.Data
__getattribute__(self, k)SUAVE.Core.Data.Data
__init__(self, *args, **kwarg)SUAVE.Core.Data.Data
__iter__(self)SUAVE.Core.Data.Data
__new__(cls, *args, **kwarg)SUAVE.Core.Data.Data
__setattr__(self, k, v)SUAVE.Core.Data.Data
__str__(self, indent='')SUAVE.Core.Data.Data
append(self, value, key=None)SUAVE.Core.Data.Data
append_or_update(self, other)SUAVE.Core.Data.Data
CDff (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface_Results)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface_Results
Cl (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface_Results)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface_Results
CL (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface_Results)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface_Results
Cm (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface_Results)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface_Results
Cn (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface_Results)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface_Results
CY (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface_Results)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface_Results
dataname(self)SUAVE.Core.Data.Data
deep_get(self, keys)SUAVE.Core.Data.Data
deep_set(self, keys, val)SUAVE.Core.Data.Data
deflection (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface_Results)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface_Results
do_recursive(self, method, other=None, default=None)SUAVE.Core.Data.Data
e (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface_Results)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface_Results
get_bases(self)SUAVE.Core.Data.Data
itervalues(self)SUAVE.Core.Data.Data
pack_array(self, output='vector')SUAVE.Core.Data.Data
tag (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface_Results)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface_Results
typestring(self)SUAVE.Core.Data.Data
unpack_array(self, M)SUAVE.Core.Data.Data
update(self, other)SUAVE.Core.Data.Data
values(self)SUAVE.Core.Data.Data
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface__Results.html b/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface__Results.html new file mode 100644 index 00000000..a4823f88 --- /dev/null +++ b/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface__Results.html @@ -0,0 +1,234 @@ + + + + + + + +SUAVE: SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface_Results Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
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+
+ +
+
+
+ +
+ +
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+ +
+ +
+ +
+
SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface_Results Class Reference
+
+
+
+Inheritance diagram for SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface_Results:
+
+
+ + +SUAVE.Core.Data.Data + +
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Core.Data.Data
def __getattribute__ (self, k)
 
def __setattr__ (self, k, v)
 
def __delattr__ (self, k)
 
def __new__ (cls, *args, **kwarg)
 
def typestring (self)
 
def dataname (self)
 
def __str__ (self, indent='')
 
def __init__ (self, *args, **kwarg)
 
def __iter__ (self)
 
def itervalues (self)
 
def values (self)
 
def update (self, other)
 
def append_or_update (self, other)
 
def get_bases (self)
 
def append (self, value, key=None)
 
def deep_set (self, keys, val)
 
def deep_get (self, keys)
 
def pack_array (self, output='vector')
 
def unpack_array (self, M)
 
def do_recursive (self, method, other=None, default=None)
 
+ + + + + + + + + + + + + + + + + + + +

+Public Attributes

tag
 
deflection
 
CL
 
CY
 
Cl
 
Cm
 
Cn
 
CDff
 
e
 
+

Detailed Description

+
This class defines the control surface geometry and deflection
+

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface_Results.__defaults__ ( self)
+
+
Sets the defaults of the control surface on the aircraft wing
+
+

Reimplemented from SUAVE.Core.Data.Data.

+ +
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Methods/Aerodynamics/AVL/Data/Wing.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface__Results.js b/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface__Results.js new file mode 100644 index 00000000..4116f61e --- /dev/null +++ b/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface__Results.js @@ -0,0 +1,13 @@ +var classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface__Results = +[ + [ "__defaults__", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface__Results.html#abb619aa70223d22d90ff1b4cfc719700", null ], + [ "CDff", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface__Results.html#ae40c5d1ee7dcbd7f8db6dc008eac2a63", null ], + [ "CL", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface__Results.html#a832a813f02c875366b4b3a2c9ea990a1", null ], + [ "Cl", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface__Results.html#ae87e4349057cc991f3d22d1c5acdf472", null ], + [ "Cm", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface__Results.html#ab2d7bd8eb7d2b5e9534d407ab62e268e", null ], + [ "Cn", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface__Results.html#a5d135095f30b10a666a91ec8a1fa1a19", null ], + [ "CY", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface__Results.html#a15ea6613e174bc325a08f93b8afb12b5", null ], + [ "deflection", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface__Results.html#a1ed51afa09a454c0688f88c74d2a5609", null ], + [ "e", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface__Results.html#a92ff5d79055e9bca9eb97a8a5ce295fb", null ], + [ "tag", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface__Results.html#a3ed1ab3e060f19b308674f4ee4638efb", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface__Results.png b/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface__Results.png new file mode 100644 index 00000000..e3d0ada2 Binary files /dev/null and b/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Control__Surface__Results.png differ diff --git a/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Section-members.html b/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Section-members.html index 00b64bf7..a343d108 100644 --- a/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Section-members.html +++ b/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Section-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -101,22 +108,24 @@ __defaults__(self)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Section __delattr__(self, k)SUAVE.Core.Data.Data __getattribute__(self, k)SUAVE.Core.Data.Data - __init__(self, args, kwarg)SUAVE.Core.Data.Data + __init__(self, *args, **kwarg)SUAVE.Core.Data.Data __iter__(self)SUAVE.Core.Data.Data - __new__(cls, args, kwarg)SUAVE.Core.Data.Data + __new__(cls, *args, **kwarg)SUAVE.Core.Data.Data __setattr__(self, k, v)SUAVE.Core.Data.Data __str__(self, indent='')SUAVE.Core.Data.Data airfoil_coord_file (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Section)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Section append(self, value, key=None)SUAVE.Core.Data.Data append_control_surface(self, control)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Section - chord (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Section)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Section - control_surfaces (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Section)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Section - dataname(self)SUAVE.Core.Data.Data - deep_get(self, keys)SUAVE.Core.Data.Data - deep_set(self, keys, val)SUAVE.Core.Data.Data - do_recursive(self, method, other=None, default=None)SUAVE.Core.Data.Data - get_bases(self)SUAVE.Core.Data.Data - itervalues(self)SUAVE.Core.Data.Data + append_or_update(self, other)SUAVE.Core.Data.Data + chord (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Section)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Section + control_surfaces (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Section)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Section + dataname(self)SUAVE.Core.Data.Data + deep_get(self, keys)SUAVE.Core.Data.Data + deep_set(self, keys, val)SUAVE.Core.Data.Data + do_recursive(self, method, other=None, default=None)SUAVE.Core.Data.Data + get_bases(self)SUAVE.Core.Data.Data + itervalues(self)SUAVE.Core.Data.Data + naca_airfoil (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Section)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Section origin (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Section)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Section pack_array(self, output='vector')SUAVE.Core.Data.Data tag (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Section)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Section @@ -132,7 +141,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Section.html b/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Section.html index a0964e5b..064b1b0c 100644 --- a/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Section.html +++ b/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Section.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Section Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -106,8 +113,8 @@ SUAVE.Core.Data.Data - -
+ + @@ -122,18 +129,16 @@ - - - - + + - - + + @@ -142,6 +147,8 @@ + + @@ -171,6 +178,9 @@ + + @@ -179,7 +189,7 @@

Public Member Functions

 
def __delattr__ (self, k)
 
def __defaults__ (self)
 
def __new__ (cls, args, kwarg)
 
def __new__ (cls, *args, **kwarg)
 
def typestring (self)
 
def dataname (self)
 
def __str__ (self, indent='')
 
def __init__ (self, args, kwarg)
 
def __init__ (self, *args, **kwarg)
 
def __iter__ (self)
 
def itervalues (self)
 
def update (self, other)
 
def append_or_update (self, other)
 
def get_bases (self)
 
def append (self, value, key=None)
 twist
 
naca_airfoil
 
 airfoil_coord_file
 
 

Detailed Description

-
A class that defines the sections of the aircraft wing in AVL.
+
This class defines the sections of the aircraft wing in AVL.
 Each section can be thought of as a trapezoid
 
 Assumptions:
@@ -229,6 +239,8 @@ 

SUAVE.Core.Data.Data.

+

@@ -286,7 +298,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Section.js b/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Section.js index 7762420c..6f148c7d 100644 --- a/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Section.js +++ b/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Section.js @@ -5,6 +5,7 @@ var classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Section = [ "airfoil_coord_file", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Section.html#abd0183b7faac5f2c02397afb471aa667", null ], [ "chord", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Section.html#a7b76228bb44c3a1e477439185e428af6", null ], [ "control_surfaces", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Section.html#afc85152833f0c6c44bc1cf9bd960b756", null ], + [ "naca_airfoil", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Section.html#a62572473e0f2954248391fcfd6651905", null ], [ "origin", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Section.html#a1e74b5c3cbee04e629ebf425b6ee75d4", null ], [ "tag", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Section.html#a2e01bb6c59e37d1e6b37571b0709da36", null ], [ "twist", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Section.html#ab9c9fb32b0c7178626a8b105e696064d", null ] diff --git a/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Wing-members.html b/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Wing-members.html index bf109ba3..76a319c6 100644 --- a/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Wing-members.html +++ b/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Wing-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -98,36 +105,37 @@

This is the complete list of members for SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing, including all inherited members.

- + - + - + - - - - - - - - - - - - - - - - - - - - - + + + + + + + + + + + + + + + + + + + + + +
__defaults__(self) (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing
__defaults__(self)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing
__delattr__(self, k)SUAVE.Core.Data.Data
__getattribute__(self, k)SUAVE.Core.Data.Data
__init__(self, args, kwarg)SUAVE.Core.Data.Data
__init__(self, *args, **kwarg)SUAVE.Core.Data.Data
__iter__(self)SUAVE.Core.Data.Data
__new__(cls, args, kwarg)SUAVE.Core.Data.Data
__new__(cls, *args, **kwarg)SUAVE.Core.Data.Data
__setattr__(self, k, v)SUAVE.Core.Data.Data
__str__(self, indent='')SUAVE.Core.Data.Data
append(self, value, key=None)SUAVE.Core.Data.Data
append_section(self, section)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing
configuration (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing
control_surfaces (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing
dataname(self)SUAVE.Core.Data.Data
deep_get(self, keys)SUAVE.Core.Data.Data
deep_set(self, keys, val)SUAVE.Core.Data.Data
dihedral (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing
do_recursive(self, method, other=None, default=None)SUAVE.Core.Data.Data
get_bases(self)SUAVE.Core.Data.Data
itervalues(self)SUAVE.Core.Data.Data
origin (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing
pack_array(self, output='vector')SUAVE.Core.Data.Data
sections (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing
sweep (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing
symmetric (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing
tag (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing
typestring(self)SUAVE.Core.Data.Data
unpack_array(self, M)SUAVE.Core.Data.Data
update(self, other)SUAVE.Core.Data.Data
values(self)SUAVE.Core.Data.Data
vertical (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing
append_or_update(self, other)SUAVE.Core.Data.Data
append_section(self, section)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing
configuration (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing
control_surfaces (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing
dataname(self)SUAVE.Core.Data.Data
deep_get(self, keys)SUAVE.Core.Data.Data
deep_set(self, keys, val)SUAVE.Core.Data.Data
dihedral (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing
do_recursive(self, method, other=None, default=None)SUAVE.Core.Data.Data
get_bases(self)SUAVE.Core.Data.Data
itervalues(self)SUAVE.Core.Data.Data
origin (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing
pack_array(self, output='vector')SUAVE.Core.Data.Data
sections (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing
sweep (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing
symmetric (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing
tag (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing
typestring(self)SUAVE.Core.Data.Data
unpack_array(self, M)SUAVE.Core.Data.Data
update(self, other)SUAVE.Core.Data.Data
values(self)SUAVE.Core.Data.Data
vertical (defined in SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing)SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing
@@ -135,7 +143,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Wing.html b/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Wing.html index e5e48c90..835e8fdf 100644 --- a/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Wing.html +++ b/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Wing_1_1Wing.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -106,13 +113,12 @@ SUAVE.Core.Data.Data - -
+ + - + @@ -123,18 +129,16 @@ - - - - + + - - + + @@ -143,6 +147,8 @@ + + @@ -189,7 +195,7 @@

Public Member Functions

-def __defaults__ (self)
def __defaults__ (self)
 
def append_section (self, section)
 
 
def __delattr__ (self, k)
 
def __defaults__ (self)
 
def __new__ (cls, args, kwarg)
 
def __new__ (cls, *args, **kwarg)
 
def typestring (self)
 
def dataname (self)
 
def __str__ (self, indent='')
 
def __init__ (self, args, kwarg)
 
def __init__ (self, *args, **kwarg)
 
def __iter__ (self)
 
def itervalues (self)
 
def update (self, other)
 
def append_or_update (self, other)
 
def get_bases (self)
 
def append (self, value, key=None)
 

Detailed Description

-
A class that defines parameters of the AVL aircraft wing
+
This class that defines parameters of the AVL aircraft wing
 
 Assumptions:
     None
@@ -206,6 +212,42 @@
 Properties Used:
     N/A
 

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+ + + + + + + + +
def SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing.__defaults__ ( self)
+
+
A stub for all classes that come later
+    
+    Assumptions:
+    N/A
+    
+    Source:
+    N/A
+    
+    Inputs:
+    N/A
+    
+    Outputs:
+    N/A
+    
+    Properties Used:
+    N/A    
+
+

Reimplemented from SUAVE.Core.Data.Data.

+ +
+

◆ append_section()

@@ -231,7 +273,7 @@

-
adds a segment to the wing 
+
Adds a segment to the wing 


The documentation for this class was generated from the following file:
diff --git a/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1Supersonic__Zero_1_1Drag_1_1Cubic__Spline__Blender_1_1Cubic__Spline__Blender-members.html b/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1Supersonic__Zero_1_1Drag_1_1Cubic__Spline__Blender_1_1Cubic__Spline__Blender-members.html new file mode 100644 index 00000000..5858a30b --- /dev/null +++ b/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1Supersonic__Zero_1_1Drag_1_1Cubic__Spline__Blender_1_1Cubic__Spline__Blender-members.html @@ -0,0 +1,124 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ + + + + + diff --git a/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1Supersonic__Zero_1_1Drag_1_1Cubic__Spline__Blender_1_1Cubic__Spline__Blender.html b/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1Supersonic__Zero_1_1Drag_1_1Cubic__Spline__Blender_1_1Cubic__Spline__Blender.html new file mode 100644 index 00000000..a66b372c --- /dev/null +++ b/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1Supersonic__Zero_1_1Drag_1_1Cubic__Spline__Blender_1_1Cubic__Spline__Blender.html @@ -0,0 +1,293 @@ + + + + + + + +SUAVE: SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.Cubic_Spline_Blender.Cubic_Spline_Blender Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.Cubic_Spline_Blender.Cubic_Spline_Blender Class Reference
+
+
+ + + + + + + + +

+Public Member Functions

def __init__ (self, x_start, x_end)
 
def compute (self, x)
 
def eta_transform (self, x)
 
+ + + + + +

+Public Attributes

x_start
 
x_end
 
+

Detailed Description

+
This is a cubic spline function that can be used to blend two type of calculations
+without knowing the end points. It preserves continuous first derivatives.
+
+Assumptions:
+None
+
+Source:
+Information at:
+https://en.wikipedia.org/wiki/Cubic_Hermite_spline
+

Constructor & Destructor Documentation

+ +

◆ __init__()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.Cubic_Spline_Blender.Cubic_Spline_Blender.__init__ ( self,
 x_start,
 x_end 
)
+
+
This sets the default start and end position.
+
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+None
+
+Outputs:
+None
+
+Properties Used:
+N/A
+
+
+
+

Member Function Documentation

+ +

◆ compute()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.Cubic_Spline_Blender.Cubic_Spline_Blender.compute ( self,
 x 
)
+
+
This computes the y value along a normalized spline
+
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+None
+
+Outputs:
+None
+
+Properties Used:
+N/A
+
+
+
+ +

◆ eta_transform()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.Cubic_Spline_Blender.Cubic_Spline_Blender.eta_transform ( self,
 x 
)
+
+
Normalizes the transformation
+
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+None
+
+Outputs:
+None
+
+Properties Used:
+N/A
+
+
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Methods/Aerodynamics/Supersonic_Zero/Drag/Cubic_Spline_Blender.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1Supersonic__Zero_1_1Drag_1_1Cubic__Spline__Blender_1_1Cubic__Spline__Blender.js b/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1Supersonic__Zero_1_1Drag_1_1Cubic__Spline__Blender_1_1Cubic__Spline__Blender.js new file mode 100644 index 00000000..21979157 --- /dev/null +++ b/doxygen/classSUAVE_1_1Methods_1_1Aerodynamics_1_1Supersonic__Zero_1_1Drag_1_1Cubic__Spline__Blender_1_1Cubic__Spline__Blender.js @@ -0,0 +1,8 @@ +var classSUAVE_1_1Methods_1_1Aerodynamics_1_1Supersonic__Zero_1_1Drag_1_1Cubic__Spline__Blender_1_1Cubic__Spline__Blender = +[ + [ "__init__", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1Supersonic__Zero_1_1Drag_1_1Cubic__Spline__Blender_1_1Cubic__Spline__Blender.html#afff7a719089ea8178f152d196ea2ec0f", null ], + [ "compute", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1Supersonic__Zero_1_1Drag_1_1Cubic__Spline__Blender_1_1Cubic__Spline__Blender.html#aeb32772385d70b536506f803147dc5c2", null ], + [ "eta_transform", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1Supersonic__Zero_1_1Drag_1_1Cubic__Spline__Blender_1_1Cubic__Spline__Blender.html#a6017f424807c71a3deab1c81eef3de17", null ], + [ "x_end", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1Supersonic__Zero_1_1Drag_1_1Cubic__Spline__Blender_1_1Cubic__Spline__Blender.html#ad4de563711c610b928bccdb2cf3228d5", null ], + [ "x_start", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1Supersonic__Zero_1_1Drag_1_1Cubic__Spline__Blender_1_1Cubic__Spline__Blender.html#a7f59c602476376ec2264aafb29085321", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Methods_1_1Utilities_1_1Cubic__Spline__Blender_1_1Cubic__Spline__Blender-members.html b/doxygen/classSUAVE_1_1Methods_1_1Utilities_1_1Cubic__Spline__Blender_1_1Cubic__Spline__Blender-members.html new file mode 100644 index 00000000..f0802491 --- /dev/null +++ b/doxygen/classSUAVE_1_1Methods_1_1Utilities_1_1Cubic__Spline__Blender_1_1Cubic__Spline__Blender-members.html @@ -0,0 +1,124 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ + + + + + diff --git a/doxygen/classSUAVE_1_1Methods_1_1Utilities_1_1Cubic__Spline__Blender_1_1Cubic__Spline__Blender.html b/doxygen/classSUAVE_1_1Methods_1_1Utilities_1_1Cubic__Spline__Blender_1_1Cubic__Spline__Blender.html new file mode 100644 index 00000000..4dadbccd --- /dev/null +++ b/doxygen/classSUAVE_1_1Methods_1_1Utilities_1_1Cubic__Spline__Blender_1_1Cubic__Spline__Blender.html @@ -0,0 +1,293 @@ + + + + + + + +SUAVE: SUAVE.Methods.Utilities.Cubic_Spline_Blender.Cubic_Spline_Blender Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Methods.Utilities.Cubic_Spline_Blender.Cubic_Spline_Blender Class Reference
+
+
+ + + + + + + + +

+Public Member Functions

def __init__ (self, x_start, x_end)
 
def compute (self, x)
 
def eta_transform (self, x)
 
+ + + + + +

+Public Attributes

x_start
 
x_end
 
+

Detailed Description

+
This is a cubic spline function that can be used to blend two type of calculations
+without knowing the end points. It preserves continuous first derivatives.
+
+Assumptions:
+None
+
+Source:
+Information at:
+https://en.wikipedia.org/wiki/Cubic_Hermite_spline
+

Constructor & Destructor Documentation

+ +

◆ __init__()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Utilities.Cubic_Spline_Blender.Cubic_Spline_Blender.__init__ ( self,
 x_start,
 x_end 
)
+
+
This sets the default start and end position.
+
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+None
+
+Outputs:
+None
+
+Properties Used:
+N/A
+
+
+
+

Member Function Documentation

+ +

◆ compute()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Utilities.Cubic_Spline_Blender.Cubic_Spline_Blender.compute ( self,
 x 
)
+
+
This computes the y value along a normalized spline
+
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+None
+
+Outputs:
+None
+
+Properties Used:
+N/A
+
+
+
+ +

◆ eta_transform()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Utilities.Cubic_Spline_Blender.Cubic_Spline_Blender.eta_transform ( self,
 x 
)
+
+
Normalizes the transformation
+
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+None
+
+Outputs:
+None
+
+Properties Used:
+N/A
+
+
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Methods/Utilities/Cubic_Spline_Blender.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Methods_1_1Utilities_1_1Cubic__Spline__Blender_1_1Cubic__Spline__Blender.js b/doxygen/classSUAVE_1_1Methods_1_1Utilities_1_1Cubic__Spline__Blender_1_1Cubic__Spline__Blender.js new file mode 100644 index 00000000..56e5ef52 --- /dev/null +++ b/doxygen/classSUAVE_1_1Methods_1_1Utilities_1_1Cubic__Spline__Blender_1_1Cubic__Spline__Blender.js @@ -0,0 +1,8 @@ +var classSUAVE_1_1Methods_1_1Utilities_1_1Cubic__Spline__Blender_1_1Cubic__Spline__Blender = +[ + [ "__init__", "classSUAVE_1_1Methods_1_1Utilities_1_1Cubic__Spline__Blender_1_1Cubic__Spline__Blender.html#ac62246c89508c2a196d9a12c42241f4a", null ], + [ "compute", "classSUAVE_1_1Methods_1_1Utilities_1_1Cubic__Spline__Blender_1_1Cubic__Spline__Blender.html#aa80ca48b142c80fe3d791547f6dce500", null ], + [ "eta_transform", "classSUAVE_1_1Methods_1_1Utilities_1_1Cubic__Spline__Blender_1_1Cubic__Spline__Blender.html#a97b32ecf60f95d6bf842e8b5edfe39fe", null ], + [ "x_end", "classSUAVE_1_1Methods_1_1Utilities_1_1Cubic__Spline__Blender_1_1Cubic__Spline__Blender.html#a6f68ca2fc9f111d4d650b0da00a659ae", null ], + [ "x_start", "classSUAVE_1_1Methods_1_1Utilities_1_1Cubic__Spline__Blender_1_1Cubic__Spline__Blender.html#a4fedebf819716f0167c524f75689caf4", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Optimization_1_1Nexus_1_1Nexus-members.html b/doxygen/classSUAVE_1_1Optimization_1_1Nexus_1_1Nexus-members.html index df6b0803..bb7d02e4 100644 --- a/doxygen/classSUAVE_1_1Optimization_1_1Nexus_1_1Nexus-members.html +++ b/doxygen/classSUAVE_1_1Optimization_1_1Nexus_1_1Nexus-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -101,43 +108,46 @@ __defaults__(self)SUAVE.Optimization.Nexus.Nexus __delattr__(self, k)SUAVE.Core.Data.Data __getattribute__(self, k)SUAVE.Core.Data.Data - __init__(self, args, kwarg)SUAVE.Core.Data.Data + __init__(self, *args, **kwarg)SUAVE.Core.Data.Data __iter__(self)SUAVE.Core.Data.Data - __new__(cls, args, kwarg)SUAVE.Core.Data.Data + __new__(cls, *args, **kwarg)SUAVE.Core.Data.Data __setattr__(self, k, v)SUAVE.Core.Data.Data __str__(self, indent='')SUAVE.Core.Data.Data all_constraints(self, x=None)SUAVE.Optimization.Nexus.Nexus analyses (defined in SUAVE.Optimization.Nexus.Nexus)SUAVE.Optimization.Nexus.Nexus append(self, value, key=None)SUAVE.Core.Data.Data - constraints_individual(self, x=None)SUAVE.Optimization.Nexus.Nexus - dataname(self)SUAVE.Core.Data.Data - deep_get(self, keys)SUAVE.Core.Data.Data - deep_set(self, keys, val)SUAVE.Core.Data.Data - do_recursive(self, method, other=None, default=None)SUAVE.Core.Data.Data - equality_constraint(self, x=None)SUAVE.Optimization.Nexus.Nexus - evaluate(self, x=None)SUAVE.Optimization.Nexus.Nexus - evaluation_count (defined in SUAVE.Optimization.Nexus.Nexus)SUAVE.Optimization.Nexus.Nexus - fidelity_level (defined in SUAVE.Optimization.Nexus.Nexus)SUAVE.Optimization.Nexus.Nexus - finite_difference(self, x, diff_interval=1e-8)SUAVE.Optimization.Nexus.Nexus + append_or_update(self, other)SUAVE.Core.Data.Data + constraints_individual(self, x=None)SUAVE.Optimization.Nexus.Nexus + dataname(self)SUAVE.Core.Data.Data + deep_get(self, keys)SUAVE.Core.Data.Data + deep_set(self, keys, val)SUAVE.Core.Data.Data + do_recursive(self, method, other=None, default=None)SUAVE.Core.Data.Data + equality_constraint(self, x=None)SUAVE.Optimization.Nexus.Nexus + evaluate(self, x=None)SUAVE.Optimization.Nexus.Nexus + evaluation_count (defined in SUAVE.Optimization.Nexus.Nexus)SUAVE.Optimization.Nexus.Nexus + fidelity_level (defined in SUAVE.Optimization.Nexus.Nexus)SUAVE.Optimization.Nexus.Nexus + finite_difference(self, x, diff_interval=1e-8)SUAVE.Optimization.Nexus.Nexus + force_evaluate (defined in SUAVE.Optimization.Nexus.Nexus)SUAVE.Optimization.Nexus.Nexus get_bases(self)SUAVE.Core.Data.Data - inequality_constraint(self, x=None)SUAVE.Optimization.Nexus.Nexus - itervalues(self)SUAVE.Core.Data.Data - last_fidelity (defined in SUAVE.Optimization.Nexus.Nexus)SUAVE.Optimization.Nexus.Nexus - last_inputs (defined in SUAVE.Optimization.Nexus.Nexus)SUAVE.Optimization.Nexus.Nexus - missions (defined in SUAVE.Optimization.Nexus.Nexus)SUAVE.Optimization.Nexus.Nexus - objective(self, x=None)SUAVE.Optimization.Nexus.Nexus - optimization_problem (defined in SUAVE.Optimization.Nexus.Nexus)SUAVE.Optimization.Nexus.Nexus - pack_array(self, output='vector')SUAVE.Core.Data.Data - procedure (defined in SUAVE.Optimization.Nexus.Nexus)SUAVE.Optimization.Nexus.Nexus - results (defined in SUAVE.Optimization.Nexus.Nexus)SUAVE.Optimization.Nexus.Nexus - summary (defined in SUAVE.Optimization.Nexus.Nexus)SUAVE.Optimization.Nexus.Nexus - translate(self, x=None)SUAVE.Optimization.Nexus.Nexus - typestring(self)SUAVE.Core.Data.Data - unpack_array(self, M)SUAVE.Core.Data.Data - unpack_inputs(self, x=None)SUAVE.Optimization.Nexus.Nexus - update(self, other)SUAVE.Core.Data.Data - values(self)SUAVE.Core.Data.Data - vehicle_configurations (defined in SUAVE.Optimization.Nexus.Nexus)SUAVE.Optimization.Nexus.Nexus + hard_bounded_inputs (defined in SUAVE.Optimization.Nexus.Nexus)SUAVE.Optimization.Nexus.Nexus + inequality_constraint(self, x=None)SUAVE.Optimization.Nexus.Nexus + itervalues(self)SUAVE.Core.Data.Data + last_fidelity (defined in SUAVE.Optimization.Nexus.Nexus)SUAVE.Optimization.Nexus.Nexus + last_inputs (defined in SUAVE.Optimization.Nexus.Nexus)SUAVE.Optimization.Nexus.Nexus + missions (defined in SUAVE.Optimization.Nexus.Nexus)SUAVE.Optimization.Nexus.Nexus + objective(self, x=None)SUAVE.Optimization.Nexus.Nexus + optimization_problem (defined in SUAVE.Optimization.Nexus.Nexus)SUAVE.Optimization.Nexus.Nexus + pack_array(self, output='vector')SUAVE.Core.Data.Data + procedure (defined in SUAVE.Optimization.Nexus.Nexus)SUAVE.Optimization.Nexus.Nexus + results (defined in SUAVE.Optimization.Nexus.Nexus)SUAVE.Optimization.Nexus.Nexus + summary (defined in SUAVE.Optimization.Nexus.Nexus)SUAVE.Optimization.Nexus.Nexus + translate(self, x=None)SUAVE.Optimization.Nexus.Nexus + typestring(self)SUAVE.Core.Data.Data + unpack_array(self, M)SUAVE.Core.Data.Data + unpack_inputs(self, x=None)SUAVE.Optimization.Nexus.Nexus + update(self, other)SUAVE.Core.Data.Data + values(self)SUAVE.Core.Data.Data + vehicle_configurations (defined in SUAVE.Optimization.Nexus.Nexus)SUAVE.Optimization.Nexus.Nexus
@@ -145,7 +155,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Optimization_1_1Nexus_1_1Nexus.html b/doxygen/classSUAVE_1_1Optimization_1_1Nexus_1_1Nexus.html index 3a807b3c..7d23d62a 100644 --- a/doxygen/classSUAVE_1_1Optimization_1_1Nexus_1_1Nexus.html +++ b/doxygen/classSUAVE_1_1Optimization_1_1Nexus_1_1Nexus.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Optimization.Nexus.Nexus Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -106,8 +113,8 @@ SUAVE.Core.Data.Data - -
+ + @@ -138,18 +145,16 @@ - - - - + + - - + + @@ -158,6 +163,8 @@ + + @@ -208,6 +215,12 @@ + + + +

Public Member Functions

 
def __delattr__ (self, k)
 
def __defaults__ (self)
 
def __new__ (cls, args, kwarg)
 
def __new__ (cls, *args, **kwarg)
 
def typestring (self)
 
def dataname (self)
 
def __str__ (self, indent='')
 
def __init__ (self, args, kwarg)
 
def __init__ (self, *args, **kwarg)
 
def __iter__ (self)
 
def itervalues (self)
 
def update (self, other)
 
def append_or_update (self, other)
 
def get_bases (self)
 
def append (self, value, key=None)
 evaluation_count
 
force_evaluate
 
hard_bounded_inputs
 

Detailed Description

noun (plural same or nexuses)
@@ -256,6 +269,8 @@ 

SUAVE.Core.Data.Data.

+

@@ -674,7 +689,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Optimization_1_1Nexus_1_1Nexus.js b/doxygen/classSUAVE_1_1Optimization_1_1Nexus_1_1Nexus.js index e7829923..8f6e0afb 100644 --- a/doxygen/classSUAVE_1_1Optimization_1_1Nexus_1_1Nexus.js +++ b/doxygen/classSUAVE_1_1Optimization_1_1Nexus_1_1Nexus.js @@ -13,6 +13,8 @@ var classSUAVE_1_1Optimization_1_1Nexus_1_1Nexus = [ "analyses", "classSUAVE_1_1Optimization_1_1Nexus_1_1Nexus.html#a7540bae0fa705aedd67732e6a4f2fd03", null ], [ "evaluation_count", "classSUAVE_1_1Optimization_1_1Nexus_1_1Nexus.html#a0e0a0b0d2ba3e3cd1381569156f1f2ff", null ], [ "fidelity_level", "classSUAVE_1_1Optimization_1_1Nexus_1_1Nexus.html#aea9b128c29d6dc551ac15263d0e2267c", null ], + [ "force_evaluate", "classSUAVE_1_1Optimization_1_1Nexus_1_1Nexus.html#a1b71ecd9205cdee6e020beb50922e180", null ], + [ "hard_bounded_inputs", "classSUAVE_1_1Optimization_1_1Nexus_1_1Nexus.html#a9b62669b43a4ee0837fb3c0b689b4baa", null ], [ "last_fidelity", "classSUAVE_1_1Optimization_1_1Nexus_1_1Nexus.html#ac4c2045d9bc469e48c23a7b5f96ecb84", null ], [ "last_inputs", "classSUAVE_1_1Optimization_1_1Nexus_1_1Nexus.html#a4a62b5f7d690c3b4390ccd4f54fd6a45", null ], [ "missions", "classSUAVE_1_1Optimization_1_1Nexus_1_1Nexus.html#a3b13fe94b3835bb58af3aca92ec95a16", null ], diff --git a/doxygen/classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region_1_1Trust__Region-members.html b/doxygen/classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region_1_1Trust__Region-members.html index 1bec311b..b9def6e3 100644 --- a/doxygen/classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region_1_1Trust__Region-members.html +++ b/doxygen/classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region_1_1Trust__Region-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -101,31 +108,32 @@ __defaults__(self)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region.Trust_Region __delattr__(self, k)SUAVE.Core.Data.Data __getattribute__(self, k)SUAVE.Core.Data.Data - __init__(self, args, kwarg)SUAVE.Core.Data.Data + __init__(self, *args, **kwarg)SUAVE.Core.Data.Data __iter__(self)SUAVE.Core.Data.Data - __new__(cls, args, kwarg)SUAVE.Core.Data.Data + __new__(cls, *args, **kwarg)SUAVE.Core.Data.Data __setattr__(self, k, v)SUAVE.Core.Data.Data __str__(self, indent='')SUAVE.Core.Data.Data append(self, value, key=None)SUAVE.Core.Data.Data - contract_threshold (defined in SUAVE.Optimization.Package_Setups.TRMM.Trust_Region.Trust_Region)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region.Trust_Region - contraction_factor (defined in SUAVE.Optimization.Package_Setups.TRMM.Trust_Region.Trust_Region)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region.Trust_Region - dataname(self)SUAVE.Core.Data.Data - deep_get(self, keys)SUAVE.Core.Data.Data - deep_set(self, keys, val)SUAVE.Core.Data.Data - do_recursive(self, method, other=None, default=None)SUAVE.Core.Data.Data - evaluate_function(self, f, gviol)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region.Trust_Region - expand_threshold (defined in SUAVE.Optimization.Package_Setups.TRMM.Trust_Region.Trust_Region)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region.Trust_Region - expansion_factor (defined in SUAVE.Optimization.Package_Setups.TRMM.Trust_Region.Trust_Region)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region.Trust_Region - get_bases(self)SUAVE.Core.Data.Data - initial_size (defined in SUAVE.Optimization.Package_Setups.TRMM.Trust_Region.Trust_Region)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region.Trust_Region - itervalues(self)SUAVE.Core.Data.Data - minimum_size (defined in SUAVE.Optimization.Package_Setups.TRMM.Trust_Region.Trust_Region)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region.Trust_Region - pack_array(self, output='vector')SUAVE.Core.Data.Data - size (defined in SUAVE.Optimization.Package_Setups.TRMM.Trust_Region.Trust_Region)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region.Trust_Region - typestring(self)SUAVE.Core.Data.Data - unpack_array(self, M)SUAVE.Core.Data.Data - update(self, other)SUAVE.Core.Data.Data - values(self)SUAVE.Core.Data.Data + append_or_update(self, other)SUAVE.Core.Data.Data + contract_threshold (defined in SUAVE.Optimization.Package_Setups.TRMM.Trust_Region.Trust_Region)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region.Trust_Region + contraction_factor (defined in SUAVE.Optimization.Package_Setups.TRMM.Trust_Region.Trust_Region)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region.Trust_Region + dataname(self)SUAVE.Core.Data.Data + deep_get(self, keys)SUAVE.Core.Data.Data + deep_set(self, keys, val)SUAVE.Core.Data.Data + do_recursive(self, method, other=None, default=None)SUAVE.Core.Data.Data + evaluate_function(self, f, gviol)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region.Trust_Region + expand_threshold (defined in SUAVE.Optimization.Package_Setups.TRMM.Trust_Region.Trust_Region)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region.Trust_Region + expansion_factor (defined in SUAVE.Optimization.Package_Setups.TRMM.Trust_Region.Trust_Region)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region.Trust_Region + get_bases(self)SUAVE.Core.Data.Data + initial_size (defined in SUAVE.Optimization.Package_Setups.TRMM.Trust_Region.Trust_Region)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region.Trust_Region + itervalues(self)SUAVE.Core.Data.Data + minimum_size (defined in SUAVE.Optimization.Package_Setups.TRMM.Trust_Region.Trust_Region)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region.Trust_Region + pack_array(self, output='vector')SUAVE.Core.Data.Data + size (defined in SUAVE.Optimization.Package_Setups.TRMM.Trust_Region.Trust_Region)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region.Trust_Region + typestring(self)SUAVE.Core.Data.Data + unpack_array(self, M)SUAVE.Core.Data.Data + update(self, other)SUAVE.Core.Data.Data + values(self)SUAVE.Core.Data.Data
@@ -133,7 +141,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region_1_1Trust__Region.html b/doxygen/classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region_1_1Trust__Region.html index 052fbb10..b99eea1a 100644 --- a/doxygen/classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region_1_1Trust__Region.html +++ b/doxygen/classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region_1_1Trust__Region.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Optimization.Package_Setups.TRMM.Trust_Region.Trust_Region Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -106,8 +113,8 @@ SUAVE.Core.Data.Data - -
+ + @@ -122,18 +129,16 @@ - - - - + + - - + + @@ -142,6 +147,8 @@ + + @@ -221,6 +228,8 @@

SUAVE.Core.Data.Data.

+ @@ -285,7 +294,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region__Optimization_1_1Trust__Region__Optimization-members.html b/doxygen/classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region__Optimization_1_1Trust__Region__Optimization-members.html index ea04db6c..704ad2e6 100644 --- a/doxygen/classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region__Optimization_1_1Trust__Region__Optimization-members.html +++ b/doxygen/classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region__Optimization_1_1Trust__Region__Optimization-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Member Functions

 
def __delattr__ (self, k)
 
def __defaults__ (self)
 
def __new__ (cls, args, kwarg)
 
def __new__ (cls, *args, **kwarg)
 
def typestring (self)
 
def dataname (self)
 
def __str__ (self, indent='')
 
def __init__ (self, args, kwarg)
 
def __init__ (self, *args, **kwarg)
 
def __iter__ (self)
 
def itervalues (self)
 
def update (self, other)
 
def append_or_update (self, other)
 
def get_bases (self)
 
def append (self, value, key=None)
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -101,27 +108,29 @@ __defaults__(self)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization __delattr__(self, k)SUAVE.Core.Data.Data __getattribute__(self, k)SUAVE.Core.Data.Data - __init__(self, args, kwarg)SUAVE.Core.Data.Data + __init__(self, *args, **kwarg)SUAVE.Core.Data.Data __iter__(self)SUAVE.Core.Data.Data - __new__(cls, args, kwarg)SUAVE.Core.Data.Data + __new__(cls, *args, **kwarg)SUAVE.Core.Data.Data __setattr__(self, k, v)SUAVE.Core.Data.Data __str__(self, indent='')SUAVE.Core.Data.Data accuracy_ratio(self, f_center, f_hi, f_corr, g_viol_center, g_viol_hi, g_viol_corr, tr)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization append(self, value, key=None)SUAVE.Core.Data.Data - calculate_constraint_violation(self, gval, lb, ub)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization - calculate_correction(self, f, df, g, dg, tr)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization - convergence_tolerance (defined in SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization - dataname(self)SUAVE.Core.Data.Data - deep_get(self, keys)SUAVE.Core.Data.Data - deep_set(self, keys, val)SUAVE.Core.Data.Data - difference_interval (defined in SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization - do_recursive(self, method, other=None, default=None)SUAVE.Core.Data.Data - evaluate_constraints(self, x, problem=None, corrections=None, tr=None, lb=None, ub=None)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization - evaluate_corrected_model(self, x, problem=None, corrections=None, tr=None)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization - evaluate_model(self, problem, x, der_flag=True)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization - evaluation_order (defined in SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization - fidelity_levels (defined in SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization - get_bases(self)SUAVE.Core.Data.Data + append_or_update(self, other)SUAVE.Core.Data.Data + calculate_constraint_violation(self, gval, lb, ub)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization + calculate_correction(self, f, df, g, dg, tr)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization + convergence_tolerance (defined in SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization + dataname(self)SUAVE.Core.Data.Data + deep_get(self, keys)SUAVE.Core.Data.Data + deep_set(self, keys, val)SUAVE.Core.Data.Data + difference_interval (defined in SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization + do_recursive(self, method, other=None, default=None)SUAVE.Core.Data.Data + evaluate_constraints(self, x, problem=None, corrections=None, tr=None, lb=None, ub=None)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization + evaluate_corrected_model(self, x, problem=None, corrections=None, tr=None, return_cons=False)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization + evaluate_model(self, problem, x, der_flag=True)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization + evaluation_order (defined in SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization + fidelity_levels (defined in SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization + get_bases(self)SUAVE.Core.Data.Data + initialize_SLSQP_constraints(self, con, problem, corrections, tr) (defined in SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization itervalues(self)SUAVE.Core.Data.Data optimize(self, problem, print_output=False)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization optimizer (defined in SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization @@ -137,9 +146,10 @@ trust_region_max_iterations (defined in SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization typestring(self)SUAVE.Core.Data.Data unpack_array(self, M)SUAVE.Core.Data.Data - update(self, other)SUAVE.Core.Data.Data - update_tr_size(self, rho, tr, accepted)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization - values(self)SUAVE.Core.Data.Data + unpack_constraints_slsqp(self, x, con_ind, sign, edge, problem, corrections, tr) (defined in SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization + update(self, other)SUAVE.Core.Data.Data + update_tr_size(self, rho, tr, accepted)SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization + values(self)SUAVE.Core.Data.Data
@@ -147,7 +157,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region__Optimization_1_1Trust__Region__Optimization.html b/doxygen/classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region__Optimization_1_1Trust__Region__Optimization.html index b937fce7..58335038 100644 --- a/doxygen/classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region__Optimization_1_1Trust__Region__Optimization.html +++ b/doxygen/classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region__Optimization_1_1Trust__Region__Optimization.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization.Trust_Region_Optimization Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -106,8 +113,8 @@ SUAVE.Core.Data.Data - -
+ + @@ -117,8 +124,8 @@ - - + + @@ -131,6 +138,12 @@ + + + + @@ -138,18 +151,16 @@ - - - - + + - - + + @@ -158,6 +169,8 @@ + + @@ -256,6 +269,8 @@

SUAVE.Core.Data.Data.

+ @@ -556,8 +571,8 @@

-

◆ evaluate_corrected_model()

+ +

◆ evaluate_corrected_model()

@@ -590,7 +605,13 @@

- + + + + + + + @@ -918,7 +939,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region__Optimization_1_1Trust__Region__Optimization.js b/doxygen/classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region__Optimization_1_1Trust__Region__Optimization.js index 1657312b..96b9c198 100644 --- a/doxygen/classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region__Optimization_1_1Trust__Region__Optimization.js +++ b/doxygen/classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region__Optimization_1_1Trust__Region__Optimization.js @@ -5,10 +5,12 @@ var classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region__Opti [ "calculate_constraint_violation", "classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region__Optimization_1_1Trust__Region__Optimization.html#ae762fcbbe9ff61309c645680cf7ac24b", null ], [ "calculate_correction", "classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region__Optimization_1_1Trust__Region__Optimization.html#a8acaabb3bd8cb0d67d6d33dd69f4cb2f", null ], [ "evaluate_constraints", "classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region__Optimization_1_1Trust__Region__Optimization.html#acba95060955b293232cd7215397584c4", null ], - [ "evaluate_corrected_model", "classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region__Optimization_1_1Trust__Region__Optimization.html#a4714077a34faa3add6305b6aa14bd62c", null ], + [ "evaluate_corrected_model", "classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region__Optimization_1_1Trust__Region__Optimization.html#a8fe6735c35a588f86fd7326acd12ebaa", null ], [ "evaluate_model", "classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region__Optimization_1_1Trust__Region__Optimization.html#ac182b46b7d513c7745520f5421cc4cd4", null ], + [ "initialize_SLSQP_constraints", "classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region__Optimization_1_1Trust__Region__Optimization.html#af674f5240a676b1ce0b7bfd06458ff31", null ], [ "optimize", "classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region__Optimization_1_1Trust__Region__Optimization.html#a41444575f97d7ce4a60ab05e25d4c39f", null ], [ "scale_vals", "classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region__Optimization_1_1Trust__Region__Optimization.html#a9a074a8e7cf8603b560333fd309fd8d3", null ], + [ "unpack_constraints_slsqp", "classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region__Optimization_1_1Trust__Region__Optimization.html#a01877d2aec26bbe67846e72c0fcd2d1b", null ], [ "update_tr_size", "classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region__Optimization_1_1Trust__Region__Optimization.html#a8b053bf1bf439b9e0a7c152b8b1b7faf", null ], [ "convergence_tolerance", "classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region__Optimization_1_1Trust__Region__Optimization.html#ace708c4c014c74e98e33a590a280b661", null ], [ "difference_interval", "classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region__Optimization_1_1Trust__Region__Optimization.html#ad3226034b0686052ff6e865e19443e73", null ], diff --git a/doxygen/classSUAVE_1_1Optimization_1_1Package__Setups_1_1additive__setup_1_1Additive__Solver-members.html b/doxygen/classSUAVE_1_1Optimization_1_1Package__Setups_1_1additive__setup_1_1Additive__Solver-members.html new file mode 100644 index 00000000..ffb79883 --- /dev/null +++ b/doxygen/classSUAVE_1_1Optimization_1_1Package__Setups_1_1additive__setup_1_1Additive__Solver-members.html @@ -0,0 +1,134 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+

Public Member Functions

 
def evaluate_model (self, problem, x, der_flag=True)
 
def evaluate_corrected_model (self, x, problem=None, corrections=None, tr=None)
 
def evaluate_corrected_model (self, x, problem=None, corrections=None, tr=None, return_cons=False)
 
def evaluate_constraints (self, x, problem=None, corrections=None, tr=None, lb=None, ub=None)
 
def calculate_constraint_violation (self, gval, lb, ub)
 
def update_tr_size (self, rho, tr, accepted)
 
+def initialize_SLSQP_constraints (self, con, problem, corrections, tr)
 
+def unpack_constraints_slsqp (self, x, con_ind, sign, edge, problem, corrections, tr)
 
- Public Member Functions inherited from SUAVE.Core.Data.Data
def __getattribute__ (self, k)
 
 
def __delattr__ (self, k)
 
def __defaults__ (self)
 
def __new__ (cls, args, kwarg)
 
def __new__ (cls, *args, **kwarg)
 
def typestring (self)
 
def dataname (self)
 
def __str__ (self, indent='')
 
def __init__ (self, args, kwarg)
 
def __init__ (self, *args, **kwarg)
 
def __iter__ (self)
 
def itervalues (self)
 
def update (self, other)
 
def append_or_update (self, other)
 
def get_bases (self)
 
def append (self, value, key=None)
 tr = None tr = None,
 return_cons = False 
+ + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
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SUAVE.Optimization.Package_Setups.additive_setup.Additive_Solver Member List
+
+
+ +

This is the complete list of members for SUAVE.Optimization.Package_Setups.additive_setup.Additive_Solver, including all inherited members.

+ + + + + + + + + + + + + + + + +
__init__(self) (defined in SUAVE.Optimization.Package_Setups.additive_setup.Additive_Solver)SUAVE.Optimization.Package_Setups.additive_setup.Additive_Solver
Additive_Solve(self, problem, num_fidelity_levels=2, num_samples=10, max_iterations=10, tolerance=1e-6, opt_type='basic', num_starts=3, print_output=True)SUAVE.Optimization.Package_Setups.additive_setup.Additive_Solver
const_list (defined in SUAVE.Optimization.Package_Setups.additive_setup.Additive_Solver)SUAVE.Optimization.Package_Setups.additive_setup.Additive_Solver
evaluate_corrected_model(self, x, problem=None, obj_surrogate=None, cons_surrogate=None)SUAVE.Optimization.Package_Setups.additive_setup.Additive_Solver
evaluate_expected_improvement(self, x, problem=None, obj_surrogate=None, cons_surrogate=None, fstar=np.inf, cons=None)SUAVE.Optimization.Package_Setups.additive_setup.Additive_Solver
evaluate_model(self, problem, x, cons)SUAVE.Optimization.Package_Setups.additive_setup.Additive_Solver
expected_improvement_carpet(self, lbs, ubs, problem, obj_surrogate, cons_surrogate, fstar, show_log_improvement=False)SUAVE.Optimization.Package_Setups.additive_setup.Additive_Solver
global_optimizer (defined in SUAVE.Optimization.Package_Setups.additive_setup.Additive_Solver)SUAVE.Optimization.Package_Setups.additive_setup.Additive_Solver
initialize_opt_vals(self, opt_prob, obj, inp, x_low_bound, x_up_bound, con_low_edge, con_up_edge, nam, con, x_eval)SUAVE.Optimization.Package_Setups.additive_setup.Additive_Solver
initialize_opt_vals_SHGO(self, obj, inp, x_low_bound, x_up_bound, con_low_edge, con_up_edge, nam, con, problem, cons_surr) (defined in SUAVE.Optimization.Package_Setups.additive_setup.Additive_Solver)SUAVE.Optimization.Package_Setups.additive_setup.Additive_Solver
initialize_opt_vals_SLSQP(self, obj, inp, x_low_bound, x_up_bound, con_low_edge, con_up_edge, nam, con, x_eval, problem, cons_surr) (defined in SUAVE.Optimization.Package_Setups.additive_setup.Additive_Solver)SUAVE.Optimization.Package_Setups.additive_setup.Additive_Solver
local_optimizer (defined in SUAVE.Optimization.Package_Setups.additive_setup.Additive_Solver)SUAVE.Optimization.Package_Setups.additive_setup.Additive_Solver
run_objective_optimization(self, opt_prob, problem, f_additive_surrogate, g_additive_surrogate)SUAVE.Optimization.Package_Setups.additive_setup.Additive_Solver
scale_vals(self, inp, con, ini, bnd, scl)SUAVE.Optimization.Package_Setups.additive_setup.Additive_Solver
unpack_constraints_slsqp(self, x, con_ind, sign, edge, problem, cons_surrogate) (defined in SUAVE.Optimization.Package_Setups.additive_setup.Additive_Solver)SUAVE.Optimization.Package_Setups.additive_setup.Additive_Solver
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Optimization_1_1Package__Setups_1_1additive__setup_1_1Additive__Solver.html b/doxygen/classSUAVE_1_1Optimization_1_1Package__Setups_1_1additive__setup_1_1Additive__Solver.html new file mode 100644 index 00000000..bfa8e2dc --- /dev/null +++ b/doxygen/classSUAVE_1_1Optimization_1_1Package__Setups_1_1additive__setup_1_1Additive__Solver.html @@ -0,0 +1,168 @@ + + + + + + + +SUAVE: SUAVE.Optimization.Package_Setups.additive_setup.Additive_Solver Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Optimization.Package_Setups.additive_setup.Additive_Solver Class Reference
+
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + +

+Public Member Functions

+def __init__ (self)
 
def Additive_Solve (self, problem, num_fidelity_levels=2, num_samples=10, max_iterations=10, tolerance=1e-6, opt_type='basic', num_starts=3, print_output=True)
 
def evaluate_model (self, problem, x, cons)
 
def evaluate_corrected_model (self, x, problem=None, obj_surrogate=None, cons_surrogate=None)
 
def evaluate_expected_improvement (self, x, problem=None, obj_surrogate=None, cons_surrogate=None, fstar=np.inf, cons=None)
 
def expected_improvement_carpet (self, lbs, ubs, problem, obj_surrogate, cons_surrogate, fstar, show_log_improvement=False)
 
def scale_vals (self, inp, con, ini, bnd, scl)
 
def initialize_opt_vals (self, opt_prob, obj, inp, x_low_bound, x_up_bound, con_low_edge, con_up_edge, nam, con, x_eval)
 
+def unpack_constraints_slsqp (self, x, con_ind, sign, edge, problem, cons_surrogate)
 
+def initialize_opt_vals_SLSQP (self, obj, inp, x_low_bound, x_up_bound, con_low_edge, con_up_edge, nam, con, x_eval, problem, cons_surr)
 
+def initialize_opt_vals_SHGO (self, obj, inp, x_low_bound, x_up_bound, con_low_edge, con_up_edge, nam, con, problem, cons_surr)
 
def run_objective_optimization (self, opt_prob, problem, f_additive_surrogate, g_additive_surrogate)
 
+ + + + + + + +

+Public Attributes

local_optimizer
 
global_optimizer
 
const_list
 
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Optimization/Package_Setups/additive_setup.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Optimization_1_1Package__Setups_1_1additive__setup_1_1Additive__Solver.js b/doxygen/classSUAVE_1_1Optimization_1_1Package__Setups_1_1additive__setup_1_1Additive__Solver.js new file mode 100644 index 00000000..abff6379 --- /dev/null +++ b/doxygen/classSUAVE_1_1Optimization_1_1Package__Setups_1_1additive__setup_1_1Additive__Solver.js @@ -0,0 +1,18 @@ +var classSUAVE_1_1Optimization_1_1Package__Setups_1_1additive__setup_1_1Additive__Solver = +[ + [ "__init__", "classSUAVE_1_1Optimization_1_1Package__Setups_1_1additive__setup_1_1Additive__Solver.html#a67b342a8c319534f283c411ac6cf9343", null ], + [ "Additive_Solve", "group__Optimization-Package__Setups.html#ga8f9c498581a443c5b268bc995f4771d7", null ], + [ "evaluate_corrected_model", "group__Optimization-Package__Setups.html#ga9fd8c25ffe84afec24ae5842fd01bc59", null ], + [ "evaluate_expected_improvement", "group__Optimization-Package__Setups.html#ga2fce77878956493ab46ed6d86b7c7028", null ], + [ "evaluate_model", "group__Optimization-Package__Setups.html#ga1aa96d868702f99a0b15f58bf5eca0ce", null ], + [ "expected_improvement_carpet", "group__Optimization-Package__Setups.html#ga75d4008576d2b1539a517bdde5147089", null ], + [ "initialize_opt_vals", "group__Optimization-Package__Setups.html#gaa25a2e15b4183507a2a1ec0725bfe9ce", null ], + [ "initialize_opt_vals_SHGO", "classSUAVE_1_1Optimization_1_1Package__Setups_1_1additive__setup_1_1Additive__Solver.html#a3ed5234a9d08fa498209795564f98170", null ], + [ "initialize_opt_vals_SLSQP", "classSUAVE_1_1Optimization_1_1Package__Setups_1_1additive__setup_1_1Additive__Solver.html#af283532316e0c64be86fd54a617d8c2a", null ], + [ "run_objective_optimization", "group__Optimization-Package__Setups.html#ga4977676388001bfa1045dd9ed14448a1", null ], + [ "scale_vals", "group__Optimization-Package__Setups.html#ga9466bd27f5f4934f91f5f60643747db3", null ], + [ "unpack_constraints_slsqp", "classSUAVE_1_1Optimization_1_1Package__Setups_1_1additive__setup_1_1Additive__Solver.html#ad883c9771bea5836f237b3b290f55385", null ], + [ "const_list", "classSUAVE_1_1Optimization_1_1Package__Setups_1_1additive__setup_1_1Additive__Solver.html#acea558bc124369bdb24d36be705d25bb", null ], + [ "global_optimizer", "classSUAVE_1_1Optimization_1_1Package__Setups_1_1additive__setup_1_1Additive__Solver.html#a0ac9f00c61750deb76d07acd2a96d2ff", null ], + [ "local_optimizer", "classSUAVE_1_1Optimization_1_1Package__Setups_1_1additive__setup_1_1Additive__Solver.html#acc82b35025ef9fdc7296163643cc822f", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Optimization_1_1Surrogate__Optimization_1_1Surrogate__Optimization-members.html b/doxygen/classSUAVE_1_1Optimization_1_1Surrogate__Optimization_1_1Surrogate__Optimization-members.html index cc82e6b7..1148f6c8 100644 --- a/doxygen/classSUAVE_1_1Optimization_1_1Surrogate__Optimization_1_1Surrogate__Optimization-members.html +++ b/doxygen/classSUAVE_1_1Optimization_1_1Surrogate__Optimization_1_1Surrogate__Optimization-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -101,32 +108,33 @@ __defaults__(self)SUAVE.Optimization.Surrogate_Optimization.Surrogate_Optimization __delattr__(self, k)SUAVE.Core.Data.Data __getattribute__(self, k)SUAVE.Core.Data.Data - __init__(self, args, kwarg)SUAVE.Core.Data.Data + __init__(self, *args, **kwarg)SUAVE.Core.Data.Data __iter__(self)SUAVE.Core.Data.Data - __new__(cls, args, kwarg)SUAVE.Core.Data.Data + __new__(cls, *args, **kwarg)SUAVE.Core.Data.Data __setattr__(self, k, v)SUAVE.Core.Data.Data __str__(self, indent='')SUAVE.Core.Data.Data append(self, value, key=None)SUAVE.Core.Data.Data - build_surrogate(self)SUAVE.Optimization.Surrogate_Optimization.Surrogate_Optimization - dataname(self)SUAVE.Core.Data.Data - deep_get(self, keys)SUAVE.Core.Data.Data - deep_set(self, keys, val)SUAVE.Core.Data.Data - do_recursive(self, method, other=None, default=None)SUAVE.Core.Data.Data - get_bases(self)SUAVE.Core.Data.Data - iterative_optimization(self)SUAVE.Optimization.Surrogate_Optimization.Surrogate_Optimization - itervalues(self)SUAVE.Core.Data.Data - max_iterations (defined in SUAVE.Optimization.Surrogate_Optimization.Surrogate_Optimization)SUAVE.Optimization.Surrogate_Optimization.Surrogate_Optimization - number_of_points (defined in SUAVE.Optimization.Surrogate_Optimization.Surrogate_Optimization)SUAVE.Optimization.Surrogate_Optimization.Surrogate_Optimization - optimization_filename (defined in SUAVE.Optimization.Surrogate_Optimization.Surrogate_Optimization)SUAVE.Optimization.Surrogate_Optimization.Surrogate_Optimization - optimizer (defined in SUAVE.Optimization.Surrogate_Optimization.Surrogate_Optimization)SUAVE.Optimization.Surrogate_Optimization.Surrogate_Optimization - pack_array(self, output='vector')SUAVE.Core.Data.Data - problem (defined in SUAVE.Optimization.Surrogate_Optimization.Surrogate_Optimization)SUAVE.Optimization.Surrogate_Optimization.Surrogate_Optimization - sample_plan (defined in SUAVE.Optimization.Surrogate_Optimization.Surrogate_Optimization)SUAVE.Optimization.Surrogate_Optimization.Surrogate_Optimization - surrogate_model (defined in SUAVE.Optimization.Surrogate_Optimization.Surrogate_Optimization)SUAVE.Optimization.Surrogate_Optimization.Surrogate_Optimization - typestring(self)SUAVE.Core.Data.Data - unpack_array(self, M)SUAVE.Core.Data.Data - update(self, other)SUAVE.Core.Data.Data - values(self)SUAVE.Core.Data.Data + append_or_update(self, other)SUAVE.Core.Data.Data + build_surrogate(self)SUAVE.Optimization.Surrogate_Optimization.Surrogate_Optimization + dataname(self)SUAVE.Core.Data.Data + deep_get(self, keys)SUAVE.Core.Data.Data + deep_set(self, keys, val)SUAVE.Core.Data.Data + do_recursive(self, method, other=None, default=None)SUAVE.Core.Data.Data + get_bases(self)SUAVE.Core.Data.Data + iterative_optimization(self)SUAVE.Optimization.Surrogate_Optimization.Surrogate_Optimization + itervalues(self)SUAVE.Core.Data.Data + max_iterations (defined in SUAVE.Optimization.Surrogate_Optimization.Surrogate_Optimization)SUAVE.Optimization.Surrogate_Optimization.Surrogate_Optimization + number_of_points (defined in SUAVE.Optimization.Surrogate_Optimization.Surrogate_Optimization)SUAVE.Optimization.Surrogate_Optimization.Surrogate_Optimization + optimization_filename (defined in SUAVE.Optimization.Surrogate_Optimization.Surrogate_Optimization)SUAVE.Optimization.Surrogate_Optimization.Surrogate_Optimization + optimizer (defined in SUAVE.Optimization.Surrogate_Optimization.Surrogate_Optimization)SUAVE.Optimization.Surrogate_Optimization.Surrogate_Optimization + pack_array(self, output='vector')SUAVE.Core.Data.Data + problem (defined in SUAVE.Optimization.Surrogate_Optimization.Surrogate_Optimization)SUAVE.Optimization.Surrogate_Optimization.Surrogate_Optimization + sample_plan (defined in SUAVE.Optimization.Surrogate_Optimization.Surrogate_Optimization)SUAVE.Optimization.Surrogate_Optimization.Surrogate_Optimization + surrogate_model (defined in SUAVE.Optimization.Surrogate_Optimization.Surrogate_Optimization)SUAVE.Optimization.Surrogate_Optimization.Surrogate_Optimization + typestring(self)SUAVE.Core.Data.Data + unpack_array(self, M)SUAVE.Core.Data.Data + update(self, other)SUAVE.Core.Data.Data + values(self)SUAVE.Core.Data.Data
@@ -134,7 +142,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Optimization_1_1Surrogate__Optimization_1_1Surrogate__Optimization.html b/doxygen/classSUAVE_1_1Optimization_1_1Surrogate__Optimization_1_1Surrogate__Optimization.html index 7caf7c42..21d50c76 100644 --- a/doxygen/classSUAVE_1_1Optimization_1_1Surrogate__Optimization_1_1Surrogate__Optimization.html +++ b/doxygen/classSUAVE_1_1Optimization_1_1Surrogate__Optimization_1_1Surrogate__Optimization.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Optimization.Surrogate_Optimization.Surrogate_Optimization Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -106,8 +113,8 @@ SUAVE.Core.Data.Data - -
+ + @@ -124,18 +131,16 @@ - - - - + + - - + + @@ -144,6 +149,8 @@ + + @@ -226,6 +233,8 @@

SUAVE.Core.Data.Data.

+ @@ -308,7 +317,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1compat_1_1ChainMap-members.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1compat_1_1ChainMap-members.html index 26bc3709..9db606e9 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1compat_1_1ChainMap-members.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1compat_1_1ChainMap-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Member Functions

 
def __delattr__ (self, k)
 
def __defaults__ (self)
 
def __new__ (cls, args, kwarg)
 
def __new__ (cls, *args, **kwarg)
 
def typestring (self)
 
def dataname (self)
 
def __str__ (self, indent='')
 
def __init__ (self, args, kwarg)
 
def __init__ (self, *args, **kwarg)
 
def __iter__ (self)
 
def itervalues (self)
 
def update (self, other)
 
def append_or_update (self, other)
 
def get_bases (self)
 
def append (self, value, key=None)
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -102,7 +109,7 @@ __contains__(self, key) (defined in SUAVE.Plugins.pint.compat.ChainMap)SUAVE.Plugins.pint.compat.ChainMap __delitem__(self, key) (defined in SUAVE.Plugins.pint.compat.ChainMap)SUAVE.Plugins.pint.compat.ChainMap __getitem__(self, key) (defined in SUAVE.Plugins.pint.compat.ChainMap)SUAVE.Plugins.pint.compat.ChainMap - __init__(self, maps)SUAVE.Plugins.pint.compat.ChainMap + __init__(self, *maps)SUAVE.Plugins.pint.compat.ChainMap __iter__(self) (defined in SUAVE.Plugins.pint.compat.ChainMap)SUAVE.Plugins.pint.compat.ChainMap __len__(self) (defined in SUAVE.Plugins.pint.compat.ChainMap)SUAVE.Plugins.pint.compat.ChainMap __missing__(self, key) (defined in SUAVE.Plugins.pint.compat.ChainMap)SUAVE.Plugins.pint.compat.ChainMap @@ -110,12 +117,12 @@ __setitem__(self, key, value) (defined in SUAVE.Plugins.pint.compat.ChainMap)SUAVE.Plugins.pint.compat.ChainMap clear(self) (defined in SUAVE.Plugins.pint.compat.ChainMap)SUAVE.Plugins.pint.compat.ChainMap copy(self) (defined in SUAVE.Plugins.pint.compat.ChainMap)SUAVE.Plugins.pint.compat.ChainMap - fromkeys(cls, iterable, args) (defined in SUAVE.Plugins.pint.compat.ChainMap)SUAVE.Plugins.pint.compat.ChainMap + fromkeys(cls, iterable, *args) (defined in SUAVE.Plugins.pint.compat.ChainMap)SUAVE.Plugins.pint.compat.ChainMap get(self, key, default=None) (defined in SUAVE.Plugins.pint.compat.ChainMap)SUAVE.Plugins.pint.compat.ChainMap maps (defined in SUAVE.Plugins.pint.compat.ChainMap)SUAVE.Plugins.pint.compat.ChainMap new_child(self, m=None)SUAVE.Plugins.pint.compat.ChainMap parents(self) (defined in SUAVE.Plugins.pint.compat.ChainMap)SUAVE.Plugins.pint.compat.ChainMap - pop(self, key, args) (defined in SUAVE.Plugins.pint.compat.ChainMap)SUAVE.Plugins.pint.compat.ChainMap + pop(self, key, *args) (defined in SUAVE.Plugins.pint.compat.ChainMap)SUAVE.Plugins.pint.compat.ChainMap popitem(self) (defined in SUAVE.Plugins.pint.compat.ChainMap)SUAVE.Plugins.pint.compat.ChainMap
@@ -124,7 +131,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1compat_1_1ChainMap.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1compat_1_1ChainMap.html index a78e7b4c..5ecb0495 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1compat_1_1ChainMap.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1compat_1_1ChainMap.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Plugins.pint.compat.ChainMap Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -106,13 +113,13 @@ SUAVE.Plugins.pint.context.ContextChain - -
+ + - - + + @@ -137,9 +144,9 @@ - - + + @@ -157,9 +164,9 @@ - - + + @@ -180,8 +187,8 @@ Lookups search the underlying mappings successively until a key is found. In contrast, writes, updates, and deletions only operate on the first mapping.

Constructor & Destructor Documentation

- -

◆ __init__()

+ +

◆ __init__()

@@ -195,7 +202,7 @@

- + @@ -251,7 +258,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1compat_1_1ChainMap.js b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1compat_1_1ChainMap.js index bb308f52..b2107b5e 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1compat_1_1ChainMap.js +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1compat_1_1ChainMap.js @@ -1,6 +1,6 @@ var classSUAVE_1_1Plugins_1_1pint_1_1compat_1_1ChainMap = [ - [ "__init__", "classSUAVE_1_1Plugins_1_1pint_1_1compat_1_1ChainMap.html#a08c0cf81ad757d1525d8bd7a66d8bfd7", null ], + [ "__init__", "classSUAVE_1_1Plugins_1_1pint_1_1compat_1_1ChainMap.html#aeb92660fe473901d5f25692947a8bde4", null ], [ "__bool__", "classSUAVE_1_1Plugins_1_1pint_1_1compat_1_1ChainMap.html#a04baa3be7a2b38d89a1732b2fb2eccd7", null ], [ "__contains__", "classSUAVE_1_1Plugins_1_1pint_1_1compat_1_1ChainMap.html#a445afea0490070ab9bdac5af137f3b20", null ], [ "__delitem__", "classSUAVE_1_1Plugins_1_1pint_1_1compat_1_1ChainMap.html#a973ff4147b37bfed88b6d076e3d876ee", null ], @@ -12,11 +12,11 @@ var classSUAVE_1_1Plugins_1_1pint_1_1compat_1_1ChainMap = [ "__setitem__", "classSUAVE_1_1Plugins_1_1pint_1_1compat_1_1ChainMap.html#a4ed7f98b3c9abef8981c68c3d65f557b", null ], [ "clear", "classSUAVE_1_1Plugins_1_1pint_1_1compat_1_1ChainMap.html#a81b5f193fca2292e9570503915cc3524", null ], [ "copy", "classSUAVE_1_1Plugins_1_1pint_1_1compat_1_1ChainMap.html#a6eecd826aa5e8d2d627bbbb3ddd58ff3", null ], - [ "fromkeys", "classSUAVE_1_1Plugins_1_1pint_1_1compat_1_1ChainMap.html#a27941f49e012a57da0d4813914f5b047", null ], + [ "fromkeys", "classSUAVE_1_1Plugins_1_1pint_1_1compat_1_1ChainMap.html#a23c0af57db7d6925b003200e57172ae1", null ], [ "get", "classSUAVE_1_1Plugins_1_1pint_1_1compat_1_1ChainMap.html#a06f2023726361c38b22802b3c87572db", null ], [ "new_child", "classSUAVE_1_1Plugins_1_1pint_1_1compat_1_1ChainMap.html#a7eeedde1c0cba8c8db7f7f854ee11666", null ], [ "parents", "classSUAVE_1_1Plugins_1_1pint_1_1compat_1_1ChainMap.html#aef325b6e0d4996dcd0dd93da962c5d77", null ], - [ "pop", "classSUAVE_1_1Plugins_1_1pint_1_1compat_1_1ChainMap.html#a2abc190b0cc931b6267524280261a70a", null ], + [ "pop", "classSUAVE_1_1Plugins_1_1pint_1_1compat_1_1ChainMap.html#a833008db3bbc4849b96f812e0a8613ba", null ], [ "popitem", "classSUAVE_1_1Plugins_1_1pint_1_1compat_1_1ChainMap.html#ad6d9a5b6240759c6507b179ddcad6ef3", null ], [ "maps", "classSUAVE_1_1Plugins_1_1pint_1_1compat_1_1ChainMap.html#a8cd3d83071702cfd016a6931d3569aa7", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1context_1_1Context-members.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1context_1_1Context-members.html index 27c42eee..5a7be3ae 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1context_1_1Context-members.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1context_1_1Context-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Member Functions

def __init__ (self, maps)
 
def __init__ (self, *maps)
 
def __missing__ (self, key)
 
def __repr__ (self)
 
-def fromkeys (cls, iterable, args)
 
+def fromkeys (cls, iterable, *args)
 
def copy (self)
 
def popitem (self)
 
-def pop (self, key, args)
 
+def pop (self, key, *args)
 
def clear (self)
 
  maps 
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1context_1_1Context.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1context_1_1Context.html index dd383675..a6bc1430 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1context_1_1Context.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1context_1_1Context.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Plugins.pint.context.Context Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -104,9 +111,7 @@ Inheritance diagram for SUAVE.Plugins.pint.context.Context:
- - - +
- - + + @@ -216,8 +221,8 @@

-

◆ from_context()

+ +

◆ from_context()

@@ -237,7 +242,7 @@

- + @@ -348,7 +353,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1context_1_1Context.js b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1context_1_1Context.js index e2ad58b9..3450e1df 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1context_1_1Context.js +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1context_1_1Context.js @@ -2,7 +2,7 @@ var classSUAVE_1_1Plugins_1_1pint_1_1context_1_1Context = [ [ "__init__", "classSUAVE_1_1Plugins_1_1pint_1_1context_1_1Context.html#a711c56099d5f4a057c17a2e291271ee2", null ], [ "add_transformation", "classSUAVE_1_1Plugins_1_1pint_1_1context_1_1Context.html#a6c6e5ca70615d646dc9aa6f42c606d58", null ], - [ "from_context", "classSUAVE_1_1Plugins_1_1pint_1_1context_1_1Context.html#a66f98a4dd9ae08e15b32961914f5641b", null ], + [ "from_context", "classSUAVE_1_1Plugins_1_1pint_1_1context_1_1Context.html#ab227befa54441a0c5e6bbb57bb48f936", null ], [ "from_lines", "classSUAVE_1_1Plugins_1_1pint_1_1context_1_1Context.html#aeb8be96e54ea025d281ab6ce89656295", null ], [ "remove_transformation", "classSUAVE_1_1Plugins_1_1pint_1_1context_1_1Context.html#a9289ff4f315744f7d3f72ba5e0af1a98", null ], [ "transform", "classSUAVE_1_1Plugins_1_1pint_1_1context_1_1Context.html#abb6b6f8bbf8264656eb0d35a0a6be9b2", null ], diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1context_1_1ContextChain-members.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1context_1_1ContextChain-members.html index fd456075..6ebe1f21 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1context_1_1ContextChain-members.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1context_1_1ContextChain-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

@@ -114,8 +119,8 @@

def __init__ (self, name, aliases=(), defaults=None)
 
def from_context (cls, context, defaults)
 
def from_context (cls, context, **defaults)
 
def from_lines (cls, lines, to_base_func=None)
 
 **  defaults 
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -102,8 +109,8 @@ __contains__(self, key) (defined in SUAVE.Plugins.pint.compat.ChainMap)SUAVE.Plugins.pint.compat.ChainMap __delitem__(self, key) (defined in SUAVE.Plugins.pint.compat.ChainMap)SUAVE.Plugins.pint.compat.ChainMap __getitem__(self, key) (defined in SUAVE.Plugins.pint.compat.ChainMap)SUAVE.Plugins.pint.compat.ChainMap - __init__(self, args, kwargs) (defined in SUAVE.Plugins.pint.context.ContextChain)SUAVE.Plugins.pint.context.ContextChain - SUAVE::Plugins::pint::compat::ChainMap.__init__(self, maps)SUAVE.Plugins.pint.compat.ChainMap + __init__(self, *args, **kwargs) (defined in SUAVE.Plugins.pint.context.ContextChain)SUAVE.Plugins.pint.context.ContextChain + SUAVE::Plugins::pint::compat::ChainMap.__init__(self, *maps)SUAVE.Plugins.pint.compat.ChainMap __iter__(self) (defined in SUAVE.Plugins.pint.compat.ChainMap)SUAVE.Plugins.pint.compat.ChainMap __len__(self) (defined in SUAVE.Plugins.pint.compat.ChainMap)SUAVE.Plugins.pint.compat.ChainMap __missing__(self, key) (defined in SUAVE.Plugins.pint.compat.ChainMap)SUAVE.Plugins.pint.compat.ChainMap @@ -112,14 +119,14 @@ clear(self) (defined in SUAVE.Plugins.pint.compat.ChainMap)SUAVE.Plugins.pint.compat.ChainMap copy(self) (defined in SUAVE.Plugins.pint.compat.ChainMap)SUAVE.Plugins.pint.compat.ChainMap defaults(self) (defined in SUAVE.Plugins.pint.context.ContextChain)SUAVE.Plugins.pint.context.ContextChain - fromkeys(cls, iterable, args) (defined in SUAVE.Plugins.pint.compat.ChainMap)SUAVE.Plugins.pint.compat.ChainMap + fromkeys(cls, iterable, *args) (defined in SUAVE.Plugins.pint.compat.ChainMap)SUAVE.Plugins.pint.compat.ChainMap get(self, key, default=None) (defined in SUAVE.Plugins.pint.compat.ChainMap)SUAVE.Plugins.pint.compat.ChainMap graph(self)SUAVE.Plugins.pint.context.ContextChain - insert_contexts(self, contexts)SUAVE.Plugins.pint.context.ContextChain + insert_contexts(self, *contexts)SUAVE.Plugins.pint.context.ContextChain maps (defined in SUAVE.Plugins.pint.context.ContextChain)SUAVE.Plugins.pint.context.ContextChain new_child(self, m=None)SUAVE.Plugins.pint.compat.ChainMap parents(self) (defined in SUAVE.Plugins.pint.compat.ChainMap)SUAVE.Plugins.pint.compat.ChainMap - pop(self, key, args) (defined in SUAVE.Plugins.pint.compat.ChainMap)SUAVE.Plugins.pint.compat.ChainMap + pop(self, key, *args) (defined in SUAVE.Plugins.pint.compat.ChainMap)SUAVE.Plugins.pint.compat.ChainMap popitem(self) (defined in SUAVE.Plugins.pint.compat.ChainMap)SUAVE.Plugins.pint.compat.ChainMap remove_contexts(self, n)SUAVE.Plugins.pint.context.ContextChain transform(self, src, dst, registry, value)SUAVE.Plugins.pint.context.ContextChain @@ -130,7 +137,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1context_1_1ContextChain.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1context_1_1ContextChain.html index 1ef6be29..8190dbe5 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1context_1_1ContextChain.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1context_1_1ContextChain.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Plugins.pint.context.ContextChain Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -106,16 +113,16 @@ SUAVE.Plugins.pint.compat.ChainMap - -
+ + - - - - + + + + - - + + @@ -152,9 +159,9 @@ - - + + @@ -172,9 +179,9 @@ - - + + @@ -212,8 +219,8 @@

-

◆ insert_contexts()

+ +

◆ insert_contexts()

@@ -227,7 +234,7 @@

- + @@ -335,7 +342,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1context_1_1ContextChain.js b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1context_1_1ContextChain.js index 318cc48f..7365b56c 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1context_1_1ContextChain.js +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1context_1_1ContextChain.js @@ -1,9 +1,9 @@ var classSUAVE_1_1Plugins_1_1pint_1_1context_1_1ContextChain = [ - [ "__init__", "classSUAVE_1_1Plugins_1_1pint_1_1context_1_1ContextChain.html#a9af3606e14dd2ca683a6dfb088d7d6e2", null ], + [ "__init__", "classSUAVE_1_1Plugins_1_1pint_1_1context_1_1ContextChain.html#a395c967bbaebef4a9b89d025f1c7aacd", null ], [ "defaults", "classSUAVE_1_1Plugins_1_1pint_1_1context_1_1ContextChain.html#ae480e50e871f32994f9bee8ca90f9328", null ], [ "graph", "classSUAVE_1_1Plugins_1_1pint_1_1context_1_1ContextChain.html#ad1f3b9b56633a6940846b225b4e7025d", null ], - [ "insert_contexts", "classSUAVE_1_1Plugins_1_1pint_1_1context_1_1ContextChain.html#a3cfbdc06d4624200eabf3f5be9409d18", null ], + [ "insert_contexts", "classSUAVE_1_1Plugins_1_1pint_1_1context_1_1ContextChain.html#a0b6ac0401436632fdd6685e401c817eb", null ], [ "remove_contexts", "classSUAVE_1_1Plugins_1_1pint_1_1context_1_1ContextChain.html#a5f6e660044e5ca4e2abe5459f71b0741", null ], [ "transform", "classSUAVE_1_1Plugins_1_1pint_1_1context_1_1ContextChain.html#a133967cefcb49a5c012dbd97dbd204e0", null ], [ "maps", "classSUAVE_1_1Plugins_1_1pint_1_1context_1_1ContextChain.html#a59fa2befb0e787b0f3d61a9b03977225", null ] diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1measurement_1_1Measurement-members.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1measurement_1_1Measurement-members.html index f374b1e7..4889e563 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1measurement_1_1Measurement-members.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1measurement_1_1Measurement-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Member Functions

-def __init__ (self, args, kwargs)
 
def insert_contexts (self, contexts)
 
+def __init__ (self, *args, **kwargs)
 
def insert_contexts (self, *contexts)
 
def remove_contexts (self, n)
 
@@ -126,8 +133,8 @@
def transform (self, src, dst, registry, value)
 
- Public Member Functions inherited from SUAVE.Plugins.pint.compat.ChainMap
def __init__ (self, maps)
 
def __init__ (self, *maps)
 
def __missing__ (self, key)
 
def __repr__ (self)
 
-def fromkeys (cls, iterable, args)
 
+def fromkeys (cls, iterable, *args)
 
def copy (self)
 
def popitem (self)
 
-def pop (self, key, args)
 
+def pop (self, key, *args)
 
def clear (self)
 
  contexts 
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -117,7 +124,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1measurement_1_1Measurement.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1measurement_1_1Measurement.html index 06ad5bf2..d00d1256 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1measurement_1_1Measurement.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1measurement_1_1Measurement.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Plugins.pint.measurement.Measurement Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -102,9 +109,7 @@ Inheritance diagram for SUAVE.Plugins.pint.measurement.Measurement:
- - - +
@@ -57,9 +60,11 @@

@@ -164,7 +169,7 @@ + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1quantity_1_1__Exception-members.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1quantity_1_1__Exception-members.html index 24dd1cbc..4422defe 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1quantity_1_1__Exception-members.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1quantity_1_1__Exception-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -107,7 +114,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1quantity_1_1__Exception.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1quantity_1_1__Exception.html index ac99bffd..35bea46a 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1quantity_1_1__Exception.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1quantity_1_1__Exception.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Plugins.pint.quantity._Exception Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -103,9 +110,7 @@ Inheritance diagram for SUAVE.Plugins.pint.quantity._Exception:
- - - +
@@ -57,9 +60,11 @@

@@ -131,7 +136,7 @@ + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1quantity_1_1__Quantity-members.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1quantity_1_1__Quantity-members.html index c4bdf108..b431863f 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1quantity_1_1__Quantity-members.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1quantity_1_1__Quantity-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -136,7 +143,7 @@ __sub__(self, other) (defined in SUAVE.Plugins.pint.quantity._Quantity)SUAVE.Plugins.pint.quantity._Quantity __truediv__(self, other) (defined in SUAVE.Plugins.pint.quantity._Quantity)SUAVE.Plugins.pint.quantity._Quantity add_sub(self, other, op) (defined in SUAVE.Plugins.pint.quantity._Quantity)SUAVE.Plugins.pint.quantity._Quantity - clip(self, first=None, second=None, out=None, kwargs) (defined in SUAVE.Plugins.pint.quantity._Quantity)SUAVE.Plugins.pint.quantity._Quantity + clip(self, first=None, second=None, out=None, **kwargs) (defined in SUAVE.Plugins.pint.quantity._Quantity)SUAVE.Plugins.pint.quantity._Quantity compare(self, other, op) (defined in SUAVE.Plugins.pint.quantity._Quantity)SUAVE.Plugins.pint.quantity._Quantity default_format (defined in SUAVE.Plugins.pint.quantity._Quantity)SUAVE.Plugins.pint.quantity._Quantitystatic dimensionality (defined in SUAVE.Plugins.pint.quantity._Quantity)SUAVE.Plugins.pint.quantity._Quantity @@ -144,13 +151,13 @@ dimensionless(self)SUAVE.Plugins.pint.quantity._Quantity fill(self, value) (defined in SUAVE.Plugins.pint.quantity._Quantity)SUAVE.Plugins.pint.quantity._Quantity iadd_sub(self, other, op) (defined in SUAVE.Plugins.pint.quantity._Quantity)SUAVE.Plugins.pint.quantity._Quantity - ito(self, other=None, contexts, ctx_kwargs)SUAVE.Plugins.pint.quantity._Quantity + ito(self, other=None, *contexts, **ctx_kwargs)SUAVE.Plugins.pint.quantity._Quantity ito_base_units(self)SUAVE.Plugins.pint.quantity._Quantity magnitude(self)SUAVE.Plugins.pint.quantity._Quantity plus_minus(self, error, relative=False) (defined in SUAVE.Plugins.pint.quantity._Quantity)SUAVE.Plugins.pint.quantity._Quantity put(self, indices, values, mode='raise') (defined in SUAVE.Plugins.pint.quantity._Quantity)SUAVE.Plugins.pint.quantity._Quantity searchsorted(self, v, side='left') (defined in SUAVE.Plugins.pint.quantity._Quantity)SUAVE.Plugins.pint.quantity._Quantity - to(self, other=None, contexts, ctx_kwargs)SUAVE.Plugins.pint.quantity._Quantity + to(self, other=None, *contexts, **ctx_kwargs)SUAVE.Plugins.pint.quantity._Quantity to_base_units(self)SUAVE.Plugins.pint.quantity._Quantity tolist(self) (defined in SUAVE.Plugins.pint.quantity._Quantity)SUAVE.Plugins.pint.quantity._Quantity unitless(self)SUAVE.Plugins.pint.quantity._Quantity @@ -163,7 +170,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1quantity_1_1__Quantity.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1quantity_1_1__Quantity.html index 32156839..a578568e 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1quantity_1_1__Quantity.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1quantity_1_1__Quantity.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Plugins.pint.quantity._Quantity Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -104,9 +111,7 @@ Inheritance diagram for SUAVE.Plugins.pint.quantity._Quantity:
- - - +
- - - - + + + + @@ -228,9 +233,9 @@ - - + + @@ -330,8 +335,8 @@

-

◆ ito()

+ +

◆ ito()

@@ -351,13 +356,13 @@

- + - + @@ -412,8 +417,8 @@

-

◆ to()

+ +

◆ to()

@@ -433,13 +438,13 @@

- + - + @@ -526,7 +531,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1quantity_1_1__Quantity.js b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1quantity_1_1__Quantity.js index febd6c23..3fd4d752 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1quantity_1_1__Quantity.js +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1quantity_1_1__Quantity.js @@ -38,19 +38,19 @@ var classSUAVE_1_1Plugins_1_1pint_1_1quantity_1_1__Quantity = [ "__sub__", "classSUAVE_1_1Plugins_1_1pint_1_1quantity_1_1__Quantity.html#a712bc04dda3307e276752766657069f8", null ], [ "__truediv__", "classSUAVE_1_1Plugins_1_1pint_1_1quantity_1_1__Quantity.html#ab5cc1b9acb082072048f5bff7ec7aa2b", null ], [ "add_sub", "classSUAVE_1_1Plugins_1_1pint_1_1quantity_1_1__Quantity.html#a19a9a4de08a98ae04eaa773a60ff8061", null ], - [ "clip", "classSUAVE_1_1Plugins_1_1pint_1_1quantity_1_1__Quantity.html#a91fa8c415e48c447f5445892af2118f2", null ], + [ "clip", "classSUAVE_1_1Plugins_1_1pint_1_1quantity_1_1__Quantity.html#a358cd39a9820d2fead4d62fefa039a41", null ], [ "compare", "classSUAVE_1_1Plugins_1_1pint_1_1quantity_1_1__Quantity.html#aa071e1967f08122d87b31a975a9a9b30", null ], [ "dimensionality", "classSUAVE_1_1Plugins_1_1pint_1_1quantity_1_1__Quantity.html#a7b58beaba890bc04287d88868ff53992", null ], [ "dimensionless", "classSUAVE_1_1Plugins_1_1pint_1_1quantity_1_1__Quantity.html#aaab2af1a8b18cfe97737c2b9a5030cb2", null ], [ "fill", "classSUAVE_1_1Plugins_1_1pint_1_1quantity_1_1__Quantity.html#a6564563fa66ec68494220d5f8ab83a13", null ], [ "iadd_sub", "classSUAVE_1_1Plugins_1_1pint_1_1quantity_1_1__Quantity.html#acf0321ecab3ed01395278249dc20265f", null ], - [ "ito", "classSUAVE_1_1Plugins_1_1pint_1_1quantity_1_1__Quantity.html#a6170671af193518aea49ec83c9073a34", null ], + [ "ito", "classSUAVE_1_1Plugins_1_1pint_1_1quantity_1_1__Quantity.html#af1a9b3e80309aa7f33e19bba2c539263", null ], [ "ito_base_units", "classSUAVE_1_1Plugins_1_1pint_1_1quantity_1_1__Quantity.html#acc236c11d5b4589e560cbeff59303bd9", null ], [ "magnitude", "classSUAVE_1_1Plugins_1_1pint_1_1quantity_1_1__Quantity.html#a3bd1b43240b5fce56634b4deb32a39d1", null ], [ "plus_minus", "classSUAVE_1_1Plugins_1_1pint_1_1quantity_1_1__Quantity.html#a670b05e0e689107251dcb907b2c3210d", null ], [ "put", "classSUAVE_1_1Plugins_1_1pint_1_1quantity_1_1__Quantity.html#ad53369fcfac028d80b76203992b5f004", null ], [ "searchsorted", "classSUAVE_1_1Plugins_1_1pint_1_1quantity_1_1__Quantity.html#a97693d163004db250af604d0d031dedd", null ], - [ "to", "classSUAVE_1_1Plugins_1_1pint_1_1quantity_1_1__Quantity.html#a45b9f65d52ad040bd437e24894758d33", null ], + [ "to", "classSUAVE_1_1Plugins_1_1pint_1_1quantity_1_1__Quantity.html#af4d26b457768b42deb3cf1d4747404fa", null ], [ "to_base_units", "classSUAVE_1_1Plugins_1_1pint_1_1quantity_1_1__Quantity.html#a1af9ee17b9199ca21d5e4329ce7e2dc7", null ], [ "tolist", "classSUAVE_1_1Plugins_1_1pint_1_1quantity_1_1__Quantity.html#acbb6bc3838aabe3ede0e8cec02a10834", null ], [ "unitless", "classSUAVE_1_1Plugins_1_1pint_1_1quantity_1_1__Quantity.html#a9cddd0d4dbd8023faa89c1c0d89e4d30", null ], diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1TestCase-members.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1TestCase-members.html index 261c8cd9..3424d5f2 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1TestCase-members.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1TestCase-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

@@ -139,10 +144,10 @@

 
def dimensionality (self)
 
def ito (self, other=None, contexts, ctx_kwargs)
 
def to (self, other=None, contexts, ctx_kwargs)
 
def ito (self, other=None, *contexts, **ctx_kwargs)
 
def to (self, other=None, *contexts, **ctx_kwargs)
 
def ito_base_units (self)
 
def to_base_units (self)
def __bool__ (self)
 
-def clip (self, first=None, second=None, out=None, kwargs)
 
+def clip (self, first=None, second=None, out=None, **kwargs)
 
def fill (self, value)
 
  contexts,
 **  ctx_kwargs 
  contexts,
 **  ctx_kwargs 
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -111,7 +118,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1TestCase.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1TestCase.html index cc49444c..584b328a 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1TestCase.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1TestCase.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Plugins.pint.testsuite.TestCase Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -114,8 +121,8 @@ SUAVE.Plugins.pint.testsuite.test_quantity.TestQuantity SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs SUAVE.Plugins.pint.testsuite.test_unit.TestRegistry - -
+ + @@ -152,7 +159,7 @@ + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1ndarray.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1ndarray.html index 52db82be..22d051d9 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1ndarray.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1ndarray.html @@ -1,9 +1,9 @@ - + - +SUAVE: SUAVE.Plugins.pint.testsuite.ndarray Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ @@ -57,9 +60,11 @@

Public Member Functions

SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -99,9 +106,7 @@ Inheritance diagram for SUAVE.Plugins.pint.testsuite.ndarray:
- - - +

The documentation for this class was generated from the following file:
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Plugins/pint/testsuite/__init__.py
  • @@ -114,7 +119,7 @@ + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__contexts_1_1TestContexts-members.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__contexts_1_1TestContexts-members.html index e171d46e..9641d5f0 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__contexts_1_1TestContexts-members.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__contexts_1_1TestContexts-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -124,7 +131,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__contexts_1_1TestContexts.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__contexts_1_1TestContexts.html index 3a800107..7fecf0d9 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__contexts_1_1TestContexts.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__contexts_1_1TestContexts.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Plugins.pint.testsuite.test_contexts.TestContexts Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -102,9 +109,7 @@ Inheritance diagram for SUAVE.Plugins.pint.testsuite.test_contexts.TestContexts:
- - - +
@@ -57,9 +60,11 @@

@@ -178,7 +183,7 @@ + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__contexts_1_1TestDefinedContexts-members.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__contexts_1_1TestDefinedContexts-members.html index a0bff5a2..0c9a36f2 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__contexts_1_1TestDefinedContexts-members.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__contexts_1_1TestDefinedContexts-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -114,7 +121,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__contexts_1_1TestDefinedContexts.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__contexts_1_1TestDefinedContexts.html index ee19277c..f70257ae 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__contexts_1_1TestDefinedContexts.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__contexts_1_1TestDefinedContexts.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Plugins.pint.testsuite.test_contexts.TestDefinedContexts Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -106,8 +113,8 @@ SUAVE.Plugins.pint.testsuite.TestCase - -
+ + @@ -158,7 +165,7 @@ + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__contexts_1_1TestHandler-members.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__contexts_1_1TestHandler-members.html index 999a2a3e..065d6225 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__contexts_1_1TestHandler-members.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__contexts_1_1TestHandler-members.html @@ -1,9 +1,9 @@ - + - +SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ @@ -57,9 +60,11 @@

Public Member Functions

SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -108,7 +115,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__contexts_1_1TestHandler.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__contexts_1_1TestHandler.html index 505a27cc..ccff7d8c 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__contexts_1_1TestHandler.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__contexts_1_1TestHandler.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Plugins.pint.testsuite.test_contexts.TestHandler Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -102,9 +109,7 @@ Inheritance diagram for SUAVE.Plugins.pint.testsuite.test_contexts.TestHandler:
- - - +
@@ -57,9 +60,11 @@

@@ -130,7 +135,7 @@ + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__issues_1_1TestIssues-members.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__issues_1_1TestIssues-members.html index 312bb974..a2132d43 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__issues_1_1TestIssues-members.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__issues_1_1TestIssues-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -115,7 +122,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__issues_1_1TestIssues.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__issues_1_1TestIssues.html index 44200a42..37aaf02c 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__issues_1_1TestIssues.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__issues_1_1TestIssues.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Plugins.pint.testsuite.test_issues.TestIssues Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -102,9 +109,7 @@ Inheritance diagram for SUAVE.Plugins.pint.testsuite.test_issues.TestIssues:
- - - +
@@ -57,9 +60,11 @@

@@ -151,7 +156,7 @@ + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__issues_1_1TestIssuesNP-members.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__issues_1_1TestIssuesNP-members.html index ee78bf31..4226fec0 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__issues_1_1TestIssuesNP-members.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__issues_1_1TestIssuesNP-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -121,7 +128,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__issues_1_1TestIssuesNP.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__issues_1_1TestIssuesNP.html index 08ea3f9a..4a8198ba 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__issues_1_1TestIssuesNP.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__issues_1_1TestIssuesNP.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Plugins.pint.testsuite.test_issues.TestIssuesNP Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -106,8 +113,8 @@ SUAVE.Plugins.pint.testsuite.TestCase - -
+ + @@ -179,7 +186,7 @@ + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__measurement_1_1TestMeasurement-members.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__measurement_1_1TestMeasurement-members.html index 89c1137a..9ad21c52 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__measurement_1_1TestMeasurement-members.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__measurement_1_1TestMeasurement-members.html @@ -1,9 +1,9 @@ - + - +SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ @@ -57,9 +60,11 @@

Public Member Functions

SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -116,7 +123,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__measurement_1_1TestMeasurement.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__measurement_1_1TestMeasurement.html index 671acc5c..a538f722 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__measurement_1_1TestMeasurement.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__measurement_1_1TestMeasurement.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Plugins.pint.testsuite.test_measurement.TestMeasurement Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -106,8 +113,8 @@ SUAVE.Plugins.pint.testsuite.TestCase - -
+ + @@ -164,7 +171,7 @@ + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__numpy_1_1TestBitTwiddlingUfuncs-members.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__numpy_1_1TestBitTwiddlingUfuncs-members.html index f76d4b13..05a248f9 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__numpy_1_1TestBitTwiddlingUfuncs-members.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__numpy_1_1TestBitTwiddlingUfuncs-members.html @@ -1,9 +1,9 @@ - + - +SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ @@ -57,9 +60,11 @@

Public Member Functions

SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -101,7 +108,7 @@ assertAlmostEqual(self, first, second, places=None, msg=None, delta=None) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase assertAlmostEqualRelError(self, first, second, rel, msg=None) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase assertEqual(self, first, second, msg=None) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs - assertRaisesMsg(self, msg, ExcType, func, args, kwargs) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs + assertRaisesMsg(self, msg, ExcType, func, *args, **kwargs) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs assertSequenceEqual(self, seq1, seq2, msg=None, seq_type=None) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase FORCE_NDARRAY (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncsstatic q1(self) (defined in SUAVE.Plugins.pint.testsuite.test_numpy.TestBitTwiddlingUfuncs)SUAVE.Plugins.pint.testsuite.test_numpy.TestBitTwiddlingUfuncs @@ -126,7 +133,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__numpy_1_1TestBitTwiddlingUfuncs.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__numpy_1_1TestBitTwiddlingUfuncs.html index e210e5cd..d02cd6ad 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__numpy_1_1TestBitTwiddlingUfuncs.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__numpy_1_1TestBitTwiddlingUfuncs.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Plugins.pint.testsuite.test_numpy.TestBitTwiddlingUfuncs Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -106,8 +113,8 @@ SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs SUAVE.Plugins.pint.testsuite.TestCase - -
+ + @@ -145,30 +152,15 @@ def  - - - - - - - - - - - - + + @@ -219,7 +211,7 @@ + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__numpy_1_1TestNumpyMethods-members.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__numpy_1_1TestNumpyMethods-members.html index 0780bbf8..0d96375f 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__numpy_1_1TestNumpyMethods-members.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__numpy_1_1TestNumpyMethods-members.html @@ -1,9 +1,9 @@ - + - +SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ @@ -57,9 +60,11 @@

Public Member Functions

test_right_shift (self)
 
- Public Member Functions inherited from SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs
-def qless (self)
 
-def qs (self)
 
-def q1 (self)
 
-def q2 (self)
 
-def qm (self)
 
def qi (self)
 
def assertEqual (self, first, second, msg=None)
 
-def assertRaisesMsg (self, msg, ExcType, func, args, kwargs)
 
+def assertRaisesMsg (self, msg, ExcType, func, *args, **kwargs)
 
- Public Member Functions inherited from SUAVE.Plugins.pint.testsuite.TestCase
def setUpClass (cls)
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -151,7 +158,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__numpy_1_1TestNumpyMethods.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__numpy_1_1TestNumpyMethods.html index 77549b90..6985998d 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__numpy_1_1TestNumpyMethods.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__numpy_1_1TestNumpyMethods.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyMethods Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -106,8 +113,8 @@ SUAVE.Plugins.pint.testsuite.TestCase - -
+ + @@ -287,7 +294,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__numpy_1_1TestNumpyNotSupported-members.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__numpy_1_1TestNumpyNotSupported-members.html index 2b4f0014..6b6b132e 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__numpy_1_1TestNumpyNotSupported-members.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__numpy_1_1TestNumpyNotSupported-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Member Functions

SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -101,7 +108,7 @@ assertAlmostEqual(self, first, second, places=None, msg=None, delta=None) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase assertAlmostEqualRelError(self, first, second, rel, msg=None) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase assertEqual(self, first, second, msg=None) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs - assertRaisesMsg(self, msg, ExcType, func, args, kwargs) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs + assertRaisesMsg(self, msg, ExcType, func, *args, **kwargs) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs assertSequenceEqual(self, seq1, seq2, msg=None, seq_type=None) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase FORCE_NDARRAY (defined in SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyNotSupported)SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyNotSupportedstatic q1(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs @@ -129,7 +136,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__numpy_1_1TestNumpyNotSupported.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__numpy_1_1TestNumpyNotSupported.html index d7e2ce77..5b8a681c 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__numpy_1_1TestNumpyNotSupported.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__numpy_1_1TestNumpyNotSupported.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Plugins.pint.testsuite.test_numpy.TestNumpyNotSupported Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -107,8 +114,8 @@ SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs SUAVE.Plugins.pint.testsuite.TestCase - -
+ + @@ -152,9 +159,9 @@ - - + + @@ -376,7 +383,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__pitheorem_1_1TestPiTheorem-members.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__pitheorem_1_1TestPiTheorem-members.html index 4a386a78..536b5519 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__pitheorem_1_1TestPiTheorem-members.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__pitheorem_1_1TestPiTheorem-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Member Functions

def assertEqual (self, first, second, msg=None)
 
-def assertRaisesMsg (self, msg, ExcType, func, args, kwargs)
 
+def assertRaisesMsg (self, msg, ExcType, func, *args, **kwargs)
 
- Public Member Functions inherited from SUAVE.Plugins.pint.testsuite.TestCase
def setUpClass (cls)
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -114,7 +121,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__pitheorem_1_1TestPiTheorem.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__pitheorem_1_1TestPiTheorem.html index f0ca1512..1b5b6a44 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__pitheorem_1_1TestPiTheorem.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__pitheorem_1_1TestPiTheorem.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Plugins.pint.testsuite.test_pitheorem.TestPiTheorem Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -106,8 +113,8 @@ SUAVE.Plugins.pint.testsuite.TestCase - -
+ + @@ -158,7 +165,7 @@ + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__quantity_1_1TestDimensions-members.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__quantity_1_1TestDimensions-members.html index 7d8fb185..02c84811 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__quantity_1_1TestDimensions-members.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__quantity_1_1TestDimensions-members.html @@ -1,9 +1,9 @@ - + - +SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ @@ -57,9 +60,11 @@

Public Member Functions

SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -114,7 +121,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__quantity_1_1TestDimensions.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__quantity_1_1TestDimensions.html index d906202a..4fbf698a 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__quantity_1_1TestDimensions.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__quantity_1_1TestDimensions.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Plugins.pint.testsuite.test_quantity.TestDimensions Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -106,8 +113,8 @@ SUAVE.Plugins.pint.testsuite.TestCase - -
+ + @@ -158,7 +165,7 @@ + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__quantity_1_1TestQuantity-members.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__quantity_1_1TestQuantity-members.html index a36051cf..3aeb3432 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__quantity_1_1TestQuantity-members.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__quantity_1_1TestQuantity-members.html @@ -1,9 +1,9 @@ - + - +SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ @@ -57,9 +60,11 @@

Public Member Functions

SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -134,7 +141,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__quantity_1_1TestQuantity.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__quantity_1_1TestQuantity.html index 9832e327..80cdc34f 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__quantity_1_1TestQuantity.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__quantity_1_1TestQuantity.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Plugins.pint.testsuite.test_quantity.TestQuantity Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -106,8 +113,8 @@ SUAVE.Plugins.pint.testsuite.TestCase - -
+ + @@ -218,7 +225,7 @@ + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestComparisonUfuncs-members.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestComparisonUfuncs-members.html index 7d54f8e0..5fac3798 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestComparisonUfuncs-members.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestComparisonUfuncs-members.html @@ -1,9 +1,9 @@ - + - +SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ @@ -57,9 +60,11 @@

Public Member Functions

SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -101,7 +108,7 @@ assertAlmostEqual(self, first, second, places=None, msg=None, delta=None) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase assertAlmostEqualRelError(self, first, second, rel, msg=None) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase assertEqual(self, first, second, msg=None) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs - assertRaisesMsg(self, msg, ExcType, func, args, kwargs) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs + assertRaisesMsg(self, msg, ExcType, func, *args, **kwargs) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs assertSequenceEqual(self, seq1, seq2, msg=None, seq_type=None) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase FORCE_NDARRAY (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncsstatic q1(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs @@ -126,7 +133,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestComparisonUfuncs.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestComparisonUfuncs.html index f49b0eda..abbcd670 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestComparisonUfuncs.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestComparisonUfuncs.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Plugins.pint.testsuite.test_umath.TestComparisonUfuncs Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -106,8 +113,8 @@ SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs SUAVE.Plugins.pint.testsuite.TestCase - -
+ + @@ -151,9 +158,9 @@ - - + + @@ -204,7 +211,7 @@ + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestFloatingUfuncs-members.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestFloatingUfuncs-members.html index 827024e8..e02121c4 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestFloatingUfuncs-members.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestFloatingUfuncs-members.html @@ -1,9 +1,9 @@ - + - +SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ @@ -57,9 +60,11 @@

Public Member Functions

def assertEqual (self, first, second, msg=None)
 
-def assertRaisesMsg (self, msg, ExcType, func, args, kwargs)
 
+def assertRaisesMsg (self, msg, ExcType, func, *args, **kwargs)
 
- Public Member Functions inherited from SUAVE.Plugins.pint.testsuite.TestCase
def setUpClass (cls)
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -101,7 +108,7 @@ assertAlmostEqual(self, first, second, places=None, msg=None, delta=None) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase assertAlmostEqualRelError(self, first, second, rel, msg=None) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase assertEqual(self, first, second, msg=None) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs - assertRaisesMsg(self, msg, ExcType, func, args, kwargs) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs + assertRaisesMsg(self, msg, ExcType, func, *args, **kwargs) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs assertSequenceEqual(self, seq1, seq2, msg=None, seq_type=None) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase FORCE_NDARRAY (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncsstatic q1(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs @@ -135,7 +142,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestFloatingUfuncs.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestFloatingUfuncs.html index 6ccf7feb..d1d2868c 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestFloatingUfuncs.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestFloatingUfuncs.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Plugins.pint.testsuite.test_umath.TestFloatingUfuncs Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -106,8 +113,8 @@ SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs SUAVE.Plugins.pint.testsuite.TestCase - -
+ + @@ -178,9 +185,9 @@ - - + + @@ -240,7 +247,7 @@ + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestMathUfuncs-members.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestMathUfuncs-members.html index 09807270..2575f561 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestMathUfuncs-members.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestMathUfuncs-members.html @@ -1,9 +1,9 @@ - + - +SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ @@ -57,9 +60,11 @@

Public Member Functions

def assertEqual (self, first, second, msg=None)
 
-def assertRaisesMsg (self, msg, ExcType, func, args, kwargs)
 
+def assertRaisesMsg (self, msg, ExcType, func, *args, **kwargs)
 
- Public Member Functions inherited from SUAVE.Plugins.pint.testsuite.TestCase
def setUpClass (cls)
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -101,7 +108,7 @@ assertAlmostEqual(self, first, second, places=None, msg=None, delta=None) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase assertAlmostEqualRelError(self, first, second, rel, msg=None) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase assertEqual(self, first, second, msg=None) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs - assertRaisesMsg(self, msg, ExcType, func, args, kwargs) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs + assertRaisesMsg(self, msg, ExcType, func, *args, **kwargs) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs assertSequenceEqual(self, seq1, seq2, msg=None, seq_type=None) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase FORCE_NDARRAY (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncsstatic q1(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs @@ -144,7 +151,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestMathUfuncs.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestMathUfuncs.html index e8385c41..b13acc34 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestMathUfuncs.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestMathUfuncs.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Plugins.pint.testsuite.test_umath.TestMathUfuncs Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -106,8 +113,8 @@ SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs SUAVE.Plugins.pint.testsuite.TestCase - -
+ + @@ -205,9 +212,9 @@ - - + + @@ -280,7 +287,7 @@ + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestTrigUfuncs-members.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestTrigUfuncs-members.html index e42bb591..51549bbb 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestTrigUfuncs-members.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestTrigUfuncs-members.html @@ -1,9 +1,9 @@ - + - +SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ @@ -57,9 +60,11 @@

Public Member Functions

def assertEqual (self, first, second, msg=None)
 
-def assertRaisesMsg (self, msg, ExcType, func, args, kwargs)
 
+def assertRaisesMsg (self, msg, ExcType, func, *args, **kwargs)
 
- Public Member Functions inherited from SUAVE.Plugins.pint.testsuite.TestCase
def setUpClass (cls)
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -101,7 +108,7 @@ assertAlmostEqual(self, first, second, places=None, msg=None, delta=None) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase assertAlmostEqualRelError(self, first, second, rel, msg=None) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase assertEqual(self, first, second, msg=None) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs - assertRaisesMsg(self, msg, ExcType, func, args, kwargs) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs + assertRaisesMsg(self, msg, ExcType, func, *args, **kwargs) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs assertSequenceEqual(self, seq1, seq2, msg=None, seq_type=None) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase FORCE_NDARRAY (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncsstatic q1(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs @@ -136,7 +143,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestTrigUfuncs.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestTrigUfuncs.html index 165edb15..a4d3b915 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestTrigUfuncs.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestTrigUfuncs.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Plugins.pint.testsuite.test_umath.TestTrigUfuncs Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -106,8 +113,8 @@ SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs SUAVE.Plugins.pint.testsuite.TestCase - -
+ + @@ -181,9 +188,9 @@ - - + + @@ -244,7 +251,7 @@ + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestUFuncs-members.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestUFuncs-members.html index fe484478..5700e4f0 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestUFuncs-members.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestUFuncs-members.html @@ -1,9 +1,9 @@ - + - +SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ @@ -57,9 +60,11 @@

Public Member Functions

def assertEqual (self, first, second, msg=None)
 
-def assertRaisesMsg (self, msg, ExcType, func, args, kwargs)
 
+def assertRaisesMsg (self, msg, ExcType, func, *args, **kwargs)
 
- Public Member Functions inherited from SUAVE.Plugins.pint.testsuite.TestCase
def setUpClass (cls)
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -101,7 +108,7 @@ assertAlmostEqual(self, first, second, places=None, msg=None, delta=None) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase assertAlmostEqualRelError(self, first, second, rel, msg=None) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase assertEqual(self, first, second, msg=None) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs - assertRaisesMsg(self, msg, ExcType, func, args, kwargs) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs + assertRaisesMsg(self, msg, ExcType, func, *args, **kwargs) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs assertSequenceEqual(self, seq1, seq2, msg=None, seq_type=None) (defined in SUAVE.Plugins.pint.testsuite.TestCase)SUAVE.Plugins.pint.testsuite.TestCase FORCE_NDARRAY (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncsstatic q1(self) (defined in SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs)SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs @@ -120,7 +127,7 @@
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diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestUFuncs.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestUFuncs.html index b12a2f6d..ca461da3 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestUFuncs.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestUFuncs.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Plugins.pint.testsuite.test_umath.TestUFuncs Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -112,8 +119,8 @@ SUAVE.Plugins.pint.testsuite.test_umath.TestFloatingUfuncs SUAVE.Plugins.pint.testsuite.test_umath.TestMathUfuncs SUAVE.Plugins.pint.testsuite.test_umath.TestTrigUfuncs - -
+ + @@ -138,9 +145,9 @@ - - + + @@ -182,7 +189,7 @@ + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestUFuncs.js b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestUFuncs.js index f086140c..a9aa4bfe 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestUFuncs.js +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestUFuncs.js @@ -1,7 +1,7 @@ var classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestUFuncs = [ [ "assertEqual", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestUFuncs.html#a0c0e2b1e640261526b45d75815041eed", null ], - [ "assertRaisesMsg", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestUFuncs.html#af0f187e9627726c315aa2addfc3372b8", null ], + [ "assertRaisesMsg", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestUFuncs.html#a0d683aa00ff259ade2ecfbf37648d833", null ], [ "q1", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestUFuncs.html#a369fea855eac711f52da20a83b2c42f7", null ], [ "q2", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestUFuncs.html#ad738197b70e5b38c835aa534e623fa0d", null ], [ "qi", "classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__umath_1_1TestUFuncs.html#acaa99eee28562bc9eeb3b5a925ad7cf1", null ], diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestConverter-members.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestConverter-members.html index 05944554..b75208d6 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestConverter-members.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestConverter-members.html @@ -1,9 +1,9 @@ - + - +SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ @@ -57,9 +60,11 @@

Public Member Functions

def assertEqual (self, first, second, msg=None)
 
-def assertRaisesMsg (self, msg, ExcType, func, args, kwargs)
 
+def assertRaisesMsg (self, msg, ExcType, func, *args, **kwargs)
 
- Public Member Functions inherited from SUAVE.Plugins.pint.testsuite.TestCase
def setUpClass (cls)
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -107,7 +114,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestConverter.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestConverter.html index edb572fd..08b194ca 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestConverter.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestConverter.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Plugins.pint.testsuite.test_unit.TestConverter Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -102,9 +109,7 @@ Inheritance diagram for SUAVE.Plugins.pint.testsuite.test_unit.TestConverter:
- - - +
@@ -57,9 +60,11 @@

@@ -127,7 +132,7 @@ + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestDefinition-members.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestDefinition-members.html index 01b415dc..86825902 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestDefinition-members.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestDefinition-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -109,7 +116,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestDefinition.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestDefinition.html index bd6a7c65..fefabdea 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestDefinition.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestDefinition.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Plugins.pint.testsuite.test_unit.TestDefinition Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -102,9 +109,7 @@ Inheritance diagram for SUAVE.Plugins.pint.testsuite.test_unit.TestDefinition:
- - - +
@@ -57,9 +60,11 @@

@@ -133,7 +138,7 @@ + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestRegistry-members.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestRegistry-members.html index 14b65555..e2e71543 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestRegistry-members.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestRegistry-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -127,7 +134,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestRegistry.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestRegistry.html index 1240bf3b..204d4120 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestRegistry.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestRegistry.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Plugins.pint.testsuite.test_unit.TestRegistry Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -106,8 +113,8 @@ SUAVE.Plugins.pint.testsuite.TestCase - -
+ + @@ -216,7 +223,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestUnitsContainer-members.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestUnitsContainer-members.html index d0e9f55e..7c5daf52 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestUnitsContainer-members.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestUnitsContainer-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Member Functions

SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -111,7 +118,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestUnitsContainer.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestUnitsContainer.html index 21d16833..2140f006 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestUnitsContainer.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__unit_1_1TestUnitsContainer.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Plugins.pint.testsuite.test_unit.TestUnitsContainer Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -102,9 +109,7 @@ Inheritance diagram for SUAVE.Plugins.pint.testsuite.test_unit.TestUnitsContainer:
- - - +
@@ -57,9 +60,11 @@

@@ -139,7 +144,7 @@ + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__util_1_1TestStringProcessor-members.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__util_1_1TestStringProcessor-members.html index 3b8b011f..dd79d501 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__util_1_1TestStringProcessor-members.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__util_1_1TestStringProcessor-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -107,7 +114,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__util_1_1TestStringProcessor.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__util_1_1TestStringProcessor.html index 00013c86..42892669 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__util_1_1TestStringProcessor.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1testsuite_1_1test__util_1_1TestStringProcessor.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Plugins.pint.testsuite.test_util.TestStringProcessor Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -102,9 +109,7 @@ Inheritance diagram for SUAVE.Plugins.pint.testsuite.test_util.TestStringProcessor:
- - - +
@@ -57,9 +60,11 @@

@@ -127,7 +132,7 @@ + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1Converter-members.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1Converter-members.html index 5d4eaaea..d11088c2 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1Converter-members.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1Converter-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -107,7 +114,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1Converter.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1Converter.html index e3a1935b..845a755e 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1Converter.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1Converter.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Plugins.pint.unit.Converter Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -106,8 +113,8 @@ SUAVE.Plugins.pint.unit.OffsetConverter SUAVE.Plugins.pint.unit.ScaleConverter - -
+ + @@ -131,7 +138,7 @@ + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1Definition-members.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1Definition-members.html index be8f9a3f..45077c84 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1Definition-members.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1Definition-members.html @@ -1,9 +1,9 @@ - + - +SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ @@ -57,9 +60,11 @@

Public Member Functions

SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -112,7 +119,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1Definition.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1Definition.html index af921960..e2ba2c9d 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1Definition.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1Definition.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Plugins.pint.unit.Definition Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -107,8 +114,8 @@ SUAVE.Plugins.pint.unit.DimensionDefinition SUAVE.Plugins.pint.unit.PrefixDefinition SUAVE.Plugins.pint.unit.UnitDefinition - -
+ + @@ -181,7 +188,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1DimensionDefinition-members.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1DimensionDefinition-members.html index eceed6aa..608c6d98 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1DimensionDefinition-members.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1DimensionDefinition-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Member Functions

SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -115,7 +122,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1DimensionDefinition.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1DimensionDefinition.html index e23cb84b..0a844905 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1DimensionDefinition.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1DimensionDefinition.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Plugins.pint.unit.DimensionDefinition Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -106,8 +113,8 @@ SUAVE.Plugins.pint.unit.Definition - -
+ + @@ -158,7 +165,7 @@ + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1DimensionalityError-members.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1DimensionalityError-members.html index 2bdc147b..45bb66cc 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1DimensionalityError-members.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1DimensionalityError-members.html @@ -1,9 +1,9 @@ - + - +SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ @@ -57,9 +60,11 @@

Public Member Functions

SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -111,7 +118,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1DimensionalityError.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1DimensionalityError.html index 9f8e5824..22672401 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1DimensionalityError.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1DimensionalityError.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Plugins.pint.unit.DimensionalityError Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -103,9 +110,7 @@ Inheritance diagram for SUAVE.Plugins.pint.unit.DimensionalityError:
- - - +
@@ -57,9 +60,11 @@

@@ -145,7 +150,7 @@ + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1OffsetConverter-members.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1OffsetConverter-members.html index b144f9ae..4e5abe47 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1OffsetConverter-members.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1OffsetConverter-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -110,7 +117,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1OffsetConverter.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1OffsetConverter.html index 68ea4c42..c003ad9f 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1OffsetConverter.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1OffsetConverter.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Plugins.pint.unit.OffsetConverter Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -106,8 +113,8 @@ SUAVE.Plugins.pint.unit.Converter - -
+ + @@ -120,13 +127,6 @@ - - - - -

Public Member Functions

def from_reference (self, value)
 
- Public Member Functions inherited from SUAVE.Plugins.pint.unit.Converter
-def to_reference (self, value)
 
-def from_reference (self, value)
 
@@ -150,7 +150,7 @@ + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1PrefixDefinition-members.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1PrefixDefinition-members.html index f7d82d72..c3bbc456 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1PrefixDefinition-members.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1PrefixDefinition-members.html @@ -1,9 +1,9 @@ - + - +SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ @@ -57,9 +60,11 @@

Public Attributes

SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -112,7 +119,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1PrefixDefinition.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1PrefixDefinition.html index 5ddab04a..51fad00c 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1PrefixDefinition.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1PrefixDefinition.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Plugins.pint.unit.PrefixDefinition Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -105,8 +112,8 @@ SUAVE.Plugins.pint.unit.Definition - -
+ + @@ -114,9 +121,6 @@ def  - - @@ -57,9 +60,11 @@

Public Member Functions

__init__ (self, name, symbol, aliases, converter)
 
- Public Member Functions inherited from SUAVE.Plugins.pint.unit.Definition
-def __init__ (self, name, symbol, aliases, converter)
 
def from_string (cls, definition)
 
@@ -148,7 +152,7 @@ + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1ScaleConverter-members.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1ScaleConverter-members.html index 95a00787..dbfee516 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1ScaleConverter-members.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1ScaleConverter-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -109,7 +116,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1ScaleConverter.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1ScaleConverter.html index 7d0b58c6..50590aa3 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1ScaleConverter.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1ScaleConverter.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Plugins.pint.unit.ScaleConverter Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -106,8 +113,8 @@ SUAVE.Plugins.pint.unit.Converter - -
+ + @@ -120,13 +127,6 @@ - - - - -

Public Member Functions

def from_reference (self, value)
 
- Public Member Functions inherited from SUAVE.Plugins.pint.unit.Converter
-def to_reference (self, value)
 
-def from_reference (self, value)
 
@@ -147,7 +147,7 @@ + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UndefinedUnitError-members.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UndefinedUnitError-members.html index 6ba8afaf..3e3e0b24 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UndefinedUnitError-members.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UndefinedUnitError-members.html @@ -1,9 +1,9 @@ - + - +SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ @@ -57,9 +60,11 @@

Public Attributes

SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -108,7 +115,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UndefinedUnitError.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UndefinedUnitError.html index 8069616e..4ea630cd 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UndefinedUnitError.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UndefinedUnitError.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Plugins.pint.unit.UndefinedUnitError Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -103,9 +110,7 @@ Inheritance diagram for SUAVE.Plugins.pint.unit.UndefinedUnitError:
- - - +
@@ -57,9 +60,11 @@

@@ -136,7 +141,7 @@ + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitDefinition-members.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitDefinition-members.html index 01b45cf7..0616f10d 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitDefinition-members.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitDefinition-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -115,7 +122,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitDefinition.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitDefinition.html index addafb2c..1bda64ca 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitDefinition.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitDefinition.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Plugins.pint.unit.UnitDefinition Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -106,8 +113,8 @@ SUAVE.Plugins.pint.unit.Definition - -
+ + @@ -161,7 +168,7 @@ + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry-members.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry-members.html index 3bd05f81..5e7d6fb0 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry-members.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry-members.html @@ -1,9 +1,9 @@ - + - +SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ @@ -57,9 +60,11 @@

Public Member Functions

SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -103,20 +110,20 @@ __getitem__(self, item) (defined in SUAVE.Plugins.pint.unit.UnitRegistry)SUAVE.Plugins.pint.unit.UnitRegistry __init__(self, filename='', force_ndarray=False, default_to_delta=True) (defined in SUAVE.Plugins.pint.unit.UnitRegistry)SUAVE.Plugins.pint.unit.UnitRegistry add_context(self, context)SUAVE.Plugins.pint.unit.UnitRegistry - context(self, names, kwargs)SUAVE.Plugins.pint.unit.UnitRegistry + context(self, *names, **kwargs)SUAVE.Plugins.pint.unit.UnitRegistry convert(self, value, src, dst)SUAVE.Plugins.pint.unit.UnitRegistry default_format(self)SUAVE.Plugins.pint.unit.UnitRegistry default_format(self, value) (defined in SUAVE.Plugins.pint.unit.UnitRegistry)SUAVE.Plugins.pint.unit.UnitRegistry default_to_delta (defined in SUAVE.Plugins.pint.unit.UnitRegistry)SUAVE.Plugins.pint.unit.UnitRegistry define(self, definition)SUAVE.Plugins.pint.unit.UnitRegistry disable_contexts(self, n=None)SUAVE.Plugins.pint.unit.UnitRegistry - enable_contexts(self, names_or_contexts, kwargs)SUAVE.Plugins.pint.unit.UnitRegistry + enable_contexts(self, *names_or_contexts, **kwargs)SUAVE.Plugins.pint.unit.UnitRegistry get_base_units(self, input_units)SUAVE.Plugins.pint.unit.UnitRegistry get_dimensionality(self, input_units)SUAVE.Plugins.pint.unit.UnitRegistry get_name(self, name_or_alias)SUAVE.Plugins.pint.unit.UnitRegistry get_symbol(self, name_or_alias)SUAVE.Plugins.pint.unit.UnitRegistry load_definitions(self, file, is_resource=False)SUAVE.Plugins.pint.unit.UnitRegistry - parse_expression(self, input_string, values)SUAVE.Plugins.pint.unit.UnitRegistry + parse_expression(self, input_string, **values)SUAVE.Plugins.pint.unit.UnitRegistry parse_unit_name(self, unit_name)SUAVE.Plugins.pint.unit.UnitRegistry parse_units(self, input_string, to_delta=None)SUAVE.Plugins.pint.unit.UnitRegistry pi_theorem(self, quantities)SUAVE.Plugins.pint.unit.UnitRegistry @@ -131,7 +138,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry.html index b2a0cf9a..b26d7c13 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Plugins.pint.unit.UnitRegistry Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -103,9 +110,7 @@ Inheritance diagram for SUAVE.Plugins.pint.unit.UnitRegistry:
- - - +
- + - - + + - - + + @@ -159,8 +164,8 @@ - - + +

@@ -127,16 +132,16 @@

def default_format (self, value)
 
def add_context (self, context)
def add_context (self, context)
 
def remove_context (self, name_or_alias)
 
def enable_contexts (self, names_or_contexts, kwargs)
 
def enable_contexts (self, *names_or_contexts, **kwargs)
 
def disable_contexts (self, n=None)
 
def context (self, names, kwargs)
 
def context (self, *names, **kwargs)
 
def define (self, definition)
 
def load_definitions (self, file, is_resource=False)
 
def parse_units (self, input_string, to_delta=None)
 
def parse_expression (self, input_string, values)
 
def parse_expression (self, input_string, **values)
 
def wraps (self, ret, args, strict=True)
 
@@ -217,8 +222,8 @@

-

◆ context()

+ +

◆ context()

@@ -232,13 +237,13 @@

- + - + @@ -409,8 +414,8 @@

-

◆ enable_contexts()

+ +

◆ enable_contexts()

@@ -424,13 +429,13 @@

- + - + @@ -607,8 +612,8 @@

-

◆ parse_expression()

+ +

◆ parse_expression()

@@ -628,7 +633,7 @@

- + @@ -874,7 +879,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry.js b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry.js index 50a27be8..390ca26d 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry.js +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry.js @@ -5,19 +5,19 @@ var classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry = [ "__getattr__", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry.html#ac33b542eb0eeea598bae96697b189a43", null ], [ "__getitem__", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry.html#a11e5efd5afad852f9682b4deea4bf137", null ], [ "add_context", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry.html#ad8dae43dc3a09546da8da6bc5999c12f", null ], - [ "context", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry.html#aeff4a616272690ba06ee479f8e22ce8e", null ], + [ "context", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry.html#a8b7d034907ecbf7a7a44f8cfc9f708db", null ], [ "convert", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry.html#a82fa3e84687f39f5dd80025393e92379", null ], [ "default_format", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry.html#add51f2c695a5642f18b8e8c1bfe18b92", null ], [ "default_format", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry.html#a066a3b0927b04e46fc8c41033291b5af", null ], [ "define", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry.html#ad425bb5f74509eb34c5719e602973151", null ], [ "disable_contexts", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry.html#a0bb62e9743a85b15186679308dda1c13", null ], - [ "enable_contexts", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry.html#a36d3fc68e8e142fd5f9a0c687cd61b60", null ], + [ "enable_contexts", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry.html#a3e78ddd3d5827de8b10eec11993fc952", null ], [ "get_base_units", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry.html#a7efb7e1108fc7b043804b80c54605f4f", null ], [ "get_dimensionality", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry.html#addb56049afe22c3ee7700905c1d35559", null ], [ "get_name", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry.html#a52fc0919e39a5ed8fe52b74db841ad2f", null ], [ "get_symbol", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry.html#a231bac0fb58eed32470c45563c97525d", null ], [ "load_definitions", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry.html#af207ae7d1ba346823ca5cf012db5fde0", null ], - [ "parse_expression", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry.html#acd7fda180374b5f9e201f3d912cd472d", null ], + [ "parse_expression", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry.html#a6f482a0680a92a68597562536b66afd7", null ], [ "parse_unit_name", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry.html#ad6d0be3333825fca3e8899da06caa654", null ], [ "parse_units", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry.html#a4686109f23abf7863f7a5f13f5b3b910", null ], [ "pi_theorem", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitRegistry.html#abcaeffa218bba609463a749926fa070f", null ], diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitsContainer-members.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitsContainer-members.html index d1fe9ca6..905d5a61 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitsContainer-members.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitsContainer-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@
  names,
 **  kwargs 
  names_or_contexts,
 **  kwargs 
 **  values 
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitsContainer.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitsContainer.html index c8b19be9..ce2a435b 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitsContainer.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitsContainer.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Plugins.pint.unit.UnitsContainer Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -102,16 +109,14 @@ Inheritance diagram for SUAVE.Plugins.pint.unit.UnitsContainer:
- - - +
- - + + @@ -172,7 +177,7 @@ + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitsContainer.js b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitsContainer.js index c634ffe3..079d5d43 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitsContainer.js +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitsContainer.js @@ -1,6 +1,6 @@ var classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitsContainer = [ - [ "__init__", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitsContainer.html#abd5b9d529b8ac7790cef30323dd7733a", null ], + [ "__init__", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitsContainer.html#aa63f2604568713daf19715a57960d5fa", null ], [ "__copy__", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitsContainer.html#a3d53d1f6aa698a55f153920d76f3c0a6", null ], [ "__eq__", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitsContainer.html#a1eddb87e46ff10130f0f129e9f14455e", null ], [ "__format__", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitsContainer.html#abafa11b17931a1f2fa64551686e2837a", null ], diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1util_1_1ParserHelper-members.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1util_1_1ParserHelper-members.html index 8f413168..04b4c92a 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1util_1_1ParserHelper-members.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1util_1_1ParserHelper-members.html @@ -1,9 +1,9 @@ - + - +SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ @@ -57,9 +60,11 @@

Public Member Functions

-def __init__ (self, args, kwargs)
 
+def __init__ (self, *args, **kwargs)
 
def __missing__ (self, key)
 
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -98,7 +105,7 @@

This is the complete list of members for SUAVE.Plugins.pint.util.ParserHelper, including all inherited members.

- + @@ -118,7 +125,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1util_1_1ParserHelper.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1util_1_1ParserHelper.html index 8fd6806c..4475f4da 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1util_1_1ParserHelper.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1util_1_1ParserHelper.html @@ -1,9 +1,9 @@ - + - +SUAVE: SUAVE.Plugins.pint.util.ParserHelper Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ @@ -57,9 +60,11 @@
__init__(self, scale=1, args, kwargs) (defined in SUAVE.Plugins.pint.util.ParserHelper)SUAVE.Plugins.pint.util.ParserHelper
__init__(self, scale=1, *args, **kwargs) (defined in SUAVE.Plugins.pint.util.ParserHelper)SUAVE.Plugins.pint.util.ParserHelper
__missing__(self, key) (defined in SUAVE.Plugins.pint.util.ParserHelper)SUAVE.Plugins.pint.util.ParserHelper
__mul__(self, other) (defined in SUAVE.Plugins.pint.util.ParserHelper)SUAVE.Plugins.pint.util.ParserHelper
__pow__(self, other) (defined in SUAVE.Plugins.pint.util.ParserHelper)SUAVE.Plugins.pint.util.ParserHelper
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -103,16 +110,14 @@ Inheritance diagram for SUAVE.Plugins.pint.util.ParserHelper:
- - - +
- - + + @@ -225,7 +230,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1util_1_1ParserHelper.js b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1util_1_1ParserHelper.js index 2fb6bc09..124a8ea4 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1util_1_1ParserHelper.js +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1util_1_1ParserHelper.js @@ -1,6 +1,6 @@ var classSUAVE_1_1Plugins_1_1pint_1_1util_1_1ParserHelper = [ - [ "__init__", "classSUAVE_1_1Plugins_1_1pint_1_1util_1_1ParserHelper.html#a12668c59c16e90b2155712517c441dd2", null ], + [ "__init__", "classSUAVE_1_1Plugins_1_1pint_1_1util_1_1ParserHelper.html#a31d435bed9386b8799be0d604b66160e", null ], [ "__missing__", "classSUAVE_1_1Plugins_1_1pint_1_1util_1_1ParserHelper.html#a9c5c4db62dfa441bfa2d7b68ad58004c", null ], [ "__mul__", "classSUAVE_1_1Plugins_1_1pint_1_1util_1_1ParserHelper.html#a5e70f6d38c62aedf089276a599221f95", null ], [ "__pow__", "classSUAVE_1_1Plugins_1_1pint_1_1util_1_1ParserHelper.html#abf72397f2627620e4537fcc06bd536cc", null ], diff --git a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1util_1_1ndarray.html b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1util_1_1ndarray.html index 32b31904..38c04f4b 100644 --- a/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1util_1_1ndarray.html +++ b/doxygen/classSUAVE_1_1Plugins_1_1pint_1_1util_1_1ndarray.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Plugins.pint.util.ndarray Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Member Functions

-def __init__ (self, scale=1, args, kwargs)
 
+def __init__ (self, scale=1, *args, **kwargs)
 
def from_word (cls, input_word)
 
def from_string (cls, input_string)
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -99,9 +106,7 @@ Inheritance diagram for SUAVE.Plugins.pint.util.ndarray:
- - - +

The documentation for this class was generated from the following file:
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Plugins/pint/util.py
  • @@ -114,7 +119,7 @@ + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop-members.html b/doxygen/classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop-members.html deleted file mode 100644 index 392588ca..00000000 --- a/doxygen/classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop-members.html +++ /dev/null @@ -1,147 +0,0 @@ - - - - - - - -SUAVE: Member List - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.1.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
-
- - - -
-
- -
-
-
- -
- -
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- -
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-
SUAVE.Sizing.Sizing_Loop.Sizing_Loop Member List
-
-
- -

This is the complete list of members for SUAVE.Sizing.Sizing_Loop.Sizing_Loop, including all inherited members.

- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
__defaults__(self)SUAVE.Sizing.Sizing_Loop.Sizing_Loop
__delattr__(self, k)SUAVE.Core.Data.Data
__getattribute__(self, k)SUAVE.Core.Data.Data
__init__(self, args, kwarg)SUAVE.Core.Data.Data
__iter__(self)SUAVE.Core.Data.Data
__new__(cls, args, kwarg)SUAVE.Core.Data.Data
__setattr__(self, k, v)SUAVE.Core.Data.Data
__str__(self, indent='')SUAVE.Core.Data.Data
append(self, value, key=None)SUAVE.Core.Data.Data
broyden_update(self, y, err, sizing_evaluation, nexus, scaling, iter, iteration_options)SUAVE.Sizing.Sizing_Loop.Sizing_Loop
damped_newton_update(self, y, err, sizing_evaluation, nexus, scaling, iter, iteration_options) (defined in SUAVE.Sizing.Sizing_Loop.Sizing_Loop)SUAVE.Sizing.Sizing_Loop.Sizing_Loop
dataname(self)SUAVE.Core.Data.Data
deep_get(self, keys)SUAVE.Core.Data.Data
deep_set(self, keys, val)SUAVE.Core.Data.Data
default_scaling (defined in SUAVE.Sizing.Sizing_Loop.Sizing_Loop)SUAVE.Sizing.Sizing_Loop.Sizing_Loop
default_y (defined in SUAVE.Sizing.Sizing_Loop.Sizing_Loop)SUAVE.Sizing.Sizing_Loop.Sizing_Loop
do_recursive(self, method, other=None, default=None)SUAVE.Core.Data.Data
evaluate(self, nexus) (defined in SUAVE.Sizing.Sizing_Loop.Sizing_Loop)SUAVE.Sizing.Sizing_Loop.Sizing_Loop
get_bases(self)SUAVE.Core.Data.Data
initial_step (defined in SUAVE.Sizing.Sizing_Loop.Sizing_Loop)SUAVE.Sizing.Sizing_Loop.Sizing_Loop
iteration_options (defined in SUAVE.Sizing.Sizing_Loop.Sizing_Loop)SUAVE.Sizing.Sizing_Loop.Sizing_Loop
itervalues(self)SUAVE.Core.Data.Data
maximum_iterations (defined in SUAVE.Sizing.Sizing_Loop.Sizing_Loop)SUAVE.Sizing.Sizing_Loop.Sizing_Loop
newton_raphson_update(self, y, err, sizing_evaluation, nexus, scaling, iter, iteration_options)SUAVE.Sizing.Sizing_Loop.Sizing_Loop
output_filename (defined in SUAVE.Sizing.Sizing_Loop.Sizing_Loop)SUAVE.Sizing.Sizing_Loop.Sizing_Loop
pack_array(self, output='vector')SUAVE.Core.Data.Data
sizing_evaluation (defined in SUAVE.Sizing.Sizing_Loop.Sizing_Loop)SUAVE.Sizing.Sizing_Loop.Sizing_Loop
successive_substitution_update(self, y, err, sizing_evaluation, nexus, scaling, iter, iteration_options)SUAVE.Sizing.Sizing_Loop.Sizing_Loop
tolerance (defined in SUAVE.Sizing.Sizing_Loop.Sizing_Loop)SUAVE.Sizing.Sizing_Loop.Sizing_Loop
typestring(self)SUAVE.Core.Data.Data
unpack_array(self, M)SUAVE.Core.Data.Data
update(self, other)SUAVE.Core.Data.Data
update_method (defined in SUAVE.Sizing.Sizing_Loop.Sizing_Loop)SUAVE.Sizing.Sizing_Loop.Sizing_Loop
values(self)SUAVE.Core.Data.Data
write_threshhold (defined in SUAVE.Sizing.Sizing_Loop.Sizing_Loop)SUAVE.Sizing.Sizing_Loop.Sizing_Loop
-
- - - - diff --git a/doxygen/classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.html b/doxygen/classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.html deleted file mode 100644 index 211dd940..00000000 --- a/doxygen/classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.html +++ /dev/null @@ -1,437 +0,0 @@ - - - - - - - -SUAVE: SUAVE.Sizing.Sizing_Loop.Sizing_Loop Class Reference - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.1.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
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- - - -
-
- -
-
-
- -
- -
-
- - -
- -
- -
- -
-
SUAVE.Sizing.Sizing_Loop.Sizing_Loop Class Reference
-
-
-
-Inheritance diagram for SUAVE.Sizing.Sizing_Loop.Sizing_Loop:
-
-
- - -SUAVE.Core.Data.Data - -
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

-Public Member Functions

def __defaults__ (self)
 
-def evaluate (self, nexus)
 
def successive_substitution_update (self, y, err, sizing_evaluation, nexus, scaling, iter, iteration_options)
 
def newton_raphson_update (self, y, err, sizing_evaluation, nexus, scaling, iter, iteration_options)
 
def broyden_update (self, y, err, sizing_evaluation, nexus, scaling, iter, iteration_options)
 
-def damped_newton_update (self, y, err, sizing_evaluation, nexus, scaling, iter, iteration_options)
 
- Public Member Functions inherited from SUAVE.Core.Data.Data
def __getattribute__ (self, k)
 
def __setattr__ (self, k, v)
 
def __delattr__ (self, k)
 
def __defaults__ (self)
 
def __new__ (cls, args, kwarg)
 
def typestring (self)
 
def dataname (self)
 
def __str__ (self, indent='')
 
def __init__ (self, args, kwarg)
 
def __iter__ (self)
 
def itervalues (self)
 
def values (self)
 
def update (self, other)
 
def get_bases (self)
 
def append (self, value, key=None)
 
def deep_set (self, keys, val)
 
def deep_get (self, keys)
 
def pack_array (self, output='vector')
 
def unpack_array (self, M)
 
def do_recursive (self, method, other=None, default=None)
 
- - - - - - - - - - - - - - - - - - - - - -

-Public Attributes

tolerance
 
initial_step
 
update_method
 
default_y
 
default_scaling
 
maximum_iterations
 
output_filename
 
sizing_evaluation
 
write_threshhold
 
iteration_options
 
-

Member Function Documentation

- -

◆ __defaults__()

- -
-
- - - - - - - - -
def SUAVE.Sizing.Sizing_Loop.Sizing_Loop.__defaults__ ( self)
-
-
Data class that solves a fixed point iteration problem to size the aircraft. Includes
-a variety of methods to solve the subproblem, including successive substitution, newton-raphson,
-broyden's method, as well as a damped newton method. Also includes machine learning algorithms
-from scikit-learn to aid in finding a good initial guess for your sizing parameters.
-
-
-
- -

◆ broyden_update()

- -
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- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Sizing.Sizing_Loop.Sizing_Loop.broyden_update ( self,
 y,
 err,
 sizing_evaluation,
 nexus,
 scaling,
 iter,
 iteration_options 
)
-
-
uses an approximation to update the Jacobian without
-the use of finite differencing
-
-
- -

◆ newton_raphson_update()

- -
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def SUAVE.Sizing.Sizing_Loop.Sizing_Loop.newton_raphson_update ( self,
 y,
 err,
 sizing_evaluation,
 nexus,
 scaling,
 iter,
 iteration_options 
)
-
-
Finite differences the problem to calculate the Jacobian, then
-tries to use that to zero the residual
-
-
-
- -

◆ successive_substitution_update()

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def SUAVE.Sizing.Sizing_Loop.Sizing_Loop.successive_substitution_update ( self,
 y,
 err,
 sizing_evaluation,
 nexus,
 scaling,
 iter,
 iteration_options 
)
-
-
Uses a successive substitution update to try to zero the residual
-
-
-
-
The documentation for this class was generated from the following file:
    -
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Sizing/Sizing_Loop.py
  • -
-
-
- - - - diff --git a/doxygen/classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.js b/doxygen/classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.js deleted file mode 100644 index a25366f3..00000000 --- a/doxygen/classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.js +++ /dev/null @@ -1,19 +0,0 @@ -var classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop = -[ - [ "__defaults__", "classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.html#a178ec5c05131960d4fa8d5ad6e3c3e11", null ], - [ "broyden_update", "classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.html#a52d275bd606778420dde57df5c710ced", null ], - [ "damped_newton_update", "classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.html#a5942e4cd16b9a18ed372e79d4e8dbd70", null ], - [ "evaluate", "classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.html#a153a6ac6de2d18f130320b5e871756de", null ], - [ "newton_raphson_update", "classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.html#afee06f0c84b5023393a68b8163024939", null ], - [ "successive_substitution_update", "classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.html#a4222e0b4efa8045836ef6fb1ba94a6f3", null ], - [ "default_scaling", "classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.html#addd0442dc00517c1db5c0de356e75e68", null ], - [ "default_y", "classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.html#ac3d271509f69df8f90e10e2bf709413e", null ], - [ "initial_step", "classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.html#a5afe4453cdff685473f8f94cb6f054df", null ], - [ "iteration_options", "classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.html#af4d73d77d7b7748b08cd8e5f6cedf4fd", null ], - [ "maximum_iterations", "classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.html#a880e2af1ba6856fd9ba640aaa2b78136", null ], - [ "output_filename", "classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.html#a8bd8cbf5a638d448371e44a2f59fb4bd", null ], - [ "sizing_evaluation", "classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.html#aa9f5e946792b134387052287be34a531", null ], - [ "tolerance", "classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.html#ab945e6e09e3783f41580e291da29559f", null ], - [ "update_method", "classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.html#a82aceccafa7e1f519154a06057f02fe9", null ], - [ "write_threshhold", "classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.html#afb271146361bd7c3157ded88876df9e9", null ] -]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.png b/doxygen/classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.png deleted file mode 100644 index 1a60e12c..00000000 Binary files a/doxygen/classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.png and /dev/null differ diff --git a/doxygen/classSUAVE_1_1Surrogate_1_1Surrogate__Problem_1_1Surrogate__Problem-members.html b/doxygen/classSUAVE_1_1Surrogate_1_1Surrogate__Problem_1_1Surrogate__Problem-members.html index e5544bd2..7c121e4c 100644 --- a/doxygen/classSUAVE_1_1Surrogate_1_1Surrogate__Problem_1_1Surrogate__Problem-members.html +++ b/doxygen/classSUAVE_1_1Surrogate_1_1Surrogate__Problem_1_1Surrogate__Problem-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -98,29 +105,30 @@

This is the complete list of members for SUAVE.Surrogate.Surrogate_Problem.Surrogate_Problem, including all inherited members.

- + - + - + - - - - - - - - - - - - - - + + + + + + + + + + + + + + +
__defaults__(self) (defined in SUAVE.Surrogate.Surrogate_Problem.Surrogate_Problem)SUAVE.Surrogate.Surrogate_Problem.Surrogate_Problem
__defaults__(self)SUAVE.Surrogate.Surrogate_Problem.Surrogate_Problem
__delattr__(self, k)SUAVE.Core.Data.Data
__getattribute__(self, k)SUAVE.Core.Data.Data
__init__(self, args, kwarg)SUAVE.Core.Data.Data
__init__(self, *args, **kwarg)SUAVE.Core.Data.Data
__iter__(self)SUAVE.Core.Data.Data
__new__(cls, args, kwarg)SUAVE.Core.Data.Data
__new__(cls, *args, **kwarg)SUAVE.Core.Data.Data
__setattr__(self, k, v)SUAVE.Core.Data.Data
__str__(self, indent='')SUAVE.Core.Data.Data
append(self, value, key=None)SUAVE.Core.Data.Data
compute(self, x)SUAVE.Surrogate.Surrogate_Problem.Surrogate_Problem
constraints_surrogates (defined in SUAVE.Surrogate.Surrogate_Problem.Surrogate_Problem)SUAVE.Surrogate.Surrogate_Problem.Surrogate_Problem
dataname(self)SUAVE.Core.Data.Data
deep_get(self, keys)SUAVE.Core.Data.Data
deep_set(self, keys, val)SUAVE.Core.Data.Data
do_recursive(self, method, other=None, default=None)SUAVE.Core.Data.Data
get_bases(self)SUAVE.Core.Data.Data
itervalues(self)SUAVE.Core.Data.Data
obj_surrogate (defined in SUAVE.Surrogate.Surrogate_Problem.Surrogate_Problem)SUAVE.Surrogate.Surrogate_Problem.Surrogate_Problem
pack_array(self, output='vector')SUAVE.Core.Data.Data
typestring(self)SUAVE.Core.Data.Data
unpack_array(self, M)SUAVE.Core.Data.Data
update(self, other)SUAVE.Core.Data.Data
values(self)SUAVE.Core.Data.Data
append_or_update(self, other)SUAVE.Core.Data.Data
compute(self, x)SUAVE.Surrogate.Surrogate_Problem.Surrogate_Problem
constraints_surrogates (defined in SUAVE.Surrogate.Surrogate_Problem.Surrogate_Problem)SUAVE.Surrogate.Surrogate_Problem.Surrogate_Problem
dataname(self)SUAVE.Core.Data.Data
deep_get(self, keys)SUAVE.Core.Data.Data
deep_set(self, keys, val)SUAVE.Core.Data.Data
do_recursive(self, method, other=None, default=None)SUAVE.Core.Data.Data
get_bases(self)SUAVE.Core.Data.Data
itervalues(self)SUAVE.Core.Data.Data
obj_surrogate (defined in SUAVE.Surrogate.Surrogate_Problem.Surrogate_Problem)SUAVE.Surrogate.Surrogate_Problem.Surrogate_Problem
pack_array(self, output='vector')SUAVE.Core.Data.Data
typestring(self)SUAVE.Core.Data.Data
unpack_array(self, M)SUAVE.Core.Data.Data
update(self, other)SUAVE.Core.Data.Data
values(self)SUAVE.Core.Data.Data
@@ -128,7 +136,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Surrogate_1_1Surrogate__Problem_1_1Surrogate__Problem.html b/doxygen/classSUAVE_1_1Surrogate_1_1Surrogate__Problem_1_1Surrogate__Problem.html index fc9b6464..91ac44b1 100644 --- a/doxygen/classSUAVE_1_1Surrogate_1_1Surrogate__Problem_1_1Surrogate__Problem.html +++ b/doxygen/classSUAVE_1_1Surrogate_1_1Surrogate__Problem_1_1Surrogate__Problem.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Surrogate.Surrogate_Problem.Surrogate_Problem Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -106,13 +113,12 @@ SUAVE.Core.Data.Data - -
+ + - + @@ -123,18 +129,16 @@ - - - - + + - - + + @@ -143,6 +147,8 @@ + + @@ -171,6 +177,42 @@
Callable data structure that computes a surrogate 
 prediction of the problem vs. a point x
 

Member Function Documentation

+ +

◆ __defaults__()

+ +
+
+

Public Member Functions

-def __defaults__ (self)
def __defaults__ (self)
 
def compute (self, x)
 
 
def __delattr__ (self, k)
 
def __defaults__ (self)
 
def __new__ (cls, args, kwarg)
 
def __new__ (cls, *args, **kwarg)
 
def typestring (self)
 
def dataname (self)
 
def __str__ (self, indent='')
 
def __init__ (self, args, kwarg)
 
def __init__ (self, *args, **kwarg)
 
def __iter__ (self)
 
def itervalues (self)
 
def update (self, other)
 
def append_or_update (self, other)
 
def get_bases (self)
 
def append (self, value, key=None)
+ + + + + + + +
def SUAVE.Surrogate.Surrogate_Problem.Surrogate_Problem.__defaults__ ( self)
+
+
A stub for all classes that come later
+    
+    Assumptions:
+    N/A
+    
+    Source:
+    N/A
+    
+    Inputs:
+    N/A
+    
+    Outputs:
+    N/A
+    
+    Properties Used:
+    N/A    
+
+

Reimplemented from SUAVE.Core.Data.Data.

+ +
+

◆ compute()

@@ -216,7 +258,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Vehicle_1_1Costs-members.html b/doxygen/classSUAVE_1_1Vehicle_1_1Costs-members.html index 79744c92..d20e1686 100644 --- a/doxygen/classSUAVE_1_1Vehicle_1_1Costs-members.html +++ b/doxygen/classSUAVE_1_1Vehicle_1_1Costs-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -101,26 +108,27 @@ __defaults__(self)SUAVE.Vehicle.Costs __delattr__(self, k)SUAVE.Core.Data.Data __getattribute__(self, k)SUAVE.Core.Data.Data - __init__(self, args, kwarg)SUAVE.Core.Data.Data + __init__(self, *args, **kwarg)SUAVE.Core.Data.Data __iter__(self)SUAVE.Core.Data.Data - __new__(cls, args, kwarg)SUAVE.Core.Data.Data + __new__(cls, *args, **kwarg)SUAVE.Core.Data.Data __setattr__(self, k, v)SUAVE.Core.Data.Data __str__(self, indent='')SUAVE.Core.Data.Data append(self, value, key=None)SUAVE.Core.Data.Data - dataname(self)SUAVE.Core.Data.Data - deep_get(self, keys)SUAVE.Core.Data.Data - deep_set(self, keys, val)SUAVE.Core.Data.Data - do_recursive(self, method, other=None, default=None)SUAVE.Core.Data.Data - get_bases(self)SUAVE.Core.Data.Data - industrial (defined in SUAVE.Vehicle.Costs)SUAVE.Vehicle.Costs - itervalues(self)SUAVE.Core.Data.Data - operating (defined in SUAVE.Vehicle.Costs)SUAVE.Vehicle.Costs - pack_array(self, output='vector')SUAVE.Core.Data.Data - tag (defined in SUAVE.Vehicle.Costs)SUAVE.Vehicle.Costs - typestring(self)SUAVE.Core.Data.Data - unpack_array(self, M)SUAVE.Core.Data.Data - update(self, other)SUAVE.Core.Data.Data - values(self)SUAVE.Core.Data.Data + append_or_update(self, other)SUAVE.Core.Data.Data + dataname(self)SUAVE.Core.Data.Data + deep_get(self, keys)SUAVE.Core.Data.Data + deep_set(self, keys, val)SUAVE.Core.Data.Data + do_recursive(self, method, other=None, default=None)SUAVE.Core.Data.Data + get_bases(self)SUAVE.Core.Data.Data + industrial (defined in SUAVE.Vehicle.Costs)SUAVE.Vehicle.Costs + itervalues(self)SUAVE.Core.Data.Data + operating (defined in SUAVE.Vehicle.Costs)SUAVE.Vehicle.Costs + pack_array(self, output='vector')SUAVE.Core.Data.Data + tag (defined in SUAVE.Vehicle.Costs)SUAVE.Vehicle.Costs + typestring(self)SUAVE.Core.Data.Data + unpack_array(self, M)SUAVE.Core.Data.Data + update(self, other)SUAVE.Core.Data.Data + values(self)SUAVE.Core.Data.Data
@@ -128,7 +136,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Vehicle_1_1Costs.html b/doxygen/classSUAVE_1_1Vehicle_1_1Costs.html index 9f5467dc..ad7dd0b2 100644 --- a/doxygen/classSUAVE_1_1Vehicle_1_1Costs.html +++ b/doxygen/classSUAVE_1_1Vehicle_1_1Costs.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Vehicle.Costs Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -106,8 +113,8 @@ SUAVE.Core.Data.Data - -
+ + @@ -120,18 +127,16 @@ - - - - + + - - + + @@ -140,6 +145,8 @@ + + @@ -207,6 +214,8 @@

SUAVE.Core.Data.Data.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Vehicle_1_1Vehicle-members.html b/doxygen/classSUAVE_1_1Vehicle_1_1Vehicle-members.html index 52b74d06..20dbd4c1 100644 --- a/doxygen/classSUAVE_1_1Vehicle_1_1Vehicle-members.html +++ b/doxygen/classSUAVE_1_1Vehicle_1_1Vehicle-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Member Functions

 
def __delattr__ (self, k)
 
def __defaults__ (self)
 
def __new__ (cls, args, kwarg)
 
def __new__ (cls, *args, **kwarg)
 
def typestring (self)
 
def dataname (self)
 
def __str__ (self, indent='')
 
def __init__ (self, args, kwarg)
 
def __init__ (self, *args, **kwarg)
 
def __iter__ (self)
 
def itervalues (self)
 
def update (self, other)
 
def append_or_update (self, other)
 
def get_bases (self)
 
def append (self, value, key=None)
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -101,37 +108,42 @@ __defaults__(self)SUAVE.Vehicle.Vehicle __delattr__(self, k)SUAVE.Core.Data.Data __getattribute__(self, k)SUAVE.Core.Data.Data - __init__(self, args, kwarg)SUAVE.Vehicle.Vehicle + __init__(self, *args, **kwarg)SUAVE.Vehicle.Vehicle __iter__(self)SUAVE.Core.Data.Data - __new__(cls, args, kwarg)SUAVE.Core.Data.Data + __new__(cls, *args, **kwarg)SUAVE.Core.Data.Data __setattr__(self, k, v)SUAVE.Core.Data.Data __str__(self, indent='')SUAVE.Core.Data.Data append(self, value, key=None)SUAVE.Core.Data.Data append_component(self, component)SUAVE.Vehicle.Vehicle + append_or_update(self, other)SUAVE.Core.Data.Data + center_of_gravity(self)SUAVE.Vehicle.Vehicle costs (defined in SUAVE.Vehicle.Vehicle)SUAVE.Vehicle.Vehicle dataname(self)SUAVE.Core.Data.Data deep_get(self, keys)SUAVE.Core.Data.Data deep_set(self, keys, val)SUAVE.Core.Data.Data do_recursive(self, method, other=None, default=None)SUAVE.Core.Data.Data - energy (defined in SUAVE.Vehicle.Vehicle)SUAVE.Vehicle.Vehicle - envelope (defined in SUAVE.Vehicle.Vehicle)SUAVE.Vehicle.Vehicle - find_component_root(self, component)SUAVE.Vehicle.Vehicle - fuselages (defined in SUAVE.Vehicle.Vehicle)SUAVE.Vehicle.Vehicle - get_bases(self)SUAVE.Core.Data.Data - itervalues(self)SUAVE.Core.Data.Data + envelope (defined in SUAVE.Vehicle.Vehicle)SUAVE.Vehicle.Vehicle + find_component_root(self, component)SUAVE.Vehicle.Vehicle + fuselages (defined in SUAVE.Vehicle.Vehicle)SUAVE.Vehicle.Vehicle + get_bases(self)SUAVE.Core.Data.Data + itervalues(self)SUAVE.Core.Data.Data + landing_gear (defined in SUAVE.Vehicle.Vehicle)SUAVE.Vehicle.Vehicle mass_properties (defined in SUAVE.Vehicle.Vehicle)SUAVE.Vehicle.Vehicle - max_lift_coefficient_factor (defined in SUAVE.Vehicle.Vehicle)SUAVE.Vehicle.Vehicle - pack_array(self, output='vector')SUAVE.Core.Data.Data - passengers (defined in SUAVE.Vehicle.Vehicle)SUAVE.Vehicle.Vehicle - propulsors (defined in SUAVE.Vehicle.Vehicle)SUAVE.Vehicle.Vehicle + nacelles (defined in SUAVE.Vehicle.Vehicle)SUAVE.Vehicle.Vehicle + networks (defined in SUAVE.Vehicle.Vehicle)SUAVE.Vehicle.Vehicle + pack_array(self, output='vector')SUAVE.Core.Data.Data + passengers (defined in SUAVE.Vehicle.Vehicle)SUAVE.Vehicle.Vehicle + payload (defined in SUAVE.Vehicle.Vehicle)SUAVE.Vehicle.Vehicle + performance (defined in SUAVE.Vehicle.Vehicle)SUAVE.Vehicle.Vehicle reference_area (defined in SUAVE.Vehicle.Vehicle)SUAVE.Vehicle.Vehicle - systems (defined in SUAVE.Vehicle.Vehicle)SUAVE.Vehicle.Vehicle - tag (defined in SUAVE.Vehicle.Vehicle)SUAVE.Vehicle.Vehicle - typestring(self)SUAVE.Core.Data.Data - unpack_array(self, M)SUAVE.Core.Data.Data - update(self, other)SUAVE.Core.Data.Data - values(self)SUAVE.Core.Data.Data - wings (defined in SUAVE.Vehicle.Vehicle)SUAVE.Vehicle.Vehicle + sum_mass(self)SUAVE.Vehicle.Vehicle + systems (defined in SUAVE.Vehicle.Vehicle)SUAVE.Vehicle.Vehicle + tag (defined in SUAVE.Vehicle.Vehicle)SUAVE.Vehicle.Vehicle + typestring(self)SUAVE.Core.Data.Data + unpack_array(self, M)SUAVE.Core.Data.Data + update(self, other)SUAVE.Core.Data.Data + values(self)SUAVE.Core.Data.Data + wings (defined in SUAVE.Vehicle.Vehicle)SUAVE.Vehicle.Vehicle
@@ -139,7 +151,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Vehicle_1_1Vehicle.html b/doxygen/classSUAVE_1_1Vehicle_1_1Vehicle.html index a340acec..0751b5ee 100644 --- a/doxygen/classSUAVE_1_1Vehicle_1_1Vehicle.html +++ b/doxygen/classSUAVE_1_1Vehicle_1_1Vehicle.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Vehicle.Vehicle Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -105,20 +112,25 @@
-SUAVE.Core.Data.Data - -
+SUAVE.Core.Data.Data +SUAVE.Components.Configs.Config.Config + + - - + + + + + + @@ -126,18 +138,14 @@ - - - - + + - - @@ -146,6 +154,8 @@ + + @@ -172,33 +182,39 @@ - - - - + + + + + + + + - - + +

Public Member Functions

def __defaults__ (self)
 
def __init__ (self, args, kwarg)
 
def __init__ (self, *args, **kwarg)
 
def find_component_root (self, component)
 
def append_component (self, component)
 
def sum_mass (self)
 
def center_of_gravity (self)
 
- Public Member Functions inherited from SUAVE.Core.Data.Data
def __getattribute__ (self, k)
 
 
def __delattr__ (self, k)
 
def __defaults__ (self)
 
def __new__ (cls, args, kwarg)
 
def __new__ (cls, *args, **kwarg)
 
def typestring (self)
 
def dataname (self)
 
def __str__ (self, indent='')
 
def __init__ (self, args, kwarg)
 
def __iter__ (self)
 
def itervalues (self)
 
def update (self, other)
 
def append_or_update (self, other)
 
def get_bases (self)
 
def append (self, value, key=None)
 wings
 
propulsors
 
energy
 
networks
 
nacelles
 
 systems
 
 mass_properties
 
payload
 
 costs
 
 envelope
 
landing_gear
 
 reference_area
 
 passengers
 
max_lift_coefficient_factor
 
performance
 

Detailed Description

SUAVE Vehicle container class with database + input / output functionality
@@ -209,8 +225,8 @@
 Source:
 None
 

Constructor & Destructor Documentation

- -

◆ __init__()

+ +

◆ __init__()

Member Function Documentation

@@ -291,6 +309,10 @@

SUAVE.Core.Data.Data.

+ +

Reimplemented in SUAVE.Components.Configs.Config.Config.

+ @@ -337,6 +359,41 @@

+

◆ center_of_gravity()

+ +
+
+ + + + + + + + +
def SUAVE.Vehicle.Vehicle.center_of_gravity ( self)
+
+
will recursively search the data tree and sum
+    any Comp.Mass_Properties.mass, and return the total sum
+    
+    Assumptions:
+    None
+    
+    Source:
+    N/A
+    
+    Inputs:
+    None
+    
+    Outputs:
+    None
+    
+    Properties Used:
+    None
+
+
+

◆ find_component_root()

@@ -381,6 +438,40 @@

+

◆ sum_mass()

+ +
+
+ + + + + + + + +
def SUAVE.Vehicle.Vehicle.sum_mass ( self)
+
+
Regresses through the vehicle and sums the masses
+
+    Assumptions:
+    None
+    
+    Source:
+    N/A
+    
+    Inputs:
+    None
+    
+    Outputs:
+    None
+    
+    Properties Used:
+    None
+
+
+

The documentation for this class was generated from the following file:
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Vehicle.py
@@ -392,7 +483,7 @@

SUAVE + doxygen 1.8.15 diff --git a/doxygen/classSUAVE_1_1Vehicle_1_1Vehicle.js b/doxygen/classSUAVE_1_1Vehicle_1_1Vehicle.js index f7a3c59c..074b4fa8 100644 --- a/doxygen/classSUAVE_1_1Vehicle_1_1Vehicle.js +++ b/doxygen/classSUAVE_1_1Vehicle_1_1Vehicle.js @@ -1,17 +1,21 @@ var classSUAVE_1_1Vehicle_1_1Vehicle = [ - [ "__init__", "classSUAVE_1_1Vehicle_1_1Vehicle.html#ae6908bd99e7d8f4708f4fbcf64ec821d", null ], + [ "__init__", "classSUAVE_1_1Vehicle_1_1Vehicle.html#a25c012a6150c6702a2d850eed55b1964", null ], [ "__defaults__", "classSUAVE_1_1Vehicle_1_1Vehicle.html#ab279ed6a6b71a4a34fd5e07595b5d640", null ], [ "append_component", "classSUAVE_1_1Vehicle_1_1Vehicle.html#a33e2631545860ec0f2d89affae0569e7", null ], + [ "center_of_gravity", "classSUAVE_1_1Vehicle_1_1Vehicle.html#ad24633dacee7e977358e0cd7a76e6f89", null ], [ "find_component_root", "classSUAVE_1_1Vehicle_1_1Vehicle.html#aa5f8c6794e64be4f87f2fc5848d1c5bf", null ], + [ "sum_mass", "classSUAVE_1_1Vehicle_1_1Vehicle.html#ac95d257d25ef319a1812d1dfb8030ace", null ], [ "costs", "classSUAVE_1_1Vehicle_1_1Vehicle.html#a5a86ec750966687ee01ecd04f18f9b61", null ], - [ "energy", "classSUAVE_1_1Vehicle_1_1Vehicle.html#a8dd71874edebf03de72c240406ef6fed", null ], [ "envelope", "classSUAVE_1_1Vehicle_1_1Vehicle.html#af627044c07d1d292a963abafad9ad4f8", null ], [ "fuselages", "classSUAVE_1_1Vehicle_1_1Vehicle.html#aa5a1c52d2f0be67663a3a84b5f918182", null ], + [ "landing_gear", "classSUAVE_1_1Vehicle_1_1Vehicle.html#a0f7d7dd2ed5b6bf65ac9ec88c971d53f", null ], [ "mass_properties", "classSUAVE_1_1Vehicle_1_1Vehicle.html#aa8694bc77300ae2ff815e9d59f3775e3", null ], - [ "max_lift_coefficient_factor", "classSUAVE_1_1Vehicle_1_1Vehicle.html#a763d9473ea2c6f89f8da5f07a8521adc", null ], + [ "nacelles", "classSUAVE_1_1Vehicle_1_1Vehicle.html#ae4704f435e56947b2a7ce0eea7621023", null ], + [ "networks", "classSUAVE_1_1Vehicle_1_1Vehicle.html#aeae8e8827bbba3e52d519cbf140a3ebf", null ], [ "passengers", "classSUAVE_1_1Vehicle_1_1Vehicle.html#afc67cdf2695b8ecc92f5f067639c3ada", null ], - [ "propulsors", "classSUAVE_1_1Vehicle_1_1Vehicle.html#a50c78d84e282ec3b88d50d5596cdba2c", null ], + [ "payload", "classSUAVE_1_1Vehicle_1_1Vehicle.html#afebfa5278a827144682c786b58939be9", null ], + [ "performance", "classSUAVE_1_1Vehicle_1_1Vehicle.html#a2de4d7b944e7b6b9561afa7018e77e1e", null ], [ "reference_area", "classSUAVE_1_1Vehicle_1_1Vehicle.html#a60668c7b9710b4df0a667ec8e9c0d7dd", null ], [ "systems", "classSUAVE_1_1Vehicle_1_1Vehicle.html#ab8b0b39ab3b930928b161151cacfdc59", null ], [ "tag", "classSUAVE_1_1Vehicle_1_1Vehicle.html#a91d0af7fac13cf22c95a7d085ec96dbf", null ], diff --git a/doxygen/classSUAVE_1_1Vehicle_1_1Vehicle.png b/doxygen/classSUAVE_1_1Vehicle_1_1Vehicle.png index d50776ed..22b07da1 100644 Binary files a/doxygen/classSUAVE_1_1Vehicle_1_1Vehicle.png and b/doxygen/classSUAVE_1_1Vehicle_1_1Vehicle.png differ diff --git a/doxygen/classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Container-members.html b/doxygen/classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Container-members.html new file mode 100644 index 00000000..90a9f36e --- /dev/null +++ b/doxygen/classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Container-members.html @@ -0,0 +1,151 @@ + + + + + + + +SUAVE: Member List + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
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+
+ + + +
+
+ +
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+
+ +
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SUAVE.Vehicle.Vehicle_Mass_Container Member List
+
+
+ +

This is the complete list of members for SUAVE.Vehicle.Vehicle_Mass_Container, including all inherited members.

+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
__defaults__(self)SUAVE.Vehicle.Vehicle_Mass_Properties
append(self, value, key=None)SUAVE.Vehicle.Vehicle_Mass_Container
cargo (defined in SUAVE.Vehicle.Vehicle_Mass_Properties)SUAVE.Vehicle.Vehicle_Mass_Properties
center_of_gravity (defined in SUAVE.Vehicle.Vehicle_Mass_Properties)SUAVE.Vehicle.Vehicle_Mass_Properties
Container (defined in SUAVE.Components.Component.Container)SUAVE.Components.Component.Containerstatic
crew (defined in SUAVE.Vehicle.Vehicle_Mass_Properties)SUAVE.Vehicle.Vehicle_Mass_Properties
fuel (defined in SUAVE.Vehicle.Vehicle_Mass_Properties)SUAVE.Vehicle.Vehicle_Mass_Properties
generative_design_char_max_bounds (defined in SUAVE.Vehicle.Vehicle_Mass_Properties)SUAVE.Vehicle.Vehicle_Mass_Properties
generative_design_char_min_bounds (defined in SUAVE.Vehicle.Vehicle_Mass_Properties)SUAVE.Vehicle.Vehicle_Mass_Properties
generative_design_characteristics (defined in SUAVE.Vehicle.Vehicle_Mass_Properties)SUAVE.Vehicle.Vehicle_Mass_Properties
generative_design_max_per_vehicle (defined in SUAVE.Vehicle.Vehicle_Mass_Properties)SUAVE.Vehicle.Vehicle_Mass_Properties
generative_design_minimum (defined in SUAVE.Vehicle.Vehicle_Mass_Properties)SUAVE.Vehicle.Vehicle_Mass_Properties
generative_design_special_parent (defined in SUAVE.Vehicle.Vehicle_Mass_Properties)SUAVE.Vehicle.Vehicle_Mass_Properties
get_children(self)SUAVE.Vehicle.Vehicle_Mass_Container
landing (defined in SUAVE.Vehicle.Vehicle_Mass_Properties)SUAVE.Vehicle.Vehicle_Mass_Properties
mass (defined in SUAVE.Components.Mass_Properties.Mass_Properties)SUAVE.Components.Mass_Properties.Mass_Properties
max_cargo (defined in SUAVE.Vehicle.Vehicle_Mass_Properties)SUAVE.Vehicle.Vehicle_Mass_Properties
max_fuel (defined in SUAVE.Vehicle.Vehicle_Mass_Properties)SUAVE.Vehicle.Vehicle_Mass_Properties
max_landing (defined in SUAVE.Vehicle.Vehicle_Mass_Properties)SUAVE.Vehicle.Vehicle_Mass_Properties
max_payload (defined in SUAVE.Vehicle.Vehicle_Mass_Properties)SUAVE.Vehicle.Vehicle_Mass_Properties
max_takeoff (defined in SUAVE.Vehicle.Vehicle_Mass_Properties)SUAVE.Vehicle.Vehicle_Mass_Properties
max_zero_fuel (defined in SUAVE.Vehicle.Vehicle_Mass_Properties)SUAVE.Vehicle.Vehicle_Mass_Properties
moments_of_inertia (defined in SUAVE.Components.Mass_Properties.Mass_Properties)SUAVE.Components.Mass_Properties.Mass_Properties
operating_empty (defined in SUAVE.Vehicle.Vehicle_Mass_Properties)SUAVE.Vehicle.Vehicle_Mass_Properties
passenger (defined in SUAVE.Vehicle.Vehicle_Mass_Properties)SUAVE.Vehicle.Vehicle_Mass_Properties
payload (defined in SUAVE.Vehicle.Vehicle_Mass_Properties)SUAVE.Vehicle.Vehicle_Mass_Properties
sum_mass(self)SUAVE.Components.Physical_Component.Container
tag (defined in SUAVE.Vehicle.Vehicle_Mass_Properties)SUAVE.Vehicle.Vehicle_Mass_Properties
takeoff (defined in SUAVE.Vehicle.Vehicle_Mass_Properties)SUAVE.Vehicle.Vehicle_Mass_Properties
total_moment(self)SUAVE.Components.Physical_Component.Container
volume (defined in SUAVE.Components.Mass_Properties.Mass_Properties)SUAVE.Components.Mass_Properties.Mass_Properties
zero_fuel_center_of_gravity (defined in SUAVE.Vehicle.Vehicle_Mass_Properties)SUAVE.Vehicle.Vehicle_Mass_Properties
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Container.html b/doxygen/classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Container.html new file mode 100644 index 00000000..21004af8 --- /dev/null +++ b/doxygen/classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Container.html @@ -0,0 +1,326 @@ + + + + + + + +SUAVE: SUAVE.Vehicle.Vehicle_Mass_Container Class Reference + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
SUAVE.Vehicle.Vehicle_Mass_Container Class Reference
+
+
+
+Inheritance diagram for SUAVE.Vehicle.Vehicle_Mass_Container:
+
+
+ + +SUAVE.Components.Physical_Component.Container +SUAVE.Vehicle.Vehicle_Mass_Properties +SUAVE.Components.Component.Container +SUAVE.Components.Mass_Properties.Mass_Properties + +
+ + + + + + + + + + + + + + +

+Public Member Functions

def append (self, value, key=None)
 
def get_children (self)
 
- Public Member Functions inherited from SUAVE.Components.Physical_Component.Container
def sum_mass (self)
 
def total_moment (self)
 
- Public Member Functions inherited from SUAVE.Vehicle.Vehicle_Mass_Properties
def __defaults__ (self)
 
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Additional Inherited Members

- Public Attributes inherited from SUAVE.Vehicle.Vehicle_Mass_Properties
tag
 
operating_empty
 
max_takeoff
 
takeoff
 
max_landing
 
landing
 
max_cargo
 
cargo
 
max_payload
 
payload
 
passenger
 
crew
 
max_fuel
 
fuel
 
max_zero_fuel
 
center_of_gravity
 
zero_fuel_center_of_gravity
 
generative_design_max_per_vehicle
 
generative_design_special_parent
 
generative_design_characteristics
 
generative_design_minimum
 
generative_design_char_min_bounds
 
generative_design_char_max_bounds
 
- Public Attributes inherited from SUAVE.Components.Mass_Properties.Mass_Properties
mass
 
volume
 
center_of_gravity
 
moments_of_inertia
 
- Static Public Attributes inherited from SUAVE.Components.Component.Container
Container
 
+

Member Function Documentation

+ +

◆ append()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Vehicle.Vehicle_Mass_Container.append ( self,
 value,
 key = None 
)
+
+
Appends the vehicle mass, but only let's one ever exist. Keeps the newest one
+
+Assumptions:
+None
+    
+Source:
+N/A
+    
+Inputs:
+None
+    
+Outputs:
+None
+    
+Properties Used:
+N/A
+
+
+
+ +

◆ get_children()

+ +
+
+ + + + + + + + +
def SUAVE.Vehicle.Vehicle_Mass_Container.get_children ( self)
+
+
Returns the components that can go inside
+
+Assumptions:
+None
+    
+Source:
+N/A
+    
+Inputs:
+None
+    
+Outputs:
+None
+    
+Properties Used:
+N/A
+
+
+
+
The documentation for this class was generated from the following file:
    +
  • /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Vehicle.py
  • +
+
+
+ + + + diff --git a/doxygen/classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Container.js b/doxygen/classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Container.js new file mode 100644 index 00000000..6abf0761 --- /dev/null +++ b/doxygen/classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Container.js @@ -0,0 +1,5 @@ +var classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Container = +[ + [ "append", "classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Container.html#aa5a7f60f213f87c3945eb98ef1ba020a", null ], + [ "get_children", "classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Container.html#ab4c7fb4940867569fcb32b30c175f52e", null ] +]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Container.png b/doxygen/classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Container.png new file mode 100644 index 00000000..d4dd2d9f Binary files /dev/null and b/doxygen/classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Container.png differ diff --git a/doxygen/classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties-members.html b/doxygen/classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties-members.html index 14c01378..8bfdfeb0 100644 --- a/doxygen/classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties-members.html +++ b/doxygen/classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties-members.html @@ -1,9 +1,9 @@ - + - + SUAVE: Member List @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -103,6 +110,12 @@ center_of_gravity (defined in SUAVE.Vehicle.Vehicle_Mass_Properties)SUAVE.Vehicle.Vehicle_Mass_Properties crew (defined in SUAVE.Vehicle.Vehicle_Mass_Properties)SUAVE.Vehicle.Vehicle_Mass_Properties fuel (defined in SUAVE.Vehicle.Vehicle_Mass_Properties)SUAVE.Vehicle.Vehicle_Mass_Properties + generative_design_char_max_bounds (defined in SUAVE.Vehicle.Vehicle_Mass_Properties)SUAVE.Vehicle.Vehicle_Mass_Properties + generative_design_char_min_bounds (defined in SUAVE.Vehicle.Vehicle_Mass_Properties)SUAVE.Vehicle.Vehicle_Mass_Properties + generative_design_characteristics (defined in SUAVE.Vehicle.Vehicle_Mass_Properties)SUAVE.Vehicle.Vehicle_Mass_Properties + generative_design_max_per_vehicle (defined in SUAVE.Vehicle.Vehicle_Mass_Properties)SUAVE.Vehicle.Vehicle_Mass_Properties + generative_design_minimum (defined in SUAVE.Vehicle.Vehicle_Mass_Properties)SUAVE.Vehicle.Vehicle_Mass_Properties + generative_design_special_parent (defined in SUAVE.Vehicle.Vehicle_Mass_Properties)SUAVE.Vehicle.Vehicle_Mass_Properties landing (defined in SUAVE.Vehicle.Vehicle_Mass_Properties)SUAVE.Vehicle.Vehicle_Mass_Properties mass (defined in SUAVE.Components.Mass_Properties.Mass_Properties)SUAVE.Components.Mass_Properties.Mass_Properties max_cargo (defined in SUAVE.Vehicle.Vehicle_Mass_Properties)SUAVE.Vehicle.Vehicle_Mass_Properties @@ -115,9 +128,10 @@ operating_empty (defined in SUAVE.Vehicle.Vehicle_Mass_Properties)SUAVE.Vehicle.Vehicle_Mass_Properties passenger (defined in SUAVE.Vehicle.Vehicle_Mass_Properties)SUAVE.Vehicle.Vehicle_Mass_Properties payload (defined in SUAVE.Vehicle.Vehicle_Mass_Properties)SUAVE.Vehicle.Vehicle_Mass_Properties - takeoff (defined in SUAVE.Vehicle.Vehicle_Mass_Properties)SUAVE.Vehicle.Vehicle_Mass_Properties - volume (defined in SUAVE.Components.Mass_Properties.Mass_Properties)SUAVE.Components.Mass_Properties.Mass_Properties - zero_fuel_center_of_gravity (defined in SUAVE.Vehicle.Vehicle_Mass_Properties)SUAVE.Vehicle.Vehicle_Mass_Properties + tag (defined in SUAVE.Vehicle.Vehicle_Mass_Properties)SUAVE.Vehicle.Vehicle_Mass_Properties + takeoff (defined in SUAVE.Vehicle.Vehicle_Mass_Properties)SUAVE.Vehicle.Vehicle_Mass_Properties + volume (defined in SUAVE.Components.Mass_Properties.Mass_Properties)SUAVE.Components.Mass_Properties.Mass_Properties + zero_fuel_center_of_gravity (defined in SUAVE.Vehicle.Vehicle_Mass_Properties)SUAVE.Vehicle.Vehicle_Mass_Properties
@@ -125,7 +139,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties.html b/doxygen/classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties.html index bf21bdfa..a7a2617c 100644 --- a/doxygen/classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties.html +++ b/doxygen/classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE.Vehicle.Vehicle_Mass_Properties Class Reference @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -106,19 +113,20 @@ SUAVE.Components.Mass_Properties.Mass_Properties - -
+SUAVE.Vehicle.Vehicle_Mass_Container + + - - -

Public Member Functions

def __defaults__ (self)
 
- Public Member Functions inherited from SUAVE.Components.Mass_Properties.Mass_Properties
def __defaults__ (self)
 
+ + @@ -167,6 +175,24 @@ + + + + + + + + + + + + @@ -223,6 +249,8 @@

SUAVE.Components.Mass_Properties.Mass_Properties.

+
The documentation for this class was generated from the following file: diff --git a/doxygen/classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties.js b/doxygen/classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties.js index d14260e3..d20355f2 100644 --- a/doxygen/classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties.js +++ b/doxygen/classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties.js @@ -5,6 +5,12 @@ var classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties = [ "center_of_gravity", "classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties.html#ad36a0a734f8ae4b41f05e283661c586f", null ], [ "crew", "classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties.html#a39046a61d2b3ed8b384979511664d599", null ], [ "fuel", "classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties.html#affb84ea67f2a0b653e28e89508600ecb", null ], + [ "generative_design_char_max_bounds", "classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties.html#adc0bef021dc3d87224247bc59763d6e5", null ], + [ "generative_design_char_min_bounds", "classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties.html#a7b2f4e790b10f791ca74b82cf64f8f24", null ], + [ "generative_design_characteristics", "classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties.html#ad0344e991b9ede653865ac7b9ca9e356", null ], + [ "generative_design_max_per_vehicle", "classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties.html#aa3c8f7e9eb55d9d96916a7d8d166fd7c", null ], + [ "generative_design_minimum", "classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties.html#a191eaacd413eff5750357aa1b4f1e51c", null ], + [ "generative_design_special_parent", "classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties.html#aaa9c637e89cbe7a255894b91ce81d938", null ], [ "landing", "classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties.html#a07f79f8b79143a05e0b7ca66682064cf", null ], [ "max_cargo", "classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties.html#af57c262dd32191437d3ee529406e17e9", null ], [ "max_fuel", "classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties.html#ad32f98f3ed16911912400e1b7e24140e", null ], @@ -15,6 +21,7 @@ var classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties = [ "operating_empty", "classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties.html#ac40e731a21e2e1bb5184af4cdd318b94", null ], [ "passenger", "classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties.html#a68699c58cb0d984fd6d59abb422c659e", null ], [ "payload", "classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties.html#a7626274633166b37c23dd5236ec70925", null ], + [ "tag", "classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties.html#ac4d3be566140d1dceac66e0e54b2f6cd", null ], [ "takeoff", "classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties.html#a5c8f0a58b0892e19cae442c9630423d9", null ], [ "zero_fuel_center_of_gravity", "classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties.html#afb63d59caed1c5937f3596caa7feec43", null ] ]; \ No newline at end of file diff --git a/doxygen/classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties.png b/doxygen/classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties.png index 970f4e9e..fcd60767 100644 Binary files a/doxygen/classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties.png and b/doxygen/classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties.png differ diff --git a/doxygen/classes.html b/doxygen/classes.html index a47eeeff..39020165 100644 --- a/doxygen/classes.html +++ b/doxygen/classes.html @@ -1,9 +1,9 @@ - + - + SUAVE: Class Index @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@

Public Attributes

tag
 
 operating_empty
 
 zero_fuel_center_of_gravity
 
generative_design_max_per_vehicle
 
generative_design_special_parent
 
generative_design_characteristics
 
generative_design_minimum
 
generative_design_char_min_bounds
 
generative_design_char_max_bounds
 
- Public Attributes inherited from SUAVE.Components.Mass_Properties.Mass_Properties
 mass
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -98,92 +105,102 @@
_ | a | b | c | d | e | f | g | h | i | j | l | m | n | o | p | r | s | t | u | v | w
- - - + + + + - - - - - - - - - - - - - - - - - - - - - + + + + + + + + + + + + + + + + + + + + + + + + + + + - - - - - - + + + + + + + + + + - - - - - - - - - - - - + + + + + + + + + + + - - - - - - - + + + + + + + + - - - - - - - - - - - - + + + + + + + + + + + +
  _  
-
Constant_Speed_Constant_Angle (SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle)   Fuselage (SUAVE.Components.Fuselages.Fuselage)   Payload (SUAVE.Components.Energy.Peripherals.Payload)   
  t  
-
Constant_Speed_Constant_Angle (SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle)   
  g  
-
Payload (SUAVE.Components.Payloads.Payload)   
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_Quantity (SUAVE.Plugins.pint.quantity)   Constant_Speed_Constant_Angle_Noise (SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle_Noise)   Gas (SUAVE.Attributes.Gases.Gas)   Physical_Component (SUAVE.Components.Physical_Component)   TestBitTwiddlingUfuncs (SUAVE.Plugins.pint.testsuite.test_numpy)   
Constant_Speed_Constant_Altitude_Loiter (SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude_Loiter)   Fuel_Tank (SUAVE.Components.Energy.Storages.Fuel_Tanks.Fuel_Tank)   Operating_Costs (SUAVE.Components.Costs.Costs)   Supersonic_OpenVSP_Wave_Drag (SUAVE.Analyses.Aerodynamics.Supersonic_OpenVSP_Wave_Drag)   
Constant_Speed_Constant_Angle (SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle)   Fuselage (SUAVE.Components.Fuselages.Fuselage)   Optimized (SUAVE.Analyses.Mission.Segments.Climb.Optimized)   Supersonic_Zero (SUAVE.Analyses.Aerodynamics.Supersonic_Zero)   
_Exception (SUAVE.Plugins.pint.quantity)   Constant_Speed_Constant_Angle (SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle)   
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output (SUAVE.Core.redirect)   Surrogate_Optimization (SUAVE.Optimization.Surrogate_Optimization)   
_Quantity (SUAVE.Plugins.pint.quantity)   Constant_Speed_Constant_Angle_Noise (SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Angle_Noise)   
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Surrogate_Problem (SUAVE.Surrogate.Surrogate_Problem)   
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Constant_Speed_Constant_Rate (SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Rate)   Gaseous_H2 (SUAVE.Attributes.Propellants.Gaseous_H2)   Planet (SUAVE.Analyses.Planets.Planet)   TestCase (SUAVE.Plugins.pint.testsuite)   
Constant_Speed_Constant_Rate (SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Rate)   Gearbox (SUAVE.Components.Energy.Converters.Gearbox)   Planet (SUAVE.Attributes.Planets.Planet)   TestComparisonUfuncs (SUAVE.Plugins.pint.testsuite.test_umath)   
AERODAS (SUAVE.Analyses.Aerodynamics.AERODAS)   Constant_Speed_Linear_Altitude (SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Linear_Altitude)   Geometry (SUAVE.Analyses.Geometry.Geometry)   PrefixDefinition (SUAVE.Plugins.pint.unit)   TestContexts (SUAVE.Plugins.pint.testsuite.test_contexts)   
Aerodynamic (SUAVE.Analyses.Mission.Segments.Aerodynamic)   Constant_Temperature (SUAVE.Analyses.Atmospheric.Constant_Temperature)   Given_Weight (SUAVE.Analyses.Mission.Vary_Cruise.Given_Weight)   Process (SUAVE.Analyses.Process)   TestConverter (SUAVE.Plugins.pint.testsuite.test_unit)   
Aerodynamics (SUAVE.Analyses.Aerodynamics.Aerodynamics)   Constant_Temperature (SUAVE.Attributes.Atmospheres.Earth.Constant_Temperature)   Ground (SUAVE.Analyses.Mission.Segments.Ground.Ground)   Process_Geometry (SUAVE.Analyses.Aerodynamics.Process_Geometry)   TestDefinedContexts (SUAVE.Plugins.pint.testsuite.test_contexts)   
Aerodynamics (SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics)   Constant_Throttle_Constant_Altitude (SUAVE.Analyses.Mission.Segments.Cruise.Constant_Throttle_Constant_Altitude)   
  h  
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Propellant (SUAVE.Attributes.Propellants.Propellant)   TestDefinition (SUAVE.Plugins.pint.testsuite.test_unit)   
Air (SUAVE.Attributes.Gases.Air)   Constant_Throttle_Constant_Speed (SUAVE.Analyses.Mission.Segments.Climb.Constant_Throttle_Constant_Speed)   Propeller (SUAVE.Components.Energy.Converters.Propeller)   TestDimensions (SUAVE.Plugins.pint.testsuite.test_quantity)   
Aircraft (SUAVE.Methods.Aerodynamics.AVL.Data.Aircraft)   Container (SUAVE.Analyses.Mission.Segments.Segment)   Horizontal_Tail (SUAVE.Components.Wings.Horizontal_Tail)   Propeller_Lo_Fid (SUAVE.Components.Energy.Converters.Propeller_Lo_Fid)   TestFloatingUfuncs (SUAVE.Plugins.pint.testsuite.test_umath)   
Airfoil (SUAVE.Components.Wings.Airfoils.Airfoil)   Container (SUAVE.Analyses.Analysis)   Hover (SUAVE.Analyses.Mission.Segments.Hover.Hover)   Property (SUAVE.Core.DataOrdered)   TestHandler (SUAVE.Plugins.pint.testsuite.test_contexts)   
Airport (SUAVE.Attributes.Airports.Airport)   Container (SUAVE.Components.Fuselages.Fuselage)   
  i  
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Propulsor (SUAVE.Components.Propulsors.Propulsor)   TestIssues (SUAVE.Plugins.pint.testsuite.test_issues)   
All_At_Once (SUAVE.Analyses.Mission.All_At_Once)   Container (SUAVE.Components.Payloads.Payload)   Propulsor_Surrogate (SUAVE.Components.Energy.Networks.Propulsor_Surrogate)   TestIssuesNP (SUAVE.Plugins.pint.testsuite.test_issues)   
Aluminum_Air (SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Aluminum_Air)   Container (SUAVE.Components.Physical_Component)   Industrial_Costs (SUAVE.Components.Costs.Costs)   
  r  
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TestMathUfuncs (SUAVE.Plugins.pint.testsuite.test_umath)   
Analysis (SUAVE.Analyses.Analysis)   Container (SUAVE.Components.Propulsors.Propulsor)   Inputs (SUAVE.Methods.Aerodynamics.AVL.Data.Inputs)   TestMeasurement (SUAVE.Plugins.pint.testsuite.test_measurement)   
Atmosphere (SUAVE.Attributes.Atmospheres.Atmosphere)   Container (SUAVE.Analyses.Mission.Segments.Conditions.State)   
  j  
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Ram (SUAVE.Components.Energy.Converters.Ram)   TestNumpyMethods (SUAVE.Plugins.pint.testsuite.test_numpy)   
Atmospheric (SUAVE.Analyses.Atmospheric.Atmospheric)   Container (SUAVE.Core.Container)   Ramjet (SUAVE.Components.Energy.Networks.Ramjet)   TestNumpyNotSupported (SUAVE.Plugins.pint.testsuite.test_numpy)   
Attributes (SUAVE.Input_Output.XML.Data)   Container (SUAVE.Core.Diffed_Data)   Jet_A (SUAVE.Attributes.Propellants.Jet_A)   Residuals (SUAVE.Analyses.Mission.Segments.Conditions.Residuals)   TestPiTheorem (SUAVE.Plugins.pint.testsuite.test_pitheorem)   
Aviation_Gasoline (SUAVE.Attributes.Propellants.Aviation_Gasoline)   Container (SUAVE.Methods.Aerodynamics.AVL.Data.Cases)   Jet_A1 (SUAVE.Attributes.Propellants.Jet_A1)   Results (SUAVE.Analyses.Aerodynamics.Results)   TestQuantity (SUAVE.Plugins.pint.testsuite.test_quantity)   
Avionics (SUAVE.Components.Energy.Peripherals.Avionics)   Container (SUAVE.Analyses.Mission.Mission)   
  l  
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Run_Case (SUAVE.Methods.Aerodynamics.AVL.Data.Cases)   TestRegistry (SUAVE.Plugins.pint.testsuite.test_unit)   
AVL (SUAVE.Analyses.Stability.AVL)   Container (SUAVE.Components.Component)   Runway (SUAVE.Attributes.Airports.Runway)   TestStringProcessor (SUAVE.Plugins.pint.testsuite.test_util)   
AVL (SUAVE.Analyses.Aerodynamics.AVL)   ContainerOrdered (SUAVE.Core.ContainerOrdered)   Landing (SUAVE.Analyses.Mission.Segments.Ground.Landing)   
  s  
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TestTrigUfuncs (SUAVE.Plugins.pint.testsuite.test_umath)   
AVL_Discretization_Settings (SUAVE.Methods.Aerodynamics.AVL.Data.Settings)   Context (SUAVE.Plugins.pint.context)   Landing_Gear (SUAVE.Components.Landing_Gear.Landing_Gear)   TestUFuncs (SUAVE.Plugins.pint.testsuite.test_umath)   
AVL_Inviscid (SUAVE.Analyses.Aerodynamics.AVL_Inviscid)   ContextChain (SUAVE.Plugins.pint.context)   Lift_Forward_Propulsor (SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor)   Satellite (SUAVE.Components.Payloads.Satellite)   TestUnitsContainer (SUAVE.Plugins.pint.testsuite.test_unit)   
Constant_Speed_Constant_Angle_Noise (SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Angle_Noise)   Gas (SUAVE.Attributes.Gases.Gas)   System (SUAVE.Components.Systems.System)   
Constant_Speed_Constant_Rate (SUAVE.Analyses.Mission.Segments.Descent.Constant_Speed_Constant_Rate)   Gaseous_H2 (SUAVE.Attributes.Propellants.Gaseous_H2)   Paint (SUAVE.Attributes.Solids.Paint)   
  t  
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Acrylic (SUAVE.Attributes.Solids.Acrylic)   Constant_Speed_Constant_Rate (SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Constant_Rate)   Gearbox (SUAVE.Components.Energy.Converters.Gearbox)   ParserHelper (SUAVE.Plugins.pint.util)   
Additive_Solver (SUAVE.Optimization.Package_Setups.additive_setup)   Constant_Speed_Linear_Altitude (SUAVE.Analyses.Mission.Segments.Climb.Constant_Speed_Linear_Altitude)   Generator_Zero_Fid (SUAVE.Components.Energy.Converters.Generator_Zero_Fid)   Payload (SUAVE.Components.Energy.Peripherals.Payload)   Takeoff (SUAVE.Analyses.Mission.Segments.Ground.Takeoff)   
AERODAS (SUAVE.Analyses.Aerodynamics.AERODAS)   Constant_Temperature (SUAVE.Analyses.Atmospheric.Constant_Temperature)   Given_State_of_Charge (SUAVE.Analyses.Mission.Variable_Range_Cruise.Given_State_of_Charge)   Payload (SUAVE.Components.Payloads.Payload)   TestBitTwiddlingUfuncs (SUAVE.Plugins.pint.testsuite.test_numpy)   
Aerodynamic (SUAVE.Analyses.Mission.Segments.Aerodynamic)   Constant_Temperature (SUAVE.Attributes.Atmospheres.Earth.Constant_Temperature)   Given_Weight (SUAVE.Analyses.Mission.Variable_Range_Cruise.Given_Weight)   Physical_Component (SUAVE.Components.Physical_Component)   TestCase (SUAVE.Plugins.pint.testsuite)   
Aerodynamics (SUAVE.Analyses.Aerodynamics.Aerodynamics)   Constant_Throttle_Constant_Altitude (SUAVE.Analyses.Mission.Segments.Cruise.Constant_Throttle_Constant_Altitude)   Ground (SUAVE.Analyses.Mission.Segments.Ground.Ground)   Planet (SUAVE.Analyses.Planets.Planet)   TestComparisonUfuncs (SUAVE.Plugins.pint.testsuite.test_umath)   
Aerodynamics (SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics)   Constant_Throttle_Constant_Speed (SUAVE.Analyses.Mission.Segments.Climb.Constant_Throttle_Constant_Speed)   
  h  
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Planet (SUAVE.Attributes.Planets.Planet)   TestContexts (SUAVE.Plugins.pint.testsuite.test_contexts)   
Aileron (SUAVE.Components.Wings.Control_Surfaces.Aileron)   Container (SUAVE.Methods.Aerodynamics.AVL.Data.Cases)   PrefixDefinition (SUAVE.Plugins.pint.unit)   TestConverter (SUAVE.Plugins.pint.testsuite.test_unit)   
Air (SUAVE.Attributes.Gases.Air)   Container (SUAVE.Analyses.Analysis)   Horizontal_Tail (SUAVE.Components.Wings.Horizontal_Tail)   Process (SUAVE.Analyses.Process)   TestDefinedContexts (SUAVE.Plugins.pint.testsuite.test_contexts)   
Aircraft (SUAVE.Methods.Aerodynamics.AVL.Data.Aircraft)   Container (SUAVE.Components.Component)   Hover (SUAVE.Analyses.Mission.Segments.Hover.Hover)   Process_Geometry (SUAVE.Analyses.Aerodynamics.Process_Geometry)   TestDefinition (SUAVE.Plugins.pint.testsuite.test_unit)   
Airfoil (SUAVE.Components.Airfoils.Airfoil)   Container (SUAVE.Analyses.Mission.Segments.Segment)   HTS_DC_Supply (SUAVE.Components.Energy.Distributors.HTS_DC_Supply)   Propellant (SUAVE.Attributes.Propellants.Propellant)   TestDimensions (SUAVE.Plugins.pint.testsuite.test_quantity)   
Airport (SUAVE.Attributes.Airports.Airport)   Container (SUAVE.Components.Energy.Networks.Network)   
  i  
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Propeller (SUAVE.Components.Energy.Converters.Propeller)   TestFloatingUfuncs (SUAVE.Plugins.pint.testsuite.test_umath)   
All_At_Once (SUAVE.Analyses.Mission.All_At_Once)   Container (SUAVE.Analyses.Mission.Segments.Conditions.State)   Propeller_Lo_Fid (SUAVE.Components.Energy.Converters.Propeller_Lo_Fid)   TestHandler (SUAVE.Plugins.pint.testsuite.test_contexts)   
All_Moving_Surface (SUAVE.Components.Wings.All_Moving_Surface)   Container (SUAVE.Components.Fuselages.Fuselage)   Industrial_Costs (SUAVE.Components.Costs.Costs)   Property (SUAVE.Core.DataOrdered)   TestIssues (SUAVE.Plugins.pint.testsuite.test_issues)   
Aluminum (SUAVE.Attributes.Solids.Aluminum)   Container (SUAVE.Analyses.Mission.Mission)   Inputs (SUAVE.Methods.Aerodynamics.AVL.Data.Inputs)   Propulsor_Surrogate (SUAVE.Components.Energy.Networks.Propulsor_Surrogate)   TestIssuesNP (SUAVE.Plugins.pint.testsuite.test_issues)   
Aluminum_Air (SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Aluminum_Air)   Container (SUAVE.Components.Payloads.Payload)   Internal_Combustion_Engine (SUAVE.Components.Energy.Converters.Internal_Combustion_Engine)   PyCycle (SUAVE.Components.Energy.Networks.PyCycle)   TestMathUfuncs (SUAVE.Plugins.pint.testsuite.test_umath)   
Aluminum_Rib (SUAVE.Attributes.Solids.Aluminum_Rib)   Container (SUAVE.Components.Physical_Component)   Internal_Combustion_Propeller (SUAVE.Components.Energy.Networks.Internal_Combustion_Propeller)   
  r  
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TestMeasurement (SUAVE.Plugins.pint.testsuite.test_measurement)   
Analysis (SUAVE.Analyses.Analysis)   Container (SUAVE.Components.Wings.Wing)   Internal_Combustion_Propeller_Constant_Speed (SUAVE.Components.Energy.Networks.Internal_Combustion_Propeller_Constant_Speed)   TestNumpyMethods (SUAVE.Plugins.pint.testsuite.test_numpy)   
Atmosphere (SUAVE.Attributes.Atmospheres.Atmosphere)   Container (SUAVE.Core.Container)   
  j  
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Ram (SUAVE.Components.Energy.Converters.Ram)   TestNumpyNotSupported (SUAVE.Plugins.pint.testsuite.test_numpy)   
Atmospheric (SUAVE.Analyses.Atmospheric.Atmospheric)   Container (SUAVE.Core.Diffed_Data)   Ramjet (SUAVE.Components.Energy.Networks.Ramjet)   TestPiTheorem (SUAVE.Plugins.pint.testsuite.test_pitheorem)   
Attributes (SUAVE.Input_Output.XML.Data)   ContainerOrdered (SUAVE.Core.ContainerOrdered)   Jet_A (SUAVE.Attributes.Propellants.Jet_A)   Residuals (SUAVE.Analyses.Mission.Segments.Conditions.Residuals)   TestQuantity (SUAVE.Plugins.pint.testsuite.test_quantity)   
Aviation_Gasoline (SUAVE.Attributes.Propellants.Aviation_Gasoline)   Context (SUAVE.Plugins.pint.context)   Jet_A1 (SUAVE.Attributes.Propellants.Jet_A1)   Rocket_Combustor (SUAVE.Components.Energy.Converters.Rocket_Combustor)   TestRegistry (SUAVE.Plugins.pint.testsuite.test_unit)   
Avionics (SUAVE.Components.Energy.Peripherals.Avionics)   ContextChain (SUAVE.Plugins.pint.context)   JP7 (SUAVE.Attributes.Propellants.JP7)   Rocket_Thrust (SUAVE.Components.Energy.Processes.Rocket_Thrust)   TestStringProcessor (SUAVE.Plugins.pint.testsuite.test_util)   
AVL (SUAVE.Analyses.Stability.AVL)   Control_Surface (SUAVE.Methods.Aerodynamics.AVL.Data.Wing)   
  l  
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Rotor (SUAVE.Components.Energy.Converters.Rotor)   TestTrigUfuncs (SUAVE.Plugins.pint.testsuite.test_umath)   
AVL (SUAVE.Analyses.Aerodynamics.AVL)   Control_Surface (SUAVE.Components.Wings.Control_Surfaces.Control_Surface)   Rotor_Wake_Fidelity_One (SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_One)   TestUFuncs (SUAVE.Plugins.pint.testsuite.test_umath)   
AVL_Inviscid (SUAVE.Analyses.Aerodynamics.AVL_Inviscid)   Control_Surface_Data (SUAVE.Methods.Aerodynamics.AVL.Data.Wing)   Landing (SUAVE.Analyses.Mission.Segments.Ground.Landing)   Rotor_Wake_Fidelity_Two (SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_Two)   TestUnitsContainer (SUAVE.Plugins.pint.testsuite.test_unit)   
  b  
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Control_Surface (SUAVE.Components.Wings.Control_Surface)   Lifting_Line (SUAVE.Analyses.Aerodynamics.Lifting_Line)   ScaleConverter (SUAVE.Plugins.pint.unit)   Thrust (SUAVE.Components.Energy.Processes.Thrust)   
Control_Surface (SUAVE.Methods.Aerodynamics.AVL.Data.Wing)   Linear_Mach_Constant_Rate (SUAVE.Analyses.Mission.Segments.Descent.Linear_Mach_Constant_Rate)   Section (SUAVE.Components.Lofted_Body)   Tree_Element (SUAVE.Input_Output.D3JS.Tree_Element)   
Basic (SUAVE.Analyses.Mission.Segments.Conditions.Basic)   Control_Surface_Section (SUAVE.Components.Wings.Control_Surface)   Linear_Mach_Constant_Rate (SUAVE.Analyses.Mission.Segments.Climb.Linear_Mach_Constant_Rate)   Section (SUAVE.Methods.Aerodynamics.AVL.Data.Wing)   TreeBuilder (SUAVE.Input_Output.XML.load)   
Battery (SUAVE.Components.Energy.Storages.Batteries.Battery)   Converter (SUAVE.Plugins.pint.unit)   Linear_Speed_Constant_Rate (SUAVE.Analyses.Mission.Segments.Climb.Linear_Speed_Constant_Rate)   SectionContainer (SUAVE.Components.Lofted_Body)   Trust_Region (SUAVE.Optimization.Package_Setups.TRMM.Trust_Region)   
Battery_Ducted_Fan (SUAVE.Components.Energy.Networks.Battery_Ducted_Fan)   Costs (SUAVE.Vehicle)   Liquid (SUAVE.Attributes.Liquids.Liquid)   Segment (SUAVE.Analyses.Mission.Segments.Segment)   Trust_Region_Optimization (SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization)   
Battery_Propeller (SUAVE.Components.Energy.Networks.Battery_Propeller)   Costs (SUAVE.Analyses.Costs.Costs)   Liquid_Natural_Gas (SUAVE.Attributes.Propellants.Liquid_Natural_Gas)   Segment (SUAVE.Components.Wings.Segment)   Turbine (SUAVE.Components.Energy.Converters.Turbine)   
Body (SUAVE.Methods.Aerodynamics.AVL.Data.Body)   Curve (SUAVE.Components.Lofted_Body)   Lithium_Air (SUAVE.Components.Energy.Storages.Batteries.Variable_Mass.Lithium_Air)   Segment (SUAVE.Components.Lofted_Body)   Turbofan (SUAVE.Components.Energy.Networks.Turbofan)   
Control_Surface_Results (SUAVE.Methods.Aerodynamics.AVL.Data.Wing)   Landing_Gear (SUAVE.Components.Landing_Gear.Landing_Gear)   Rotor_Wake_Fidelity_Zero (SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_Zero)   Thrust (SUAVE.Components.Energy.Processes.Thrust)   
Converter (SUAVE.Plugins.pint.unit)   Lift_Cruise (SUAVE.Components.Energy.Networks.Lift_Cruise)   Rudder (SUAVE.Components.Wings.Control_Surfaces.Rudder)   Tree_Element (SUAVE.Input_Output.D3JS.Tree_Element)   
Basic (SUAVE.Analyses.Mission.Segments.Conditions.Basic)   Copper (SUAVE.Attributes.Solids.Copper)   Lift_Rotor (SUAVE.Components.Energy.Converters.Lift_Rotor)   Run_Case (SUAVE.Methods.Aerodynamics.AVL.Data.Cases)   TreeBuilder (SUAVE.Input_Output.XML.load)   
Battery (SUAVE.Components.Energy.Storages.Batteries.Battery)   Costs (SUAVE.Vehicle)   Lifting_Line (SUAVE.Analyses.Aerodynamics.Lifting_Line)   
  s  
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Trust_Region (SUAVE.Optimization.Package_Setups.TRMM.Trust_Region)   
Battery_Cell_Cycler (SUAVE.Components.Energy.Networks.Battery_Cell_Cycler)   Costs (SUAVE.Analyses.Costs.Costs)   Linear_Mach_Constant_Rate (SUAVE.Analyses.Mission.Segments.Descent.Linear_Mach_Constant_Rate)   Trust_Region_Optimization (SUAVE.Optimization.Package_Setups.TRMM.Trust_Region_Optimization)   
Battery_Charge_Discharge (SUAVE.Analyses.Mission.Segments.Ground.Battery_Charge_Discharge)   Cryocooler (SUAVE.Components.Energy.Cooling.Cryocooler)   Linear_Mach_Constant_Rate (SUAVE.Analyses.Mission.Segments.Climb.Linear_Mach_Constant_Rate)   ScaleConverter (SUAVE.Plugins.pint.unit)   Turbine (SUAVE.Components.Energy.Converters.Turbine)   
Battery_Ducted_Fan (SUAVE.Components.Energy.Networks.Battery_Ducted_Fan)   Cryogen (SUAVE.Attributes.Cryogens.Cryogen)   Linear_Speed_Constant_Rate (SUAVE.Analyses.Mission.Segments.Climb.Linear_Speed_Constant_Rate)   Scramjet (SUAVE.Components.Energy.Networks.Scramjet)   Turboelectric (SUAVE.Components.Energy.Converters.Turboelectric)   
Battery_Propeller (SUAVE.Components.Energy.Networks.Battery_Propeller)   Cryogenic_Heat_Exchanger (SUAVE.Components.Energy.Cooling.Cryogenic_Heat_Exchanger)   Liquid_H2 (SUAVE.Attributes.Cryogens.Liquid_H2)   Section (SUAVE.Methods.Aerodynamics.AVL.Data.Wing)   Turboelectric_HTS_Ducted_Fan (SUAVE.Components.Energy.Networks.Turboelectric_HTS_Ducted_Fan)   
Bidirectional_Carbon_Fiber (SUAVE.Attributes.Solids.Bidirectional_Carbon_Fiber)   Cryogenic_Lead (SUAVE.Components.Energy.Distributors.Cryogenic_Lead)   Liquid_H2 (SUAVE.Attributes.Propellants.Liquid_H2)   Section (SUAVE.Components.Lofted_Body)   Turbofan (SUAVE.Components.Energy.Networks.Turbofan)   
Body (SUAVE.Methods.Aerodynamics.AVL.Data.Body)   Cubic_Spline_Blender (SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.Cubic_Spline_Blender)   Liquid_Natural_Gas (SUAVE.Attributes.Propellants.Liquid_Natural_Gas)   Section_Container (SUAVE.Components.Lofted_Body)   Turbojet_Super (SUAVE.Components.Energy.Networks.Turbojet_Super)   
  c  
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CurveContainer (SUAVE.Components.Lofted_Body)   Lithium_Ion (SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion)   SegmentContainer (SUAVE.Components.Wings.Segment)   Turbojet_Super (SUAVE.Components.Energy.Networks.Turbojet_Super)   
  d  
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Lithium_Sulfur (SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Sulfur)   Sequential_Segments (SUAVE.Analyses.Mission.Sequential_Segments)   
  u  
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Cubic_Spline_Blender (SUAVE.Methods.Utilities.Cubic_Spline_Blender)   Liquid_Rocket (SUAVE.Components.Energy.Networks.Liquid_Rocket)   Segment (SUAVE.Analyses.Mission.Segments.Segment)   
  u  
Cargo (SUAVE.Components.Payloads.Cargo)   Loads (SUAVE.Analyses.Loads.Loads)   Set_Speed_Set_Altitude (SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude)   
ChainMap (SUAVE.Plugins.pint.compat)   Data (SUAVE.Core.Data)   Lofted_Body (SUAVE.Components.Lofted_Body)   Set_Speed_Set_Throttle (SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Throttle)   UndefinedUnitError (SUAVE.Plugins.pint.unit)   
Climb (SUAVE.Analyses.Mission.Segments.Hover.Climb)   Data (SUAVE.Input_Output.XML.Data)   
  m  
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Settings (SUAVE.Analyses.Settings)   UnitDefinition (SUAVE.Plugins.pint.unit)   
CO2 (SUAVE.Attributes.Gases.CO2)   DataOrdered (SUAVE.Core.DataOrdered)   Settings (SUAVE.Methods.Aerodynamics.AVL.Data.Settings)   UnitRegistry (SUAVE.Plugins.pint.unit)   
Combustor (SUAVE.Components.Energy.Converters.Combustor)   Definition (SUAVE.Plugins.pint.unit)   Main_Landing_Gear (SUAVE.Components.Landing_Gear.Main_Landing_Gear)   Shaft_Power_Off_Take (SUAVE.Components.Energy.Converters.Shaft_Power_Off_Take)   UnitsContainer (SUAVE.Plugins.pint.unit)   
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} -dl.bug -{ - margin-left:-7px; - padding-left: 3px; - border-left:4px solid; - border-color: #C08050; +dl.deprecated { + margin-left: -7px; + padding-left: 3px; + border-left: 4px solid; + border-color: #505050; +} + +dl.deprecated.DocNodeRTL { + margin-left: 0; + padding-left: 0; + border-left: 0; + margin-right: -7px; + padding-right: 3px; + border-right: 4px solid; + border-color: #505050; +} + +dl.todo { + margin-left: -7px; + padding-left: 3px; + border-left: 4px solid; + border-color: #00C0E0; +} + +dl.todo.DocNodeRTL { + margin-left: 0; + padding-left: 0; + border-left: 0; + margin-right: -7px; + padding-right: 3px; + border-right: 4px solid; + border-color: #00C0E0; +} + +dl.test { + margin-left: -7px; + padding-left: 3px; + border-left: 4px solid; + border-color: #3030E0; +} + +dl.test.DocNodeRTL { + margin-left: 0; + padding-left: 0; + border-left: 0; + margin-right: -7px; + padding-right: 3px; + border-right: 4px solid; + border-color: #3030E0; +} + +dl.bug { + margin-left: -7px; + padding-left: 3px; + border-left: 4px solid; + border-color: #C08050; +} + +dl.bug.DocNodeRTL { + margin-left: 0; + padding-left: 0; + border-left: 0; + margin-right: -7px; + padding-right: 3px; + border-right: 4px solid; + border-color: #C08050; } dl.section dd { @@ -1263,6 +1369,11 @@ div.toc { width: 200px; } +.PageDocRTL-title div.toc { + float: left !important; + text-align: right; +} + div.toc li { background: url("bdwn.png") no-repeat scroll 0 5px transparent; font: 10px/1.2 Verdana,DejaVu Sans,Geneva,sans-serif; @@ -1271,6 +1382,12 @@ div.toc li { padding-top: 2px; } +.PageDocRTL-title div.toc li { + background-position-x: right !important; + padding-left: 0 !important; + padding-right: 10px; +} + div.toc h3 { font: bold 12px/1.2 Arial,FreeSans,sans-serif; color: #181818; @@ -1300,6 +1417,26 @@ div.toc li.level4 { margin-left: 45px; } +.PageDocRTL-title div.toc li.level1 { + margin-left: 0 !important; + margin-right: 0; +} + +.PageDocRTL-title div.toc li.level2 { + margin-left: 0 !important; + margin-right: 15px; +} + +.PageDocRTL-title div.toc li.level3 { + margin-left: 0 !important; + margin-right: 30px; +} + +.PageDocRTL-title div.toc li.level4 { + margin-left: 0 !important; + margin-right: 45px; +} + .inherit_header { font-weight: bold; color: gray; @@ -1413,7 +1550,7 @@ tr.heading h2 { } #powerTip.n:after, #powerTip.ne:after, #powerTip.nw:after { - border-top-color: #ffffff; + border-top-color: #FFFFFF; border-width: 10px; margin: 0px -10px; } @@ -1441,7 +1578,7 @@ tr.heading h2 { } #powerTip.s:after, #powerTip.se:after, #powerTip.sw:after { - border-bottom-color: #ffffff; + border-bottom-color: #FFFFFF; border-width: 10px; margin: 0px -10px; } @@ -1468,7 +1605,7 @@ tr.heading h2 { left: 100%; } #powerTip.e:after { - border-left-color: #ffffff; + border-left-color: #FFFFFF; border-width: 10px; top: 50%; margin-top: -10px; @@ -1484,7 +1621,7 @@ tr.heading h2 { right: 100%; } #powerTip.w:after { - border-right-color: #ffffff; + border-right-color: #FFFFFF; border-width: 10px; top: 50%; margin-top: -10px; @@ -1573,7 +1710,7 @@ table.markdownTable tr { } th.markdownTableHeadLeft, th.markdownTableHeadRight, th.markdownTableHeadCenter, th.markdownTableHeadNone { - background-color: #374F7F; + background-color: #0B0B0B; color: #FFFFFF; font-size: 110%; padding-bottom: 4px; @@ -1592,5 +1729,36 @@ th.markdownTableHeadCenter, td.markdownTableBodyCenter { text-align: center } +.DocNodeRTL { + text-align: right; + direction: rtl; +} + +.DocNodeLTR { + text-align: left; + direction: ltr; +} + +table.DocNodeRTL { + width: auto; + margin-right: 0; + margin-left: auto; +} +table.DocNodeLTR { + width: auto; + margin-right: auto; + margin-left: 0; +} + +tt, code, kbd, samp +{ + display: inline-block; + direction:ltr; +} /* @end */ + +u { + text-decoration: underline; +} + diff --git a/doxygen/doxygen.svg b/doxygen/doxygen.svg new file mode 100644 index 00000000..4d4819f2 --- /dev/null +++ b/doxygen/doxygen.svg @@ -0,0 +1,26 @@ + + + + + + + + + + + + + + + + + + + + + + + + + + diff --git a/doxygen/dynsections.js b/doxygen/dynsections.js index 85e18369..ea0a7b39 100644 --- a/doxygen/dynsections.js +++ b/doxygen/dynsections.js @@ -1,3 +1,26 @@ +/* + @licstart The following is the entire license notice for the + JavaScript code in this file. + + Copyright (C) 1997-2017 by Dimitri van Heesch + + This program is free software; you can redistribute it and/or modify + it under the terms of the GNU General Public License as published by + the Free Software Foundation; either version 2 of the License, or + (at your option) any later version. + + This program is distributed in the hope that it will be useful, + but WITHOUT ANY WARRANTY; without even the implied warranty of + MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the + GNU General Public License for more details. + + You should have received a copy of the GNU General Public License along + with this program; if not, write to the Free Software Foundation, Inc., + 51 Franklin Street, Fifth Floor, Boston, MA 02110-1301 USA. + + @licend The above is the entire license notice + for the JavaScript code in this file + */ function toggleVisibility(linkObj) { var base = $(linkObj).attr('id'); @@ -15,7 +38,7 @@ function toggleVisibility(linkObj) summary.hide(); $(linkObj).removeClass('closed').addClass('opened'); $(trigger).attr('src',src.substring(0,src.length-10)+'open.png'); - } + } return false; } @@ -94,4 +117,4 @@ function toggleInherit(id) $(img).attr('src',src.substring(0,src.length-10)+'open.png'); } } - +/* @license-end */ diff --git a/doxygen/functions.html b/doxygen/functions.html index 2d5a80e5..e24d45de 100644 --- a/doxygen/functions.html +++ b/doxygen/functions.html @@ -1,9 +1,9 @@ - + - + SUAVE: Class Members @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -93,11 +100,12 @@
Here is a list of all documented class members with links to the class documentation for each member:
-

- _ -

diff --git a/doxygen/functions_a.html b/doxygen/functions_a.html index 21b6195f..ff80568a 100644 --- a/doxygen/functions_a.html +++ b/doxygen/functions_a.html @@ -1,9 +1,9 @@ - + - + SUAVE: Class Members @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@
- +
@@ -73,7 +78,9 @@
@@ -100,25 +107,58 @@

- a -

diff --git a/doxygen/functions_b.html b/doxygen/functions_b.html index 52de364c..24e1b1a8 100644 --- a/doxygen/functions_b.html +++ b/doxygen/functions_b.html @@ -1,9 +1,9 @@ - + - + SUAVE: Class Members @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
diff --git a/doxygen/functions_c.html b/doxygen/functions_c.html index f238b463..f1b9e43e 100644 --- a/doxygen/functions_c.html +++ b/doxygen/functions_c.html @@ -1,9 +1,9 @@ - + - + SUAVE: Class Members @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -100,6 +107,15 @@

- c -

@@ -199,7 +229,7 @@

- c -

class  SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude.Set_Speed_Set_Altitude   +class  SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Altitude_No_Propulsion.Set_Speed_Set_Altitude_No_Propulsion +  class  SUAVE.Analyses.Mission.Segments.Single_Point.Set_Speed_Set_Throttle.Set_Speed_Set_Throttle   @@ -118,7 +127,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/group__Analyses-Mission-Segments-Single__Point.js b/doxygen/group__Analyses-Mission-Segments-Single__Point.js index 6cb78042..9f31f94a 100644 --- a/doxygen/group__Analyses-Mission-Segments-Single__Point.js +++ b/doxygen/group__Analyses-Mission-Segments-Single__Point.js @@ -8,6 +8,13 @@ var group__Analyses_Mission_Segments_Single__Point = [ "x_accel", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Altitude_1_1Set__Speed__Set__Altitude.html#a56b1e1aff3d78e49f323c92bdc11b1d0", null ], [ "z_accel", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Altitude_1_1Set__Speed__Set__Altitude.html#a2739c0df766a5d1fbf576ab1484ca9e8", null ] ] ], + [ "Set_Speed_Set_Altitude_No_Propulsion", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Altitude__No_660be05666a18eb7201c7425b4456ff1.html", [ + [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Altitude__No_660be05666a18eb7201c7425b4456ff1.html#a1d0bccee24392981b447353a6a6e58bd", null ], + [ "air_speed", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Altitude__No_660be05666a18eb7201c7425b4456ff1.html#a77412ee8002a16d1cc1b07fe89909fae", null ], + [ "altitude", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Altitude__No_660be05666a18eb7201c7425b4456ff1.html#a8205a608d30e1d4e730618d89de852fc", null ], + [ "distance", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Altitude__No_660be05666a18eb7201c7425b4456ff1.html#adb78847a4e63ce7211c4b53bc425d8fd", null ], + [ "z_accel", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Altitude__No_660be05666a18eb7201c7425b4456ff1.html#a102fad69c2663702f98dd82dbff6dbfd", null ] + ] ], [ "Set_Speed_Set_Throttle", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Throttle_1_1Set__Speed__Set__Throttle.html", [ [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Throttle_1_1Set__Speed__Set__Throttle.html#a1d031a6b1908cc3dda51144295d6e419", null ], [ "air_speed", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Single__Point_1_1Set__Speed__Set__Throttle_1_1Set__Speed__Set__Throttle.html#abb7625cbc9cc662f2c76868f26cb0690", null ], diff --git a/doxygen/group__Analyses-Mission-Segments-Transition.html b/doxygen/group__Analyses-Mission-Segments-Transition.html new file mode 100644 index 00000000..35b9a886 --- /dev/null +++ b/doxygen/group__Analyses-Mission-Segments-Transition.html @@ -0,0 +1,129 @@ + + + + + + + +SUAVE: Transition + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
Transition
+
+
+ +

Segments for transition flight. +More...

+ + + + +

+Classes

class  SUAVE.Analyses.Mission.Segments.Transition.Constant_Acceleration_Constant_Angle_Linear_Climb.Constant_Acceleration_Constant_Angle_Linear_Climb
 
+

Detailed Description

+

Segments for transition flight.

+
+
+ + + + diff --git a/doxygen/group__Analyses-Mission-Segments-Transition.js b/doxygen/group__Analyses-Mission-Segments-Transition.js new file mode 100644 index 00000000..53d59d5a --- /dev/null +++ b/doxygen/group__Analyses-Mission-Segments-Transition.js @@ -0,0 +1,13 @@ +var group__Analyses_Mission_Segments_Transition = +[ + [ "Constant_Acceleration_Constant_Angle_Linear_Climb", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Transition_1_1Constant__Acceleration__Constant_2295952caac21c4a49a6ece0c9d2ce15.html", [ + [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Transition_1_1Constant__Acceleration__Constant_2295952caac21c4a49a6ece0c9d2ce15.html#a401f5d5529d22d5bb1030815a8e23535", null ], + [ "acceleration", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Transition_1_1Constant__Acceleration__Constant_2295952caac21c4a49a6ece0c9d2ce15.html#ace5a252f6ba01615cbe914e35e4f6e18", null ], + [ "altitude_end", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Transition_1_1Constant__Acceleration__Constant_2295952caac21c4a49a6ece0c9d2ce15.html#a30f50c155d138d070c7adb42369f767f", null ], + [ "altitude_start", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Transition_1_1Constant__Acceleration__Constant_2295952caac21c4a49a6ece0c9d2ce15.html#a793d6afc8124dc9108e5803c99d08810", null ], + [ "climb_angle", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Transition_1_1Constant__Acceleration__Constant_2295952caac21c4a49a6ece0c9d2ce15.html#ac3049b06489d272c11719565230ef478", null ], + [ "pitch_final", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Transition_1_1Constant__Acceleration__Constant_2295952caac21c4a49a6ece0c9d2ce15.html#a5159c089bfa470004259d49311abf2c4", null ], + [ "pitch_initial", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Transition_1_1Constant__Acceleration__Constant_2295952caac21c4a49a6ece0c9d2ce15.html#a466b4c626cb3ef2bbea23bbc6f6cb9a5", null ], + [ "true_course", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Transition_1_1Constant__Acceleration__Constant_2295952caac21c4a49a6ece0c9d2ce15.html#afcc7bb3471f3a6c045c178796f0bfd0a", null ] + ] ] +]; \ No newline at end of file diff --git a/doxygen/group__Analyses-Mission-Segments.html b/doxygen/group__Analyses-Mission-Segments.html index ca7b33d3..923a2b0f 100644 --- a/doxygen/group__Analyses-Mission-Segments.html +++ b/doxygen/group__Analyses-Mission-Segments.html @@ -1,9 +1,9 @@ - + - + SUAVE: Segment @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -125,6 +132,9 @@  Single_Point  Single point segments.
  + Transition + Segments for transition flight.
+  @@ -146,7 +156,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/group__Analyses-Mission-Segments.js b/doxygen/group__Analyses-Mission-Segments.js index d3f9741c..2d849f36 100644 --- a/doxygen/group__Analyses-Mission-Segments.js +++ b/doxygen/group__Analyses-Mission-Segments.js @@ -4,22 +4,24 @@ var group__Analyses_Mission_Segments = [ "Conditions", "group__Analyses-Mission-Segments-Conditions.html", "group__Analyses-Mission-Segments-Conditions" ], [ "Cruise", "group__Analyses-Mission-Segments-Cruise.html", "group__Analyses-Mission-Segments-Cruise" ], [ "Descent", "group__Analyses-Mission-Segments-Descent.html", "group__Analyses-Mission-Segments-Descent" ], - [ "Ground", "group__Analyses-Mission-Segments-Ground.html", null ], + [ "Ground", "group__Analyses-Mission-Segments-Ground.html", "group__Analyses-Mission-Segments-Ground" ], [ "Hover", "group__Analyses-Mission-Segments-Hover.html", "group__Analyses-Mission-Segments-Hover" ], [ "Single_Point", "group__Analyses-Mission-Segments-Single__Point.html", "group__Analyses-Mission-Segments-Single__Point" ], + [ "Transition", "group__Analyses-Mission-Segments-Transition.html", "group__Analyses-Mission-Segments-Transition" ], [ "Aerodynamic", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Aerodynamic_1_1Aerodynamic.html", [ [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Aerodynamic_1_1Aerodynamic.html#aed8adfea20e60c1456b6d163e6ad9279", null ], [ "temperature_deviation", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Aerodynamic_1_1Aerodynamic.html#ae878a8247dcffc628bdaccf944b08aaf", null ] ] ], [ "Segment", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Segment.html", [ [ "__defaults__", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Segment.html#aedc70c28743a1190d7b5b773d8b2b548", null ], - [ "compile", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Segment.html#aec843c0340b90e2c9b8f9cb94821b285", null ], [ "converge", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Segment.html#a4175e96a7e4e98d141c3cdb0500dfe88", null ], [ "evaluate", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Segment.html#a473372a75a561da7d96c9295b87db9a1", null ], - [ "finalize", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Segment.html#a0e2bf84e3c5b3e100b7386d1010755e5", null ], - [ "initialize", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Segment.html#acf1d0173938f3aa4ca3ad09c2422bee7", null ], - [ "iterate", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Segment.html#abe02a0e410fe1e801ba5695c617599d9", null ], + [ "finalize", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Segment.html#aff1929fe616e571238044187976708f8", null ], + [ "initialize", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Segment.html#ac1efae3755cf09bc4074de2b8f0d384d", null ], + [ "iterate", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Segment.html#a91e0c868326bac7136e8e53b123d12b3", null ], + [ "merged", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Segment.html#a1aa95e802ed5bd775fc4410cbe64dd23", null ], [ "analyses", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Segment.html#a48471a8adc5732e6a2132075d4e7e604", null ], + [ "conditions", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Segment.html#adf7fee48d4584636779c77dd886b8c19", null ], [ "process", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Segment.html#a6d5fcdf31038cb9d460812c9b5760bb5", null ], [ "settings", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Segment.html#a6633aaa7cae9aba9d6efdb0213869c2b", null ], [ "state", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Segment.html#a9e2d7e168109e4cd1f29669c0f906ccb", null ] diff --git a/doxygen/group__Analyses-Mission-Variable__Range__Cruise.html b/doxygen/group__Analyses-Mission-Variable__Range__Cruise.html new file mode 100644 index 00000000..77d271c9 --- /dev/null +++ b/doxygen/group__Analyses-Mission-Variable__Range__Cruise.html @@ -0,0 +1,120 @@ + + + + + + + +SUAVE: Vary_Range_Cruise + + + + + + + + + + + + + + + +
+
+

Classes

+ + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + + +
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
Vary_Range_Cruise
+
+
+ +

Variable cruise mission setups. +More...

+

Variable cruise mission setups.

+
+
+ + + + diff --git a/doxygen/group__Analyses-Mission-Vary__Cruise.html b/doxygen/group__Analyses-Mission-Vary__Cruise.html deleted file mode 100644 index 5b58af98..00000000 --- a/doxygen/group__Analyses-Mission-Vary__Cruise.html +++ /dev/null @@ -1,122 +0,0 @@ - - - - - - - -SUAVE: Vary_Cruise - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.1.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
-
- - - -
-
- -
-
-
- -
- -
-
- - -
- -
- -
- -
-
Vary_Cruise
-
-
- -

Variable cruise mission setups. -More...

- - - - -

-Classes

class  SUAVE.Analyses.Mission.Vary_Cruise.Given_Weight.Given_Weight
 
-

Detailed Description

-

Variable cruise mission setups.

-
-
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SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -107,8 +114,8 @@  Segment  Segment analyses to setup each part of a mission to fly.
  - Vary_Cruise - Variable cruise mission setups.
Vary_Range_Cruise + Variable cruise mission setups.
  @@ -57,9 +60,11 @@

@@ -131,7 +138,7 @@
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SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -105,6 +112,8 @@ Classes

class  SUAVE.Analyses.Noise.Fidelity_One.Fidelity_One   +class  SUAVE.Analyses.Noise.Fidelity_Zero.Fidelity_Zero +  class  SUAVE.Analyses.Noise.Noise.Noise   @@ -117,7 +126,7 @@
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+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
Propulsion
+
+
+ +

These are the analyses that control aerodynamic evaluations. +More...

+ + + + + + + + +

+Classes

class  SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_One.Rotor_Wake_Fidelity_One
 
class  SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_Two.Rotor_Wake_Fidelity_Two
 
class  SUAVE.Analyses.Propulsion.Rotor_Wake_Fidelity_Zero.Rotor_Wake_Fidelity_Zero
 
+

Detailed Description

+

These are the analyses that control aerodynamic evaluations.

+
+
+ + + + diff --git a/doxygen/group__Analyses-Propulsion.js b/doxygen/group__Analyses-Propulsion.js new file mode 100644 index 00000000..647a1624 --- /dev/null +++ b/doxygen/group__Analyses-Propulsion.js @@ -0,0 +1,39 @@ +var group__Analyses_Propulsion = +[ + [ "Rotor_Wake_Fidelity_One", "classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__One_1_1Rotor__Wake__Fidelity__One.html", [ + [ "__defaults__", "classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__One_1_1Rotor__Wake__Fidelity__One.html#a9f54fadb95e9f51087030b970b1124ec", null ], + [ "evaluate", "classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__One_1_1Rotor__Wake__Fidelity__One.html#aa4fdeeec634d4073e9c7058578f456dc", null ], + [ "evaluate_slipstream", "classSUAVE_1_1Analyses_1_1Propulsion_1_1Rotor__Wake__Fidelity__One_1_1Rotor__Wake__Fidelity__One.html#a2d342edbaeded9cd28f6f025fa699944", null ], + [ "evaluate_wake_velocities", 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SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -115,7 +122,7 @@
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SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -115,7 +122,7 @@
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SUAVE -  1.1.0 -
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An Aerospace Vehicle Environment for Designing Future Aircraft
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Structures
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This is the analysis that controls vehicle structure evaluations. -More...

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-Classes

class  SUAVE.Analyses.Structures.Structures.Structures
 
-

Detailed Description

-

This is the analysis that controls vehicle structure evaluations.

-
-
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SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
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SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -116,26 +123,20 @@  Energy  This is the analysis that controls energy network evaluations.
  - Geometry - This is the analysis that controls vehicle geometry evaluations.
-  - Loads - This is the analysis that controls vehicle load evaluations.
-   Mission  Mission Analyses to setup each part of a mission to fly.
   Noise  These are the analyses that control noise evaluations.
  + Propulsion + These are the analyses that control aerodynamic evaluations.
+   Sizing  This is the analysis that controls vehicle sizing evaluations.
   Stability   - Structures - This is the analysis that controls vehicle structure evaluations.
-   Weights  Classes that represent the types of aircraft configuration weight computations.
  @@ -150,8 +151,6 @@   class  SUAVE.Analyses.Settings.Settings   -class  SUAVE.Analyses.Surrogate.Surrogate -  class  SUAVE.Analyses.Vehicle.Vehicle   @@ -165,7 +164,7 @@
    + doxygen 1.8.15
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+ - + SUAVE: Airports @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -105,8 +112,6 @@ Classes

class  SUAVE.Attributes.Airports.Airport.Airport   -class  SUAVE.Attributes.Airports.Runway.Runway

Detailed Description

These are airport related classes.

@@ -117,7 +122,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/group__Attributes-Airports.js b/doxygen/group__Attributes-Airports.js index 083a090a..66359da8 100644 --- a/doxygen/group__Attributes-Airports.js +++ b/doxygen/group__Attributes-Airports.js @@ -6,9 +6,5 @@ var group__Attributes_Airports = [ "atmosphere", "classSUAVE_1_1Attributes_1_1Airports_1_1Airport_1_1Airport.html#a67a9bede56cdd73aa673e5a1b36f7790", null ], [ "delta_isa", "classSUAVE_1_1Attributes_1_1Airports_1_1Airport_1_1Airport.html#a62abe14755e7944ad08f587861c17452", null ], [ "tag", "classSUAVE_1_1Attributes_1_1Airports_1_1Airport_1_1Airport.html#a1cf3dc8bf593783283bf1a807385fb31", null ] - ] ], - [ "Runway", "classSUAVE_1_1Attributes_1_1Airports_1_1Runway_1_1Runway.html", [ - [ "__defaults__", "classSUAVE_1_1Attributes_1_1Airports_1_1Runway_1_1Runway.html#a952b090516a9563fc9f040c891493737", null ], - [ "tag", "classSUAVE_1_1Attributes_1_1Airports_1_1Runway_1_1Runway.html#a90f4ba576b4d5091fb0ce8caf86bf9e3", null ] ] ] ]; \ No newline at end of file diff --git a/doxygen/group__Attributes-Atmospheres-Earth.html b/doxygen/group__Attributes-Atmospheres-Earth.html index 74d1ef47..a2eff511 100644 --- a/doxygen/group__Attributes-Atmospheres-Earth.html +++ b/doxygen/group__Attributes-Atmospheres-Earth.html @@ -1,9 +1,9 @@ - + - + SUAVE: Earth @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -117,7 +124,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/group__Attributes-Atmospheres.html b/doxygen/group__Attributes-Atmospheres.html index 51957e24..80cb5196 100644 --- a/doxygen/group__Attributes-Atmospheres.html +++ b/doxygen/group__Attributes-Atmospheres.html @@ -1,9 +1,9 @@ - + - + SUAVE: Atmospheres @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -122,7 +129,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/group__Attributes-Constants.html b/doxygen/group__Attributes-Constants.html index ba4b9ef8..c08912e1 100644 --- a/doxygen/group__Attributes-Constants.html +++ b/doxygen/group__Attributes-Constants.html @@ -1,9 +1,9 @@ - + - + SUAVE: Constants @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -118,7 +125,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/group__Attributes-Cryogens.html b/doxygen/group__Attributes-Cryogens.html new file mode 100644 index 00000000..49954c3c --- /dev/null +++ b/doxygen/group__Attributes-Cryogens.html @@ -0,0 +1,132 @@ + + + + + + + +SUAVE: Cryogens + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
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+
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+
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Cryogens
+
+
+ +

Common Cryogensclasses. +More...

+ + + + + + +

+Classes

class  SUAVE.Attributes.Cryogens.Cryogen.Cryogen
 
class  SUAVE.Attributes.Cryogens.Liquid_H2.Liquid_H2
 
+

Detailed Description

+

Common Cryogens

+

classes.

+
+
+ + + + diff --git a/doxygen/group__Attributes-Cryogens.js b/doxygen/group__Attributes-Cryogens.js new file mode 100644 index 00000000..dd461529 --- /dev/null +++ b/doxygen/group__Attributes-Cryogens.js @@ -0,0 +1,43 @@ +var group__Attributes_Cryogens = +[ + [ "Cryogen", "classSUAVE_1_1Attributes_1_1Cryogens_1_1Cryogen_1_1Cryogen.html", [ + [ "__defaults__", "classSUAVE_1_1Attributes_1_1Cryogens_1_1Cryogen_1_1Cryogen.html#a6695bd894a18c4606c3152f1e02a7cb8", null ], + [ "density", "classSUAVE_1_1Attributes_1_1Cryogens_1_1Cryogen_1_1Cryogen.html#a1f2a64574576781c4ec69cb07dc4e970", null ], + [ "energy_density", "classSUAVE_1_1Attributes_1_1Cryogens_1_1Cryogen_1_1Cryogen.html#aff97f38e154ad4e4f73be178cfb03c30", null ], + [ "specific_energy", "classSUAVE_1_1Attributes_1_1Cryogens_1_1Cryogen_1_1Cryogen.html#a3409badeb47caa3af5a020a48962702e", null ], + [ "tag", "classSUAVE_1_1Attributes_1_1Cryogens_1_1Cryogen_1_1Cryogen.html#aadc789e0b77af5c884190512d386c15f", null ], + [ "temperatures", "classSUAVE_1_1Attributes_1_1Cryogens_1_1Cryogen_1_1Cryogen.html#a046182673df6f86f9037544fa16f1dda", null ] + ] ], + [ "Liquid_H2", "classSUAVE_1_1Attributes_1_1Cryogens_1_1Liquid__H2_1_1Liquid__H2.html", [ + [ "__defaults__", "classSUAVE_1_1Attributes_1_1Cryogens_1_1Liquid__H2_1_1Liquid__H2.html#ab1d4a2b48ff1fa6275b871336d791d53", null ], + [ "antoine_A", "classSUAVE_1_1Attributes_1_1Cryogens_1_1Liquid__H2_1_1Liquid__H2.html#a65b3956ff58f28ded611ade97c2bcdc0", null ], + [ "antoine_B", "classSUAVE_1_1Attributes_1_1Cryogens_1_1Liquid__H2_1_1Liquid__H2.html#a6d2a00fd87f97c1d82667a25f2434266", null ], + [ "antoine_C", "classSUAVE_1_1Attributes_1_1Cryogens_1_1Liquid__H2_1_1Liquid__H2.html#aee2776689a216088c6ec7a609c658e90", null ], + [ "antoine_maxT", "classSUAVE_1_1Attributes_1_1Cryogens_1_1Liquid__H2_1_1Liquid__H2.html#ac78d8d5401526a974f870d5593b2e464", null ], + [ "antoine_minT", "classSUAVE_1_1Attributes_1_1Cryogens_1_1Liquid__H2_1_1Liquid__H2.html#a0afd0a104f76188c69954e8541c2158d", null ], + [ "density", "classSUAVE_1_1Attributes_1_1Cryogens_1_1Liquid__H2_1_1Liquid__H2.html#a1840ac226c62bff1da96cda3068dd16d", null ], + [ "energy_density", "classSUAVE_1_1Attributes_1_1Cryogens_1_1Liquid__H2_1_1Liquid__H2.html#a6ce8d0eb930bc6d3161b81f234230bcc", null ], + [ "GCP_C0", "classSUAVE_1_1Attributes_1_1Cryogens_1_1Liquid__H2_1_1Liquid__H2.html#a02026ebdd1a21d2af167bb9eab53a4d3", null ], + [ "GCP_C1", "classSUAVE_1_1Attributes_1_1Cryogens_1_1Liquid__H2_1_1Liquid__H2.html#a8735df262a79967862d835148c201976", null ], + [ "GCP_C2", "classSUAVE_1_1Attributes_1_1Cryogens_1_1Liquid__H2_1_1Liquid__H2.html#a180387be40236024a484b8fd297ffd9e", null ], + [ "GCP_C3", "classSUAVE_1_1Attributes_1_1Cryogens_1_1Liquid__H2_1_1Liquid__H2.html#a8c5398141b8685bc6e071c8338c1709b", null ], + [ "GCP_maxT", "classSUAVE_1_1Attributes_1_1Cryogens_1_1Liquid__H2_1_1Liquid__H2.html#a74a4ba3a6770276763b339554d89e15f", null ], + [ "GCP_minT", "classSUAVE_1_1Attributes_1_1Cryogens_1_1Liquid__H2_1_1Liquid__H2.html#a2748b52d67de9b65f162572b39ce8bb8", null ], + [ "H_C0", "classSUAVE_1_1Attributes_1_1Cryogens_1_1Liquid__H2_1_1Liquid__H2.html#a66a857479fc3c81364e21d985da51918", null ], + [ "H_C1", "classSUAVE_1_1Attributes_1_1Cryogens_1_1Liquid__H2_1_1Liquid__H2.html#a290bcc13cccfeb1aea11c502d8bcb442", null ], + [ "H_C2", "classSUAVE_1_1Attributes_1_1Cryogens_1_1Liquid__H2_1_1Liquid__H2.html#aec0802d6a5c0807a1c381d47930338d1", null ], + [ "H_C3", "classSUAVE_1_1Attributes_1_1Cryogens_1_1Liquid__H2_1_1Liquid__H2.html#afbd5cc2821ae2f1c1a59af3b97daf87b", null ], + [ "H_maxP", "classSUAVE_1_1Attributes_1_1Cryogens_1_1Liquid__H2_1_1Liquid__H2.html#ab960db759a2a9298c65e1115e55b78d5", null ], + [ "H_minP", "classSUAVE_1_1Attributes_1_1Cryogens_1_1Liquid__H2_1_1Liquid__H2.html#ac5520f1dba0a0ea179e56fcf68aabe1e", null ], + [ "LCP_C0", "classSUAVE_1_1Attributes_1_1Cryogens_1_1Liquid__H2_1_1Liquid__H2.html#ad98e3cb4b4ee87871038091a1ee2c247", null ], + [ "LCP_C1", "classSUAVE_1_1Attributes_1_1Cryogens_1_1Liquid__H2_1_1Liquid__H2.html#a3191c371d4fb650c167ab9f0f2c7d17b", null ], + [ "LCP_C2", "classSUAVE_1_1Attributes_1_1Cryogens_1_1Liquid__H2_1_1Liquid__H2.html#a50199bbc7e990c7ab73bdaa885d5e62f", null ], + [ "LCP_C3", "classSUAVE_1_1Attributes_1_1Cryogens_1_1Liquid__H2_1_1Liquid__H2.html#a6f7f633625cc6fadbbc0403ca2a4b7ef", null ], + [ "LCP_maxT", "classSUAVE_1_1Attributes_1_1Cryogens_1_1Liquid__H2_1_1Liquid__H2.html#a42211cdf547377f1e7db67b92b444f3b", null ], + [ "LCP_minT", "classSUAVE_1_1Attributes_1_1Cryogens_1_1Liquid__H2_1_1Liquid__H2.html#a0c33a8c5ee69c862292b7f872909b7cc", null ], + [ "specific_energy", "classSUAVE_1_1Attributes_1_1Cryogens_1_1Liquid__H2_1_1Liquid__H2.html#a9cc5af91e5e2eee9835cf20453e97a48", null ], + [ "specific_heat", "classSUAVE_1_1Attributes_1_1Cryogens_1_1Liquid__H2_1_1Liquid__H2.html#ab0944652103384257c768e2256823aff", null ], + [ "tag", "classSUAVE_1_1Attributes_1_1Cryogens_1_1Liquid__H2_1_1Liquid__H2.html#acd4cff907907de9710c8d05304dae9d2", null ], + [ "vaporization_enthalpy", "classSUAVE_1_1Attributes_1_1Cryogens_1_1Liquid__H2_1_1Liquid__H2.html#a8cf0c17f0526d6ea72df96214604b10c", null ] + ] ] +]; \ No newline at end of file diff --git a/doxygen/group__Attributes-Gases.html b/doxygen/group__Attributes-Gases.html index abb2aa16..17c3ec3c 100644 --- a/doxygen/group__Attributes-Gases.html +++ b/doxygen/group__Attributes-Gases.html @@ -1,9 +1,9 @@ - + - + SUAVE: Gases @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -122,7 +129,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/group__Attributes-Gases.js b/doxygen/group__Attributes-Gases.js index 5bc04e08..bdac08c4 100644 --- a/doxygen/group__Attributes-Gases.js +++ b/doxygen/group__Attributes-Gases.js @@ -6,20 +6,26 @@ var group__Attributes_Gases = [ "compute_cp", "classSUAVE_1_1Attributes_1_1Gases_1_1Air_1_1Air.html#af2049f5193f71254180aa25263b253a9", null ], [ "compute_density", "classSUAVE_1_1Attributes_1_1Gases_1_1Air_1_1Air.html#a7e7724b5a0f3b55f1d22207de5eb95c3", null ], [ "compute_gamma", "classSUAVE_1_1Attributes_1_1Gases_1_1Air_1_1Air.html#a30b8f6bcf3ad36115e67d482ec406602", null ], + [ "compute_prandtl_number", "classSUAVE_1_1Attributes_1_1Gases_1_1Air_1_1Air.html#a8b971e95f9452e799a97df4562c0be3f", null ], [ "compute_speed_of_sound", "classSUAVE_1_1Attributes_1_1Gases_1_1Air_1_1Air.html#a86d93dc502a49cdf39a1d8f063021776", null ], + [ "compute_thermal_conductivity", "classSUAVE_1_1Attributes_1_1Gases_1_1Air_1_1Air.html#a60bddea705c18fc66874956b7b0693ee", null ], [ "gas_specific_constant", "classSUAVE_1_1Attributes_1_1Gases_1_1Air_1_1Air.html#a971ac13cf64d6a8c4e5e184e3cee8666", null ], - [ "molecular_mass", "classSUAVE_1_1Attributes_1_1Gases_1_1Air_1_1Air.html#afb2bd7b10f13b0aa8d9a1fd2b78d9309", null ] + [ "molecular_mass", "classSUAVE_1_1Attributes_1_1Gases_1_1Air_1_1Air.html#afb2bd7b10f13b0aa8d9a1fd2b78d9309", null ], + [ "specific_heat_capacity", "classSUAVE_1_1Attributes_1_1Gases_1_1Air_1_1Air.html#a598d6233a65ab1ef033edd7e85611c9b", null ], + [ "tag", "classSUAVE_1_1Attributes_1_1Gases_1_1Air_1_1Air.html#a849d84b197c029d5c4d17df55af0dec9", null ] ] ], [ "CO2", "classSUAVE_1_1Attributes_1_1Gases_1_1CO2_1_1CO2.html", [ [ "__defaults__", "classSUAVE_1_1Attributes_1_1Gases_1_1CO2_1_1CO2.html#af5f8d34d26d75384069a564e850c26cf", null ], [ "gas_specific_constant", "classSUAVE_1_1Attributes_1_1Gases_1_1CO2_1_1CO2.html#a2f45f35a4c6870cef5748765f10b6a95", null ], - [ "molecular_mass", "classSUAVE_1_1Attributes_1_1Gases_1_1CO2_1_1CO2.html#ac6f75e5944b60254978d9815a738d333", null ] + [ "molecular_mass", "classSUAVE_1_1Attributes_1_1Gases_1_1CO2_1_1CO2.html#ac6f75e5944b60254978d9815a738d333", null ], + [ "tag", "classSUAVE_1_1Attributes_1_1Gases_1_1CO2_1_1CO2.html#a46659782a6d23b2db21a550817f55c76", null ] ] ], [ "Gas", "classSUAVE_1_1Attributes_1_1Gases_1_1Gas_1_1Gas.html", [ [ "__defaults__", "classSUAVE_1_1Attributes_1_1Gases_1_1Gas_1_1Gas.html#a57159410d8c1a8e43da05f8faa255288", null ], [ "composition", "classSUAVE_1_1Attributes_1_1Gases_1_1Gas_1_1Gas.html#a890da3c2d8264228bcb0ac9936d16e35", null ], [ "gas_specific_constant", "classSUAVE_1_1Attributes_1_1Gases_1_1Gas_1_1Gas.html#a9472faacd37b54512bd462b4ec467f70", null ], - [ "molecular_mass", "classSUAVE_1_1Attributes_1_1Gases_1_1Gas_1_1Gas.html#af1a58498a684124a1bddd171eed7a8af", null ] + [ "molecular_mass", "classSUAVE_1_1Attributes_1_1Gases_1_1Gas_1_1Gas.html#af1a58498a684124a1bddd171eed7a8af", null ], + [ "tag", "classSUAVE_1_1Attributes_1_1Gases_1_1Gas_1_1Gas.html#a4115a2705cde25362b9746f2b6931a58", null ] ] ], [ "Steam", "classSUAVE_1_1Attributes_1_1Gases_1_1Steam_1_1Steam.html", [ [ "__defaults__", "classSUAVE_1_1Attributes_1_1Gases_1_1Steam_1_1Steam.html#a7175c34a32620fd4799bee6c0a318c64", null ], @@ -30,6 +36,7 @@ var group__Attributes_Gases = [ "compute_gamma", "classSUAVE_1_1Attributes_1_1Gases_1_1Steam_1_1Steam.html#a66d54aac1e188e801ca276ca2d48fdd8", null ], [ "compute_speed_of_sound", "classSUAVE_1_1Attributes_1_1Gases_1_1Steam_1_1Steam.html#a86ba9c1313cae71b544a4be1edf05bad", null ], [ "gas_specific_constant", "classSUAVE_1_1Attributes_1_1Gases_1_1Steam_1_1Steam.html#ab45dc8c7c1186e41c21deb0a2ff1d82e", null ], - [ "molecular_mass", "classSUAVE_1_1Attributes_1_1Gases_1_1Steam_1_1Steam.html#a54398bd1c5ff2db7e010ce52851621b0", null ] + [ "molecular_mass", "classSUAVE_1_1Attributes_1_1Gases_1_1Steam_1_1Steam.html#a54398bd1c5ff2db7e010ce52851621b0", null ], + [ "tag", "classSUAVE_1_1Attributes_1_1Gases_1_1Steam_1_1Steam.html#a0bb346fc022f10b6a2575b9472678e41", null ] ] ] ]; \ No newline at end of file diff --git a/doxygen/group__Attributes-Liquids.html b/doxygen/group__Attributes-Liquids.html deleted file mode 100644 index 93687733..00000000 --- a/doxygen/group__Attributes-Liquids.html +++ /dev/null @@ -1,125 +0,0 @@ - - - - - - - -SUAVE: Liquids - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.1.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
-
- - - -
-
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Liquids
-
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Common liquidsclasses. -More...

- - - - - - -

-Classes

class  SUAVE.Attributes.Liquids.Liquid.Liquid
 
class  SUAVE.Attributes.Liquids.Water.Water
 
-

Detailed Description

-

Common liquids

-

classes.

-
-
- - - - diff --git a/doxygen/group__Attributes-Liquids.js b/doxygen/group__Attributes-Liquids.js deleted file mode 100644 index 644f376c..00000000 --- a/doxygen/group__Attributes-Liquids.js +++ /dev/null @@ -1,20 +0,0 @@ -var group__Attributes_Liquids = -[ - [ "Liquid", "classSUAVE_1_1Attributes_1_1Liquids_1_1Liquid_1_1Liquid.html", [ - [ "__defaults__", "classSUAVE_1_1Attributes_1_1Liquids_1_1Liquid_1_1Liquid.html#a7a914b29e3f95b7e3077924fdab26b75", null ], - [ "boiling_point", "classSUAVE_1_1Attributes_1_1Liquids_1_1Liquid_1_1Liquid.html#a12a13ffeb5bb6578b37361055d5338c2", null ], - [ "composition", "classSUAVE_1_1Attributes_1_1Liquids_1_1Liquid_1_1Liquid.html#a31ff0cf7acd5fda18cb2b60d83af9621", null ], - [ "density", "classSUAVE_1_1Attributes_1_1Liquids_1_1Liquid_1_1Liquid.html#a2d467e83e2ffebbb799f88c27acf279e", null ], - [ "heat_of_vaporization", "classSUAVE_1_1Attributes_1_1Liquids_1_1Liquid_1_1Liquid.html#a85f870a09a056ef2b1eedd43899c9a2c", null ], - [ "molecular_mass", "classSUAVE_1_1Attributes_1_1Liquids_1_1Liquid_1_1Liquid.html#a08a7c2c7a09bfda8f90e5e5a7185df2f", null ] - ] ], - [ "Water", "classSUAVE_1_1Attributes_1_1Liquids_1_1Water_1_1Water.html", [ - [ "__defaults__", "classSUAVE_1_1Attributes_1_1Liquids_1_1Water_1_1Water.html#a26e34166234e5e4e859b1518457236f6", null ], - [ "compute_absolute_viscosity", "classSUAVE_1_1Attributes_1_1Liquids_1_1Water_1_1Water.html#afed25d8331b81ad9da36630f1c9ce0d8", null ], - [ "compute_cp", "classSUAVE_1_1Attributes_1_1Liquids_1_1Water_1_1Water.html#a2f39eb3e6e84ed4134aa572bccb21261", null ], - [ "boiling_point", "classSUAVE_1_1Attributes_1_1Liquids_1_1Water_1_1Water.html#a448bd07a86d29731585666cc182ec2eb", null ], - [ "density", "classSUAVE_1_1Attributes_1_1Liquids_1_1Water_1_1Water.html#ac5f6687060722912a9faa90a640913eb", null ], - [ "heat_of_vaporization", "classSUAVE_1_1Attributes_1_1Liquids_1_1Water_1_1Water.html#ae5986eb8fb5b5bef379c1ae53ac9c65b", null ], - [ "molecular_mass", "classSUAVE_1_1Attributes_1_1Liquids_1_1Water_1_1Water.html#a4121d521d9f3a398495d406c42c67348", null ] - ] ] -]; \ No newline at end of file diff --git a/doxygen/group__Attributes-Planets.html b/doxygen/group__Attributes-Planets.html index 3ca4f19c..3674800c 100644 --- a/doxygen/group__Attributes-Planets.html +++ b/doxygen/group__Attributes-Planets.html @@ -1,9 +1,9 @@ - + - + SUAVE: Planets @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -105,8 +112,6 @@ Classes

class  SUAVE.Attributes.Planets.Earth.Earth   -class  SUAVE.Attributes.Planets.Mars.Mars -  class  SUAVE.Attributes.Planets.Planet.Planet   @@ -120,7 +125,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/group__Attributes-Planets.js b/doxygen/group__Attributes-Planets.js index 977550d9..d0a96305 100644 --- a/doxygen/group__Attributes-Planets.js +++ b/doxygen/group__Attributes-Planets.js @@ -2,18 +2,13 @@ var group__Attributes_Planets = [ [ "Earth", "classSUAVE_1_1Attributes_1_1Planets_1_1Earth_1_1Earth.html", [ [ "__defaults__", "classSUAVE_1_1Attributes_1_1Planets_1_1Earth_1_1Earth.html#af9d701e61dcaa8db64215d233dbab41e", null ], + [ "compute_gravity", "classSUAVE_1_1Attributes_1_1Planets_1_1Earth_1_1Earth.html#a5b855aafeb2f8305e1c40dba7347a529", null ], [ "HitchHikersGuide", "classSUAVE_1_1Attributes_1_1Planets_1_1Earth_1_1Earth.html#ab7c1fd327fdcc282f3c074679ac7b4f5", null ], [ "mass", "classSUAVE_1_1Attributes_1_1Planets_1_1Earth_1_1Earth.html#ab153ac9436b492099517ed685efcddbf", null ], [ "mean_radius", "classSUAVE_1_1Attributes_1_1Planets_1_1Earth_1_1Earth.html#a6f45b05a9497a24d54cf3f11c1d0aeba", null ], [ "sea_level_gravity", "classSUAVE_1_1Attributes_1_1Planets_1_1Earth_1_1Earth.html#a7d7d8928e3a052946e0c48bb90ca8e4d", null ], [ "tag", "classSUAVE_1_1Attributes_1_1Planets_1_1Earth_1_1Earth.html#a421ca1bfa3d0594813b3160438caac98", null ] ] ], - [ "Mars", "classSUAVE_1_1Attributes_1_1Planets_1_1Mars_1_1Mars.html", [ - [ "__defaults__", "classSUAVE_1_1Attributes_1_1Planets_1_1Mars_1_1Mars.html#a6a69df61b3f4613a5bb317eafe141525", null ], - [ "mass", "classSUAVE_1_1Attributes_1_1Planets_1_1Mars_1_1Mars.html#a86e73c31eea6ce54a0ac517234181eff", null ], - [ "mean_radius", "classSUAVE_1_1Attributes_1_1Planets_1_1Mars_1_1Mars.html#a843cbafebe8b18e69b4cc8d8590bd69b", null ], - [ "sea_level_gravity", "classSUAVE_1_1Attributes_1_1Planets_1_1Mars_1_1Mars.html#aa4c5f4ccd0aa0f3e036b016dcb48917a", null ] - ] ], [ "Planet", "classSUAVE_1_1Attributes_1_1Planets_1_1Planet_1_1Planet.html", [ [ "__defaults__", "classSUAVE_1_1Attributes_1_1Planets_1_1Planet_1_1Planet.html#ad2e5a754d11025380430fc1077b33fbf", null ], [ "mass", "classSUAVE_1_1Attributes_1_1Planets_1_1Planet_1_1Planet.html#ac5c620d87e383037b8d2573eeb9516b4", null ], diff --git a/doxygen/group__Attributes-Propellants.html b/doxygen/group__Attributes-Propellants.html index 1f2c6ee5..a91f5bad 100644 --- a/doxygen/group__Attributes-Propellants.html +++ b/doxygen/group__Attributes-Propellants.html @@ -1,9 +1,9 @@ - + - + SUAVE: Propellants @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
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+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
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+ + + + + + +
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+
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+ +
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SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -112,12 +119,12 @@  Constants  Contains basic data for atmospheres.
  + Cryogens + Common Cryogensclasses.
+   Gases  Common gasesclasses.
  - Liquids - Common liquidsclasses.
-   Planets  Available planetsclasses.
  @@ -134,7 +141,7 @@
    + doxygen 1.8.15
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+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
Airfoils
+
+
+ + + + +

+Classes

class  SUAVE.Components.Airfoils.Airfoil.Airfoil
 
+

Detailed Description

+
+
+ + + + diff --git a/doxygen/group__Components-Airfoils.js b/doxygen/group__Components-Airfoils.js new file mode 100644 index 00000000..46819675 --- /dev/null +++ b/doxygen/group__Components-Airfoils.js @@ -0,0 +1,11 @@ +var group__Components_Airfoils = +[ + [ "Airfoil", "classSUAVE_1_1Components_1_1Airfoils_1_1Airfoil_1_1Airfoil.html", [ + [ "__defaults__", "classSUAVE_1_1Components_1_1Airfoils_1_1Airfoil_1_1Airfoil.html#a99c8fb72187cf75c949120c0bda56da7", null ], + [ "coordinate_file", "classSUAVE_1_1Components_1_1Airfoils_1_1Airfoil_1_1Airfoil.html#a8f361107e12e0d17b945176c76d0a291", null ], + [ "naca_4_series_airfoil", "classSUAVE_1_1Components_1_1Airfoils_1_1Airfoil_1_1Airfoil.html#a093a730dc8d697bd410f3872f122ca27", null ], + [ "points", "classSUAVE_1_1Components_1_1Airfoils_1_1Airfoil_1_1Airfoil.html#adb24bbb3f131149cfcf7af8a7345c8c2", null ], + [ "tag", "classSUAVE_1_1Components_1_1Airfoils_1_1Airfoil_1_1Airfoil.html#a1d5e04a8bd3064f0631d5ada5e483f39", null ], + [ "thickness_to_chord", "classSUAVE_1_1Components_1_1Airfoils_1_1Airfoil_1_1Airfoil.html#a5d2963e60ebb338047c0bca2242eea1a", null ] + ] ] +]; \ No newline at end of file diff --git a/doxygen/group__Components-Configs.html b/doxygen/group__Components-Configs.html index 85f8dca7..da0ac3d2 100644 --- a/doxygen/group__Components-Configs.html +++ b/doxygen/group__Components-Configs.html @@ -1,9 +1,9 @@ - + - + SUAVE: Configs @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -115,7 +122,7 @@
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SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -117,7 +124,7 @@
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+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
Charging
+
+
+ + + + +

+Classes

class  SUAVE.Components.Energy.Charging.Charging.Charging
 
+

Detailed Description

+
+
+ + + + diff --git a/doxygen/group__Components-Energy-Charging.js b/doxygen/group__Components-Energy-Charging.js new file mode 100644 index 00000000..6ca251b1 --- /dev/null +++ b/doxygen/group__Components-Energy-Charging.js @@ -0,0 +1,8 @@ +var group__Components_Energy_Charging = +[ + [ "Charging", "classSUAVE_1_1Components_1_1Energy_1_1Charging_1_1Charging_1_1Charging.html", [ + [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Charging_1_1Charging_1_1Charging.html#a0b21dc5aa5f4c1618dff7a2269d9256f", null ], + [ "C_rate", "classSUAVE_1_1Components_1_1Energy_1_1Charging_1_1Charging_1_1Charging.html#aab57eaee1dd67d50d4f84e0146836104", null ], + [ "SOC_cutoff", "classSUAVE_1_1Components_1_1Energy_1_1Charging_1_1Charging_1_1Charging.html#a808e76e8a2e6de2a1329d3423bb2c291", null ] + ] ] +]; \ No newline at end of file diff --git a/doxygen/group__Components-Energy-Converters.html b/doxygen/group__Components-Energy-Converters.html index 7fdbddd3..da9ed4e9 100644 --- a/doxygen/group__Components-Energy-Converters.html +++ b/doxygen/group__Components-Energy-Converters.html @@ -1,9 +1,9 @@ - + - + SUAVE: Converters @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -109,6 +116,8 @@   class  SUAVE.Components.Energy.Converters.Compressor.Compressor   +class  SUAVE.Components.Energy.Converters.de_Laval_Nozzle.de_Laval_Nozzle +  class  SUAVE.Components.Energy.Converters.Expansion_Nozzle.Expansion_Nozzle   class  SUAVE.Components.Energy.Converters.Fan.Fan @@ -117,8 +126,16 @@   class  SUAVE.Components.Energy.Converters.Gearbox.Gearbox   +class  SUAVE.Components.Energy.Converters.Generator_Zero_Fid.Generator_Zero_Fid +  +class  SUAVE.Components.Energy.Converters.Internal_Combustion_Engine.Internal_Combustion_Engine +  +class  SUAVE.Components.Energy.Converters.Lift_Rotor.Lift_Rotor +  class  SUAVE.Components.Energy.Converters.Motor.Motor   +class  SUAVE.Components.Energy.Converters.Motor_HTS_Rotor.Motor_HTS_Rotor +  class  SUAVE.Components.Energy.Converters.Motor_Lo_Fid.Motor_Lo_Fid   class  SUAVE.Components.Energy.Converters.Propeller.Propeller @@ -127,17 +144,22 @@   class  SUAVE.Components.Energy.Converters.Ram.Ram   +class  SUAVE.Components.Energy.Converters.Rocket_Combustor.Rocket_Combustor +  +class  SUAVE.Components.Energy.Converters.Rotor.Rotor +  class  SUAVE.Components.Energy.Converters.Shaft_Power_Off_Take.Shaft_Power_Off_Take   class  SUAVE.Components.Energy.Converters.Solar_Panel.Solar_Panel
-

Solar_Panel Class

- More...
  class  SUAVE.Components.Energy.Converters.Supersonic_Nozzle.Supersonic_Nozzle   class  SUAVE.Components.Energy.Converters.Turbine.Turbine   +class  SUAVE.Components.Energy.Converters.Turboelectric.Turboelectric +  +class  SUAVE.Components.Energy.Cooling.Cryogenic_Heat_Exchanger.Cryogenic_Heat_Exchanger

Detailed Description

Energy components meant to be used within an energy network.

@@ -149,7 +171,7 @@

Generated by - doxygen 1.8.14 + doxygen 1.8.15

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+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
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+
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+ + + +
+
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+
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+ +
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Cooling
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+
+ +

Components that cryogenically cool others. +More...

+

Components that cryogenically cool others.

+
+
+ + + + diff --git a/doxygen/group__Components-Energy-Distributors.html b/doxygen/group__Components-Energy-Distributors.html index 08bcf8b7..597e491f 100644 --- a/doxygen/group__Components-Energy-Distributors.html +++ b/doxygen/group__Components-Energy-Distributors.html @@ -1,9 +1,9 @@ - + - + SUAVE: Distributors @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
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+
+ + + + + + + + +
+
SUAVE +  2.5.0 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
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+
Nacelles
+
+
+ +

Nacelle.py. +More...

+

Nacelle.py.

+

Created: Jul 2021, M. Clarke

+
+
+ + + + diff --git a/doxygen/group__Components-Energy-Networks.html b/doxygen/group__Components-Energy-Networks.html index a2ff5aa0..d18af85a 100644 --- a/doxygen/group__Components-Energy-Networks.html +++ b/doxygen/group__Components-Energy-Networks.html @@ -1,9 +1,9 @@ - + - + SUAVE: Networks @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
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@license-end */ @@ -33,7 +36,7 @@ @@ -57,9 +60,11 @@

Classes

class  SUAVE.Components.Energy.Networks.Battery_Cell_Cycler.Battery_Cell_Cycler
 
class  SUAVE.Components.Energy.Networks.Battery_Ducted_Fan.Battery_Ducted_Fan
 
class  SUAVE.Components.Energy.Networks.Battery_Propeller.Battery_Propeller
 
class  SUAVE.Components.Energy.Networks.Dual_Battery_Ducted_Fan.Dual_Battery_Ducted_Fan
 
class  SUAVE.Components.Energy.Networks.Ducted_Fan.Ducted_Fan
 
class  SUAVE.Components.Energy.Networks.Lift_Forward_Propulsor.Lift_Forward_Propulsor
class  SUAVE.Components.Energy.Networks.Internal_Combustion_Propeller.Internal_Combustion_Propeller
 
class  SUAVE.Components.Energy.Networks.Internal_Combustion_Propeller_Constant_Speed.Internal_Combustion_Propeller_Constant_Speed
 
class  SUAVE.Components.Energy.Networks.Lift_Cruise.Lift_Cruise
 
class  SUAVE.Components.Energy.Networks.Liquid_Rocket.Liquid_Rocket
 
class  SUAVE.Components.Energy.Networks.Network.Network
 
class  SUAVE.Components.Energy.Networks.Network.Container
 
class  SUAVE.Components.Energy.Networks.Propulsor_Surrogate.Propulsor_Surrogate
 
class  SUAVE.Components.Energy.Networks.PyCycle.PyCycle
 
class  SUAVE.Components.Energy.Networks.Ramjet.Ramjet
 
class  SUAVE.Components.Energy.Networks.Scramjet.Scramjet
 
class  SUAVE.Components.Energy.Networks.Serial_Hybrid_Ducted_Fan.Serial_Hybrid_Ducted_Fan
 
class  SUAVE.Components.Energy.Networks.Solar.Solar
 
class  SUAVE.Components.Energy.Networks.Solar_Low_Fidelity.Solar_Low_Fidelity
 
class  SUAVE.Components.Energy.Networks.Turboelectric_HTS_Ducted_Fan.Turboelectric_HTS_Ducted_Fan
 
class  SUAVE.Components.Energy.Networks.Turbofan.Turbofan
 
class  SUAVE.Components.Energy.Networks.Turbojet_Super.Turbojet_Super
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -117,7 +124,7 @@
    + doxygen 1.8.15
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SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -103,6 +110,8 @@ + + @@ -117,7 +126,7 @@
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Classes

class  SUAVE.Components.Energy.Processes.Rocket_Thrust.Rocket_Thrust
 
class  SUAVE.Components.Energy.Processes.Solar_Radiation.Solar_Radiation
 
class  SUAVE.Components.Energy.Processes.Thrust.Thrust
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -105,6 +112,10 @@ Classes

class  SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion.Lithium_Ion   +class  SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion_LiFePO4_18650.Lithium_Ion_LiFePO4_18650 +  +class  SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion_LiNiMnCoO2_18650.Lithium_Ion_LiNiMnCoO2_18650 +  class  SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Sulfur.Lithium_Sulfur   @@ -117,7 +128,7 @@
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SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -117,7 +124,7 @@
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SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -125,7 +132,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/group__Components-Energy-Storages-Batteries.js b/doxygen/group__Components-Energy-Storages-Batteries.js index bd3902f2..096c6d29 100644 --- a/doxygen/group__Components-Energy-Storages-Batteries.js +++ b/doxygen/group__Components-Energy-Storages-Batteries.js @@ -4,14 +4,17 @@ var group__Components_Energy_Storages_Batteries = [ "Variable_Mass", "group__Components-Energy-Storages-Batteries-Variable__Mass.html", "group__Components-Energy-Storages-Batteries-Variable__Mass" ], [ "Battery", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.html", [ [ "__defaults__", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.html#a529cffa04fba4664bd432349f14fe268", null ], - [ "energy_calc", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.html#aa65c7a1b8d7ff1b54685851fb8d8f2cd", null ], + [ "chemistry", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.html#a42d0b6739ed87941a1b3a463ea3058f9", null ], + [ "current_capacitor_charge", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.html#a5ddf82deeb13f9bbae7c60cbfe3a3bfb", null ], [ "current_energy", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.html#ab75d672bb965c5aec6968c38e1fec34e", null ], - [ "discharge_model", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.html#ac1e376177175252082d5b465a7915f7a", null ], + [ "discharge_performance_map", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.html#a9930464c6ac27fbf2c1e5986451e1bdb", null ], [ "energy_density", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.html#af6ab54f2a19d11ce4b6362a21610c96c", null ], + [ "initial_temperature", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.html#a443530ab6d7d61e4a9c962a1060d6175", null ], [ "max_energy", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.html#a26fea5041ae1d5bb54a6a816420191a8", null ], [ "max_power", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.html#a216ae6ac99fb528716599d14c64a1888", null ], [ "max_voltage", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.html#af34d6af1003c3d903a9eef49f1a7f368", null ], [ "ragone", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.html#acfe3bfad30bd53b5c4608a7660606832", null ], - [ "resistance", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.html#a53d46e3ffe1570d23a4423005dd608a9", null ] + [ "resistance", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.html#a53d46e3ffe1570d23a4423005dd608a9", null ], + [ "specific_heat_capacity", "classSUAVE_1_1Components_1_1Energy_1_1Storages_1_1Batteries_1_1Battery_1_1Battery.html#a36b9efe4eec78bd29abd52176fd6033f", null ] ] ] ]; \ No newline at end of file diff --git a/doxygen/group__Components-Energy-Storages-Fuel__Tanks.html b/doxygen/group__Components-Energy-Storages-Fuel__Tanks.html new file mode 100644 index 00000000..a82374af --- /dev/null +++ b/doxygen/group__Components-Energy-Storages-Fuel__Tanks.html @@ -0,0 +1,120 @@ + + + + + + + +SUAVE: Fuel_Tanks + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
Fuel_Tanks
+
+
+ +

Contains different fuel tank types. +More...

+

Contains different fuel tank types.

+
+
+ + + + diff --git a/doxygen/group__Components-Energy-Storages.html b/doxygen/group__Components-Energy-Storages.html index f39bb19d..50e0e0d5 100644 --- a/doxygen/group__Components-Energy-Storages.html +++ b/doxygen/group__Components-Energy-Storages.html @@ -1,9 +1,9 @@ - + - + SUAVE: Storages @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -106,6 +113,9 @@  Batteries  Contains different battery types, separated into variable mass (metal-air) and constant mass batteries.
  + Fuel_Tanks + Contains different fuel tank types.

Detailed Description

Energy components that store energy (such as batteries)

@@ -116,7 +126,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/group__Components-Energy-Storages.js b/doxygen/group__Components-Energy-Storages.js index 8a91c41f..d35f0ca3 100644 --- a/doxygen/group__Components-Energy-Storages.js +++ b/doxygen/group__Components-Energy-Storages.js @@ -1,4 +1,5 @@ var group__Components_Energy_Storages = [ - [ "Batteries", "group__Components-Energy-Storages-Batteries.html", "group__Components-Energy-Storages-Batteries" ] + [ "Batteries", "group__Components-Energy-Storages-Batteries.html", "group__Components-Energy-Storages-Batteries" ], + [ "Fuel_Tanks", "group__Components-Energy-Storages-Fuel__Tanks.html", null ] ]; \ No newline at end of file diff --git a/doxygen/group__Components-Energy.html b/doxygen/group__Components-Energy.html index 720e0c17..30317783 100644 --- a/doxygen/group__Components-Energy.html +++ b/doxygen/group__Components-Energy.html @@ -1,9 +1,9 @@ - + - + SUAVE: Energy @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -103,9 +110,14 @@ + + + + + @@ -132,7 +144,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/group__Components-Energy.js b/doxygen/group__Components-Energy.js index a873683e..77eb5223 100644 --- a/doxygen/group__Components-Energy.js +++ b/doxygen/group__Components-Energy.js @@ -1,6 +1,8 @@ var group__Components_Energy = [ + [ "Charging", "group__Components-Energy-Charging.html", "group__Components-Energy-Charging" ], [ "Converters", "group__Components-Energy-Converters.html", "group__Components-Energy-Converters" ], + [ "Cooling", "group__Components-Energy-Cooling.html", null ], [ "Distributors", "group__Components-Energy-Distributors.html", "group__Components-Energy-Distributors" ], [ "Networks", "group__Components-Energy-Networks.html", "group__Components-Energy-Networks" ], [ "Peripherals", "group__Components-Energy-Peripherals.html", "group__Components-Energy-Peripherals" ], diff --git a/doxygen/group__Components-Landing__Gear.js b/doxygen/group__Components-Landing__Gear.js new file mode 100644 index 00000000..a65b13d2 --- /dev/null +++ b/doxygen/group__Components-Landing__Gear.js @@ -0,0 +1,23 @@ +var group__Components_Landing__Gear = +[ + [ "Landing_Gear", "classSUAVE_1_1Components_1_1Landing__Gear_1_1Landing__Gear_1_1Landing__Gear.html", [ + [ "__defaults__", "classSUAVE_1_1Components_1_1Landing__Gear_1_1Landing__Gear_1_1Landing__Gear.html#a5b545fccc3b0b5f05e8e3008d5c5a8cf", null ], + [ "tag", "classSUAVE_1_1Components_1_1Landing__Gear_1_1Landing__Gear_1_1Landing__Gear.html#aed0f1965909ce50ae9e3e79c4c802fd0", null ] + ] ], + [ "Main_Landing_Gear", "classSUAVE_1_1Components_1_1Landing__Gear_1_1Main__Landing__Gear_1_1Main__Landing__Gear.html", [ + [ "__defaults__", "classSUAVE_1_1Components_1_1Landing__Gear_1_1Main__Landing__Gear_1_1Main__Landing__Gear.html#a49f8c147fcead8400fbf06ba5607257c", null ], + [ "strut_length", "classSUAVE_1_1Components_1_1Landing__Gear_1_1Main__Landing__Gear_1_1Main__Landing__Gear.html#a0746446ff4e556f4bfaa8e8133269cf8", null ], + [ "tag", "classSUAVE_1_1Components_1_1Landing__Gear_1_1Main__Landing__Gear_1_1Main__Landing__Gear.html#afef7bd4ee2b5f3df712b783c14ab7efc", null ], + [ "tire_diameter", "classSUAVE_1_1Components_1_1Landing__Gear_1_1Main__Landing__Gear_1_1Main__Landing__Gear.html#a3fdc93cc5f4a391eeff8ce20588a422d", null ], + [ "units", "classSUAVE_1_1Components_1_1Landing__Gear_1_1Main__Landing__Gear_1_1Main__Landing__Gear.html#adf90062bd324cc58d3fa5c4165412f50", null ], + [ "wheels", "classSUAVE_1_1Components_1_1Landing__Gear_1_1Main__Landing__Gear_1_1Main__Landing__Gear.html#abcfe6aac23f12d46d7c1eaa686982d41", null ] + ] ], + [ "Nose_Landing_Gear", "classSUAVE_1_1Components_1_1Landing__Gear_1_1Nose__Landing__Gear_1_1Nose__Landing__Gear.html", [ + [ "__defaults__", "classSUAVE_1_1Components_1_1Landing__Gear_1_1Nose__Landing__Gear_1_1Nose__Landing__Gear.html#ac5ad8f513c8037bdcafe89490ae9b771", null ], + [ "strut_length", "classSUAVE_1_1Components_1_1Landing__Gear_1_1Nose__Landing__Gear_1_1Nose__Landing__Gear.html#ab9bd2221e3bc7debc15df18403b3d039", null ], + [ "tag", "classSUAVE_1_1Components_1_1Landing__Gear_1_1Nose__Landing__Gear_1_1Nose__Landing__Gear.html#aa1d302486ac5d47da8154f0b52470a39", null ], + [ "tire_diameter", "classSUAVE_1_1Components_1_1Landing__Gear_1_1Nose__Landing__Gear_1_1Nose__Landing__Gear.html#ab0f697c45997ba5b6de8021eef2850be", null ], + [ "units", "classSUAVE_1_1Components_1_1Landing__Gear_1_1Nose__Landing__Gear_1_1Nose__Landing__Gear.html#a4d7fc084dfa42ced1729cd0949e5db24", null ], + [ "wheels", "classSUAVE_1_1Components_1_1Landing__Gear_1_1Nose__Landing__Gear_1_1Nose__Landing__Gear.html#a6ba38038577df2b45650d9452cb87cda", null ] + ] ] +]; \ No newline at end of file diff --git a/doxygen/group__Components-Nacelles.html b/doxygen/group__Components-Nacelles.html new file mode 100644 index 00000000..f6b385e9 --- /dev/null +++ b/doxygen/group__Components-Nacelles.html @@ -0,0 +1,131 @@ + + + + + + + +SUAVE: Nacelles + + + + + + + + + + + + + + + +
+
+

Modules

 Charging
 
 Converters
 Energy components meant to be used within an energy network.
 
 Cooling
 Components that cryogenically cool others.
 
 Distributors
 Components that move energy/control energy/power in a network.
 
+ + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + + +
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
Nacelles
+
+
+ +

These typically contain the primary payload of the vehicle. +More...

+ + + + +

+Classes

class  SUAVE.Components.Nacelles.Nacelle.Nacelle
 
+

Detailed Description

+

These typically contain the primary payload of the vehicle.

+

Nacelle.py.

+

Created: Jul 2021, M. Clarke

+
+
+ + + + diff --git a/doxygen/group__Components-Nacelles.js b/doxygen/group__Components-Nacelles.js new file mode 100644 index 00000000..445a6f52 --- /dev/null +++ b/doxygen/group__Components-Nacelles.js @@ -0,0 +1,24 @@ +var group__Components_Nacelles = +[ + [ "Nacelle", "classSUAVE_1_1Components_1_1Nacelles_1_1Nacelle_1_1Nacelle.html", [ + [ "__defaults__", "classSUAVE_1_1Components_1_1Nacelles_1_1Nacelle_1_1Nacelle.html#ae5ddc3db6efb431b82fb2bbf5b824ca2", null ], + [ "append_airfoil", "classSUAVE_1_1Components_1_1Nacelles_1_1Nacelle_1_1Nacelle.html#a2530f804f8e38063f63333349e33a5a4", null ], + [ "append_segment", "classSUAVE_1_1Components_1_1Nacelles_1_1Nacelle_1_1Nacelle.html#aa8629381a1b7492ed80554788a99e6a6", null ], + [ "body_to_nac_vel", "classSUAVE_1_1Components_1_1Nacelles_1_1Nacelle_1_1Nacelle.html#a5621a1639a60c0d0449be4b9c6fe614e", null ], + [ "nac_vel_to_body", "classSUAVE_1_1Components_1_1Nacelles_1_1Nacelle_1_1Nacelle.html#a5ffbb24f270eb3aa06a5db2ac4f4e260", null ], + [ "vec_to_vel", "classSUAVE_1_1Components_1_1Nacelles_1_1Nacelle_1_1Nacelle.html#a72d645271916069fd62b434dc576e410", null ], + [ "aerodynamic_center", "classSUAVE_1_1Components_1_1Nacelles_1_1Nacelle_1_1Nacelle.html#a4e5c12076105f48ff5b93b3cb0934679", null ], + [ "Airfoil", "classSUAVE_1_1Components_1_1Nacelles_1_1Nacelle_1_1Nacelle.html#a715f3490c583270191a11198f1a2640e", null ], + [ "areas", "classSUAVE_1_1Components_1_1Nacelles_1_1Nacelle_1_1Nacelle.html#ac6cd1e9d61a9b251a7bf5de1f28ae41c", null ], + [ "cowling_airfoil_angle", "classSUAVE_1_1Components_1_1Nacelles_1_1Nacelle_1_1Nacelle.html#acbbad4e6b16b36dbe1ceee15433abed8", null ], + [ "diameter", "classSUAVE_1_1Components_1_1Nacelles_1_1Nacelle_1_1Nacelle.html#aa5f1ac06d95f975c10fd19337110c137", null ], + [ "differential_pressure", "classSUAVE_1_1Components_1_1Nacelles_1_1Nacelle_1_1Nacelle.html#ad765cc9ec62046f2d4452828bf16cfd9", null ], + [ "flow_through", "classSUAVE_1_1Components_1_1Nacelles_1_1Nacelle_1_1Nacelle.html#ae9bda35371563e3eb6c464f06c797e47", null ], + [ "inlet_diameter", "classSUAVE_1_1Components_1_1Nacelles_1_1Nacelle_1_1Nacelle.html#a41935580f02f87271c3fc17d85034820", null ], + [ "length", "classSUAVE_1_1Components_1_1Nacelles_1_1Nacelle_1_1Nacelle.html#aceda1593b44746cc2b5c9aa2cbeccf1e", null ], + [ "orientation_euler_angles", "classSUAVE_1_1Components_1_1Nacelles_1_1Nacelle_1_1Nacelle.html#ab8e853f87560d4fc26cd0a816b16f77f", null ], + [ "origin", "classSUAVE_1_1Components_1_1Nacelles_1_1Nacelle_1_1Nacelle.html#a745ce2dc66c1914eb4c2513f3b222fff", null ], + [ "Segments", "classSUAVE_1_1Components_1_1Nacelles_1_1Nacelle_1_1Nacelle.html#a6d9ae942479fe9a052fe4df862280dd6", null ], + [ "tag", "classSUAVE_1_1Components_1_1Nacelles_1_1Nacelle_1_1Nacelle.html#ac5fe3503dfd989dfd9ce58f6552e8b8b", null ] + ] ] +]; \ No newline at end of file diff --git a/doxygen/group__Components-Payloads.html b/doxygen/group__Components-Payloads.html index 257aba95..e7dda04f 100644 --- a/doxygen/group__Components-Payloads.html +++ b/doxygen/group__Components-Payloads.html @@ -1,9 +1,9 @@ - + - + SUAVE: Payloads @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -103,21 +110,16 @@ - - - - - -

Classes

class  SUAVE.Components.Payloads.Cargo.Cargo
 
class  SUAVE.Components.Payloads.Payload.Payload
 
class  SUAVE.Components.Payloads.Payload.Container
 
class  SUAVE.Components.Payloads.Person.Person
 
class  SUAVE.Components.Payloads.Satellite.Satellite
 

Detailed Description

Available payload components

init.py.

-

Created: Modified: Feb 2016, T. MacDonald

+

Created:

+

Modified: Feb 2016, T. MacDonald

@@ -125,7 +127,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/group__Components-Payloads.js b/doxygen/group__Components-Payloads.js index 34bb390a..4554c72c 100644 --- a/doxygen/group__Components-Payloads.js +++ b/doxygen/group__Components-Payloads.js @@ -1,20 +1,8 @@ var group__Components_Payloads = [ - [ "Cargo", "classSUAVE_1_1Components_1_1Payloads_1_1Cargo_1_1Cargo.html", [ - [ "__defaults__", "classSUAVE_1_1Components_1_1Payloads_1_1Cargo_1_1Cargo.html#a4f97de17ea1ae1c4e6e68e3a6307952e", null ], - [ "tag", "classSUAVE_1_1Components_1_1Payloads_1_1Cargo_1_1Cargo.html#a0113edcfd4ad704eed565e3201d5a5fb", null ] - ] ], [ "Payload", "classSUAVE_1_1Components_1_1Payloads_1_1Payload_1_1Payload.html", [ [ "__defaults__", "classSUAVE_1_1Components_1_1Payloads_1_1Payload_1_1Payload.html#a8ab675e813585c3036cfeffcbd976f33", null ], [ "tag", "classSUAVE_1_1Components_1_1Payloads_1_1Payload_1_1Payload.html#aa90c294700820fd00984a65f0da3417a", null ] ] ], - [ "Container", "classSUAVE_1_1Components_1_1Payloads_1_1Payload_1_1Container.html", null ], - [ "Person", "classSUAVE_1_1Components_1_1Payloads_1_1Person_1_1Person.html", [ - [ "__defaults__", "classSUAVE_1_1Components_1_1Payloads_1_1Person_1_1Person.html#a057b4069cf1182ae815f9ac23828a483", null ], - [ "tag", "classSUAVE_1_1Components_1_1Payloads_1_1Person_1_1Person.html#a8a256ceea2c9695987a0760609a2fd3a", null ] - ] ], - [ "Satellite", "classSUAVE_1_1Components_1_1Payloads_1_1Satellite_1_1Satellite.html", [ - [ "__defaults__", "classSUAVE_1_1Components_1_1Payloads_1_1Satellite_1_1Satellite.html#a0dd0be04f50f34e19e8c5130a4d38956", null ], - [ "tag", "classSUAVE_1_1Components_1_1Payloads_1_1Satellite_1_1Satellite.html#a11c080c0b8112d73fe2eb41668bf5809", null ] - ] ] + [ "Container", "classSUAVE_1_1Components_1_1Payloads_1_1Payload_1_1Container.html", null ] ]; \ No newline at end of file diff --git a/doxygen/group__Components-Propulsors.html b/doxygen/group__Components-Propulsors.html index d1f8fa2b..56b273a1 100644 --- a/doxygen/group__Components-Propulsors.html +++ b/doxygen/group__Components-Propulsors.html @@ -1,9 +1,9 @@ - + - + SUAVE: Propulsors @@ -13,14 +13,13 @@ - @@ -33,13 +32,13 @@ Logo
SUAVE -  1.1.0 +  2.4.0
An Aerospace Vehicle Environment for Designing Future Aircraft
- @@ -48,7 +47,7 @@ onblur="searchBox.OnSearchFieldFocus(false)" onkeyup="searchBox.OnSearchFieldChange(event)"/> - +
@@ -57,9 +56,11 @@ - +
@@ -73,7 +74,9 @@
@@ -115,9 +118,7 @@ diff --git a/doxygen/group__Components-Propulsors.js b/doxygen/group__Components-Propulsors.js index 82e6f1cf..dfbdceeb 100644 --- a/doxygen/group__Components-Propulsors.js +++ b/doxygen/group__Components-Propulsors.js @@ -2,9 +2,17 @@ var group__Components_Propulsors = [ [ "Propulsor", "classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Propulsor.html", [ [ "__defaults__", "classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Propulsor.html#a1a13b12fb63990dcd51c6ecc46c83f21", null ], - [ "tag", "classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Propulsor.html#a297d16d03533b9da160be9d970073588", null ] + [ "areas", "classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Propulsor.html#a7a272c60a24251274736178759b23670", null ], + [ "engine_length", "classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Propulsor.html#ace561d0f1785a664db4b0819bbd52ac1", null ], + [ "generative_design_max_per_vehicle", "classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Propulsor.html#a227b12da3c263476f6590fc0b20ae168", null ], + [ "nacelle_diameter", "classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Propulsor.html#afb86b97c48b3de4244e5b0b1a6eb1596", null ], + [ "non_dimensional_origin", "classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Propulsor.html#a5de38c53079018f365142c9a53284def", null ], + [ "number_of_engines", "classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Propulsor.html#a858187796822a9a4c783cd74aab0d717", null ], + [ "tag", "classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Propulsor.html#a297d16d03533b9da160be9d970073588", null ], + [ "wing_mounted", "classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Propulsor.html#ab4bb759ed381dabbe1f40027aa20230a", null ] ] ], [ "Container", "classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Container.html", [ - [ "evaluate_thrust", "classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Container.html#a42e24eef8ee7108c8f99379060824724", null ] + [ "evaluate_thrust", "classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Container.html#a42e24eef8ee7108c8f99379060824724", null ], + [ "get_children", "classSUAVE_1_1Components_1_1Propulsors_1_1Propulsor_1_1Container.html#a36a16c1656b07b2be4ac4e2e9bde3b2e", null ] ] ] ]; \ No newline at end of file diff --git a/doxygen/group__Components-Systems.html b/doxygen/group__Components-Systems.html index 00fc81db..14a31083 100644 --- a/doxygen/group__Components-Systems.html +++ b/doxygen/group__Components-Systems.html @@ -1,9 +1,9 @@ - + - + SUAVE: Systems @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@
- +
@@ -73,7 +78,9 @@
@@ -115,7 +122,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/group__Components-Systems.js b/doxygen/group__Components-Systems.js index 19c27eb1..418fdabf 100644 --- a/doxygen/group__Components-Systems.js +++ b/doxygen/group__Components-Systems.js @@ -4,8 +4,7 @@ var group__Components_Systems = [ "__defaults__", "classSUAVE_1_1Components_1_1Systems_1_1System_1_1System.html#afc1811095781c3b874ab279c8449b53a", null ], [ "accessories", "classSUAVE_1_1Components_1_1Systems_1_1System_1_1System.html#a22ad3a5dc4d33c9c53a2d01897173e99", null ], [ "control", "classSUAVE_1_1Components_1_1Systems_1_1System_1_1System.html#adb487ae49fd4892c42ef0cd2ffdd9530", null ], - [ "mass_properties", "classSUAVE_1_1Components_1_1Systems_1_1System_1_1System.html#ac257d2d78c0da7c92ddd9cf16256bfe5", null ], - [ "position", "classSUAVE_1_1Components_1_1Systems_1_1System_1_1System.html#ae3836f93b6ac5c6bab29ec4074b8ff38", null ], + [ "origin", "classSUAVE_1_1Components_1_1Systems_1_1System_1_1System.html#a552a352294cfe4dbd1b6869e2a7851c5", null ], [ "tag", "classSUAVE_1_1Components_1_1Systems_1_1System_1_1System.html#a4fa86faee2bbe57bbd444c14417e1e76", null ] ] ] ]; \ No newline at end of file diff --git a/doxygen/group__Components-Wings-Airfoils.html b/doxygen/group__Components-Wings-Airfoils.html index 1c9a37ba..bdcac393 100644 --- a/doxygen/group__Components-Wings-Airfoils.html +++ b/doxygen/group__Components-Wings-Airfoils.html @@ -1,9 +1,9 @@ - + - + SUAVE: Airfoils @@ -13,14 +13,13 @@ - @@ -33,13 +32,13 @@ Logo
SUAVE -  1.1.0 +  2.4.0
An Aerospace Vehicle Environment for Designing Future Aircraft
- @@ -48,7 +47,7 @@ onblur="searchBox.OnSearchFieldFocus(false)" onkeyup="searchBox.OnSearchFieldChange(event)"/> - +
@@ -57,9 +56,11 @@ - +
@@ -73,7 +74,9 @@
@@ -92,8 +95,7 @@
Airfoils
@@ -106,68 +108,17 @@ Classes

class  SUAVE.Components.Wings.Airfoils.Airfoil.Airfoil   - - - -

-Functions

def SUAVE.Components.Wings.Airfoils.load_airfoils.load_airfoils (directory, extension='.dat')
 

Detailed Description

init.py

-

Created: Modified: Feb 2016, T. MacDonald

-

Function Documentation

- -

◆ load_airfoils()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Components.Wings.Airfoils.load_airfoils.load_airfoils ( directory,
 extension = '.dat' 
)
-
-
Loads airfoil cooridinate points from .dat file
-
-Assumptions:
-None
-
-Source:
-N/A
-
-Inputs:
-None
-
-Outputs:
-None
-
-Properties Used:
-N/A
-
-
-
+

Created:
+ Modified: Feb 2016, T. MacDonald Modified: Feb 2020, M. Clarke

diff --git a/doxygen/group__Components-Wings-Airfoils.js b/doxygen/group__Components-Wings-Airfoils.js index 81bcb9fd..f4b952e5 100644 --- a/doxygen/group__Components-Wings-Airfoils.js +++ b/doxygen/group__Components-Wings-Airfoils.js @@ -2,11 +2,9 @@ var group__Components_Wings_Airfoils = [ [ "Airfoil", "classSUAVE_1_1Components_1_1Wings_1_1Airfoils_1_1Airfoil_1_1Airfoil.html", [ [ "__defaults__", "classSUAVE_1_1Components_1_1Wings_1_1Airfoils_1_1Airfoil_1_1Airfoil.html#aebc33642fbd2cee33d7238535c4ed955", null ], - [ "import_airfoil_dat", "classSUAVE_1_1Components_1_1Wings_1_1Airfoils_1_1Airfoil_1_1Airfoil.html#a2fa4f8f73f27a56e42ae3ea2df7584a8", null ], [ "coordinate_file", "classSUAVE_1_1Components_1_1Wings_1_1Airfoils_1_1Airfoil_1_1Airfoil.html#ad622a4ec18682cda7a5392a9a190f1e3", null ], [ "points", "classSUAVE_1_1Components_1_1Wings_1_1Airfoils_1_1Airfoil_1_1Airfoil.html#a17ef2e1e3e857a5397db8b47044092d3", null ], [ "tag", "classSUAVE_1_1Components_1_1Wings_1_1Airfoils_1_1Airfoil_1_1Airfoil.html#ab960bdfdc567919896007568600ce750", null ], [ "thickness_to_chord", "classSUAVE_1_1Components_1_1Wings_1_1Airfoils_1_1Airfoil_1_1Airfoil.html#a23f121ba0dabb98693c6b5881d01a028", null ] - ] ], - [ "load_airfoils", "group__Components-Wings-Airfoils.html#gafe2d51e774137ad0e2e132da1bd8255b", null ] + ] ] ]; \ No newline at end of file diff --git a/doxygen/group__Components-Wings-Control__Surfaces.html b/doxygen/group__Components-Wings-Control__Surfaces.html new file mode 100644 index 00000000..4c2f82d0 --- /dev/null +++ b/doxygen/group__Components-Wings-Control__Surfaces.html @@ -0,0 +1,140 @@ + + + + + + + +SUAVE: Control_Surfaces + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ + + + + + diff --git a/doxygen/group__Components-Wings-Control__Surfaces.js b/doxygen/group__Components-Wings-Control__Surfaces.js new file mode 100644 index 00000000..fe5ea688 --- /dev/null +++ b/doxygen/group__Components-Wings-Control__Surfaces.js @@ -0,0 +1,46 @@ +var group__Components_Wings_Control__Surfaces = +[ + [ "Aileron", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Aileron_1_1Aileron.html", [ + [ "__defaults__", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Aileron_1_1Aileron.html#a1aef6c2fff4e4610f8c3957e970eba1b", null ], + [ "hinge_fraction", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Aileron_1_1Aileron.html#a0335292c5a97375a2bddc0983b813d44", null ], + [ "sign_duplicate", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Aileron_1_1Aileron.html#ac25dc134f708135060c5cb2b266054b6", null ], + [ "tag", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Aileron_1_1Aileron.html#afc38a662433e229cb08f4861a4ad43e6", null ] + ] ], + [ "Control_Surface", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Control__Surface_1_1Control__Surface.html", [ + [ "__defaults__", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Control__Surface_1_1Control__Surface.html#a266272aaf7c761a92f0d4263d08ec6f6", null ], + [ "chord_fraction", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Control__Surface_1_1Control__Surface.html#ad310ffe2632c5f8aafc423137a8e7790", null ], + [ "configuration_type", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Control__Surface_1_1Control__Surface.html#abe8c19fab542263392f677464859fd5b", null ], + [ "deflection", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Control__Surface_1_1Control__Surface.html#ab384c96474818b75e512327dac1a124c", null ], + [ "gain", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Control__Surface_1_1Control__Surface.html#a068ded7bfe62fcd99af1546b09e7f413", null ], + [ "hinge_fraction", 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"classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Elevator_1_1Elevator.html", [ + [ "__defaults__", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Elevator_1_1Elevator.html#a14963fc6797c8433c15b0ae135e765c4", null ], + [ "hinge_fraction", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Elevator_1_1Elevator.html#aff3c52011ae60ea6fc8a57609f50fd7e", null ], + [ "sign_duplicate", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Elevator_1_1Elevator.html#a7820e96e94fa54a3a83014ff1e4e8530", null ], + [ "tag", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Elevator_1_1Elevator.html#afa594ff8374a2c1ad267a913ff851e9f", null ] + ] ], + [ "Flap", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Flap_1_1Flap.html", [ + [ "__defaults__", "classSUAVE_1_1Components_1_1Wings_1_1Control__Surfaces_1_1Flap_1_1Flap.html#a71a66ce5826c44d8f027db149ae4430a", null ], + [ "hinge_fraction", 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b/doxygen/group__Components-Wings.html @@ -1,9 +1,9 @@ - + - + SUAVE: Wings @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -137,7 +147,7 @@
    + doxygen 1.8.15
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+ - + SUAVE: Components @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -104,6 +111,8 @@ + + @@ -116,15 +125,18 @@ - - + + + + + + + + - - - @@ -146,11 +158,7 @@ - - - - - + @@ -161,7 +169,10 @@

Modules

 Airfoils
 
 Configs
 This is the component that defines the template for vehicle configurations.
 
 Fuselages
 Components traditionally considered to be the fuselage of a vehicle.
 
 Landing Gear
 Components considered are the Main and Nose Landing Gear.
 Landing Gear
 Components considered are the Main and Nose Landing Gear.
 
 Lofted_Body_Segment
 Components traditionally considered to be the fuselage of a vehicle.
 
 Nacelles
 These typically contain the primary payload of the vehicle.
 
 Payloads
 Available payload componentsinit.py.
 
 Propulsors
 These are the components used to provide thrust to a vehicle.
 
 Systems
 These are the components which define a vehicle's onboard systems.
 
 
class  SUAVE.Components.Lofted_Body.Section
 
class  SUAVE.Components.Lofted_Body.Curve
 
class  SUAVE.Components.Lofted_Body.SectionContainer
 
class  SUAVE.Components.Lofted_Body.CurveContainer
class  SUAVE.Components.Lofted_Body.Section_Container
 
class  SUAVE.Components.Mass_Properties.Mass_Properties
 

Detailed Description

Components are classes that represent objects that are put together to form a vehicle.

-

They contain default variables and may contain functions that operate on these variables.

+

init.py

+

They contain default variables and may contain functions that operate on these variables.

+

Created:

+

Modified: Feb 2016, T. MacDonald Modified: Feb 2020, M. Clarke

@@ -169,7 +180,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/group__Components.js b/doxygen/group__Components.js index a922ad13..ffac0129 100644 --- a/doxygen/group__Components.js +++ b/doxygen/group__Components.js @@ -1,16 +1,21 @@ var group__Components = [ + [ "Airfoils", "group__Components-Airfoils.html", "group__Components-Airfoils" ], [ "Configs", "group__Components-Configs.html", "group__Components-Configs" ], [ "Costs", "group__Components-Costs.html", "group__Components-Costs" ], [ "Energy", "group__Components-Energy.html", "group__Components-Energy" ], [ "Fuselages", "group__components-fuselages.html", "group__components-fuselages" ], - [ "Landing Gear", "group__components-landing__gear.html", null ], + [ "Landing Gear", "group__Components-Landing__Gear.html", "group__Components-Landing__Gear" ], + [ "Lofted_Body_Segment", "group__components-Lofted__Body__Segment.html", null ], + [ "Nacelles", "group__Components-Nacelles.html", "group__Components-Nacelles" ], [ "Payloads", "group__Components-Payloads.html", "group__Components-Payloads" ], - [ "Propulsors", "group__Components-Propulsors.html", "group__Components-Propulsors" ], [ "Systems", "group__Components-Systems.html", "group__Components-Systems" ], [ "Wings", "group__Components-Wings.html", "group__Components-Wings" ], [ "Component", "classSUAVE_1_1Components_1_1Component_1_1Component.html", [ [ "__defaults__", "classSUAVE_1_1Components_1_1Component_1_1Component.html#a2d9252624c70b5d919bc9ec4809aaeff", null ], + [ "generative_design_characteristics", "classSUAVE_1_1Components_1_1Component_1_1Component.html#a9b0142ce837eb8fd7f11b0581acee372", null ], + [ "generative_design_max_per_vehicle", "classSUAVE_1_1Components_1_1Component_1_1Component.html#ae7305ad76eff4eb0eeb3ef2eaa198cbb", null ], + [ "generative_design_special_parent", "classSUAVE_1_1Components_1_1Component_1_1Component.html#aa6dedec164a94dbb1d776aeb42589475", null ], [ "origin", "classSUAVE_1_1Components_1_1Component_1_1Component.html#a73f01c28d509653b176d616ddf5774d6", null ], [ "tag", "classSUAVE_1_1Components_1_1Component_1_1Component.html#a03eb542a5d248132cad459e2b1da0712", null ] ] ], @@ -22,6 +27,7 @@ var group__Components = [ "alt_vc", "classSUAVE_1_1Components_1_1Envelope_1_1Envelope.html#a9fa1d524f7072f9d99a79b7a4960e59f", null ], [ "gust", "classSUAVE_1_1Components_1_1Envelope_1_1Envelope.html#a817cbf39aeec6758432ee3eab3f4b882", null ], [ "limit_load", "classSUAVE_1_1Components_1_1Envelope_1_1Envelope.html#ad9653f50cbbd9323878da353fe49e6fe", null ], + [ "limit_loads", "classSUAVE_1_1Components_1_1Envelope_1_1Envelope.html#a112b162587abd43e313aede02cfcf9c9", null ], [ "maneuver", "classSUAVE_1_1Components_1_1Envelope_1_1Envelope.html#a49d434a90895935ad7a89d77db9f763e", null ], [ "max_ceiling", "classSUAVE_1_1Components_1_1Envelope_1_1Envelope.html#a3d0278765533a69d81e74c9da73d6677", null ], [ "maximum_dynamic_pressure", "classSUAVE_1_1Components_1_1Envelope_1_1Envelope.html#a510c802653d940134add99ab206a186c", null ], @@ -31,7 +37,6 @@ var group__Components = ] ], [ "Lofted_Body", "classSUAVE_1_1Components_1_1Lofted__Body_1_1Lofted__Body.html", [ [ "__defaults__", "classSUAVE_1_1Components_1_1Lofted__Body_1_1Lofted__Body.html#a9a41b92aeca26b01f43527677f0f715a", null ], - [ "Sections", "classSUAVE_1_1Components_1_1Lofted__Body_1_1Lofted__Body.html#a436ac8f3ad1b562b09051693377b70df", null ], [ "Segments", "classSUAVE_1_1Components_1_1Lofted__Body_1_1Lofted__Body.html#ad997a3fd0531a8c08fe66cd427b27391", null ], [ "tag", "classSUAVE_1_1Components_1_1Lofted__Body_1_1Lofted__Body.html#a9be10450331f26faa3e4f6e222e12ee1", null ] ] ], @@ -43,18 +48,13 @@ var group__Components = ] ], [ "Section", "classSUAVE_1_1Components_1_1Lofted__Body_1_1Section.html", [ [ "__defaults__", "classSUAVE_1_1Components_1_1Lofted__Body_1_1Section.html#a18e362879f7fe5a3c64d9320eff94a07", null ], - [ "Curves", "classSUAVE_1_1Components_1_1Lofted__Body_1_1Section.html#a5fea20dce1b6cebb2ea0bde9f41d7393", null ], [ "next", "classSUAVE_1_1Components_1_1Lofted__Body_1_1Section.html#afc04bc14b1deba0e6a9a3b7e2a7f1973", null ], [ "prev", "classSUAVE_1_1Components_1_1Lofted__Body_1_1Section.html#a4a00ad1e29432ac6ff0a0b7a30f8e3eb", null ], [ "tag", "classSUAVE_1_1Components_1_1Lofted__Body_1_1Section.html#adcd5d2ed1bb07f1fe5cd326c10341d85", null ] ] ], - [ "Curve", "classSUAVE_1_1Components_1_1Lofted__Body_1_1Curve.html", [ - [ "__defaults__", "classSUAVE_1_1Components_1_1Lofted__Body_1_1Curve.html#a843aec6fd606521a8c2336e992438158", null ], - [ "points", "classSUAVE_1_1Components_1_1Lofted__Body_1_1Curve.html#a3f471917d7e9ebdab3b61771389ddd21", null ], - [ "tag", "classSUAVE_1_1Components_1_1Lofted__Body_1_1Curve.html#aa3d06b7633c0175e5b5020576d767c89", null ] + [ "Section_Container", "classSUAVE_1_1Components_1_1Lofted__Body_1_1Section__Container.html", [ + [ "get_children", "classSUAVE_1_1Components_1_1Lofted__Body_1_1Section__Container.html#a345540bcc35295bf4ac162292381fa8c", null ] ] ], - [ "SectionContainer", "classSUAVE_1_1Components_1_1Lofted__Body_1_1SectionContainer.html", null ], - [ "CurveContainer", "classSUAVE_1_1Components_1_1Lofted__Body_1_1CurveContainer.html", null ], [ "Mass_Properties", "classSUAVE_1_1Components_1_1Mass__Properties_1_1Mass__Properties.html", [ [ "__defaults__", "classSUAVE_1_1Components_1_1Mass__Properties_1_1Mass__Properties.html#ac9cfb57a83a0c203a8d0c99b5b5202c2", null ], [ "center_of_gravity", "classSUAVE_1_1Components_1_1Mass__Properties_1_1Mass__Properties.html#a466525e75a39a1e738884a13296c29d1", null ], @@ -70,6 +70,7 @@ var group__Components = [ "tag", "classSUAVE_1_1Components_1_1Physical__Component_1_1Physical__Component.html#a262d78a38d51f7f484f930155843edff", null ] ] ], [ "Container", "classSUAVE_1_1Components_1_1Physical__Component_1_1Container.html", [ - [ "sum_mass", "classSUAVE_1_1Components_1_1Physical__Component_1_1Container.html#ae51f620275537cac1c60ba136c68735e", null ] + [ "sum_mass", "classSUAVE_1_1Components_1_1Physical__Component_1_1Container.html#ae51f620275537cac1c60ba136c68735e", null ], + [ "total_moment", "classSUAVE_1_1Components_1_1Physical__Component_1_1Container.html#a7c5629c0cc965bad4c8799fd7616f3e4", null ] ] ] ]; \ No newline at end of file diff --git a/doxygen/group__Core.html b/doxygen/group__Core.html index fa8beadf..ad6a14c4 100644 --- a/doxygen/group__Core.html +++ b/doxygen/group__Core.html @@ -1,9 +1,9 @@ - + - + SUAVE: Core @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -125,6 +132,8 @@   def SUAVE.Core.Arrays.atleast_2d (A, oned_as='row')   +def SUAVE.Core.Arrays.append_array (A=None, B=None) +  def SUAVE.Core.Units.__rmul__ (self, other)   def SUAVE.Core.Units.__rdiv__ (self, other) @@ -221,6 +230,51 @@

+

◆ append_array()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Core.Arrays.append_array ( A = None,
 B = None 
)
+
+
A stacking operation used by merged to put together data structures
+
+    Assumptions:
+    None
+
+    Source:
+    N/A
+
+    Inputs:
+    A [array]
+    B [array]
+
+    Outputs:
+    array
+
+    Properties Used:
+    None
+
+
+

◆ atleast_2d()

@@ -340,7 +394,7 @@

Generated by - doxygen 1.8.14 + doxygen 1.8.15

diff --git a/doxygen/group__Core.js b/doxygen/group__Core.js index e5898df6..413382b5 100644 --- a/doxygen/group__Core.js +++ b/doxygen/group__Core.js @@ -1,21 +1,23 @@ var group__Core = [ [ "Container", "classSUAVE_1_1Core_1_1Container_1_1Container.html", [ - [ "__init__", "classSUAVE_1_1Core_1_1Container_1_1Container.html#a7cbac1bbad1dd3279655f10d8315ffb2", null ], + [ "__init__", "classSUAVE_1_1Core_1_1Container_1_1Container.html#ade60f359bbe42e43d4688674fca339a4", null ], [ "__defaults__", "classSUAVE_1_1Core_1_1Container_1_1Container.html#a566ffa56d67a534512525e5212065568", null ], [ "append", "classSUAVE_1_1Core_1_1Container_1_1Container.html#a0f2652c760244b0128b854b9dce9a774", null ], - [ "extend", "classSUAVE_1_1Core_1_1Container_1_1Container.html#a6e9b7dbfa8ffa88162d698d32318b22d", null ] + [ "extend", "classSUAVE_1_1Core_1_1Container_1_1Container.html#a6e9b7dbfa8ffa88162d698d32318b22d", null ], + [ "get_children", "classSUAVE_1_1Core_1_1Container_1_1Container.html#ac8cc25ab031c7085e6b1e961ff562fcd", null ] ] ], [ "Data", "classSUAVE_1_1Core_1_1Data_1_1Data.html", [ - [ "__init__", "classSUAVE_1_1Core_1_1Data_1_1Data.html#a9662296ec537f32756a3db527d76f0d8", null ], + [ "__init__", "classSUAVE_1_1Core_1_1Data_1_1Data.html#a53cdb6dff3faeb47d13b68f989012733", null ], [ "__defaults__", "classSUAVE_1_1Core_1_1Data_1_1Data.html#aaf592cb5828e2e77556cb96137be6509", null ], [ "__delattr__", "classSUAVE_1_1Core_1_1Data_1_1Data.html#a2540d3d9f85dbedb84b4a677d559a6b3", null ], [ "__getattribute__", "classSUAVE_1_1Core_1_1Data_1_1Data.html#a3a9e65571555260186c6ae54cfeeea3c", null ], [ "__iter__", "classSUAVE_1_1Core_1_1Data_1_1Data.html#a98f17bb9cd886ccc1110c3c18d1c12d3", null ], - [ "__new__", "classSUAVE_1_1Core_1_1Data_1_1Data.html#a348c73ed2549fa7ffbe432e03bbffcd8", null ], + [ "__new__", "classSUAVE_1_1Core_1_1Data_1_1Data.html#a5bf781781988c1d31bd4c2deca7fdb08", null ], [ "__setattr__", "classSUAVE_1_1Core_1_1Data_1_1Data.html#aaceda3bf72e5beb15e59bf079edba2ce", null ], [ "__str__", "classSUAVE_1_1Core_1_1Data_1_1Data.html#a7847accf45dc18262cb7ceca42f74156", null ], [ "append", "classSUAVE_1_1Core_1_1Data_1_1Data.html#a69c46e0c3a6b4e0edc62596ab0af232b", null ], + [ "append_or_update", "classSUAVE_1_1Core_1_1Data_1_1Data.html#ad78beab7014e25a1b0d11b094a8df22b", null ], [ "dataname", "classSUAVE_1_1Core_1_1Data_1_1Data.html#ad25649de315ac95f3059ee0cad6294c6", null ], [ "deep_get", "classSUAVE_1_1Core_1_1Data_1_1Data.html#a3bbf5c11c2462b89b0a3df6dcaacf501", null ], [ "deep_set", "classSUAVE_1_1Core_1_1Data_1_1Data.html#a84ba0de5ac002c9fd4fc2953f5d452d4", null ], @@ -29,17 +31,16 @@ var group__Core = [ "values", "classSUAVE_1_1Core_1_1Data_1_1Data.html#a39740d68c8db37fceca74366dac74470", null ] ] ], [ "DataOrdered", "classSUAVE_1_1Core_1_1DataOrdered_1_1DataOrdered.html", [ - [ "__init__", "classSUAVE_1_1Core_1_1DataOrdered_1_1DataOrdered.html#a32224efd77bc24aea74d33999e4481f2", null ], + [ "__init__", "classSUAVE_1_1Core_1_1DataOrdered_1_1DataOrdered.html#a8e20af0ef213f277078958966e6fa7c5", null ], [ "__defaults__", "classSUAVE_1_1Core_1_1DataOrdered_1_1DataOrdered.html#a45c6bab8cd0a7b4aa27464d642cd7a5e", null ], [ "__delattr__", "classSUAVE_1_1Core_1_1DataOrdered_1_1DataOrdered.html#a44eb78bf6c80590d5cb5fc726c7f3184", null ], [ "__eq__", "classSUAVE_1_1Core_1_1DataOrdered_1_1DataOrdered.html#a645e8940eb0f28f92e629b125d79e0e1", null ], [ "__getitem__", "classSUAVE_1_1Core_1_1DataOrdered_1_1DataOrdered.html#a2a4d54c5646822649f356d80ed8d5001", null ], [ "__iter__", "classSUAVE_1_1Core_1_1DataOrdered_1_1DataOrdered.html#a727a22d1550136cdd217dc06981483db", null ], - [ "__iter__", "classSUAVE_1_1Core_1_1DataOrdered_1_1DataOrdered.html#a727a22d1550136cdd217dc06981483db", null ], + [ "__iter_basic__", "classSUAVE_1_1Core_1_1DataOrdered_1_1DataOrdered.html#aa500118acb942ad788ee2694f764104e", null ], [ "__len__", "classSUAVE_1_1Core_1_1DataOrdered_1_1DataOrdered.html#a1474cad96213dedce62249375071e51c", null ], - [ "__new__", "classSUAVE_1_1Core_1_1DataOrdered_1_1DataOrdered.html#ae7f8ca82a6526fdd42b49a4d4cd5bc0e", null ], + [ "__new__", "classSUAVE_1_1Core_1_1DataOrdered_1_1DataOrdered.html#add46625ec81f96d6b591547ea41b034a", null ], [ "__reduce__", "classSUAVE_1_1Core_1_1DataOrdered_1_1DataOrdered.html#ad384e66a99054e3a8f12c83b6a84c93d", null ], - [ "__repr__", "classSUAVE_1_1Core_1_1DataOrdered_1_1DataOrdered.html#a14e6ece7703001986b937d76716150c6", null ], [ "__setattr__", "classSUAVE_1_1Core_1_1DataOrdered_1_1DataOrdered.html#afc623fdd952face9c05101a11e71baed", null ], [ "__setitem__", "classSUAVE_1_1Core_1_1DataOrdered_1_1DataOrdered.html#ad4449f7906047b8638173be32929176d", null ], [ "__str__", "classSUAVE_1_1Core_1_1DataOrdered_1_1DataOrdered.html#abce8790556fa9730b7fdbd99f85a6416", null ], @@ -51,6 +52,7 @@ var group__Core = [ "get", "classSUAVE_1_1Core_1_1DataOrdered_1_1DataOrdered.html#a0fa21939a6607e52c6ec64f0df530da6", null ], [ "get_bases", "classSUAVE_1_1Core_1_1DataOrdered_1_1DataOrdered.html#a70121d322ad7d8f87ed8a493d9a91531", null ], [ "has_key", "classSUAVE_1_1Core_1_1DataOrdered_1_1DataOrdered.html#a0b2be2982aab545624276df6126050a0", null ], + [ "hasattr", "classSUAVE_1_1Core_1_1DataOrdered_1_1DataOrdered.html#a66994af42b97fb5d3c01bf1b301ddce2", null ], [ "items", "classSUAVE_1_1Core_1_1DataOrdered_1_1DataOrdered.html#a636e98cfed893d934ebfa3802beedfb7", null ], [ "iteritems", "classSUAVE_1_1Core_1_1DataOrdered_1_1DataOrdered.html#aa217f7f5308b213b95df7ee5d5cfeda1", null ], [ "iterkeys", "classSUAVE_1_1Core_1_1DataOrdered_1_1DataOrdered.html#a2b50d5ad6676e71674d02afbbdf08bed", null ], @@ -88,6 +90,7 @@ var group__Core = ] ], [ "__rdiv__", "group__Core.html#gaf0ce0cda1ac231d4d5699dd489ed2f06", null ], [ "__rmul__", "group__Core.html#ga8a2d75777a02c701f631195beb8e2405", null ], + [ "append_array", "group__Core.html#ga5141278f955291e7a5d7b9eaec2a47a0", null ], [ "atleast_2d", "group__Core.html#gaa0276e257945cceecb8f8f928926238e", null ], [ "atleast_2d_col", "group__Core.html#ga2127e06d0a8662bd68e102b81144abf3", null ], [ "atleast_2d_row", "group__Core.html#ga0aeae3001fe9329679917612c8b698c6", null ] diff --git a/doxygen/group__Input__Output-D3JS.html b/doxygen/group__Input__Output-D3JS.html index bb90abd7..2f1faa69 100644 --- a/doxygen/group__Input__Output-D3JS.html +++ b/doxygen/group__Input__Output-D3JS.html @@ -1,9 +1,9 @@ - + - + SUAVE: D3JS @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -221,7 +228,7 @@

Generated by - doxygen 1.8.14 + doxygen 1.8.15

diff --git a/doxygen/group__Input__Output-FreeMind.html b/doxygen/group__Input__Output-FreeMind.html index c1e81b76..a88aa2ac 100644 --- a/doxygen/group__Input__Output-FreeMind.html +++ b/doxygen/group__Input__Output-FreeMind.html @@ -1,9 +1,9 @@ - + - + SUAVE: FreeMind @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -208,7 +215,7 @@

Generated by - doxygen 1.8.14 + doxygen 1.8.15

diff --git a/doxygen/group__Input__Output-GMSH.html b/doxygen/group__Input__Output-GMSH.html index 891adb48..921e1d09 100644 --- a/doxygen/group__Input__Output-GMSH.html +++ b/doxygen/group__Input__Output-GMSH.html @@ -1,9 +1,9 @@ - + - + SUAVE: GMSH @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -228,7 +235,7 @@

Generated by - doxygen 1.8.14 + doxygen 1.8.15

diff --git a/doxygen/group__Input__Output-OpenVSP.html b/doxygen/group__Input__Output-OpenVSP.html index 8a7d61a8..16021427 100644 --- a/doxygen/group__Input__Output-OpenVSP.html +++ b/doxygen/group__Input__Output-OpenVSP.html @@ -1,9 +1,9 @@ - + - + SUAVE: OpenVSP @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -103,10 +110,52 @@ - - - - + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + @@ -215,110 +264,155 @@

-

◆ get_vsp_areas()

+ +

◆ apply_properties()

Functions

def SUAVE.Input_Output.OpenVSP.get_vsp_areas.get_vsp_areas (tag)
 
def SUAVE.Input_Output.OpenVSP.vsp_write.write (vehicle, tag)
 
def SUAVE.Input_Output.OpenVSP.get_fuel_tank_properties.get_fuel_tank_properties (vehicle, tag, fuel_tank_set_index=3, slices_for_calculation=100)
 
def SUAVE.Input_Output.OpenVSP.get_fuel_tank_properties.apply_properties (vehicle, fuel_tanks)
 
def SUAVE.Input_Output.OpenVSP.get_fuel_tank_properties.get_fuel_tanks (vehicle)
 
def SUAVE.Input_Output.OpenVSP.get_vsp_measurements.get_vsp_measurements (filename='Unnamed_CompGeom.csv', measurement_type='wetted_area')
 
def SUAVE.Input_Output.OpenVSP.vsp_fuselage.read_vsp_fuselage (fuselage_id, fux_idx, sym_flag, units_type='SI', fineness=True, use_scaling=True)
 
def SUAVE.Input_Output.OpenVSP.vsp_fuselage.write_vsp_fuselage (fuselage, area_tags, main_wing, fuel_tank_set_ind, OML_set_ind)
 
def SUAVE.Input_Output.OpenVSP.vsp_fuselage.find_fuse_u_coordinate (x_target, fuse_id, fuel_tank_tag)
 
def SUAVE.Input_Output.OpenVSP.vsp_fuselage.write_fuselage_conformal_fuel_tank (fuse_id, fuel_tank, fuel_tank_set_ind)
 
def SUAVE.Input_Output.OpenVSP.vsp_nacelle.write_vsp_nacelle (nacelle, OML_set_ind)
 
def SUAVE.Input_Output.OpenVSP.vsp_nacelle.read_vsp_nacelle (nacelle_id, vsp_nacelle_type, units_type='SI')
 
def SUAVE.Input_Output.OpenVSP.vsp_propeller.read_vsp_propeller (prop_id, units_type='SI', write_airfoil_file=True)
 
def SUAVE.Input_Output.OpenVSP.vsp_propeller.write_vsp_propeller_bem (vsp_bem_filename, propeller)
 
def SUAVE.Input_Output.OpenVSP.vsp_propeller.make_header_text (vsp_bem, prop)
 
def SUAVE.Input_Output.OpenVSP.vsp_propeller.make_section_text (vsp_bem, prop)
 
def SUAVE.Input_Output.OpenVSP.vsp_propeller.make_airfoil_text (vsp_bem, prop)
 
def SUAVE.Input_Output.OpenVSP.vsp_read.vsp_read (tag, units_type='SI', specified_network=None, use_scaling=True)
 
def SUAVE.Input_Output.OpenVSP.vsp_wing.read_vsp_wing (wing_id, units_type='SI', write_airfoil_file=True, use_scaling=True)
 
def SUAVE.Input_Output.OpenVSP.vsp_wing.write_vsp_wing (vehicle, wing, area_tags, fuel_tank_set_ind, OML_set_ind)
 
def SUAVE.Input_Output.OpenVSP.vsp_wing.write_vsp_control_surface (wing_id, ctrl_surf, n_segments)
 
def SUAVE.Input_Output.OpenVSP.vsp_wing.write_wing_conformal_fuel_tank (vehicle, wing, wing_id, fuel_tank, fuel_tank_set_ind)
 
def SUAVE.Input_Output.OpenVSP.vsp_wing.get_vsp_trim_from_SUAVE_trim (seg_span_percents, vsp_segment_breaks, trim)
 
def SUAVE.Input_Output.OpenVSP.vsp_wing.convert_sweep (sweep, sweep_loc, new_sweep_loc, AR, taper)
 
def SUAVE.Input_Output.OpenVSP.vsp_write.write (vehicle, tag, fuel_tank_set_ind=3, verbose=True, write_file=True, OML_set_ind=4, write_igs=False)
 
def SUAVE.Input_Output.OpenVSP.write_vsp_mesh.write_vsp_mesh (geometry, tag, half_mesh_flag, growth_ratio, growth_limiting_flag)
 
def SUAVE.Input_Output.OpenVSP.write_vsp_mesh.set_sources (geometry)
- + - + + + + + + + + + + +
def SUAVE.Input_Output.OpenVSP.get_vsp_areas.get_vsp_areas def SUAVE.Input_Output.OpenVSP.get_fuel_tank_properties.apply_properties (  tag)vehicle,
 fuel_tanks 
)
-
This calls OpenVSP to compute the wetted areas of a previously written vehicle.
+
Apply fuel tank properties from OpenVSP to the SUAVE vehicle.
 
 Assumptions:
-Vehicle must be open in OpenVSP (via recently used vsp_write)
-All components have different tags. Repeated tags are added together under the
-assumption that this represents multiple engines or similar. Areas computed from
-repeated tags in this way may need to be divided by the number of entities later 
-before assignment. This is because some analyses may multiply an assigned area
-by number of engines, for example.
+Fuel tanks exists in the fuselage and wings only
 
 Source:
 N/A
 
 Inputs:
-None
+vehicle.fuselages.*.Fuel_Tanks.*.tag     [-]
+vehicle.wings.*.Fuel_Tanks.*.tag         [-]
+fuel_tanks.
+  tag                                    [-]
+  center_of_gravity                      [m]
+  fuel_mass_when_full                    [kg]
+  volume                                 [m^3]
+  
 
-Outputs:
-wetted_areas   [m^2] - Dictionary with wetted areas for each component, with component tags as the keys.
+Outputs:    
+vehicle.fuselages.*.Fuel_Tanks.*.mass_properties.
+  center_of_gravity                      [m]
+  fuel_mass_when_full                    [kg]
+  fuel_volume_when_full                  [m^3]
+vehicle.wings.*.Fuel_Tanks.*.mass_properties.
+  center_of_gravity                      [m]
+  fuel_mass_when_full                    [kg]
+  fuel_volume_when_full                  [m^3]
+  
 
 Properties Used:
 N/A
 
- -

◆ set_sources()

+ +

◆ convert_sweep()

- + - + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Input_Output.OpenVSP.write_vsp_mesh.set_sources def SUAVE.Input_Output.OpenVSP.vsp_wing.convert_sweep (  geometry)sweep,
 sweep_loc,
 new_sweep_loc,
 AR,
 taper 
)
-
This sets meshing sources in a way similar to the OpenVSP default. Some source values can
-also be optionally specified as below.
+
This converts arbitrary sweep into a desired sweep given
+wing geometry.
 
 Assumptions:
 None
 
 Source:
-https://github.com/OpenVSP/OpenVSP (with some modifications)
+N/A
 
 Inputs:
-geometry.
-  wings.*.                              (passed to add_segment_sources())
-    tag                                 <string>
-    Segments.*.percent_span_location    [-] (.1 is 10%)
-    Segments.*.root_chord_percent       [-] (.1 is 10%)
-    chords.root                         [m]
-    chords.tip                          [m]
-    vsp_mesh                            (optional) - This holds settings that are used in add_segment_sources
-  fuselages.*.
-    tag                                 <string>
-    vsp_mesh.                           (optional)
-      length                            [m]
-      radius                            [m]
-    lengths.total                       (only used if vsp_mesh is not defined for the fuselage)
+sweep               [degrees]
+sweep_loc           [unitless]
+new_sweep_loc       [unitless]
+AR                  [unitless]
+taper               [unitless]
 
 Outputs:
-<tag>.stl                               
+quarter chord sweep
 
 Properties Used:
 N/A
 
- -

◆ write()

+ +

◆ find_fuse_u_coordinate()

- + - + + + + + + + - + @@ -327,84 +421,38 @@

-
This writes a SUAVE vehicle to OpenVSP format. It will take wing segments into account
-if they are specified in the vehicle setup file.
+
Determines the u coordinate of an OpenVSP fuselage that matches an x coordinate
 
 Assumptions:
-Vehicle is composed of conventional shape fuselages, wings, and propulsors. Any propulsor
-that should be created in tagged as 'turbofan'.
+Fuselage is aligned with the x axis
 
 Source:
 N/A
 
 Inputs:
-wings.*.    (* is all keys)
-  origin                                  [m] in all three dimensions
-  spans.projected                         [m]
-  chords.root                             [m]
-  chords.tip                              [m]
-  sweeps.quarter_chord                    [radians]
-  twists.root                             [radians]
-  twists.tip                              [radians]
-  thickness_to_chord                      [-]
-  dihedral                                [radians]
-  tag                                     <string>
-  Segments.*. (optional)
-    twist                                 [radians]
-    percent_span_location                 [-]  .1 is 10%
-    root_chord_percent                    [-]  .1 is 10%
-    dihedral_outboard                     [radians]
-    sweeps.quarter_chord                  [radians]
-    thickness_to_chord                    [-]
-propulsors.turbofan. (optional)
-  number_of_engines                       [-]
-  engine_length                           [m]
-  nacelle_diameter                        [m]
-  origin                                  [m] in all three dimension, should have as many origins as engines
-  OpenVSP_simple (optional)               <boolean> if False (default) create a flow through nacelle, if True creates a roughly biparabolic shape
-fuselages.fuselage (optional)
-  width                                   [m]
-  lengths.total                           [m]
-  heights.
-    maximum                               [m]
-    at_quarter_length                     [m]
-    at_wing_root_quarter_chord            [m]
-    at_three_quarters_length              [m]
-  effective_diameter                      [m]
-  fineness.nose                           [-] ratio of nose section length to fuselage width
-  fineness.tail                           [-] ratio of tail section length to fuselage width
-  tag                                     <string>
-  OpenVSP_values.  (optional)
-    nose.top.angle                        [degrees]
-    nose.top.strength                     [-] this determines how much the specified angle influences that shape
-    nose.side.angle                       [degrees]
-    nose.side.strength                    [-]
-    nose.TB_Sym                           <boolean> determines if top angle is mirrored on bottom
-    nose.z_pos                            [-] z position of the nose as a percentage of fuselage length (.1 is 10%)
-    tail.top.angle                        [degrees]
-    tail.top.strength                     [-]
-    tail.z_pos (optional, 0.02 default)   [-] z position of the tail as a percentage of fuselage length (.1 is 10%)
-
+x_target      [m]
+fuse_id       <str>
+fuel_tank_tag <str>
 
 Outputs:
-<tag>.vsp3           This is the OpenVSP representation of the aircraft
+u_current     [-] u coordinate for the requests x position
 
 Properties Used:
 N/A
 
-
-

◆ write_vsp_mesh()

+ +

◆ get_fuel_tank_properties()

def SUAVE.Input_Output.OpenVSP.vsp_write.write def SUAVE.Input_Output.OpenVSP.vsp_fuselage.find_fuse_u_coordinate (  vehicle, x_target,
 fuse_id,
 tag fuel_tank_tag 
- + - + @@ -416,19 +464,105 @@

- + - + + + + + + + +
def SUAVE.Input_Output.OpenVSP.write_vsp_mesh.write_vsp_mesh def SUAVE.Input_Output.OpenVSP.get_fuel_tank_properties.get_fuel_tank_properties (  geometry, vehicle,
 half_mesh_flag, fuel_tank_set_index = 3,
 growth_ratio, slices_for_calculation = 100 
)
+
+
+ +

◆ get_fuel_tanks()

+ +
+
+ + + + + + + + +
def SUAVE.Input_Output.OpenVSP.get_fuel_tank_properties.get_fuel_tanks ( vehicle)
+
+
Creates a data structure with fuel tanks based on 
+fuel tanks present in the vehicle
+
+Assumptions:
+Fuel tanks exists in the fuselage and wings only
+
+Source:
+N/A
+
+Inputs:
+vehicle.fuselages.*.Fuel_Tanks.*.tag     [-]
+vehicle.wings.*.Fuel_Tanks.*.tag         [-]
+
+Outputs:    
+fuel_tanks.tag                           [-]
+
+Properties Used:
+N/A
+
+
+
+ +

◆ get_vsp_measurements()

+ +
+
+
Compute OpenVSP span trim coordinates based on SUAVE coordinates
+
+Assumptions:
+Wing does not have end caps
+
 Source:
 N/A
 
 Inputs:
-geometry.                                 - Also passed to set_sources
-  wings.main_wing.chords.mean_aerodynamic [m]
-half_mesh_flag                            <boolean>  determines if a symmetry plane is created
-growth_ratio                              [-]        growth ratio for the mesh
-growth_limiting_flag                      <boolean>  determines if 3D growth limiting is used
+seg_span_percents   [-] range of 0 to 1
+vsp_segment_breaks  [-] range of 0 to 1
+trim                [-] range of 0 to 1 (SUAVE value)
 
 Outputs:
-<tag>.stl                               
+trim                [-] OpenVSP trim value
+
+Properties Used:
+N/A
+
+
+
+ +

◆ make_airfoil_text()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Input_Output.OpenVSP.vsp_propeller.make_airfoil_text ( vsp_bem,
 prop 
)
+
+
This function writes the airfoil geometry into the vsp file
+Assumptions:
+    None
+
+Source:
+    None
+Inputs:
+    vsp_bem - OpenVSP .bem file
+    prop    - SUAVE propeller data structure
+
+Outputs:
+    NA
+Properties Used:
+    N/A
+
+
+
+ +

◆ make_header_text()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Input_Output.OpenVSP.vsp_propeller.make_header_text ( vsp_bem,
 prop 
)
+
+
This function writes the header of the OpenVSP .bem file
+Assumptions:
+    None
+
+Source:
+    None
+Inputs:
+    vsp_bem - OpenVSP .bem file
+    prop    - SUAVE propeller data structure
+
+Outputs:
+    NA
+Properties Used:
+    N/A
+
+
+
+ +

◆ make_section_text()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Input_Output.OpenVSP.vsp_propeller.make_section_text ( vsp_bem,
 prop 
)
+
+
This function writes the sectional information of the propeller
+Assumptions:
+    None
+
+Source:
+    None
+Inputs:
+    vsp_bem - OpenVSP .bem file
+    prop    - SUAVE propeller data structure
+
+Outputs:
+    NA
+Properties Used:
+    N/A
+
+
+
+ +

◆ read_vsp_fuselage()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Input_Output.OpenVSP.vsp_fuselage.read_vsp_fuselage ( fuselage_id,
 fux_idx,
 sym_flag,
 units_type = 'SI',
 fineness = True,
 use_scaling = True 
)
+
+
This reads an OpenVSP fuselage geometry and writes it to a SUAVE fuselage format.
+
+Assumptions:
+1. OpenVSP fuselage is "conventionally shaped" (generally narrow at nose and tail, wider in center). 
+2. Fuselage is designed in VSP as it appears in real life. That is, the VSP model does not rely on
+   superficial elements such as canopies, stacks, or additional fuselages to cover up internal lofting oddities.
+3. This program will NOT account for multiple geometries comprising the fuselage. For example: a wingbox mounted beneath
+   is a separate geometry and will NOT be processed.
+4. Fuselage origin is located at nose. VSP file origin can be located anywhere, preferably at the forward tip
+   of the vehicle or in front (to make all X-coordinates of vehicle positive).
+5. Written for OpenVSP 3.21.1
+
+Source:
+N/A
+
+Inputs:
+0. Pre-loaded VSP vehicle in memory, via vsp_read.
+1. VSP 10-digit geom ID for fuselage.
+2. Units_type set to 'SI' (default) or 'Imperial'.
+3. Boolean for whether or not to compute fuselage finenesses (default = True).
+4. Boolean for whether or not to use the scaling from OpenVSP (default = True).
+
+Outputs:
+
+Writes SUAVE fuselage, with these geometries:           (all defaults are SI, but user may specify Imperial)
+
+    Fuselages.Fuselage.         
+        origin                                  [m] in all three dimensions
+        width                                   [m]
+        lengths.
+          total                                 [m]
+          nose                                  [m]
+          tail                                  [m]
+        heights.
+          maximum                               [m]
+          at_quarter_length                     [m]
+          at_three_quarters_length              [m]
+        effective_diameter                      [m]
+        fineness.nose                           [-] ratio of nose section length to fuselage effective diameter
+        fineness.tail                           [-] ratio of tail section length to fuselage effective diameter
+        areas.wetted                            [m^2]
+        tag                                     <string>
+        segment[].   (segments are in ordered container and callable by number)
+          vsp.shape                               [point,circle,round_rect,general_fuse,fuse_file]
+          vsp.xsec_id                             <10 digit string>
+          percent_x_location
+          percent_z_location
+          height
+          width
+          length
+          effective_diameter
+          tag
+        vsp.xsec_num                              <integer of fuselage segment quantity>
+        vsp.xsec_surf_id                          <10 digit string>
+
+Properties Used:
+N/A
+
+
+
+ +

◆ read_vsp_nacelle()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Input_Output.OpenVSP.vsp_nacelle.read_vsp_nacelle ( nacelle_id,
 vsp_nacelle_type,
 units_type = 'SI' 
)
+
+
This reads an OpenVSP stack geometry or body of revolution and writes it to a SUAVE nacelle format.
+If an airfoil is defined in body-of-revolution, its coordinates are not read in due to absence of
+API functions in VSP.
+
+Assumptions: 
+
+Source:
+N/A
+
+Inputs:
+0. Pre-loaded VSP vehicle in memory, via vsp_read.
+1. VSP 10-digit geom ID for nacelle.
+2. Units_type set to 'SI' (default) or 'Imperial'. 
+
+Outputs:
+Writes SUAVE nacelle, with these geometries:           (all defaults are SI, but user may specify Imperial)
+
+    Nacelles.Nacelle.   
+        origin                  [m] in all three dimensions
+        width                   [m]
+        lengths                 [m]
+        heights                 [m]
+        tag                     <string>
+        segment[].   (segments are in ordered container and callable by number) 
+          percent_x_location    [unitless]
+          percent_z_location    [unitless]
+          height                [m]
+          width                 [m]
+
+Properties Used:
+N/A
+
+
+
+ +

◆ read_vsp_propeller()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Input_Output.OpenVSP.vsp_propeller.read_vsp_propeller ( prop_id,
 units_type = 'SI',
 write_airfoil_file = True 
)
+
+
This reads an OpenVSP propeller geometry and writes it into a SUAVE propeller format.
+
+Assumptions:
+1. Written for OpenVSP 3.24.0
+
+Source:
+N/A
+
+Inputs:
+1. VSP 10-digit geom ID for prop.
+2. units_type set to 'SI' (default) or 'Imperial'.
+3. write_airfoil_file set to True (default) or False
+4. number_of_radial_stations is the radial discretization used to extract the propeller design from OpenVSP
+
+Outputs:
+Writes SUAVE propeller/rotor object, with these geometries, from VSP:
+    prop.
+        origin                                  [m] in all three dimensions
+        orientation             [deg] in all three dimensions
+        number_of_blades            [-]
+        tip_radius              [m]
+        hub_radius              [m]
+        twist_distribution          [deg]
+        chord_distribution          [m]
+        radius_distribution         [m]
+        sweep_distribution          [deg]
+        mid_chord_alignment         [m]
+        max_thickness_distribution      [m]
+        thickness_to_chord          [-]
+        blade_solidity              [-]
+        rotation                    [-]
+        thickness_to_chord                      [-]
+            beta34                                  [radians]
+            pre_cone                                [radians]
+            rake                                    [radians]
+            skew                                    [radians]
+            axial                                   [radians]
+            tangential                              [radians]
+        dihedral                                [radians]
+        symmetric                               <boolean>
+        tag                                     <string>
+        Segments.
+          tag                                   <string>
+          twist                                 [radians]
+          percent_span_location                 [-]  .1 is 10%
+          root_chord_percent                    [-]  .1 is 10%
+          dihedral_outboard                     [radians]
+          sweeps.quarter_chord                  [radians]
+          thickness_to_chord                    [-]
+          airfoil                               <NACA 4-series, 6 series, or airfoil file>
+
+Properties Used:
+N/A
+
+
+
+ +

◆ read_vsp_wing()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Input_Output.OpenVSP.vsp_wing.read_vsp_wing ( wing_id,
 units_type = 'SI',
 write_airfoil_file = True,
 use_scaling = True 
)
+
+
This reads an OpenVSP wing vehicle geometry and writes it into a SUAVE wing format.
+
+Assumptions:
+1. OpenVSP wing is divided into segments ("XSecs" in VSP).
+2. Written for OpenVSP 3.21.1
+
+Source:
+N/A
+
+Inputs:
+1. VSP 10-digit geom ID for wing.
+2. units_type set to 'SI' (default) or 'Imperial'.
+3. Boolean for whether or not to write an airfoil file(default = True).
+4. Boolean for whether or not to use the scaling from OpenVSP (default = True).
+
+Outputs:
+Writes SUAVE wing object, with these geometries, from VSP:
+    Wings.Wing.    (* is all keys)
+        origin                                  [m] in all three dimensions
+        spans.projected                         [m]
+        chords.root                             [m]
+        chords.tip                              [m]
+        aspect_ratio                            [-]
+        sweeps.quarter_chord                    [radians]
+        twists.root                             [radians]
+        twists.tip                              [radians]
+        thickness_to_chord                      [-]
+        dihedral                                [radians]
+        symmetric                               <boolean>
+        tag                                     <string>
+        areas.reference                         [m^2]
+        areas.wetted                            [m^2]
+        Segments.
+          tag                                   <string>
+          twist                                 [radians]
+          percent_span_location                 [-]  .1 is 10%
+          root_chord_percent                    [-]  .1 is 10%
+          dihedral_outboard                     [radians]
+          sweeps.quarter_chord                  [radians]
+          thickness_to_chord                    [-]
+          airfoil                               <NACA 4-series, 6 series, or airfoil file>
+
+Properties Used:
+N/A
+
+
+
+ +

◆ set_sources()

+ +
+
+ + + + + + + + +
def SUAVE.Input_Output.OpenVSP.write_vsp_mesh.set_sources ( geometry)
+
+
This sets meshing sources in a way similar to the OpenVSP default. Some source values can
+also be optionally specified as below.
+
+Assumptions:
+None
+
+Source:
+https://github.com/OpenVSP/OpenVSP (with some modifications)
+
+Inputs:
+geometry.
+  wings.*.                              (passed to add_segment_sources())
+    tag                                 <string>
+    Segments.*.percent_span_location    [-] (.1 is 10%)
+    Segments.*.root_chord_percent       [-] (.1 is 10%)
+    chords.root                         [m]
+    chords.tip                          [m]
+    vsp_mesh                            (optional) - This holds settings that are used in add_segment_sources
+  fuselages.*.
+    tag                                 <string>
+    vsp_mesh.                           (optional)
+      length                            [m]
+      radius                            [m]
+    lengths.total                       (only used if vsp_mesh is not defined for the fuselage)
+
+Outputs:
+<tag>.stl                               
+
+Properties Used:
+N/A
+
+
+
+ +

◆ vsp_read()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Input_Output.OpenVSP.vsp_read.vsp_read ( tag,
 units_type = 'SI',
 specified_network = None,
 use_scaling = True 
)
+
+
This reads an OpenVSP vehicle geometry and writes it into a SUAVE vehicle format.
+Includes wings, fuselages, and propellers.
+
+Assumptions:
+1. OpenVSP vehicle is composed of conventionally shaped fuselages, wings, and propellers. 
+1a. OpenVSP fuselage: generally narrow at nose and tail, wider in center). 
+1b. Fuselage is designed in VSP as it appears in real life. That is, the VSP model does not rely on
+   superficial elements such as canopies, stacks, or additional fuselages to cover up internal lofting oddities.
+1c. This program will NOT account for multiple geometries comprising the fuselage. For example: a wingbox mounted beneath
+   is a separate geometry and will NOT be processed.
+2. Fuselage origin is located at nose. VSP file origin can be located anywhere, preferably at the forward tip
+   of the vehicle or in front (to make all X-coordinates of vehicle positive).
+3. Written for OpenVSP 3.21.1
+
+Source:
+N/A
+
+Inputs:
+1. A tag for an XML file in format .vsp3.
+2. Units_type set to 'SI' (default) or 'Imperial'
+3. User-specified network
+4. Boolean for whether or not to use the scaling from OpenVSP (default = True).
+
+Outputs:
+Writes SUAVE vehicle with these geometries from VSP:    (All values default to SI. Any other 2nd argument outputs Imperial.)
+    Wings.Wing.    (* is all keys)
+        origin                                  [m] in all three dimensions
+        spans.projected                         [m]
+        chords.root                             [m]
+        chords.tip                              [m]
+        aspect_ratio                            [-]
+        sweeps.quarter_chord                    [radians]
+        twists.root                             [radians]
+        twists.tip                              [radians]
+        thickness_to_chord                      [-]
+        dihedral                                [radians]
+        symmetric                               <boolean>
+        tag                                     <string>
+        areas.reference                         [m^2]
+        areas.wetted                            [m^2]
+        Segments.
+          tag                                   <string>
+          twist                                 [radians]
+          percent_span_location                 [-]  .1 is 10%
+          root_chord_percent                    [-]  .1 is 10%
+          dihedral_outboard                     [radians]
+          sweeps.quarter_chord                  [radians]
+          thickness_to_chord                    [-]
+          airfoil                               <NACA 4-series, 6 series, or airfoil file>
+
+    Fuselages.Fuselage.         
+        origin                                  [m] in all three dimensions
+        width                                   [m]
+        lengths.
+          total                                 [m]
+          nose                                  [m]
+          tail                                  [m]
+        heights.
+          maximum                               [m]
+          at_quarter_length                     [m]
+          at_three_quarters_length              [m]
+        effective_diameter                      [m]
+        fineness.nose                           [-] ratio of nose section length to fuselage effective diameter
+        fineness.tail                           [-] ratio of tail section length to fuselage effective diameter
+        areas.wetted                            [m^2]
+        tag                                     <string>
+        segment[].   (segments are in ordered container and callable by number)
+          vsp.shape                               [point,circle,round_rect,general_fuse,fuse_file]
+          vsp.xsec_id                             <10 digit string>
+          percent_x_location
+          percent_z_location
+          height
+          width
+          length
+          effective_diameter
+          tag
+        vsp.xsec_num                              <integer of fuselage segment quantity>
+        vsp.xsec_surf_id                          <10 digit string>
+
+    Propellers.Propeller.
+        location[X,Y,Z]                            [radians]
+        rotation[X,Y,Z]                            [radians]
+        tip_radius                                 [m]
+            hub_radius                                 [m] 
+
+Properties Used:
+N/A
+
+
+
+ +

◆ write()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Input_Output.OpenVSP.vsp_write.write ( vehicle,
 tag,
 fuel_tank_set_ind = 3,
 verbose = True,
 write_file = True,
 OML_set_ind = 4,
 write_igs = False 
)
+
+
This writes a SUAVE vehicle to OpenVSP format. It will take wing segments into account
+if they are specified in the vehicle setup file.
+
+Assumptions:
+Vehicle is composed of conventional shape fuselages, wings, and networks. Any network
+that should be created is tagged as 'turbofan'.
+
+Source:
+N/A
+
+Inputs:
+vehicle.
+  tag                                       [-]
+  wings.*.    (* is all keys)
+    origin                                  [m] in all three dimensions
+    spans.projected                         [m]
+    chords.root                             [m]
+    chords.tip                              [m]
+    sweeps.quarter_chord                    [radians]
+    twists.root                             [radians]
+    twists.tip                              [radians]
+    thickness_to_chord                      [-]
+    dihedral                                [radians]
+    tag                                     <string>
+    Segments.*. (optional)
+      twist                                 [radians]
+      percent_span_location                 [-]  .1 is 10%
+      root_chord_percent                    [-]  .1 is 10%
+      dihedral_outboard                     [radians]
+      sweeps.quarter_chord                  [radians]
+      thickness_to_chord                    [-]
+  networks.turbofan. (optional)
+    number_of_engines                       [-]
+    nacelle_diameter                        [m]
+    origin                                  [m] in all three dimension, should have as many origins as engines
+    OpenVSP_simple (optional)               <boolean> if False (default) create a flow through nacelle, if True creates a roughly biparabolic shape
+  fuselages.fuselage (optional)
+    width                                   [m]
+    lengths.total                           [m]
+    heights.
+      maximum                               [m]
+      at_quarter_length                     [m]
+      at_wing_root_quarter_chord            [m]
+      at_three_quarters_length              [m]
+    effective_diameter                      [m]
+    fineness.nose                           [-] ratio of nose section length to fuselage width
+    fineness.tail                           [-] ratio of tail section length to fuselage width
+    tag                                     <string>
+    OpenVSP_values.  (optional)
+      nose.top.angle                        [degrees]
+      nose.top.strength                     [-] this determines how much the specified angle influences that shape
+      nose.side.angle                       [degrees]
+      nose.side.strength                    [-]
+      nose.TB_Sym                           <boolean> determines if top angle is mirrored on bottom
+      nose.z_pos                            [-] z position of the nose as a percentage of fuselage length (.1 is 10%)
+      tail.top.angle                        [degrees]
+      tail.top.strength                     [-]
+      tail.z_pos (optional, 0.02 default)   [-] z position of the tail as a percentage of fuselage length (.1 is 10%)
+fuel_tank_set_index                         <int> OpenVSP object set containing the fuel tanks    
+
+Outputs:
+<tag>.vsp3           This is the OpenVSP representation of the aircraft
+
+Properties Used:
+N/A
+
+
+
+ +

◆ write_fuselage_conformal_fuel_tank()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Input_Output.OpenVSP.vsp_fuselage.write_fuselage_conformal_fuel_tank ( fuse_id,
 fuel_tank,
 fuel_tank_set_ind 
)
+
+
This writes a conformal fuel tank in a fuselage.
+
+Assumptions:
+Fuselage is aligned with the x axis
+
+Source:
+N/A
+
+Inputs:
+fuse_id                                     <str>
+fuel_tank.
+  inward_offset                             [m]
+  start_length_percent                      [-] .1 is 10%
+  end_length_percent                        [-]
+  fuel_type.density                         [kg/m^3]
+fuel_tank_set_ind                           <int>
+
+Outputs:
+Operates on the active OpenVSP model, no direct output
+
+Properties Used:
+N/A
+
+
+
+ +

◆ write_vsp_control_surface()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Input_Output.OpenVSP.vsp_wing.write_vsp_control_surface ( wing_id,
 ctrl_surf,
 n_segments 
)
+
+
This writes a control surface in a wing.
+
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+wind_id              <str>
+ctrl_surf            [-]
+n_segments           int, number of wing segments
+
+Outputs:
+Operates on the active OpenVSP model, no direct output
+
+Properties Used:
+N/A
+
+
+
+ +

◆ write_vsp_fuselage()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Input_Output.OpenVSP.vsp_fuselage.write_vsp_fuselage ( fuselage,
 area_tags,
 main_wing,
 fuel_tank_set_ind,
 OML_set_ind 
)
+
+
This writes a fuselage into OpenVSP format.
+
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+fuselage
+  width                                   [m]
+  lengths.total                           [m]
+  heights.
+    maximum                               [m]
+    at_quarter_length                     [m]
+    at_wing_root_quarter_chord            [m]
+    at_three_quarters_length              [m]
+  effective_diameter                      [m]
+  fineness.nose                           [-] ratio of nose section length to fuselage width
+  fineness.tail                           [-] ratio of tail section length to fuselage width
+  tag                                     <string>
+  OpenVSP_values.  (optional)
+    nose.top.angle                        [degrees]
+    nose.top.strength                     [-] this determines how much the specified angle influences that shape
+    nose.side.angle                       [degrees]
+    nose.side.strength                    [-]
+    nose.TB_Sym                           <boolean> determines if top angle is mirrored on bottom
+    nose.z_pos                            [-] z position of the nose as a percentage of fuselage length (.1 is 10%)
+    tail.top.angle                        [degrees]
+    tail.top.strength                     [-]
+    tail.z_pos (optional, 0.02 default)   [-] z position of the tail as a percentage of fuselage length (.1 is 10%)
+  Segments. (optional)
+    width                                 [m]
+    height                                [m]
+    percent_x_location                    [-] .1 is 10% length
+    percent_z_location                    [-] .1 is 10% length
+area_tags                                 <dict> used to keep track of all tags needed in wetted area computation           
+main_wing.origin                          [m]
+main_wing.chords.root                     [m]
+fuel_tank_set_index                       <int> OpenVSP object set containing the fuel tanks    
+
+Outputs:
+Operates on the active OpenVSP model, no direct output
+
+Properties Used:
+N/A
+
+
+
+ +

◆ write_vsp_mesh()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Input_Output.OpenVSP.write_vsp_mesh.write_vsp_mesh ( geometry,
 tag,
 half_mesh_flag,
 growth_ratio,
 growth_limiting_flag 
)
+
+
This create an .stl surface mesh based on a vehicle stored in a .vsp3 file.
+
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+geometry.                                 - Also passed to set_sources
+  wings.main_wing.chords.mean_aerodynamic [m]
+half_mesh_flag                            <boolean>  determines if a symmetry plane is created
+growth_ratio                              [-]        growth ratio for the mesh
+growth_limiting_flag                      <boolean>  determines if 3D growth limiting is used
+
+Outputs:
+<tag>.stl                               
+
+Properties Used:
+N/A
+
+
+
+ +

◆ write_vsp_nacelle()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Input_Output.OpenVSP.vsp_nacelle.write_vsp_nacelle ( nacelle,
 OML_set_ind 
)
+
+
This converts nacelles into OpenVSP format.
+
+Assumptions: 
+1. If nacelle segments are defined, geometry written to OpenVSP is of type "StackGeom". 
+   1.a  This type of nacelle can be either set as flow through or not flow through.
+   1.b  Segments are defined in a similar manner to fuselage segments. See geometric 
+        documentation in SUAVE-Components-Nacelles-Nacelle
+
+2. If nacelle segments are not defined, geometry written to OpenVSP is of type "BodyofRevolution".
+   2.a This type of nacelle can be either set as flow through or not flow through.
+   2.b BodyofRevolution can be either be a 4 digit airfoil (type string) or super ellipse (default)
+Source:
+N/A
+Inputs: 
+  nacelle.
+  origin                              [m] in all three dimension, should have as many origins as engines 
+  length                              [m]
+  diameter                            [m]
+  flow_through                        <boolean> if True create a flow through nacelle, if False create a cylinder
+  segment(optional).
+     width                            [m]
+     height                           [m]
+     lenght                           [m]
+     percent_x_location               [m]     
+     percent_y_location               [m]        
+     percent_z_location               [m] 
+   
+Outputs:
+Operates on the active OpenVSP model, no direct output
+Properties Used:
+N/A
+
+
+
+ +

◆ write_vsp_propeller_bem()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Input_Output.OpenVSP.vsp_propeller.write_vsp_propeller_bem ( vsp_bem_filename,
 propeller 
)
+
+
This functions writes a .bem file for OpenVSP
+Assumptions:
+    None
+
+Source:
+    None
+Inputs:
+    OpenVSP .bem filename
+    SUAVE Propeller Data Structure
+Outputs:
+    OpenVSP .bem file
+Properties Used:
+    N/A
+
+
+
+ +

◆ write_vsp_wing()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Input_Output.OpenVSP.vsp_wing.write_vsp_wing ( vehicle,
 wing,
 area_tags,
 fuel_tank_set_ind,
 OML_set_ind 
)
+
+
This write a given wing into OpenVSP format
+
+Assumptions:
+If wing segments are defined, they must cover the full span.
+(may work in some other cases, but functionality will not be maintained)
+
+Source:
+N/A
+
+Inputs:
+vehicle                                   [-] vehicle data structure
+wing.
+  origin                                  [m] in all three dimensions
+  spans.projected                         [m]
+  chords.root                             [m]
+  chords.tip                              [m]
+  sweeps.quarter_chord                    [radians]
+  twists.root                             [radians]
+  twists.tip                              [radians]
+  thickness_to_chord                      [-]
+  dihedral                                [radians]
+  tag                                     <string>
+  Segments.*. (optional)
+    twist                                 [radians]
+    percent_span_location                 [-]  .1 is 10%
+    root_chord_percent                    [-]  .1 is 10%
+    dihedral_outboard                     [radians]
+    sweeps.quarter_chord                  [radians]
+    thickness_to_chord                    [-]
+area_tags                                 <dict> used to keep track of all tags needed in wetted area computation
+fuel_tank_set_index                       <int> OpenVSP object set containing the fuel tanks
+
+Outputs:
+area_tags                                 <dict> used to keep track of all tags needed in wetted area computation
+wing_id                                   <str>  OpenVSP ID for given wing
+
+Properties Used:
+N/A
+
+
+
+ +

◆ write_wing_conformal_fuel_tank()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Input_Output.OpenVSP.vsp_wing.write_wing_conformal_fuel_tank ( vehicle,
 wing,
 wing_id,
 fuel_tank,
 fuel_tank_set_ind 
)
+
+
This writes a conformal fuel tank in a wing.
+
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+vehicle                                     [-] vehicle data structure
+wing.Segments.*.percent_span_location       [-]
+wing.spans.projected                        [m]
+wind_id                                     <str>
+fuel_tank.
+  inward_offset                             [m]
+  start_chord_percent                       [-] .1 is 10%
+  end_chord_percent                         [-]
+  start_span_percent                        [-]
+  end_span_percent                          [-]
+  fuel_type.density                         [kg/m^3]
+fuel_tank_set_ind                           <int>
+
+Outputs:
+Operates on the active OpenVSP model, no direct output
 
 Properties Used:
 N/A
@@ -467,7 +1947,7 @@ 

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SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@
- +
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SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
diff --git a/doxygen/group__Input__Output-SUAVE.html b/doxygen/group__Input__Output-SUAVE.html index a15a232f..186e3d44 100644 --- a/doxygen/group__Input__Output-SUAVE.html +++ b/doxygen/group__Input__Output-SUAVE.html @@ -1,9 +1,9 @@ - + - + SUAVE: SUAVE @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
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SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
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SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -137,7 +144,7 @@
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SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
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SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
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@@ -123,7 +130,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/group__Methods-Aerodynamics-AVL-Data.js b/doxygen/group__Methods-Aerodynamics-AVL-Data.js index 7720246c..afac0865 100644 --- a/doxygen/group__Methods-Aerodynamics-AVL-Data.js +++ b/doxygen/group__Methods-Aerodynamics-AVL-Data.js @@ -22,12 +22,15 @@ var group__Methods_Aerodynamics_AVL_Data = ] ], [ "Run_Case", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Run__Case.html", [ [ "__defaults__", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Run__Case.html#a6a9108165be8c60598d8040c1b3c5203", null ], - [ "append_control_deflection", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Run__Case.html#a0204b074d5dad2d32d5b221ad922dc2a", null ], + [ "aero_result_filename_1", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Run__Case.html#ab2020f583786f08fad116df7bd0d4fcd", null ], + [ "aero_result_filename_2", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Run__Case.html#acec5a3e0dfb52539fdc3136618caa5ea", null ], + [ "aero_result_filename_3", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Run__Case.html#a1f8d22469b8f3d78585a16babe48d570", null ], + [ "aero_result_filename_4", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Run__Case.html#a86724b57e2dcf8b5b43686e5bfcf230f", null ], [ "conditions", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Run__Case.html#a3eddb7985cac1df2f93fd4c90b5d14f2", null ], - [ "eigen_result_filename", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Run__Case.html#ae88894a124bdf653ae64543605114198", null ], + [ "eigen_result_filename_1", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Run__Case.html#a4e4049020099e3a1e9cfa6be5d7dbcc2", null ], + [ "eigen_result_filename_2", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Run__Case.html#a4f5c4e7bc7d3f75def3b7eb38f0da65f", null ], [ "index", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Run__Case.html#a5271bb99f849f5f6dca450f1f293023a", null ], [ "mass", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Run__Case.html#a92517a94d9e4bb763fceaca80c3a4b25", null ], - [ "result_filename", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Run__Case.html#a8cbb7d2798c08a5e631204180b4bd9c2", null ], [ "stability_and_control", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Run__Case.html#a5958cefee53f8e33db6a32520c7b7f91", null ], [ "tag", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1AVL_1_1Data_1_1Cases_1_1Run__Case.html#a94540c93dbd0009db6b3b022c9a3fbdc", null ] ] ], diff --git a/doxygen/group__Methods-Aerodynamics-AVL.html b/doxygen/group__Methods-Aerodynamics-AVL.html index d8ade134..d422faf4 100644 --- a/doxygen/group__Methods-Aerodynamics-AVL.html +++ b/doxygen/group__Methods-Aerodynamics-AVL.html @@ -1,9 +1,9 @@ - + - + SUAVE: AVL @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -109,97 +116,41 @@ - - - - - - + + - - + + - - - - - - + + + +

Functions

def SUAVE.Methods.Aerodynamics.AVL.create_avl_datastructure.create_avl_datastructure (geometry, conditions)
 
def SUAVE.Methods.Aerodynamics.AVL.initialize_inputs.initialize_inputs (geometry, configuration, conditions)
 
def SUAVE.Methods.Aerodynamics.AVL.purge_directory.purge_directory (path, purge_subdirectories=False)
 
def SUAVE.Methods.Aerodynamics.AVL.create_avl_datastructure.translate_avl_wing (suave_wing)
 
def SUAVE.Methods.Aerodynamics.AVL.purge_files.purge_files (filenames_array, directory='')
 
def SUAVE.Methods.Aerodynamics.AVL.read_results.read_results (avl_object)
 
def SUAVE.Methods.Aerodynamics.AVL.run_analysis.run_analysis (avl_object)
 
def SUAVE.Methods.Aerodynamics.AVL.run_analysis.run_analysis (avl_object, print_output)
 
def SUAVE.Methods.Aerodynamics.AVL.translate_data.translate_conditions_to_cases (avl, conditions)
 
def SUAVE.Methods.Aerodynamics.AVL.write_geometry.write_geometry (avl_object, spanwise_vortices_per_meter)
 
def SUAVE.Methods.Aerodynamics.AVL.write_input_deck.write_input_deck (avl_object)
 
def SUAVE.Methods.Aerodynamics.AVL.write_run_cases.write_run_cases (avl_object)
 
def SUAVE.Methods.Aerodynamics.AVL.write_geometry.write_geometry (avl_object, run_script_path)
 
def SUAVE.Methods.Aerodynamics.AVL.write_input_deck.write_input_deck (avl_object, trim_aircraft, control_surfaces)
 

Detailed Description

Functions to AVL calculations.

Function Documentation

- -

◆ create_avl_datastructure()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Aerodynamics.AVL.create_avl_datastructure.create_avl_datastructure ( geometry,
 conditions 
)
-
-
This translates the aircraft geometry into the format used in the AVL run file
-
-Assumptions:
-    None
-    
-Source:
-    Drela, M. and Youngren, H., AVL, http://web.mit.edu/drela/Public/web/avle
-    
-Inputs:
-    geometry    
-    
-Outputs:
-    avl_inputs
-    
-Properties Used:
-    N/A
-
-
-
- -

◆ initialize_inputs()

+ +

◆ purge_files()

- + - - - - - - - + - + @@ -208,94 +159,77 @@

-
This intializes the functions used in the AVL class
+
Purges folder folder of conflicting files
 
 Assumptions:
         None
-
+ 
 Source:
-        None
+    Drela, M. and Youngren, H., AVL, http://web.mit.edu/drela/Public/web/avl
 
 Inputs:
-        avl_inputs - passed into the write_geometry, write_run_cases and write_input_deck functions
+    None
 
 Outputs:
-        avl_imputs
+        None
 
 Properties Used:
-        N/A
+    N/A
 
-
-

◆ purge_directory()

+ +

◆ read_results()

def SUAVE.Methods.Aerodynamics.AVL.initialize_inputs.initialize_inputs def SUAVE.Methods.Aerodynamics.AVL.purge_files.purge_files (  geometry,
 configuration, filenames_array,
 conditions directory = '' 
- + - - - - - - - - - + - -
def SUAVE.Methods.Aerodynamics.AVL.purge_directory.purge_directory def SUAVE.Methods.Aerodynamics.AVL.read_results.read_results (  path,
 purge_subdirectories = False 
avl_object) )
-
Deletes the contents of a directory, then the directory itself.
-If purge_subdirectories is True, subdirectories of the directory will also
-be purged, recursively. In this case, the directory specified in the 'path'
-argument will always be removed at the end of this function. 
-However, if purge_subdirectories is False, files in 'path' will be deleted,
-but subdirectories and their contents will be left untouched. In this case, 
-the directory ('path' argument) will only be removed if it contains no
-subdirectories.
-
+
This functions reads the results from the results text file created 
+at the end of an AVL function call
 
 Assumptions:
-        None
+    None
     
 Source:
-    None
+    Drela, M. and Youngren, H., AVL, http://web.mit.edu/drela/Public/web/avl
 
 Inputs:
     None
 
 Outputs:
-    None
+    results     
 
 Properties Used:
     N/A
 
- -

◆ purge_files()

+ +

◆ run_analysis()

- + - + - + @@ -304,88 +238,56 @@

-
Purges folder folder of conflicting files
-
-Assumptions:
-        None
- 
-Source:
-    Drela, M. and Youngren, H., AVL, http://web.mit.edu/drela/Public/web/avl
-
-Inputs:
-    None
-
-Outputs:
-        None
-
-Properties Used:
-    N/A
-
- - -
-

◆ read_results()

- -
-
-

def SUAVE.Methods.Aerodynamics.AVL.purge_files.purge_files def SUAVE.Methods.Aerodynamics.AVL.run_analysis.run_analysis (  filenames_array, avl_object,
 directory = '' print_output 
- - - - - - - -
def SUAVE.Methods.Aerodynamics.AVL.read_results.read_results ( avl_object)
-
-
This functions reads the results from the results text file created 
-at the end of an AVL function call
+
This calls the AVL executable and runs an analysis
 
 Assumptions:
     None
     
 Source:
-    Drela, M. and Youngren, H., AVL, http://web.mit.edu/drela/Public/web/avl
-
-Inputs:
     None
 
+Inputs:
+    avl_object - passed into the  call_avl function  
+    
 Outputs:
-    results     
+    results
 
 Properties Used:
     N/A
 
- -

◆ run_analysis()

+ +

◆ translate_avl_wing()

- + - +
def SUAVE.Methods.Aerodynamics.AVL.run_analysis.run_analysis def SUAVE.Methods.Aerodynamics.AVL.create_avl_datastructure.translate_avl_wing (  avl_object)suave_wing)
-
This calls the AVL executable and runs an analysis
+
Translates wing geometry from the vehicle setup to AVL format
 
 Assumptions:
     None
-    
+
 Source:
     None
 
 Inputs:
-    avl_object - passed into the  call_avl function  
-    
+    suave_wing.tag                                                          [-]
+    suave_wing.symmetric                                                    [boolean]
+    suave_wing.verical                                                      [boolean]
+    suave_wing - passed into the populate_wing_sections function            [data stucture]
+
 Outputs:
-    results
+    w - aircraft wing in AVL format                                         [data stucture] 
 
 Properties Used:
     N/A
@@ -440,8 +342,8 @@ 

-

◆ write_geometry()

+ +

◆ write_geometry()

@@ -456,7 +358,7 @@

  - spanwise_vortices_per_meter  + run_script_path  @@ -485,8 +387,8 @@

-

◆ write_input_deck()

+ +

◆ write_input_deck()

- -

◆ write_run_cases()

- -
-
- - - + + - + + + + +
def SUAVE.Methods.Aerodynamics.AVL.write_run_cases.write_run_cases (  avl_object)control_surfaces 
)
-
This function writes the run cases used in the AVL batch analysis
-
+
This function writes the execution steps used in the AVL call
 Assumptions:
     None
     
 Source:
     Drela, M. and Youngren, H., AVL, http://web.mit.edu/drela/Public/web/avl
-
 Inputs:
-    avl_object.current_status.batch_file                    [-]
-    avl_object.geometry.mass_properties.center_of_gravity   [meters]
-
+    avl_object
 Outputs:
     None
-
+ 
 Properties Used:
     N/A
 
@@ -561,7 +441,7 @@

Generated by - doxygen 1.8.14 + doxygen 1.8.15

diff --git a/doxygen/group__Methods-Aerodynamics-AVL.js b/doxygen/group__Methods-Aerodynamics-AVL.js index 3e0ef8d5..541442b5 100644 --- a/doxygen/group__Methods-Aerodynamics-AVL.js +++ b/doxygen/group__Methods-Aerodynamics-AVL.js @@ -1,14 +1,11 @@ var group__Methods_Aerodynamics_AVL = [ [ "Data", "group__Methods-Aerodynamics-AVL-Data.html", "group__Methods-Aerodynamics-AVL-Data" ], - [ "create_avl_datastructure", "group__Methods-Aerodynamics-AVL.html#gac8a412b08b68fa155f5bd1d066f527e6", null ], - [ "initialize_inputs", "group__Methods-Aerodynamics-AVL.html#gaf1b797405da7d00146eac597e13280ea", null ], - [ "purge_directory", "group__Methods-Aerodynamics-AVL.html#ga1c0662bfaf8c7d1512dae0ad94fbda27", null ], [ "purge_files", "group__Methods-Aerodynamics-AVL.html#ga51c715bd682c9cda6dca2b017265218f", null ], [ "read_results", "group__Methods-Aerodynamics-AVL.html#ga111943e9a93d2fb37656998659a3a5f0", null ], - [ "run_analysis", "group__Methods-Aerodynamics-AVL.html#ga6c754c0ccd7480bbb1a9cc8bacf3f696", null ], + [ "run_analysis", "group__Methods-Aerodynamics-AVL.html#gaedea12850c1354360c8749cad0959297", null ], + [ "translate_avl_wing", "group__Methods-Aerodynamics-AVL.html#ga2ef302475090a759682b41bea45b7074", null ], [ "translate_conditions_to_cases", "group__Methods-Aerodynamics-AVL.html#ga7b721494da52b639d291d6fb7b9b8bf6", null ], - [ "write_geometry", "group__Methods-Aerodynamics-AVL.html#ga803c61fd15f149adf3cb052e2500e860", null ], - [ "write_input_deck", "group__Methods-Aerodynamics-AVL.html#ga5b4b731f90586149f6889a0ba256040a", null ], - [ "write_run_cases", "group__Methods-Aerodynamics-AVL.html#ga3aa7cb9305ca87e3ab5655d63d805f9e", null ] + [ "write_geometry", "group__Methods-Aerodynamics-AVL.html#gaaf8c2ef7143b8336ec7bfbe9027b8ac0", null ], + [ "write_input_deck", "group__Methods-Aerodynamics-AVL.html#gad2189eec905a618caa10b4c5681cbbe0", null ] ]; \ No newline at end of file diff --git a/doxygen/group__Methods-Aerodynamics-Airfoil__Panel__Method.html b/doxygen/group__Methods-Aerodynamics-Airfoil__Panel__Method.html new file mode 100644 index 00000000..6f72dde4 --- /dev/null +++ b/doxygen/group__Methods-Aerodynamics-Airfoil__Panel__Method.html @@ -0,0 +1,922 @@ + + + + + + + +SUAVE: Airfoil_Panel_Method + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
Airfoil_Panel_Method
+
+
+ + + + + + + + + + + + + + + + + + +

+Functions

def SUAVE.Methods.Aerodynamics.Airfoil_Panel_Method.aero_coeff.aero_coeff (x, y, cp, al, npanel)
 
def SUAVE.Methods.Aerodynamics.Airfoil_Panel_Method.airfoil_analysis.airfoil_analysis (airfoil_geometry, alpha, Re_L, npanel=100, batch_analysis=True, airfoil_stations=[0], initial_momentum_thickness=1E-5, tolerance=1E0)
 
def SUAVE.Methods.Aerodynamics.Airfoil_Panel_Method.heads_method.heads_method (npanel, nalpha, nRe, DEL_0, THETA_0, DELTA_STAR_0, TURBULENT_SURF, RE_L, TURBULENT_COORD, VE_I, DVE_I, batch_analysis, tol)
 
def SUAVE.Methods.Aerodynamics.Airfoil_Panel_Method.hess_smith.hess_smith (x_coord, y_coord, alpha, Re, npanel, batch_analyis)
 
def SUAVE.Methods.Aerodynamics.Airfoil_Panel_Method.infl_coeff.infl_coeff (x, y, xbar, ybar, st, ct, npanel, nalpha, nRe, batch_analyis)
 
def SUAVE.Methods.Aerodynamics.Airfoil_Panel_Method.panel_geometry.panel_geometry (x, y, npanel, nalpha, nRe)
 
def SUAVE.Methods.Aerodynamics.Airfoil_Panel_Method.thwaites_method.thwaites_method (npanel, nalpha, nRe, L, RE_L, X_I, VE_I, DVE_I, batch_analysis, tol, THETA_0)
 
def SUAVE.Methods.Aerodynamics.Airfoil_Panel_Method.velocity_distribution.velocity_distribution (qg, x, y, xbar, ybar, st, ct, alpha, Re, npanel)
 
+

Detailed Description

+

Function Documentation

+ +

◆ aero_coeff()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Aerodynamics.Airfoil_Panel_Method.aero_coeff.aero_coeff ( x,
 y,
 cp,
 al,
 npanel 
)
+
+
Compute airfoil force and moment coefficients about 
+                the quarter chord point          
+
+Assumptions:
+None
+
+Source:
+None                                                                    
+                                                               
+Inputs:                                                     
+x       -  Vector of x coordinates of the surface nodes      
+y       -  Vector of y coordinates of the surface nodes       
+cp      -  Vector of coefficients of pressure at the nodes  
+al      -  Angle of attack in radians                             
+npanel  -  Number of panels on the airfoil               
+                                                             
+Outputs:                                           
+cl      -  Airfoil lift coefficient                
+cd      -  Airfoil drag coefficient                                 
+cm      -  Airfoil moment coefficient about the c/4     
+ 
+   Properties Used:
+N/A
+
+
+
+ +

◆ airfoil_analysis()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Aerodynamics.Airfoil_Panel_Method.airfoil_analysis.airfoil_analysis ( airfoil_geometry,
 alpha,
 Re_L,
 npanel = 100,
 batch_analysis = True,
 airfoil_stations = [0],
 initial_momentum_thickness = 1E-5,
 tolerance = 1E0 
)
+
+
This computes the aerodynamic polars as well as the boundary layer properties of 
+an airfoil at a defined set of reynolds numbers and angle of attacks
+
+Assumptions:
+Michel Criteria used for transition
+
+Source:
+N/A
+
+Inputs: 
+airfoil_geometry   - airfoil geometry points                                                             [unitless]
+alpha              - angle of attacks                                                                    [radians]
+Re_L               - Reynolds numbers                                                                    [unitless]
+npanel             - number of airfoil panels                                                            [unitless]
+batch_analysis     - boolean : If True: the specified number of angle of attacks and Reynolds            [boolean]
+                              numbers are used to create a table of 2-D results for each combination
+                              Note: Can only accomodate one airfoil
+                              
+                              If False:The airfoils specified are run and corresponding angle of attacks 
+                              and Reynolds numbers
+                              Note: The number of airfoils, angle of attacks and reynolds numbers must 
+                              all the same dimension                     
+
+Outputs: 
+airfoil_properties.
+    AoA            - angle of attack                                                   [radians
+    Re             - Reynolds number                                                   [unitless]
+    Cl             - lift coefficients                                                 [unitless]
+    Cd             - drag coefficients                                                 [unitless]
+    Cm             - moment coefficients                                               [unitless]
+    normals        - surface normals of airfoil                                        [unitless]
+    x              - x coordinate points on airfoil                                    [unitless]
+    y              - y coordinate points on airfoil                                    [unitless]
+    x_bl           - x coordinate points on airfoil adjusted to include boundary layer [unitless]
+    y_bl           - y coordinate points on airfoil adjusted to include boundary layer [unitless]
+    Cp             - pressure coefficient distribution                                 [unitless]
+    Ue_Vinf        - ratio of boundary layer edge velocity to freestream               [unitless]
+    dVe            - derivative of boundary layer velocity                             [m/s-m]
+    theta          - momentum thickness                                                [m]
+    delta_star     - displacement thickness                                            [m]
+    delta          - boundary layer thickness                                          [m]
+    H              - shape factor                                                      [unitless]
+    Cf             - local skin friction coefficient                                   [unitless]
+    Re_theta_t     - Reynolds Number as a function of theta transition location        [unitless]
+    tr_crit        - critical transition criteria                                      [unitless]
+                    
+Properties Used:
+N/A
+
+
+
+ +

◆ heads_method()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Aerodynamics.Airfoil_Panel_Method.heads_method.heads_method ( npanel,
 nalpha,
 nRe,
 DEL_0,
 THETA_0,
 DELTA_STAR_0,
 TURBULENT_SURF,
 RE_L,
 TURBULENT_COORD,
 VE_I,
 DVE_I,
 batch_analysis,
 tol 
)
+
+
Computes the boundary layer characteristics in turbulent
+flow pressure gradients
+
+Source:
+Head, M. R., and P. Bandyopadhyay. "New aspects of turbulent boundary-layer structure."
+Journal of fluid mechanics 107 (1981): 297-338.
+
+Assumptions:
+None  
+
+Inputs: 
+nalpha         - number of angle of attacks                                                    [unitless]
+nRe            - number of reynolds numbers                                                    [unitless]
+batch_analysis - flag for batch analysis                                                       [boolean]
+DEL_0          - intital bounday layer thickness                                               [m]
+DELTA_STAR_0   - initial displacement thickness                                                [m]
+THETA_0        - initial momentum thickness                                                    [m]
+TURBULENT_SURF - normalized length of surface                                                  [unitless]
+RE_L           - Reynolds number                                                               [unitless]
+TURBULENT_COORD- x coordinate on surface of airfoil                                            [unitless] 
+VE_I           - boundary layer velocity at transition location                                [m/s-m] 
+DVE_I          - intial derivative value of boundary layer velocity at transition location     [unitless] 
+npanel         - number of points on surface                                                   [unitless]
+tol            - boundary layer error correction tolerance                                     [unitless]
+
+Outputs: 
+RESULTS.
+  X_H          - reshaped distance along airfoil surface                    [unitless]
+  THETA_H      - momentum thickness                                         [m]
+  DELTA_STAR_H - displacement thickness                                     [m] 
+  H_H          - shape factor                                               [unitless]
+  CF_H         - friction coefficient                                       [unitless]
+  RE_THETA_H   - Reynolds number as a function of momentum thickness        [unitless]
+  RE_X_H       - Reynolds number as a function of distance                  [unitless]
+  DELTA_H      - boundary layer thickness                                   [m]
+   
+Properties Used:
+N/A
+
+
+
+ +

◆ hess_smith()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Aerodynamics.Airfoil_Panel_Method.hess_smith.hess_smith ( x_coord,
 y_coord,
 alpha,
 Re,
 npanel,
 batch_analyis 
)
+
+
Computes the incompressible, inviscid flow over an airfoil of  arbitrary shape using the Hess-Smith panel method.  
+
+Assumptions:
+None
+
+Source:  "An introduction to theoretical and computational        
+                aerodynamics", J. Moran, Wiley, 1984  
+ 
+                                                 
+Inputs          
+x             -  Vector of x coordinates of the surface                  [unitess]     
+y             -  Vector of y coordinates of the surface                  [unitess] 
+batch_analyis - flag for batch analysis                                  [boolean]
+alpha         -  Airfoil angle of attack                                 [radians] 
+npanel        -  Number of panels on the airfoil.  The number of nodes   [unitess] 
+                  is equal to npanel+1, and the ith panel goes from node   
+                  i to node i+1                                
+                                                                       
+Outputs                                                      
+cl            -  Airfoil lift coefficient                         [unitless]           
+cd            -  Airfoil drag coefficient                         [unitless]      
+cm            -  Airfoil moment coefficient about the c/4         [unitless]            
+x_bar         -  Vector of x coordinates of the surface nodes     [unitless]           
+y_bar         -  Vector of y coordinates of the surface nodes     [unitless]          
+cp            -  Vector of coefficients of pressure at the nodes  [unitless]         
+
+Properties Used:
+N/A
+
+
+
+ +

◆ infl_coeff()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Aerodynamics.Airfoil_Panel_Method.infl_coeff.infl_coeff ( x,
 y,
 xbar,
 ybar,
 st,
 ct,
 npanel,
 nalpha,
 nRe,
 batch_analyis 
)
+
+
Compute the matrix of aerodynamic influence  coefficients for later use
+
+Assumptions:
+None
+
+Source:
+None 
+ 
+Inputs
+x       -  Vector of x coordinates of the surface nodes  [unitless]   
+y       -  Vector of y coordinates of the surface nodes  [unitless]   
+xbar    -  x-coordinate of the midpoint of each panel    [unitless]      
+ybar    -  y-coordinate of the midpoint of each panel    [unitless]     
+st      -  np.sin(theta) for each panel                  [radians]               
+ct      -  np.cos(theta) for each panel                  [radians]                 
+npanel  -  Number of panels on the airfoil               [unitless]       
+                                                                                        
+Outputs                                        
+ainfl   -  Aero influence coefficient matrix             [unitless]
+
+Properties Used:
+N/A
+
+
+
+ +

◆ panel_geometry()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Aerodynamics.Airfoil_Panel_Method.panel_geometry.panel_geometry ( x,
 y,
 npanel,
 nalpha,
 nRe 
)
+
+
Computes airfoil surface panelization parameters for later use in 
+the computation of the matrix of influence coefficients.        
+
+Assumptions:
+None
+
+Source:
+None 
+                                                                   
+Inputs:                                                         
+x       -  Vector of x coordinates of the surface nodes  [unitless]         
+y       -  Vector of y coordinates of the surface nodes  [unitless]      
+npanel  -  Number of panels on the airfoil               [unitless]         
+                                                                 
+Outputs:                                             
+l       -  Panel lengths                              [unitless]
+st      -  np.sin(theta) for each panel               [radians]
+ct      -  np.cos(theta) for each panel               [radians]
+xbar    -  x-coordinate of the midpoint of each panel [unitless]              
+ybar    -  y-coordinate of the midpoint of each panel [unitless]               
+
+
+Properties Used:
+N/A
+
+
+
+ +

◆ thwaites_method()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Aerodynamics.Airfoil_Panel_Method.thwaites_method.thwaites_method ( npanel,
 nalpha,
 nRe,
 L,
 RE_L,
 X_I,
 VE_I,
 DVE_I,
 batch_analysis,
 tol,
 THETA_0 
)
+
+
Computes the boundary layer characteristics in laminar 
+flow pressure gradients
+
+Source:
+Thwaites, Bryan. "Approximate calculation of the laminar boundary layer." 
+Aeronautical Quarterly 1.3 (1949): 245-280.
+
+Assumptions:
+None  
+
+Inputs:  
+npanel         - number of points on surface                                                 [unitless]
+nalpha         - number of angle of attacks                                                  [unitless]
+nRe            - number of reynolds numbers                                                  [unitless]
+batch_analysis - flag for batch analysis                                                     [boolean]
+THETA_0        - initial momentum thickness                                                  [m]
+L              - normalized length of surface                                                [unitless]
+RE_L           - Reynolds number                                                             [unitless]
+X_I            - x coordinate on surface of airfoil                                          [unitless]
+VE_I           - boundary layer velocity at transition location                              [m/s] 
+DVE_I          - initial derivative value of boundary layer velocity at transition location  [m/s-m] 
+tol            - boundary layer error correction tolerance                                   [unitless]
+
+Outputs: 
+RESULTS.
+  X_T          - reshaped distance along airfoil surface             [unitless]
+  THETA_T      - momentum thickness                                  [m]
+  DELTA_STAR_T - displacement thickness                              [m] 
+  H_T          - shape factor                                        [unitless]
+  CF_T         - friction coefficient                                [unitless]
+  RE_THETA_T   - Reynolds number as a function of momentum thickness [unitless]
+  RE_X_T       - Reynolds number as a function of distance           [unitless]
+  DELTA_T      - boundary layer thickness                            [m]
+
+Properties Used:
+N/A
+
+
+
+ +

◆ velocity_distribution()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Aerodynamics.Airfoil_Panel_Method.velocity_distribution.velocity_distribution ( qg,
 x,
 y,
 xbar,
 ybar,
 st,
 ct,
 alpha,
 Re,
 npanel 
)
+
+
Compute the tangential velocity distribution at the       
+             midpoint of each panel   
+
+Source:
+None
+
+Assumptions:
+None  
+
+Inputs:                                                    
+
+ qg          -  Vector of source/sink and vortex strengths    [unitless]          
+ x           -  Vector of x coordinates of the surface nodes  [unitless]         
+ y           -  Vector of y coordinates of the surface nodes  [unitless]            
+ xbar        -  x-coordinate of the midpoint of each panel    [unitless]           
+ ybar        -  y-coordinate of the midpoint of each panel    [unitless]           
+ st          -  np.sin(theta) for each panel                  [radians]                
+ ct          -  np.cos(theta) for each panel                  [radians]             
+ al          -  Angle of attack in radians                    [radians]             
+ npanel      -  Number of panels on the airfoil               [unitless]  
+
+ Outputs:                                                        
+
+ vt_2d        -  Vector of tangential velocities      
+
+Properties Used:
+N/A
+
+
+
+
+
+ + + + diff --git a/doxygen/group__Methods-Aerodynamics-Airfoil__Panel__Method.js b/doxygen/group__Methods-Aerodynamics-Airfoil__Panel__Method.js new file mode 100644 index 00000000..65166b3f --- /dev/null +++ b/doxygen/group__Methods-Aerodynamics-Airfoil__Panel__Method.js @@ -0,0 +1,11 @@ +var group__Methods_Aerodynamics_Airfoil__Panel__Method = +[ + [ "aero_coeff", "group__Methods-Aerodynamics-Airfoil__Panel__Method.html#ga32a7bc2bdb0ab57b62e19e9611c5ba7c", null ], + [ "airfoil_analysis", "group__Methods-Aerodynamics-Airfoil__Panel__Method.html#ga5e95fcb966cd4708ed46979e47f6e7b3", null ], + [ "heads_method", "group__Methods-Aerodynamics-Airfoil__Panel__Method.html#ga5c598bfdadcc832d298a5ee1226d1d60", null ], + [ "hess_smith", "group__Methods-Aerodynamics-Airfoil__Panel__Method.html#ga465f3403327e1879a30c912e50b19609", null ], + [ "infl_coeff", "group__Methods-Aerodynamics-Airfoil__Panel__Method.html#ga03374b94723de3befa49316b7523585b", null ], + [ "panel_geometry", "group__Methods-Aerodynamics-Airfoil__Panel__Method.html#ga01036face81d7808868522cf81d2465d", null ], + [ "thwaites_method", "group__Methods-Aerodynamics-Airfoil__Panel__Method.html#ga122d6dc3685b7620cfcdb8f6ce564a4c", null ], + [ "velocity_distribution", "group__Methods-Aerodynamics-Airfoil__Panel__Method.html#ga25dcd8dbfcc249f25815e7062711ac5c", null ] +]; \ No newline at end of file diff --git a/doxygen/group__Methods-Aerodynamics-Common-Fidelity__Zero-Drag.html b/doxygen/group__Methods-Aerodynamics-Common-Fidelity__Zero-Drag.html index 2152646b..abcc38ac 100644 --- a/doxygen/group__Methods-Aerodynamics-Common-Fidelity__Zero-Drag.html +++ b/doxygen/group__Methods-Aerodynamics-Common-Fidelity__Zero-Drag.html @@ -1,9 +1,9 @@ - + - + SUAVE: Drag @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@
- +

@@ -73,7 +78,9 @@
@@ -113,12 +120,14 @@   def SUAVE.Methods.Aerodynamics.Common.Fidelity_Zero.Drag.parasite_drag_fuselage.parasite_drag_fuselage (state, settings, geometry)   -def SUAVE.Methods.Aerodynamics.Common.Fidelity_Zero.Drag.parasite_drag_propulsor.parasite_drag_propulsor (state, settings, geometry) -  +def SUAVE.Methods.Aerodynamics.Common.Fidelity_Zero.Drag.parasite_drag_nacelle.parasite_drag_nacelle (state, settings, nacelle) +  def SUAVE.Methods.Aerodynamics.Common.Fidelity_Zero.Drag.parasite_drag_pylon.parasite_drag_pylon (state, settings, geometry)   def SUAVE.Methods.Aerodynamics.Common.Fidelity_Zero.Drag.parasite_drag_wing.parasite_drag_wing (state, settings, geometry)   +def SUAVE.Methods.Aerodynamics.Common.Fidelity_Zero.Drag.parasite_drag_wing.compute_parasite_drag (re, mac_w, Mc, Tc, xtu, xtl, sweep_w, t_c_w, Sref, Swet, C) +  def SUAVE.Methods.Aerodynamics.Common.Fidelity_Zero.Drag.parasite_total.parasite_total (state, settings, geometry)   def SUAVE.Methods.Aerodynamics.Common.Fidelity_Zero.Drag.spoiler_drag.spoiler_drag (state, settings, geometry) @@ -236,6 +245,122 @@

+

◆ compute_parasite_drag()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Aerodynamics.Common.Fidelity_Zero.Drag.parasite_drag_wing.compute_parasite_drag ( re,
 mac_w,
 Mc,
 Tc,
 xtu,
 xtl,
 sweep_w,
 t_c_w,
 Sref,
 Swet,
 C 
)
+
+
Computes the parasite drag due to wings
+
+Assumptions:
+Basic fit
+
+Source:
+adg.stanford.edu (Stanford AA241 A/B Course Notes)
+
+Inputs:
+re (Reynolds Number)    [Unitless]
+mac_w (Wing MAC)        [m]
+Mc (Mach Number)        [Unitless]
+Tc (Temperature)        [K]
+xtu (Upper Transition)  [Unitless] (percent of chord)
+xtl (Lower Transition)  [Unitless] (percent of chord)
+sweep_w (Wing Sweep)    [rad]
+t_c_w (Wing t/c)        [Unitless]
+Sref (Wing Ref Area)    [m^2]
+Swet (Wing Wetted Area) [m^2]
+C (Form Factor)         [Unitless]
+  
+Outputs:
+(u is upper, l is lower)
+wing_parasite_drag                 [Unitless]
+k_w    (Form Factor)               [Unitless]
+cf_w_u (Skin Friction Coefficient) [Unitless]
+cf_w_l                             [Unitless]
+k_comp_u (Compressibility Factor)  [Unitless]
+k_comp_l                           [Unitless]
+k_reyn_u (Reynolds Factor)         [Unitless]
+k_reyn_l                           [Unitless]
+
 Properties Used:
 N/A
 
@@ -275,21 +400,41 @@

Determines induced drag for the full aircraft Assumptions: -Based on fits +This function operates in one of three ways: + -An oswald efficiency is provided. All induced drag, inviscid and viscous, is use calculated using that factor + -A span efficiency is provided. The inviscid induced drag is calculated from that. Viscous induced drag is + calculated using the viscous_lift_dependent_drag_factor, K, and the parasite drag. + -The inviscid induced drag from the the lift calculation for each wing, usually a vortex lattice, is used. Viscous induced drag is + calculated using the viscous_lift_dependent_drag_factor, K, and the parasite drag. + + The last two options do not explicitly provide for the case where the fuselage produces an induced drag directly. Source: adg.stanford.edu (Stanford AA241 A/B Course Notes) +http://aerodesign.stanford.edu/aircraftdesign/aircraftdesign.html Inputs: -state.conditions.aerodynamics.lift_coefficient [Unitless] -state.conditions.aerodynamics.drag_breakdown.parasite.total [Unitless] -configuration.oswald_efficiency_factor [Unitless] -configuration.viscous_lift_dependent_drag_factor [Unitless] -geometry.wings['main_wing'].span_efficiency [Unitless] -geometry.wings['main_wing'].aspect_ratio [Unitless] +state.conditions.aerodynamics. + lift_coefficient [Unitless] + lift_breakdown.inviscid_wings[wings.*.tag] [Unitless] + drag_breakdown.induced.inviscid [Unitless] + drag_breakdown.induced.inviscid_wings[wings.*.tag] [Unitless] + drag_breakdown.parasite[wings.*.tag].parasite_drag_coefficient [Unitless] + drag_breakdown.parasite[wings.*.tag].reference_area [m^2] +settings.oswald_efficiency_factor [Unitless] +settings.viscous_lift_dependent_drag_factor [Unitless] +settings.span_efficiency [Unitless] + Outputs: -total_induced_drag [Unitless] +conditions.aerodynamics.drag_breakdown.induced. + total [Unitless] + viscous [Unitless] + oswald_efficiency_factor [Unitless] + viscous_wings_drag [Unitless] + +total_induced_drag [Unitless] + Properties Used: N/A @@ -340,8 +485,8 @@

-

◆ parasite_drag_propulsor()

+ +

◆ parasite_drag_nacelle()

- + @@ -432,7 +577,7 @@

- + @@ -441,7 +586,7 @@

-
Computes the parasite drag due to the propulsor
+
Computes the parasite drag due to the nacelle
 
 Assumptions:
 Basic fit
@@ -454,10 +599,10 @@ 

-
Computes the parasite drag due to pylons as a proportion of the propulsor drag
+
Computes the parasite drag due to pylons as a proportion of the network drag
 
 Assumptions:
 Basic fit
@@ -507,7 +652,7 @@ 

Generated by - doxygen 1.8.14 + doxygen 1.8.15 diff --git a/doxygen/group__Methods-Aerodynamics-Common-Fidelity__Zero-Drag.js b/doxygen/group__Methods-Aerodynamics-Common-Fidelity__Zero-Drag.js index 244d0209..e2dc4710 100644 --- a/doxygen/group__Methods-Aerodynamics-Common-Fidelity__Zero-Drag.js +++ b/doxygen/group__Methods-Aerodynamics-Common-Fidelity__Zero-Drag.js @@ -2,10 +2,11 @@ var group__Methods_Aerodynamics_Common_Fidelity__Zero_Drag = [ [ "compressibility_drag_wing", "group__Methods-Aerodynamics-Common-Fidelity__Zero-Drag.html#gaf20021fe8411a06607c40c0ddcfd7dca", null ], [ "compressibility_drag_wing_total", "group__Methods-Aerodynamics-Common-Fidelity__Zero-Drag.html#ga9492a72b7d9418c9b3260611ca92a178", null ], + [ "compute_parasite_drag", "group__Methods-Aerodynamics-Common-Fidelity__Zero-Drag.html#ga105c8a2462a994b30cc32cea275fcd76", null ], [ "induced_drag_aircraft", "group__Methods-Aerodynamics-Common-Fidelity__Zero-Drag.html#gaa045d2ec0dd318f054992b90a5c77a7b", null ], [ "miscellaneous_drag_aircraft_ESDU", "group__Methods-Aerodynamics-Common-Fidelity__Zero-Drag.html#ga1ab07fbded997c9136f554f34dbe2a17", null ], [ "parasite_drag_fuselage", "group__Methods-Aerodynamics-Common-Fidelity__Zero-Drag.html#ga6f2ba6214fc6c9cf197abd4314974783", null ], - [ "parasite_drag_propulsor", "group__Methods-Aerodynamics-Common-Fidelity__Zero-Drag.html#ga56def445cac037d343c05611841367e5", null ], + [ "parasite_drag_nacelle", "group__Methods-Aerodynamics-Common-Fidelity__Zero-Drag.html#gab1e2d3cc135b4bd5576dd80221e9ef16", null ], [ "parasite_drag_pylon", "group__Methods-Aerodynamics-Common-Fidelity__Zero-Drag.html#ga4b936aba6e18986d224e4da07a539ef8", null ], [ "parasite_drag_wing", "group__Methods-Aerodynamics-Common-Fidelity__Zero-Drag.html#ga56e33b81d00acf5955c775938336000e", null ], [ "parasite_total", "group__Methods-Aerodynamics-Common-Fidelity__Zero-Drag.html#gade82a1b666fd867c5687b582e5429836", null ], diff --git a/doxygen/group__Methods-Aerodynamics-Common-Fidelity__Zero-Helper__Functions.html b/doxygen/group__Methods-Aerodynamics-Common-Fidelity__Zero-Helper__Functions.html index fd76ac6a..d25cb239 100644 --- a/doxygen/group__Methods-Aerodynamics-Common-Fidelity__Zero-Helper__Functions.html +++ b/doxygen/group__Methods-Aerodynamics-Common-Fidelity__Zero-Helper__Functions.html @@ -1,9 +1,9 @@ - + - + SUAVE: Helper_Functions @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@
def SUAVE.Methods.Aerodynamics.Common.Fidelity_Zero.Drag.parasite_drag_propulsor.parasite_drag_propulsor def SUAVE.Methods.Aerodynamics.Common.Fidelity_Zero.Drag.parasite_drag_nacelle.parasite_drag_nacelle (   state,  geometry nacelle 
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@

@@ -109,8 +116,8 @@   def SUAVE.Methods.Aerodynamics.Common.Fidelity_Zero.Helper_Functions.compressible_turbulent_flat_plate.compressible_turbulent_flat_plate (Re, Ma, Tc)   -def SUAVE.Methods.Aerodynamics.Common.Fidelity_Zero.Helper_Functions.estimate_2ndseg_lift_drag_ratio.estimate_2ndseg_lift_drag_ratio (config) -  +def SUAVE.Methods.Aerodynamics.Common.Fidelity_Zero.Helper_Functions.estimate_2ndseg_lift_drag_ratio.estimate_2ndseg_lift_drag_ratio (state, settings, geometry) +  def SUAVE.Methods.Aerodynamics.Common.Fidelity_Zero.Helper_Functions.wave_drag_lift.wave_drag_lift (conditions, configuration, wing)   def SUAVE.Methods.Aerodynamics.Common.Fidelity_Zero.Helper_Functions.windmilling_drag.windmilling_drag (geometry, state) @@ -163,7 +170,7 @@

-

◆ estimate_2ndseg_lift_drag_ratio()

+ +

◆ estimate_2ndseg_lift_drag_ratio()

diff --git a/doxygen/group__Methods-Aerodynamics-Common-Fidelity__Zero-Helper__Functions.js b/doxygen/group__Methods-Aerodynamics-Common-Fidelity__Zero-Helper__Functions.js index 73b49647..42303124 100644 --- a/doxygen/group__Methods-Aerodynamics-Common-Fidelity__Zero-Helper__Functions.js +++ b/doxygen/group__Methods-Aerodynamics-Common-Fidelity__Zero-Helper__Functions.js @@ -3,7 +3,7 @@ var group__Methods_Aerodynamics_Common_Fidelity__Zero_Helper__Functions = [ "asymmetry_drag", "group__Methods-Aerodynamics-Common-Fidelity__Zero-Helper__Functions.html#ga660c5abf80b1e1cea8fc17e7653f6f5a", null ], [ "compressible_mixed_flat_plate", "group__Methods-Aerodynamics-Common-Fidelity__Zero-Helper__Functions.html#gaaf1cfba1bcfc31907440147d166ce637", null ], [ "compressible_turbulent_flat_plate", "group__Methods-Aerodynamics-Common-Fidelity__Zero-Helper__Functions.html#ga199c61f18da67d75ab1656d18aa0db6b", null ], - [ "estimate_2ndseg_lift_drag_ratio", "group__Methods-Aerodynamics-Common-Fidelity__Zero-Helper__Functions.html#ga39088de81585ef0043f4e930503d9b95", null ], + [ "estimate_2ndseg_lift_drag_ratio", "group__Methods-Aerodynamics-Common-Fidelity__Zero-Helper__Functions.html#gac96f7fe39f872a48c80aea5301a6cdba", null ], [ "wave_drag_lift", "group__Methods-Aerodynamics-Common-Fidelity__Zero-Helper__Functions.html#ga3347d24b977d464c4acc456c7afd591d", null ], [ "windmilling_drag", "group__Methods-Aerodynamics-Common-Fidelity__Zero-Helper__Functions.html#ga584c5c33c354ad0b542f960ef5da01f5", null ] ]; \ No newline at end of file diff --git a/doxygen/group__Methods-Aerodynamics-Common-Fidelity__Zero-Lift.html b/doxygen/group__Methods-Aerodynamics-Common-Fidelity__Zero-Lift.html index d91cf40f..f4db0745 100644 --- a/doxygen/group__Methods-Aerodynamics-Common-Fidelity__Zero-Lift.html +++ b/doxygen/group__Methods-Aerodynamics-Common-Fidelity__Zero-Lift.html @@ -1,9 +1,9 @@ - + - + SUAVE: Lift @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@
- +

@@ -73,7 +78,9 @@
@@ -106,11 +113,31 @@ def SUAVE.Methods.Aerodynamics.Common.Fidelity_Zero.Lift.aircraft_total.aircraft_total (state, settings, geometry)  aircraft_total.py More...
  +def SUAVE.Methods.Aerodynamics.Common.Fidelity_Zero.Lift.BET_calculations.compute_airfoil_aerodynamics (beta, c, r, R, B, Wa, Wt, a, nu, a_loc, a_geo, cl_sur, cd_sur, ctrl_pts, Nr, Na, tc, use_2d_analysis) +  +def SUAVE.Methods.Aerodynamics.Common.Fidelity_Zero.Lift.compute_RHS_matrix.compute_RHS_matrix (delta, phi, conditions, settings, geometry, propeller_wake_model) +  +def SUAVE.Methods.Aerodynamics.Common.Fidelity_Zero.Lift.compute_wing_induced_velocity.compute_wing_induced_velocity (VD, mach, compute_EW=False) +  +def SUAVE.Methods.Aerodynamics.Common.Fidelity_Zero.Lift.extract_wing_VD.extract_wing_collocation_points (geometry, wing_instance_idx) +  def SUAVE.Methods.Aerodynamics.Common.Fidelity_Zero.Lift.fuselage_correction.fuselage_correction (state, settings, geometry)  fuselage_correction.py More...
  -def SUAVE.Methods.Aerodynamics.Common.Fidelity_Zero.Lift.weissinger_vortex_lattice.weissinger_vortex_lattice (conditions, configuration, wing) -  +def SUAVE.Methods.Aerodynamics.Common.Fidelity_Zero.Lift.generate_vortex_distribution.generate_vortex_distribution (geometry, settings) +  +def SUAVE.Methods.Aerodynamics.Common.Fidelity_Zero.Lift.generate_vortex_distribution.generate_wing_vortex_distribution (VD, wing, n_cw, n_sw, spc, precision) +  +def SUAVE.Methods.Aerodynamics.Common.Fidelity_Zero.Lift.generate_vortex_distribution.generate_fuselage_and_nacelle_vortex_distribution (VD, fus, n_cw, n_sw, precision, model_geometry=False) +  +def SUAVE.Methods.Aerodynamics.Common.Fidelity_Zero.Lift.generate_vortex_distribution.compute_panel_area (VD) +  +def SUAVE.Methods.Aerodynamics.Common.Fidelity_Zero.Lift.generate_vortex_distribution.compute_unit_normal (VD) +  +def SUAVE.Methods.Aerodynamics.Common.Fidelity_Zero.Lift.make_VLM_wings.make_VLM_wings (geometry, settings) +  +def SUAVE.Methods.Aerodynamics.Common.Fidelity_Zero.Lift.VLM.VLM (conditions, settings, geometry) + 

Detailed Description

Lift methods that are directly specified by analyses.

@@ -148,7 +175,8 @@

aircraft_total.py

-

Created: Dec 2013, A. Variyar, Modified: Feb 2014, A. Variyar, T. Lukaczyk, T. Orra Apr 2014, A. Variyar Jan 2016, E. Botero

Returns total aircraft lift and stores values
+

Created: Dec 2013, A. Variyar, Modified: Feb 2014, A. Variyar, T. Lukaczyk, T. Orra Apr 2014, A. Variyar

+

Jan 2016, E. Botero

Returns total aircraft lift and stores values
 
 Assumptions:
 None
@@ -162,6 +190,440 @@ 

+

◆ compute_airfoil_aerodynamics()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Aerodynamics.Common.Fidelity_Zero.Lift.BET_calculations.compute_airfoil_aerodynamics ( beta,
 c,
 r,
 R,
 B,
 Wa,
 Wt,
 a,
 nu,
 a_loc,
 a_geo,
 cl_sur,
 cd_sur,
 ctrl_pts,
 Nr,
 Na,
 tc,
 use_2d_analysis 
)
+
+
Cl, Cdval = compute_airfoil_aerodynamics( beta,c,r,R,B,
+                                          Wa,Wt,a,nu,
+                                          a_loc,a_geo,cl_sur,cd_sur,
+                                          ctrl_pts,Nr,Na,tc,use_2d_analysis )
+
+Computes the aerodynamic forces at sectional blade locations. If airfoil
+geometry and locations are specified, the forces are computed using the
+airfoil polar lift and drag surrogates, accounting for the local Reynolds
+number and local angle of attack.
+
+If the airfoils are not specified, an approximation is used.
+
+Assumptions:
+N/A
+
+Source:
+N/A
+
+Inputs:
+   beta                       blade twist distribution                        [-]
+   c                          chord distribution                              [-]
+   r                          radius distribution                             [-]
+   R                          tip radius                                      [-]
+   B                          number of rotor blades                          [-]
+
+   Wa                         axial velocity                                  [-]
+   Wt                         tangential velocity                             [-]
+   a                          speed of sound                                  [-]
+   nu                         viscosity                                       [-]
+
+   a_loc                      Locations of specified airfoils                 [-]
+   a_geo                      Geometry of specified airfoil                   [-]
+   cl_sur                     Lift Coefficient Surrogates                     [-]
+   cd_sur                     Drag Coefficient Surrogates                     [-]
+   ctrl_pts                   Number of control points                        [-]
+   Nr                         Number of radial blade sections                 [-]
+   Na                         Number of azimuthal blade stations              [-]
+   tc                         Thickness to chord                              [-]
+   use_2d_analysis            Specifies 2d disc vs. 1d single angle analysis  [Boolean]
+
+Outputs:
+   Cl                       Lift Coefficients                         [-]
+   Cdval                    Drag Coefficients  (before scaling)       [-]
+   alpha                    section local angle of attack             [rad]
+
+
+ +

◆ compute_panel_area()

+ +
+
+ + + + + + + + +
def SUAVE.Methods.Aerodynamics.Common.Fidelity_Zero.Lift.generate_vortex_distribution.compute_panel_area ( VD)
+
+
This computes the area of the panels on the lifting surface of the vehicle 
+
+Assumptions: 
+None
+
+Source:   
+None
+
+Inputs:   
+VD                   - vortex distribution    
+
+Properties Used:
+N/A
+
+
+
+ +

◆ compute_RHS_matrix()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Aerodynamics.Common.Fidelity_Zero.Lift.compute_RHS_matrix.compute_RHS_matrix ( delta,
 phi,
 conditions,
 settings,
 geometry,
 propeller_wake_model 
)
+
+
This computes the right hand side matrix for the VLM. In this
+function, induced velocites from propeller wake are also included
+when relevent and where specified
+
+Source:
+1. Low-Speed Aerodynamics, Second Edition by Joseph Katz, Allen Plotkin
+Pgs. 331-338
+
+2. VORLAX Source Code
+
+Inputs:
+geometry
+    networks                                 [Unitless]
+    vehicle vortex distribution              [Unitless]
+
+conditions.aerodynamics.angle_of_attack      [radians]
+conditions.aerodynamics.side_slip_angle      [radians]
+conditions.freestream.velocity               [m/s]
+conditions.stability.dynamic.pitch_rate      [radians/s]
+conditions.stability.dynamic.roll_rate       [radians/s]
+conditions.stability.dynamic.yaw_rate        [radians/s]
+
+sur_flag    - use_surrogate flag             [Unitless]
+slipstream  - propeller_wake_model flag      [Unitless]
+delta, phi  - flow tangency angles           [radians]
+
+Outputs:
+rhs.
+    RHS
+    ONSET
+    Vx_ind_total
+    Vz_ind_total
+    V_distribution
+    dt
+    YGIRO
+    ZGIRO
+    VX
+    SCNTL
+    CCNTL
+    COD
+    SID
+
+Properties Used:
+N/A
+
+
+
+ +

◆ compute_unit_normal()

+ +
+
+ + + + + + + + +
def SUAVE.Methods.Aerodynamics.Common.Fidelity_Zero.Lift.generate_vortex_distribution.compute_unit_normal ( VD)
+
+
This computes the unit normal vector of each panel
+
+
+Assumptions: 
+None
+
+Source:
+None
+
+Inputs:   
+VD                   - vortex distribution    
+
+Properties Used:
+N/A
+
+
+
+ +

◆ compute_wing_induced_velocity()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Aerodynamics.Common.Fidelity_Zero.Lift.compute_wing_induced_velocity.compute_wing_induced_velocity ( VD,
 mach,
 compute_EW = False 
)
+
+
This computes the induced velocities at each control point of the vehicle vortex lattice 
+
+Assumptions: 
+Trailing vortex legs infinity are alligned to freestream
+
+Outside of a call to the VLM() function itself, EW does not need to be computed, as C_mn 
+provides the same information in the body-frame. 
+
+Source:  
+1. Miranda, Luis R., Robert D. Elliot, and William M. Baker. "A generalized vortex 
+lattice method for subsonic and supersonic flow applications." (1977). (NASA CR)
+
+2. VORLAX Source Code
+
+Inputs: 
+VD       - vehicle vortex distribution                    [Unitless] 
+mach                                                      [Unitless] 
+
+Outputs:                                
+C_mn     - total induced velocity matrix                  [Unitless] 
+s        - semispan of the horshoe vortex                 [m] 
+t        - tangent of the horshoe vortex                  [-] 
+CHORD    - chord length for a panel                       [m] 
+RFLAG    - sonic vortex flag                              [boolean] 
+ZETA     - tangent incidence angle of the chordwise strip [-] 
+
+Properties Used:
+N/A
+
+
+
+ +

◆ extract_wing_collocation_points()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Aerodynamics.Common.Fidelity_Zero.Lift.extract_wing_VD.extract_wing_collocation_points ( geometry,
 wing_instance_idx 
)
+
+
This extracts the collocation points of the vehicle vortex distribution
+belonging to the specified wing instance index. This is useful for slipstream
+analysis, where the wake of a propeller is included in the VLM analysis 
+of a specified wing in the vehicle.
+
+Source:
+None
+
+Inputs:
+geometry      -    SUAVE vehicle 
+wing_instance -    wing instance tag
+
+Outputs:
+VD_wing   - colocation points of vortex distribution for specified wing
+ids       - indices in the vortex distribution corresponding to specified wing
+
 Properties Used:
 N/A
 
@@ -223,14 +685,299 @@

-

◆ weissinger_vortex_lattice()

+ +

◆ generate_fuselage_and_nacelle_vortex_distribution()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Aerodynamics.Common.Fidelity_Zero.Lift.generate_vortex_distribution.generate_fuselage_and_nacelle_vortex_distribution ( VD,
 fus,
 n_cw,
 n_sw,
 precision,
 model_geometry = False 
)
+
+
This generates the vortex distribution points on a fuselage or nacelle component
+Assumptions: 
+If nacelle has segments defined, the mean width and height of the nacelle is used
+Source:   
+None
+
+Inputs:   
+VD                   - vortex distribution
+
+Properties Used:
+N/A
+
+
+
+ +

◆ generate_vortex_distribution()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Aerodynamics.Common.Fidelity_Zero.Lift.generate_vortex_distribution.generate_vortex_distribution ( geometry,
 settings 
)
+
+
Compute the coordinates of panels, vortices , control points
+and geometry used to build the influence coefficient matrix. A 
+different discretization (n_sw and n_cw) may be defined for each type
+of major section (wings and fuselages). 
+
+Control surfaces are modelled as wings, but adapt their panel density 
+to that of the area in which they reside on their own wing.   
+
+Assumptions: 
+Below is a schematic of the coordinates of an arbitrary panel  
+
+XA1 ____________________________ XB1    
+   |                            |
+   |        bound vortex        |
+XAH|  ________________________  |XBH
+   | |           XCH          | |
+   | |                        | |
+   | |                        | |     
+   | |                        | |
+   | |                        | |
+   | |           0 <--control | |       
+   | |          XC     point  | |  
+   | |                        | |
+   XA2 |_|________________________|_|XB2
+     |                        |     
+     |       trailing         |  
+     |   <--  vortex   -->    |  
+     |         legs           | 
+         
+
+In addition, all control surfaces should be appended directly
+   to the wing, not the wing segments    
+
+For control surfaces, "positve" deflection corresponds to the RH rule where the axis of rotation is the OUTBOARD-pointing hinge vector
+symmetry: the LH rule is applied to the reflected surface for non-ailerons. Ailerons follow a RH rule for both sides
+
+Source:  
+None
+
+Inputs:
+geometry.wings                                [Unitless]  
+settings.floating_point_precision             [np.dtype]
+
+Of the following settings, the user should define either the number_ atrributes or the wing_ and fuse_ attributes.
+settings.number_spanwise_vortices             - a base number of vortices to be applied to both wings and fuselages
+settings.number_chordwise_vortices            - a base number of vortices to be applied to both wings and fuselages
+settings.wing_spanwise_vortices               - the number of vortices to be applied to only the wings
+settings.wing_chordwise_vortices              - the number of vortices to be applied to only the wings
+settings.fuselage_spanwise_vortices           - the number of vortices to be applied to only the fuslages
+settings.fuselage_chordwise_vortices          - the number of vortices to be applied to only the fuselages 
+   
+Outputs:                                   
+VD - vehicle vortex distribution              [Unitless] 
+
+Properties Used:
+N/A 
+
+
+ +

◆ generate_wing_vortex_distribution()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Aerodynamics.Common.Fidelity_Zero.Lift.generate_vortex_distribution.generate_wing_vortex_distribution ( VD,
 wing,
 n_cw,
 n_sw,
 spc,
 precision 
)
+
+
This generates vortex distribution points for the given wing 
+
+Assumptions: 
+The wing is segmented and was made or modified by make_VLM_wings()
+
+For control surfaces, "positve" deflection corresponds to the RH rule where the axis of rotation is the OUTBOARD-pointing hinge vector
+symmetry: the LH rule is applied to the reflected surface for non-ailerons. Ailerons follow a RH rule for both sides
+
+The hinge_vector will only ever be calcualted on the first strip of any control/all-moving surface. It is assumed that all control
+surfaces are trapezoids, thus needing only one hinge, and that all all-moving surfaces have exactly one point of rotation.
+
+Source:   
+None
+
+Inputs:   
+VD                   - vortex distribution
+wing                 - a Data object made or modified by make_VLM_wings() to mimick a Wing object
+
+Properties Used:
+N/A
+
+
+
+ +

◆ make_VLM_wings()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Aerodynamics.Common.Fidelity_Zero.Lift.make_VLM_wings.make_VLM_wings ( geometry,
 settings 
)
+
+
This parses through geometry.wings to create a Container of Data objects.
+    Relevant VLM attributes are copied from geometry.wings to the Container.
+    After, the wing data objects are reformatted. All control surfaces are 
+    also added to the Container as Data objects representing full wings. 
+    Helper variables are then computed (most notably span_breaks) for later. 
+    
+    see make_span_break() for further details
+
+Assumptions: 
+All control surfaces are appended directly to the wing, not wing segments.
+If a given wing has no segments, it must have either .taper or .chords.root 
+    and .chords.tip defined
+
+Source:   
+None
+
+Inputs:
+geometry.
+    wings.wing.
+        twists.root
+        twists.tip
+        dihedral
+        sweeps.quarter_chord OR sweeps.leading_edge
+        thickness_to_chord
+        taper
+        chord.root
+        chords.tip
+        
+        control_surface.
+            tag
+            span_fraction_start
+            span_fraction_end
+            deflection
+            chord_fraction
+            
+settings.discretize_control_surfaces  --> set to True to generate control surface panels
+
+Properties Used:
+N/A
+
+
+
+ +

◆ VLM()

- + @@ -239,13 +986,13 @@

- + - + @@ -254,34 +1001,105 @@

-
Uses the vortex lattice method to compute the lift coefficient and induced drag component
+
Uses the vortex lattice method to compute the lift, induced drag and moment coefficients.
+
+The user has the option to discretize control surfaces using the boolean settings.discretize_control_surfaces.
+The user should be forwarned that this will cause very slight differences in results for 0 deflection due to
+the slightly different discretization.
+
+The user has the option to use the boundary conditions and induced velocities from either SUAVE
+or VORLAX. See build_RHS in compute_RHS_matrix.py for more details.
+
+By default in Vortex_Lattice, VLM performs calculations based on panel coordinates with float32 precision. 
+The user may also choose to use float16 or float64, but be warned that the latter can be memory intensive.
+
+The user should note that fully capitalized variables correspond to a VORLAX variable of the same name
+
 
 Assumptions:
-None
+The user provides either global discretezation (number_spanwise/chordwise_vortices) or
+separate discretization (wing/fuselage_spanwise/chordwise_vortices) in settings, not both.
+The set of settings not being used should be set to None.
+
+The VLM requires that the user provide a non-zero velocity that matches mach number. For
+surrogate training cases at mach 0, VLM uses a velocity of 1e-6 m/s
+
 
 Source:
-An Introduction to Theoretical and Computational Aerodynamics by Jack Moran
+1. Miranda, Luis R., Robert D. Elliot, and William M. Baker. "A generalized vortex 
+lattice method for subsonic and supersonic flow applications." (1977). (NASA CR)
+
+2. VORLAX Source Code
+
 
 Inputs:
-wing.
-  spans.projected                       [m]
-  chords.root                           [m]
-  chords.tip                            [m]
-  sweeps.quarter_chord                  [radians]
-  taper                                 [Unitless]
-  twists.root                           [radians]
-  twists.tip                            [radians]
-  symmetric                             [Boolean]
-  aspect_ratio                          [Unitless]
-  areas.reference                       [m^2]
-  vertical                              [Boolean]
-configuration.number_panels_spanwise    [Unitless]
-configuration.number_panels_chordwise   [Unitless]
-conditions.aerodynamics.angle_of_attack [radians]
+geometry.
+   reference_area                          [m^2]
+   wing.
+     spans.projected                       [m]
+     chords.root                           [m]
+     chords.tip                            [m]
+     sweeps.quarter_chord                  [radians]
+     taper                                 [Unitless]
+     twists.root                           [radians]
+     twists.tip                            [radians]
+     symmetric                             [Boolean]
+     aspect_ratio                          [Unitless]
+     areas.reference                       [m^2]
+     vertical                              [Boolean]
+     origin                                [m]
+   fuselage.
+    origin                                 [m]
+    width                                  [m]
+    heights.maximum                        [m]      
+    lengths.nose                           [m]    
+    lengths.tail                           [m]     
+    lengths.total                          [m]     
+    lengths.cabin                          [m]     
+    fineness.nose                          [Unitless]
+    fineness.tail                          [Unitless]
+    
+settings.number_spanwise_vortices          [Unitless]  <---|
+settings.number_chordwise_vortices         [Unitless]  <---|
+                                                           |--Either/or; see generate_vortex_distribution() for more details
+settings.wing_spanwise_vortices            [Unitless]  <---|
+settings.wing_chordwise_vortices           [Unitless]  <---|
+settings.fuselage_spanwise_vortices        [Unitless]  <---|
+settings.fuselage_chordwise_vortices       [Unitless]  <---|  
+   
+settings.use_surrogate                     [Unitless]
+settings.propeller_wake_model              [Unitless]
+settings.discretize_control_surfaces       [Boolean], set to True to generate control surface panels
+settings.use_VORLAX_matrix_calculation     [boolean]
+settings.floating_point_precision          [np.float16/32/64]
+   
+conditions.aerodynamics.angle_of_attack    [radians]
+conditions.aerodynamics.side_slip_angle    [radians]
+conditions.freestream.mach_number          [Unitless]
+conditions.freestream.velocity             [m/s]
+conditions.stability.dynamic.pitch_rate    [radians/s]
+conditions.stability.dynamic.roll_rate     [radians/s]
+conditions.stability.dynamic.yaw_rate      [radians/s]
+   
+
+Outputs:    
+results.
+    CL                                     [Unitless], CLTOT in VORLAX
+    CDi                                    [Unitless], CDTOT in VORLAX
+    CM                                     [Unitless], CMTOT in VORLAX
+    CYTOT                                  [Unitless], Total y force coeff
+    CRTOT                                  [Unitless], Rolling moment coeff (unscaled)
+    CRMTOT                                 [Unitless], Rolling moment coeff (scaled by w_span)
+    CNTOT                                  [Unitless], Yawing  moment coeff (unscaled)
+    CYMTOT                                 [Unitless], Yawing  moment coeff (scaled by w_span)
+    CL_wing                                [Unitless], CL  of each wing
+    CDi_wing                               [Unitless], CDi of each wing
+    cl_y                                   [Unitless], CL  of each strip
+    cdi_y                                  [Unitless], CDi of each strip
+    alpha_i                                [radians] , Induced angle of each strip in each wing (array of numpy arrays)
+    CP                                     [Unitless], Pressure coefficient of each panel
+    gamma                                  [Unitless], Vortex strengths of each panel
 
-Outputs:
-Cl                                      [Unitless]
-Cd                                      [Unitless]
 
 Properties Used:
 N/A
@@ -295,7 +1113,7 @@ 

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@@ -57,9 +60,11 @@
def SUAVE.Methods.Aerodynamics.Common.Fidelity_Zero.Lift.weissinger_vortex_lattice.weissinger_vortex_lattice def SUAVE.Methods.Aerodynamics.Common.Fidelity_Zero.Lift.VLM.VLM (   conditions,  configuration, settings,
 wing geometry 
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@

@@ -122,7 +129,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/group__Methods-Aerodynamics-Common-Gas__Dynamics.html b/doxygen/group__Methods-Aerodynamics-Common-Gas__Dynamics.html new file mode 100644 index 00000000..59d8d8bc --- /dev/null +++ b/doxygen/group__Methods-Aerodynamics-Common-Gas__Dynamics.html @@ -0,0 +1,257 @@ + + + + + + + +SUAVE: Gas_Dymamics + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
Gas_Dymamics
+
+
+ +

Gas Dynamics methods that are directly specified by analyses. +More...

+ + + + + + +

+Functions

def SUAVE.Methods.Aerodynamics.Common.Gas_Dynamics.Oblique_Shock.oblique_shock_relations (M0, gamma, theta, beta)
 
def SUAVE.Methods.Aerodynamics.Common.Gas_Dynamics.Oblique_Shock.theta_beta_mach (M0, gamma, theta, n=0)
 
+

Detailed Description

+

Gas Dynamics methods that are directly specified by analyses.

+

Function Documentation

+ +

◆ oblique_shock_relations()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Aerodynamics.Common.Gas_Dynamics.Oblique_Shock.oblique_shock_relations ( M0,
 gamma,
 theta,
 beta 
)
+
+
Computes flow quatities/ratios after undergoing 
+an oblique shock
+
+Assumptions:
+None
+
+Source:
+Chapter 12 of:
+https://web.stanford.edu/~cantwell/AA210A_Course_Material/AA210A_Course_Notes/
+
+https://arc.aiaa.org/doi/pdf/10.2514/2.2349
+
+Inputs:
+Mach, M0                             [-]
+Isentropic Expansion Factor, gamma   [-]
+Flow turn angle, theta               [rad]
+Shock Angle, beta                    [rad]
+
+Outputs:
+Mach, M1                             [-]
+Static Temperature Ratio, Tr         [-]
+Static Pressure Ratio, Pr            [-]
+Stagnation Pressure Ratio, Ptr       [-]
+
+Properties Used:
+N/A
+
+
+
+ +

◆ theta_beta_mach()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Aerodynamics.Common.Gas_Dynamics.Oblique_Shock.theta_beta_mach ( M0,
 gamma,
 theta,
 n = 0 
)
+
+
Computes shock angle of an oblique shock
+
+    Assumptions:
+    None
+
+    Source:
+    Chapter 12 of:
+    https://web.stanford.edu/~cantwell/AA210A_Course_Material/AA210A_Course_Notes/
+
+    Inputs:
+    Mach, M0                             [-]
+    Isentropic Expansion Factor, gamma   [-]
+    Flow turn angle, theta               [rad]
+    Strong Shock (0 = weak), delta       [-]
+
+    Outputs:
+    Shock Angle, Beta                    [rad]
+    
+    Properties Used:
+    N/A
+
+
+
+
+ + + + diff --git a/doxygen/group__Methods-Aerodynamics-Common-Gas__Dynamics.js b/doxygen/group__Methods-Aerodynamics-Common-Gas__Dynamics.js new file mode 100644 index 00000000..28c9a020 --- /dev/null +++ b/doxygen/group__Methods-Aerodynamics-Common-Gas__Dynamics.js @@ -0,0 +1,5 @@ +var group__Methods_Aerodynamics_Common_Gas__Dynamics = +[ + [ "oblique_shock_relations", "group__Methods-Aerodynamics-Common-Gas__Dynamics.html#gaba4cd75ec86510b8e824a5ced3cd0a89", null ], + [ "theta_beta_mach", "group__Methods-Aerodynamics-Common-Gas__Dynamics.html#gaf658ecdf28c8cffdcb868a717d2b23bd", null ] +]; \ No newline at end of file diff --git a/doxygen/group__Methods-Aerodynamics-Common.html b/doxygen/group__Methods-Aerodynamics-Common.html index 63825532..a006ca12 100644 --- a/doxygen/group__Methods-Aerodynamics-Common.html +++ b/doxygen/group__Methods-Aerodynamics-Common.html @@ -1,9 +1,9 @@ - + - + SUAVE: Common @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@
- +

@@ -73,7 +78,9 @@

@@ -116,7 +123,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/group__Methods-Aerodynamics-Fidelity__Zero-Lift.html b/doxygen/group__Methods-Aerodynamics-Fidelity__Zero-Lift.html index 62b10a1a..24bed46a 100644 --- a/doxygen/group__Methods-Aerodynamics-Fidelity__Zero-Lift.html +++ b/doxygen/group__Methods-Aerodynamics-Fidelity__Zero-Lift.html @@ -1,9 +1,9 @@ - + - + SUAVE: Lift @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@

- +
@@ -73,7 +78,9 @@
@@ -105,12 +112,10 @@ Functions

def SUAVE.Methods.Aerodynamics.Fidelity_Zero.Lift.compute_flap_lift.compute_flap_lift (t_c, flap_type, flap_chord, flap_angle, sweep, wing_Sref, wing_affected_area)   -def SUAVE.Methods.Aerodynamics.Fidelity_Zero.Lift.compute_max_lift_coeff.compute_max_lift_coeff (vehicle, conditions=None) -  +def SUAVE.Methods.Aerodynamics.Fidelity_Zero.Lift.compute_max_lift_coeff.compute_max_lift_coeff (state, settings, geometry) +  def SUAVE.Methods.Aerodynamics.Fidelity_Zero.Lift.compute_slat_lift.compute_slat_lift (slat_angle, sweep_angle)   -def SUAVE.Methods.Aerodynamics.Fidelity_Zero.Lift.wing_compressibility_correction.wing_compressibility_correction (state, settings, geometry) - 

Detailed Description

Functions to perform low-fidelity lift calculations.

@@ -195,8 +200,8 @@

-

◆ compute_max_lift_coeff()

+ +

◆ compute_max_lift_coeff()

@@ -205,13 +210,19 @@

def SUAVE.Methods.Aerodynamics.Fidelity_Zero.Lift.compute_max_lift_coeff.compute_max_lift_coeff (   - vehicle, + state, + + + + +   + settings,   - conditions = None  + geometry  @@ -229,27 +240,27 @@

-

◆ wing_compressibility_correction()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Aerodynamics.Fidelity_Zero.Lift.wing_compressibility_correction.wing_compressibility_correction ( state,
 settings,
 geometry 
)
-
-
Corrects a wings lift based on compressibility
-
-Assumptions:
-subsonic
-
-Source:
-https://stanford.edu/~cantwell/AA200_Course_Material/AA200_Course_Notes/
-
-Inputs:
-settings.fuselage_lift_correction  [-]
-state.conditions.
-  freestream.mach_number           [-]
-  aerodynamics.angle_of_attack     [radians]
-  aerodynamics.lift_coefficient    [-]
-
-Outputs:
-state.conditions.aerodynamics.
-  lift_breakdown.compressible_wings [-] CL for the wings
-  lift_coefficient                  [-]
-wings_lift_comp                     [-]
-
 Properties Used:
 N/A
 
@@ -365,7 +319,7 @@

Generated by - doxygen 1.8.14 + doxygen 1.8.15

diff --git a/doxygen/group__Methods-Aerodynamics-Fidelity__Zero-Lift.js b/doxygen/group__Methods-Aerodynamics-Fidelity__Zero-Lift.js index 55e40174..f326a003 100644 --- a/doxygen/group__Methods-Aerodynamics-Fidelity__Zero-Lift.js +++ b/doxygen/group__Methods-Aerodynamics-Fidelity__Zero-Lift.js @@ -1,7 +1,6 @@ var group__Methods_Aerodynamics_Fidelity__Zero_Lift = [ [ "compute_flap_lift", "group__Methods-Aerodynamics-Fidelity__Zero-Lift.html#gaba1f06c8eee68017b66b4f853272463b", null ], - [ "compute_max_lift_coeff", "group__Methods-Aerodynamics-Fidelity__Zero-Lift.html#ga4adc3f3425f18c8b914194a7b233fe31", null ], - [ "compute_slat_lift", "group__Methods-Aerodynamics-Fidelity__Zero-Lift.html#ga0f976657004084baf27a29d8bbf567be", null ], - [ "wing_compressibility_correction", "group__Methods-Aerodynamics-Fidelity__Zero-Lift.html#ga987c51069000f6e459d2754ed2533125", null ] + [ "compute_max_lift_coeff", "group__Methods-Aerodynamics-Fidelity__Zero-Lift.html#gadf7be432a94aedc5974f02a9a210b7b7", null ], + [ "compute_slat_lift", "group__Methods-Aerodynamics-Fidelity__Zero-Lift.html#ga0f976657004084baf27a29d8bbf567be", null ] ]; \ No newline at end of file diff --git a/doxygen/group__Methods-Aerodynamics-Fidelity__Zero.html b/doxygen/group__Methods-Aerodynamics-Fidelity__Zero.html index ab93c947..db48a71a 100644 --- a/doxygen/group__Methods-Aerodynamics-Fidelity__Zero.html +++ b/doxygen/group__Methods-Aerodynamics-Fidelity__Zero.html @@ -1,9 +1,9 @@ - + - + SUAVE: Fidelity_Zero @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@
- +

@@ -73,7 +78,9 @@
@@ -116,7 +123,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/group__Methods-Aerodynamics-Lifting__Line.html b/doxygen/group__Methods-Aerodynamics-Lifting__Line.html index 43aef7ae..5a9a7130 100644 --- a/doxygen/group__Methods-Aerodynamics-Lifting__Line.html +++ b/doxygen/group__Methods-Aerodynamics-Lifting__Line.html @@ -1,9 +1,9 @@ - + - + SUAVE: Lifting_Line @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -106,7 +113,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/group__Methods-Aerodynamics-OpenVSP__Wave__Drag.html b/doxygen/group__Methods-Aerodynamics-OpenVSP__Wave__Drag.html index 96d1770f..639a7fac 100644 --- a/doxygen/group__Methods-Aerodynamics-OpenVSP__Wave__Drag.html +++ b/doxygen/group__Methods-Aerodynamics-OpenVSP__Wave__Drag.html @@ -1,9 +1,9 @@ - + - + SUAVE: OpenVSP_Wave_Drag @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -322,7 +329,7 @@

Generated by - doxygen 1.8.14 + doxygen 1.8.15

diff --git a/doxygen/group__Methods-Aerodynamics-Supersonic__Zero-Drag.html b/doxygen/group__Methods-Aerodynamics-Supersonic__Zero-Drag.html index b2aae935..e45476c2 100644 --- a/doxygen/group__Methods-Aerodynamics-Supersonic__Zero-Drag.html +++ b/doxygen/group__Methods-Aerodynamics-Supersonic__Zero-Drag.html @@ -1,9 +1,9 @@ - + - + SUAVE: Drag @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -92,6 +99,7 @@
@@ -101,27 +109,31 @@

Functions to perform low-fidelity drag calculations including supersonic. More...

+ + + +

+Classes

class  SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.Cubic_Spline_Blender.Cubic_Spline_Blender
 
- - - - - - - - + + + + - - - - - - - + + + + + + + + + +

Functions

def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.compressibility_drag_total.compressibility_drag_total (state, settings, geometry)
 
def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.compressibility_drag_total.drag_div (Mc_ii, wing, k, cl, Sref_main)
 
def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.compressibility_drag_total.wave_drag (conditions, configuration, main_fuselage, propulsor, wing, num_engines, k, Sref_main, flag105)
 
def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.compressibility_drag_total.wave_drag_body_of_rev (total_length, Rmax, Sref)
 
def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.induced_drag_aircraft.induced_drag_aircraft (state, settings, geometry)
 
def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.compressibility_drag_total.lift_wave_drag (conditions, configuration, wing, Sref_main)
 
def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.compressibility_drag_total.drag_div (Mc_ii, wing, cl, Sref_main)
 
def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.miscellaneous_drag_aircraft.miscellaneous_drag_aircraft (state, settings, geometry)
 
def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.parasite_drag_propulsor.parasite_drag_propulsor (state, settings, geometry)
 
def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.wave_drag_body_of_rev.wave_drag_body_of_rev (total_length, Rmax, Sref)
 wave_drag_body_of_rev.py More...
 
def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.wave_drag_volume.wave_drag_volume (conditions, configuration, wing)
 
def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.parasite_drag_fuselage.parasite_drag_fuselage (state, settings, geometry)
 
def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.parasite_drag_nacelle.parasite_drag_nacelle (state, settings, nacelle)
 
def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.wave_drag_lift.wave_drag_lift (conditions, configuration, wing)
 
def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.wave_drag_volume_raymer.wave_drag_volume_raymer (vehicle, mach, scaling_factor)
 
def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.wave_drag_volume_sears_haack.wave_drag_volume_sears_haack (vehicle, mach, scaling_factor, sears_haack_type=3)
 

Detailed Description

Functions to perform low-fidelity drag calculations including supersonic.

@@ -157,26 +169,27 @@

-
Computes compressibility drag for full aircraft
+
Computes compressibility drag for full aircraft including volume drag
 
 Assumptions:
-Drag is only calculated for the wings, main fuselage, and propulsors
-Main fuselage must have tag 'fuselage'
-No lift on wings other than main wing
+None
 
 Source:
-adg.stanford.edu (Stanford AA241 A/B Course Notes)
+N/A
 
-Inputs:
+Inputs:   
+settings.
+  begin_drag_rise_mach_number                                    [Unitless]
+  end_drag_rise_mach_number                                      [Unitless]
+  peak_mach_number                                               [Unitless]
+  transonic_drag_multiplier                                      [Unitless]
+  volume_wave_drag_scaling                                       [Unitless]
 state.conditions.aerodynamics.lift_breakdown.compressible_wings  [Unitless]
 state.conditions.freestream.mach_number                          [Unitless]
+geometry.maximum_cross_sectional_area                            [m^2] (used in subfunctions)
+geometry.total_length                                            [m]   (used in subfunctions)
+geometry.reference_area                                          [m^2]
 geometry.wings                             
-geometry.fuselages['fuselage'].length_total                      [m]
-geometry.fuselages['fuselage'].effective_diameter                [m]
-geometry.propulsors[geometry.propulsors.keys()[0]].
-  nacelle_diameter                                               [m]
-  engine_length                                                  [m]
-  number_of_engines                                              [m]
 
 Outputs:
 total_compressibility_drag                                       [Unitless]
@@ -186,8 +199,8 @@ 

-

◆ drag_div()

+ +

◆ drag_div()

@@ -204,12 +217,6 @@

  wing, - - - -   - k, - @@ -235,7 +242,9 @@

-

◆ induced_drag_aircraft()

+ +

◆ lift_wave_drag()

- + - + - + - + + + + + + + @@ -285,24 +300,22 @@

-
Determines induced drag for the full aircraft
+
Determine lift wave drag for supersonic speeds
 
 Assumptions:
-Based on fits
+Basic fit
 
 Source:
-adg.stanford.edu (Stanford AA241 A/B Course Notes)
+http://aerodesign.stanford.edu/aircraftdesign/aircraftdesign.html (Stanford AA241 A/B Course Notes)
 
 Inputs:
-state.conditions.aerodynamics.lift_coefficient               [Unitless]
-state.conditions.aerodynamics.drag_breakdown.parasite.total  [Unitless]
-configuration.oswald_efficiency_factor                       [Unitless]
-configuration.viscous_lift_dependent_drag_factor             [Unitless]
-geometry.wings['main_wing'].span_efficiency                  [Unitless]
-geometry.wings['main_wing'].aspect_ratio                     [Unitless]
+conditions.freestream.mach_number [-]
+configuration                     (passed to another function)
+wing.areas.reference              [m^2]
+Sref_main                         [m^2] Main reference area
 
 Outputs:
-total_induced_drag                                           [Unitless]
+cd_c_l                            [-] Wave drag CD due to lift
 
 Properties Used:
 N/A
@@ -346,11 +359,11 @@ 

-

◆ parasite_drag_propulsor()

+ +

◆ parasite_drag_fuselage()

def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.induced_drag_aircraft.induced_drag_aircraft def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.compressibility_drag_total.lift_wave_drag (  state, conditions,
 settings, configuration,
 geometry wing,
 Sref_main 
- + @@ -394,94 +407,57 @@

-
Computes the parasite drag due to the propulsor
+
Computes the parasite drag due to the fuselage
 
 Assumptions:
 Basic fit
 
 Source:
-Raymer equation (pg 283 of Aircraft Design: A Conceptual Approach) (subsonic)
-http://adg.stanford.edu/aa241/drag/BODYFORMFACTOR.HTML (supersonic)
+http://aerodesign.stanford.edu/aircraftdesign/aircraftdesign.html (Stanford AA241 A/B Course Notes)
 
 Inputs:
 state.conditions.freestream.
   mach_number                                [Unitless]
   temperature                                [K]
   reynolds_number                            [Unitless]
-geometry.      
-  nacelle_diameter                           [m^2]
+settings.fuselage_parasite_drag_form_factor  [Unitless]
+geometry.fuselage.       
+  areas.front_projected                      [m^2]
   areas.wetted                               [m^2]
-  engine_length                              [m]
-state.conditions.aerodynamics.drag_breakdown.
-  compressible.main_wing.divergence_mach     [Unitless]
+  lengths.total                              [m]
+  effective_diameter                         [m]
 
 Outputs:
-propulsor_parasite_drag                      [Unitless]
+fuselage_parasite_drag                       [Unitless]
 
 Properties Used:
 N/A
 
-
-

◆ wave_drag()

+ +

◆ parasite_drag_nacelle()

def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.parasite_drag_propulsor.parasite_drag_propulsor def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.parasite_drag_fuselage.parasite_drag_fuselage (   state,
- + - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - + - + - + @@ -490,59 +466,56 @@

-
Use wave drag to determine compressibility drag for supersonic speeds
+
Computes the parasite drag due to the nacelle
 
 Assumptions:
 Basic fit
 
 Source:
-adg.stanford.edu (Stanford AA241 A/B Course Notes)
+Raymer equation (pg 283 of Aircraft Design: A Conceptual Approach) (subsonic)
+http://aerodesign.stanford.edu/aircraftdesign/drag/BODYFORMFACTOR.HTML (supersonic)
 
 Inputs:
-conditions.freestream.mach_number            [Unitless]
-configuration
-main_fuselage (unused)
-propulsor     (unused)
-wing.areas.reference                         [m^2]
-num_engines   (unused)
-k             (tag for wing)                 [String]
-Sref_main (main reference area)              [m^2]
-flag105   (check if calcs are for Mach 1.05) [Boolean]
-
-
+state.conditions.freestream.
+  mach_number                                [Unitless]
+  temperature                                [K]
+  reynolds_number                            [Unitless]
+geometry.      
+  nacelle.diameter                           [m^2]
+         areas.wetted                        [m^2]
+         length                              [m]
+ 
 Outputs:
-cd_c                    [Unitless]
-mcc                     [Unitless]
-MDiv                    [Unitless]
+nacelle_parasite_drag                      [Unitless]
 
 Properties Used:
 N/A
 
-
-

◆ wave_drag_body_of_rev() [1/2]

+ +

◆ wave_drag_lift()

def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.compressibility_drag_total.wave_drag def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.parasite_drag_nacelle.parasite_drag_nacelle (  conditions,
 configuration,
 main_fuselage,
 propulsor,
 wing,
 num_engines,
 k, state,
 Sref_main, settings,
 flag105 nacelle 
- + - + - + - + @@ -551,52 +524,53 @@

- -

wave_drag_body_of_rev.py

-

Created: Jun 2014, T. Macdonald Modified: Jan 2016, E. Botero

Use wave drag to determine compressibility drag a body of revolution
+
Computes wave drag due to lift
 
 Assumptions:
-Corrected Sear-Haack body 
+Main wing is the primary lift contributor
 
 Source:
-adg.stanford.edu (Stanford AA241 A/B Course Notes)
+Yoshida, Kenji. "Supersonic drag reduction technology in the scaled supersonic 
+experimental airplane project by JAXA."
 
 Inputs:
-total_length                    [m]
-Rmax (max radius)               [m]
-Sref (main wing reference area) [m^2]
+conditions.freestream.mach_number        [Unitless]
+conditions.aerodynamics.lift_coefficient [Unitless]
+wing.spans.projected                     [m]
+wing.total_length                        [m]
+wing.aspect_ratio                        [-]
 
 Outputs:
-wave_drag_body_of_rev*1.15      [Unitless]
+wave_drag_lift                           [Unitless]
 
 Properties Used:
 N/A
 
-
-

◆ wave_drag_body_of_rev() [2/2]

+ +

◆ wave_drag_volume_raymer()

def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.wave_drag_body_of_rev.wave_drag_body_of_rev def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.wave_drag_lift.wave_drag_lift (  total_length, conditions,
 Rmax, configuration,
 Sref wing 
- + - + - + - + @@ -605,50 +579,58 @@

-
Use wave drag to determine compressibility drag a body of revolution
+
Computes the volume drag
 
 Assumptions:
-Corrected Sear-Haack body 
+Basic fit
 
 Source:
-adg.stanford.edu (Stanford AA241 A/B Course Notes)
+D. Raymer, Aircraft Design: A Conceptual Approach, Fifth Ed. pg. 448-449
 
 Inputs:
-total_length                    [m]
-Rmax (max radius)               [m]
-Sref (main wing reference area) [m^2]
-
+vehicle.
+  wings.main_wing.sweeps.leading_edge [rad]
+  total_length                        [m]
+  maximum_cross_sectional_area        [m^2]
+  reference_area                      [m^2]
+  
 Outputs:
-wave_drag_body_of_rev*1.15      [Unitless]
+vehicle_wave_drag                     [Unitless]
 
 Properties Used:
 N/A
 
-
-

◆ wave_drag_volume()

+ +

◆ wave_drag_volume_sears_haack()

def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.compressibility_drag_total.wave_drag_body_of_rev def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.wave_drag_volume_raymer.wave_drag_volume_raymer (  total_length, vehicle,
 Rmax, mach,
 Sref scaling_factor 
- + - + - + - + + + + + + + @@ -657,22 +639,23 @@

-
Computes wave drag due to volume
+
Computes the volume drag
 
 Assumptions:
-Simplified equations for wing
+Basic fit
 
 Source:
-http://adg.stanford.edu/aa241/drag/ssdragcalc.html
+Sieron, Thomas R., et al. Procedures and design data for the formulation of aircraft 
+configurations. WRIGHT LAB WRIGHT-PATTERSON AFB OH, 1993. Page B-3
 
 Inputs:
-conditions.freestream.mach_number        [Unitless]
-wing.thickness_to_chord                  [Unitless]
-wing.total_length                        [m]
-wing.areas.reference                     [m^2]
-
+vehicle.
+  total_length                        [m]
+  maximum_cross_sectional_area        [m^2]
+  reference_area                      [m^2]
+  
 Outputs:
-wave_drag_volume                         [Unitless]
+vehicle_wave_drag                     [Unitless]
 
 Properties Used:
 N/A
@@ -686,7 +669,7 @@ 

Generated by - doxygen 1.8.14 + doxygen 1.8.15 diff --git a/doxygen/group__Methods-Aerodynamics-Supersonic__Zero-Drag.js b/doxygen/group__Methods-Aerodynamics-Supersonic__Zero-Drag.js index 1f56268e..d1ffe53e 100644 --- a/doxygen/group__Methods-Aerodynamics-Supersonic__Zero-Drag.js +++ b/doxygen/group__Methods-Aerodynamics-Supersonic__Zero-Drag.js @@ -1,12 +1,19 @@ var group__Methods_Aerodynamics_Supersonic__Zero_Drag = [ + [ "Cubic_Spline_Blender", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1Supersonic__Zero_1_1Drag_1_1Cubic__Spline__Blender_1_1Cubic__Spline__Blender.html", [ + [ "__init__", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1Supersonic__Zero_1_1Drag_1_1Cubic__Spline__Blender_1_1Cubic__Spline__Blender.html#afff7a719089ea8178f152d196ea2ec0f", null ], + [ "compute", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1Supersonic__Zero_1_1Drag_1_1Cubic__Spline__Blender_1_1Cubic__Spline__Blender.html#aeb32772385d70b536506f803147dc5c2", null ], + [ "eta_transform", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1Supersonic__Zero_1_1Drag_1_1Cubic__Spline__Blender_1_1Cubic__Spline__Blender.html#a6017f424807c71a3deab1c81eef3de17", null ], + [ "x_end", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1Supersonic__Zero_1_1Drag_1_1Cubic__Spline__Blender_1_1Cubic__Spline__Blender.html#ad4de563711c610b928bccdb2cf3228d5", null ], + [ "x_start", "classSUAVE_1_1Methods_1_1Aerodynamics_1_1Supersonic__Zero_1_1Drag_1_1Cubic__Spline__Blender_1_1Cubic__Spline__Blender.html#a7f59c602476376ec2264aafb29085321", null ] + ] ], [ "compressibility_drag_total", "group__Methods-Aerodynamics-Supersonic__Zero-Drag.html#ga219e16acafc09082cf24afad213e82a3", null ], - [ "drag_div", "group__Methods-Aerodynamics-Supersonic__Zero-Drag.html#gabe93280aa4a398fe7f4a846f320b6cfc", null ], - [ "induced_drag_aircraft", "group__Methods-Aerodynamics-Supersonic__Zero-Drag.html#gab4d68efaf1c50a05d83f084e6fec811f", null ], + [ "drag_div", "group__Methods-Aerodynamics-Supersonic__Zero-Drag.html#ga234ba915950ed8f64df047c0a9d3cb54", null ], + [ "lift_wave_drag", "group__Methods-Aerodynamics-Supersonic__Zero-Drag.html#ga7574bcf470833883b3eb1698af863358", null ], [ "miscellaneous_drag_aircraft", "group__Methods-Aerodynamics-Supersonic__Zero-Drag.html#ga857987b93648989ca62534896beef377", null ], - [ "parasite_drag_propulsor", "group__Methods-Aerodynamics-Supersonic__Zero-Drag.html#ga7d6bc8c6cc09e29a2ad852bea76a7318", null ], - [ "wave_drag", "group__Methods-Aerodynamics-Supersonic__Zero-Drag.html#ga72a66acea89fccf56d981b5e0c50ff91", null ], - [ "wave_drag_body_of_rev", "group__Methods-Aerodynamics-Supersonic__Zero-Drag.html#ga9e79d1f0b6914e56f64ca54283e787d2", null ], - [ "wave_drag_body_of_rev", "group__Methods-Aerodynamics-Supersonic__Zero-Drag.html#gac6d270a8abdc9f999bcbd75cfaf8a498", null ], - [ "wave_drag_volume", "group__Methods-Aerodynamics-Supersonic__Zero-Drag.html#ga610ad17cff3812c5993409c65a40df99", null ] + [ "parasite_drag_fuselage", "group__Methods-Aerodynamics-Supersonic__Zero-Drag.html#ga6bc7488251858a1e1526f90cb0ff59cc", null ], + [ "parasite_drag_nacelle", "group__Methods-Aerodynamics-Supersonic__Zero-Drag.html#ga7f302a3327b02d452296d02fd4fba8bb", null ], + [ "wave_drag_lift", "group__Methods-Aerodynamics-Supersonic__Zero-Drag.html#ga725df02201031e5d83aa0f62ad26acfb", null ], + [ "wave_drag_volume_raymer", "group__Methods-Aerodynamics-Supersonic__Zero-Drag.html#ga970bdfcb873ebeef93ccb28b579da4a3", null ], + [ "wave_drag_volume_sears_haack", "group__Methods-Aerodynamics-Supersonic__Zero-Drag.html#ga100f5e320631d6231a7ad524621f4799", null ] ]; \ No newline at end of file diff --git a/doxygen/group__Methods-Aerodynamics-Supersonic__Zero-Lift.html b/doxygen/group__Methods-Aerodynamics-Supersonic__Zero-Lift.html deleted file mode 100644 index 7f1a560c..00000000 --- a/doxygen/group__Methods-Aerodynamics-Supersonic__Zero-Lift.html +++ /dev/null @@ -1,239 +0,0 @@ - - - - - - - -SUAVE: Lift - - - - - - - - - - - - - - - -
-
-

def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.wave_drag_volume.wave_drag_volume def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Drag.wave_drag_volume_sears_haack.wave_drag_volume_sears_haack (  conditions, vehicle,
 configuration, mach,
 wing scaling_factor,
 sears_haack_type = 3 
- - - - - - - -
-
SUAVE -  1.1.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
-
- - - -
-
- -
-
-
- -
- -
-
- - -
- -
- - -
- -

Functions to perform low-fidelity lift calculations for supersonics. -More...

- - - - - - -

-Functions

def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Lift.vortex_lift.vortex_lift (state, settings, geometry)
 
def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Lift.wing_compressibility.wing_compressibility (state, settings, geometry)
 
-

Detailed Description

-

Functions to perform low-fidelity lift calculations for supersonics.

-

Function Documentation

- -

◆ vortex_lift()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Lift.vortex_lift.vortex_lift ( state,
 settings,
 geometry 
)
-
-
Computes vortex lift
-
-Assumptions:
-wing capable of vortex lift
-
-Source:
-http://adg.stanford.edu/aa241/highlift/sstclmax.html
-
-Inputs:
-states.conditions.
-  freestream.mach_number              [-]
-  aerodynamics.angle_of_attack        [radians]
-  aerodynamics.lift_coefficient       [-]
-geometry.wings.*.aspect_ratio         [Unitless]
-geometry.wings.*.sweeps.quarter_chord [radians]
-
-Outputs:
-state.conditions.aerodynamics.
-  lift_breakdown.vortex_lift          [-] CL due to vortex lift
-wings_lift                            [-] Total CL at this point
-
-Properties Used:
-N/A
-
-
-
- -

◆ wing_compressibility()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Aerodynamics.Supersonic_Zero.Lift.wing_compressibility.wing_compressibility ( state,
 settings,
 geometry 
)
-
-
Corrects a wings lift based on compressibility, allow supersonic mach number
-
-Assumptions:
-wing capable of vortex lift
-
-Source:
-https://stanford.edu/~cantwell/AA200_Course_Material/AA200_Course_Notes/
-
-Inputs:
-settings.fuselage_lift_correction  [-]
-state.conditions.
-  freestream.mach_number           [-]
-  aerodynamics.angle_of_attack     [radians]
-  aerodynamics.lift_coefficient    [-]
-
-Outputs:
-state.conditions.aerodynamics.
-  lift_breakdown.compressible_wings [-] CL for the wings
-  lift_coefficient                  [-]
-wings_lift_comp                     [-]
-
-Properties Used:
-N/A
-
-
-
-
-
- - - - diff --git a/doxygen/group__Methods-Aerodynamics-Supersonic__Zero-Lift.js b/doxygen/group__Methods-Aerodynamics-Supersonic__Zero-Lift.js deleted file mode 100644 index e807257a..00000000 --- a/doxygen/group__Methods-Aerodynamics-Supersonic__Zero-Lift.js +++ /dev/null @@ -1,5 +0,0 @@ -var group__Methods_Aerodynamics_Supersonic__Zero_Lift = -[ - [ "vortex_lift", "group__Methods-Aerodynamics-Supersonic__Zero-Lift.html#gaf1caf451d7ebd8f7449065933f6e1bf5", null ], - [ "wing_compressibility", "group__Methods-Aerodynamics-Supersonic__Zero-Lift.html#ga16916def179bf2c8fb842f664aaefd36", null ] -]; \ No newline at end of file diff --git a/doxygen/group__Methods-Aerodynamics-Supersonic__Zero.html b/doxygen/group__Methods-Aerodynamics-Supersonic__Zero.html index 60231444..07564c1d 100644 --- a/doxygen/group__Methods-Aerodynamics-Supersonic__Zero.html +++ b/doxygen/group__Methods-Aerodynamics-Supersonic__Zero.html @@ -1,9 +1,9 @@ - + - + SUAVE: Supersonic_Zero @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@

- +
@@ -73,7 +78,9 @@

@@ -106,9 +113,6 @@  Drag  Functions to perform low-fidelity drag calculations including supersonic.
  - Lift - Functions to perform low-fidelity lift calculations for supersonics.

Detailed Description

Functions to perform low-fidelity calculations including supersonics.

@@ -119,7 +123,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/group__Methods-Aerodynamics-Supersonic__Zero.js b/doxygen/group__Methods-Aerodynamics-Supersonic__Zero.js index 85073599..b6692651 100644 --- a/doxygen/group__Methods-Aerodynamics-Supersonic__Zero.js +++ b/doxygen/group__Methods-Aerodynamics-Supersonic__Zero.js @@ -1,5 +1,4 @@ var group__Methods_Aerodynamics_Supersonic__Zero = [ - [ "Drag", "group__Methods-Aerodynamics-Supersonic__Zero-Drag.html", "group__Methods-Aerodynamics-Supersonic__Zero-Drag" ], - [ "Lift", "group__Methods-Aerodynamics-Supersonic__Zero-Lift.html", "group__Methods-Aerodynamics-Supersonic__Zero-Lift" ] + [ "Drag", "group__Methods-Aerodynamics-Supersonic__Zero-Drag.html", "group__Methods-Aerodynamics-Supersonic__Zero-Drag" ] ]; \ No newline at end of file diff --git a/doxygen/group__Methods-Aerodynamics.html b/doxygen/group__Methods-Aerodynamics.html index 98f19194..f9c66dba 100644 --- a/doxygen/group__Methods-Aerodynamics.html +++ b/doxygen/group__Methods-Aerodynamics.html @@ -1,9 +1,9 @@ - + - + SUAVE: Aerodynamics @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@
- +
@@ -73,7 +78,9 @@
@@ -106,12 +113,17 @@  AERODAS  Functions to perform calculations according to AERODAS models.
  + Airfoil_Panel_Method +   AVL  Functions to AVL calculations.
   Common  These are methods that are used by several analyses.
  + Gas_Dymamics + Gas Dynamics methods that are directly specified by analyses.
+   Fidelity_Zero  Functions to perform low-fidelity calculations.
  @@ -134,7 +146,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/group__Methods-Aerodynamics.js b/doxygen/group__Methods-Aerodynamics.js index 94fe6ead..1fa4270b 100644 --- a/doxygen/group__Methods-Aerodynamics.js +++ b/doxygen/group__Methods-Aerodynamics.js @@ -1,8 +1,10 @@ var group__Methods_Aerodynamics = [ [ "AERODAS", "group__Methods-Aerodynamics-AERODAS.html", "group__Methods-Aerodynamics-AERODAS" ], + [ "Airfoil_Panel_Method", "group__Methods-Aerodynamics-Airfoil__Panel__Method.html", "group__Methods-Aerodynamics-Airfoil__Panel__Method" ], [ "AVL", "group__Methods-Aerodynamics-AVL.html", "group__Methods-Aerodynamics-AVL" ], [ "Common", "group__Methods-Aerodynamics-Common.html", "group__Methods-Aerodynamics-Common" ], + [ "Gas_Dymamics", "group__Methods-Aerodynamics-Common-Gas__Dynamics.html", "group__Methods-Aerodynamics-Common-Gas__Dynamics" ], [ "Fidelity_Zero", "group__Methods-Aerodynamics-Fidelity__Zero.html", "group__Methods-Aerodynamics-Fidelity__Zero" ], [ "Lifting_Line", "group__Methods-Aerodynamics-Lifting__Line.html", null ], [ "OpenVSP_Wave_Drag", "group__Methods-Aerodynamics-OpenVSP__Wave__Drag.html", "group__Methods-Aerodynamics-OpenVSP__Wave__Drag" ], diff --git a/doxygen/group__Methods-Center__of__Gravity.html b/doxygen/group__Methods-Center__of__Gravity.html index 616200aa..5007bd13 100644 --- a/doxygen/group__Methods-Center__of__Gravity.html +++ b/doxygen/group__Methods-Center__of__Gravity.html @@ -1,9 +1,9 @@ - + - + SUAVE: Center_of_Gravity @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -103,10 +110,12 @@ - - - - + + + + + + @@ -114,14 +123,14 @@

Detailed Description

Description.

Function Documentation

- -

◆ compute_aircraft_center_of_gravity()

+ +

◆ compute_component_centers_of_gravity()

Functions

def SUAVE.Methods.Center_of_Gravity.compute_aircraft_center_of_gravity.compute_aircraft_center_of_gravity (vehicle, nose_load_fraction=.06)
 
def SUAVE.Methods.Center_of_Gravity.compute_component_centers_of_gravity.compute_component_centers_of_gravity (vehicle, compute_propulsor_origin=False)
 
def SUAVE.Methods.Center_of_Gravity.compute_component_centers_of_gravity.compute_component_centers_of_gravity (vehicle, nose_load=0.06)
 
def SUAVE.Methods.Center_of_Gravity.compute_fuel_center_of_gravity_longitudinal_range.plot_cg_map (masses, cg_mins, cg_maxes, empty_mass=0, empty_cg=0, units='metric', special_length=None, fig_title="Available Fuel CG Distribution")
 
def SUAVE.Methods.Center_of_Gravity.compute_fuel_center_of_gravity_longitudinal_range.compute_fuel_center_of_gravity_longitudinal_range (vehicle)
 
def SUAVE.Methods.Center_of_Gravity.compute_mission_center_of_gravity.compute_mission_center_of_gravity (vehicle, mission_fuel_weight)
 compute_mission_center_of_gravity.py More...
 
- + @@ -130,7 +139,7 @@

- + @@ -139,66 +148,62 @@

-
This computes the CG for the vehicle from the assigned vehicle mass 
-properties and locations
-    
+
computes the CG of all of the vehicle components based on correlations 
+from AA241
+
 Assumptions:
 None
-    
+
 Source:
-N/A
-    
+AA 241 Notes
+
 Inputs:
 vehicle
-nose_load_fraction
-    
+
 Outputs:
-vehicle.mass_properties.center_of_gravity      [meters]
-    
+None
+
 Properties Used:
 N/A
 
-
-

◆ compute_component_centers_of_gravity()

+ +

◆ compute_fuel_center_of_gravity_longitudinal_range()

def SUAVE.Methods.Center_of_Gravity.compute_aircraft_center_of_gravity.compute_aircraft_center_of_gravity def SUAVE.Methods.Center_of_Gravity.compute_component_centers_of_gravity.compute_component_centers_of_gravity (   vehicle,  nose_load_fraction = .06 nose_load = 0.06 
- + - - - - - - - - - + - -
def SUAVE.Methods.Center_of_Gravity.compute_component_centers_of_gravity.compute_component_centers_of_gravity def SUAVE.Methods.Center_of_Gravity.compute_fuel_center_of_gravity_longitudinal_range.compute_fuel_center_of_gravity_longitudinal_range (  vehicle,
 compute_propulsor_origin = False 
vehicle) )
-
computes the CG of all of the vehicle components based on correlations 
-from AA241
+
Computes the possible longitudinal center of gravity given
+a set of fuel tanks (includes fuel weight only)
 
 Assumptions:
-None
+Fuel tanks are only in the fuselage/wings
 
 Source:
-AA 241 Notes
+N/A
 
 Inputs:
-vehicle
+vehicle.wings.*.Fuel_Tanks.mass_properties.
+  center_of_gravity       [m]
+  fuel_mass_when_full     [kg]
+vehicle.fuselages.*.Fuel_Tanks.mass_properties.
+  center_of_gravity       [m]
+  fuel_mass_when_full     [kg]
 
 Outputs:
-None
+fuel_masses               [kg] (these are arrays spanning the possible masses)
+min_cg                    [m]
+max_cg                    [m]
 
 Properties Used:
 N/A
@@ -248,6 +253,98 @@ 

+

◆ plot_cg_map()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Center_of_Gravity.compute_fuel_center_of_gravity_longitudinal_range.plot_cg_map ( masses,
 cg_mins,
 cg_maxes,
 empty_mass = 0,
 empty_cg = 0,
 units = 'metric',
 special_length = None,
 fig_title = "Available Fuel CG Distribution" 
)
+
+
Plot possible longitudinal cg positions for the fuel (or full vehicle
+if empty mass is given)
+
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+  Fuel only:
+    masses     [kg]
+    cg_mins    [m]
+    cg_maxes   [m]
+
+  Vehicle Properties (optional):
+    empty_mass [kg]
+    empty_cg   [m]
+
+Outputs:
+fig      (figure handle)
+axes     (axis handle)
+cg_mins  [m]  (incl. vehicle if vehicle properties specified)
+cg_maxes [m]  (incl. vehicle if vehicle properties specified)
+masses   [kg] (incl. vehicle if vehicle properties specified)
+
 Properties Used:
 N/A
 
@@ -260,7 +357,7 @@

Generated by - doxygen 1.8.14 + doxygen 1.8.15

diff --git a/doxygen/group__Methods-Center__of__Gravity.js b/doxygen/group__Methods-Center__of__Gravity.js index 71ecfaba..4647f539 100644 --- a/doxygen/group__Methods-Center__of__Gravity.js +++ b/doxygen/group__Methods-Center__of__Gravity.js @@ -1,6 +1,7 @@ var group__Methods_Center__of__Gravity = [ - [ "compute_aircraft_center_of_gravity", "group__Methods-Center__of__Gravity.html#gab07340ed39f8011a722913b0359beec9", null ], - [ "compute_component_centers_of_gravity", "group__Methods-Center__of__Gravity.html#gaa3b24268349627cb2f3db8131229b94f", null ], - [ "compute_mission_center_of_gravity", "group__Methods-Center__of__Gravity.html#gad04a471f2c790cce693dab0107e3f82b", null ] + [ "compute_component_centers_of_gravity", "group__Methods-Center__of__Gravity.html#gae312c0bb7a3b272dedf760319d66bd14", null ], + [ "compute_fuel_center_of_gravity_longitudinal_range", "group__Methods-Center__of__Gravity.html#gaa80111cbbe76730ccddcbba6b613240e", null ], + [ "compute_mission_center_of_gravity", "group__Methods-Center__of__Gravity.html#gad04a471f2c790cce693dab0107e3f82b", null ], + [ "plot_cg_map", "group__Methods-Center__of__Gravity.html#gace4d51359aadacc430f3d2240e709180", null ] ]; \ No newline at end of file diff --git a/doxygen/group__Methods-Cooling-Cryogen-Consumption.html b/doxygen/group__Methods-Cooling-Cryogen-Consumption.html new file mode 100644 index 00000000..d8203d36 --- /dev/null +++ b/doxygen/group__Methods-Cooling-Cryogen-Consumption.html @@ -0,0 +1,120 @@ + + + + + + + +SUAVE: Consumption + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
Consumption
+
+
+ +

Functions to evaluate the use of cryogen to provide cooling power. +More...

+

Functions to evaluate the use of cryogen to provide cooling power.

+
+
+ + + + diff --git a/doxygen/group__Methods-Cooling-Cryogen.html b/doxygen/group__Methods-Cooling-Cryogen.html new file mode 100644 index 00000000..f9efbdbf --- /dev/null +++ b/doxygen/group__Methods-Cooling-Cryogen.html @@ -0,0 +1,130 @@ + + + + + + + +SUAVE: Cryogen + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
Cryogen
+
+
+ +

Cooling by liquid (or gaseous) cryogen. +More...

+ + + + + +

+Modules

 Consumption
 Functions to evaluate the use of cryogen to provide cooling power.
 
+

Detailed Description

+

Cooling by liquid (or gaseous) cryogen.

+
+
+ + + + diff --git a/doxygen/group__Methods-Cooling-Cryogen.js b/doxygen/group__Methods-Cooling-Cryogen.js new file mode 100644 index 00000000..12ad27e1 --- /dev/null +++ b/doxygen/group__Methods-Cooling-Cryogen.js @@ -0,0 +1,4 @@ +var group__Methods_Cooling_Cryogen = +[ + [ "Consumption", "group__Methods-Cooling-Cryogen-Consumption.html", null ] +]; \ No newline at end of file diff --git a/doxygen/group__Methods-Cooling.html b/doxygen/group__Methods-Cooling.html new file mode 100644 index 00000000..5dd312ca --- /dev/null +++ b/doxygen/group__Methods-Cooling.html @@ -0,0 +1,130 @@ + + + + + + + +SUAVE: Cooling + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
Cooling
+
+
+ +

Cooling methods contain the functions for cryogenic systems such as Cryocoolers and cryogen cooling. +More...

+ + + + + +

+Modules

 Cryogen
 Cooling by liquid (or gaseous) cryogen.
 
+

Detailed Description

+

Cooling methods contain the functions for cryogenic systems such as Cryocoolers and cryogen cooling.

+
+
+ + + + diff --git a/doxygen/group__Methods-Cooling.js b/doxygen/group__Methods-Cooling.js new file mode 100644 index 00000000..cbd6042f --- /dev/null +++ b/doxygen/group__Methods-Cooling.js @@ -0,0 +1,4 @@ +var group__Methods_Cooling = +[ + [ "Cryogen", "group__Methods-Cooling-Cryogen.html", "group__Methods-Cooling-Cryogen" ] +]; \ No newline at end of file diff --git a/doxygen/group__Methods-Costs-Industrial__Costs.html b/doxygen/group__Methods-Costs-Industrial__Costs.html index b9eca1bd..118cbbbd 100644 --- a/doxygen/group__Methods-Costs-Industrial__Costs.html +++ b/doxygen/group__Methods-Costs-Industrial__Costs.html @@ -1,9 +1,9 @@ - + - + SUAVE: Industrial Costs @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@
- +

@@ -73,7 +78,9 @@
diff --git a/doxygen/group__Methods-Costs-Industrial__Costs.js b/doxygen/group__Methods-Costs-Industrial__Costs.js index 78cd4420..f71ea57d 100644 --- a/doxygen/group__Methods-Costs-Industrial__Costs.js +++ b/doxygen/group__Methods-Costs-Industrial__Costs.js @@ -1,7 +1,7 @@ var group__Methods_Costs_Industrial__Costs = [ [ "call_print", "group__Methods-Costs-Industrial__Costs.html#ga3d2583d564f60ad9654df204cef7e11a", null ], - [ "compute_industrial_costs", "group__Methods-Costs-Industrial__Costs.html#ga35a25c347a4527853d123de555e5cd38", null ], + [ "compute_industrial_costs", "group__Methods-Costs-Industrial__Costs.html#ga06d9461666e8e05bfe623f4dec03900d", null ], [ "distribute_non_recurring_cost", "group__Methods-Costs-Industrial__Costs.html#ga227d25bf208e5c3af05ea5a76e853278", null ], [ "estimate_escalation_factor", "group__Methods-Costs-Industrial__Costs.html#ga1370c8ef946e4c1e45e81b7d2f5d4139", null ], [ "estimate_hourly_rates", "group__Methods-Costs-Industrial__Costs.html#ga65197d1d30198c75c0676e6f507c11c1", null ] diff --git a/doxygen/group__Methods-Costs-Operating__Costs.html b/doxygen/group__Methods-Costs-Operating__Costs.html index a8821a8a..97c1102e 100644 --- a/doxygen/group__Methods-Costs-Operating__Costs.html +++ b/doxygen/group__Methods-Costs-Operating__Costs.html @@ -1,9 +1,9 @@ - + - + SUAVE: Operating Costs @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -135,7 +142,7 @@

Generated by - doxygen 1.8.14 + doxygen 1.8.15

diff --git a/doxygen/group__Methods-Costs.html b/doxygen/group__Methods-Costs.html index 73edbb20..a1412163 100644 --- a/doxygen/group__Methods-Costs.html +++ b/doxygen/group__Methods-Costs.html @@ -1,9 +1,9 @@ - + - + SUAVE: Costs @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -120,7 +127,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/group__Methods-Flight__Dynamics-Dynamic__Stability-Approximations.html b/doxygen/group__Methods-Flight__Dynamics-Dynamic__Stability-Approximations.html index fbc2fa1e..dc11b42c 100644 --- a/doxygen/group__Methods-Flight__Dynamics-Dynamic__Stability-Approximations.html +++ b/doxygen/group__Methods-Flight__Dynamics-Dynamic__Stability-Approximations.html @@ -1,9 +1,9 @@ - + - + SUAVE: Approximations @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -594,7 +601,7 @@

Generated by - doxygen 1.8.14 + doxygen 1.8.15

diff --git a/doxygen/group__Methods-Flight__Dynamics-Dynamic__Stability-Full__Linearized__Equations-Supporting__Functions.html b/doxygen/group__Methods-Flight__Dynamics-Dynamic__Stability-Full__Linearized__Equations-Supporting__Functions.html index 81d85ede..3a2f2b77 100644 --- a/doxygen/group__Methods-Flight__Dynamics-Dynamic__Stability-Full__Linearized__Equations-Supporting__Functions.html +++ b/doxygen/group__Methods-Flight__Dynamics-Dynamic__Stability-Full__Linearized__Equations-Supporting__Functions.html @@ -1,9 +1,9 @@ - + - + SUAVE: Supporting_Functions @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -858,7 +865,7 @@

Generated by - doxygen 1.8.14 + doxygen 1.8.15

diff --git a/doxygen/group__Methods-Flight__Dynamics-Dynamic__Stability-Full__Linearized__Equations.html b/doxygen/group__Methods-Flight__Dynamics-Dynamic__Stability-Full__Linearized__Equations.html index 3d6860f0..7fa7cb9f 100644 --- a/doxygen/group__Methods-Flight__Dynamics-Dynamic__Stability-Full__Linearized__Equations.html +++ b/doxygen/group__Methods-Flight__Dynamics-Dynamic__Stability-Full__Linearized__Equations.html @@ -1,9 +1,9 @@ - + - + SUAVE: Full_Linearized_Equations @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -447,7 +454,7 @@

Generated by - doxygen 1.8.14 + doxygen 1.8.15

diff --git a/doxygen/group__Methods-Flight__Dynamics-Dynamic__Stability.html b/doxygen/group__Methods-Flight__Dynamics-Dynamic__Stability.html index 554ec237..79b0717e 100644 --- a/doxygen/group__Methods-Flight__Dynamics-Dynamic__Stability.html +++ b/doxygen/group__Methods-Flight__Dynamics-Dynamic__Stability.html @@ -1,9 +1,9 @@ - + - + SUAVE: Dynamic_Stability @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -113,7 +120,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/group__Methods-Flight__Dynamics-Static__Stability-Approximations-Supporting__Functions.html b/doxygen/group__Methods-Flight__Dynamics-Static__Stability-Approximations-Supporting__Functions.html index f7232c55..6cc44439 100644 --- a/doxygen/group__Methods-Flight__Dynamics-Static__Stability-Approximations-Supporting__Functions.html +++ b/doxygen/group__Methods-Flight__Dynamics-Static__Stability-Approximations-Supporting__Functions.html @@ -1,9 +1,9 @@ - + - + SUAVE: Supporting_Functions @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -102,6 +109,8 @@ Functions

def SUAVE.Methods.Flight_Dynamics.Static_Stability.Approximations.Supporting_Functions.convert_sweep.convert_sweep (wing, old_ref_chord_fraction=0.0, new_ref_chord_fraction=0.25)   +def SUAVE.Methods.Flight_Dynamics.Static_Stability.Approximations.Supporting_Functions.convert_sweep.convert_sweep_segments (old_sweep, seg_a, seg_b, wing, old_ref_chord_fraction=0.0, new_ref_chord_fraction=0.25) +  def SUAVE.Methods.Flight_Dynamics.Static_Stability.Approximations.Supporting_Functions.extend_to_ref_area.extend_to_ref_area (surface)   def SUAVE.Methods.Flight_Dynamics.Static_Stability.Approximations.Supporting_Functions.trapezoid_ac_x.trapezoid_ac_x (wing) @@ -175,6 +184,101 @@

+

◆ convert_sweep_segments()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Flight_Dynamics.Static_Stability.Approximations.Supporting_Functions.convert_sweep.convert_sweep_segments ( old_sweep,
 seg_a,
 seg_b,
 wing,
 old_ref_chord_fraction = 0.0,
 new_ref_chord_fraction = 0.25 
)
+
+
This method converts the sweep of a section of a wing between two segments 
+to refer to a new chord fraction. More specifically, it converts the inboard 
+segment's (seg_a's) outboard sweep. Defaults to converting from leading-edge sweep to 
+quarter-chord sweep.
+
+Assumptions:
+    Assumes a simple trapezoidal section shape. If the input section does
+    not have a simple trapezoidal shape, this function will convert sweeps
+    for an equivalent trapezoid having the same reference sweep, aspect 
+    ratio, and taper ratio.
+
+Source:
+    Unknown
+
+Inputs:
+    old_sweep - sweep angle to convert
+
+    seg_a and seg_b - two Segment() objects with:
+        root_chord_percent    - percent of the wing's root chord
+
+    wing - a data dictionary with the fields:
+        chords.root  - root chord                              [m]
+        span         - wingspan                                [m]
+        symmetric    - symmetry                                [boolean]
+ 
+    old_ref_chord_fraction - a float value between 0 and 1.0 that 
+                             tells what fraction of the local chord
+                             the sweep line follows. (For example, 
+                             a value of 0.25 refers to quarter-chord
+                             sweep
+    new_ref_chord_fraction - a float value between 0 and 1.0 that
+                             tells what fraction of the local chord
+                             is the new reference for sweep.
+
+Outputs:
+    output - a single float value, new_sweep, which is the sweep
+             angle referenced to the new_ref_chord_fraction.
+
 Defaults:
     Defaults to converting from leading edge sweep to quater-chord sweep.
     
@@ -335,7 +439,7 @@ 

Generated by - doxygen 1.8.14 + doxygen 1.8.15

diff --git a/doxygen/group__Methods-Flight__Dynamics-Static__Stability-Approximations-Supporting__Functions.js b/doxygen/group__Methods-Flight__Dynamics-Static__Stability-Approximations-Supporting__Functions.js index 58170885..51e5b212 100644 --- a/doxygen/group__Methods-Flight__Dynamics-Static__Stability-Approximations-Supporting__Functions.js +++ b/doxygen/group__Methods-Flight__Dynamics-Static__Stability-Approximations-Supporting__Functions.js @@ -1,6 +1,7 @@ var group__Methods_Flight__Dynamics_Static__Stability_Approximations_Supporting__Functions = [ [ "convert_sweep", "group__Methods-Flight__Dynamics-Static__Stability-Approximations-Supporting__Functions.html#ga73fbf404355311e90e887d2b16718526", null ], + [ "convert_sweep_segments", "group__Methods-Flight__Dynamics-Static__Stability-Approximations-Supporting__Functions.html#ga79a7edc3abca2ab684e3ffce60b38cfc", null ], [ "extend_to_ref_area", "group__Methods-Flight__Dynamics-Static__Stability-Approximations-Supporting__Functions.html#ga1466483a340b19cb9952443921532dcc", null ], [ "trapezoid_ac_x", "group__Methods-Flight__Dynamics-Static__Stability-Approximations-Supporting__Functions.html#gac364b994a3b8fddd8e32535b7b47956b", null ], [ "trapezoid_mac", "group__Methods-Flight__Dynamics-Static__Stability-Approximations-Supporting__Functions.html#gaa93cc36245fbf7b5abd89bbfe4af0120", null ] diff --git a/doxygen/group__Methods-Flight__Dynamics-Static__Stability-Approximations-Tube__Wing.html b/doxygen/group__Methods-Flight__Dynamics-Static__Stability-Approximations-Tube__Wing.html index 507ff224..64ea95f6 100644 --- a/doxygen/group__Methods-Flight__Dynamics-Static__Stability-Approximations-Tube__Wing.html +++ b/doxygen/group__Methods-Flight__Dynamics-Static__Stability-Approximations-Tube__Wing.html @@ -1,9 +1,9 @@ - + - + SUAVE: Tube_Wing @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@
- +
@@ -73,7 +78,9 @@
@@ -239,7 +246,7 @@

Generated by - doxygen 1.8.14 + doxygen 1.8.15

diff --git a/doxygen/group__Methods-Flight__Dynamics-Static__Stability-Approximations.html b/doxygen/group__Methods-Flight__Dynamics-Static__Stability-Approximations.html index e1597217..4c8844a1 100644 --- a/doxygen/group__Methods-Flight__Dynamics-Static__Stability-Approximations.html +++ b/doxygen/group__Methods-Flight__Dynamics-Static__Stability-Approximations.html @@ -1,9 +1,9 @@ - + - + SUAVE: Approximations @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -177,7 +184,7 @@

Generated by - doxygen 1.8.14 + doxygen 1.8.15

diff --git a/doxygen/group__Methods-Flight__Dynamics-Static__Stability.html b/doxygen/group__Methods-Flight__Dynamics-Static__Stability.html index ae647beb..8e6d47cd 100644 --- a/doxygen/group__Methods-Flight__Dynamics-Static__Stability.html +++ b/doxygen/group__Methods-Flight__Dynamics-Static__Stability.html @@ -1,9 +1,9 @@ - + - + SUAVE: Static_Stability @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -92,7 +99,8 @@
Static_Stability
@@ -102,8 +110,63 @@ Modules

 Approximations   + + + +

+Functions

def SUAVE.Methods.Flight_Dynamics.Static_Stability.compute_aero_derivatives.compute_aero_derivatives (segment)
 

Detailed Description

+

Function Documentation

+ +

◆ compute_aero_derivatives()

+ +
+
+ + + + + + + + +
def SUAVE.Methods.Flight_Dynamics.Static_Stability.compute_aero_derivatives.compute_aero_derivatives ( segment)
+
+
This function computes the aerodynamic derivatives of the aircraft about a 
+mission segment, and stores them in the aero_derivatives data structure associated
+with the state conditions of the given mission segment. All derivatives are 
+computed using forward difference.
+
+Assumptions:
+   Linearized equations are used for each state variable
+
+Source:
+  N/A
+
+Inputs:
+  segment                SUAVE mission segment
+  
+Outputs: 
+   segment.state.conditions.aero_derivatives
+     .dCL_dAlpha       -   lift-curve slope                                                            [-]  
+     .dCM_dAlpha       -   derivative of pitching moment coefficient with respect to angle of attack   [-] 
+     .dCT_dAlpha       -   derivative of rotor thrust coefficient with respect to angle of attack      [-] 
+     .dCP_dAlpha       -   derivative of rotor power coefficient with respect to angle of attack       [-] 
+     .dCn_dBeta        -   derivative of yawing moment coefficient with respect to sideslip angle      [-] 
+     .dCl_dBeta        -   derivative of pitching moment with respect to angle of attack               [-] 
+     .dCT_dBeta        -   derivative of rotor thrust coefficient with respect to sideslip angle       [-] 
+     .dCP_dBeta        -   derivative of rotor power coefficient with respect to sideslip angle        [-] 
+     .dCL_dThrottle    -   derivative of lift coefficient with respect to throttle                     [-] 
+     .dCD_dThrottle    -   derivative of drag coefficient with respect to throttle                     [-] 
+     .dCT_dThrottle    -   derivative of rotor thrust coefficient with respect to throttle             [-] 
+     .dCP_dThrottle    -   derivative of rotor power coefficient with respect to throttle              [-] 
+       
+
+Properties Used:
+   N/A
+
+
@@ -111,7 +174,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/group__Methods-Flight__Dynamics-Static__Stability.js b/doxygen/group__Methods-Flight__Dynamics-Static__Stability.js index 9a171e3a..ec99a276 100644 --- a/doxygen/group__Methods-Flight__Dynamics-Static__Stability.js +++ b/doxygen/group__Methods-Flight__Dynamics-Static__Stability.js @@ -1,4 +1,5 @@ var group__Methods_Flight__Dynamics_Static__Stability = [ - [ "Approximations", "group__Methods-Flight__Dynamics-Static__Stability-Approximations.html", "group__Methods-Flight__Dynamics-Static__Stability-Approximations" ] + [ "Approximations", "group__Methods-Flight__Dynamics-Static__Stability-Approximations.html", "group__Methods-Flight__Dynamics-Static__Stability-Approximations" ], + [ "compute_aero_derivatives", "group__Methods-Flight__Dynamics-Static__Stability.html#ga71c3b45a53ae7c300e961752e84b124a", null ] ]; \ No newline at end of file diff --git a/doxygen/group__Methods-Flight__Dynamics.html b/doxygen/group__Methods-Flight__Dynamics.html index cbe97113..f1e5da68 100644 --- a/doxygen/group__Methods-Flight__Dynamics.html +++ b/doxygen/group__Methods-Flight__Dynamics.html @@ -1,9 +1,9 @@ - + - + SUAVE: Flight_Dynamics @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -117,7 +124,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/group__Methods-Geometry-Three__Dimensional.html b/doxygen/group__Methods-Geometry-Three__Dimensional.html index ccf74390..b71c4856 100644 --- a/doxygen/group__Methods-Geometry-Three__Dimensional.html +++ b/doxygen/group__Methods-Geometry-Three__Dimensional.html @@ -1,9 +1,9 @@ - + - + SUAVE: Three Dimensional @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
diff --git a/doxygen/group__Methods-Geometry-Two__Dimensional-Cross__Section-Airfoil.html b/doxygen/group__Methods-Geometry-Two__Dimensional-Cross__Section-Airfoil.html index 25e7c538..cef63f0d 100644 --- a/doxygen/group__Methods-Geometry-Two__Dimensional-Cross__Section-Airfoil.html +++ b/doxygen/group__Methods-Geometry-Two__Dimensional-Cross__Section-Airfoil.html @@ -1,9 +1,9 @@ - + - + SUAVE: Airfoil @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -103,18 +110,90 @@ - - + + + + + + + +

Functions

def SUAVE.Methods.Geometry.Two_Dimensional.Cross_Section.Airfoil.compute_naca_4series.compute_naca_4series (camber, camber_loc, thickness, npoints=200)
 
def SUAVE.Methods.Geometry.Two_Dimensional.Cross_Section.Airfoil.compute_airfoil_polars.compute_airfoil_polars (a_geo, a_polar, npoints=200, use_pre_stall_data=True)
 
def SUAVE.Methods.Geometry.Two_Dimensional.Cross_Section.Airfoil.compute_naca_4series.compute_naca_4series (camber, camber_loc, thickness, npoints=100)
 
def SUAVE.Methods.Geometry.Two_Dimensional.Cross_Section.Airfoil.compute_naca_4series.compute_naca_4series_lines (x, camber, camber_loc, thickness)
 
def SUAVE.Methods.Geometry.Two_Dimensional.Cross_Section.Airfoil.import_airfoil_dat.import_airfoil_dat (filename)
 
def SUAVE.Methods.Geometry.Two_Dimensional.Cross_Section.Airfoil.import_airfoil_geometry.import_airfoil_geometry (airfoil_geometry_files, npoints=200, surface_interpolation='cubic')
 
def SUAVE.Methods.Geometry.Two_Dimensional.Cross_Section.Airfoil.import_airfoil_polars.import_airfoil_polars (airfoil_polar_files)
 

Detailed Description

Geometry functions for two dimensional airfoils.

Function Documentation

- -

◆ compute_naca_4series()

+ +

◆ compute_airfoil_polars()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Geometry.Two_Dimensional.Cross_Section.Airfoil.compute_airfoil_polars.compute_airfoil_polars ( a_geo,
 a_polar,
 npoints = 200,
 use_pre_stall_data = True 
)
+
+
This computes the lift and drag coefficients of an airfoil in stall regimes using pre-stall
+characterstics and AERODAS formation for post stall characteristics. This is useful for 
+obtaining a more accurate prediction of wing and blade loading. Pre stall characteristics 
+are obtained in the form of a text file of airfoil polar data obtained from airfoiltools.com
+
+Assumptions:
+Uses AERODAS formulation for post stall characteristics 
+
+Source:
+Models of Lift and Drag Coefficients of Stalled and Unstalled Airfoils in Wind Turbines and Wind Tunnels
+by D Spera, 2008
+
+Inputs:
+a_geo                  <string>
+a_polar                <string>
+use_pre_stall_data     [Boolean]
+       
+
+Outputs:
+airfoil_data.
+    cl_polars          [unitless]
+    cd_polars          [unitless]      
+    aoa_sweep          [unitless]
+
+Properties Used:
+N/A
+
+
+
+ +

◆ compute_naca_4series()

@@ -141,7 +220,7 @@

  - npoints = 200  + npoints = 100  @@ -165,8 +244,15 @@

+

◆ import_airfoil_geometry()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Geometry.Two_Dimensional.Cross_Section.Airfoil.import_airfoil_geometry.import_airfoil_geometry ( airfoil_geometry_files,
 npoints = 200,
 surface_interpolation = 'cubic' 
)
+
+
This imports an airfoil geometry from a text file  and stores
+the coordinates of upper and lower surfaces as well as the mean
+camberline
+
+Assumptions:
+Works for Selig and Lednicer airfoil formats. Automatically detects which format based off first line of data. Assumes it is one of those two.
+
+Source:
+airfoiltools.com/airfoil/index - method for determining format and basic error checking
+
+Inputs:
+airfoil_geometry_files   <list of strings>
+surface_interpolation   - type of interpolation used in the SciPy function. Preferable options are linear, quardratic and cubic. 
+Full list of options can be found here : 
+https://docs.scipy.org/doc/scipy/reference/generated/scipy.interpolate.interp1d.html#scipy.interpolate.interp1d
+
+Outputs:
+airfoil_data.
+    thickness_to_chord 
+    x_coordinates 
+    y_coordinates
+    x_upper_surface
+    x_lower_surface
+    y_upper_surface
+    y_lower_surface
+    camber_coordinates  
+
+Properties Used:
+N/A
+
+
+
+ +

◆ import_airfoil_polars()

+ +
+
+ + + + + + + + +
def SUAVE.Methods.Geometry.Two_Dimensional.Cross_Section.Airfoil.import_airfoil_polars.import_airfoil_polars ( airfoil_polar_files)
+
+
This imports airfoil polars from a text file output from XFOIL or Airfoiltools.com
+
+Assumptions:
+Input airfoil polars file is obtained from XFOIL or from Airfoiltools.com
+
+Source:
+http://airfoiltools.com/
+
+Inputs:
+airfoil polar files   <list of strings>
+
+Outputs:
+data       numpy array with airfoil data
+
 Properties Used:
 N/A
 
@@ -275,7 +458,7 @@

Generated by - doxygen 1.8.14 + doxygen 1.8.15

diff --git a/doxygen/group__Methods-Geometry-Two__Dimensional-Cross__Section-Airfoil.js b/doxygen/group__Methods-Geometry-Two__Dimensional-Cross__Section-Airfoil.js index 746bfe8d..f69d6440 100644 --- a/doxygen/group__Methods-Geometry-Two__Dimensional-Cross__Section-Airfoil.js +++ b/doxygen/group__Methods-Geometry-Two__Dimensional-Cross__Section-Airfoil.js @@ -1,6 +1,9 @@ var group__Methods_Geometry_Two__Dimensional_Cross__Section_Airfoil = [ - [ "compute_naca_4series", "group__Methods-Geometry-Two__Dimensional-Cross__Section-Airfoil.html#gad9b707f99354749a179f1c932d25f8b1", null ], + [ "compute_airfoil_polars", "group__Methods-Geometry-Two__Dimensional-Cross__Section-Airfoil.html#gae0197ef91e2a70aea1339c460eafc749", null ], + [ "compute_naca_4series", "group__Methods-Geometry-Two__Dimensional-Cross__Section-Airfoil.html#ga2525303a929055b19fb06c56c2316f0d", null ], [ "compute_naca_4series_lines", "group__Methods-Geometry-Two__Dimensional-Cross__Section-Airfoil.html#gae1ae9095df65c2c151b5ad746a74c8a9", null ], - [ "import_airfoil_dat", "group__Methods-Geometry-Two__Dimensional-Cross__Section-Airfoil.html#ga68ca3b8f890d1f6714e88b276cbce559", null ] + [ "import_airfoil_dat", "group__Methods-Geometry-Two__Dimensional-Cross__Section-Airfoil.html#ga68ca3b8f890d1f6714e88b276cbce559", null ], + [ "import_airfoil_geometry", "group__Methods-Geometry-Two__Dimensional-Cross__Section-Airfoil.html#gaead0af20c28b4d2a52b21e8212d89914", null ], + [ "import_airfoil_polars", "group__Methods-Geometry-Two__Dimensional-Cross__Section-Airfoil.html#ga111b3e8f61a7a21447795d2302d9f110", null ] ]; \ No newline at end of file diff --git a/doxygen/group__Methods-Geometry-Two__Dimensional-Cross__Section-Propulsion.html b/doxygen/group__Methods-Geometry-Two__Dimensional-Cross__Section-Propulsion.html index 156976cb..5544e170 100644 --- a/doxygen/group__Methods-Geometry-Two__Dimensional-Cross__Section-Propulsion.html +++ b/doxygen/group__Methods-Geometry-Two__Dimensional-Cross__Section-Propulsion.html @@ -1,9 +1,9 @@ - + - + SUAVE: Propulsion @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@
- +

@@ -73,7 +78,9 @@
@@ -103,72 +110,14 @@ - - - - + +

Functions

def SUAVE.Methods.Geometry.Two_Dimensional.Cross_Section.Propulsion.compute_ducted_fan_geometry.compute_ducted_fan_geometry (ducted_fan, conditions)
 
def SUAVE.Methods.Geometry.Two_Dimensional.Cross_Section.Propulsion.compute_turbofan_geometry.compute_turbofan_geometry (turbofan, conditions)
 
def SUAVE.Methods.Geometry.Two_Dimensional.Cross_Section.Propulsion.compute_turbofan_geometry.compute_turbofan_geometry (turbofan, nacelle)
 

Detailed Description

Geometry functions for two dimensional propulsion measurements.

Function Documentation

- -

◆ compute_ducted_fan_geometry()

- -
-
- - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Geometry.Two_Dimensional.Cross_Section.Propulsion.compute_ducted_fan_geometry.compute_ducted_fan_geometry ( ducted_fan,
 conditions 
)
-
-
Estimates geometry for a ducted fan.
-
-Assumptions:
-None
-
-Source:
-None
-
-Inputs:
-ducted_fan.thrust.
-  mass_flow_rate_design [kg/s]
-ducted_fan.fan_nozzle.
-  outputs.velocity      [m/s]
-  outputs.density       [kg/m^3]
-  outputs.area_ratio    [-]
-conditions.freestream.
-  velocity              [m/s]
-  density               [kg/m^3]
-
-Outputs:
-ducted_fan.
-  areas.maximum         [m^2]
-  areas.wetted          [m^2]
-  nacelle_diameter      [m]
-  engine_length         [m]
-
-Properties Used:
-N/A
-
-
-
- -

◆ compute_turbofan_geometry()

+ +

◆ compute_turbofan_geometry()

diff --git a/doxygen/group__Methods-Geometry-Two__Dimensional-Cross__Section-Propulsion.js b/doxygen/group__Methods-Geometry-Two__Dimensional-Cross__Section-Propulsion.js index 9e0899e3..9a6bc51b 100644 --- a/doxygen/group__Methods-Geometry-Two__Dimensional-Cross__Section-Propulsion.js +++ b/doxygen/group__Methods-Geometry-Two__Dimensional-Cross__Section-Propulsion.js @@ -1,5 +1,4 @@ var group__Methods_Geometry_Two__Dimensional_Cross__Section_Propulsion = [ - [ "compute_ducted_fan_geometry", "group__Methods-Geometry-Two__Dimensional-Cross__Section-Propulsion.html#gabbca63e71ae9b78043c985ea40db0bab", null ], - [ "compute_turbofan_geometry", "group__Methods-Geometry-Two__Dimensional-Cross__Section-Propulsion.html#ga3ac328d4ae5282b2e4ce66d519777c73", null ] + [ "compute_turbofan_geometry", "group__Methods-Geometry-Two__Dimensional-Cross__Section-Propulsion.html#ga5b5214fb5c5a1611befc77f649cd3c01", null ] ]; \ No newline at end of file diff --git a/doxygen/group__Methods-Geometry-Two__Dimensional-Cross__Section.html b/doxygen/group__Methods-Geometry-Two__Dimensional-Cross__Section.html index 1791cba0..710a6c23 100644 --- a/doxygen/group__Methods-Geometry-Two__Dimensional-Cross__Section.html +++ b/doxygen/group__Methods-Geometry-Two__Dimensional-Cross__Section.html @@ -1,9 +1,9 @@ - + - + SUAVE: Cross Section @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@
- +
@@ -73,7 +78,9 @@
@@ -119,7 +126,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/group__Methods-Geometry-Two__Dimensional-Planform.html b/doxygen/group__Methods-Geometry-Two__Dimensional-Planform.html index e540c04d..21e2e666 100644 --- a/doxygen/group__Methods-Geometry-Two__Dimensional-Planform.html +++ b/doxygen/group__Methods-Geometry-Two__Dimensional-Planform.html @@ -1,9 +1,9 @@ - + - + SUAVE: Planform @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -106,7 +113,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/group__Methods-Geometry-Two__Dimensional.html b/doxygen/group__Methods-Geometry-Two__Dimensional.html index 6ae151b1..401fdc6c 100644 --- a/doxygen/group__Methods-Geometry-Two__Dimensional.html +++ b/doxygen/group__Methods-Geometry-Two__Dimensional.html @@ -1,9 +1,9 @@ - + - + SUAVE: Two Dimensional @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -119,7 +126,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/group__Methods-Geometry.html b/doxygen/group__Methods-Geometry.html index bd6a0910..f1365a0d 100644 --- a/doxygen/group__Methods-Geometry.html +++ b/doxygen/group__Methods-Geometry.html @@ -1,9 +1,9 @@ - + - + SUAVE: Geometry @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -120,7 +127,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/group__Methods-Missions-Segments-Climb.html b/doxygen/group__Methods-Missions-Segments-Climb.html index 50ec0e17..1c724f1e 100644 --- a/doxygen/group__Methods-Missions-Segments-Climb.html +++ b/doxygen/group__Methods-Missions-Segments-Climb.html @@ -1,9 +1,9 @@ - + - + SUAVE: Climb @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -103,66 +110,70 @@ - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +

Functions

def SUAVE.Methods.Missions.Segments.Climb.Common.unpack_unknowns (segment, state)
 
def SUAVE.Methods.Missions.Segments.Climb.Common.residual_total_forces (segment, state)
 
def SUAVE.Methods.Missions.Segments.Climb.Common.update_differentials_altitude (segment, state)
 
def SUAVE.Methods.Missions.Segments.Climb.Constant_Dynamic_Pressure_Constant_Angle.initialize_conditions_unpack_unknowns (segment, state)
 
def SUAVE.Methods.Missions.Segments.Climb.Constant_Dynamic_Pressure_Constant_Angle.residual_total_forces (segment, state)
 
def SUAVE.Methods.Missions.Segments.Climb.Constant_Dynamic_Pressure_Constant_Rate.initialize_conditions (segment, state)
 
def SUAVE.Methods.Missions.Segments.Climb.Constant_EAS_Constant_Rate.initialize_conditions (segment, state)
 
def SUAVE.Methods.Missions.Segments.Climb.Constant_Mach_Constant_Angle.initialize_conditions (segment, state)
 
def SUAVE.Methods.Missions.Segments.Climb.Constant_Mach_Constant_Rate.initialize_conditions (segment, state)
 
def SUAVE.Methods.Missions.Segments.Climb.Constant_Mach_Linear_Altitude.initialize_conditions (segment, state)
 
def SUAVE.Methods.Missions.Segments.Climb.Constant_Speed_Constant_Angle.initialize_conditions (segment, state)
 
def SUAVE.Methods.Missions.Segments.Climb.Constant_Speed_Constant_Angle_Noise.expand_state (segment, state)
 
def SUAVE.Methods.Missions.Segments.Climb.Constant_Speed_Constant_Rate.initialize_conditions (segment, state)
 
def SUAVE.Methods.Missions.Segments.Climb.Constant_Speed_Linear_Altitude.initialize_conditions (segment, state)
 Constant_Speed_Linear_Altitude.py Created: Jul 2014, SUAVE Team Modified: Jun 2017, E. More...
 
def SUAVE.Methods.Missions.Segments.Climb.Constant_Throttle_Constant_Speed.unpack_body_angle (segment, state)
 
def SUAVE.Methods.Missions.Segments.Climb.Constant_Throttle_Constant_Speed.initialize_conditions (segment, state)
 
def SUAVE.Methods.Missions.Segments.Climb.Constant_Throttle_Constant_Speed.update_differentials_altitude (segment, state)
 
-def SUAVE.Methods.Missions.Segments.Climb.Constant_Throttle_Constant_Speed.update_velocity_vector_from_wind_angle (segment, state)
 
def SUAVE.Methods.Missions.Segments.Climb.Linear_Mach_Constant_Rate.initialize_conditions (segment, state)
 
def SUAVE.Methods.Missions.Segments.Climb.Linear_Speed_Constant_Rate.initialize_conditions (segment, state)
 
def SUAVE.Methods.Missions.Segments.Climb.Optimized.unpack_unknowns (segment, state)
 
def SUAVE.Methods.Missions.Segments.Climb.Optimized.update_differentials (segment, state)
 
def SUAVE.Methods.Missions.Segments.Climb.Optimized.objective (segment, state)
 
def SUAVE.Methods.Missions.Segments.Climb.Optimized.constraints (segment, state)
 
def SUAVE.Methods.Missions.Segments.Climb.Optimized.cache_inputs (segment, state)
 
def SUAVE.Methods.Missions.Segments.Climb.Optimized.solve_linear_speed_constant_rate (segment, state)
 
def SUAVE.Methods.Missions.Segments.Climb.Common.unpack_unknowns (segment)
 
def SUAVE.Methods.Missions.Segments.Climb.Common.residual_total_forces (segment)
 
def SUAVE.Methods.Missions.Segments.Climb.Common.update_differentials_altitude (segment)
 
def SUAVE.Methods.Missions.Segments.Climb.Constant_CAS_Constant_Rate.initialize_conditions (segment)
 
def SUAVE.Methods.Missions.Segments.Climb.Constant_Dynamic_Pressure_Constant_Angle.initialize_conditions_unpack_unknowns (segment)
 
def SUAVE.Methods.Missions.Segments.Climb.Constant_Dynamic_Pressure_Constant_Angle.residual_total_forces (segment)
 
def SUAVE.Methods.Missions.Segments.Climb.Constant_Dynamic_Pressure_Constant_Rate.initialize_conditions (segment)
 
def SUAVE.Methods.Missions.Segments.Climb.Constant_EAS_Constant_Rate.initialize_conditions (segment)
 
def SUAVE.Methods.Missions.Segments.Climb.Constant_Mach_Constant_Angle.initialize_conditions (segment)
 
def SUAVE.Methods.Missions.Segments.Climb.Constant_Mach_Constant_Rate.initialize_conditions (segment)
 
def SUAVE.Methods.Missions.Segments.Climb.Constant_Mach_Linear_Altitude.initialize_conditions (segment)
 
def SUAVE.Methods.Missions.Segments.Climb.Constant_Speed_Constant_Angle.initialize_conditions (segment)
 
def SUAVE.Methods.Missions.Segments.Climb.Constant_Speed_Constant_Angle_Noise.expand_state (segment)
 
def SUAVE.Methods.Missions.Segments.Climb.Constant_Speed_Constant_Rate.initialize_conditions (segment)
 
def SUAVE.Methods.Missions.Segments.Climb.Constant_Speed_Linear_Altitude.initialize_conditions (segment)
 Constant_Speed_Linear_Altitude.py Created: Jul 2014, SUAVE Team Modified: Jun 2017, E. More...
 
def SUAVE.Methods.Missions.Segments.Climb.Constant_Throttle_Constant_Speed.unpack_body_angle (segment)
 
def SUAVE.Methods.Missions.Segments.Climb.Constant_Throttle_Constant_Speed.initialize_conditions (segment)
 
def SUAVE.Methods.Missions.Segments.Climb.Constant_Throttle_Constant_Speed.update_differentials_altitude (segment)
 
+def SUAVE.Methods.Missions.Segments.Climb.Constant_Throttle_Constant_Speed.update_velocity_vector_from_wind_angle (segment)
 
def SUAVE.Methods.Missions.Segments.Climb.Linear_Mach_Constant_Rate.initialize_conditions (segment)
 
def SUAVE.Methods.Missions.Segments.Climb.Linear_Speed_Constant_Rate.initialize_conditions (segment)
 
def SUAVE.Methods.Missions.Segments.Climb.Optimized.unpack_unknowns (segment)
 
def SUAVE.Methods.Missions.Segments.Climb.Optimized.update_differentials (segment)
 
def SUAVE.Methods.Missions.Segments.Climb.Optimized.objective (segment)
 
def SUAVE.Methods.Missions.Segments.Climb.Optimized.constraints (segment)
 
def SUAVE.Methods.Missions.Segments.Climb.Optimized.cache_inputs (segment)
 
def SUAVE.Methods.Missions.Segments.Climb.Optimized.solve_linear_speed_constant_rate (segment)
 
def SUAVE.Methods.Missions.Segments.Single_Point.Set_Speed_Set_Altitude_No_Propulsion.residual_total_force (segment)
 

Detailed Description

Climb mission methods containing the functions for setting up and solving a mission.

Function Documentation

- -

◆ cache_inputs()

+ +

◆ cache_inputs()

- -

◆ constraints()

+ +

◆ constraints()

@@ -223,8 +214,8 @@

-

◆ expand_state()

+ +

◆ expand_state()

@@ -267,8 +248,8 @@

-

◆ initialize_conditions() [1/11]

+ +

◆ initialize_conditions() [1/12]

@@ -319,42 +290,32 @@

-

◆ initialize_conditions() [2/11]

+ +

◆ initialize_conditions() [2/12]

- + - - - - + - - - - - - -
def SUAVE.Methods.Missions.Segments.Climb.Constant_Speed_Constant_Rate.initialize_conditions def SUAVE.Methods.Missions.Segments.Climb.Constant_Speed_Constant_Angle.initialize_conditions (  segment,
segment)  state 
)
Sets the specified conditions which are given for the segment type.
 
 Assumptions:
-Constant true airspeed, with a constant rate of climb
+Constant true airspeed, with a constant climb angle
 
 Source:
 N/A
 
 Inputs:
-segment.climb_rate                          [meters/second]
-segment.air_speed                           [meters/second]
+segment.climb_angle                         [radians]
+segment.air_speed                           [meter/second]
 segment.altitude_start                      [meters]
 segment.altitude_end                        [meters]
 state.numerics.dimensionless.control_points [Unitless]
@@ -370,46 +331,77 @@ 

-

◆ initialize_conditions() [3/11]

+ +

◆ initialize_conditions() [3/12]

- + - - - - + - - +
def SUAVE.Methods.Missions.Segments.Climb.Constant_Speed_Constant_Angle.initialize_conditions def SUAVE.Methods.Missions.Segments.Climb.Constant_Speed_Constant_Rate.initialize_conditions (  segment,
segment)  state 
+
+
Sets the specified conditions which are given for the segment type.
+
+Assumptions:
+Constant true airspeed, with a constant rate of climb
+
+Source:
+N/A
+
+Inputs:
+segment.climb_rate                                  [meters/second]
+segment.air_speed                                   [meters/second]
+segment.altitude_start                              [meters]
+segment.altitude_end                                [meters]
+segment.state.numerics.dimensionless.control_points [Unitless]
+conditions.freestream.density                       [kilograms/meter^3]
+
+Outputs:
+conditions.frames.inertial.velocity_vector  [meters/second]
+conditions.frames.inertial.position_vector  [meters]
+conditions.freestream.altitude              [meters]
+
+Properties Used:
+N/A
+
+
+
+ +

◆ initialize_conditions() [4/12]

+ +
+
+ + + + + - -
def SUAVE.Methods.Missions.Segments.Climb.Constant_Mach_Constant_Rate.initialize_conditions ( segment) )
Sets the specified conditions which are given for the segment type.
 
 Assumptions:
-Constant true airspeed, with a constant climb angle
+Constant Mach number, with a constant rate of climb
 
 Source:
 N/A
 
 Inputs:
-segment.climb_angle                         [radians]
-segment.air_speed                           [meter/second]
-segment.altitude_start                      [meters]
-segment.altitude_end                        [meters]
-state.numerics.dimensionless.control_points [Unitless]
-conditions.freestream.density               [kilograms/meter^3]
+segment.climb_rate                                  [meters/second]
+segment.mach                                        [Unitless]
+segment.altitude_start                              [meters]
+segment.altitude_end                                [meters]
+segment.state.numerics.dimensionless.control_points [Unitless]
+conditions.freestream.density                       [kilograms/meter^3]
 
 Outputs:
 conditions.frames.inertial.velocity_vector  [meters/second]
@@ -421,8 +413,8 @@ 

-

◆ initialize_conditions() [4/11]

+ +

◆ initialize_conditions() [5/12]

@@ -455,12 +437,12 @@

-

◆ initialize_conditions() [5/11]

+ +

◆ initialize_conditions() [6/12]

- + - - - - + - - - - - - -
def SUAVE.Methods.Missions.Segments.Climb.Constant_Mach_Constant_Rate.initialize_conditions def SUAVE.Methods.Missions.Segments.Climb.Constant_Mach_Constant_Angle.initialize_conditions (  segment,
segment)  state 
)
Sets the specified conditions which are given for the segment type.
 
 Assumptions:
-Constant Mach number, with a constant rate of climb
+Constant Mach number, with a constant angle of climb
 
 Source:
 N/A
 
 Inputs:
-segment.climb_rate                          [meters/second]
-segment.mach                                [Unitless]
-segment.altitude_start                      [meters]
-segment.altitude_end                        [meters]
-state.numerics.dimensionless.control_points [Unitless]
-conditions.freestream.density               [kilograms/meter^3]
+segment.climb_angle                                 [radians]
+segment.mach                                        [Unitless]
+segment.altitude_start                              [meters]
+segment.altitude_end                                [meters]
+segment.state.numerics.dimensionless.control_points [Unitless]
+conditions.freestream.density                       [kilograms/meter^3]
 
 Outputs:
 conditions.frames.inertial.velocity_vector  [meters/second]
@@ -523,148 +495,118 @@ 

-

◆ initialize_conditions() [6/11]

+ +

◆ initialize_conditions() [7/12]

- + - - - - + - - - - - - -
def SUAVE.Methods.Missions.Segments.Climb.Constant_Mach_Linear_Altitude.initialize_conditions def SUAVE.Methods.Missions.Segments.Climb.Linear_Speed_Constant_Rate.initialize_conditions (  segment,
segment)  state 
)
Sets the specified conditions which are given for the segment type.
 
 Assumptions:
-Constrant dynamic pressure and constant rate of climb
+Linearly changing airspeed, with a constant rate of climb
 
 Source:
 N/A
 
 Inputs:
-segment.mach                                [unitless]
-segment.dynamic_pressure                    [pascals]
-segment.altitude_start                      [meters]
+segment.climb_rate                          [meters/second]
+segment.air_speed_start                     [meters/second]
+segment.air_speed_end                       [meters/second]
 segment.altitude_end                        [meters]
-segment.distance                            [meters]
+state.numerics.dimensionless.control_points [Unitless]
+conditions.freestream.density               [kilograms/meter^3]
 
 Outputs:
 conditions.frames.inertial.velocity_vector  [meters/second]
 conditions.frames.inertial.position_vector  [meters]
 conditions.freestream.altitude              [meters]
-conditions.frames.inertial.time             [seconds]
 
 Properties Used:
 N/A
 
- -

◆ initialize_conditions() [7/11]

+ +

◆ initialize_conditions() [8/12]

- + - - - - - - - - - + - -
def SUAVE.Methods.Missions.Segments.Climb.Constant_Mach_Constant_Angle.initialize_conditions def SUAVE.Methods.Missions.Segments.Climb.Constant_Mach_Linear_Altitude.initialize_conditions (  segment,
 state 
segment) )
Sets the specified conditions which are given for the segment type.
 
 Assumptions:
-Constant Mach number, with a constant angle of climb
+Constrant dynamic pressure and constant rate of climb
 
 Source:
 N/A
 
 Inputs:
-segment.climb_angle                         [radians]
-segment.mach                                [Unitless]
+segment.mach                                [unitless]
+segment.dynamic_pressure                    [pascals]
 segment.altitude_start                      [meters]
 segment.altitude_end                        [meters]
-state.numerics.dimensionless.control_points [Unitless]
-conditions.freestream.density               [kilograms/meter^3]
+segment.distance                            [meters]
 
 Outputs:
 conditions.frames.inertial.velocity_vector  [meters/second]
 conditions.frames.inertial.position_vector  [meters]
 conditions.freestream.altitude              [meters]
+conditions.frames.inertial.time             [seconds]
 
 Properties Used:
 N/A
 
- -

◆ initialize_conditions() [8/11]

+ +

◆ initialize_conditions() [9/12]

- + - - - - + - - - - - - -
def SUAVE.Methods.Missions.Segments.Climb.Linear_Speed_Constant_Rate.initialize_conditions def SUAVE.Methods.Missions.Segments.Climb.Constant_EAS_Constant_Rate.initialize_conditions (  segment,
segment)  state 
)
Sets the specified conditions which are given for the segment type.
 
 Assumptions:
-Linearly changing airspeed, with a constant rate of climb
+Constant true airspeed with a constant rate of climb
 
 Source:
 N/A
 
 Inputs:
-segment.climb_rate                          [meters/second]
-segment.air_speed_start                     [meters/second]
-segment.air_speed_end                       [meters/second]
-segment.altitude_end                        [meters]
-state.numerics.dimensionless.control_points [Unitless]
-conditions.freestream.density               [kilograms/meter^3]
+segment.climb_rate                                  [meters/second]
+segment.equivalent_air_speed                        [meters/second]
+segment.altitude_start                              [meters]
+segment.altitude_end                                [meters]
+segment.state.numerics.dimensionless.control_points [Unitless]
+conditions.freestream.density                       [kilograms/meter^3]
 
 Outputs:
 conditions.frames.inertial.velocity_vector  [meters/second]
@@ -676,8 +618,8 @@ 

-

◆ initialize_conditions() [9/11]

+ +

◆ initialize_conditions() [10/12]

@@ -710,12 +642,12 @@

-

◆ initialize_conditions() [10/11]

+ +

◆ initialize_conditions() [11/12]

- + - - - - + - - - - - - -
def SUAVE.Methods.Missions.Segments.Climb.Constant_EAS_Constant_Rate.initialize_conditions def SUAVE.Methods.Missions.Segments.Climb.Constant_CAS_Constant_Rate.initialize_conditions (  segment,
segment)  state 
)
Sets the specified conditions which are given for the segment type.
 
 Assumptions:
-Constant true airspeed with a constant rate of climb
+Constant CAS airspeed with a constant rate of climb
 
 Source:
 N/A
 
 Inputs:
-segment.climb_rate                          [meters/second]
-segment.equivalent_air_speed                [meters/second]
-segment.altitude_start                      [meters]
-segment.altitude_end                        [meters]
-state.numerics.dimensionless.control_points [Unitless]
-conditions.freestream.density               [kilograms/meter^3]
+segment.climb_rate                                  [meters/second]
+segment.calibrated_air_speed                        [meters/second]
+segment.altitude_start                              [meters]
+segment.altitude_end                                [meters]
+segment.state.numerics.dimensionless.control_points [Unitless]
+conditions.freestream.density                       [kilograms/meter^3]
 
 Outputs:
 conditions.frames.inertial.velocity_vector  [meters/second]
@@ -778,8 +700,8 @@ 

-

◆ initialize_conditions() [11/11]

+ +

◆ initialize_conditions() [12/12]

@@ -812,12 +724,12 @@

-

◆ initialize_conditions_unpack_unknowns()

+ +

◆ initialize_conditions_unpack_unknowns()

@@ -862,15 +764,15 @@

-

◆ objective()

+ +

◆ objective()

@@ -917,28 +809,54 @@

-

◆ residual_total_forces() [1/2]

+ +

◆ residual_total_force()

- + - - - - + - - +
def SUAVE.Methods.Missions.Segments.Climb.Common.residual_total_forces def SUAVE.Methods.Missions.Segments.Single_Point.Set_Speed_Set_Altitude_No_Propulsion.residual_total_force (  segment,
segment)  state 
+
+
Takes the summation of forces and makes a residual from the accelerations.
+
+Assumptions:
+No higher order terms.
+
+Source:
+N/A
+
+Inputs:
+segment.state.conditions.frames.inertial.total_force_vector   [Newtons]
+segment.state.conditions.frames.inertial.acceleration_vector  [meter/second^2]
+segment.state.conditions.weights.total_mass                   [kilogram]
+
+Outputs:
+segment.state.residuals.force                                 [Unitless]
+
+Properties Used:
+N/A
+
+
+
+ +

◆ residual_total_forces() [1/2]

+ +
+
+ + + + + - -
def SUAVE.Methods.Missions.Segments.Climb.Common.residual_total_forces ( segment) )
@@ -951,20 +869,20 @@

-

◆ residual_total_forces() [2/2]

+ +

◆ residual_total_forces() [2/2]

@@ -997,21 +905,21 @@

-

◆ solve_linear_speed_constant_rate()

+ +

◆ solve_linear_speed_constant_rate()

@@ -1061,8 +959,8 @@

-

◆ unpack_body_angle()

+ +

◆ unpack_body_angle()

@@ -1105,28 +993,18 @@

-

◆ unpack_unknowns() [1/2]

+ +

◆ unpack_unknowns() [1/2]

- + - - - - + - - - - - - -
def SUAVE.Methods.Missions.Segments.Climb.Common.unpack_unknowns def SUAVE.Methods.Missions.Segments.Climb.Optimized.unpack_unknowns (  segment,
segment)  state 
)
@@ -1139,40 +1017,37 @@

-

◆ unpack_unknowns() [2/2]

+ +

◆ unpack_unknowns() [2/2]

- + - - - - - - - - - + - -
def SUAVE.Methods.Missions.Segments.Climb.Optimized.unpack_unknowns def SUAVE.Methods.Missions.Segments.Climb.Common.unpack_unknowns (  segment,
 state 
segment) )
@@ -1185,27 +1060,20 @@

-

◆ update_differentials()

+ +

◆ update_differentials()

-
On each iteration creates the differentials and integration funcitons from knowns about the problem. Sets the time at each point. Must return in dimensional time, with t[0] = 0. This is different from the common method as it also includes the scaling of operators.
+
On each iteration creates the differentials and integration functions from knowns about the problem. Sets the time at each point. Must return in dimensional time, with t[0] = 0. This is different from the common method as it also includes the scaling of operators.
 
     Assumptions:
     Works with a segment discretized in vertical position, altitude
@@ -1246,8 +1104,8 @@ 

-

◆ update_differentials_altitude() [1/2]

+ +

◆ update_differentials_altitude() [1/2]

- -

◆ update_differentials_altitude() [2/2]

+ +

◆ update_differentials_altitude() [2/2]

diff --git a/doxygen/group__Methods-Missions-Segments-Climb.js b/doxygen/group__Methods-Missions-Segments-Climb.js index 179153ed..400e57d5 100644 --- a/doxygen/group__Methods-Missions-Segments-Climb.js +++ b/doxygen/group__Methods-Missions-Segments-Climb.js @@ -1,28 +1,30 @@ var group__Methods_Missions_Segments_Climb = [ - [ "cache_inputs", "group__Methods-Missions-Segments-Climb.html#ga5ec6e7e89ae5204a6bbc4518b9ceca73", null ], - [ "constraints", "group__Methods-Missions-Segments-Climb.html#ga9d57e92ca2c358a479e9bfdc49dc4ac1", null ], - [ "expand_state", "group__Methods-Missions-Segments-Climb.html#gabdde25a995acf46c265e0e6fab34e8b2", null ], - [ "initialize_conditions", "group__Methods-Missions-Segments-Climb.html#gaf50de17ff1541146247a44d338b28768", null ], - [ "initialize_conditions", "group__Methods-Missions-Segments-Climb.html#ga6e68cb34033fbe00aac9627de12986fc", null ], - [ "initialize_conditions", "group__Methods-Missions-Segments-Climb.html#gafec7759517a07b28bee9be68267d6f91", null ], - [ "initialize_conditions", "group__Methods-Missions-Segments-Climb.html#gae30d8b553e31793b12ea7b5b769adf67", null ], - [ "initialize_conditions", "group__Methods-Missions-Segments-Climb.html#ga7ea38cf00e0e00585da25a0888f94a45", null ], - [ "initialize_conditions", "group__Methods-Missions-Segments-Climb.html#ga0227df0558df5ba16ade99872b6d3ebb", null ], - [ "initialize_conditions", "group__Methods-Missions-Segments-Climb.html#ga82b7151ae7fcfb604dbbddb3754008ff", null ], - [ "initialize_conditions", "group__Methods-Missions-Segments-Climb.html#ga00600dbf3ab12a10572a5f4980279c82", null ], - [ "initialize_conditions", "group__Methods-Missions-Segments-Climb.html#ga39a8d04132b0d01e604ca2761da5033f", null ], - [ "initialize_conditions", "group__Methods-Missions-Segments-Climb.html#gab2b400ae79a4a2f0d8694c20512f3afe", null ], - [ "initialize_conditions", "group__Methods-Missions-Segments-Climb.html#ga7cf88701a5d299ccd5d99cee94fd570e", null ], - [ "initialize_conditions_unpack_unknowns", "group__Methods-Missions-Segments-Climb.html#gaa128a9c20b00aac7104d6f24119b9447", null ], - [ "objective", "group__Methods-Missions-Segments-Climb.html#gafbdcd0f752087b5ec8b144fd917ec3e5", null ], - [ "residual_total_forces", "group__Methods-Missions-Segments-Climb.html#ga8817bf89f7c17d350fc861cb83a476c3", null ], - [ "residual_total_forces", "group__Methods-Missions-Segments-Climb.html#gafc8a7871277f15c01aa0c951f4f1eef1", null ], - [ "solve_linear_speed_constant_rate", "group__Methods-Missions-Segments-Climb.html#gabecf74a86a38e945e7855fbf6ed09800", null ], - [ "unpack_body_angle", "group__Methods-Missions-Segments-Climb.html#gaec4a6e3dad562d56f0cff0cd839a5800", null ], - [ "unpack_unknowns", "group__Methods-Missions-Segments-Climb.html#ga560db4e14a7bc0aed412880b7370893f", null ], - [ "unpack_unknowns", "group__Methods-Missions-Segments-Climb.html#gaeb0685a1f445cbaba03c97c00106669b", null ], - [ "update_differentials", "group__Methods-Missions-Segments-Climb.html#ga8014ac487703c19bfbb00d70a6d9971a", null ], - [ "update_differentials_altitude", "group__Methods-Missions-Segments-Climb.html#ga554da51f265e8299ebef51b7a832f48b", null ], - [ "update_differentials_altitude", "group__Methods-Missions-Segments-Climb.html#ga052a29792178588704d70ef919ed2072", null ] + [ "cache_inputs", "group__Methods-Missions-Segments-Climb.html#ga4f1df8d21ba60ace73725c24658fe34d", null ], + [ "constraints", "group__Methods-Missions-Segments-Climb.html#gabf0cd52868d8d03cead1592cb6bad69d", null ], + [ "expand_state", "group__Methods-Missions-Segments-Climb.html#ga3eab71bbf7eb3e8184528d842ce04317", null ], + [ "initialize_conditions", "group__Methods-Missions-Segments-Climb.html#ga0cec13f8ee7fbc465c141040c2c41b93", null ], + [ "initialize_conditions", "group__Methods-Missions-Segments-Climb.html#gab82c682141a52f20a5c48745fe9cee7c", null ], + [ "initialize_conditions", "group__Methods-Missions-Segments-Climb.html#gacec348ec4bd4e5b79aa8de9f5e112599", null ], + [ "initialize_conditions", "group__Methods-Missions-Segments-Climb.html#ga8423dc5828181d461be290cc8fa07aac", null ], + [ "initialize_conditions", "group__Methods-Missions-Segments-Climb.html#gae1e7d66b8a72ca3c7ca5723d33160c5f", null ], + [ "initialize_conditions", "group__Methods-Missions-Segments-Climb.html#ga9a2e3bf3d6dafe8180bc62f8273406dc", null ], + [ "initialize_conditions", "group__Methods-Missions-Segments-Climb.html#ga35332679ca247bda50214d311a177d99", null ], + [ "initialize_conditions", "group__Methods-Missions-Segments-Climb.html#gacaf2bb91cc18422b48bba0c71112c7c4", null ], + [ "initialize_conditions", "group__Methods-Missions-Segments-Climb.html#ga28af3072b0f5324d9c40d5337bcb429b", null ], + [ "initialize_conditions", "group__Methods-Missions-Segments-Climb.html#ga20eade063eeffaf3b2e177e543e01900", null ], + [ "initialize_conditions", "group__Methods-Missions-Segments-Climb.html#gae81d9cbc3d8a0247d526c55282350167", null ], + [ "initialize_conditions", "group__Methods-Missions-Segments-Climb.html#gad4ac2eef84f78bbaf8b6f045356a5416", null ], + [ "initialize_conditions_unpack_unknowns", "group__Methods-Missions-Segments-Climb.html#gaac412aa6d758b00a3afea98b7481efe9", null ], + [ "objective", "group__Methods-Missions-Segments-Climb.html#gabee9e9494aba31c073479f3959e47804", null ], + [ "residual_total_force", "group__Methods-Missions-Segments-Climb.html#ga8178a1d5bdc03afcfc4ffc4f3fea84b9", null ], + [ "residual_total_forces", "group__Methods-Missions-Segments-Climb.html#ga940322075977d776d495e4d96e6c7a5f", null ], + [ "residual_total_forces", "group__Methods-Missions-Segments-Climb.html#ga1cd6e02a6f48be1747d2a5de1933ea33", null ], + [ "solve_linear_speed_constant_rate", "group__Methods-Missions-Segments-Climb.html#ga2452cb06a9f3c9b0342410237527d9c3", null ], + [ "unpack_body_angle", "group__Methods-Missions-Segments-Climb.html#ga609ef79a88804c79c686a96d0df073ee", null ], + [ "unpack_unknowns", "group__Methods-Missions-Segments-Climb.html#ga45db4de631268261e517f5bfbd83d8ea", null ], + [ "unpack_unknowns", "group__Methods-Missions-Segments-Climb.html#ga2ee3be62c3fb9a360a31a35d6a294ee7", null ], + [ "update_differentials", "group__Methods-Missions-Segments-Climb.html#ga09c3e3aeb85eddc40665141d8252711e", null ], + [ "update_differentials_altitude", "group__Methods-Missions-Segments-Climb.html#ga1511b51c4aa33929b469c0bc92ddfe22", null ], + [ "update_differentials_altitude", "group__Methods-Missions-Segments-Climb.html#ga88bd9bbe2513d3b4da4be346d1335e1d", null ] ]; \ No newline at end of file diff --git a/doxygen/group__Methods-Missions-Segments-Common.html b/doxygen/group__Methods-Missions-Segments-Common.html index 18b22577..0bf27646 100644 --- a/doxygen/group__Methods-Missions-Segments-Common.html +++ b/doxygen/group__Methods-Missions-Segments-Common.html @@ -1,9 +1,9 @@ - + - + SUAVE: Common @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@
- +
@@ -73,7 +78,9 @@
@@ -103,80 +110,106 @@ - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +

Functions

def SUAVE.Methods.Missions.Segments.Common.Aerodynamics.update_altitude (segment, state)
 
def SUAVE.Methods.Missions.Segments.Common.Aerodynamics.update_atmosphere (segment, state)
 
def SUAVE.Methods.Missions.Segments.Common.Aerodynamics.update_freestream (segment, state)
 
def SUAVE.Methods.Missions.Segments.Common.Aerodynamics.update_aerodynamics (segment, state)
 
def SUAVE.Methods.Missions.Segments.Common.Aerodynamics.update_stability (segment, state)
 
def SUAVE.Methods.Missions.Segments.Common.Energy.initialize_battery (segment, state)
 
def SUAVE.Methods.Missions.Segments.Common.Energy.update_thrust (segment, state)
 
def SUAVE.Methods.Missions.Segments.Common.Frames.initialize_inertial_position (segment, state)
 
def SUAVE.Methods.Missions.Segments.Common.Frames.initialize_time (segment, state)
 
def SUAVE.Methods.Missions.Segments.Common.Frames.initialize_planet_position (segment, state)
 
def SUAVE.Methods.Missions.Segments.Common.Frames.update_planet_position (segment, state)
 
def SUAVE.Methods.Missions.Segments.Common.Frames.update_orientations (segment, state)
 
def SUAVE.Methods.Missions.Segments.Common.Frames.update_forces (segment, state)
 
def SUAVE.Methods.Missions.Segments.Common.Frames.integrate_inertial_horizontal_position (segment, state)
 
def SUAVE.Methods.Missions.Segments.Common.Frames.update_acceleration (segment, state)
 
def SUAVE.Methods.Missions.Segments.Common.Numerics.initialize_differentials_dimensionless (segment, state)
 
def SUAVE.Methods.Missions.Segments.Common.Numerics.update_differentials_time (segment, state)
 
def SUAVE.Methods.Missions.Segments.Common.Sub_Segments.expand_sub_segments (segment, state)
 
def SUAVE.Methods.Missions.Segments.Common.Sub_Segments.update_sub_segments (segment, state)
 
def SUAVE.Methods.Missions.Segments.Common.Sub_Segments.finalize_sub_segments (segment, state)
 
def SUAVE.Methods.Missions.Segments.Common.Sub_Segments.sequential_sub_segments (segment, state)
 
def SUAVE.Methods.Missions.Segments.Common.Weights.initialize_weights (segment, state)
 
def SUAVE.Methods.Missions.Segments.Common.Weights.update_gravity (segment, state)
 
def SUAVE.Methods.Missions.Segments.Common.Weights.update_weights (segment, state)
 
def SUAVE.Methods.Missions.Segments.Common.Aerodynamics.update_altitude (segment)
 
def SUAVE.Methods.Missions.Segments.Common.Aerodynamics.update_atmosphere (segment)
 
def SUAVE.Methods.Missions.Segments.Common.Aerodynamics.update_freestream (segment)
 
def SUAVE.Methods.Missions.Segments.Common.Aerodynamics.update_aerodynamics (segment)
 
def SUAVE.Methods.Missions.Segments.Common.Aerodynamics.update_stability (segment)
 
def SUAVE.Methods.Missions.Segments.Common.Energy.initialize_battery (segment)
 Energy.py. More...
 
def SUAVE.Methods.Missions.Segments.Common.Energy.update_thrust (segment)
 
def SUAVE.Methods.Missions.Segments.Common.Frames.initialize_inertial_position (segment)
 
def SUAVE.Methods.Missions.Segments.Common.Frames.initialize_time (segment)
 
def SUAVE.Methods.Missions.Segments.Common.Frames.initialize_planet_position (segment)
 
def SUAVE.Methods.Missions.Segments.Common.Frames.update_planet_position (segment)
 
def SUAVE.Methods.Missions.Segments.Common.Frames.update_orientations (segment)
 
def SUAVE.Methods.Missions.Segments.Common.Frames.update_forces (segment)
 
def SUAVE.Methods.Missions.Segments.Common.Frames.integrate_inertial_horizontal_position (segment)
 
def SUAVE.Methods.Missions.Segments.Common.Frames.update_acceleration (segment)
 
def SUAVE.Methods.Missions.Segments.Common.Noise.compute_noise (segment)
 Noise.py. More...
 
def SUAVE.Methods.Missions.Segments.Common.Numerics.initialize_differentials_dimensionless (segment)
 
def SUAVE.Methods.Missions.Segments.Common.Numerics.update_differentials_time (segment)
 
def SUAVE.Methods.Missions.Segments.Common.Sub_Segments.expand_sub_segments (segment)
 
def SUAVE.Methods.Missions.Segments.Common.Sub_Segments.update_sub_segments (segment)
 
def SUAVE.Methods.Missions.Segments.Common.Sub_Segments.finalize_sub_segments (segment)
 
def SUAVE.Methods.Missions.Segments.Common.Sub_Segments.sequential_sub_segments (segment)
 
def SUAVE.Methods.Missions.Segments.Common.Sub_Segments.merge_sub_segment_states (segment)
 
def SUAVE.Methods.Missions.Segments.Common.Sub_Segments.unpack_subsegments (segment)
 
def SUAVE.Methods.Missions.Segments.Common.Weights.initialize_weights (segment)
 
def SUAVE.Methods.Missions.Segments.Common.Weights.update_gravity (segment)
 
def SUAVE.Methods.Missions.Segments.Common.Weights.update_weights (segment)
 

Detailed Description

Climb mission methods containing the functions for setting up and solving a mission.

Function Documentation

- -

◆ expand_sub_segments()

+ +

◆ compute_noise()

- + - - - - + - - +
def SUAVE.Methods.Missions.Segments.Common.Sub_Segments.expand_sub_segments def SUAVE.Methods.Missions.Segments.Common.Noise.compute_noise (  segment,
segment)  state 
+
+ +

Noise.py.

+

Created: Oct 2020, M. Clarke

Evaluates the energy network to find the thrust force and mass rate
+
+    Inputs -
+        segment.analyses.noise             [Function]
+
+    Outputs
+        N/A
+
+    Assumptions -
+
+
+ +

◆ expand_sub_segments()

+ +
+
+ + + + + - -
def SUAVE.Methods.Missions.Segments.Common.Sub_Segments.expand_sub_segments ( segment) )
@@ -195,8 +228,8 @@

-

◆ finalize_sub_segments()

+ +

◆ finalize_sub_segments()

@@ -235,8 +258,8 @@

-

◆ initialize_battery()

+ +

◆ initialize_battery()

- -

◆ initialize_differentials_dimensionless()

+ +

◆ initialize_differentials_dimensionless()

@@ -323,8 +330,8 @@

-

◆ initialize_inertial_position()

+ +

◆ initialize_inertial_position()

@@ -354,21 +351,21 @@

-

◆ initialize_planet_position()

+ +

◆ initialize_planet_position()

@@ -398,14 +385,14 @@

-

◆ initialize_time()

+ +

◆ initialize_time()

@@ -460,8 +437,8 @@

-

◆ initialize_weights()

+ +

◆ initialize_weights()

@@ -491,21 +458,21 @@

-

◆ integrate_inertial_horizontal_position()

+ +

◆ integrate_inertial_horizontal_position()

@@ -535,41 +492,61 @@

-

◆ sequential_sub_segments()

+ +

◆ merge_sub_segment_states()

- + - - - - + - - +
def SUAVE.Methods.Missions.Segments.Common.Sub_Segments.sequential_sub_segments def SUAVE.Methods.Missions.Segments.Common.Sub_Segments.merge_sub_segment_states (  segment,
segment)  state 
+
+
Merges all of the sub segment states back into the main state
+
+    Assumptions:
+    N/A
+    
+    Inputs:
+    N/A
+        
+    Outputs:
+    N/A
+
+    Properties Used:
+    N/A
+
+
+ +

◆ sequential_sub_segments()

+ +
+
+ + + + + - -
def SUAVE.Methods.Missions.Segments.Common.Sub_Segments.sequential_sub_segments ( segment) )
@@ -588,28 +565,48 @@

-

◆ update_acceleration()

+ +

◆ unpack_subsegments()

- + - - - - + - - +
def SUAVE.Methods.Missions.Segments.Common.Frames.update_acceleration def SUAVE.Methods.Missions.Segments.Common.Sub_Segments.unpack_subsegments (  segment,
segment)  state 
+
+
Unpacks the unknowns from the higher level state into the sub segments
+
+    Assumptions:
+    The subsegments have numerics
+    
+    Inputs:
+    N/A
+        
+    Outputs:
+    N/A
+
+    Properties Used:
+    N/A
+
+
+ +

◆ update_acceleration()

+ +
+
+ + + + + - -
def SUAVE.Methods.Missions.Segments.Common.Frames.update_acceleration ( segment) )
@@ -619,20 +616,20 @@

-

◆ update_aerodynamics()

+ +

◆ update_aerodynamics()

@@ -664,10 +651,10 @@

-

◆ update_altitude()

+ +

◆ update_altitude()

@@ -711,18 +688,18 @@

-

◆ update_atmosphere()

+ +

◆ update_atmosphere()

@@ -758,18 +725,21 @@

-

◆ update_differentials_time()

+ +

◆ update_differentials_time()

@@ -815,8 +775,8 @@

-

◆ update_forces()

+ +

◆ update_forces()

@@ -846,17 +796,17 @@

-

◆ update_freestream()

+ +

◆ update_freestream()

@@ -897,14 +837,14 @@

-

◆ update_gravity()

+ +

◆ update_gravity()

@@ -954,8 +884,8 @@

-

◆ update_orientations()

+ +

◆ update_orientations()

- -

◆ update_weights()

+ +

◆ update_weights()

diff --git a/doxygen/group__Methods-Missions-Segments-Common.js b/doxygen/group__Methods-Missions-Segments-Common.js index 9d1e50aa..7435659e 100644 --- a/doxygen/group__Methods-Missions-Segments-Common.js +++ b/doxygen/group__Methods-Missions-Segments-Common.js @@ -1,27 +1,30 @@ var group__Methods_Missions_Segments_Common = [ - [ "expand_sub_segments", "group__Methods-Missions-Segments-Common.html#ga079e5a37c661722e1c901040dd78d544", null ], - [ "finalize_sub_segments", "group__Methods-Missions-Segments-Common.html#ga03f607d22f766fd78769caf7dc27556e", null ], - [ "initialize_battery", "group__Methods-Missions-Segments-Common.html#ga94506d993490deb6e2902784b79bb02d", null ], - [ "initialize_differentials_dimensionless", "group__Methods-Missions-Segments-Common.html#ga7277f70a1093a4c10146e45c48b88ed4", null ], - [ "initialize_inertial_position", "group__Methods-Missions-Segments-Common.html#gaf417ce9f9fc6785a6a312274f6316990", null ], - [ "initialize_planet_position", "group__Methods-Missions-Segments-Common.html#gae3fbb540567a4e08e5b0f44548328db1", null ], - [ "initialize_time", "group__Methods-Missions-Segments-Common.html#ga888fab97485f10a9335a020a6a2e818f", null ], - [ "initialize_weights", "group__Methods-Missions-Segments-Common.html#ga28afe6dccd37e6dd3e9bb5d9defc09a5", null ], - [ "integrate_inertial_horizontal_position", "group__Methods-Missions-Segments-Common.html#ga3a5b6e449d878f0c462f9b3aae5fb21e", null ], - [ "sequential_sub_segments", "group__Methods-Missions-Segments-Common.html#gac5eadfe8d73ea29bf45f9c715043f00f", null ], - [ "update_acceleration", "group__Methods-Missions-Segments-Common.html#ga1fc39f83024cb8c207f5b82baeaccf43", null ], - [ "update_aerodynamics", "group__Methods-Missions-Segments-Common.html#ga5b618bac1bc4073916460a4f76f0e4df", null ], - [ "update_altitude", "group__Methods-Missions-Segments-Common.html#gab2637dce007776f926ee1af68ba0bca6", null ], - [ "update_atmosphere", "group__Methods-Missions-Segments-Common.html#ga251ef83f6b960654414d87bc3182e181", null ], - [ "update_differentials_time", "group__Methods-Missions-Segments-Common.html#gac4217dbf63f9649cac48522146405a2b", null ], - [ "update_forces", "group__Methods-Missions-Segments-Common.html#gaf9366945be87f7cbc146b2af89ddb2dc", null ], - [ "update_freestream", "group__Methods-Missions-Segments-Common.html#ga81df0274f076e00098e713c81b3a1dd7", null ], - [ "update_gravity", "group__Methods-Missions-Segments-Common.html#ga6acbb3f963502e3d4cb49e2b0126b67e", null ], - [ "update_orientations", "group__Methods-Missions-Segments-Common.html#gab28256a8e226536e94abafb5c962101f", null ], - [ "update_planet_position", "group__Methods-Missions-Segments-Common.html#ga3f20c80c750dab6059ec090536c0b313", null ], - [ "update_stability", "group__Methods-Missions-Segments-Common.html#ga9924ff4f90b841fb8915dbd71786ed2f", null ], - [ "update_sub_segments", "group__Methods-Missions-Segments-Common.html#gab45c41851f057901a21d150205c8279a", null ], - [ "update_thrust", "group__Methods-Missions-Segments-Common.html#ga561d5582a141f6b2d2868bf3e01c0797", null ], - [ "update_weights", "group__Methods-Missions-Segments-Common.html#gab48e9a5d35173af364ff2ffc2e5be796", null ] + [ "compute_noise", "group__Methods-Missions-Segments-Common.html#gab25b3bf4461f86b25c9272cdc8954204", null ], + [ "expand_sub_segments", "group__Methods-Missions-Segments-Common.html#ga6daa88d9829c3d1d2a547810947d4a3c", null ], + [ "finalize_sub_segments", "group__Methods-Missions-Segments-Common.html#ga12ffcf4ab47cd7d28f1a9a171a6519a8", null ], + [ "initialize_battery", "group__Methods-Missions-Segments-Common.html#ga2d1fbae1a3d75b6bff959416cea6b2bc", null ], + [ "initialize_differentials_dimensionless", "group__Methods-Missions-Segments-Common.html#ga95d954f0a6106fc6808b99656bd6b124", null ], + [ "initialize_inertial_position", "group__Methods-Missions-Segments-Common.html#ga1156e790a628b711f1ba755ea263381f", null ], + [ "initialize_planet_position", "group__Methods-Missions-Segments-Common.html#gab3e06356d021abd5beac1dfc9609ade4", null ], + [ "initialize_time", "group__Methods-Missions-Segments-Common.html#ga77b0ef727f5db7b26db66b1ae5b736b4", null ], + [ "initialize_weights", "group__Methods-Missions-Segments-Common.html#gab1cfc63a475da85ea5ce24793a9d3530", null ], + [ "integrate_inertial_horizontal_position", "group__Methods-Missions-Segments-Common.html#gaf69c6bffbcabadc41affca00c1368750", null ], + [ "merge_sub_segment_states", "group__Methods-Missions-Segments-Common.html#ga977b59a06b3c24da4465eaf408b46568", null ], + [ "sequential_sub_segments", "group__Methods-Missions-Segments-Common.html#gae2ef2106e209d63c487fcc82db03a4b5", null ], + [ "unpack_subsegments", "group__Methods-Missions-Segments-Common.html#ga88d18a43598a05f4f6ca0ede91976d61", null ], + [ "update_acceleration", "group__Methods-Missions-Segments-Common.html#gad60c1db33ae02132ec99817580c1b13f", null ], + [ "update_aerodynamics", "group__Methods-Missions-Segments-Common.html#ga98e8a131c94c8ca91ea43796253af27b", null ], + [ "update_altitude", "group__Methods-Missions-Segments-Common.html#ga694fc476896214803aa0b0690024568e", null ], + [ "update_atmosphere", "group__Methods-Missions-Segments-Common.html#gaba01c26ea31658e5bbed04c56a471947", null ], + [ "update_differentials_time", "group__Methods-Missions-Segments-Common.html#ga664ff1cf31479ef070e7a1353df88f10", null ], + [ "update_forces", "group__Methods-Missions-Segments-Common.html#gaaa0ab579663550b57f10570b4008bcc0", null ], + [ "update_freestream", "group__Methods-Missions-Segments-Common.html#ga71577aa101f1e020335b9a7982d5c8f1", null ], + [ "update_gravity", "group__Methods-Missions-Segments-Common.html#ga0cf7b0afb24e96d7fda0232318db8658", null ], + [ "update_orientations", "group__Methods-Missions-Segments-Common.html#ga37e1a3f862ef062b8ebc9922c578a25b", null ], + [ "update_planet_position", "group__Methods-Missions-Segments-Common.html#ga0a70f6d415591cc5b46917721a060cf6", null ], + [ "update_stability", "group__Methods-Missions-Segments-Common.html#ga685edc13b4ddfa3bf1c5e7e423536a02", null ], + [ "update_sub_segments", "group__Methods-Missions-Segments-Common.html#ga818e25d6f45f574f9d49269a14893f8c", null ], + [ "update_thrust", "group__Methods-Missions-Segments-Common.html#gafb4c710fd0c7048ca8622d6d2779d6f4", null ], + [ "update_weights", "group__Methods-Missions-Segments-Common.html#ga36dcf82dc25085d74304894ba88f6731", null ] ]; \ No newline at end of file diff --git a/doxygen/group__Methods-Missions-Segments-Cruise.html b/doxygen/group__Methods-Missions-Segments-Cruise.html index 59d0cb08..1df66a74 100644 --- a/doxygen/group__Methods-Missions-Segments-Cruise.html +++ b/doxygen/group__Methods-Missions-Segments-Cruise.html @@ -1,9 +1,9 @@ - + - + SUAVE: Cruise @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@
- +
@@ -73,7 +78,9 @@
@@ -103,93 +110,89 @@ - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +

Functions

def SUAVE.Methods.Missions.Segments.Cruise.Common.unpack_unknowns (segment, state)
 
def SUAVE.Methods.Missions.Segments.Cruise.Common.residual_total_forces (segment, state)
 
def SUAVE.Methods.Missions.Segments.Cruise.Constant_Acceleration_Constant_Altitude.initialize_conditions (segment, state)
 Constant_Accleration_Constant_Altitude.py. More...
 
def SUAVE.Methods.Missions.Segments.Cruise.Constant_Acceleration_Constant_Altitude.residual_total_forces (segment, state)
 
def SUAVE.Methods.Missions.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude.initialize_conditions (segment, state)
 
def SUAVE.Methods.Missions.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude_Loiter.initialize_conditions (segment, state)
 
def SUAVE.Methods.Missions.Segments.Cruise.Constant_Mach_Constant_Altitude.initialize_conditions (segment, state)
 
def SUAVE.Methods.Missions.Segments.Cruise.Constant_Mach_Constant_Altitude_Loiter.initialize_conditions (segment, state)
 
def SUAVE.Methods.Missions.Segments.Cruise.Constant_Pitch_Rate_Constant_Altitude.initialize_conditions (segment, state)
 
def SUAVE.Methods.Missions.Segments.Cruise.Constant_Pitch_Rate_Constant_Altitude.residual_total_forces (segment, state)
 
def SUAVE.Methods.Missions.Segments.Cruise.Constant_Pitch_Rate_Constant_Altitude.unpack_unknowns (segment, state)
 
def SUAVE.Methods.Missions.Segments.Cruise.Constant_Speed_Constant_Altitude.initialize_conditions (segment, state)
 Constant_Speed_Constant_Altitude.py. More...
 
def SUAVE.Methods.Missions.Segments.Cruise.Constant_Speed_Constant_Altitude_Loiter.initialize_conditions (segment, state)
 
-def SUAVE.Methods.Missions.Segments.Cruise.Constant_Throttle_Constant_Altitude.unpack_unknowns (segment, state)
 
def SUAVE.Methods.Missions.Segments.Cruise.Constant_Throttle_Constant_Altitude.initialize_conditions (segment, state)
 
def SUAVE.Methods.Missions.Segments.Cruise.Constant_Throttle_Constant_Altitude.solve_residuals (segment, state)
 
def SUAVE.Methods.Missions.Segments.Cruise.Variable_Cruise_Distance.initialize_cruise_distance (segment, state)
 Variable_Cruise_Distance.py. More...
 
def SUAVE.Methods.Missions.Segments.Cruise.Variable_Cruise_Distance.unknown_cruise_distance (segment, state)
 
def SUAVE.Methods.Missions.Segments.Cruise.Variable_Cruise_Distance.residual_landing_weight (segment, state)
 
def SUAVE.Methods.Missions.Segments.Cruise.Common.unpack_unknowns (segment)
 
def SUAVE.Methods.Missions.Segments.Cruise.Common.residual_total_forces (segment)
 
def SUAVE.Methods.Missions.Segments.Cruise.Constant_Acceleration_Constant_Altitude.initialize_conditions (segment)
 Constant_Acceleration_Constant_Altitude.py. More...
 
def SUAVE.Methods.Missions.Segments.Cruise.Constant_Acceleration_Constant_Altitude.residual_total_forces (segment)
 
def SUAVE.Methods.Missions.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude.initialize_conditions (segment)
 
def SUAVE.Methods.Missions.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude_Loiter.initialize_conditions (segment)
 
def SUAVE.Methods.Missions.Segments.Cruise.Constant_Mach_Constant_Altitude.initialize_conditions (segment)
 
def SUAVE.Methods.Missions.Segments.Cruise.Constant_Mach_Constant_Altitude_Loiter.initialize_conditions (segment)
 
def SUAVE.Methods.Missions.Segments.Cruise.Constant_Pitch_Rate_Constant_Altitude.initialize_conditions (segment)
 
def SUAVE.Methods.Missions.Segments.Cruise.Constant_Pitch_Rate_Constant_Altitude.residual_total_forces (segment)
 
def SUAVE.Methods.Missions.Segments.Cruise.Constant_Pitch_Rate_Constant_Altitude.unpack_unknowns (segment)
 
def SUAVE.Methods.Missions.Segments.Cruise.Constant_Speed_Constant_Altitude.initialize_conditions (segment)
 Constant_Speed_Constant_Altitude.py. More...
 
def SUAVE.Methods.Missions.Segments.Cruise.Constant_Speed_Constant_Altitude_Loiter.initialize_conditions (segment)
 
+def SUAVE.Methods.Missions.Segments.Cruise.Constant_Throttle_Constant_Altitude.unpack_unknowns (segment)
 
def SUAVE.Methods.Missions.Segments.Cruise.Constant_Throttle_Constant_Altitude.initialize_conditions (segment)
 
def SUAVE.Methods.Missions.Segments.Cruise.Constant_Throttle_Constant_Altitude.solve_residuals (segment)
 
def SUAVE.Methods.Missions.Segments.Cruise.Variable_Cruise_Distance.initialize_cruise_distance (segment)
 Variable_Cruise_Distance.py. More...
 
def SUAVE.Methods.Missions.Segments.Cruise.Variable_Cruise_Distance.unknown_cruise_distance (segment)
 
def SUAVE.Methods.Missions.Segments.Cruise.Variable_Cruise_Distance.residual_landing_weight (segment)
 
def SUAVE.Methods.Missions.Segments.Cruise.Variable_Cruise_Distance.residual_state_of_charge (segment)
 
def SUAVE.Methods.Missions.Segments.Single_Point.Set_Speed_Set_Altitude_No_Propulsion.unpack_unknowns (segment)
 
def SUAVE.Methods.Missions.Segments.Transition.Constant_Acceleration_Constant_Angle_Linear_Climb.residual_total_forces (segment)
 
def SUAVE.Methods.Missions.Segments.Transition.Constant_Acceleration_Constant_Pitchrate_Constant_Altitude.residual_total_forces (segment)
 

Detailed Description

Cruise mission methods containing the functions for setting up and solving a mission.

Function Documentation

- -

◆ initialize_conditions() [1/9]

+ +

◆ initialize_conditions() [1/9]

- + - - - - - - - - - + - -
def SUAVE.Methods.Missions.Segments.Cruise.Constant_Acceleration_Constant_Altitude.initialize_conditions def SUAVE.Methods.Missions.Segments.Cruise.Constant_Speed_Constant_Altitude.initialize_conditions (  segment,
 state 
segment) )
-

Constant_Accleration_Constant_Altitude.py.

-

Created: Jul 2014, SUAVE Team Modified: Jan 2016, E. Botero

Sets the specified conditions which are given for the segment type.
+

Constant_Speed_Constant_Altitude.py.

+

Created: Jul 2014, SUAVE Team Modified: Jan 2016, E. Botero May 2019, T. MacDonald

Sets the specified conditions which are given for the segment type.
 
 Assumptions:
-Constant acceleration and constant altitude
+Constant speed and constant altitude
 
 Source:
 N/A
 
 Inputs:
 segment.altitude                [meters]
-segment.air_speed_start         [meters/second]
-segment.air_speed_end           [meters/second]
-segment.acceleration            [meters/second^2]
-conditions.frames.inertial.time [seconds]
+segment.distance                [meters]
+segment.speed                   [meters/second]
 
 Outputs:
 conditions.frames.inertial.velocity_vector  [meters/second]
@@ -202,45 +205,37 @@ 

-

◆ initialize_conditions() [2/9]

+ +

◆ initialize_conditions() [2/9]

- + - - - - + - - - - - - -
def SUAVE.Methods.Missions.Segments.Cruise.Constant_Speed_Constant_Altitude.initialize_conditions def SUAVE.Methods.Missions.Segments.Cruise.Constant_Acceleration_Constant_Altitude.initialize_conditions (  segment,
segment)  state 
)
-

Constant_Speed_Constant_Altitude.py.

-

Created: Jul 2014, SUAVE Team Modified: Jan 2016, E. Botero

Sets the specified conditions which are given for the segment type.
+

Constant_Acceleration_Constant_Altitude.py.

+

Created: Jul 2014, SUAVE Team Modified: Jan 2016, E. Botero May 2019, T. MacDonald Mar 2020, M. Clarke

Sets the specified conditions which are given for the segment type.
 
 Assumptions:
-Constant speed and constant altitude
+Constant acceleration and constant altitude
 
 Source:
 N/A
 
 Inputs:
 segment.altitude                [meters]
-segment.distance                [meters]
-segment.speed                   [meters/second]
+segment.air_speed_start         [meters/second]
+segment.air_speed_end           [meters/second]
+segment.acceleration            [meters/second^2]
+conditions.frames.inertial.time [seconds]
 
 Outputs:
 conditions.frames.inertial.velocity_vector  [meters/second]
@@ -253,35 +248,25 @@ 

-

◆ initialize_conditions() [3/9]

+ +

◆ initialize_conditions() [3/9]

- + - - - - + - - - - - - -
def SUAVE.Methods.Missions.Segments.Cruise.Constant_Mach_Constant_Altitude_Loiter.initialize_conditions def SUAVE.Methods.Missions.Segments.Cruise.Constant_Speed_Constant_Altitude_Loiter.initialize_conditions (  segment,
segment)  state 
)
Sets the specified conditions which are given for the segment type.
 
 Assumptions:
-Constant mach and constant altitude with set loiter time
+Constant speed and constant altitude with set loiter time
 
 Source:
 N/A
@@ -289,7 +274,7 @@ 

-

◆ initialize_conditions() [4/9]

+ +

◆ initialize_conditions() [4/9]

- + - - - - + - - - - - - -
def SUAVE.Methods.Missions.Segments.Cruise.Constant_Pitch_Rate_Constant_Altitude.initialize_conditions def SUAVE.Methods.Missions.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude.initialize_conditions (  segment,
segment)  state 
)
Sets the specified conditions which are given for the segment type.
 
 Assumptions:
-Constant acceleration and constant altitude
+Constant dynamic pressure and constant altitude
 
 Source:
 N/A
 
 Inputs:
 segment.altitude                [meters]
-segment.pitch_initial           [radians]
-segment.pitch_final             [radians]
-segment.pitch_rate              [radians/second]
+segment.distance                [meters]
+segment.dynamic_pressure        [pascals]
 
 Outputs:
-conditions.frames.body.inertial_rotations   [radians/second]
+conditions.frames.inertial.velocity_vector  [meters/second]
 conditions.frames.inertial.position_vector  [meters]
 conditions.freestream.altitude              [meters]
 conditions.frames.inertial.time             [seconds]
@@ -352,42 +326,32 @@ 

-

◆ initialize_conditions() [5/9]

+ +

◆ initialize_conditions() [5/9]

- + - - - - - - - - - + - -
def SUAVE.Methods.Missions.Segments.Cruise.Constant_Mach_Constant_Altitude.initialize_conditions def SUAVE.Methods.Missions.Segments.Cruise.Constant_Mach_Constant_Altitude_Loiter.initialize_conditions (  segment,
 state 
segment) )
Sets the specified conditions which are given for the segment type.
 
 Assumptions:
-Constant mach and constant altitude
+Constant mach and constant altitude with set loiter time
 
 Source:
 N/A
 
 Inputs:
 segment.altitude                [meters]
-segment.distance                [meters]
+segment.time                    [seconds]
 segment.mach                    [unitless]
 
 Outputs:
@@ -401,46 +365,37 @@ 

-

◆ initialize_conditions() [6/9]

+ +

◆ initialize_conditions() [6/9]

- + - - - - - - - - - + - -
def SUAVE.Methods.Missions.Segments.Cruise.Constant_Speed_Constant_Altitude_Loiter.initialize_conditions def SUAVE.Methods.Missions.Segments.Cruise.Constant_Pitch_Rate_Constant_Altitude.initialize_conditions (  segment,
 state 
segment) )
Sets the specified conditions which are given for the segment type.
 
 Assumptions:
-Constant speed and constant altitude with set loiter time
+Constant acceleration and constant altitude
 
 Source:
 N/A
 
 Inputs:
 segment.altitude                [meters]
-segment.time                    [seconds]
-segment.speed                   [meters/second]
+segment.pitch_initial           [radians]
+segment.pitch_final             [radians]
+segment.pitch_rate              [radians/second]
 
 Outputs:
-conditions.frames.inertial.velocity_vector  [meters/second]
+conditions.frames.body.inertial_rotations   [radians/second]
 conditions.frames.inertial.position_vector  [meters]
 conditions.freestream.altitude              [meters]
 conditions.frames.inertial.time             [seconds]
@@ -450,42 +405,32 @@ 

-

◆ initialize_conditions() [7/9]

+ +

◆ initialize_conditions() [7/9]

- + - - - - - - - - - + - -
def SUAVE.Methods.Missions.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude.initialize_conditions def SUAVE.Methods.Missions.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude_Loiter.initialize_conditions (  segment,
 state 
segment) )
Sets the specified conditions which are given for the segment type.
 
 Assumptions:
-Constant dynamic pressure and constant altitude
+Constant dynamic pressure and constant altitude with set loiter time
 
 Source:
 N/A
 
 Inputs:
 segment.altitude                [meters]
-segment.distance                [meters]
+segment.time                    [seconds]
 segment.dynamic_pressure        [pascals]
 
 Outputs:
@@ -499,43 +444,33 @@ 

-

◆ initialize_conditions() [8/9]

+ +

◆ initialize_conditions() [8/9]

- + - - - - + - - - - - - -
def SUAVE.Methods.Missions.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude_Loiter.initialize_conditions def SUAVE.Methods.Missions.Segments.Cruise.Constant_Mach_Constant_Altitude.initialize_conditions (  segment,
segment)  state 
)
Sets the specified conditions which are given for the segment type.
 
 Assumptions:
-Constant dynamic pressure and constant altitude with set loiter time
+Constant mach and constant altitude
 
 Source:
 N/A
 
 Inputs:
 segment.altitude                [meters]
-segment.time                    [seconds]
-segment.dynamic_pressure        [pascals]
+segment.distance                [meters]
+segment.mach                    [unitless]
 
 Outputs:
 conditions.frames.inertial.velocity_vector  [meters/second]
@@ -548,8 +483,8 @@ 

-

◆ initialize_conditions() [9/9]

+ +

◆ initialize_conditions() [9/9]

@@ -598,8 +523,8 @@

-

◆ initialize_cruise_distance()

+ +

◆ initialize_cruise_distance()

Variable_Cruise_Distance.py.

-

Created: Jul 2014, SUAVE Team Modified: Jan 2016, E. Botero

This is a method that allows your vehicle to land at prescribed landing weight
+

Created: Jul 2014, SUAVE Team Modified: Jan 2016, E. Botero Aug 2021, M. Clarke

This is a method that allows your vehicle to land at prescribed landing weight
 
 Assumptions:
 N/A
@@ -645,8 +560,8 @@ 

-

◆ residual_landing_weight()

+ +

◆ residual_landing_weight()

@@ -680,39 +585,65 @@

-

◆ residual_total_forces() [1/3]

+ +

◆ residual_state_of_charge()

- + - - - - + - - +
def SUAVE.Methods.Missions.Segments.Cruise.Common.residual_total_forces def SUAVE.Methods.Missions.Segments.Cruise.Variable_Cruise_Distance.residual_state_of_charge (  segment,
segment)  state 
+
+
This is a method that allows your vehicle to land at a prescribed state of charge.
+This takes the final weight and compares it against the prescribed state of charge.
+
+Assumptions:
+N/A
+
+Source:
+N/A
+
+Inputs:
+segment.state.segments[-1].conditions.propulsion.battery_state_of_charge [None]
+segment.target_state_of_charge                                           [None]
+
+Outputs:
+segment.state.residuals.battery_state_of_charge                          [None]
+
+Properties Used:
+N/A
+
+
+
+ +

◆ residual_total_forces() [1/5]

+ +
+
+ + + + + - -
def SUAVE.Methods.Missions.Segments.Cruise.Common.residual_total_forces ( segment) )
@@ -722,19 +653,19 @@

-

◆ residual_total_forces() [2/3]

+ +

◆ residual_total_forces() [2/5]

@@ -778,8 +699,8 @@

-

◆ residual_total_forces() [3/3]

+ +

◆ residual_total_forces() [3/5]

@@ -823,28 +734,88 @@

-

◆ solve_residuals()

+ +

◆ residual_total_forces() [4/5]

- + - + + +
def SUAVE.Methods.Missions.Segments.Cruise.Constant_Throttle_Constant_Altitude.solve_residuals def SUAVE.Methods.Missions.Segments.Transition.Constant_Acceleration_Constant_Pitchrate_Constant_Altitude.residual_total_forces (  segment, segment)
+
+
Calculates a residual based on forces
+
+    Assumptions:
+    The vehicle is not accelerating, doesn't use gravity
+    
+    Inputs:
+        segment.acceleration                   [meters/second^2]
+        segment.state.ones_row                 [vector]
+        state.conditions:
+            frames.inertial.total_force_vector [Newtons]
+            weights.total_mass                 [kg]
+        
+    Outputs:
+        state.conditions:
+            state.residuals.forces [meters/second^2]
+
+    Properties Used:
+    N/A
+
+
+ +

◆ residual_total_forces() [5/5]

+ +
+
+ - - + + - + + +
def SUAVE.Methods.Missions.Segments.Transition.Constant_Acceleration_Constant_Angle_Linear_Climb.residual_total_forces (  state segment)
+
+
Calculates a residual based on forces
+
+    Assumptions:
+    The vehicle is not accelerating, doesn't use gravity
+    
+    Inputs:
+        segment.acceleration                   [meters/second^2]
+        segment.state.ones_row                 [vector]
+        state.conditions:
+            frames.inertial.total_force_vector [Newtons]
+            weights.total_mass                 [kg]
+        
+    Outputs:
+        state.conditions:
+            state.residuals.forces [meters/second^2]
+
+    Properties Used:
+    N/A
+
+
+ +

◆ solve_residuals()

+ +
+
+ + + + + - -
def SUAVE.Methods.Missions.Segments.Cruise.Constant_Throttle_Constant_Altitude.solve_residuals ( segment) )
@@ -855,25 +826,25 @@

-

◆ unknown_cruise_distance()

+ +

◆ unknown_cruise_distance()

@@ -917,8 +878,8 @@

-

◆ unpack_unknowns() [1/2]

+ +

◆ unpack_unknowns() [1/3]

+ +

◆ unpack_unknowns() [2/3]

+ +
+
+ + + + + - -
def SUAVE.Methods.Missions.Segments.Single_Point.Set_Speed_Set_Altitude_No_Propulsion.unpack_unknowns ( segment) )
@@ -961,8 +946,8 @@

-

◆ unpack_unknowns() [2/2]

+ +

◆ unpack_unknowns() [3/3]

diff --git a/doxygen/group__Methods-Missions-Segments-Cruise.js b/doxygen/group__Methods-Missions-Segments-Cruise.js index 41dc0574..1b83711b 100644 --- a/doxygen/group__Methods-Missions-Segments-Cruise.js +++ b/doxygen/group__Methods-Missions-Segments-Cruise.js @@ -1,21 +1,25 @@ var group__Methods_Missions_Segments_Cruise = [ - [ "initialize_conditions", "group__Methods-Missions-Segments-Cruise.html#gaeceef878340ee4ca38c91d9b9d4b1825", null ], - [ "initialize_conditions", "group__Methods-Missions-Segments-Cruise.html#gae83d32238010a7766ce5f6f59c665171", null ], - [ "initialize_conditions", "group__Methods-Missions-Segments-Cruise.html#gaa1662df44e801b11b5cee1cec98ddddb", null ], - [ "initialize_conditions", "group__Methods-Missions-Segments-Cruise.html#ga1225173de6209af379d294d66aae3765", null ], - [ "initialize_conditions", "group__Methods-Missions-Segments-Cruise.html#ga2392289bf9075cc49a7e82593eff969b", null ], - [ "initialize_conditions", "group__Methods-Missions-Segments-Cruise.html#ga5629f4cd6d3db707b418a90e3b83c4cf", null ], - [ "initialize_conditions", "group__Methods-Missions-Segments-Cruise.html#ga8fe5b4a602fc2842046270b062c0725f", null ], - [ "initialize_conditions", "group__Methods-Missions-Segments-Cruise.html#ga31753e9e792ee9b624a0b0c52a339839", null ], - [ "initialize_conditions", "group__Methods-Missions-Segments-Cruise.html#gafb9a53c01768546934f739572cba457e", null ], - [ "initialize_cruise_distance", "group__Methods-Missions-Segments-Cruise.html#ga5c2953ac08ccf0627c021f6ed58b2bf5", null ], - [ "residual_landing_weight", "group__Methods-Missions-Segments-Cruise.html#gab9d38bfe2130ae943109fd2b9daaf8bd", null ], - [ "residual_total_forces", "group__Methods-Missions-Segments-Cruise.html#gad0c58596842a06b26ce45ae82de1f553", null ], - [ "residual_total_forces", "group__Methods-Missions-Segments-Cruise.html#ga94d5d0eeaad27145f52e2281d66b518d", null ], - [ "residual_total_forces", "group__Methods-Missions-Segments-Cruise.html#gadb8015617e942644480f81b10df76f6d", null ], - [ "solve_residuals", "group__Methods-Missions-Segments-Cruise.html#gac7b8afbde2853ba75656032eb9f71e40", null ], - [ "unknown_cruise_distance", "group__Methods-Missions-Segments-Cruise.html#gaf312be28fd54ce6ef3252aa138066d97", null ], - [ "unpack_unknowns", "group__Methods-Missions-Segments-Cruise.html#gac16b02c25a09a594b81e8a5846c5ec12", null ], - [ "unpack_unknowns", "group__Methods-Missions-Segments-Cruise.html#ga1a0168bbee3e90402744d6b35a6b1e74", null ] + [ "initialize_conditions", "group__Methods-Missions-Segments-Cruise.html#ga79a8e04d4b9a7ef60a20b41159716b9f", null ], + [ "initialize_conditions", "group__Methods-Missions-Segments-Cruise.html#gaa9cb4502abf3d411597efe073f1980bc", null ], + [ "initialize_conditions", "group__Methods-Missions-Segments-Cruise.html#ga88b80e3f3553dff9dc252e039e3e4c0e", null ], + [ "initialize_conditions", "group__Methods-Missions-Segments-Cruise.html#ga95c31c42eef71aaf6d81eaf2041c37e8", null ], + [ "initialize_conditions", "group__Methods-Missions-Segments-Cruise.html#gaeb26c1b79cf18f76b443c7a0bd1b664f", null ], + [ "initialize_conditions", "group__Methods-Missions-Segments-Cruise.html#gafd65f529699028d9f44a706973c9c67b", null ], + [ "initialize_conditions", "group__Methods-Missions-Segments-Cruise.html#ga3891ab9c9ad75efcade97e9256166ce0", null ], + [ "initialize_conditions", "group__Methods-Missions-Segments-Cruise.html#gaa9e0bbb165ab2c9b1a19971810a0327d", null ], + [ "initialize_conditions", "group__Methods-Missions-Segments-Cruise.html#ga32a31f8de3519a3ee9973bf128e6e30b", null ], + [ "initialize_cruise_distance", "group__Methods-Missions-Segments-Cruise.html#ga5fbb9c089e2317ecc5f01ec41d718eaa", null ], + [ "residual_landing_weight", "group__Methods-Missions-Segments-Cruise.html#gaab9cd744963f58e79de0e31b719c8a5b", null ], + [ "residual_state_of_charge", "group__Methods-Missions-Segments-Cruise.html#ga48d38d17606e2b0a53b19a6aaae0d51e", null ], + [ "residual_total_forces", "group__Methods-Missions-Segments-Cruise.html#gaafbd9d1fb34d3aefa0577719d85900d3", null ], + [ "residual_total_forces", "group__Methods-Missions-Segments-Cruise.html#ga4965e6d4c12a0e9ef199664495a29b25", null ], + [ "residual_total_forces", "group__Methods-Missions-Segments-Cruise.html#ga14c1265adeb5c7c5ecb8d871a27cdbfd", null ], + [ "residual_total_forces", "group__Methods-Missions-Segments-Cruise.html#ga17c347be29f6734619ac52092c16a54b", null ], + [ "residual_total_forces", "group__Methods-Missions-Segments-Cruise.html#ga5614ac9012f5178df121df650ba98f02", null ], + [ "solve_residuals", "group__Methods-Missions-Segments-Cruise.html#ga7e83a826f2b8b739f7dbdfb8cbe06723", null ], + [ "unknown_cruise_distance", "group__Methods-Missions-Segments-Cruise.html#ga6e72808af73f68c8b85178ef8e054ac4", null ], + [ "unpack_unknowns", "group__Methods-Missions-Segments-Cruise.html#gad28061436854da468ebbbcdd4aa7e489", null ], + [ "unpack_unknowns", "group__Methods-Missions-Segments-Cruise.html#ga9e0a1945e924aacb50a5b42284a6e483", null ], + [ "unpack_unknowns", "group__Methods-Missions-Segments-Cruise.html#gabf1dcca43c3a644839b1822542decfab", null ] ]; \ No newline at end of file diff --git a/doxygen/group__Methods-Missions-Segments-Descent.html b/doxygen/group__Methods-Missions-Segments-Descent.html index 9487819f..93d3240b 100644 --- a/doxygen/group__Methods-Missions-Segments-Descent.html +++ b/doxygen/group__Methods-Missions-Segments-Descent.html @@ -1,9 +1,9 @@ - + - + SUAVE: Descent @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@
- +

@@ -73,7 +78,9 @@
@@ -103,22 +110,24 @@ - - - - - - - - - - + + + + + + + + + + + +

Functions

def SUAVE.Methods.Missions.Segments.Descent.Constant_EAS_Constant_Rate.initialize_conditions (segment, state)
 
def SUAVE.Methods.Missions.Segments.Descent.Constant_Speed_Constant_Angle.initialize_conditions (segment, state)
 
def SUAVE.Methods.Missions.Segments.Descent.Constant_Speed_Constant_Angle_Noise.expand_state (segment, state)
 
def SUAVE.Methods.Missions.Segments.Descent.Constant_Speed_Constant_Angle_Noise.initialize_conditions (segment, state)
 
def SUAVE.Methods.Missions.Segments.Descent.Constant_Speed_Constant_Rate.initialize_conditions (segment, state)
 
def SUAVE.Methods.Missions.Segments.Descent.Constant_CAS_Constant_Rate.initialize_conditions (segment)
 
def SUAVE.Methods.Missions.Segments.Descent.Constant_EAS_Constant_Rate.initialize_conditions (segment)
 
def SUAVE.Methods.Missions.Segments.Descent.Constant_Speed_Constant_Angle.initialize_conditions (segment)
 
def SUAVE.Methods.Missions.Segments.Descent.Constant_Speed_Constant_Angle_Noise.expand_state (segment)
 
def SUAVE.Methods.Missions.Segments.Descent.Constant_Speed_Constant_Angle_Noise.initialize_conditions (segment)
 
def SUAVE.Methods.Missions.Segments.Descent.Constant_Speed_Constant_Rate.initialize_conditions (segment)
 

Detailed Description

Descent mission methods containing the functions for setting up and solving a mission.

Function Documentation

- -

◆ expand_state()

+ +

◆ expand_state()

@@ -163,45 +162,35 @@

-

◆ initialize_conditions() [1/4]

+ +

◆ initialize_conditions() [1/5]

- + - - - - - - - - - + - -
def SUAVE.Methods.Missions.Segments.Descent.Constant_Speed_Constant_Rate.initialize_conditions def SUAVE.Methods.Missions.Segments.Descent.Constant_Speed_Constant_Angle.initialize_conditions (  segment,
 state 
segment) )
Sets the specified conditions which are given for the segment type.
 
 Assumptions:
-Constant speed and constant descent rate
+Constant speed and constant descent angle
 
 Source:
 N/A
 
 Inputs:
-segment.descent_rate                        [meters/second]
-segment.altitude_start                      [meters]
-segment.altitude_end                        [meters]
-segment.air_speed                           [meters/second]
-state.numerics.dimensionless.control_points [array]
+segment.descent_angle                               [radians]
+segment.altitude_start                              [meters]
+segment.altitude_end                                [meters]
+segment.air_speed                                   [meters/second]
+segment.state.numerics.dimensionless.control_points [array]
 
 Outputs:
 conditions.frames.inertial.velocity_vector  [meters/second]
@@ -214,45 +203,35 @@ 

-

◆ initialize_conditions() [2/4]

+ +

◆ initialize_conditions() [2/5]

- + - - - - - - - - - + - -
def SUAVE.Methods.Missions.Segments.Descent.Constant_Speed_Constant_Angle.initialize_conditions def SUAVE.Methods.Missions.Segments.Descent.Constant_Speed_Constant_Rate.initialize_conditions (  segment,
 state 
segment) )
Sets the specified conditions which are given for the segment type.
 
 Assumptions:
-Constant speed and constant descent angle
+Constant speed and constant descent rate
 
 Source:
 N/A
 
 Inputs:
-segment.descent_angle                       [radians]
-segment.altitude_start                      [meters]
-segment.altitude_end                        [meters]
-segment.air_speed                           [meters/second]
-state.numerics.dimensionless.control_points [array]
+segment.descent_rate                                [meters/second]
+segment.altitude_start                              [meters]
+segment.altitude_end                                [meters]
+segment.air_speed                                   [meters/second]
+segment.state.numerics.dimensionless.control_points [array]
 
 Outputs:
 conditions.frames.inertial.velocity_vector  [meters/second]
@@ -265,8 +244,8 @@ 

-

◆ initialize_conditions() [3/4]

+ +

◆ initialize_conditions() [3/5]

+ +

◆ initialize_conditions() [4/5]

+ +
+
+ + + + + - -
def SUAVE.Methods.Missions.Segments.Descent.Constant_CAS_Constant_Rate.initialize_conditions ( segment) )
@@ -299,11 +309,11 @@

-

◆ initialize_conditions() [4/4]

+ +

◆ initialize_conditions() [5/5]

diff --git a/doxygen/group__Methods-Missions-Segments-Descent.js b/doxygen/group__Methods-Missions-Segments-Descent.js index a0881df9..a562dfe4 100644 --- a/doxygen/group__Methods-Missions-Segments-Descent.js +++ b/doxygen/group__Methods-Missions-Segments-Descent.js @@ -1,8 +1,9 @@ var group__Methods_Missions_Segments_Descent = [ - [ "expand_state", "group__Methods-Missions-Segments-Descent.html#gaf42a40b22cba7bb56609d82dd1b675d9", null ], - [ "initialize_conditions", "group__Methods-Missions-Segments-Descent.html#gabbd9496321d7bc45c1796b734d2f4b38", null ], - [ "initialize_conditions", "group__Methods-Missions-Segments-Descent.html#gac8fb34b9581a8fa70713a2ad9d5fa03b", null ], - [ "initialize_conditions", "group__Methods-Missions-Segments-Descent.html#gad7dddc4ee25bf0b1e76687a266ad0025", null ], - [ "initialize_conditions", "group__Methods-Missions-Segments-Descent.html#ga217350b7498475f50bd2893122404dfa", null ] + [ "expand_state", "group__Methods-Missions-Segments-Descent.html#ga898644367b4428d8823439b7e6655d5d", null ], + [ "initialize_conditions", "group__Methods-Missions-Segments-Descent.html#gad6c9b018b7f2c6fd8fb86153bd10ce32", null ], + [ "initialize_conditions", "group__Methods-Missions-Segments-Descent.html#ga709d141110269a5584e1e1e5ad75db85", null ], + [ "initialize_conditions", "group__Methods-Missions-Segments-Descent.html#gaf838417b317552701252b4a4088ad671", null ], + [ "initialize_conditions", "group__Methods-Missions-Segments-Descent.html#ga9601cd791273c490a10467e6aefeaa3e", null ], + [ "initialize_conditions", "group__Methods-Missions-Segments-Descent.html#ga8a3eb0f2d72ac083762d76c50e462263", null ] ]; \ No newline at end of file diff --git a/doxygen/group__Methods-Missions-Segments-Ground.html b/doxygen/group__Methods-Missions-Segments-Ground.html index 6a2640e6..28c0188c 100644 --- a/doxygen/group__Methods-Missions-Segments-Ground.html +++ b/doxygen/group__Methods-Missions-Segments-Ground.html @@ -1,9 +1,9 @@ - + - + SUAVE: Ground @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@
- +

@@ -73,7 +78,9 @@
@@ -103,26 +110,32 @@ - - - - - - - - - - - - - - + + + + + + + + + + + + + + + + + +

Functions

def SUAVE.Methods.Missions.Segments.Ground.Common.unpack_unknowns (segment, state)
 
def SUAVE.Methods.Missions.Segments.Ground.Common.initialize_conditions (segment, state)
 
def SUAVE.Methods.Missions.Segments.Ground.Common.compute_ground_forces (segment, state)
 
def SUAVE.Methods.Missions.Segments.Ground.Common.compute_forces (segment, state)
 
def SUAVE.Methods.Missions.Segments.Ground.Common.solve_residuals (segment, state)
 
def SUAVE.Methods.Missions.Segments.Ground.Landing.initialize_conditions (segment, state)
 
def SUAVE.Methods.Missions.Segments.Ground.Takeoff.initialize_conditions (segment, state)
 
+def SUAVE.Methods.Missions.Segments.Ground.Battery_Charge_Discharge.unpack_unknowns (segment)
 
+def SUAVE.Methods.Missions.Segments.Ground.Battery_Charge_Discharge.initialize_conditions (segment)
 
def SUAVE.Methods.Missions.Segments.Ground.Common.unpack_unknowns (segment)
 
def SUAVE.Methods.Missions.Segments.Ground.Common.initialize_conditions (segment)
 
def SUAVE.Methods.Missions.Segments.Ground.Common.compute_ground_forces (segment)
 
def SUAVE.Methods.Missions.Segments.Ground.Common.compute_forces (segment)
 
def SUAVE.Methods.Missions.Segments.Ground.Common.solve_residuals (segment)
 
def SUAVE.Methods.Missions.Segments.Ground.Landing.initialize_conditions (segment)
 
def SUAVE.Methods.Missions.Segments.Ground.Takeoff.initialize_conditions (segment)
 

Detailed Description

Descent mission methods containing the functions for setting up and solving a mission.

Function Documentation

- -

◆ compute_forces()

+ +

◆ compute_forces()

@@ -150,7 +153,6 @@

-

◆ compute_ground_forces()

+ +

◆ compute_ground_forces()

Compute the rolling friction on the aircraft 
 
 Assumptions:
-Does a force balance to calculate the load on the wheels using only lift. Uses only a single friction coefficient.
+    Does a force balance to calculate the load on the wheels using only lift. Uses only a single friction coefficient.
 
 Source:
-N/A
+    N/A
 
 Inputs:
 conditions:
@@ -207,35 +199,25 @@ 

-

◆ initialize_conditions() [1/3]

+ +

◆ initialize_conditions() [1/3]

- + - - - - - - - - - + - -
def SUAVE.Methods.Missions.Segments.Ground.Takeoff.initialize_conditions def SUAVE.Methods.Missions.Segments.Ground.Landing.initialize_conditions (  segment,
 state 
segment) )
@@ -248,42 +230,30 @@

-

◆ initialize_conditions() [2/3]

+ +

◆ initialize_conditions() [2/3]

- + - - - - - - - - - + - -
def SUAVE.Methods.Missions.Segments.Ground.Landing.initialize_conditions def SUAVE.Methods.Missions.Segments.Ground.Takeoff.initialize_conditions (  segment,
 state 
segment) )
@@ -296,20 +266,22 @@

-

◆ initialize_conditions() [3/3]

+ +

◆ initialize_conditions() [3/3]

- -

◆ solve_residuals()

+ +

◆ solve_residuals()

@@ -389,24 +341,23 @@

-

◆ unpack_unknowns()

+ +

◆ unpack_unknowns()

diff --git a/doxygen/group__Methods-Missions-Segments-Ground.js b/doxygen/group__Methods-Missions-Segments-Ground.js index ab822c8e..653de3db 100644 --- a/doxygen/group__Methods-Missions-Segments-Ground.js +++ b/doxygen/group__Methods-Missions-Segments-Ground.js @@ -1,10 +1,10 @@ var group__Methods_Missions_Segments_Ground = [ - [ "compute_forces", "group__Methods-Missions-Segments-Ground.html#ga85d169294fd62de7c701bc919ee98edc", null ], - [ "compute_ground_forces", "group__Methods-Missions-Segments-Ground.html#gaa3bd9d26957028bad0bedf8c65003279", null ], - [ "initialize_conditions", "group__Methods-Missions-Segments-Ground.html#ga5197a82000f2be0f17faa141c7b5e710", null ], - [ "initialize_conditions", "group__Methods-Missions-Segments-Ground.html#ga5a0f970144080b1a249a75ca5f39fbfc", null ], - [ "initialize_conditions", "group__Methods-Missions-Segments-Ground.html#ga5fa0a3728e6f7a2ff4ca2d264bf618b4", null ], - [ "solve_residuals", "group__Methods-Missions-Segments-Ground.html#gaafc05476619f88953ab2020d62f7c39f", null ], - [ "unpack_unknowns", "group__Methods-Missions-Segments-Ground.html#ga07708893d61d25bb85382fef856dbfe7", null ] + [ "compute_forces", "group__Methods-Missions-Segments-Ground.html#gae64c37d6a29d78ae277b23fad5bcdbab", null ], + [ "compute_ground_forces", "group__Methods-Missions-Segments-Ground.html#gac5702eba1de48280db1cc6cfd765e1f0", null ], + [ "initialize_conditions", "group__Methods-Missions-Segments-Ground.html#ga79f76a5ba13922fac5d38d05c7d966d3", null ], + [ "initialize_conditions", "group__Methods-Missions-Segments-Ground.html#gac79b8586dc810232e67adf72526b5bb7", null ], + [ "initialize_conditions", "group__Methods-Missions-Segments-Ground.html#gaca353ce0fc41da8f58e8670d46c3496b", null ], + [ "solve_residuals", "group__Methods-Missions-Segments-Ground.html#ga4bc1c4547c0fe6a5ab8e6b52d29eb29c", null ], + [ "unpack_unknowns", "group__Methods-Missions-Segments-Ground.html#ga2c4a7fad9df1b6121632c58967de2e10", null ] ]; \ No newline at end of file diff --git a/doxygen/group__Methods-Missions-Segments-Hover.html b/doxygen/group__Methods-Missions-Segments-Hover.html index c4adfec5..d9636684 100644 --- a/doxygen/group__Methods-Missions-Segments-Hover.html +++ b/doxygen/group__Methods-Missions-Segments-Hover.html @@ -1,9 +1,9 @@ - + - + SUAVE: Hover @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@
- +
@@ -73,7 +78,9 @@
@@ -103,26 +110,26 @@ - - - - - - - - - - - - - - + + + + + + + + + + + + + +

Functions

def SUAVE.Methods.Missions.Segments.Hover.Climb.initialize_conditions (segment, state)
 Climb.py. More...
 
def SUAVE.Methods.Missions.Segments.Hover.Common.unpack_unknowns (segment, state)
 Common.py. More...
 
def SUAVE.Methods.Missions.Segments.Hover.Common.residual_total_forces (segment, state)
 
def SUAVE.Methods.Missions.Segments.Hover.Descent.initialize_conditions (segment, state)
 Descent.py. More...
 
def SUAVE.Methods.Missions.Segments.Hover.Hover.initialize_conditions (segment, state)
 Hover.py. More...
 
def SUAVE.Methods.Missions.Segments.Hover.Climb.initialize_conditions (segment)
 Climb.py. More...
 
def SUAVE.Methods.Missions.Segments.Hover.Common.unpack_unknowns (segment)
 Common.py. More...
 
def SUAVE.Methods.Missions.Segments.Hover.Common.residual_total_forces (segment)
 
def SUAVE.Methods.Missions.Segments.Hover.Descent.initialize_conditions (segment)
 Descent.py. More...
 
def SUAVE.Methods.Missions.Segments.Hover.Hover.initialize_conditions (segment)
 Hover.py. More...
 

Detailed Description

Hover mission methods containing the functions for setting up and solving a mission.

Function Documentation

- -

◆ initialize_conditions() [1/3]

+ +

◆ initialize_conditions() [1/3]

@@ -157,11 +154,11 @@

-

◆ initialize_conditions() [2/3]

+ +

◆ initialize_conditions() [2/3]

- + - - - - - - - - - + - -
def SUAVE.Methods.Missions.Segments.Hover.Hover.initialize_conditions def SUAVE.Methods.Missions.Segments.Hover.Descent.initialize_conditions (  segment,
 state 
segment) )
-

Hover.py.

+

Descent.py.

Created: Jan 2016, E. Botero Modified:

Sets the specified conditions which are given for the segment type.
 
 Assumptions:
@@ -210,10 +197,11 @@ 

-

◆ initialize_conditions() [3/3]

+ +

◆ initialize_conditions() [3/3]

- + - - - - - - - - - + - -
def SUAVE.Methods.Missions.Segments.Hover.Descent.initialize_conditions def SUAVE.Methods.Missions.Segments.Hover.Hover.initialize_conditions (  segment,
 state 
segment) )
-

Descent.py.

-

Created: Jan 2016, E. Botero Modified:

Sets the specified conditions which are given for the segment type.
+

Hover.py.

+

Created: Jan 2016, E. Botero Modified: May 2019, T. MacDonald Mar 2020, M. Clarke

Sets the specified conditions which are given for the segment type.
 
 Assumptions:
 Descent segment with a constant rate.
@@ -262,9 +240,8 @@ 

-

◆ residual_total_forces()

+ +

◆ residual_total_forces()

@@ -320,8 +287,8 @@

-

◆ unpack_unknowns()

+ +

◆ unpack_unknowns()

diff --git a/doxygen/group__Methods-Missions-Segments-Hover.js b/doxygen/group__Methods-Missions-Segments-Hover.js index 78d98f5d..605fe79e 100644 --- a/doxygen/group__Methods-Missions-Segments-Hover.js +++ b/doxygen/group__Methods-Missions-Segments-Hover.js @@ -1,8 +1,8 @@ var group__Methods_Missions_Segments_Hover = [ - [ "initialize_conditions", "group__Methods-Missions-Segments-Hover.html#ga9328ce0d2ebc56f4ab7bc415c77ad377", null ], - [ "initialize_conditions", "group__Methods-Missions-Segments-Hover.html#gacb4620638688fa39b69e8ca3c24622e9", null ], - [ "initialize_conditions", "group__Methods-Missions-Segments-Hover.html#ga302afed2dba4fc73d087f885c604f74a", null ], - [ "residual_total_forces", "group__Methods-Missions-Segments-Hover.html#ga4573e7a193846ce40e8e86d6286a77f9", null ], - [ "unpack_unknowns", "group__Methods-Missions-Segments-Hover.html#ga1cf7c2ad01008b2535a9356aab7ee480", null ] + [ "initialize_conditions", "group__Methods-Missions-Segments-Hover.html#ga7152105a81283c08382919021862a533", null ], + [ "initialize_conditions", "group__Methods-Missions-Segments-Hover.html#gafb2a4517f4b78efbf735c71cbecf9b5a", null ], + [ "initialize_conditions", "group__Methods-Missions-Segments-Hover.html#gaf14905f3c14633f36fecc73f2b3e345b", null ], + [ "residual_total_forces", "group__Methods-Missions-Segments-Hover.html#gab21c4ee1e0a1dbe923181117110a8dd6", null ], + [ "unpack_unknowns", "group__Methods-Missions-Segments-Hover.html#ga08f323271a12ad72607cd519dae764a1", null ] ]; \ No newline at end of file diff --git a/doxygen/group__Methods-Missions-Segments-Single__Point.html b/doxygen/group__Methods-Missions-Segments-Single__Point.html index 392d9f40..60a1a774 100644 --- a/doxygen/group__Methods-Missions-Segments-Single__Point.html +++ b/doxygen/group__Methods-Missions-Segments-Single__Point.html @@ -1,9 +1,9 @@ - + - + SUAVE: Single_Point @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@
- +
@@ -73,7 +78,9 @@
@@ -103,22 +110,24 @@ - - - - - - - - - - + + + + + + + + + + + +

Functions

def SUAVE.Methods.Missions.Segments.Single_Point.Set_Speed_Set_Altitude.initialize_conditions (segment, state)
 
def SUAVE.Methods.Missions.Segments.Single_Point.Set_Speed_Set_Altitude.update_weights (segment, state)
 
def SUAVE.Methods.Missions.Segments.Single_Point.Set_Speed_Set_Throttle.initialize_conditions (segment, state)
 
def SUAVE.Methods.Missions.Segments.Single_Point.Set_Speed_Set_Throttle.update_weights (segment, state)
 
def SUAVE.Methods.Missions.Segments.Single_Point.Set_Speed_Set_Throttle.unpack_unknowns (segment, state)
 
def SUAVE.Methods.Missions.Segments.Single_Point.Set_Speed_Set_Altitude.initialize_conditions (segment)
 
def SUAVE.Methods.Missions.Segments.Single_Point.Set_Speed_Set_Altitude.update_weights (segment)
 
def SUAVE.Methods.Missions.Segments.Single_Point.Set_Speed_Set_Altitude_No_Propulsion.initialize_conditions (segment)
 
def SUAVE.Methods.Missions.Segments.Single_Point.Set_Speed_Set_Throttle.initialize_conditions (segment)
 
def SUAVE.Methods.Missions.Segments.Single_Point.Set_Speed_Set_Throttle.update_weights (segment)
 
def SUAVE.Methods.Missions.Segments.Single_Point.Set_Speed_Set_Throttle.unpack_unknowns (segment)
 

Detailed Description

Single Point mission methods containing the functions for setting up and solving a mission.

Function Documentation

- -

◆ initialize_conditions() [1/2]

+ +

◆ initialize_conditions() [1/3]

@@ -168,8 +167,8 @@

-

◆ initialize_conditions() [2/2]

+ +

◆ initialize_conditions() [2/3]

@@ -206,7 +195,7 @@

-

◆ unpack_unknowns()

+ +

◆ initialize_conditions() [3/3]

- + - - - - + - - +
def SUAVE.Methods.Missions.Segments.Single_Point.Set_Speed_Set_Throttle.unpack_unknowns def SUAVE.Methods.Missions.Segments.Single_Point.Set_Speed_Set_Altitude_No_Propulsion.initialize_conditions (  segment,
segment)  state 
+
+
Sets the specified conditions which are given for the segment type.
+
+Assumptions:
+A fixed speed and altitude
+
+Source:
+N/A
+
+Inputs:
+segment.altitude                            [meters]
+segment.air_speed                           [meters/second]
+segment.z_accel                             [meters/second^2]
+
+Outputs:
+conditions.frames.inertial.acceleration_vector [meters/second^2]
+conditions.frames.inertial.velocity_vector     [meters/second]
+conditions.frames.inertial.position_vector     [meters]
+conditions.freestream.altitude                 [meters]
+conditions.frames.inertial.time                [seconds]
+
+Properties Used:
+N/A
+
+
+
+ +

◆ unpack_unknowns()

+ +
+
+ + + + + - -
def SUAVE.Methods.Missions.Segments.Single_Point.Set_Speed_Set_Throttle.unpack_unknowns ( segment) )
@@ -251,12 +270,12 @@

-

◆ update_weights() [1/2]

+ +

◆ update_weights() [1/2]

@@ -311,8 +320,8 @@

-

◆ update_weights() [2/2]

+ +

◆ update_weights() [2/2]

diff --git a/doxygen/group__Methods-Missions-Segments-Single__Point.js b/doxygen/group__Methods-Missions-Segments-Single__Point.js index d3401a1c..4991ab24 100644 --- a/doxygen/group__Methods-Missions-Segments-Single__Point.js +++ b/doxygen/group__Methods-Missions-Segments-Single__Point.js @@ -1,8 +1,9 @@ var group__Methods_Missions_Segments_Single__Point = [ - [ "initialize_conditions", "group__Methods-Missions-Segments-Single__Point.html#gaab3442c514383fad1367ab5bdefdc1f8", null ], - [ "initialize_conditions", "group__Methods-Missions-Segments-Single__Point.html#ga090e629e786b91635afbecc678c9cd9e", null ], - [ "unpack_unknowns", "group__Methods-Missions-Segments-Single__Point.html#gaa50cc92ee0391088fb1e5adb35a35ddd", null ], - [ "update_weights", "group__Methods-Missions-Segments-Single__Point.html#ga0e4950f3684d067bab0a32c92b74b07e", null ], - [ "update_weights", "group__Methods-Missions-Segments-Single__Point.html#gabc3632cdc444579b2fb132baafbe76de", null ] + [ "initialize_conditions", "group__Methods-Missions-Segments-Single__Point.html#ga1706b4226f6ef7905f7673ab79c23e99", null ], + [ "initialize_conditions", "group__Methods-Missions-Segments-Single__Point.html#ga3f8060f2a8b42d62427332a0cc8d5f6b", null ], + [ "initialize_conditions", "group__Methods-Missions-Segments-Single__Point.html#gac9ccfcd750cfb15bad47feb59835620a", null ], + [ "unpack_unknowns", "group__Methods-Missions-Segments-Single__Point.html#gad196e795abec33b961dca88873fb1b6a", null ], + [ "update_weights", "group__Methods-Missions-Segments-Single__Point.html#ga93f0e3713dd2d0d1cb29fb2ba1256c1c", null ], + [ "update_weights", "group__Methods-Missions-Segments-Single__Point.html#ga6a0ee5bf82d7625c75441b6809b05a36", null ] ]; \ No newline at end of file diff --git a/doxygen/group__Methods-Missions-Segments-Transition.html b/doxygen/group__Methods-Missions-Segments-Transition.html new file mode 100644 index 00000000..34c38a94 --- /dev/null +++ b/doxygen/group__Methods-Missions-Segments-Transition.html @@ -0,0 +1,217 @@ + + + + + + + +SUAVE: Transition + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
Transition
+
+
+ +

Transition mission methods containing the functions for setting up and solving a mission. +More...

+ + + + + + + +

+Functions

def SUAVE.Methods.Missions.Segments.Transition.Constant_Acceleration_Constant_Angle_Linear_Climb.initialize_conditions (segment)
 
def SUAVE.Methods.Missions.Segments.Transition.Constant_Acceleration_Constant_Pitchrate_Constant_Altitude.initialize_conditions (segment)
 Constant_Acceleration_Constant_Pitchrate_Constant_Altitude.py. More...
 
+

Detailed Description

+

Transition mission methods containing the functions for setting up and solving a mission.

+

Function Documentation

+ +

◆ initialize_conditions() [1/2]

+ +
+
+ + + + + + + + +
def SUAVE.Methods.Missions.Segments.Transition.Constant_Acceleration_Constant_Angle_Linear_Climb.initialize_conditions ( segment)
+
+
Sets the specified conditions which are given for the segment type.
+
+Assumptions:
+Constant acceleration and constant altitude
+
+Source:
+N/A
+
+Inputs:
+segment.altitude                [meters]
+segment.air_speed_start         [meters/second]
+segment.air_speed_end           [meters/second]
+segment.acceleration            [meters/second^2]
+conditions.frames.inertial.time [seconds]
+
+Outputs:
+conditions.frames.inertial.velocity_vector  [meters/second]
+conditions.frames.inertial.position_vector  [meters]
+conditions.freestream.altitude              [meters]
+conditions.frames.inertial.time             [seconds]
+
+Properties Used:
+N/A
+
+
+
+ +

◆ initialize_conditions() [2/2]

+ +
+
+ + + + + + + + +
def SUAVE.Methods.Missions.Segments.Transition.Constant_Acceleration_Constant_Pitchrate_Constant_Altitude.initialize_conditions ( segment)
+
+ +

Constant_Acceleration_Constant_Pitchrate_Constant_Altitude.py.

+

Created: Jul 2014, SUAVE Team Modified: Jan 2016, E. Botero

Sets the specified conditions which are given for the segment type.
+
+Assumptions:
+Constant acceleration and constant altitude
+
+Source:
+N/A
+
+Inputs:
+segment.altitude                [meters]
+segment.air_speed_start         [meters/second]
+segment.air_speed_end           [meters/second]
+segment.acceleration            [meters/second^2]
+conditions.frames.inertial.time [seconds]
+
+Outputs:
+conditions.frames.inertial.velocity_vector  [meters/second]
+conditions.frames.inertial.position_vector  [meters]
+conditions.freestream.altitude              [meters]
+conditions.frames.inertial.time             [seconds]
+
+Properties Used:
+N/A
+
+
+
+
+
+ + + + diff --git a/doxygen/group__Methods-Missions-Segments-Transition.js b/doxygen/group__Methods-Missions-Segments-Transition.js new file mode 100644 index 00000000..2bbf20fe --- /dev/null +++ b/doxygen/group__Methods-Missions-Segments-Transition.js @@ -0,0 +1,5 @@ +var group__Methods_Missions_Segments_Transition = +[ + [ "initialize_conditions", "group__Methods-Missions-Segments-Transition.html#gaa89c32794ff3c0e07de5fe043b83d42e", null ], + [ "initialize_conditions", "group__Methods-Missions-Segments-Transition.html#ga585e7de3376bc84c36bb9a0f0088e117", null ] +]; \ No newline at end of file diff --git a/doxygen/group__Methods-Missions-Segments.html b/doxygen/group__Methods-Missions-Segments.html index 0d592458..367b3faa 100644 --- a/doxygen/group__Methods-Missions-Segments.html +++ b/doxygen/group__Methods-Missions-Segments.html @@ -1,9 +1,9 @@ - + - + SUAVE: Segments @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@
- +
@@ -73,7 +78,9 @@
@@ -125,31 +132,34 @@  Single_Point  Single Point mission methods containing the functions for setting up and solving a mission.
  + Transition + Transition mission methods containing the functions for setting up and solving a mission.
+  - - - - - - - - - - - - - - - - + + + + + + + + + + + + + + + +

Functions

def SUAVE.Methods.Missions.Segments.converge_root.converge_root (segment, state)
 
def SUAVE.Methods.Missions.Segments.converge_root.iterate (unknowns, segment, state)
 
def SUAVE.Methods.Missions.Segments.optimize.converge_opt (segment, state)
 
def SUAVE.Methods.Missions.Segments.optimize.get_objective (unknowns, segment, state)
 
def SUAVE.Methods.Missions.Segments.optimize.get_econstraints (unknowns, segment, state)
 
def SUAVE.Methods.Missions.Segments.optimize.make_bnds (unknowns, segment, state)
 
def SUAVE.Methods.Missions.Segments.optimize.get_ieconstraints (unknowns, segment, state)
 
def SUAVE.Methods.Missions.Segments.optimize.get_problem_pyopt (unknowns, segment, state)
 
def SUAVE.Methods.Missions.Segments.converge_root.converge_root (segment)
 
def SUAVE.Methods.Missions.Segments.converge_root.iterate (unknowns, segment)
 
def SUAVE.Methods.Missions.Segments.optimize.converge_opt (segment)
 
def SUAVE.Methods.Missions.Segments.optimize.get_objective (unknowns, segment)
 
def SUAVE.Methods.Missions.Segments.optimize.get_econstraints (unknowns, segment)
 
def SUAVE.Methods.Missions.Segments.optimize.make_bnds (unknowns, segment)
 
def SUAVE.Methods.Missions.Segments.optimize.get_ieconstraints (unknowns, segment)
 
def SUAVE.Methods.Missions.Segments.optimize.get_problem_pyopt (unknowns, segment)
 

Detailed Description

Mission Segment folders containing the functions for setting up and solving a mission.

Function Documentation

- -

◆ converge_opt()

+ +

◆ converge_opt()

@@ -184,7 +184,6 @@

-

◆ converge_root()

+ +

◆ converge_root()

@@ -229,9 +218,7 @@

-

◆ get_econstraints()

+ +

◆ get_econstraints()

@@ -260,13 +247,7 @@

  - segment, - - - - -   - state  + segment  @@ -290,8 +271,8 @@

-

◆ get_ieconstraints()

+ +

◆ get_ieconstraints()

@@ -306,13 +287,7 @@

  - segment, - - - - -   - state  + segment  @@ -321,12 +296,14 @@

-
Runs the mission if the inequality constraint values are needed
+
Runs the mission if the inequality constraint values are needed, these are specific to a climb
 
     Assumptions:
     Time only goes forward
     CL is less than a specified limit
+    CL is greater than zero
     All altitudes are greater than zero
+    The vehicle accelerates not decelerates
     
     Inputs:
     state.unknowns      [Data]
@@ -338,8 +315,8 @@ 

-

◆ get_objective()

+ +

◆ get_objective()

@@ -354,13 +331,7 @@

  - segment, - - - - -   - state  + segment  @@ -384,8 +355,8 @@

-

◆ get_problem_pyopt()

+ +

◆ get_problem_pyopt()

@@ -400,13 +371,7 @@

  - segment, - - - - -   - state  + segment  @@ -434,8 +399,8 @@

-

◆ iterate()

+ +

◆ iterate()

@@ -450,13 +415,7 @@

  - segment, - - - - -   - state  + segment  @@ -485,8 +444,8 @@

-

◆ make_bnds()

+ +

◆ make_bnds()

diff --git a/doxygen/group__Methods-Missions-Segments.js b/doxygen/group__Methods-Missions-Segments.js index de95bafd..223d1111 100644 --- a/doxygen/group__Methods-Missions-Segments.js +++ b/doxygen/group__Methods-Missions-Segments.js @@ -7,12 +7,13 @@ var group__Methods_Missions_Segments = [ "Ground", "group__Methods-Missions-Segments-Ground.html", "group__Methods-Missions-Segments-Ground" ], [ "Hover", "group__Methods-Missions-Segments-Hover.html", "group__Methods-Missions-Segments-Hover" ], [ "Single_Point", "group__Methods-Missions-Segments-Single__Point.html", "group__Methods-Missions-Segments-Single__Point" ], - [ "converge_opt", "group__Methods-Missions-Segments.html#ga6a15ecfced108358c27c0f4a8ed532cb", null ], - [ "converge_root", "group__Methods-Missions-Segments.html#ga13921466d6f6f405b48229bd2a2e9fa5", null ], - [ "get_econstraints", "group__Methods-Missions-Segments.html#ga17833fb35560ed7c1616cbd7039091ad", null ], - [ "get_ieconstraints", "group__Methods-Missions-Segments.html#gaf5f56473e84fbfa6ae39a3cf22fb8419", null ], - [ "get_objective", "group__Methods-Missions-Segments.html#gade8f58fd70859197f15ad050a9be4e70", null ], - [ "get_problem_pyopt", "group__Methods-Missions-Segments.html#ga1c03859f235b7957e3ff47ef8be0c0e6", null ], - [ "iterate", "group__Methods-Missions-Segments.html#gad082382d971ef537dfe9b8dbeed7a776", null ], - [ "make_bnds", "group__Methods-Missions-Segments.html#ga0c332a9e67af11deb7921508a7a09c72", null ] + [ "Transition", "group__Methods-Missions-Segments-Transition.html", "group__Methods-Missions-Segments-Transition" ], + [ "converge_opt", "group__Methods-Missions-Segments.html#gaa3ba00f069d941a28aa7a97da59d9231", null ], + [ "converge_root", "group__Methods-Missions-Segments.html#gaf8a167521653f53559575d11e8be5a0a", null ], + [ "get_econstraints", "group__Methods-Missions-Segments.html#ga09a52dbb450b9d2843d0592976ed813d", null ], + [ "get_ieconstraints", "group__Methods-Missions-Segments.html#ga92eef3823782034e0401cb473a6f2eb8", null ], + [ "get_objective", "group__Methods-Missions-Segments.html#gab46860b50110e128ca4739f8d77ebfa2", null ], + [ "get_problem_pyopt", "group__Methods-Missions-Segments.html#gad44cf44c86e577aba6a2c938cfe920d2", null ], + [ "iterate", "group__Methods-Missions-Segments.html#ga0bffa8833412fa21f25e89aaa92833b5", null ], + [ "make_bnds", "group__Methods-Missions-Segments.html#gaeecd675d5c13fdca781220883cabcb4e", null ] ]; \ No newline at end of file diff --git a/doxygen/group__Methods-Missions.html b/doxygen/group__Methods-Missions.html index a3392dd9..7447f944 100644 --- a/doxygen/group__Methods-Missions.html +++ b/doxygen/group__Methods-Missions.html @@ -1,9 +1,9 @@ - + - + SUAVE: Missions @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@
- +

@@ -73,7 +78,9 @@
@@ -116,7 +123,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/group__Methods-Noise-Certification.html b/doxygen/group__Methods-Noise-Certification.html new file mode 100644 index 00000000..3c2b8633 --- /dev/null +++ b/doxygen/group__Methods-Noise-Certification.html @@ -0,0 +1,262 @@ + + + + + + + +SUAVE: Certification + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
Certification
+
+
+ + + + + + + + +

+Functions

def SUAVE.Methods.Noise.Certification.approach_noise.approach_noise (analyses, noise_configs)
 
def SUAVE.Methods.Noise.Certification.flyover_noise.flyover_noise (analyses, noise_configs)
 
def SUAVE.Methods.Noise.Certification.sideline_noise.sideline_noise (analyses, noise_configs)
 
+

Detailed Description

+

Function Documentation

+ +

◆ approach_noise()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Noise.Certification.approach_noise.approach_noise ( analyses,
 noise_configs 
)
+
+
This method calculates approach noise of a turbofan aircraft
+        
+Assumptions:
+    N/A
+
+Source:
+    N/A 
+
+Inputs:
+    analyses        - data structure of SUAVE analyses                [None]
+    noise_configs   - data structure for SUAVE vehicle configurations [None]
+
+Outputs: 
+    SPL             - sound pressure level                            [dB]
+
+Properties Used:
+    N/A 
+
+
+ +

◆ flyover_noise()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Noise.Certification.flyover_noise.flyover_noise ( analyses,
 noise_configs 
)
+
+
This method calculates flyover noise of a turbofan aircraft
+        
+Assumptions:
+    N/A
+
+Source:
+    N/A 
+
+Inputs:
+    analyses        - data structure of SUAVE analyses                [None]
+    noise_configs   - data structure for SUAVE vehicle configurations [None]
+
+Outputs: 
+    SPL             - sound pressure level                            [dB]
+
+Properties Used:
+    N/A 
+
+
+ +

◆ sideline_noise()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Noise.Certification.sideline_noise.sideline_noise ( analyses,
 noise_configs 
)
+
+
This method calculates sideline noise of a turbofan aircraft
+        
+Assumptions:
+    N/A
+
+Source:
+    N/A 
+
+Inputs:
+    analyses        - data structure of SUAVE analyses                [None]
+    noise_configs   - data structure for SUAVE vehicle configurations [None]
+
+Outputs: 
+    SPL             - sound pressure level                            [dB]
+
+Properties Used:
+    N/A 
+
+
+
+
+ + + + diff --git a/doxygen/group__Methods-Noise-Certification.js b/doxygen/group__Methods-Noise-Certification.js new file mode 100644 index 00000000..8498797c --- /dev/null +++ b/doxygen/group__Methods-Noise-Certification.js @@ -0,0 +1,6 @@ +var group__Methods_Noise_Certification = +[ + [ "approach_noise", "group__Methods-Noise-Certification.html#ga48dd5b2fe44935ff10a213dabc5aa138", null ], + [ "flyover_noise", "group__Methods-Noise-Certification.html#ga81ced96922969ce3638e1dde15b524bd", null ], + [ "sideline_noise", "group__Methods-Noise-Certification.html#gaa43d28831e8b50bdfdd41cdd903421e3", null ] +]; \ No newline at end of file diff --git a/doxygen/group__Methods-Noise-Correlation.html b/doxygen/group__Methods-Noise-Correlation.html new file mode 100644 index 00000000..f4fc24d7 --- /dev/null +++ b/doxygen/group__Methods-Noise-Correlation.html @@ -0,0 +1,116 @@ + + + + + + + +SUAVE: Correlation + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.0 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
Correlation
+
+
+
+
+ + + + diff --git a/doxygen/group__Methods-Noise-Correlations.html b/doxygen/group__Methods-Noise-Correlations.html deleted file mode 100644 index 69d0139b..00000000 --- a/doxygen/group__Methods-Noise-Correlations.html +++ /dev/null @@ -1,113 +0,0 @@ - - - - - - - -SUAVE: Correlations - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.1.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
-
- - - -
-
- -
-
-
- -
- -
-
- - -
- -
- -
-
-
Correlations
-
-
- -

Correlation type methods for calculating noise. -More...

-

Correlation type methods for calculating noise.

-
-
- - - - diff --git a/doxygen/group__Methods-Noise-Fidelity.html b/doxygen/group__Methods-Noise-Fidelity.html new file mode 100644 index 00000000..ac1987eb --- /dev/null +++ b/doxygen/group__Methods-Noise-Fidelity.html @@ -0,0 +1,120 @@ + + + + + + + +SUAVE: Zero Fidelity Zero + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
Zero Fidelity Zero
+
+
+ +

Correlation type methods for calculating noise. +More...

+

Correlation type methods for calculating noise.

+
+
+ + + + diff --git a/doxygen/group__Methods-Noise-Fidelity__One-Airframe.html b/doxygen/group__Methods-Noise-Fidelity__One-Airframe.html index f6904d5d..9c4d81b7 100644 --- a/doxygen/group__Methods-Noise-Fidelity__One-Airframe.html +++ b/doxygen/group__Methods-Noise-Fidelity__One-Airframe.html @@ -1,9 +1,9 @@ - + - + SUAVE: Airframe @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@

- +
@@ -73,7 +78,9 @@

@@ -91,6 +98,8 @@
+
Airframe
@@ -98,7 +107,545 @@

Fidelity One level noise calculations for the airframe components. More...

+ + + + + + + + + + + + +

+Functions

def SUAVE.Methods.Noise.Fidelity_One.Airframe.noise_airframe_Fink.noise_airframe_Fink (segment, analyses, config, settings, ioprint=0, filename=0)
 
def SUAVE.Methods.Noise.Fidelity_One.Airframe.noise_clean_wing.noise_clean_wing (S, b, ND, IsHorz, velocity, viscosity, M, phi, theta, distance, frequency)
 
def SUAVE.Methods.Noise.Fidelity_One.Airframe.noise_landing_gear.noise_landing_gear (D, H, wheels, M, velocity, phi, theta, distance, frequency)
 
def SUAVE.Methods.Noise.Fidelity_One.Airframe.noise_leading_edge_slat.noise_leading_edge_slat (SPL_wing, Sw, bw, velocity, viscosity, M, phi, theta, distance, frequency)
 
def SUAVE.Methods.Noise.Fidelity_One.Airframe.noise_trailing_edge_flap.noise_trailing_edge_flap (Sf, cf, deltaf, slots, velocity, M, phi, theta, distance, frequency)
 
+

Detailed Description

Fidelity One level noise calculations for the airframe components.

+

Function Documentation

+ +

◆ noise_airframe_Fink()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Noise.Fidelity_One.Airframe.noise_airframe_Fink.noise_airframe_Fink ( segment,
 analyses,
 config,
 settings,
 ioprint = 0,
 filename = 0 
)
+
+
This computes the noise from different sources of the airframe for a given vehicle for a constant altitude flight. 
+
+Assumptions:
+    Correlation based 
+ 
+Source:
+    Fink, Martin R. Airframe noise prediction method. No. UTRC/R77-912607-11. UNITED 
+    TECHNOLOGIES RESEARCH CENTER EAST HARTFORD CT, 1977.  
+           
+Inputs:
+    vehicle  - SUAVE type vehicle
+
+    includes these fields:
+        S                          - Wing Area
+        bw                         - Wing Span
+        Sht                        - Horizontal tail area
+        bht                        - Horizontal tail span
+        Svt                        - Vertical tail area
+        bvt                        - Vertical tail span
+        deltaf                     - Flap deflection
+        Sf                         - Flap area
+        cf                         - Flap chord
+        slots                      - Number of slots (Flap type)
+        Dp                         - Main landing gear tyre diameter
+        Hp                         - Main lading gear strut length
+        Dn                         - Nose landing gear tyre diameter
+        Hn                         - Nose landing gear strut length
+        wheels                     - Number of wheels
+
+    airport   - SUAVE type airport data, with followig fields:
+        atmosphere                  - Airport atmosphere (SUAVE type)
+        altitude                    - Airport altitude
+        delta_isa                   - ISA Temperature deviation
+        
+    noise segment - flight path data, containing:
+        distance_vector             - distance from the source location to observer
+        angle                       - polar angle from the source to the observer
+        phi                         - azimuthal angle from the source to the observer
+
+
+Outputs: One Third Octave Band SPL [dB]
+    SPL_wing                        - Sound Pressure Level of the clean wing
+    SPLht                           - Sound Pressure Level of the horizontal tail
+    SPLvt                           - Sound Pressure Level of the vertical tail
+    SPL_flap                        - Sound Pressure Level of the flaps trailing edge
+    SPL_slat                        - Sound Pressure Level of the slat leading edge
+    SPL_main_landing_gear           - Sound Pressure Level og the main landing gear
+    SPL_nose_landing_gear           - Sound Pressure Level of the nose landing gear
+
+Properties Used:
+    N/A      
+
+
+ +

◆ noise_clean_wing()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Noise.Fidelity_One.Airframe.noise_clean_wing.noise_clean_wing ( S,
 b,
 ND,
 IsHorz,
 velocity,
 viscosity,
 M,
 phi,
 theta,
 distance,
 frequency 
)
+
+
This computes the 1/3 octave band sound pressure level and the overall sound pressure level from the clean wing,
+for a wing with area S (sq.ft) and span b (ft).  ND is a constant set to 0 for clean wings and set to 1 for propeller
+airplanes, jet transports with numerous large trailing edge flap tracks, flaps extended, or slats extended. ISHORZ must be set to 1.
+This function can be used for the horizontal tail by inserting the appropriate tail area and span. For a vertical tail, its appropriate
+area and height are used and ISHORZ must be set to 0.
+
+Assumptions:
+    Correlation based.  
+
+Source:
+   SAE Model
+   
+Inputs:
+        S                          - Wing Area [sq.ft]
+        b                          - Wing Span [ft]
+        ND                         - Costant from the method
+        IsHoriz                    - Costant from the method
+        deltaw                     - Wing Turbulent Boundary Layer thickness [ft]
+        velocity                   - Aircraft speed [kts]
+        viscosity                  - Dynamic viscosity
+        M                          - Mach number
+        phi                        - Azimuthal angle [rad]
+        theta                      - Polar angle [rad]
+        distance                   - Distance from airplane to observer, evaluated at retarded time [ft]
+        frequency                  - Frequency array [Hz]
+
+
+
+Outputs: One Third Octave Band SPL [dB]
+    SPL                              - Sound Pressure Level of the clean wing [dB]
+    OASPL                            - Overall Sound Pressure Level of the clean wing [dB]
+
+Properties Used:
+    None
+
+
+ +

◆ noise_landing_gear()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Noise.Fidelity_One.Airframe.noise_landing_gear.noise_landing_gear ( D,
 H,
 wheels,
 M,
 velocity,
 phi,
 theta,
 distance,
 frequency 
)
+
+
This calculates the Landing gear 1/3 octave band sound pressure level and overall sound pressure level
+for a tyre diameter D, a strut length H and WHEELS number of  wheels per unit.
+
+Assumptions:
+    Correlation based.
+
+Source:
+    None
+
+
+Inputs:
+    D         - Landing gear tyre diameter                                     [ft]
+    H         - Lading gear strut length                                       [ft]
+    wheels    - Number of wheels per unit                                      [-]
+    M         - Mach number                                                    [-]
+    velocity  - Aircraft speed                                                 [kts]
+    phi       - Azimuthal angle                                                [rad]
+    theta     - Polar angle                                                    [rad]
+    distance  - Distance from airplane to observer, evaluated at retarded time [ft]
+    frequemcy - Frequency array                                                [Hz] 
+
+Outputs: One Third Octave Band SPL [dB]
+    SPL           - Sound Pressure Level of the landing gear         [dB]
+    OASPL         - Overall Sound Pressure Level of the landing gear [dB]
+
+
+Source:
+    SAE ARP 876D
+
+Inputs:
+    Ce = wing chord length at the engine location - as figure 7.3 of the SAE ARP 876D                    [m]                          
+    Xe = fan exit location downstream of the leading edge (Xe<Ce) - as figure 7.3 of the SAE ARP 876D    [m] 
+    Ye = separation distance from the wing chord line to nozzle lip - as figure 7.3 of the SAE ARP 876D  [m] 
+    theta_s                                                                                              [rad]
+    Diameter_mixed                                                                                       [m] 
+
+Outputs:
+    INST_s          [-]
+
+Properties Used: 
+    N/A 
+
+
+ +

◆ noise_leading_edge_slat()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Noise.Fidelity_One.Airframe.noise_leading_edge_slat.noise_leading_edge_slat ( SPL_wing,
 Sw,
 bw,
 velocity,
 viscosity,
 M,
 phi,
 theta,
 distance,
 frequency 
)
+
+
This calculates the noise from the slat leading edge as a 1/3 octave band sound pressure level. 
+
+ Assumptions:
+     Correlation based.
+     
+ Inputs:
+         SPL_wing                   - Sound Pressure Level of the clean wing                         [dB]
+         Sw                         - Wing Area                                                      [sq.ft]
+         bw                         - Wing Span                                                      [ft] 
+         velocity                   - Aircraft speed                                                 [kts]
+         viscosity                  - Dynamic viscosity                                              [kg m^-1s^-1]
+         M                          - Mach number                                                    [unitless]
+         phi                        - Azimuthal angle                                                [rad]
+         theta                      - Polar angle                                                    [rad]
+         distance                   - Distance from airplane to observer, evaluated at retarded time [ft]
+         frequency                  - Frequency array                                                [Hz]
+                                                                                                     
+ Outputs: One Third Octave Band SPL                                                                  [dB]
+     SPL                             - Sound Pressure Level of the slat leading edge                 [dB]
+
+Properties Used:
+    None    
+
+
+
+ +

◆ noise_trailing_edge_flap()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Noise.Fidelity_One.Airframe.noise_trailing_edge_flap.noise_trailing_edge_flap ( Sf,
 cf,
 deltaf,
 slots,
 velocity,
 M,
 phi,
 theta,
 distance,
 frequency 
)
+
+
This calculates the noise from the flap trailing edge as a 1/3 octave band sound pressure level.
+
+Assumptions:
+    Correlation based.
+    
+Inputs:
+    Sf         - Flap area                                                      [sq.ft]
+    cf         - Flap chord                                                     [ft]
+    deltaf     - Flap deflection                                                [rad]
+    slots      - Number of slots                                                (Flap type)
+    velocity   - Aircraft speed                                                 [kts]
+    M          - Mach number                                                    [Unitless]
+    phi        - Azimuthal angle                                                [rad]
+    theta      - Polar angle                                                    [rad]
+    distance   - Distance from airplane to observer, evaluated at retarded time [ft]
+    frequency  - Frequency array                                                [Hz]
+    
+Outputs: One Third Octave Band SPL                                              [dB]
+    SPL                
+ 
+Properties Used:
+    N/A 
+
+

@@ -106,7 +653,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/group__Methods-Noise-Fidelity__One-Airframe.js b/doxygen/group__Methods-Noise-Fidelity__One-Airframe.js new file mode 100644 index 00000000..d4b5f2ee --- /dev/null +++ b/doxygen/group__Methods-Noise-Fidelity__One-Airframe.js @@ -0,0 +1,8 @@ +var group__Methods_Noise_Fidelity__One_Airframe = +[ + [ "noise_airframe_Fink", "group__Methods-Noise-Fidelity__One-Airframe.html#ga702a77b2ac10121455091e79b3707128", null ], + [ "noise_clean_wing", "group__Methods-Noise-Fidelity__One-Airframe.html#gae4e40c87edaeed794f229ff07eb102c7", null ], + [ "noise_landing_gear", "group__Methods-Noise-Fidelity__One-Airframe.html#ga96efb073f88b68a0838ed850b492af3e", null ], + [ "noise_leading_edge_slat", "group__Methods-Noise-Fidelity__One-Airframe.html#gacc9075bff25bfe9ef8dd91f7da32191e", null ], + [ "noise_trailing_edge_flap", "group__Methods-Noise-Fidelity__One-Airframe.html#ga552c6d0103dab2cf012662a7649ae9e9", null ] +]; \ No newline at end of file diff --git a/doxygen/group__Methods-Noise-Fidelity__One-Engine.html b/doxygen/group__Methods-Noise-Fidelity__One-Engine.html index d85072f5..97c15bb5 100644 --- a/doxygen/group__Methods-Noise-Fidelity__One-Engine.html +++ b/doxygen/group__Methods-Noise-Fidelity__One-Engine.html @@ -1,9 +1,9 @@ - + - + SUAVE: Engine @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@

- +
@@ -73,7 +78,9 @@
@@ -91,6 +98,8 @@
@@ -98,7 +107,954 @@

Fidelity One level noise calculations for the engine. More...

+ + + + + + + + + + + + + + + + + + + + +

+Functions

def SUAVE.Methods.Noise.Fidelity_One.Engine.angle_of_attack_effect.angle_of_attack_effect (AoA, Mach_aircraft, theta_m)
 
def SUAVE.Methods.Noise.Fidelity_One.Engine.external_plug_effect.external_plug_effect (Velocity_primary, Velocity_secondary, Velocity_mixed, Diameter_primary, Diameter_secondary, Diameter_mixed, Plug_diameter, sound_ambient, theta_p, theta_s, theta_m)
 
def SUAVE.Methods.Noise.Fidelity_One.Engine.ground_proximity_effect.ground_proximity_effect (Velocity_mixed, sound_ambient, theta_m, engine_height, Diameter_mixed, frequency)
 
def SUAVE.Methods.Noise.Fidelity_One.Engine.jet_installation_effect.jet_installation_effect (Xe, Ye, Ce, theta_s, Diameter_mixed)
 
def SUAVE.Methods.Noise.Fidelity_One.Engine.mixed_noise_component.mixed_noise_component (SPL_m, Velocity_primary, theta_m, sound_ambient, Velocity_secondary, Velocity_aircraft, Area_primary, Area_secondary, DSPL_m, EX_m, Str_m, Velocity_mixed, XBPR)
 
def SUAVE.Methods.Noise.Fidelity_One.Engine.noise_SAE.noise_SAE (turbofan, segment, analyses, config, settings, ioprint=0, filename=0)
 
def SUAVE.Methods.Noise.Fidelity_One.Engine.noise_source_location.noise_source_location (B, Xo, zk, Diameter_primary, theta_p, Area_primary, Area_secondary, distance_microphone, Diameter_secondary, theta, theta_s, theta_m, Diameter_mixed, Velocity_primary, Velocity_secondary, Velocity_mixed, Velocity_aircraft, sound_ambient, Str_m, Str_s)
 
def SUAVE.Methods.Noise.Fidelity_One.Engine.primary_noise_component.primary_noise_component (SPL_p, Velocity_primary, Temperature_primary, R_gas, theta_p, DVPS, sound_ambient, Velocity_secondary, Velocity_aircraft, Area_primary, Area_secondary, DSPL_p, EX_p, Str_p)
 
def SUAVE.Methods.Noise.Fidelity_One.Engine.secondary_noise_component.secondary_noise_component (SPL_s, Velocity_primary, theta_s, sound_ambient, Velocity_secondary, Velocity_aircraft, Area_primary, Area_secondary, DSPL_s, EX_s, Str_s)
 
+

Detailed Description

Fidelity One level noise calculations for the engine.

+

Function Documentation

+ +

◆ angle_of_attack_effect()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Noise.Fidelity_One.Engine.angle_of_attack_effect.angle_of_attack_effect ( AoA,
 Mach_aircraft,
 theta_m 
)
+
+
This calculates the angle of attack effect, in decibels, to be added 
+to the predicted mixed jet noise level. 
+    
+Assumptions:
+    N/A
+
+Source:
+    SAE Model
+
+Inputs:   
+    AoA           angle of attack         [rad]
+    Mach_aircraft mach number of aircraft [Unitless]
+    theta_m       emission angle          [rad]                
+
+Outputs:
+    ATK_m         angle of attack effect  [Unitless]    
+
+Properties Used:
+    None 
+
+
+
+ +

◆ external_plug_effect()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Noise.Fidelity_One.Engine.external_plug_effect.external_plug_effect ( Velocity_primary,
 Velocity_secondary,
 Velocity_mixed,
 Diameter_primary,
 Diameter_secondary,
 Diameter_mixed,
 Plug_diameter,
 sound_ambient,
 theta_p,
 theta_s,
 theta_m 
)
+
+
This function calculates the adjustments, in decibels, to be added to the predicted jet noise levels due to
+external plugs in coaxial jets.
+
+Assumptions:
+    N/A
+
+Source:
+    N/A
+
+Inputs: 
+    Velocity_primary      [m/s]
+    Velocity_secondary    [m/s]
+    Velocity_mixed        [m/s]
+    Diameter_primary      [m]
+    Diameter_secondary    [m]
+    Diameter_mixed        [m]
+    Plug_diameter         [m]
+    sound_ambient         [dB]
+    theta_p               [rad]
+    theta_s               [rad]
+    theta_m               [rad]
+
+Outputs: 
+    PG_p        [dB]
+    PG_s        [dB]
+    PG_m        [dB]
+
+Properties Used:
+    N/A  
+
+
+
+ +

◆ ground_proximity_effect()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Noise.Fidelity_One.Engine.ground_proximity_effect.ground_proximity_effect ( Velocity_mixed,
 sound_ambient,
 theta_m,
 engine_height,
 Diameter_mixed,
 frequency 
)
+
+
This function calculates the ground proximity effect, in decibels, and is used for full-scale 
+engine test stand.
+    
+Assumptions:
+    N/A
+
+Source:
+    N/A
+
+Inputs:
+    Velocity_mixed  [m/s]
+    sound_ambient   [SPL]
+    theta_m         [rad]
+    engine_height   [m]
+    Diameter_mixed  [m]
+    frequency       [1/s]
+
+Outputs:
+    GPROX_m         [dB]
+
+Properties Used:
+    N/A 
+
+
+
+ +

◆ jet_installation_effect()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Noise.Fidelity_One.Engine.jet_installation_effect.jet_installation_effect ( Xe,
 Ye,
 Ce,
 theta_s,
 Diameter_mixed 
)
+
+
This calculates the installation effect, in decibels, to be added to the predicted secondary jet noise level.
+
+Assumptions:
+    N/A
+
+Source:
+    SAE ARP876D: Gas Turbine Jet Exhaust Noise Prediction
+
+Inputs:
+    Ce = wing chord length at the engine location - as figure 7.3 of the SAE ARP 876D                    [m]                          
+    Xe = fan exit location downstream of the leading edge (Xe<Ce) - as figure 7.3 of the SAE ARP 876D    [m] 
+    Ye = separation distance from the wing chord line to nozzle lip - as figure 7.3 of the SAE ARP 876D  [m] 
+    theta_s                                                                                              [rad]
+    Diameter_mixed                                                                                       [m] 
+
+Outputs:
+    INST_s          [-]
+
+Properties Used: 
+    N/A 
+
+
+
+ +

◆ mixed_noise_component()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Noise.Fidelity_One.Engine.mixed_noise_component.mixed_noise_component ( SPL_m,
 Velocity_primary,
 theta_m,
 sound_ambient,
 Velocity_secondary,
 Velocity_aircraft,
 Area_primary,
 Area_secondary,
 DSPL_m,
 EX_m,
 Str_m,
 Velocity_mixed,
 XBPR 
)
+
+
This function calculates the noise contribution of the mixed jet component
+
+Assumptions:
+    N/A
+
+Source:
+    None
+
+Inputs:
+    SPL_m               [dB]
+    Velocity_primary    [m/s]
+    theta_m             [rad]
+    sound_ambient       [SPL]
+    Velocity_secondary  [m/s]
+    Velocity_aircraft   [m/s]
+    Area_primary        [m^2]
+    Area_secondary      [m^2]
+    DSPL_m              [SPL]
+    EX_m
+    Str_m
+    Velocity_mixed      [m/s]
+    XBPR                   
+
+Outputs:
+    SPL_m                [dB]
+
+Properties Used: 
+    N/A 
+
+
+
+ +

◆ noise_SAE()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Noise.Fidelity_One.Engine.noise_SAE.noise_SAE ( turbofan,
 segment,
 analyses,
 config,
 settings,
 ioprint = 0,
 filename = 0 
)
+
+
This method predicts the free-field 1/3 Octave Band SPL of coaxial subsonic
+   jets for turbofan engines under the following conditions:
+   a) Flyover (observer on ground)
+   b) Static (observer on ground)
+   c) In-flight or in-flow (observer on airplane or in a wind tunnel)
+
+Assumptions:
+    SAE ARP876D: Gas Turbine Jet Exhaust Noise Prediction
+
+Inputs:
+    vehicle  - SUAVE type vehicle 
+    includes these fields:
+        Velocity_primary           - Primary jet flow velocity                           [m/s]
+        Temperature_primary        - Primary jet flow temperature                        [m/s]
+        Pressure_primary           - Primary jet flow pressure                           [Pa]
+        Area_primary               - Area of the primary nozzle                          [m^2]
+        Velocity_secondary         - Secondary jet flow velocity                         [m/s]
+        Temperature_secondary      - Secondary jet flow temperature                      [m/s]
+        Pressure_secondary         - Secondary jet flow pressure                         [Pa]
+        Area_secondary             - Area of the secondary nozzle                        [m^2]
+        AOA                        - Angle of attack                                     [rad]
+        Velocity_aircraft          - Aircraft velocity                                   [m/s]
+        Altitude                   - Altitude                                            [m]
+        N1                         - Fan rotational speed                                [rpm]
+        EXA                        - Distance from fan face to fan exit/ fan diameter    [m]
+        Plug_diameter              - Diameter of the engine external plug                [m]
+        Engine_height              - Engine centerline height above the ground plane     [m]
+        distance_microphone        - Distance from the nozzle exhaust to the microphones [m]
+        angles                     - Array containing the desired polar angles           [rad]
+
+
+    airport   - SUAVE type airport data, with followig fields:
+        atmosphere                  - Airport atmosphere (SUAVE type)
+        altitude                    - Airport altitude
+        delta_isa                   - ISA Temperature deviation
+
+
+Outputs: One Third Octave Band SPL [dB]
+    SPL_p                           - Sound Pressure Level of the primary jet            [dB]
+    SPL_s                           - Sound Pressure Level of the secondary jet          [dB]
+    SPL_m                           - Sound Pressure Level of the mixed jet              [dB]
+    SPL_total                       - Sound Pressure Level of the total jet noise        [dB]
+
+
+ +

◆ noise_source_location()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Noise.Fidelity_One.Engine.noise_source_location.noise_source_location ( B,
 Xo,
 zk,
 Diameter_primary,
 theta_p,
 Area_primary,
 Area_secondary,
 distance_microphone,
 Diameter_secondary,
 theta,
 theta_s,
 theta_m,
 Diameter_mixed,
 Velocity_primary,
 Velocity_secondary,
 Velocity_mixed,
 Velocity_aircraft,
 sound_ambient,
 Str_m,
 Str_s 
)
+
+
This function calculates the noise source location
+
+Assumptions:
+    None
+
+Source:
+    None
+
+Inputs: 
+    B                         [-]
+    Xo                        [-]
+    zk                        [-]
+    Diameter_primary          [m]
+    theta_p                   [rad]
+    Area_primary              [m^2]
+    Area_secondary            [m^2]
+    distance_microphone       [m]
+    Diameter_secondary        [m]
+    theta                     [rad]
+    theta_s                   [rad]
+    theta_m                   [rad]
+    Diameter_mixed            [m]
+    Velocity_primary          [m/s]
+    Velocity_secondary        [m/s]
+    Velocity_mixed            [m/s]
+    Velocity_aircraft         [m/s]
+    sound_ambient             [dB]
+    Str_m                     [-]
+    Str_s                     [-]
+
+Outputs: 
+    theta_p  [rad]
+    theta_s  [rad]
+    theta_m  [rad]
+
+Properties Used:
+    N/A 
+
+
+ +

◆ primary_noise_component()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Noise.Fidelity_One.Engine.primary_noise_component.primary_noise_component ( SPL_p,
 Velocity_primary,
 Temperature_primary,
 R_gas,
 theta_p,
 DVPS,
 sound_ambient,
 Velocity_secondary,
 Velocity_aircraft,
 Area_primary,
 Area_secondary,
 DSPL_p,
 EX_p,
 Str_p 
)
+
+
This function calculates the noise contribution of the primary jet component
+
+    Assumptions:
+    Empirical based procedure.
+
+Source: 
+    None
+    
+Inputs:
+    noise_data     - SUAVE type vehicle
+
+Outputs:
+    OASPL          - Overall Sound Pressure Level            [dB]
+    PNL            - Perceived Noise Level                   [dB]
+    PNL_dBA        - Perceived Noise Level A-weighted level  [dBA]
+    EPNdB_takeoff  - Takeoff Effective Perceived Noise Level [EPNdB]
+    EPNdB_landing  - Landing Effective Perceived Noise Level [EPNdB]  
+
+Properties Used:
+    N/A  
+
+
+ +

◆ secondary_noise_component()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Noise.Fidelity_One.Engine.secondary_noise_component.secondary_noise_component ( SPL_s,
 Velocity_primary,
 theta_s,
 sound_ambient,
 Velocity_secondary,
 Velocity_aircraft,
 Area_primary,
 Area_secondary,
 DSPL_s,
 EX_s,
 Str_s 
)
+
+
This function calculates the noise contribution of the secondary jet component
+
+Assumptions:
+    None
+
+Source:
+    None
+
+Inputs:
+    SPL_s               [dB]
+    Velocity_primary    [m/s]
+    theta_s             [rad]
+    sound_ambient       [dB]
+    Velocity_secondary  [m/s]
+    Velocity_aircraft   [m/s]
+    Area_primary        [m^2]
+    Area_secondary      [m^2]
+    DSPL_s              [dB]
+    EX_s                [-]
+    Str_s               [-]
+
+Outputs: 
+    SPL_s               [dB]
+
+Properties Used:
+    N/A 
+
+
@@ -106,7 +1062,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/group__Methods-Noise-Fidelity__One-Engine.js b/doxygen/group__Methods-Noise-Fidelity__One-Engine.js new file mode 100644 index 00000000..0400bf31 --- /dev/null +++ b/doxygen/group__Methods-Noise-Fidelity__One-Engine.js @@ -0,0 +1,12 @@ +var group__Methods_Noise_Fidelity__One_Engine = +[ + [ "angle_of_attack_effect", "group__Methods-Noise-Fidelity__One-Engine.html#ga6c2634ad48b4eeb15caf72f4e076118b", null ], + [ "external_plug_effect", "group__Methods-Noise-Fidelity__One-Engine.html#gaf3380812851c925479dcf7ac041d6209", null ], + [ "ground_proximity_effect", "group__Methods-Noise-Fidelity__One-Engine.html#gad5c78faf395996a43add4d856ffab94b", null ], + [ "jet_installation_effect", "group__Methods-Noise-Fidelity__One-Engine.html#ga1f59f748a26f7ce9ef8b646040fff87f", null ], + [ "mixed_noise_component", "group__Methods-Noise-Fidelity__One-Engine.html#ga86562c9603fd0f1116bcd03912b0f2fa", null ], + [ "noise_SAE", "group__Methods-Noise-Fidelity__One-Engine.html#gaf1c733612790d7ce60f2dfbb140cbd4a", null ], + [ "noise_source_location", "group__Methods-Noise-Fidelity__One-Engine.html#ga80902a73b33d0cded267184f4a46fdb6", null ], + [ "primary_noise_component", "group__Methods-Noise-Fidelity__One-Engine.html#gae11fb8e4c2002ea94f9b824bd427643e", null ], + [ "secondary_noise_component", "group__Methods-Noise-Fidelity__One-Engine.html#gafb723142afd97b337ed305018f9bff55", null ] +]; \ No newline at end of file diff --git a/doxygen/group__Methods-Noise-Fidelity__One-Noise__Tools.html b/doxygen/group__Methods-Noise-Fidelity__One-Noise__Tools.html index 7b246325..f3d7c2ed 100644 --- a/doxygen/group__Methods-Noise-Fidelity__One-Noise__Tools.html +++ b/doxygen/group__Methods-Noise-Fidelity__One-Noise__Tools.html @@ -1,9 +1,9 @@ - + - + SUAVE: Noise Tools @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@
- +

@@ -73,7 +78,9 @@
@@ -91,6 +98,8 @@
+
Noise Tools
@@ -98,7 +107,1051 @@

Various functions that are used to calculate noise using the fidelity one level. More...

+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Functions

def SUAVE.Methods.Noise.Fidelity_One.Noise_Tools.atmospheric_attenuation.atmospheric_attenuation (dist)
 
def SUAVE.Methods.Noise.Fidelity_One.Noise_Tools.compute_noise.compute_noise (config, analyses, noise_segment, noise_settings)
 
def SUAVE.Methods.Noise.Fidelity_One.Noise_Tools.compute_noise_evaluation_locations.compute_ground_noise_evaluation_locations (settings, segment)
 
def SUAVE.Methods.Noise.Fidelity_One.Noise_Tools.compute_noise_evaluation_locations.compute_building_noise_evaluation_locations (settings, segment)
 
def SUAVE.Methods.Noise.Fidelity_One.Noise_Tools.dbA_noise.dbA_noise (SPL)
 
def SUAVE.Methods.Noise.Fidelity_One.Noise_Tools.decibel_arithmetic.pressure_ratio_to_SPL_arithmetic (p_pref_total)
 
def SUAVE.Methods.Noise.Fidelity_One.Noise_Tools.decibel_arithmetic.SPL_arithmetic (SPL, sum_axis=2)
 
def SUAVE.Methods.Noise.Fidelity_One.Noise_Tools.decibel_arithmetic.SPL_spectra_arithmetic (SPL)
 
def SUAVE.Methods.Noise.Fidelity_One.Noise_Tools.epnl_noise.epnl_noise (PNLT)
 
def SUAVE.Methods.Noise.Fidelity_One.Noise_Tools.generate_microphone_points.generate_ground_microphone_points (min_x, max_x, min_y, max_y, N_x, N_y)
 
def SUAVE.Methods.Noise.Fidelity_One.Noise_Tools.generate_microphone_points.generate_building_microphone_points (building_locations, building_dimensions, N_x, N_y, N_z)
 
def SUAVE.Methods.Noise.Fidelity_One.Noise_Tools.noise_certification_limits.noise_certification_limits (results, vehicle)
 
def SUAVE.Methods.Noise.Fidelity_One.Noise_Tools.noise_geometric.noise_geometric (noise_segment, analyses, config)
 
def SUAVE.Methods.Noise.Fidelity_One.Noise_Tools.noise_tone_correction.noise_tone_correction (SPL)
 
def SUAVE.Methods.Noise.Fidelity_One.Noise_Tools.pnl_noise.pnl_noise (SPL)
 
def SUAVE.Methods.Noise.Fidelity_One.Noise_Tools.print_airframe_output.print_airframe_output (SAE_Airframe_Noise_Outputs)
 
def SUAVE.Methods.Noise.Fidelity_One.Noise_Tools.print_engine_output.print_engine_output (SAE_Engine_Noise_Outputs)
 
def SUAVE.Methods.Noise.Fidelity_One.Noise_Tools.print_propeller_output.print_propeller_output (speed, nsteps, time, altitude, RPM, theta, dist, PNL, PNL_dBA)
 
def SUAVE.Methods.Noise.Fidelity_One.Noise_Tools.senel_noise.senel_noise (SPLt_dBA_max)
 
def SUAVE.Methods.Noise.Fidelity_One.Noise_Tools.SPL_harmonic_to_third_octave.SPL_harmonic_to_third_octave (SPL, f, settings)
 
def SUAVE.Methods.Noise.Fidelity_One.Propeller.compute_source_coordinates.compute_blade_section_source_coordinates (AoA, acoustic_outputs, rotors, mls, settings)
 
+

Detailed Description

Various functions that are used to calculate noise using the fidelity one level.

+

Function Documentation

+ +

◆ atmospheric_attenuation()

+ +
+
+ + + + + + + + +
def SUAVE.Methods.Noise.Fidelity_One.Noise_Tools.atmospheric_attenuation.atmospheric_attenuation ( dist)
+
+
This calculates a the atmospheric attenuation of sound for each frequency band
+as a function of the distance from the source to the observer. 
+
+Assumptions:
+   N/A
+
+Source:
+   SAE Model for a standard day.
+    
+Inputs:
+    dist - Array with the distance vector from the aircraft (source) to the 
+        microphone position (observer)                                              [m]
+
+Outputs: 
+    delta_spl - The delta sound pressure level to be reduced from the lossless SPL 
+    condition                                                                       [dB]
+
+Properties Used:
+    None 
+
+
+
+ +

◆ compute_blade_section_source_coordinates()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Noise.Fidelity_One.Propeller.compute_source_coordinates.compute_blade_section_source_coordinates ( AoA,
 acoustic_outputs,
 rotors,
 mls,
 settings 
)
+
+
This calculated the position vector from a point source to the observer 
+        
+Assumptions:
+    N/A
+ 
+Source:
+    N/A  
+ 
+Inputs:  
+    AoA                            - aircraft angle ofattack                     [rad]
+    acoustic_outputs               - outputs from propeller aerodynamic analysis [None]   
+    mls                            - microphone locations                        [m]   
+    rotors                         - rotors on network                           [None]  
+    settings                       - noise calculation settings                  [None]
+ 
+Outputs: 
+    blade_section_position_vectors - position vector of rotor blade sections     [m]
+ 
+Properties Used:
+    N/A       
+
+
+
+ +

◆ compute_building_noise_evaluation_locations()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Noise.Fidelity_One.Noise_Tools.compute_noise_evaluation_locations.compute_building_noise_evaluation_locations ( settings,
 segment 
)
+
+
This computes the relative locations on the surface in the computational domain where the 
+propogated sound is computed.   
+        
+Assumptions: 
+    Acoustic scattering is not modeled
+
+Source:
+    N/A  
+
+Inputs:  
+    settings.urban_canyon_microphone_locations          - array of microphone locations on a building(s)  [meters] 
+    segment.conditions.frames.inertial.position_vector  - position of aircraft                            [boolean]                                     
+
+Outputs: 
+BM_THETA   - angle measured from building microphone in the x-z plane from microphone to aircraft 
+BM_PHI     - angle measured from building microphone in the y-z plane from microphone to aircraft 
+UCML       - building microphone locations
+num_b_mic  - number of building microphones
+
+Properties Used:
+    N/A       
+
+
+
+ +

◆ compute_ground_noise_evaluation_locations()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Noise.Fidelity_One.Noise_Tools.compute_noise_evaluation_locations.compute_ground_noise_evaluation_locations ( settings,
 segment 
)
+
+
This computes the relative locations on the surface in the computational domain where the 
+propogated sound is computed. Vectors point from observer/microphone to aircraft/source  
+        
+Assumptions: 
+    Acoustic scattering is not modeled
+
+Source:
+    N/A  
+
+Inputs:  
+    settings.ground_microphone_locations                - array of microphone locations on the ground  [meters] 
+    segment.conditions.frames.inertial.position_vector  - position of aircraft                         [boolean]                                          
+
+Outputs: 
+GM_THETA   - angle measured from ground microphone in the x-z plane from microphone to aircraft 
+GM_PHI     - angle measured from ground microphone in the y-z plane from microphone to aircraft 
+GML        - ground microphone locations
+num_gm_mic - number of ground microphones
+ 
+Properties Used:
+    N/A       
+
+
+
+ +

◆ compute_noise()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Noise.Fidelity_One.Noise_Tools.compute_noise.compute_noise ( config,
 analyses,
 noise_segment,
 noise_settings 
)
+
+
This method computes the noise of a turbofan aircraft
+        
+Assumptions:
+    N/A
+
+Source:
+    N/A 
+
+Inputs:
+    config.
+    networks.turbofan     - SUAVE turbofan data structure               [None]
+    output_file           - flag to write noise outout to file          [Boolean]
+    output_file_engine    - flag to write engine outout to file         [Boolean]
+    print_output          - flag to print outout to file                [Boolean]
+    engine_flag           - flag to include engine in noise calculation [Boolean]
+    
+Outputs: 
+    noise_sum                                                           [dB]
+
+Properties Used:
+    N/A 
+
+
+ +

◆ dbA_noise()

+ +
+
+ + + + + + + + +
def SUAVE.Methods.Noise.Fidelity_One.Noise_Tools.dbA_noise.dbA_noise ( SPL)
+
+
This method calculates the A-weighted level from a 1/3 octave band noise spectra 
+        
+Assumptions:
+    N/A
+
+Source:
+    N/A 
+
+Inputs:
+    SPL     - Sound Pressure Level in 1/3 octave band
+
+Outputs: [dB]
+    SPL_dbA - A-weighted Sound Pressure Level in dBA 
+
+Properties Used:
+    N/A 
+
+
+ +

◆ epnl_noise()

+ +
+
+ + + + + + + + +
def SUAVE.Methods.Noise.Fidelity_One.Noise_Tools.epnl_noise.epnl_noise ( PNLT)
+
+
This method calculates de effective perceived noise level (EPNL) based on a
+time history Perceived Noise Level with Tone Correction (PNLT).
+ 
+Assumptions:
+    N/A
+
+Source:
+    N/A
+
+Inputs:
+    PNLT - Perceived Noise Level with Tone Correction  [PNLdB]
+ 
+ Outputs:
+    EPNL - Effective Perceived Noise Level in          [EPNdB]
+ 
+Properties Used:
+    N/A  
+
+
+
+ +

◆ generate_building_microphone_points()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Noise.Fidelity_One.Noise_Tools.generate_microphone_points.generate_building_microphone_points ( building_locations,
 building_dimensions,
 N_x,
 N_y,
 N_z 
)
+
+
This computes the absolute microphone/observer locations on the surface of rectilinear buildinsg. 
+        
+Assumptions:
+    Microhpone locations are uniformly distributed on the surface
+
+Source:
+    N/A  
+
+Inputs:  
+    building_locations             - cartesian coordinates of the base of buildings                [meters]
+    building_dimensions            - dimensions of buildings [length,width,height]                 [meters] 
+    building_microphone_resolution - resolution of microphone array                                [unitless]
+    N_x                            - discretization of points in x dimension on building surface   [meters]
+    N_y                            - discretization of points in y dimension on building surface   [meters]
+    N_z                            - discretization of points in z dimension on building surface   [meters]
+    
+Outputs: 
+    building_mic_locations         - cartesian coordiates of all microphones defined on buildings  [meters]
+                          
+
+Properties Used:
+    N/A       
+
+
+
+ +

◆ generate_ground_microphone_points()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Noise.Fidelity_One.Noise_Tools.generate_microphone_points.generate_ground_microphone_points ( min_x,
 max_x,
 min_y,
 max_y,
 N_x,
 N_y 
)
+
+
This computes the absolute microphone/observer locations on level ground. 
+        
+Assumptions:
+    None
+
+Source:
+    N/A  
+
+Inputs:   
+    min_x - minimum x coordinate of noise evaluation plane [meters]
+    max_x - maximum x coordinate of noise evaluation plane [meters]
+    min_y - minimum y coordinate of noise evaluation plane [meters]
+    max_x - maximim y coordinate of noise evaluation plane [meters]
+    N_x   - number of microphones on x-axis 
+    N_y   - number of microphones on y-axis 
+
+Outputs: 
+    gm_mic_locations   - cartesian coordiates of all microphones defined  [meters] 
+
+Properties Used:
+    N/A       
+
+
+
+ +

◆ noise_certification_limits()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Noise.Fidelity_One.Noise_Tools.noise_certification_limits.noise_certification_limits ( results,
 vehicle 
)
+
+
This computes the certification noise limits as a function of the aircraft weight [lbs] 
+and number of engines for each segment.
+
+Assumptions:
+    None
+
+Source:
+    SAE 
+    
+Inputs:
+    vehicle  - SUAVE type vehicle
+    results
+
+Outputs: Noise limits in EPNL
+    noise_approach_limit  - Approach noise limit as a function of the landing weight, [EPNdB]
+    noise_flyover_limit   - Flyover noise limit as a function of the takeoff weight,  [EPNdB]
+    noise_sideline_limit  - Sideline noise limit as a function of the takeoff weight, [EPNdB]
+
+Properties Used:
+    None
+
+
+
+ +

◆ noise_geometric()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Noise.Fidelity_One.Noise_Tools.noise_geometric.noise_geometric ( noise_segment,
 analyses,
 config 
)
+
+
This computes the geometric parameters for the noise tools: distance and emission angles for 
+both polar and azimuthal angles.
+ 
+Assumptions:
+    For sideline condition we assume the maximum noise at takeoff occurs at 1000ft from the ground.     
+    
+Inputs:
+    noise_segment    - SUAVE type vehicle                                                             [Unitless]
+    analyses                                                                                          [Unitless]
+    config                                                                                            [Unitless]
+    mic_loc          - ground microphone index                                                        [meters]            
+
+Outputs:
+    noise_segment.
+       dist  - Distance vector from the aircraft position in relation to the microphone coordinates,     [meters]
+       theta - Polar angle emission vector relatively to the aircraft to the microphone coordinates,     [rad]
+       phi   - Azimuthal angle emission vector relatively to the aircraft to the microphone coordinates, [rad]
+
+Properties Used:
+    None     
+
+
+
+ +

◆ noise_tone_correction()

+ +
+
+ + + + + + + + +
def SUAVE.Methods.Noise.Fidelity_One.Noise_Tools.noise_tone_correction.noise_tone_correction ( SPL)
+
+
This method calculates de correction for spectral irregularities by means of
+    a correction tone factor
+    
+Assumptions:
+    None
+
+Source:
+    None 
+
+Inputs:
+    SPL                     - Sound Pressure Level in 1/3 octave band
+
+Outputs: 
+    tone_correction_max     - Maximum tone correction for a time history signal 
+    
+Properties Used:
+    N/A     
+
+
+
+ +

◆ pnl_noise()

+ +
+
+ + + + + + + + +
def SUAVE.Methods.Noise.Fidelity_One.Noise_Tools.pnl_noise.pnl_noise ( SPL)
+
+
This method calculates de Perceived Noise Level PNL from a 1/3 octave band noise spectra
+ 
+Assumptions:
+    None
+
+Source:
+    None
+ 
+Inputs:
+    SPL - Sound Pressure Level in 1/3 octave band  [dB]
+   
+Outputs:
+    PNL - Perceived Noise Level                    [dB]
+   
+Properties Used:
+    N/A    
+
+
+
+ +

◆ pressure_ratio_to_SPL_arithmetic()

+ +
+
+ + + + + + + + +
def SUAVE.Methods.Noise.Fidelity_One.Noise_Tools.decibel_arithmetic.pressure_ratio_to_SPL_arithmetic ( p_pref_total)
+
+
This computes the total SPL given mutiple acoustic pressure ratios 
+of one of mutiple sources
+
+Assumptions:
+    None
+
+Source:
+    None
+
+Inputs:
+    Pressure Ratios       [unitless]
+
+Outputs: 
+    Sound Pressure Level  [decibel]
+
+Properties Used:
+    N/A 
+
+
+ +

◆ print_airframe_output()

+ +
+
+ + + + + + + + +
def SUAVE.Methods.Noise.Fidelity_One.Noise_Tools.print_airframe_output.print_airframe_output ( SAE_Airframe_Noise_Outputs)
+
+
This prints the airframe noise of a turbofan aircraft
+
+Assumptions:
+   N/A
+
+Inputs: 
+   SAE_Airframe_Noise_Outputs  - Airframe Noise Data Structure  
+
+Outputs:  
+    N/A
+    
+Properties Used:
+    None 
+
+
+
+ +

◆ print_engine_output()

+ +
+
+ + + + + + + + +
def SUAVE.Methods.Noise.Fidelity_One.Noise_Tools.print_engine_output.print_engine_output ( SAE_Engine_Noise_Outputs)
+
+
This prints the engine noise of a turbofan aircraft
+
+Assumptions:
+   N/A
+
+Inputs: 
+   SAE_Engine_Noise_Outputs  - Engine Noise Data Structure  
+
+Outputs:  
+    N/A
+    
+Properties Used:
+    None 
+
+
+
+ +

◆ print_propeller_output()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Noise.Fidelity_One.Noise_Tools.print_propeller_output.print_propeller_output ( speed,
 nsteps,
 time,
 altitude,
 RPM,
 theta,
 dist,
 PNL,
 PNL_dBA 
)
+
+
This prints the noise of a propeller aircraft using SAE noise analysis methods
+
+Assumptions:
+   N/A
+
+Inputs:
+speed     aircraft speed                     [m/s]
+nsteps    numer of timesteps                 [unitless]
+time      time                               [s]
+altitude  aircraft altitude                  [m]
+RPM       rpm of propeller                   [unitless]
+theta     emission angle                     [rad]
+dist      emission distance                  [m]
+PNL       perceived noise level              [dB]
+PNL_dBA   A -weighted perceived noise level  [dBa]
+
+Outputs:  
+    N/A
+    
+Properties Used:
+    None 
+
+
+
+ +

◆ senel_noise()

+ +
+
+ + + + + + + + +
def SUAVE.Methods.Noise.Fidelity_One.Noise_Tools.senel_noise.senel_noise ( SPLt_dBA_max)
+
+
This method calculates the effective perceived noise level (EPNL) based on a time history 
+Perceived Noise Level with Tone Correction (PNLT).
+
+Assumptions:
+    None
+
+Source:
+    None  
+
+Inputs:
+    PNLT                     - Perceived Noise Level with Tone Correction [Unitless]
+
+Outputs: 
+    EPNL                     - Effective Perceived Noise Level            [EPNdB]
+    
+Properties Used:
+    N/A     
+
+
+
+ +

◆ SPL_arithmetic()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Noise.Fidelity_One.Noise_Tools.decibel_arithmetic.SPL_arithmetic ( SPL,
 sum_axis = 2 
)
+
+
This computes the total SPL from multiple sources 
+using decibel arithmetic  
+
+Assumptions:
+    None
+
+Source:
+    None
+
+Inputs:
+    SPL  -  Sound Pressure Level        [dB]
+
+Outputs: 
+    SPL  -  Sound Pressure Level        [dB]
+
+Properties Used:
+    N/A 
+
+
+ +

◆ SPL_harmonic_to_third_octave()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Noise.Fidelity_One.Noise_Tools.SPL_harmonic_to_third_octave.SPL_harmonic_to_third_octave ( SPL,
 f,
 settings 
)
+
+
This method converts the SPL spectrum from blade harmonic passing frequency
+to thrid octave spectrum
+
+Assumptions:
+    N/A
+
+Source: 
+
+Inputs:
+    SPL                    - sound pressure level                          [dB] 
+    f                      - blade passing spectrum frequencies            [Hz]
+    settings.    
+        center_frequencies - center frequencies of the 1/3 octave spectrum [dB]  
+        lower_frequencies  - lower frequencies of the 1/3 octave spectrum  [dB]
+        upper_frequencies  - upper frequencies of the 1/3 octave spectrum  [dB]
+    
+
+Outputs:
+    SPL_third_octave       - SPL in the 1/3 octave spectrum                [dB] 
+
+Properties Used:
+    N/A 
+
+
+ +

◆ SPL_spectra_arithmetic()

+ +
+
+ + + + + + + + +
def SUAVE.Methods.Noise.Fidelity_One.Noise_Tools.decibel_arithmetic.SPL_spectra_arithmetic ( SPL)
+
+
This computes the total SPL spectra from multiple sources 
+using decibel arithmetic  
+
+Assumptions:
+    None
+
+Source:
+    None
+
+Inputs:
+    SPL  -  Sound Pressure Level        [dB]
+
+Outputs: 
+    SPL  -  Sound Pressure Level        [dB]
+
+Properties Used:
+    N/A 
+
+
@@ -106,7 +1159,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/group__Methods-Noise-Fidelity__One-Noise__Tools.js b/doxygen/group__Methods-Noise-Fidelity__One-Noise__Tools.js new file mode 100644 index 00000000..5bccf69b --- /dev/null +++ b/doxygen/group__Methods-Noise-Fidelity__One-Noise__Tools.js @@ -0,0 +1,24 @@ +var group__Methods_Noise_Fidelity__One_Noise__Tools = +[ + [ "atmospheric_attenuation", "group__Methods-Noise-Fidelity__One-Noise__Tools.html#ga1f2076ee762678ad79eeb6ddd1015cec", null ], + [ "compute_blade_section_source_coordinates", "group__Methods-Noise-Fidelity__One-Noise__Tools.html#ga0c2f7123fbd258dd44ccf2da880be986", null ], + [ "compute_building_noise_evaluation_locations", "group__Methods-Noise-Fidelity__One-Noise__Tools.html#ga2115c6ef489f9235ca79940d1698ded8", null ], + [ "compute_ground_noise_evaluation_locations", "group__Methods-Noise-Fidelity__One-Noise__Tools.html#ga6fbec5b86e9ca21288cc9cb488c54362", null ], + [ "compute_noise", "group__Methods-Noise-Fidelity__One-Noise__Tools.html#gab44505e2927a707bfea159420992627d", null ], + [ "dbA_noise", "group__Methods-Noise-Fidelity__One-Noise__Tools.html#gadaf4c1f708ce6f685beba70788ab3162", null ], + [ "epnl_noise", "group__Methods-Noise-Fidelity__One-Noise__Tools.html#gac214e879fce345848be72c5bccc5e026", null ], + [ "generate_building_microphone_points", "group__Methods-Noise-Fidelity__One-Noise__Tools.html#ga4358b9c1e9d041c3ba8e64608154c49c", null ], + [ "generate_ground_microphone_points", "group__Methods-Noise-Fidelity__One-Noise__Tools.html#ga839682011109b34622019da19b522b24", null ], + [ "noise_certification_limits", "group__Methods-Noise-Fidelity__One-Noise__Tools.html#ga0315605f7f0309472b10d24acb13821f", null ], + [ "noise_geometric", "group__Methods-Noise-Fidelity__One-Noise__Tools.html#ga70dc77566e5b6ac7726497db66a92c77", null ], + [ "noise_tone_correction", "group__Methods-Noise-Fidelity__One-Noise__Tools.html#ga2e7b219f0aca430b099643652c0b2e6a", null ], + [ "pnl_noise", "group__Methods-Noise-Fidelity__One-Noise__Tools.html#gad177dfb3205d4bacb8936058e1052c9e", null ], + [ "pressure_ratio_to_SPL_arithmetic", "group__Methods-Noise-Fidelity__One-Noise__Tools.html#ga4f5f73ae49f0fd0a1b26fa23aeff5653", null ], + [ "print_airframe_output", "group__Methods-Noise-Fidelity__One-Noise__Tools.html#ga52c0b7dd2d69cee1af5039f5ba78a40c", null ], + [ "print_engine_output", "group__Methods-Noise-Fidelity__One-Noise__Tools.html#ga1e93c540c3d94c2d289fd93292b31101", null ], + [ "print_propeller_output", "group__Methods-Noise-Fidelity__One-Noise__Tools.html#gad6d95048563f835f37edbdf9d55a2d35", null ], + [ "senel_noise", "group__Methods-Noise-Fidelity__One-Noise__Tools.html#gac0cebe7fa42fd7cc55e2f42e71b5fe87", null ], + [ "SPL_arithmetic", "group__Methods-Noise-Fidelity__One-Noise__Tools.html#ga30a2d00ed78223394db8ef28d1d24715", null ], + [ "SPL_harmonic_to_third_octave", "group__Methods-Noise-Fidelity__One-Noise__Tools.html#ga47ec8dbd2f8972a6f00e1d102a840966", null ], + [ "SPL_spectra_arithmetic", "group__Methods-Noise-Fidelity__One-Noise__Tools.html#ga30c1a7b84da8ee14072c46ba693b4f6f", null ] +]; \ No newline at end of file diff --git a/doxygen/group__Methods-Noise-Fidelity__One.html b/doxygen/group__Methods-Noise-Fidelity__One.html index 9d9d2e3e..bafc6048 100644 --- a/doxygen/group__Methods-Noise-Fidelity__One.html +++ b/doxygen/group__Methods-Noise-Fidelity__One.html @@ -1,9 +1,9 @@ - + - + SUAVE: Fidelity_One @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@
- +
@@ -73,7 +78,9 @@

@@ -122,7 +129,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/group__Methods-Noise-Fidelity__One.js b/doxygen/group__Methods-Noise-Fidelity__One.js index 53c72142..f1c797a0 100644 --- a/doxygen/group__Methods-Noise-Fidelity__One.js +++ b/doxygen/group__Methods-Noise-Fidelity__One.js @@ -1,6 +1,6 @@ var group__Methods_Noise_Fidelity__One = [ - [ "Airframe", "group__Methods-Noise-Fidelity__One-Airframe.html", null ], - [ "Engine", "group__Methods-Noise-Fidelity__One-Engine.html", null ], - [ "Noise Tools", "group__Methods-Noise-Fidelity__One-Noise__Tools.html", null ] + [ "Airframe", "group__Methods-Noise-Fidelity__One-Airframe.html", "group__Methods-Noise-Fidelity__One-Airframe" ], + [ "Engine", "group__Methods-Noise-Fidelity__One-Engine.html", "group__Methods-Noise-Fidelity__One-Engine" ], + [ "Noise Tools", "group__Methods-Noise-Fidelity__One-Noise__Tools.html", "group__Methods-Noise-Fidelity__One-Noise__Tools" ] ]; \ No newline at end of file diff --git a/doxygen/group__Methods-Noise-Fidelity__Zero.html b/doxygen/group__Methods-Noise-Fidelity__Zero.html new file mode 100644 index 00000000..cc70191f --- /dev/null +++ b/doxygen/group__Methods-Noise-Fidelity__Zero.html @@ -0,0 +1,193 @@ + + + + + + + +SUAVE: Fidelity_Zero + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
Fidelity_Zero
+
+
+ +

Correlation type methods for calculating noise. +More...

+ + + + +

+Functions

def SUAVE.Methods.Noise.Fidelity_Zero.shevell.shevell (weight_landing, number_of_engines, thrust_sea_level, thrust_landing)
 
+

Detailed Description

+

Correlation type methods for calculating noise.

+

Function Documentation

+ +

◆ shevell()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Noise.Fidelity_Zero.shevell.shevell ( weight_landing,
 number_of_engines,
 thrust_sea_level,
 thrust_landing 
)
+
+
This uses correlations from Shevell, also used in AA241A/B, to calculate the sources for noise
+
+Assumptions:
+None
+
+Source:
+Stanford AA 241A/B Notes : http://aerodesign.stanford.edu/aircraftdesign/aircraftdesign.html
+
+Inputs:
+    weight_landing     [newtons]
+    number_of_engines  [int]
+    thrust_sea_level   [newtons]
+    thrust_landing     [newtons]
+
+Outputs:
+    output.
+        takeoff        [float]
+        side_line      [float]
+        landing        [float]
+
+Properties Used:
+    baseline noise = 101.
+    various tuned correlations
+
+
+
+
+
+ + + + diff --git a/doxygen/group__Methods-Noise-Fidelity__Zero.js b/doxygen/group__Methods-Noise-Fidelity__Zero.js new file mode 100644 index 00000000..c6467b0e --- /dev/null +++ b/doxygen/group__Methods-Noise-Fidelity__Zero.js @@ -0,0 +1,4 @@ +var group__Methods_Noise_Fidelity__Zero = +[ + [ "shevell", "group__Methods-Noise-Fidelity__Zero.html#ga9408ead0cc82e40fcb427b0f14ac2962", null ] +]; \ No newline at end of file diff --git a/doxygen/group__Methods-Noise.html b/doxygen/group__Methods-Noise.html index 8c429189..a67a8d5c 100644 --- a/doxygen/group__Methods-Noise.html +++ b/doxygen/group__Methods-Noise.html @@ -1,9 +1,9 @@ - + - + SUAVE: Noise @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@
- +

@@ -73,7 +78,9 @@
@@ -103,12 +110,17 @@ - - + + + + + + +

Modules

 Correlations
 Correlation type methods for calculating noise.
 Certification
 
 Fidelity_One
 Description.
 
 Zero Fidelity Zero
 Correlation type methods for calculating noise.
 
 Fidelity_Zero
 Correlation type methods for calculating noise.
 

Detailed Description

Description.

@@ -119,7 +131,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/group__Methods-Noise.js b/doxygen/group__Methods-Noise.js index bf6727da..b7a57874 100644 --- a/doxygen/group__Methods-Noise.js +++ b/doxygen/group__Methods-Noise.js @@ -1,5 +1,7 @@ var group__Methods_Noise = [ - [ "Correlations", "group__Methods-Noise-Correlations.html", null ], - [ "Fidelity_One", "group__Methods-Noise-Fidelity__One.html", "group__Methods-Noise-Fidelity__One" ] + [ "Certification", "group__Methods-Noise-Certification.html", "group__Methods-Noise-Certification" ], + [ "Fidelity_One", "group__Methods-Noise-Fidelity__One.html", "group__Methods-Noise-Fidelity__One" ], + [ "Zero Fidelity Zero", "group__Methods-Noise-Fidelity.html", null ], + [ "Fidelity_Zero", "group__Methods-Noise-Fidelity__Zero.html", "group__Methods-Noise-Fidelity__Zero" ] ]; \ No newline at end of file diff --git a/doxygen/group__Methods-Performance.html b/doxygen/group__Methods-Performance.html index ca551681..d3f25e3d 100644 --- a/doxygen/group__Methods-Performance.html +++ b/doxygen/group__Methods-Performance.html @@ -1,9 +1,9 @@ - + - + SUAVE: Performance @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@
- +
@@ -73,7 +78,9 @@
@@ -103,23 +110,217 @@ + + + + + + - - + + - - - - + + + +

Functions

def SUAVE.Methods.Performance.electric_payload_range.electric_payload_range (vehicle, mission, cruise_segment_tag, display_plot=True)
 
def SUAVE.Methods.Performance.electric_V_h_diagram.electric_V_h_diagram (vehicle, analyses, CL_max, delta_isa=0., grid_points=20., altitude_ceiling=2e4 *Units.ft, max_speed=130 *Units['m/s'], test_omega=800. *Units.rpm, display_plot=True)
 
def SUAVE.Methods.Performance.estimate_landing_field_length.estimate_landing_field_length (vehicle, analyses, airport)
 
def SUAVE.Methods.Performance.estimate_stall_speed.estimate_stall_speed (vehicle_mass, reference_area, altitude, maximum_lift_coefficient)
 
def SUAVE.Methods.Performance.estimate_take_off_field_length.estimate_take_off_field_length (vehicle, analyses, airport, compute_2nd_seg_climb=0)
 
def SUAVE.Methods.Performance.find_takeoff_weight_given_tofl.find_takeoff_weight_given_tofl (vehicle, analyses, airport, target_tofl)
 
def SUAVE.Methods.Performance.find_take_off_weight_given_tofl.find_take_off_weight_given_tofl (vehicle, analyses, airport, target_tofl)
 
def SUAVE.Methods.Performance.payload_range.payload_range (vehicle, mission, cruise_segment_tag, reserves=0.)
 
def SUAVE.Methods.Performance.size_mission_range_given_weights.size_mission_range_given_weights (vehicle, mission, cruise_segment_tag, mission_payload, takeoff_weight=0., reserve_fuel=0.)
 
def SUAVE.Methods.Performance.size_weights_given_mission_range.size_weights_given_mission_range (vehicle, mission, cruise_segment_tag, mission_payload, target_range, reserve_fuel=0.)
 
def SUAVE.Methods.Performance.propeller_single_point.propeller_single_point (energy_network, analyses, pitch, omega, altitude, delta_isa, speed, i_prop=0, plots=False, print_results=False)
 
def SUAVE.Methods.Performance.V_n_diagram.V_n_diagram (vehicle, analyses, weight, altitude, delta_ISA)
 

Detailed Description

This is a set of basic aircraft performance estimation functions.

It includes field length and range calculations.

Function Documentation

+ +

◆ electric_payload_range()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Performance.electric_payload_range.electric_payload_range ( vehicle,
 mission,
 cruise_segment_tag,
 display_plot = True 
)
+
+
electric_payload_range(vehicle,
+                       mission,
+                       cruise_segment_tag,
+                       display_plot=True):
+
+    Calculates and optionally displays a payload range diagram for a
+    Variable Cruise Distance - State of Charge SUAVE Mission and Vehicle.
+
+    Sources:
+    N/A
+
+    Assumptions:
+
+    Assumes use of Battery Propeller Energy Network
+
+    Inputs:
+
+        vehicle                         SUAVE Vehicle Structure
+            .mass_properties            SUAVE Mass Properties Structure
+                .operating_empty        Vehicle Operating Empty Mass    [kg]
+                .max_payload            Vehicle Maximum Payload Mass    [kg]
+                .max_takeoff            Vehicle Maximum Takeoff Mass    [kg]
+
+        mission                         SUAVE Mission Structure
+            .Variable_Range_Cruise      Mission Type
+                .Given_State_of_Charge  Convergence Criteria
+            .cruise_tag                 Mission Segment Tag             [String]
+            .target_state_of_charge     End Mission State of Charge     [Unitless]
+
+        cruise_segment_tag              mission.cruise_tag              [String]
+
+    Outputs:
+
+        payload_range = Data()
+            .range                      [0, Max PLD Range, Ferry Range] [m]
+            .payload                    [Max PLD, Max PLD , 0]          [kg]
+            .takeoff_weight             [MTOW, MTOW, OEW]               [kg]
+
+
+
+ +

◆ electric_V_h_diagram()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Performance.electric_V_h_diagram.electric_V_h_diagram ( vehicle,
 analyses,
 CL_max,
 delta_isa = 0.,
 grid_points = 20.,
 altitude_ceiling = 2e4 * Units.ft,
 max_speed = 130 * Units['m/s'],
 test_omega = 800. * Units.rpm,
 display_plot = True 
)
+
+
electric_V_h_diagram(vehicle,
+                        analyses,
+                        delta_isa = 0.,
+                        grid_points = 20.,
+                        altitude_ceiling = 2e4 * Units.ft,
+                        max_speed = 130 * Units['m/s'],
+                        test_omega = 800. * Units.rpm,
+                        display_plot = True,
+                        climb_rate_contours = [0.]
+                        ):
+
+    Calculates and optionally displays climb rate and contours thereof over
+    a specified airspeed and altitude range. Climb rate determination ref.
+    Raymer, "Aircraft Design: A Conceptual Approach"
+
+    Sources:
+    D. Raymer, "Aircraft Design: A Conceptual Approach"
+
+    Assumptions:
+
+    Assumes use of Battery Propeller Energy Network
+
+    Inputs:
+
+        vehicle                         SUAVE Vehicle Structure
+            .mass_properties
+                .takeoff                                            [kg]
+        analyses                        SUAVE Analyses Structure
+            .atmosphere
+                .planet
+                    .sea_level_gravity                              [m/s^2]
+        delta_isa                       ISA Temperature Offset      [deg. K/C]
+        grid_points                     Num. Test Points per Dim.   [Int]
+        altitude_ceiling                Maximum Test Altitude       [User Set]
+        max_speed                       Maximum Test Speed          [User Set]
+        test_omega                      Maximum Power Prop Speed    [User Set]
+        display_plot                    Flag for Plot Generation    [Boolean] 
+
+    Outputs:
+
+        climb_rate                      Climb Rates at Test Points  [ft/min]
+
+
+

◆ estimate_landing_field_length()

@@ -178,6 +379,62 @@

+

◆ estimate_stall_speed()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Performance.estimate_stall_speed.estimate_stall_speed ( vehicle_mass,
 reference_area,
 altitude,
 maximum_lift_coefficient 
)
+
+
Calculates the stall speed of an aircraft at a given altitude and a maximum lift coefficient.
+
+    Sources:
+    N/A
+
+    Assumptions:
+    None 
+
+    Inputs:
+        vehicle_mass                    vehicle mass             [kg]
+        reference_area                  vehicle reference area   [m^2] 
+        altitude                        cruise altitude          [m]
+        maximum_lift_coefficient        maximum lift coefficient [unitless] 
+        
+    Outputs: 
+        V_stall                         stall speed              [m/s]
+
+
+

◆ estimate_take_off_field_length()

@@ -236,7 +493,7 @@

-

◆ find_takeoff_weight_given_tofl()

+ +

◆ find_take_off_weight_given_tofl()

- + @@ -377,47 +634,71 @@

-

◆ size_mission_range_given_weights()

+ +

◆ propeller_single_point()

def SUAVE.Methods.Performance.find_takeoff_weight_given_tofl.find_takeoff_weight_given_tofl def SUAVE.Methods.Performance.find_take_off_weight_given_tofl.find_take_off_weight_given_tofl (   vehicle,
- + - + - + - + + + + + + + + + + + + + - + - + - + + + + + + + + + + + + + @@ -426,42 +707,71 @@

-
Calculates a vehicle's range and fuel for a given takeoff weight and payload
-
-Assumptions:
-Constant altitude cruise
-
-Source:
-N/A
-
-Inputs:
-vehicle.mass_properties.
-  operating_empty                     [kg]
-  takeoff                             [kg]
-mission.segments[0].analyses.weights.
-  mass_properties.takeoff             [kg]
-cruise_segment_tag                    <string>
-mission_payload                       [kg]
-takeoff_weight (optional)             [kg]
-reserve_fuel                          [kg]
-
-Outputs:
-distance                              [m]
-fuel                                  [kg]
-
-Properties Used:
-N/A
+
propeller_single_point(energy_network,
+                          analyses,
+                          pitch,
+                          omega,
+                          altitude,
+                          delta_isa,
+                          speed,
+                          plots=False,
+                          print_results=False):
+
+    Uses SUAVE's BEVW propeller model to evaluate propeller performance at a
+    single altitude, pitch command, and angular velocity. Can be used indep-
+    endently, or as part of creation of a propller maps or flight envelopes.
+
+    Sources:
+    N/A
+
+    Assumptions:
+
+    Assumes use of Battery Propeller Energy Network, All Assumptions of
+    the BEVW model.
+
+    Inputs:
+
+        energy_network       SUAVE Energy Network
+            .propeller       SUAVE Propeller Data Structure
+
+        analyses             SUAVE Analyses Structure
+            .atmosphere      SUAVE Atmosphere Analysis Object
+
+        pitch                Propeller Pitch/Collective                    [User Set]
+        omega                Test Angular Velocity                         [User Set]
+        altitude             Test Altitude                                 [User Set]
+        delta_isa            Atmosphere Temp Offset                        [K]
+        speed                Propeller Intake Speed                        [User Set]
+        HFW                  Flag for use of helical fixed wake for rotor  [Boolean]
+        plots                Flag for Plot Generation                      [Boolean]
+        print_results        Flag for Terminal Output                      [Boolean]
+
+    Outputs:
+
+        results                             SUAVE Data Object
+            .thrust                         BEVW Thrust Prediction      [N]
+            .torque                         BEVW Torque Prediction      [N-m]
+            .power                          BEVW Power Prediction       [W]
+            .power_coefficient              BEVW Cp Prediction          [Unitless]
+            .efficiency                     BEVW Efficiency Prediction  [Unitless]
+            .induced_axial_velocity         BEVW Ind. V_a Prediction    [m/s]
+            .induced_tangential_velocity    BEVW Ind. V_tPrediction     [m/s]
+            .radial_distribution            BEVW Radial Stations        [m]
+            .thrust_distribution            BEVW T Dist. Prediction     [N/m]
+            .torque_distribution            BEVW Q Dist. Prediction     [(N-m)/m]
+            .tangential_velocity            BEVW V_t Prediction         [m/s]
+            .axial_velocity                 BEVW V_a Prediction         [m/s]
 
-
-

◆ size_weights_given_mission_range()

+ +

◆ V_n_diagram()

def SUAVE.Methods.Performance.size_mission_range_given_weights.size_mission_range_given_weights def SUAVE.Methods.Performance.propeller_single_point.propeller_single_point (  vehicle, energy_network,
 mission, analyses,
 cruise_segment_tag, pitch,
 omega,
 altitude,
 mission_payload, delta_isa,
 takeoff_weight = 0., speed,
 reserve_fuel = 0. i_prop = 0,
 plots = False,
 print_results = False 
- + @@ -470,31 +780,25 @@

- - - - - - - + - + - + - + @@ -503,34 +807,37 @@

-
Calculates a vehicle's fuel and takeoff weight for a given range. Also returns the range.
-
-Assumptions:
-Constant altitude cruise
+
Computes a V-n diagram for a given aircraft and given regulations for ISA conditions
 
 Source:
-N/A
+S. Gudmundsson "General Aviation Aircraft Design: Applied Methods and Procedures", Butterworth-Heinemann; 1 edition
+CFR FAR Part 23: https://www.ecfr.gov/cgi-bin/text-idx?SID=0e6a13c7c1de7f501d0eb0a4d71418bd&mc=true&tpl=/ecfrbrowse/Title14/14cfr23_main_02.tpl
+CFR FAR Part 25: https://www.ecfr.gov/cgi-bin/text-idx?tpl=/ecfrbrowse/Title14/14cfr25_main_02.tpl
 
 Inputs:
-vehicle.mass_properties.
-  operating_empty                     [kg]
-  max_zero_fuel                       [kg]
-  max_takeoff                         [kg]
-  max_payload                         [kg]
-  max_fuel                            [kg]
-mission                               [SUAVE data structure]
-cruise_segment_tag                    <string>
-mission_payload                       [kg]
-target_range                          [m]
-reserve_fuel (optional)               [kg]
+analyses.base.atmosphere               [SUAVE data type]
+vehicle.
+  reference_area                       [m^2]
+  maximum_lift_coefficient             [Unitless]
+  minimum_lift_coefficient             [Unitless]
+  chords.mean_aerodynamic              [m]
+  envelope.FARpart_number              [Unitless]
+    limit_loads.positive               [Unitless]
+    limit_loads.negative               [Unitless]
+    cruise_mach                        [Unitless]
+weight                                 [kg]
+altitude                               [m]
+delta_ISA                              [deg C]
 
 Outputs:
-distance                              [m]
-fuel                                  [kg]
-tow                                   [kg]
+V_n_data
 
 Properties Used:
 N/A
+
+Description:
+The script creates an aircraft V-n diagram based on the input parameters specified by the user.
+Depending on the certification flag, an appropriate diagram, output and log files are created.
 
@@ -541,7 +848,7 @@

Generated by - doxygen 1.8.14 + doxygen 1.8.15 diff --git a/doxygen/group__Methods-Performance.js b/doxygen/group__Methods-Performance.js index e94d5a91..4deeacc3 100644 --- a/doxygen/group__Methods-Performance.js +++ b/doxygen/group__Methods-Performance.js @@ -1,9 +1,12 @@ var group__Methods_Performance = [ + [ "electric_payload_range", "group__Methods-Performance.html#ga55d437856775d9b4665f79ff64e049af", null ], + [ "electric_V_h_diagram", "group__Methods-Performance.html#ga5ae69085f2cfc628cf91ec9845690785", null ], [ "estimate_landing_field_length", "group__Methods-Performance.html#ga938d16e3a48381c15d259c87588d5fc5", null ], + [ "estimate_stall_speed", "group__Methods-Performance.html#ga8eb517a7f25188f9ecc77136c0cc8c0d", null ], [ "estimate_take_off_field_length", "group__Methods-Performance.html#ga02d56e7967cb530e3f0e4fea121599bd", null ], - [ "find_takeoff_weight_given_tofl", "group__Methods-Performance.html#ga42e523c866aa6dcc695a6c587eaf0123", null ], + [ "find_take_off_weight_given_tofl", "group__Methods-Performance.html#ga8f5076bde3c82c3a6b2d6f07cd4d64f0", null ], [ "payload_range", "group__Methods-Performance.html#gab6d53e36ef47e7ccd43b25ea7bab6c40", null ], - [ "size_mission_range_given_weights", "group__Methods-Performance.html#ga183d28f783ad524339c6deb9cf3cf46c", null ], - [ "size_weights_given_mission_range", "group__Methods-Performance.html#ga71b994da90770582a5f3d3bff7e2fc3a", null ] + [ "propeller_single_point", "group__Methods-Performance.html#gaf86c59d2f4dabb49deb21a513190fd13", null ], + [ "V_n_diagram", "group__Methods-Performance.html#ga64d1044ea54a608b4a8c4a51c3d79c12", null ] ]; \ No newline at end of file diff --git a/doxygen/group__Methods-Power-Battery-Discharge.html b/doxygen/group__Methods-Power-Battery-Discharge.html index b6d6345b..a0739a46 100644 --- a/doxygen/group__Methods-Power-Battery-Discharge.html +++ b/doxygen/group__Methods-Power-Battery-Discharge.html @@ -1,9 +1,9 @@ - + - + SUAVE: Discharge @@ -13,14 +13,13 @@ - @@ -33,13 +32,13 @@

@@ -57,9 +56,11 @@
def SUAVE.Methods.Performance.size_weights_given_mission_range.size_weights_given_mission_range def SUAVE.Methods.Performance.V_n_diagram.V_n_diagram (   vehicle,  mission,
 cruise_segment_tag, analyses,
 mission_payload, weight,
 target_range, altitude,
 reserve_fuel = 0. delta_ISA 
SUAVE -  1.1.0 +  2.4.0
An Aerospace Vehicle Environment for Designing Future Aircraft
- @@ -48,7 +47,7 @@ onblur="searchBox.OnSearchFieldFocus(false)" onkeyup="searchBox.OnSearchFieldChange(event)"/> - +
- +
@@ -73,7 +74,9 @@

@@ -168,9 +171,7 @@

diff --git a/doxygen/group__Methods-Power-Battery-Ragone.html b/doxygen/group__Methods-Power-Battery-Ragone.html index f173463e..da7b9be3 100644 --- a/doxygen/group__Methods-Power-Battery-Ragone.html +++ b/doxygen/group__Methods-Power-Battery-Ragone.html @@ -1,9 +1,9 @@ - + - + SUAVE: Ragone @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@

- +
@@ -73,7 +78,9 @@

@@ -294,7 +301,7 @@

Generated by - doxygen 1.8.14 + doxygen 1.8.15

diff --git a/doxygen/group__Methods-Power-Battery-Sizing.html b/doxygen/group__Methods-Power-Battery-Sizing.html index e375975f..4eab067c 100644 --- a/doxygen/group__Methods-Power-Battery-Sizing.html +++ b/doxygen/group__Methods-Power-Battery-Sizing.html @@ -1,9 +1,9 @@ - + - + SUAVE: Sizing @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@
- +
@@ -73,7 +78,9 @@
@@ -103,14 +110,77 @@ + + - - + + +

Functions

def SUAVE.Methods.Power.Battery.Sizing.initialize_from_circuit_configuration.initialize_from_circuit_configuration (battery, module_weight_factor=1.42)
 
def SUAVE.Methods.Power.Battery.Sizing.initialize_from_energy_and_power.initialize_from_energy_and_power (battery, energy, power, max='hard')
 
def SUAVE.Methods.Power.Battery.Sizing.initialize_from_mass.initialize_from_mass (battery, mass)
 
def SUAVE.Methods.Power.Battery.Sizing.initialize_from_mass.initialize_from_mass (battery, module_weight_factor=1.42)
 initialize_from_mass.py More...
 

Detailed Description

Functions to size battery from mass, specific energy, and specific power.

Function Documentation

+ +

◆ initialize_from_circuit_configuration()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Power.Battery.Sizing.initialize_from_circuit_configuration.initialize_from_circuit_configuration ( battery,
 module_weight_factor = 1.42 
)
+
+
Calculate pack level properties of battery using cell 
+properties and module configuraton
+
+Assumptions:
+Total battery pack mass contains build-up factor (1.42) for battery casing,
+internal wires, thermal management system and battery management system 
+Factor computed using information of battery properties for X-57 Maxwell 
+Aircraft
+
+Source:
+Cell Charge: Chin, J. C., Schnulo, S. L., Miller, T. B., Prokopius, K., and Gray, 
+J., Battery Performance Modeling on Maxwell X-57",AIAA Scitech, San Diego, CA,
+2019. URLhttp://openmdao.org/pubs/chin_battery_performance_x57_2019.pdf.     
+
+Inputs:
+mass              
+battery.cell
+  nominal_capacity    [amp-hours]            
+  nominal_voltage     [volts]
+  pack_config         [unitless]
+  mass                [kilograms]
+                      
+Outputs:              
+ battery.             
+   max_energy         [watt-hours]
+   max_power          [watts]
+   initial_max_energy [watt-hours]
+   specific_energy    [watt-hours/kilogram]
+   charging_voltage   [volts]
+   charging_current   [amps]
+   mass_properties.
+    mass              [kilograms] 
+
+
+

◆ initialize_from_energy_and_power()

@@ -169,8 +239,8 @@

-

◆ initialize_from_mass()

+ +

◆ initialize_from_mass()

diff --git a/doxygen/group__Methods-Power-Battery-Sizing.js b/doxygen/group__Methods-Power-Battery-Sizing.js index 6cabc561..7935602c 100644 --- a/doxygen/group__Methods-Power-Battery-Sizing.js +++ b/doxygen/group__Methods-Power-Battery-Sizing.js @@ -1,5 +1,6 @@ var group__Methods_Power_Battery_Sizing = [ + [ "initialize_from_circuit_configuration", "group__Methods-Power-Battery-Sizing.html#gafbdd621a55d789f06314d56b63488caa", null ], [ "initialize_from_energy_and_power", "group__Methods-Power-Battery-Sizing.html#ga87ecd44d90a6e2da93c783e7da06eaf0", null ], - [ "initialize_from_mass", "group__Methods-Power-Battery-Sizing.html#ga47f170235ace9f4f3bf06f1857155164", null ] + [ "initialize_from_mass", "group__Methods-Power-Battery-Sizing.html#ga64adcee791fa4cfe0d21153e3ec5dbe5", null ] ]; \ No newline at end of file diff --git a/doxygen/group__Methods-Power-Battery-State__Estimation__Models.html b/doxygen/group__Methods-Power-Battery-State__Estimation__Models.html new file mode 100644 index 00000000..9ee347f7 --- /dev/null +++ b/doxygen/group__Methods-Power-Battery-State__Estimation__Models.html @@ -0,0 +1,120 @@ + + + + + + + +SUAVE: State_Estimation_Models + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
State_Estimation_Models
+
+
+ +

Functions to evaluate battery state variables. +More...

+

Functions to evaluate battery state variables.

+
+
+ + + + diff --git a/doxygen/group__Methods-Power-Battery-Variable__Mass.html b/doxygen/group__Methods-Power-Battery-Variable__Mass.html index 3a40a9f9..44be0498 100644 --- a/doxygen/group__Methods-Power-Battery-Variable__Mass.html +++ b/doxygen/group__Methods-Power-Battery-Variable__Mass.html @@ -1,9 +1,9 @@ - + - + SUAVE: Variable_Mass @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@
- +

@@ -73,7 +78,9 @@
@@ -194,7 +201,7 @@

Generated by - doxygen 1.8.14 + doxygen 1.8.15

diff --git a/doxygen/group__Methods-Power-Battery.html b/doxygen/group__Methods-Power-Battery.html index 84d7c44a..34408d9d 100644 --- a/doxygen/group__Methods-Power-Battery.html +++ b/doxygen/group__Methods-Power-Battery.html @@ -1,9 +1,9 @@ - + - + SUAVE: Battery @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@
- +
@@ -73,7 +78,9 @@

@@ -92,7 +99,8 @@
Battery
@@ -103,8 +111,8 @@ - - + + @@ -115,9 +123,263 @@ +

Modules

 Discharge
 Functions to evaluate battery discharge losses and voltage requirements.
 State_Estimation_Models
 Functions to evaluate battery state variables.
 
 Ragone
 Functions to evaluate a Ragone of the battery.
 Variable_Mass
 Functions pertaining to variable mass batteries (such as metal air)
 
+ + + + + + + +

+Functions

def SUAVE.Methods.Power.Battery.append_initial_battery_conditions.append_initial_battery_conditions (segment, battery)
 
def SUAVE.Methods.Power.Battery.compute_net_generated_battery_heat.compute_net_generated_battery_heat (n_total, battery, Q_heat_gen, numerics)
 
def SUAVE.Methods.Power.Battery.pack_battery_conditions.pack_battery_conditions (conditions, battery, avionics_payload_power, P)
 pack_battery_conditions.py More...
 

Detailed Description

Functions pertaining to battery discharge and sizing.

+

Function Documentation

+ +

◆ append_initial_battery_conditions()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Power.Battery.append_initial_battery_conditions.append_initial_battery_conditions ( segment,
 battery 
)
+
+
Packs the initial battery conditions
+
+    Assumptions:
+    Battery temperature is set to one degree hotter than ambient 
+    temperature for robust convergence. Initial mission energy, maxed aged energy, and 
+    initial segment energy are the same. Cycle day is zero unless specified, resistance_growth_factor and
+    capacity_fade_factor is one unless specified in the segment
+
+    Source:
+    N/A
+
+    Inputs:  
+        atmosphere.temperature             [Kelvin]
+        
+        Optional:
+        segment.
+             battery_cycle_day                  [unitless]
+             battery_pack_temperature           [Kelvin]
+             battery_charge_throughput          [Ampere-Hours] 
+             battery_resistance_growth_factor   [unitless]
+             battery_capacity_fade_factor       [unitless]
+             battery_discharge                  [boolean]
+             increment_battery_cycle_day        [boolean]
+           
+    Outputs:
+        segment
+           battery_discharge                    [boolean]
+           increment_battery_cycle_day          [boolean]
+        segment.state.conditions.propulsion
+           battery_discharge_flag               [boolean]
+           battery_max_initial_energy           [watts]
+           battery_energy                       [watts]
+           battery_max_aged_energy              [watts]    
+           battery_pack_temperature             [kelvin]
+           battery_cycle_day                    [int]
+           battery_cell_charge_throughput       [Ampere-Hours] 
+           battery_resistance_growth_factor     [unitless]
+           battery_capacity_fade_factor         [unitless]
+
+
+
+
+    Properties Used:
+    None
+
+
+
+ +

◆ compute_net_generated_battery_heat()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Power.Battery.compute_net_generated_battery_heat.compute_net_generated_battery_heat ( n_total,
 battery,
 Q_heat_gen,
 numerics 
)
+
+
Computes the net heat generated in a battery during cycling. 
+
+Assumptions:
+1) Battery pack cell heat transfer can be modelled as a cooling columns in a cross-flow
+2) Isothermal battery cell - the temperature at the center of the cell is the same at 
+the surface of the cell
+
+Source: 
+Heat Transfer Model:
+Pakowski, Zdzisław. "Fundamentals of Heat and Mass Transfer, Frank P Incropera,
+David P DeWitt, Theodore L Bergman, Adrienne S Lavine, J. Wiley & Sons, Hoboken
+NJ (2007), 997 pp." (2007): 1683-1684.,  Chapter 7 pg 437-446 
+
+Inputs:  
+    battery. 
+          h                         (heat transfer coefficient)  [W/(m^2*K)] 
+          As_cell                   (battery cell surface area)  [meters^2]
+          H_cell                    (battery cell height)        [meters]
+          T_ambient                 (ambient temperature)        [Kelvin]
+          T_current                 (pack temperature)           [Kelvin]
+          T_cell                    (battery cell temperature)   [Kelvin] 
+          heat_transfer_efficiency                               [unitless]
+  
+  Outputs:
+    battery. 
+         net_power                                               [Watts] 
+ 
+
+Properties Used:
+None 
+
+
+
+ +

◆ pack_battery_conditions()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Power.Battery.pack_battery_conditions.pack_battery_conditions ( conditions,
 battery,
 avionics_payload_power,
 P 
)
+
+ +

pack_battery_conditions.py

+

Created: Sep 2021, M. Clarke

Packs the results from the network into propulsion data structures.
+
+    Assumptions:
+    None
+
+    Source:
+    N/A
+
+    Inputs: 
+    battery.
+           inputs.current                  [Amperes]
+           current_energy                  [Joules]
+           voltage_open_circuit            [Volts]
+           voltage_under_load              [Volts] 
+           inputs.power_in                 [Watts]
+           max_energy                      [Joules]
+           cell_charge_throughput          [Ampere-hours]
+           age                             [days]
+           internal_resistance             [Ohms]
+           state_of_charge                 [unitless]
+           pack_temperature                [Kelvin]
+           mass_properties.mass            [kilograms] 
+           cell_voltage_under_load         [Volts]  
+           cell_voltage_open_circuit       [Volts]  
+           cell_current                    [Amperes]
+           cell_temperature                [Kelvin] 
+           heat_energy_generated           [Joules]
+           cell_joule_heat_fraction        [unitless]  
+           cell_entropy_heat_fraction      [unitless] 
+           
+    Outputs:
+        conditions.propulsion.
+           battery_current                    [Amperes]
+           battery_energy                     [Joules]     
+           battery_voltage_open_circuit       [Volts]     
+           battery_voltage_under_load         [Volts]      
+           battery_power_draw                 [Watts]     
+           battery_max_aged_energy            [Joules]        
+           battery_cycle_day                  [unitless]
+           battery_internal_resistance        [Ohms]
+           battery_state_of_charge            [unitless]
+           battery_pack_temperature           [Kelvin]
+           battery_efficiency                 [unitless]
+           payload_efficiency                 [unitless]
+           battery_specfic_power              [Watt-hours/kilogram]     
+           electronics_efficiency             [unitless]
+           battery_cell_power_draw            [Watts]
+           battery_cell_energy                [Joules]
+           battery_cell_voltage_under_load    [Volts]  
+           battery_cell_voltage_open_circuit  [Volts]  
+           battery_cell_current               [Amperes]
+           battery_cell_temperature           [Kelvin]
+           battery_cell_charge_throughput     [Ampere-Hours]
+           battery_cell_heat_energy_generated [Joules]
+           battery_cell_joule_heat_fraction   [unitless]  
+           battery_cell_entropy_heat_fraction [unitless] 
+
+    Properties Used:
+    None
+
+
+

@@ -125,7 +387,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/group__Methods-Power-Battery.js b/doxygen/group__Methods-Power-Battery.js index 3b80e502..cdc8f728 100644 --- a/doxygen/group__Methods-Power-Battery.js +++ b/doxygen/group__Methods-Power-Battery.js @@ -1,7 +1,10 @@ var group__Methods_Power_Battery = [ - [ "Discharge", "group__Methods-Power-Battery-Discharge.html", "group__Methods-Power-Battery-Discharge" ], + [ "State_Estimation_Models", "group__Methods-Power-Battery-State__Estimation__Models.html", null ], [ "Ragone", "group__Methods-Power-Battery-Ragone.html", "group__Methods-Power-Battery-Ragone" ], [ "Sizing", "group__Methods-Power-Battery-Sizing.html", "group__Methods-Power-Battery-Sizing" ], - [ "Variable_Mass", "group__Methods-Power-Battery-Variable__Mass.html", "group__Methods-Power-Battery-Variable__Mass" ] + [ "Variable_Mass", "group__Methods-Power-Battery-Variable__Mass.html", "group__Methods-Power-Battery-Variable__Mass" ], + [ "append_initial_battery_conditions", "group__Methods-Power-Battery.html#ga5192afc20c7fa0cebe875647638fae9b", null ], + [ "compute_net_generated_battery_heat", "group__Methods-Power-Battery.html#gaf8a4ff96d76d1f6e9153f7f16a700145", null ], + [ "pack_battery_conditions", "group__Methods-Power-Battery.html#ga839a4cfa069265f012f4f5d5d39503d6", null ] ]; \ No newline at end of file diff --git a/doxygen/group__Methods-Power-Fuel__Cell-Chemistry.html b/doxygen/group__Methods-Power-Fuel__Cell-Chemistry.html deleted file mode 100644 index 292e32dc..00000000 --- a/doxygen/group__Methods-Power-Fuel__Cell-Chemistry.html +++ /dev/null @@ -1,182 +0,0 @@ - - - - - - - -SUAVE: Chemistry - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.1.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
-
- - - - - - -
-
-
- - - -
-
- -
-
-
- -
- -
-
- - -
- -
- -
- -
-
Chemistry
-
-
- -

Fuel_Cell methods contain the functions for the fuel cell analyses. -More...

- - - - -

-Functions

def SUAVE.Methods.Power.Fuel_Cell.Chemistry.hydrogen.hydrogen (fuel_cell, conditions, numerics)
 
-

Detailed Description

-

Fuel_Cell methods contain the functions for the fuel cell analyses.

-

Function Documentation

- -

◆ hydrogen()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Power.Fuel_Cell.Chemistry.hydrogen.hydrogen ( fuel_cell,
 conditions,
 numerics 
)
-
-
Calculates chemical properties of fuel cell exhaust
- 
-   Assumptions: 
-   Stoichiometric reaction
-   
-   
-   Inputs:
-   fuel_cell.
-     efficiency                     [dimensionless]
-     inputs.
-       power_in                     [Watts]
-     propellant.
-       tag
-       specific_energy              [J/kg]
-     oxidizer.
-       Composition.
-         O2
-   thermo.
-     gamma                          [dimensionless]
-     cp                             [J/kg-K]
-     Tt(to be modified)             [K]
-     Pt(to be modified)             [Pa]
-   
-   Outputs:
-     mdot                           [kg/s]
-     mdot+mdot_air                  [kg/s]
-
-
-
-
- - - - diff --git a/doxygen/group__Methods-Power-Fuel__Cell-Chemistry.js b/doxygen/group__Methods-Power-Fuel__Cell-Chemistry.js deleted file mode 100644 index 427a9574..00000000 --- a/doxygen/group__Methods-Power-Fuel__Cell-Chemistry.js +++ /dev/null @@ -1,4 +0,0 @@ -var group__Methods_Power_Fuel__Cell_Chemistry = -[ - [ "hydrogen", "group__Methods-Power-Fuel__Cell-Chemistry.html#gae19781cb3391103fa518fbb0bee0b7dd", null ] -]; \ No newline at end of file diff --git a/doxygen/group__Methods-Power-Fuel__Cell-Discharge.html b/doxygen/group__Methods-Power-Fuel__Cell-Discharge.html index a0b7ec1c..8a1c17e2 100644 --- a/doxygen/group__Methods-Power-Fuel__Cell-Discharge.html +++ b/doxygen/group__Methods-Power-Fuel__Cell-Discharge.html @@ -1,9 +1,9 @@ - + - + SUAVE: Discharge @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@
- +
@@ -73,7 +78,9 @@
@@ -399,7 +406,7 @@

Generated by - doxygen 1.8.14 + doxygen 1.8.15

diff --git a/doxygen/group__Methods-Power-Fuel__Cell-Sizing.html b/doxygen/group__Methods-Power-Fuel__Cell-Sizing.html index be233aed..c10fcfb2 100644 --- a/doxygen/group__Methods-Power-Fuel__Cell-Sizing.html +++ b/doxygen/group__Methods-Power-Fuel__Cell-Sizing.html @@ -1,9 +1,9 @@ - + - + SUAVE: Sizing @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@
- +
@@ -73,7 +78,9 @@

@@ -204,7 +211,7 @@

Generated by - doxygen 1.8.14 + doxygen 1.8.15

diff --git a/doxygen/group__Methods-Power-Fuel__Cell.html b/doxygen/group__Methods-Power-Fuel__Cell.html index 87e89f33..f8ecfc0e 100644 --- a/doxygen/group__Methods-Power-Fuel__Cell.html +++ b/doxygen/group__Methods-Power-Fuel__Cell.html @@ -1,9 +1,9 @@ - + - + SUAVE: Fuel_Cell @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@
- +
@@ -73,7 +78,9 @@
@@ -103,9 +110,6 @@ - - - @@ -122,7 +126,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/group__Methods-Power-Fuel__Cell.js b/doxygen/group__Methods-Power-Fuel__Cell.js index 431561f5..d0daa9ec 100644 --- a/doxygen/group__Methods-Power-Fuel__Cell.js +++ b/doxygen/group__Methods-Power-Fuel__Cell.js @@ -1,6 +1,5 @@ var group__Methods_Power_Fuel__Cell = [ - [ "Chemistry", "group__Methods-Power-Fuel__Cell-Chemistry.html", "group__Methods-Power-Fuel__Cell-Chemistry" ], [ "Discharge", "group__Methods-Power-Fuel__Cell-Discharge.html", "group__Methods-Power-Fuel__Cell-Discharge" ], [ "Sizing", "group__Methods-Power-Fuel__Cell-Sizing.html", "group__Methods-Power-Fuel__Cell-Sizing" ] ]; \ No newline at end of file diff --git a/doxygen/group__Methods-Power-Turboelectric-Discharge.html b/doxygen/group__Methods-Power-Turboelectric-Discharge.html new file mode 100644 index 00000000..1d8d5c01 --- /dev/null +++ b/doxygen/group__Methods-Power-Turboelectric-Discharge.html @@ -0,0 +1,181 @@ + + + + + + + +SUAVE: Discharge + + + + + + + + + + + + + + + +
+
+

Modules

 Chemistry
 Fuel_Cell methods contain the functions for the fuel cell analyses.
 
 Discharge
 Functions to evaluate fuel cell discharge losses and voltage requirements.
 
+ + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
Discharge
+
+
+ +

Functions to evaluate the use of a turboelectric powertrain to provide electric power. +More...

+ + + + + +

+Functions

def SUAVE.Methods.Power.Turboelectric.Discharge.zero_fidelity.zero_fidelity (turboelectric, conditions, numerics)
 zero_fidelity.py More...
 
+

Detailed Description

+

Functions to evaluate the use of a turboelectric powertrain to provide electric power.

+

Function Documentation

+ +

◆ zero_fidelity()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Power.Turboelectric.Discharge.zero_fidelity.zero_fidelity ( turboelectric,
 conditions,
 numerics 
)
+
+ +

zero_fidelity.py

+

Created : Nov 2019, K. Hamilton

Modified: Nov 2021, S. Claridge

+

Zero Fidelity

+
Assumptions:
+constant efficiency
+
+Inputs:
+    turboelectric.
+        inputs.
+            power_in              [W]
+        propellant.
+            specific_energy       [J/kg]
+        efficiency    
+
+Outputs:
+    mdot                          [kg/s]
+
+
+
+
+ + + + diff --git a/doxygen/group__Methods-Power-Turboelectric-Discharge.js b/doxygen/group__Methods-Power-Turboelectric-Discharge.js new file mode 100644 index 00000000..768b4d0d --- /dev/null +++ b/doxygen/group__Methods-Power-Turboelectric-Discharge.js @@ -0,0 +1,4 @@ +var group__Methods_Power_Turboelectric_Discharge = +[ + [ "zero_fidelity", "group__Methods-Power-Turboelectric-Discharge.html#gaac01b1273836e84c1901fddc58467d77", null ] +]; \ No newline at end of file diff --git a/doxygen/group__Methods-Power-Turboelectric-Sizing.html b/doxygen/group__Methods-Power-Turboelectric-Sizing.html new file mode 100644 index 00000000..d13e831d --- /dev/null +++ b/doxygen/group__Methods-Power-Turboelectric-Sizing.html @@ -0,0 +1,180 @@ + + + + + + + +SUAVE: Sizing + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
+
+
+ +

Turboelectric methods contain the functions for analyses where a turboelectric powertrain provieds the required electric power. +More...

+ + + + +

+Functions

def SUAVE.Methods.Power.Turboelectric.Sizing.initialize_from_power.initialize_from_power (turboelectric, power, conditions)
 
+

Detailed Description

+

Turboelectric methods contain the functions for analyses where a turboelectric powertrain provieds the required electric power.

+

Function Documentation

+ +

◆ initialize_from_power()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Power.Turboelectric.Sizing.initialize_from_power.initialize_from_power ( turboelectric,
 power,
 conditions 
)
+
+
assigns the mass of a single turboelectric generator based on the power and specific power
+Assumptions:
+Power output is derated relative to the air pressure. 100% power is considered a mean sea level.
+
+Inputs:
+power                 [J]
+turboelectric.
+  specific_power      [W/kg]
+conditions.
+  freestream_pressure [Pa]
+
+
+Outputs:
+turboelectric.
+  mass_properties.
+    mass         [kg]
+
+
+
+
+
+ + + + diff --git a/doxygen/group__Methods-Power-Turboelectric-Sizing.js b/doxygen/group__Methods-Power-Turboelectric-Sizing.js new file mode 100644 index 00000000..50423f72 --- /dev/null +++ b/doxygen/group__Methods-Power-Turboelectric-Sizing.js @@ -0,0 +1,4 @@ +var group__Methods_Power_Turboelectric_Sizing = +[ + [ "initialize_from_power", "group__Methods-Power-Turboelectric-Sizing.html#gab8a1cf11bf63b2f96a840c839e15b5dc", null ] +]; \ No newline at end of file diff --git a/doxygen/group__Methods-Power-Turboelectric.html b/doxygen/group__Methods-Power-Turboelectric.html new file mode 100644 index 00000000..fdda74da --- /dev/null +++ b/doxygen/group__Methods-Power-Turboelectric.html @@ -0,0 +1,134 @@ + + + + + + + +SUAVE: Turboelectric + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
Turboelectric
+
+
+ +

Turboelectric methods contain the functions for investigating vehicle electric power supplied by a turboelectric powertrain. +More...

+ + + + + + + + +

+Modules

 Discharge
 Functions to evaluate the use of a turboelectric powertrain to provide electric power.
 
 Sizing
 Turboelectric methods contain the functions for analyses where a turboelectric powertrain provieds the required electric power.
 
+

Detailed Description

+

Turboelectric methods contain the functions for investigating vehicle electric power supplied by a turboelectric powertrain.

+

Created by modifying existing Fuel_Cell methods.

+
+
+ + + + diff --git a/doxygen/group__Methods-Power-Turboelectric.js b/doxygen/group__Methods-Power-Turboelectric.js new file mode 100644 index 00000000..77543909 --- /dev/null +++ b/doxygen/group__Methods-Power-Turboelectric.js @@ -0,0 +1,5 @@ +var group__Methods_Power_Turboelectric = +[ + [ "Discharge", "group__Methods-Power-Turboelectric-Discharge.html", "group__Methods-Power-Turboelectric-Discharge" ], + [ "Sizing", "group__Methods-Power-Turboelectric-Sizing.html", "group__Methods-Power-Turboelectric-Sizing" ] +]; \ No newline at end of file diff --git a/doxygen/group__Methods-Power.html b/doxygen/group__Methods-Power.html index ad9e9a90..32681e36 100644 --- a/doxygen/group__Methods-Power.html +++ b/doxygen/group__Methods-Power.html @@ -1,9 +1,9 @@ - + - + SUAVE: Power @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@
- +

@@ -73,7 +78,9 @@
@@ -109,6 +116,9 @@  Fuel_Cell  Fuel_Cell methods contain the functions for the fuel cell analyses.
  + Turboelectric + Turboelectric methods contain the functions for investigating vehicle electric power supplied by a turboelectric powertrain.

Detailed Description

Power methods contain the functions for electric systems such as batteries and fuel cells.

@@ -119,7 +129,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/group__Methods-Power.js b/doxygen/group__Methods-Power.js index 54443297..21c65c94 100644 --- a/doxygen/group__Methods-Power.js +++ b/doxygen/group__Methods-Power.js @@ -1,5 +1,6 @@ var group__Methods_Power = [ [ "Battery", "group__Methods-Power-Battery.html", "group__Methods-Power-Battery" ], - [ "Fuel_Cell", "group__Methods-Power-Fuel__Cell.html", "group__Methods-Power-Fuel__Cell" ] + [ "Fuel_Cell", "group__Methods-Power-Fuel__Cell.html", "group__Methods-Power-Fuel__Cell" ], + [ "Turboelectric", "group__Methods-Power-Turboelectric.html", "group__Methods-Power-Turboelectric" ] ]; \ No newline at end of file diff --git a/doxygen/group__Methods-Propulsion-Rotor__Wake-Fidelity__One.html b/doxygen/group__Methods-Propulsion-Rotor__Wake-Fidelity__One.html new file mode 100644 index 00000000..5b431710 --- /dev/null +++ b/doxygen/group__Methods-Propulsion-Rotor__Wake-Fidelity__One.html @@ -0,0 +1,579 @@ + + + + + + + +SUAVE: Fidelity_One + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
Fidelity_One
+
+
+ +

Rotor wake methods that are directly specified by analyses. +More...

+ + + + + + + + + + + + + + + + +

+Functions

def SUAVE.Methods.Propulsion.Rotor_Wake.Fidelity_One.compute_fidelity_one_inflow_velocities.compute_fidelity_one_inflow_velocities (wake, prop, WD)
 
def SUAVE.Methods.Propulsion.Rotor_Wake.Fidelity_One.compute_wake_induced_velocity.compute_wake_induced_velocity (WD, VD, cpts, azi_start_idx=0, sigma=0.11, suppress_root=False)
 
def SUAVE.Methods.Propulsion.Rotor_Wake.Fidelity_One.compute_wake_induced_velocity.vortex (X, Y, Z, X1, Y1, Z1, X2, Y2, Z2, sigma, GAMMA=1, bv=False, WD=None, use_regularization_kernal=True)
 
def SUAVE.Methods.Propulsion.Rotor_Wake.Fidelity_One.compute_wake_induced_velocity.regularization_kernel (COEF_in, sigma)
 
def SUAVE.Methods.Propulsion.Rotor_Wake.Fidelity_One.fidelity_one_wake_convergence.fidelity_one_wake_convergence (wake, rotor, wake_inputs)
 
def SUAVE.Methods.Propulsion.Rotor_Wake.Fidelity_One.generate_fidelity_one_wake_shape.generate_fidelity_one_wake_shape (wake, rotor)
 
def SUAVE.Methods.Propulsion.Rotor_Wake.Fidelity_One.generate_fidelity_one_wake_shape.initialize_distributions (Nr, Na, B, n_wts, m, VD)
 
+

Detailed Description

+

Rotor wake methods that are directly specified by analyses.

+

Function Documentation

+ +

◆ compute_fidelity_one_inflow_velocities()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Propulsion.Rotor_Wake.Fidelity_One.compute_fidelity_one_inflow_velocities.compute_fidelity_one_inflow_velocities ( wake,
 prop,
 WD 
)
+
+
Assumptions:
+    None
+
+Source:
+    N/A
+Inputs:
+    wake - rotor wake
+    prop - rotor instance
+    WD   - wake vortex distribution
+Outputs:
+    Va   - axial velocity, shape (ctrl_pts, Nr, Na); axis 2 in direction of rotation       [m/s]
+    Vt   - tangential velocity, shape (ctrl_pts, Nr, Na); axis 2 in direction of rotation    [m/s]
+
+
+
+ +

◆ compute_wake_induced_velocity()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Propulsion.Rotor_Wake.Fidelity_One.compute_wake_induced_velocity.compute_wake_induced_velocity ( WD,
 VD,
 cpts,
 azi_start_idx = 0,
 sigma = 0.11,
 suppress_root = False 
)
+
+
This computes the velocity induced by the Fidelity One semi-prescribed vortex wake (PVW)
+on lifting surface control points
+
+Assumptions:  
+
+Source:   
+
+Inputs: 
+WD     - helical wake distribution points               [Unitless] 
+VD     - vortex distribution points on lifting surfaces [Unitless] 
+cpts   - control points in segment                      [Unitless] 
+
+Properties Used:
+N/A
+
+
+
+ +

◆ fidelity_one_wake_convergence()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Propulsion.Rotor_Wake.Fidelity_One.fidelity_one_wake_convergence.fidelity_one_wake_convergence ( wake,
 rotor,
 wake_inputs 
)
+
+
This converges on the wake shape for the fidelity-one rotor wake.
+
+Assumptions:
+None
+
+Source:
+N/A
+
+Inputs:
+wake        - rotor wake
+rotor       - rotor
+wake_inputs - inputs passed from the BET rotor spin function
+
+Outputs:
+None
+
+Properties Used:
+None
+
+
+
+ +

◆ generate_fidelity_one_wake_shape()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Propulsion.Rotor_Wake.Fidelity_One.generate_fidelity_one_wake_shape.generate_fidelity_one_wake_shape ( wake,
 rotor 
)
+
+
This generates the propeller wake control points and vortex distribution that make up the prescribed vortex wake. 
+All (x,y,z) coordinates are in the vehicle frame of reference (X points nose to tail).
+
+Assumptions:
+   None
+
+Source: 
+   None
+
+Inputs:
+   rotor  -  A SUAVE rotor component for which the wake is generated
+
+
+ +

◆ initialize_distributions()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Propulsion.Rotor_Wake.Fidelity_One.generate_fidelity_one_wake_shape.initialize_distributions ( Nr,
 Na,
 B,
 n_wts,
 m,
 VD 
)
+
+
Initializes the matrices for the wake vortex distributions.
+
+Assumptions:
+    None
+
+Source:
+    N/A
+    
+Inputs:
+   Nr    - number of radial blade elemnts
+   Na    - number of azimuthal start positions
+   B     - number of rotor blades
+   n_wts - total number of wake time steps in wake simulation
+   m     - number of control points to evaluate
+   VD    - vehicle vortex distribution
+   
+Outputs:
+   VD  - Vortex distribution
+   WD  - Wake vortex distribution
+
+Properties:
+   N/A
+
+
+ +

◆ regularization_kernel()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Propulsion.Rotor_Wake.Fidelity_One.compute_wake_induced_velocity.regularization_kernel ( COEF_in,
 sigma 
)
+
+
Regularization kernel used to prevent singularities
+
+Assumptions
+Spreads the vortex core over the radius sigma
+
+Source
+   Winckelmans, "Topics in Vortex Methods for the Computation of Three-and Two-dimensional 
+   Incompressible Unsteady Flows", 1989.
+
+Inputs:
+   COEF    Biot-Savart Kernel
+   sigma   regularization radius
+
+Outputs:
+   KAPPA   Regularization Kernel
+   
+Properties Used:
+N/A
+
+
+ +

◆ vortex()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Propulsion.Rotor_Wake.Fidelity_One.compute_wake_induced_velocity.vortex ( X,
 Y,
 Z,
 X1,
 Y1,
 Z1,
 X2,
 Y2,
 Z2,
 sigma,
 GAMMA = 1,
 bv = False,
 WD = None,
 use_regularization_kernal = True 
)
+
+
This computes the velocity induced on a control point by a segment
+of a horseshoe vortex that points from point 1 to point 2 for a filament with
+positive vortex strength.
+
+Assumptions:  
+None 
+
+Source: 
+Low-Speed Aerodynamics, Second Edition by Joseph katz, Allen Plotkin
+Pgs. 584(Literature), 579-586 (Fortran Code implementation)
+
+Inputs:
+GAMMA       - propeller/rotor circulation
+[X,Y,Z]     - location of control point  
+[X1,Y1,Z1]  - location of point 1 
+[X2,Y2,Z2]  - location of point 2
+Properties Used:
+N/A
+
+
+
+
+ + + + diff --git a/doxygen/group__Methods-Propulsion-Rotor__Wake-Fidelity__One.js b/doxygen/group__Methods-Propulsion-Rotor__Wake-Fidelity__One.js new file mode 100644 index 00000000..b0afce52 --- /dev/null +++ b/doxygen/group__Methods-Propulsion-Rotor__Wake-Fidelity__One.js @@ -0,0 +1,10 @@ +var group__Methods_Propulsion_Rotor__Wake_Fidelity__One = +[ + [ "compute_fidelity_one_inflow_velocities", "group__Methods-Propulsion-Rotor__Wake-Fidelity__One.html#ga40aaaebd67b1ed3a57fc6d183e316100", null ], + [ "compute_wake_induced_velocity", "group__Methods-Propulsion-Rotor__Wake-Fidelity__One.html#ga1727bccb0d701f2961dcc10852635b84", null ], + [ "fidelity_one_wake_convergence", "group__Methods-Propulsion-Rotor__Wake-Fidelity__One.html#gaa53ccc7f754b3660308e11f55fc0dc9a", null ], + [ "generate_fidelity_one_wake_shape", "group__Methods-Propulsion-Rotor__Wake-Fidelity__One.html#ga71ac0b21c3b6e9932edad059e72c988a", null ], + [ "initialize_distributions", "group__Methods-Propulsion-Rotor__Wake-Fidelity__One.html#ga026220649bdb6e01dd2a9fe868758817", null ], + [ "regularization_kernel", "group__Methods-Propulsion-Rotor__Wake-Fidelity__One.html#ga6d17985938d9aea65023967b7d5c7b1e", null ], + [ "vortex", "group__Methods-Propulsion-Rotor__Wake-Fidelity__One.html#ga17c3da1cdcb1727905ecd724a8b899bf", null ] +]; \ No newline at end of file diff --git a/doxygen/group__Methods-Propulsion-Rotor__Wake-Fidelity__Zero.html b/doxygen/group__Methods-Propulsion-Rotor__Wake-Fidelity__Zero.html new file mode 100644 index 00000000..9bf1bb65 --- /dev/null +++ b/doxygen/group__Methods-Propulsion-Rotor__Wake-Fidelity__Zero.html @@ -0,0 +1,127 @@ + + + + + + + +SUAVE: Fidelity_Zero + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
Fidelity_Zero
+
+
+ +

Rotor wake methods that are directly specified by analyses. +More...

+

Rotor wake methods that are directly specified by analyses.

+

fidelity_zero_wake_convergence.py

+

compute_wake_contraction_matrix.py

+

compute_fidelity_zero_induced_velocity.py

+

Created: Jun 2021, R. Erhard

+

Created: Sep 2020, M. Clarke Jul 2021, E. Botero

Sep 2021, R. Erhard

+

Imports

+

Created: Feb 2022, R. Erhard Modified:

+
+
+ + + + diff --git a/doxygen/group__Methods-Propulsion-Rotor__Wake.html b/doxygen/group__Methods-Propulsion-Rotor__Wake.html new file mode 100644 index 00000000..b11d6ae0 --- /dev/null +++ b/doxygen/group__Methods-Propulsion-Rotor__Wake.html @@ -0,0 +1,133 @@ + + + + + + + +SUAVE: Rotor_Wake + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
Rotor_Wake
+
+
+ +

Rotor_Wake provides the functions needed to perform analyses. +More...

+ + + + + + + + +

+Modules

 Fidelity_One
 Rotor wake methods that are directly specified by analyses.
 
 Fidelity_Zero
 Rotor wake methods that are directly specified by analyses.
 
+

Detailed Description

+

Rotor_Wake provides the functions needed to perform analyses.

+
+
+ + + + diff --git a/doxygen/group__Methods-Propulsion-Rotor__Wake.js b/doxygen/group__Methods-Propulsion-Rotor__Wake.js new file mode 100644 index 00000000..f5e9d186 --- /dev/null +++ b/doxygen/group__Methods-Propulsion-Rotor__Wake.js @@ -0,0 +1,5 @@ +var group__Methods_Propulsion_Rotor__Wake = +[ + [ "Fidelity_One", "group__Methods-Propulsion-Rotor__Wake-Fidelity__One.html", "group__Methods-Propulsion-Rotor__Wake-Fidelity__One" ], + [ "Fidelity_Zero", "group__Methods-Propulsion-Rotor__Wake-Fidelity__Zero.html", null ] +]; \ No newline at end of file diff --git a/doxygen/group__Methods-Propulsion.html b/doxygen/group__Methods-Propulsion.html index d375259b..5a1cd1fc 100644 --- a/doxygen/group__Methods-Propulsion.html +++ b/doxygen/group__Methods-Propulsion.html @@ -1,9 +1,9 @@ - + - + SUAVE: Propulsion @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@
- +
@@ -73,7 +78,9 @@
@@ -92,6 +99,7 @@
Propulsion
@@ -101,17 +109,31 @@

Description. More...

+ + + + +

+Modules

 Rotor_Wake
 Rotor_Wake provides the functions needed to perform analyses.
 
- - + + + + + + + + + + @@ -126,10 +148,14 @@ - - - - + + + + + + + +

Functions

def SUAVE.Methods.Propulsion.ducted_fan_sizing.ducted_fan_sizing (ducted_fan, mach_number=None, altitude=None, delta_isa=0, conditions=None)
 
def SUAVE.Methods.Propulsion.electric_motor_sizing.size_from_kv (motor, kv)
 
def SUAVE.Methods.Propulsion.electric_motor_sizing.size_from_kv (motor)
 
def SUAVE.Methods.Propulsion.electric_motor_sizing.size_from_mass (motor)
 
def SUAVE.Methods.Propulsion.electric_motor_sizing.size_optimal_motor (motor, prop)
 
def SUAVE.Methods.Propulsion.electric_motor_sizing.optimize_kv (io, v, omeg, etam, Q, kv_lower_bound=0.01, Res_lower_bound=0.001, kv_upper_bound=100, Res_upper_bound=10)
 
def SUAVE.Methods.Propulsion.fm_id.fm_id (M, gamma)
 fm_id.py More...
 
def SUAVE.Methods.Propulsion.fm_solver.fm_solver (area_ratio, M0, gamma)
 
def SUAVE.Methods.Propulsion.liquid_rocket_sizing.liquid_rocket_sizing (liquid_rocket, altitude=None, delta_isa=0, conditions=None)
 
def SUAVE.Methods.Propulsion.nozzle_calculations.exit_Mach_shock (area_ratio, gamma, Pt_out, P0)
 
def SUAVE.Methods.Propulsion.nozzle_calculations.mach_area (area_ratio, gamma, subsonic)
 
def SUAVE.Methods.Propulsion.rayleigh.rayleigh (gamma, M0, TtR)
 
def SUAVE.Methods.Propulsion.rayleighflow.rayleighflow (gamma, M0, TtR)
 
def SUAVE.Methods.Propulsion.turbofan_nox_emission_index.turbofan_nox_emission_index (turbofan, state)
 
def SUAVE.Methods.Propulsion.scramjet_sizing.scramjet_sizing (scramjet, mach_number=None, altitude=None, delta_isa=0, conditions=None)
 
def SUAVE.Methods.Propulsion.serial_HTS_turboelectric_sizing.serial_HTS_turboelectric_sizing (Turboelectric_HTS_Ducted_Fan, mach_number=None, altitude=None, delta_isa=0, conditions=None, cryo_cold_temp=50.0, cryo_amb_temp=300.0)
 
def SUAVE.Methods.Propulsion.shock_train.shock_train (M0, gamma, nbr_shocks, theta)
 
def SUAVE.Methods.Propulsion.turbofan_emission_index.turbofan_emission_index (turbofan, state)
 

Detailed Description

Description.

@@ -335,6 +361,47 @@

+

◆ liquid_rocket_sizing()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Propulsion.liquid_rocket_sizing.liquid_rocket_sizing ( liquid_rocket,
 altitude = None,
 delta_isa = 0,
 conditions = None 
)
+
+
This function sizes a liquid_rocket for the input design conditions.
+
+
+

◆ mach_area()

@@ -424,6 +491,88 @@

+

◆ optimize_kv()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Propulsion.electric_motor_sizing.optimize_kv ( io,
 v,
 omeg,
 etam,
 Q,
 kv_lower_bound = 0.01,
 Res_lower_bound = 0.001,
 kv_upper_bound = 100,
 Res_upper_bound = 10 
)
+
+
Optimizer for compute_optimal_motor_parameters function  
+
+Source:
+N/A
+
+Inputs:
+motor    (to be modified)
+
+Outputs:
+motor.
+  speed_constant     [untiless]
+  no_load_current    [amps]
+
+
+

◆ pressure_ratio_isentropic()

@@ -558,8 +707,7 @@

-
This function sizes a ramjet for the input design conditions.
-
+
This function sizes a ramjet for the input design conditions.

@@ -608,29 +756,41 @@

-

◆ rayleighflow()

+ +

◆ scramjet_sizing()

- + - + - + - + + + + + + + + + + + + + @@ -639,38 +799,124 @@

-
Function that takes in a input (output) Mach number and a stagnation
-temperature ratio and yields an output (input) Mach number, according
-to the Rayleigh line flow equation. The function also outputs the stagnation
-pressure ratio
+
This function sizes a scramjet for the input design conditions.
+
+ + +
+

◆ serial_HTS_turboelectric_sizing()

-Inputs: -M0 [dimensionless] -gamma [dimensionless] -Ttr [dimensionless] +
+
+

def SUAVE.Methods.Propulsion.rayleighflow.rayleighflow def SUAVE.Methods.Propulsion.scramjet_sizing.scramjet_sizing (  gamma, scramjet,
 M0, mach_number = None,
 TtR altitude = None,
 delta_isa = 0,
 conditions = None 
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Propulsion.serial_HTS_turboelectric_sizing.serial_HTS_turboelectric_sizing ( Turboelectric_HTS_Ducted_Fan,
 mach_number = None,
 altitude = None,
 delta_isa = 0,
 conditions = None,
 cryo_cold_temp = 50.0,
 cryo_amb_temp = 300.0 
)
+
+
create and evaluate a serial hybrid network that follows the power flow:
+Turboelectric Generators -> Motor Drivers -> Electric Poropulsion Motors
+where the electric motors have cryogenically cooled HTS rotors that follow the power flow:
+Turboelectric Generators -> Current Supplies -> HTS Rotor Coils
+and
+Turboelectric Generators -> Cryocooler <- HTS Rotor Heat Load
+There is also the capability for the HTS components to be cryogenically cooled using liquid or gaseous cryogen, howver this is not sized other than applying a factor to the cryocooler required power.
 
-Outputs:
-M1      [dimensionless]
-Ptr     [dimensionless]
+ Assumptions: + One powertrain model represents all engines in the model. + There are no transmission losses between components + the shaft torque and power required from the fan is the same as what would be required from the fan of a turbofan engine. + + Source: + N/A + + Inputs: + Turboelectric_HTS_Ducted_Fan Serial HTYS hybrid ducted fan network object (to be modified) + mach_number + altitude [meters] + delta_isa temperature difference [K] + conditions ordered dict object + + Outputs: + N/A + + Properties Used: + N/A

- -

◆ size_from_kv()

+ +

◆ shock_train()

- + - + + + + + + + - + + + + + + + @@ -679,6 +925,43 @@

+
Function that takes in Mach,gamma, number of expected oblique , and 
+wedge angle of inlet and calculates the flow properties after under going said
+oblique shicks.  It verifies if all oblique shocks actually take place, depending
+on inlet condition.
+
+Assumptions:
+No shock interactions
+
+Inputs:
+M           [-]
+gamma       [-]
+nbr_shocks  [-]
+theta       [rad]
+
+Outputs:
+Tr          [-]
+Ptr         [-]
+
+Source:
+https://web.stanford.edu/~cantwell/AA210A_Course_Material/AA210A_Course_Notes/
+ + +
+

◆ size_from_kv()

+ +
+
+

def SUAVE.Methods.Propulsion.electric_motor_sizing.size_from_kv def SUAVE.Methods.Propulsion.shock_train.shock_train (  motor, M0,
 gamma,
 kv nbr_shocks,
 theta 
+ + + + + + + +
def SUAVE.Methods.Propulsion.electric_motor_sizing.size_from_kv ( motor)
+
Determines a motors mass based on the speed constant KV
 
 Source:
@@ -686,7 +969,7 @@ 

-

◆ turbofan_nox_emission_index()

+ +

◆ size_from_mass()

+ +
+
+ + + + + + + + +
def SUAVE.Methods.Propulsion.electric_motor_sizing.size_from_mass ( motor)
+
+
Sizes motor from mass
+
+Source:
+Gur, O., Rosen, A, AIAA 2008-5916.
+
+Inputs:
+motor.    (to be modified)
+  mass               [kg]
+
+Outputs:
+motor.
+  resistance         [ohms]
+  no_load_current    [amps] 
+
+
+
+ +

◆ size_optimal_motor()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Propulsion.electric_motor_sizing.size_optimal_motor ( motor,
 prop 
)
+
+
Optimizes the motor to obtain the best combination of speed constant and resistance values
+by essentially sizing the motor for a design RPM value. Note that this design RPM 
+value can be compute from design tip mach  
+
+Assumptions:
+motor design performance occurs at 90% nominal voltage to account for off design conditions 
+
+Source:
+N/A
+
+Inputs:
+prop.
+  design_torque          [Nm]
+  angular_velocity       [rad/s]
+  origin                 [m]
+  
+motor.     
+  no_load_current        [amps]
+  mass_properties.mass   [kg]
+  
+Outputs:
+motor.
+  speed_constant         [untiless]
+  design_torque          [Nm] 
+  motor.resistance       [Ohms]
+  motor.angular_velocity [rad/s]
+  motor.origin           [m]
+
+
+
+ +

◆ turbofan_emission_index()

- + @@ -720,7 +1089,7 @@

-
Outputs a turbofan's nox_emission_index takens from a regression calculated
+
Outputs a turbofan's emission_index takens from a regression calculated
 from NASA's Engine Performance Program (NEPP)
 
 Inputs:
@@ -733,9 +1102,19 @@ 

Generated by - doxygen 1.8.14 + doxygen 1.8.15 diff --git a/doxygen/group__Methods-Propulsion.js b/doxygen/group__Methods-Propulsion.js index 53d27621..3303c9a0 100644 --- a/doxygen/group__Methods-Propulsion.js +++ b/doxygen/group__Methods-Propulsion.js @@ -1,16 +1,23 @@ var group__Methods_Propulsion = [ + [ "Rotor_Wake", "group__Methods-Propulsion-Rotor__Wake.html", "group__Methods-Propulsion-Rotor__Wake" ], [ "ducted_fan_sizing", "group__Methods-Propulsion.html#ga3e6153003ae73397bf8d06367e10e9ba", null ], [ "exit_Mach_shock", "group__Methods-Propulsion.html#gaacf435ba19015caf25a08dae08baa6a3", null ], [ "fm_id", "group__Methods-Propulsion.html#gae720e196160d2c3fdc45c57ff3e2f4bb", null ], [ "fm_solver", "group__Methods-Propulsion.html#ga47f175130d1d19883d8df534fd93fcdb", null ], + [ "liquid_rocket_sizing", "group__Methods-Propulsion.html#gafeca1c92d1db8a7f3bb1825f3e8af6f5", null ], [ "mach_area", "group__Methods-Propulsion.html#ga3144faf7ddbd2565a65cb6aebe0028b9", null ], [ "normal_shock", "group__Methods-Propulsion.html#gab5feaa0bf6416dfd4852ca8833236690", null ], + [ "optimize_kv", "group__Methods-Propulsion.html#gab4466f11794955e948b98afa5d36ef2e", null ], [ "pressure_ratio_isentropic", "group__Methods-Propulsion.html#ga448bd8878bb3fb399e1ef118fe928543", null ], [ "pressure_ratio_shock_in_nozzle", "group__Methods-Propulsion.html#ga316b77e7dfea02ba5dfc96b3d76f54d7", null ], [ "ramjet_sizing", "group__Methods-Propulsion.html#ga0b31c5b143439d1296cfdb8f7dc5d4a3", null ], [ "rayleigh", "group__Methods-Propulsion.html#ga7343e43e60f66f0486c780fccae07fd0", null ], - [ "rayleighflow", "group__Methods-Propulsion.html#ga78c2cdcbd5eb6d7cd9adbc5f6f8cc4a3", null ], - [ "size_from_kv", "group__Methods-Propulsion.html#ga7448a7c9da5a37c6912b33fd90c98306", null ], - [ "turbofan_nox_emission_index", "group__Methods-Propulsion.html#gabc52d81a51c667a4bad13558e252ba07", null ] + [ "scramjet_sizing", "group__Methods-Propulsion.html#ga1f7790df2723b1121dbdbe0fd795adde", null ], + [ "serial_HTS_turboelectric_sizing", "group__Methods-Propulsion.html#ga1d8c38e3c7b20af688906d6184625f32", null ], + [ "shock_train", "group__Methods-Propulsion.html#gaa391dbea29bed7099ae2de99774ac536", null ], + [ "size_from_kv", "group__Methods-Propulsion.html#gaaceccf2f0fd7ef2c51ac7752700230dc", null ], + [ "size_from_mass", "group__Methods-Propulsion.html#gabfa7508a797c8be14c4ea5bab83b05c7", null ], + [ "size_optimal_motor", "group__Methods-Propulsion.html#ga2a7a8cf66349899da013fd287f10a6f7", null ], + [ "turbofan_emission_index", "group__Methods-Propulsion.html#ga073857d84ade0f28134bf8340dfc3330", null ] ]; \ No newline at end of file diff --git a/doxygen/group__Methods-Utilities-Chebyshev.html b/doxygen/group__Methods-Utilities-Chebyshev.html index 578da48f..b81119b0 100644 --- a/doxygen/group__Methods-Utilities-Chebyshev.html +++ b/doxygen/group__Methods-Utilities-Chebyshev.html @@ -1,9 +1,9 @@ - + - + SUAVE: Chebyshev @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@
def SUAVE.Methods.Propulsion.turbofan_nox_emission_index.turbofan_nox_emission_index def SUAVE.Methods.Propulsion.turbofan_emission_index.turbofan_emission_index (   turbofan,
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@

@@ -103,16 +110,16 @@ - - - - + + + +

Functions

def SUAVE.Methods.Utilities.Chebyshev.chebyshev_data.chebyshev_data (N=16, integration=True, options)
 
def SUAVE.Methods.Utilities.Chebyshev.linear_data.linear_data (N=16, integration=True, options)
 
def SUAVE.Methods.Utilities.Chebyshev.chebyshev_data.chebyshev_data (N=16, integration=True, **options)
 
def SUAVE.Methods.Utilities.Chebyshev.linear_data.linear_data (N=16, integration=True, **options)
 

Detailed Description

These functions provide methods for discrete derivative and integral calculations.

Function Documentation

- -

◆ chebyshev_data()

+ +

◆ chebyshev_data()

@@ -132,7 +139,7 @@

-   + **  options  @@ -173,8 +180,8 @@

-

◆ linear_data()

+ +

◆ linear_data()

diff --git a/doxygen/group__Methods-Utilities-Chebyshev.js b/doxygen/group__Methods-Utilities-Chebyshev.js index 733e8249..aa1af15c 100644 --- a/doxygen/group__Methods-Utilities-Chebyshev.js +++ b/doxygen/group__Methods-Utilities-Chebyshev.js @@ -1,5 +1,5 @@ var group__Methods_Utilities_Chebyshev = [ - [ "chebyshev_data", "group__Methods-Utilities-Chebyshev.html#ga52d35a64916a9bce3b636e296f4ef53b", null ], - [ "linear_data", "group__Methods-Utilities-Chebyshev.html#ga63215eedc2e365dd6273325e8a142b48", null ] + [ "chebyshev_data", "group__Methods-Utilities-Chebyshev.html#ga981c893b8ddd22558db27cb6a73ff757", null ], + [ "linear_data", "group__Methods-Utilities-Chebyshev.html#gac83ee04f724538788375ce2d449302ea", null ] ]; \ No newline at end of file diff --git a/doxygen/group__Methods-Utilities.html b/doxygen/group__Methods-Utilities.html index 74907b6d..fbd6a7fb 100644 --- a/doxygen/group__Methods-Utilities.html +++ b/doxygen/group__Methods-Utilities.html @@ -1,9 +1,9 @@ - + - + SUAVE: Utilities @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@
- +

@@ -73,7 +78,9 @@
@@ -93,6 +100,7 @@
Utilities
@@ -108,6 +116,11 @@  These functions provide methods for discrete derivative and integral calculations.
  + + + +

+Classes

class  SUAVE.Methods.Utilities.Cubic_Spline_Blender.Cubic_Spline_Blender
 
@@ -236,7 +249,7 @@

Generated by - doxygen 1.8.14 + doxygen 1.8.15 diff --git a/doxygen/group__Methods-Utilities.js b/doxygen/group__Methods-Utilities.js index d1da47b9..0f84d391 100644 --- a/doxygen/group__Methods-Utilities.js +++ b/doxygen/group__Methods-Utilities.js @@ -1,6 +1,13 @@ var group__Methods_Utilities = [ [ "Chebyshev", "group__Methods-Utilities-Chebyshev.html", "group__Methods-Utilities-Chebyshev" ], + [ "Cubic_Spline_Blender", "classSUAVE_1_1Methods_1_1Utilities_1_1Cubic__Spline__Blender_1_1Cubic__Spline__Blender.html", [ + [ "__init__", "classSUAVE_1_1Methods_1_1Utilities_1_1Cubic__Spline__Blender_1_1Cubic__Spline__Blender.html#ac62246c89508c2a196d9a12c42241f4a", null ], + [ "compute", "classSUAVE_1_1Methods_1_1Utilities_1_1Cubic__Spline__Blender_1_1Cubic__Spline__Blender.html#aa80ca48b142c80fe3d791547f6dce500", null ], + [ "eta_transform", "classSUAVE_1_1Methods_1_1Utilities_1_1Cubic__Spline__Blender_1_1Cubic__Spline__Blender.html#a97b32ecf60f95d6bf842e8b5edfe39fe", null ], + [ "x_end", "classSUAVE_1_1Methods_1_1Utilities_1_1Cubic__Spline__Blender_1_1Cubic__Spline__Blender.html#a6f68ca2fc9f111d4d650b0da00a659ae", null ], + [ "x_start", "classSUAVE_1_1Methods_1_1Utilities_1_1Cubic__Spline__Blender_1_1Cubic__Spline__Blender.html#a4fedebf819716f0167c524f75689caf4", null ] + ] ], [ "latin_hypercube_sampling", "group__Methods-Utilities.html#gad7f4326f99edc2e3d142e7d2a0fffcf0", null ], [ "soft_max", "group__Methods-Utilities.html#ga839620ce7852f1839a0d851f4a21475d", null ] ]; \ No newline at end of file diff --git a/doxygen/group__Methods-Weights-Buildups-Common.html b/doxygen/group__Methods-Weights-Buildups-Common.html new file mode 100644 index 00000000..df4cd43d --- /dev/null +++ b/doxygen/group__Methods-Weights-Buildups-Common.html @@ -0,0 +1,569 @@ + + + + + + + +SUAVE: Common + + + + + + + + + + + + + + + +
+
+

Functions

def SUAVE.Methods.Utilities.latin_hypercube_sampling.latin_hypercube_sampling (num_dimensions, num_samples, bounds=None, criterion='random')
+ + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
+
+
+ +

The Common buildup methods are those which are shared between vehicle types utilizing buildup weight methods. +More...

+ + + + + + + + + + +

+Functions

def SUAVE.Methods.Weights.Buildups.Common.fuselage.fuselage (config, maximum_g_load=3.8, landing_impact_factor=3.5, safety_factor=1.5)
 
def SUAVE.Methods.Weights.Buildups.Common.prop.prop (prop, maximum_lifting_thrust, chord_to_radius_ratio=0.1, thickness_to_chord=0.12, root_to_radius_ratio=0.1, moment_to_lift_ratio=0.02, spanwise_analysis_points=5, safety_factor=1.5, margin_factor=1.2, forward_web_locations=[0.25, 0.35], shear_center=0.25, speed_of_sound=340.294, tip_max_mach_number=0.65)
 
def SUAVE.Methods.Weights.Buildups.Common.wing.wing (wing, config, max_thrust, num_analysis_points=10, safety_factor=1.5, max_g_load=3.8, moment_to_lift_ratio=0.02, lift_to_drag_ratio=7, forward_web_locations=[0.25, 0.35], rear_web_locations=[0.65, 0.75], shear_center_location=0.25, margin_factor=1.2)
 
def SUAVE.Methods.Weights.Buildups.Common.wiring.wiring (wing, config, cablePower)
 
+

Detailed Description

+

The Common buildup methods are those which are shared between vehicle types utilizing buildup weight methods.

+

Function Documentation

+ +

◆ fuselage()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Weights.Buildups.Common.fuselage.fuselage ( config,
 maximum_g_load = 3.8,
 landing_impact_factor = 3.5,
 safety_factor = 1.5 
)
+
+
Calculates the structural mass of a fuselage for an eVTOL vehicle,
+    assuming a structural keel taking bending an torsional loads.
+    
+    Assumptions:
+    Assumes an elliptical fuselage. Intended for use with the following
+    SUAVE vehicle types, but may be used elsewhere:
+
+        Electric Multicopter
+        Electric Vectored_Thrust
+        Electric Stopped Rotor
+
+    Originally written as part of an AA 290 project intended for trade study
+    of the above vehicle types.
+
+    If vehicle model does not have material properties assigned, appropriate
+    assumptions are made based on SUAVE's Solids Attributes library.
+    
+    Sources:
+    Project Vahana Conceptual Trade Study
+
+    Inputs:
+
+        config                      SUAVE Vehicle Configuration
+        max_g_load                  Max Accelerative Load During Flight [Unitless]
+        landing_impact_factor       Maximum Load Multiplier on Landing  [Unitless]
+
+    Outputs:
+
+        weight:                 Estimated Fuselage Mass             [kg]
+    
+    Properties Used:
+    Material Properties of Imported SUAVE Solids
+
+
+
+ +

◆ prop()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Weights.Buildups.Common.prop.prop ( prop,
 maximum_lifting_thrust,
 chord_to_radius_ratio = 0.1,
 thickness_to_chord = 0.12,
 root_to_radius_ratio = 0.1,
 moment_to_lift_ratio = 0.02,
 spanwise_analysis_points = 5,
 safety_factor = 1.5,
 margin_factor = 1.2,
 forward_web_locations = [0.25, 0.35],
 shear_center = 0.25,
 speed_of_sound = 340.294,
 tip_max_mach_number = 0.65 
)
+
+
weight = SUAVE.Methods.Weights.Buildups.Common.prop(
+        prop,
+        maximum_thrust,
+        chord_to_radius_ratio = 0.1,
+        thickness_to_chord = 0.12,
+        root_to_radius_ratio = 0.1,
+        moment_to_lift_ratio = 0.02,
+        spanwise_analysis_points = 5,
+        safety_factor = 1.5,
+        margin_factor = 1.2,
+        forward_web_locationss = [0.25, 0.35],
+        shear_center = 0.25,
+        speed_of_sound = 340.294,
+        tip_max_mach_number = 0.65)
+
+    Assumptions:
+    Calculates propeller blade pass for an eVTOL vehicle based on assumption
+    of a NACA airfoil prop, an assumed cm/cl, tip Mach limit, and structural
+    geometry.
+
+    Intended for use with the following SUAVE vehicle types, but may be used
+    elsewhere:
+
+        Electric Multicopter
+        Electric Vectored_Thrust
+        Electric Stopped Rotor
+
+    Originally written as part of an AA 290 project inteded for trade study
+    of the above vehicle types.
+
+    If vehicle model does not have material properties assigned, appropriate
+    assumptions are made based on SUAVE's Solids Attributes library.
+    
+    Sources:
+    Project Vahana Conceptual Trade Study
+
+    Inputs:
+
+        prop                        SUAVE Propeller Data Structure
+        maximum_thrust              Maximum Design Thrust               [N]
+        chord_to_radius_ratio       Chord to Blade Radius               [Unitless]
+        thickness_to_chord          Blade Thickness to Chord            [Unitless]
+        root_to_radius_ratio        Root Structure to Blade Radius      [Unitless]
+        moment_to_lift_ratio        Coeff. of Moment to Coeff. of Lift  [Unitless]
+        spanwise_analysis_points    Analysis Points for Sizing          [Unitless]
+        safety_factor               Design Safety Factor                [Unitless]
+        margin_factor               Allowable Extra Mass Fraction       [Unitless]
+        forward_web_locationss      Location of Forward Spar Webbing    [m]
+        shear_center                Location of Shear Center            [m]
+        speed_of_sound              Local Speed of Sound                [m/s]
+        tip_max_mach_number         Allowable Tip Mach Number           [Unitless]
+
+    Outputs:
+
+        weight:                 Propeller Mass                      [kg]
+        
+    Properties Used:
+    Material properties of imported SUAVE Solids
+
+
+
+ +

◆ wing()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Weights.Buildups.Common.wing.wing ( wing,
 config,
 max_thrust,
 num_analysis_points = 10,
 safety_factor = 1.5,
 max_g_load = 3.8,
 moment_to_lift_ratio = 0.02,
 lift_to_drag_ratio = 7,
 forward_web_locations = [0.25, 0.35],
 rear_web_locations = [0.65, 0.75],
 shear_center_location = 0.25,
 margin_factor = 1.2 
)
+
+
weight = SUAVE.Methods.Weights.Buildups.Common.wing(
+        wing,
+        config,
+        maxThrust,
+        numAnalysisPoints,
+        safety_factor,
+        max_g_load,
+        moment_to_lift_ratio,
+        lift_to_drag_ratio,
+        forward_web_locations = [0.25, 0.35],
+        rear_web_locations = [0.65, 0.75],
+        shear_center = 0.25,
+        margin_factor = 1.2)
+
+    Calculates the structural mass of a wing for an eVTOL vehicle based on
+    assumption of NACA airfoil wing, an assumed L/D, cm/cl, and structural
+    geometry.
+
+    Intended for use with the following SUAVE vehicle types, but may be used
+    elsewhere:
+
+        Electric Multicopter
+        Electric Vectored_Thrust
+        Electric Stopped Rotor
+
+    Originally written as part of an AA 290 project intended for trade study
+    of the above vehicle types plus an electric multicopter.
+
+    If no materials are assigned to vehicle model, appropriate assumptions
+    are made based on SUAVE's Solids Attributes library.
+    
+    Sources:
+    Project Vahana Conceptual Trade Study
+
+    Inputs:
+
+        wing                          SUAVE Wing Data Structure           [None]
+             winglet_fraction         winglet fraction                    [Unitless]
+             motor_spanwise_locations spanwise fraction location of motor [Unitless]
+        config                        SUAVE Config Data Structure         [None]
+        maxThrust                     Maximum Thrust                      [N]
+        numAnalysisPoints             Analysis Points for Sizing          [Unitless]
+        safety_factor                 Design Safety Factor                [Unitless]
+        max_g_load                    Maximum Accelerative Load           [Unitless]
+        moment_to_lift_ratio          Coeff. of Moment to Coeff. of Lift  [Unitless]
+        lift_to_drag_ratio            Coeff. of Lift to Coeff. of Drag    [Unitless]
+        forward_web_locations         Location of Forward Spar Webbing    [m]
+        rear_web_locations            Location of Rear Spar Webbing       [m]
+        shear_center                  Location of Shear Center            [m]
+        margin_factor                 Allowable Extra Mass Fraction       [Unitless]
+
+    Outputs:
+
+        weight:                       Wing Mass                           [kg]
+
+
+
+ +

◆ wiring()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Weights.Buildups.Common.wiring.wiring ( wing,
 config,
 cablePower 
)
+
+
weight = SUAVE.Methods.Weights.Buildups.Common.wiring(
+        wing,
+        config, 
+        cablePower)
+    
+    Assumptions:
+    Calculates mass of wiring required for a wing, including DC power
+    cables and communication cables, assuming power cables run an average of
+    half the fuselage length and height in addition to reaching the motor
+    location on the wingspan, and that communication and sesor  wires run an
+    additional length based on the fuselage and wing dimensions.
+
+    Intended for use with the following SUAVE vehicle types, but may be used
+    elsewhere:
+
+        Electric Multicopter
+        Electric Vectored_Thrust
+        Electric Stopped Rotor
+
+    Originally written as part of an AA 290 project intended for trade study
+    of the above vehicle types.
+    
+    Sources:
+    Project Vahana Conceptual Trade Study
+
+    Inputs:
+
+        config                      SUAVE Config Data Structure
+        motor_spanwise_locations    Motor Semi-Span Fractions       [Unitless]
+        max_power_draw              Maximum DC Power Draw           [W]
+
+    Outputs:
+
+        weight:                     Wiring Mass                     [kg]
+
+
+
+
+ + + + diff --git a/doxygen/group__Methods-Weights-Buildups-Common.js b/doxygen/group__Methods-Weights-Buildups-Common.js new file mode 100644 index 00000000..e60464f6 --- /dev/null +++ b/doxygen/group__Methods-Weights-Buildups-Common.js @@ -0,0 +1,7 @@ +var group__Methods_Weights_Buildups_Common = +[ + [ "fuselage", "group__Methods-Weights-Buildups-Common.html#gaf8650ce6b96c5aa3f90dc9a482ea3f55", null ], + [ "prop", "group__Methods-Weights-Buildups-Common.html#ga7c70b99ea11ee3e742477541c527bea8", null ], + [ "wing", "group__Methods-Weights-Buildups-Common.html#ga023fd2faaeb307a459bb67cc4fb0cba9", null ], + [ "wiring", "group__Methods-Weights-Buildups-Common.html#ga77ea4e9dfcf5842b0a9febb0ef5eb281", null ] +]; \ No newline at end of file diff --git a/doxygen/group__Methods-Weights-Buildups-EVTOL.html b/doxygen/group__Methods-Weights-Buildups-EVTOL.html new file mode 100644 index 00000000..8fd10fc7 --- /dev/null +++ b/doxygen/group__Methods-Weights-Buildups-EVTOL.html @@ -0,0 +1,120 @@ + + + + + + + +SUAVE: EVTOL + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
+
+
+ +

The empty method that is called by the analysis. +More...

+

The empty method that is called by the analysis.

+
+
+ + + + diff --git a/doxygen/group__Methods-Weights-Buildups.html b/doxygen/group__Methods-Weights-Buildups.html new file mode 100644 index 00000000..6cd2cc58 --- /dev/null +++ b/doxygen/group__Methods-Weights-Buildups.html @@ -0,0 +1,133 @@ + + + + + + + +SUAVE: Buildups + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
Buildups
+
+
+ +

Buildup weight methods provide weight breakdowns for vehicles based on part-by-part sizing. +More...

+ + + + + + + + +

+Modules

 Common
 The Common buildup methods are those which are shared between vehicle types utilizing buildup weight methods.
 
 EVTOL
 The empty method that is called by the analysis.
 
+

Detailed Description

+

Buildup weight methods provide weight breakdowns for vehicles based on part-by-part sizing.

+
+
+ + + + diff --git a/doxygen/group__Methods-Weights-Buildups.js b/doxygen/group__Methods-Weights-Buildups.js new file mode 100644 index 00000000..a0db4f9d --- /dev/null +++ b/doxygen/group__Methods-Weights-Buildups.js @@ -0,0 +1,5 @@ +var group__Methods_Weights_Buildups = +[ + [ "Common", "group__Methods-Weights-Buildups-Common.html", "group__Methods-Weights-Buildups-Common" ], + [ "EVTOL", "group__Methods-Weights-Buildups-EVTOL.html", null ] +]; \ No newline at end of file diff --git a/doxygen/group__Methods-Weights-Correlations-BWB.html b/doxygen/group__Methods-Weights-Correlations-BWB.html index 243f2ef1..83e9f10e 100644 --- a/doxygen/group__Methods-Weights-Correlations-BWB.html +++ b/doxygen/group__Methods-Weights-Correlations-BWB.html @@ -1,9 +1,9 @@ - + - + SUAVE: BWB @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@
- +
@@ -73,7 +78,9 @@

@@ -109,8 +116,6 @@   def SUAVE.Methods.Weights.Correlations.BWB.empty.empty (vehicle)   -def SUAVE.Methods.Weights.Correlations.BWB.systems.systems (num_seats, ctrl_type, S_h, S_gross_w, ac_type) - 

Detailed Description

Provides structural weight correlations for a BWB concept.

@@ -242,16 +247,18 @@

-
This is for a BWB aircraft configuration. 
+
This is for a BWB aircraft configuration.
 
 Assumptions:
-     calculated aircraft weight from correlations created per component of historical aircraft
-  
-Source: 
+     Calculated aircraft weight from correlations created per component of historical aircraft
+     The wings are made out of aluminum.
+     A wing with the tag 'main_wing' exists.
+
+Source:
     N/A
-     
+
 Inputs:
-    engine - a data dictionary with the fields:                    
+    engine - a data dictionary with the fields:
         thrust_sls - sea level static thrust of a single engine                                        [Newtons]
 
     wing - a data dictionary with the fields:
@@ -263,7 +270,7 @@ 

-

◆ systems()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Weights.Correlations.BWB.systems.systems ( num_seats,
 ctrl_type,
 S_h,
 S_gross_w,
 ac_type 
)
-
-
Calculate the weight of the different engine systems on the aircraft
-
-Assumptions:
-    numbers based on FAA regulations and correlations from previous aircraft
-            
-Source:
-    N/A  
-
-Inputs:
-    num_seats - total number of seats on the aircraft                                                   [dimensionless]
-    ctrl_type - specifies if the control system is fully power, partially powered, or not powered       [dimensionless]
-    S_h - area of the BWB outer aileron                                                                 [meters**2]
-    S_gross_w - area of the wing                                                                        [meters**2]
-    ac_type - determines type of instruments, electronics, and operating items based on type of vehicle [dimensionless]
-
-Outputs:
-    output - a data dictionary with fields:
-        wt_flt_ctrl - weight of the flight control system                                               [kilograms]
-        wt_apu - weight of the apu                                                                      [kilograms]
-        wt_hyd_pnu - weight of the hydraulics and pneumatics                                            [kilograms]
-        wt_instruments - weight of the instruments and navigational equipment                           [kilograms]
-        wt_avionics - weight of the avionics                                                            [kilograms]
-        wt_opitems - weight of the optional items based on the type of aircraft                         [kilograms]
-        wt_elec - weight of the electrical items                                                        [kilograms]
-        wt_ac - weight of the air conditioning and anti-ice system                                      [kilograms]
-        wt_furnish - weight of the furnishings in the fuselage                                          [kilograms]
-    
 Properties Used:
 N/A
 
@@ -378,7 +310,7 @@

Generated by - doxygen 1.8.14 + doxygen 1.8.15

diff --git a/doxygen/group__Methods-Weights-Correlations-BWB.js b/doxygen/group__Methods-Weights-Correlations-BWB.js index 8c23c589..364a1e2f 100644 --- a/doxygen/group__Methods-Weights-Correlations-BWB.js +++ b/doxygen/group__Methods-Weights-Correlations-BWB.js @@ -2,6 +2,5 @@ var group__Methods_Weights_Correlations_BWB = [ [ "aft_centerbody", "group__Methods-Weights-Correlations-BWB.html#ga6fbf6d817a459d781b07fa73faeee5ad", null ], [ "cabin", "group__Methods-Weights-Correlations-BWB.html#gaf79b9d073d3341d628c056ca69469809", null ], - [ "empty", "group__Methods-Weights-Correlations-BWB.html#ga94172601f2f840265bd87601800de860", null ], - [ "systems", "group__Methods-Weights-Correlations-BWB.html#ga49462fb84af76259349c80f42402decf", null ] + [ "empty", "group__Methods-Weights-Correlations-BWB.html#ga94172601f2f840265bd87601800de860", null ] ]; \ No newline at end of file diff --git a/doxygen/group__Methods-Weights-Correlations-Common.html b/doxygen/group__Methods-Weights-Correlations-Common.html index ec402def..b35069dc 100644 --- a/doxygen/group__Methods-Weights-Correlations-Common.html +++ b/doxygen/group__Methods-Weights-Correlations-Common.html @@ -1,9 +1,9 @@ - + - + SUAVE: Common @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@
- +

@@ -73,7 +78,9 @@
@@ -103,19 +110,20 @@ - - - - - - - + + + + + + + +

Functions

def SUAVE.Methods.Weights.Correlations.Common.landing_gear.landing_gear (TOW, landing_gear_wt_factor=0.04)
 landing_gear.py More...
 
def SUAVE.Methods.Weights.Correlations.Common.payload.payload (TOW, empty, num_pax, wt_cargo, wt_passenger=195 *Units.lbs, wt_baggage=30 *Units.lbs)
 
def SUAVE.Methods.Weights.Correlations.Common.wing_main.wing_main (S_gross_w, b, lambda_w, t_c_w, sweep_w, Nult, TOW, wt_zf)
 
def SUAVE.Methods.Weights.Correlations.Common.landing_gear.landing_gear (vehicle, landing_gear_wt_factor=0.04)
 
def SUAVE.Methods.Weights.Correlations.Common.payload.payload (vehicle, wt_passenger=195 *Units.lbs, wt_baggage=30 *Units.lbs)
 
def SUAVE.Methods.Weights.Correlations.Common.systems.systems (vehicle)
 
def SUAVE.Methods.Weights.Correlations.Common.wing_main.wing_main (vehicle, wing, rho, sigma, computation_type='segmented')
 

Detailed Description

Provides structural weight correlations for aircraft components applicable to all aircraft configurations.

Function Documentation

- -

◆ landing_gear()

+ +

◆ landing_gear()

@@ -124,7 +132,7 @@

def SUAVE.Methods.Weights.Correlations.Common.landing_gear.landing_gear (   - TOW, + vehicle, @@ -139,9 +147,7 @@

- -

landing_gear.py

-

Created: Jan 2014, A. Wendorff Modified: Feb 2016, E. Botero Jul 2017, M. Clarke

Calculate the weight of the landing gear assuming that the gear 
+
Calculate the weight of the landing gear assuming that the gear 
 weight is 4 percent of the takeoff weight        
 
 Assumptions:
@@ -162,8 +168,8 @@ 

-

◆ payload()

+ +

◆ payload()

@@ -172,37 +178,19 @@

def SUAVE.Methods.Weights.Correlations.Common.payload.payload (   - TOW, - - - - -   - empty, + vehicle,   - num_pax, + wt_passenger = 195 * Units.lbs,   - wt_cargo, - - - - -   - wt_passenger = 195*Units.lbs, - - - - -   - wt_baggage = 30*Units.lbs  + wt_baggage = 30 * Units.lbs  @@ -240,59 +228,91 @@

-

◆ wing_main()

+ +

◆ systems()

- + - - - - + - - - - - - - - +
def SUAVE.Methods.Weights.Correlations.Common.wing_main.wing_main def SUAVE.Methods.Weights.Correlations.Common.systems.systems (  S_gross_w,
vehicle)  b,
 lambda_w,
+
+
Calculate the weight of the different engine systems on the aircraft
+
+Assumptions:
+    numbers based on FAA regulations and correlations from previous aircraft
+
+Source:
+    http://aerodesign.stanford.edu/aircraftdesign/structures/componentweight.html
+
+   Inputs:
+   vehicle.passengers - total number of seats on the aircraft                                     [dimensionless]
+   vehicle.systems.control - specifies if the control system is fully power,
+                                partially powered, or not powered                                 [dimensionless]
+   wing.areas.reference - area of the horizontal tail                                             [meters**2]
+   wing.areas.reference - area of the vertical tail                                               [meters**2]
+   vehicle.reference_area - area of the wing                                                      [meters**2]
+   vehicle.systems.accessories - determines type of instruments, electronics,
+                                    and operating items based on type of vehicle                  [dimensionless]
+
+   Outputs:
+   output - a data dictionary with fields:
+       wt_flt_ctrl - weight of the flight control system                                               [kilograms]
+       wt_apu - weight of the apu                                                                      [kilograms]
+       wt_hyd_pnu - weight of the hydraulics and pneumatics                                            [kilograms]
+       wt_instruments - weight of the instruments and navigational equipment                           [kilograms]
+       wt_avionics - weight of the avionics                                                            [kilograms]
+       wt_opitems - weight of the optional items based on the type of aircraft                         [kilograms]
+       wt_elec - weight of the electrical items                                                        [kilograms]
+       wt_ac - weight of the air conditioning and anti-ice system                                      [kilograms]
+       wt_furnish - weight of the furnishings in the fuselage                                          [kilograms]
+
+Properties Used:
+    N/A
+
+
+
+ +

◆ wing_main()

+ +
+
+ - - + + - + - + - + - + - + @@ -301,29 +321,33 @@

-
Calculate the wing weight of the aircraft based on the fully-stressed 
+
Calculate the wing weight of the aircraft based on the fully-stressed
 bending weight of the wing box
 
 Assumptions:
-    calculated total wing weight based on a bending index and actual data 
-    from 15 transport aircraft 
+    calculated total wing weight based on a bending index and actual data
+    from 15 transport aircraft
+
+Source:
+    http://aerodesign.stanford.edu/aircraftdesign/AircraftDesign.html
+    search for: Derivation of the Wing Weight Index
 
-Source: 
-    N/A
-    
 Inputs:
-    S_gross_w - area of the wing                 [meters**2]
-    b - span of the wing                         [meters**2]
-    lambda_w - taper ratio of the wing           [dimensionless]
-    t_c_w - thickness-to-chord ratio of the wing [dimensionless]
-    sweep_w - sweep of the wing                  [radians]
-    Nult - ultimate load factor of the aircraft  [dimensionless]
-    TOW - maximum takeoff weight of the aircraft [kilograms]
-    wt_zf - zero fuel weight of the aircraft     [kilograms]
+    vehicle - data dictionary with vehicle properties                   [dimensionless]
+        -.mass_properties.max_takeoff: MTOW                             [kilograms]
+        -.mass_properties.max_zero_fuel: zero fuel weight aircraft      [kilograms]
+        -.envelope.ultimate_load: ultimate load factor
+    wing    - data dictionary with specific wing properties             [dimensionless]
+        -.areas.reference: wing reference surface area                  [m^2]
+        -.sweeps.quarter_chord: quarter chord sweep angle               [deg]
+        -.spans.projected: wing span                                    [m]
+        -.thickness_to_chord: thickness to chord of wing
+        -.taper: taper ratio of wing
+        -.chords.root: root chord                                       [m]
 
 Outputs:
-    weight - weight of the wing                  [kilograms]          
-    
+    weight - weight of the wing                  [kilograms]
+
 Properties Used:
     N/A
 
@@ -336,7 +360,7 @@

Generated by - doxygen 1.8.14 + doxygen 1.8.15 diff --git a/doxygen/group__Methods-Weights-Correlations-Common.js b/doxygen/group__Methods-Weights-Correlations-Common.js index ff27346f..2462c587 100644 --- a/doxygen/group__Methods-Weights-Correlations-Common.js +++ b/doxygen/group__Methods-Weights-Correlations-Common.js @@ -1,6 +1,7 @@ var group__Methods_Weights_Correlations_Common = [ - [ "landing_gear", "group__Methods-Weights-Correlations-Common.html#ga8a44f526125ceed65e6d2f27fe5aa82c", null ], - [ "payload", "group__Methods-Weights-Correlations-Common.html#gacf280c435b3294c568c1b374d0ff7c3b", null ], - [ "wing_main", "group__Methods-Weights-Correlations-Common.html#gaeaee339d59dc928ac31ef8a65ddbde33", null ] + [ "landing_gear", "group__Methods-Weights-Correlations-Common.html#ga42672c79ab61f01f25b8ce74ebc1257c", null ], + [ "payload", "group__Methods-Weights-Correlations-Common.html#ga2de3c7f22ce15fd31873c550b6d4d5ac", null ], + [ "systems", "group__Methods-Weights-Correlations-Common.html#ga2897edee5eaf6837a18d9af88a15529f", null ], + [ "wing_main", "group__Methods-Weights-Correlations-Common.html#gaf5fffaf27a31a52788dc9087c96aff06", null ] ]; \ No newline at end of file diff --git a/doxygen/group__Methods-Weights-Correlations-FLOPS.html b/doxygen/group__Methods-Weights-Correlations-FLOPS.html new file mode 100644 index 00000000..df959c73 --- /dev/null +++ b/doxygen/group__Methods-Weights-Correlations-FLOPS.html @@ -0,0 +1,1204 @@ + + + + + + + +SUAVE: Methods-Weights-Correlations-FLOPS + + + + + + + + + + + + + + + +
+
+

def SUAVE.Methods.Weights.Correlations.Common.wing_main.wing_main (  t_c_w, vehicle,
 sweep_w, wing,
 Nult, rho,
 TOW, sigma,
 wt_zf computation_type = 'segmented' 
+ + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
Methods-Weights-Correlations-FLOPS
+
+
+ +

Provides structural weight correlations for aircraft components based on the FLOPS method. +More...

+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +

+Functions

def SUAVE.Methods.Weights.Correlations.FLOPS.fuselage.fuselage_weight_FLOPS (vehicle)
 
def SUAVE.Methods.Weights.Correlations.FLOPS.landing_gear.landing_gear_FLOPS (vehicle)
 
def SUAVE.Methods.Weights.Correlations.FLOPS.operating_items.operating_items_FLOPS (vehicle)
 
def SUAVE.Methods.Weights.Correlations.FLOPS.payload.payload_FLOPS (vehicle, weight_per_passenger=165. *Units.lb)
 
def SUAVE.Methods.Weights.Correlations.FLOPS.prop_system.total_prop_flops (vehicle, prop)
 
def SUAVE.Methods.Weights.Correlations.FLOPS.prop_system.nacelle_FLOPS (prop, nacelle)
 
def SUAVE.Methods.Weights.Correlations.FLOPS.prop_system.thrust_reverser_FLOPS (prop)
 
def SUAVE.Methods.Weights.Correlations.FLOPS.prop_system.misc_engine_FLOPS (vehicle, prop, nacelle)
 
def SUAVE.Methods.Weights.Correlations.FLOPS.prop_system.fuel_system_FLOPS (vehicle, NENG)
 
def SUAVE.Methods.Weights.Correlations.FLOPS.prop_system.engine_FLOPS (vehicle, prop)
 
def SUAVE.Methods.Weights.Correlations.FLOPS.systems.systems_FLOPS (vehicle)
 
def SUAVE.Methods.Weights.Correlations.FLOPS.tail.tail_vertical_FLOPS (vehicle, wing)
 
def SUAVE.Methods.Weights.Correlations.FLOPS.wing.wing_weight_FLOPS (vehicle, wing, WPOD, complexity, settings, num_main_wings)
 
def SUAVE.Methods.Weights.Correlations.FLOPS.wing.generate_wing_stations (fuselage_width, wing)
 
def SUAVE.Methods.Weights.Correlations.FLOPS.wing.generate_int_stations (NSD, ETA)
 
def SUAVE.Methods.Weights.Correlations.FLOPS.wing.calculate_load (ETA)
 
def SUAVE.Methods.Weights.Correlations.FLOPS.wing.find_sweep (y, lst_y, swp)
 
def SUAVE.Methods.Weights.Correlations.FLOPS.wing.get_spanwise_engine (networks, SEMISPAN)
 
def SUAVE.Methods.Weights.Correlations.FLOPS.wing.wing_weight_constants_FLOPS (ac_type)
 
def SUAVE.Methods.Weights.Correlations.FLOPS.wing.determine_fuselage_chord (fuselage_width, wing)
 
+

Detailed Description

+

Provides structural weight correlations for aircraft components based on the FLOPS method.

+

Function Documentation

+ +

◆ calculate_load()

+ +
+
+ + + + + + + + +
def SUAVE.Methods.Weights.Correlations.FLOPS.wing.calculate_load ( ETA)
+
+
Returns load factor assuming elliptical load distribution
+
+    Assumptions:
+
+    Source:
+        The Flight Optimization System Weight Estimation Method
+
+    Inputs:
+        ETA: list of spanwise locations of all sections of the wing
+
+   Outputs:
+       PS: load factor at every location in ETA assuming elliptical load distribution
+
+    Properties Used:
+        N/A
+
+
+
+ +

◆ determine_fuselage_chord()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Weights.Correlations.FLOPS.wing.determine_fuselage_chord ( fuselage_width,
 wing 
)
+
+
Determine chord at wing and fuselage intersection
+
+    Assumptions:
+        Fuselage side of body is between first and second wing segments.
+
+    Source:
+        The Flight Optimization System Weight Estimation Method
+
+    Inputs:
+        fuselage_width: width of fuselage                                   [m]
+        wing: data dictionary with wing properties
+                -.taper: taper ratio
+                -.sweeps.quarter_chord: quarter chord sweep angle           [deg]
+                -.thickness_to_chord: thickness to chord
+                -.spans.projected: wing span                                [m]
+                -.chords.root: root chord                                   [m]
+            -.fuselages.fuselage.width: fuselage width                      [m]
+   Outputs:
+       chord: chord length of wing where wing intersects the fuselage wall [ft]
+
+    Properties Used:
+        N/A
+
+
+
+ +

◆ engine_FLOPS()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Weights.Correlations.FLOPS.prop_system.engine_FLOPS ( vehicle,
 prop 
)
+
+
Calculates the dry engine weight based on the FLOPS method
+    Assumptions:
+        Rated thrust per scaled engine and rated thurst for baseline are the same
+        Engine weight scaling parameter is 1.15
+        Enginge inlet weight scaling exponent is 1
+        Baseline inlet weight is 0 lbs as in example files FLOPS
+        Baseline nozzle weight is 0 lbs as in example files FLOPS
+
+    Source:
+        The Flight Optimization System Weight Estimation Method
+
+    Inputs:
+        vehicle - data dictionary with vehicle properties                   [dimensionless]
+            -.systems.accessories: type of aircraft (short-range, commuter
+                                                    medium-range, long-range,
+                                                    sst, cargo)
+        prop    - data dictionary for the specific network that is being estimated [dimensionless]
+            -.sealevel_static_thrust: sealevel static thrust of engine  [N]
+
+    Outputs:
+        WENG: dry engine weight                                         [kg]
+
+    Properties Used:
+        N/A
+
+
+
+ +

◆ find_sweep()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Weights.Correlations.FLOPS.wing.find_sweep ( y,
 lst_y,
 swp 
)
+
+
Finds sweep angle for a certain y-location along the wing
+
+    Assumptions:
+
+    Source:
+        The Flight Optimization System Weight Estimation Method
+
+    Inputs:
+        y: spanwise location
+        lst_y: list of spanwise stations where sweep is known (eg sections)
+        swp: list of quarter chord sweep angles at the locations listed in lst_y
+
+   Outputs:
+       swps: sweep angle at y
+
+    Properties Used:
+        N/A
+
+
+
+ +

◆ fuel_system_FLOPS()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Weights.Correlations.FLOPS.prop_system.fuel_system_FLOPS ( vehicle,
 NENG 
)
+
+
Calculates the weight of the fuel system based on the FLOPS method
+    Assumptions:
+
+    Source:
+        The Flight Optimization System Weight Estimation Method
+
+    Inputs:
+        vehicle - data dictionary with vehicle properties                   [dimensionless]
+            -.design_mach_number: design mach number
+            -.mass_properties.max_zero_fuel: maximum zero fuel weight   [kg]
+
+    Outputs:
+        WFSYS: Fuel system weight                                       [kg]
+
+    Properties Used:
+        N/A
+
+
+
+ +

◆ fuselage_weight_FLOPS()

+ +
+
+ + + + + + + + +
def SUAVE.Methods.Weights.Correlations.FLOPS.fuselage.fuselage_weight_FLOPS ( vehicle)
+
+
Calculate the weight of the fuselage of a transport aircraft
+
+    Assumptions:
+        NFUSE = 1, only one fuselage (it's possible to modify this in future work)
+        delta_isa = 0, for pressure calculations
+        Fuselage is tagged as 'fuselage'
+
+    Source:
+        The Flight Optimization System Weight Estimation Method
+
+    Inputs:
+        vehicle - data dictionary with vehicle properties                    [dimensionless]
+            -.networks: data dictionary containing all propulsion properties
+            -.fuselages['fuselage'].lengths.total: fuselage total length      [meters]
+            -.fuselages['fuselage'].width: fuselage width                    [meters]
+            -.fuselages['fuselage'].heights.maximum: fuselage maximum height [meters]
+            -.envelope.ultimate_load: ultimate load factor (default: 3.75)
+            -.systems.accessories: type of aircraft (short-range, commuter
+                                                    medium-range, long-range,
+                                                    sst, cargo)
+            -.mass_properties.max_takeoff: MTOW                              [kilograms]
+            -.design_mach_number: design mach number for cruise flight
+
+    Outputs:
+        WFUSE - weight of the fuselage                                      [kilograms]
+
+    Properties Used:
+        N/A
+
+
+
+ +

◆ generate_int_stations()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Weights.Correlations.FLOPS.wing.generate_int_stations ( NSD,
 ETA 
)
+
+
Divides half of the wing in integration stations
+
+    Assumptions:
+
+    Source:
+        The Flight Optimization System Weight Estimation Method
+
+    Inputs:
+        NSD: number of integration stations requested
+        ETA: list of spanwise locations of all sections of the wing
+
+   Outputs:
+       NS: actual number of integration stations
+       Y: spanwise locations of the integrations stations normalized by half span
+
+    Properties Used:
+        N/A
+
+
+
+ +

◆ generate_wing_stations()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Weights.Correlations.FLOPS.wing.generate_wing_stations ( fuselage_width,
 wing 
)
+
+
Divides half the wing in sections, using the defined sections
+    and adding a section at the intersection of wing and fuselage
+
+    Assumptions:
+
+    Source:
+        The Flight Optimization System Weight Estimation Method
+
+    Inputs:
+        fuselage_width: fuselage width                                      [m]
+        wing: data dictionary with wing properties
+                -.taper: taper ration wing
+                -.sweeps.quarter_chord: quarter chord sweep angle           [deg]
+                -.thickness_to_chord: thickness to chord
+                -.spans.projected: wing span                                [m]
+                -.chords.root: root chord                                   [m]
+                -.tip.root: tip chord                                       [m]
+                -.twists.root: twist of wing at root                        [deg]
+                -.twists.tip: twist of wing at tip                          [deg]
+                -.Segments: trapezoidal segments of the wing
+
+   Outputs:
+       ETA: spanwise location of the sections normalized by half span
+       C: chord lengths at every spanwise location in ETA normalized by half span
+       T: thickness to chord ratio at every span wise location in ETA
+       SWP: quarter chord sweep angle at every span wise location in ETA
+
+    Properties Used:
+        N/A
+
+
+
+ +

◆ get_spanwise_engine()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Weights.Correlations.FLOPS.wing.get_spanwise_engine ( networks,
 SEMISPAN 
)
+
+
Returns EETA for the engine locations along the wing
+
+    Assumptions:
+
+    Source:
+        The Flight Optimization System Weight Estimation Method
+
+    Inputs:
+        networks: data dictionary with all the engine properties
+            -.wing_mounted: list of boolean if engine is mounted to wing
+            -.number_of_engines: number of engines
+            -.origin: origin of the engine
+        SEMISPAN: half span                                 [m]
+   Outputs:
+       EETA: span wise locations of the engines mounted to the wing normalized by the half span
+
+    Properties Used:
+        N/A
+
+
+
+ +

◆ landing_gear_FLOPS()

+ +
+
+ + + + + + + + +
def SUAVE.Methods.Weights.Correlations.FLOPS.landing_gear.landing_gear_FLOPS ( vehicle)
+
+
Calculate the weight of the main and nose landing gear of a transport aircraft
+
+    Assumptions:
+        No fighter jet, change DFTE to 1 for a fighter jet
+        Aircraft is not meant for carrier operations, change CARBAS to 1 for carrier-based aircraft
+
+    Source:
+        The Flight Optimization System Weight Estimation Method
+
+    Inputs:
+        vehicle - data dictionary with vehicle properties                   [dimensionless]
+            -.networks: data dictionary containing all propulsion properties
+            -.design_range: design range of aircraft                        [nmi]
+            -.systems.accessories: type of aircraft (short-range, commuter
+                                                    medium-range, long-range,
+                                                    sst, cargo)
+            -.mass_properties.max_takeoff: MTOW                              [kilograms]
+            -.nacelles['nacelle']                                            [meters]
+            -.wings['main_wing'].dihedral                                    [radians]
+            -.fuselages['fuselage'].width: fuselage width                    [meters]
+            -.fuselages['fuselage'].lengths.total: fuselage total length     [meters]
+
+
+    Outputs:
+        output - data dictionary with main and nose landing gear weights    [kilograms]
+                output.main, output.nose
+
+    Properties Used:
+        N/A
+
+
+
+ +

◆ misc_engine_FLOPS()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Weights.Correlations.FLOPS.prop_system.misc_engine_FLOPS ( vehicle,
 prop,
 nacelle 
)
+
+
Calculates the miscellaneous engine weight based on the FLOPS method, electrical control system weight
+    and starter engine weight
+    
+    Assumptions:
+        1) All nacelles are identical
+        2) The number of nacelles is the same as the number of engines 
+
+    Source:
+        The Flight Optimization System Weight Estimation Method
+
+    Inputs:
+        vehicle - data dictionary with vehicle properties                            [dimensionless]
+             -.design_mach_number: design mach number
+        prop    - data dictionary for the specific network that is being estimated [dimensionless]
+            -.number_of_engines: number of engines
+            -.sealevel_static_thrust: sealevel static thrust of engine               [N]
+        nacelle              
+            -.diameter: diameter of nacelle                                          [m]
+          
+    Outputs:              
+        WEC: electrical engine control system weight                                 [kg]
+        WSTART: starter engine weight                                                [kg]
+
+    Properties Used:
+        N/A
+
+
+
+ +

◆ nacelle_FLOPS()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Weights.Correlations.FLOPS.prop_system.nacelle_FLOPS ( prop,
 nacelle 
)
+
+
Calculates the nacelle weight based on the FLOPS method
+
+    Assumptions:
+        1) All nacelles are identical
+        2) The number of nacelles is the same as the number of engines 
+
+    Source:
+        Aircraft Design: A Conceptual Approach
+
+    Inputs:
+        prop    - data dictionary for the specific network that is being estimated [dimensionless]
+            -.number_of_engines: number of engines
+            -.engine_lenght: total length of engine                                  [m]
+            -.sealevel_static_thrust: sealevel static thrust of engine               [N]
+        nacelle.             
+            -.diameter: diameter of nacelle                                          [m]
+        WENG    - dry engine weight                                                  [kg]
+         
+         
+    Outputs:             
+        WNAC: nacelle weight                                                         [kg]
+
+    Properties Used:
+        N/A
+
+
+
+ +

◆ operating_items_FLOPS()

+ +
+
+ + + + + + + + +
def SUAVE.Methods.Weights.Correlations.FLOPS.operating_items.operating_items_FLOPS ( vehicle)
+
+
Calculate the weight of operating items, including:
+    - crew
+    - baggage
+    - unusable fuel
+    - engine oil
+    - passenger service
+    - ammunition and non-fixed weapons
+    - cargo containers
+
+    Assumptions:
+        If no tanks are specified, 5 fuel tanks are assumed (includes main and auxiliary tanks)
+        If the number of coach seats is not defined, then it assumed that 5% of
+            of the seats are first class and an additional 10 % are business class.
+        If the number of coach seats is defined, then the additional seats are 1/4 first class
+            and 3/4 business class
+
+    Source:
+        The Flight Optimization System Weight Estimation Method
+
+    Inputs:
+        vehicle - data dictionary with vehicle properties                   [dimensionless]
+            -.networks: data dictionary containing all propulsion properties
+                -.number_of_engines: number of engines
+                -.sealevel_static_thrust: thrust at sea level               [N]
+            -.reference_area: wing surface area                             [m^2]
+            -.mass_properties.max_takeoff: MTOW                             [kilograms]
+            -.passengers: number of passengers in aircraft
+            -.design_mach_number: design mach number for cruise flight
+            -.design_range: design range of aircraft                        [nmi]
+            -.mass_properties.cargo: weight of cargo carried                [kilograms]
+
+    Outputs:
+        output - data dictionary with weights                               [kilograms]
+                - output.oper_items: unusable fuel, engine oil, passenger service weight and cargo containers
+                - output.flight_crew: flight crew weight
+                - output.flight_attendants: flight attendants weight
+                - output.total: total operating items weight
+
+    Properties Used:
+        N/A
+
+
+
+ +

◆ payload_FLOPS()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Weights.Correlations.FLOPS.payload.payload_FLOPS ( vehicle,
 weight_per_passenger = 165. * Units.lb 
)
+
+
Calculate the payload weight, including:
+    - passenger and carry-on weight
+    - baggage weight
+    - cargo weight
+
+    Assumptions:
+        None
+
+    Source:
+        The Flight Optimization System Weight Estimation Method
+
+    Inputs:
+        vehicle - data dictionary with vehicle properties                   [dimensionless]
+            -.passengers: number of passengers in aircraft
+            -.design_range: design range of aircraft                        [nmi]
+            -.mass_properties.cargo: weight of cargo carried                [kilograms]
+
+    Outputs:
+        output - data dictionary with weights                               [kilograms]
+                - output.passengers: passenger weight
+                - output.baggage: baggage weight
+                - output.cargo: cargo weight
+                - output.total: total payload weight
+
+    Properties Used:
+        N/A
+
+
+
+ +

◆ systems_FLOPS()

+ +
+
+ + + + + + + + +
def SUAVE.Methods.Weights.Correlations.FLOPS.systems.systems_FLOPS ( vehicle)
+
+
Calculate the system weight of the aircraft including:
+    -  flight control system
+    - apu weight
+    - hydraulics and pneumatics weight
+    - intstrumentation weight
+    - avionics weight
+    - electrical system weight
+    - air-condtioning weight
+    - furnishing weight
+    - anti-ice weight
+
+Assumptions:
+    1) No variable sweep, change VARSWP to 1 is variable sweep in aicraft
+    2) Hydraulic pressure is 3000 psf (HYDR)
+    3) 1 fuselage named fuselage. Function could be modified to allow multiple fuselages by
+       relaxing this assumption.
+
+Source:
+    The Flight Optimization System Weight Estimation Method
+
+   Inputs:
+    vehicle - data dictionary with vehicle properties                   [dimensionless]
+        -.networks: data dictionary containing all propulsion properties
+            -.number_of_engines: number of engines
+            -.sealevel_static_thrust: thrust at sea level               [N]
+        -.fuselages['fuselage'].lengths.total: fuselage total length    [meters]
+        -.fuselages['fuselage'].width: fuselage width                   [meters]
+        -.fuselages['fuselage'].heights.maximum: fuselage maximum height[meters]
+        -.mass_properties.max_takeoff: MTOW                             [kilograms]
+        -.design_mach_number: design mach number for cruise flight
+        -.design_range: design range of aircraft                        [nmi]
+        -.passengers: number of passengers in aircraft
+        -.wings['main_wing']: data dictionary with main wing properties
+            -.sweeps.quarter_chord: quarter chord sweep                 [deg]
+            -.areas.reference: wing surface area                        [m^2]
+            -.spans.projected: projected span of wing                   [m]
+            -.flap_ratio: flap surface area over wing surface area
+
+   Outputs:
+   output - a data dictionary with fields:
+       wt_flt_ctrl - weight of the flight control system                                [kilograms]
+       wt_apu - weight of the apu                                                       [kilograms]
+       wt_hyd_pnu - weight of the hydraulics and pneumatics                             [kilograms]
+       wt_instruments - weight of the instruments and navigational equipment            [kilograms]
+       wt_avionics - weight of the avionics                                             [kilograms]
+       wt_elec - weight of the electrical items                                         [kilograms]
+       wt_ac - weight of the air conditioning and anti-ice system                       [kilograms]
+       wt_furnish - weight of the furnishings in the fuselage                           [kilograms]
+       wt_anti_ice - weight of anti-ice system                                          [kilograms]
+
+Properties Used:
+    N/A
+
+
+
+ +

◆ tail_vertical_FLOPS()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Weights.Correlations.FLOPS.tail.tail_vertical_FLOPS ( vehicle,
 wing 
)
+
+
Calculate the vertical tail weight
+
+    Assumptions:
+       Conventional tail configuration
+
+    Source:
+        The Flight Optimization System Weight Estimation Method
+
+   Inputs:
+        vehicle - data dictionary with vehicle properties                   [dimensionless]
+            -.mass_properties.max_takeoff: MTOW                             [kilograms]
+        wing - data dictionary with vertical tail properties                [dimensionless]
+            -.taper: taper of wing
+            -.areas.reference: surface area of wing                         [m^2]
+
+   Outputs:
+        WVT - vertical tail weight                                          [kilograms]
+
+    Properties Used:
+        N/A
+
+
+ +

◆ thrust_reverser_FLOPS()

+ +
+
+ + + + + + + + +
def SUAVE.Methods.Weights.Correlations.FLOPS.prop_system.thrust_reverser_FLOPS ( prop)
+
+
Calculates the weight of the thrust reversers of the aircraft
+
+    Assumptions:
+
+    Source:
+        The Flight Optimization System Weight Estimation Method
+
+    Inputs:
+        prop    - data dictionary for the specific network that is being estimated [dimensionless]
+            -.number_of_engines: number of engines
+            -.sealevel_static_thrust: sealevel static thrust of engine  [N]
+
+    Outputs:
+        WTHR: Thrust reversers weight                                   [kg]
+
+    Properties Used:
+        N/A
+
+
+
+ +

◆ total_prop_flops()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Weights.Correlations.FLOPS.prop_system.total_prop_flops ( vehicle,
 prop 
)
+
+
Calculate the weight of propulsion system, including:
+    - dry engine weight
+    - fuel system weight
+    - thurst reversers weight
+    - electrical system weight
+    - starter engine weight
+    - nacelle weight
+    - cargo containers
+
+    Assumptions:
+        1) Rated thrust per scaled engine and rated thurst for baseline are the same
+        2) Engine weight scaling parameter is 1.15
+        3) Enginge inlet weight scaling exponent is 1
+        4) Baseline inlet weight is 0 lbs as in example files FLOPS
+        5) Baseline nozzle weight is 0 lbs as in example files FLOPS
+
+    Source:
+        The Flight Optimization System Weight Estimation Method
+
+    Inputs:
+        vehicle - data dictionary with vehicle properties                   [dimensionless]
+            -.design_mach_number: design mach number for cruise flight
+            -.mass_properties.max_zero_fuel: zero fuel weight               [kg]
+            -.systems.accessories: type of aircraft (short-range, commuter
+                                                    medium-range, long-range,
+                                                    sst, cargo)
+        nacelle - data dictionary with propulsion system properties 
+            -.diameter: diameter of nacelle                                 [meters]
+            -.length: length of complete engine assembly                    [meters]
+        prop.
+            -.sealevel_static_thrust: thrust at sea level                   [N]
+
+
+    Outputs:
+        output - data dictionary with weights                               [kilograms]
+                - output.wt_prop: total propulsive system weight
+                - output.wt_thrust_reverser: thurst reverser weight
+                - output.starter: starter engine weight
+                - output.wt_engine_controls: engine controls weight
+                - output.fuel_system: fuel system weight
+                - output.nacelle: nacelle weight
+                - output.wt_eng: dry engine weight
+
+    Properties Used:
+        N/A
+
+
+
+ +

◆ wing_weight_constants_FLOPS()

+ +
+
+ + + + + + + + +
def SUAVE.Methods.Weights.Correlations.FLOPS.wing.wing_weight_constants_FLOPS ( ac_type)
+
+
Defines wing weight constants as defined by FLOPS
+    Inputs: ac_type - determines type of instruments, electronics, and operating items based on types:
+            "short-range", "medium-range", "long-range", "business", "cargo", "commuter", "sst"
+    Outputs: list of coefficients used in weight estimations
+
+
+ +

◆ wing_weight_FLOPS()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Weights.Correlations.FLOPS.wing.wing_weight_FLOPS ( vehicle,
 wing,
 WPOD,
 complexity,
 settings,
 num_main_wings 
)
+
+
Calculate the wing weight based on the flops method. The wing weight consists of:
+    - Total Wing Shear Material and Control Surface Weight
+    - Total Wing Miscellaneous Items Weight
+    - Total Wing Bending Material Weight
+
+    Assumptions:
+        Wing is elliptically loaded
+        Gloved wing area is 0
+        Load between multiple main wings is distributed equally
+        Wing sweep is fixed
+
+    Source:
+        The Flight Optimization System Weight Estimation Method
+
+   Inputs:
+        vehicle - data dictionary with vehicle properties                   [dimensionless]
+            -.reference_area: wing surface area                             [m^2]
+            -.mass_properties.max_takeoff: MTOW                             [kilograms]
+            -.envelope.ultimate_load: ultimate load factor (default: 3.75)
+            -.systems.accessories: type of aircraft (short-range, commuter
+                                                    medium-range, long-range,
+                                                    sst, cargo)
+            -.fuselages.fuselage.width: width of the fuselage               [m]
+         -wing: data dictionary with wing properties
+                -.taper: taper ratio
+                -.sweeps.quarter_chord: quarter chord sweep angle           [deg]
+                -.thickness_to_chord: thickness to chord
+                -.spans.projected: wing span                                [m]
+                -.chords.root: root chord                                   [m]
+                -.tip.root: tip chord                                       [m]
+                -.twists.root: twist of wing at root                        [deg]
+                -.twists.tip: twist of wing at tip                          [deg]
+                -.flap_ratio: flap surface area over wing surface area
+             -.networks: data dictionary containing all propulsion properties
+                -.number_of_engines: number of engines
+                -.sealevel_static_thrust: thrust at sea level               [N]
+        WPOD - weight of engine pod including the nacelle                   [kilograms]
+        complexity - "simple" or "complex" depending on the wing weight method chosen
+
+   Outputs:
+        WWING - wing weight                                          [kilograms]
+
+    Properties Used:
+        N/A
+
+
+
+
+
+ + + + diff --git a/doxygen/group__Methods-Weights-Correlations-FLOPS.js b/doxygen/group__Methods-Weights-Correlations-FLOPS.js new file mode 100644 index 00000000..5d8d6d56 --- /dev/null +++ b/doxygen/group__Methods-Weights-Correlations-FLOPS.js @@ -0,0 +1,23 @@ +var group__Methods_Weights_Correlations_FLOPS = +[ + [ "calculate_load", "group__Methods-Weights-Correlations-FLOPS.html#ga45e89e2bae02d180af523a88d5c3ed5a", null ], + [ "determine_fuselage_chord", "group__Methods-Weights-Correlations-FLOPS.html#gae5e92af22c52818904fb68c652eb7482", null ], + [ "engine_FLOPS", "group__Methods-Weights-Correlations-FLOPS.html#ga7d31b324a51706581de339de69d319dc", null ], + [ "find_sweep", "group__Methods-Weights-Correlations-FLOPS.html#gaab1f3007dc6d603ab4e4dfd772e95e88", null ], + [ "fuel_system_FLOPS", "group__Methods-Weights-Correlations-FLOPS.html#gaf55c761bb3df60b24b03399c8f973443", null ], + [ "fuselage_weight_FLOPS", "group__Methods-Weights-Correlations-FLOPS.html#ga0f045b0dd9253ca64a8465cfcb52d3d0", null ], + [ "generate_int_stations", "group__Methods-Weights-Correlations-FLOPS.html#ga3960adc19bb2b3fd1d95d5c2a262f28d", null ], + [ "generate_wing_stations", "group__Methods-Weights-Correlations-FLOPS.html#gad540171d902bb2006bcf718f8ba0915f", null ], + [ "get_spanwise_engine", "group__Methods-Weights-Correlations-FLOPS.html#ga27340489f45a5fe354df4955da035b3c", null ], + [ "landing_gear_FLOPS", "group__Methods-Weights-Correlations-FLOPS.html#gafcd2b158260d211ab8f71a855cfb88b3", null ], + [ "misc_engine_FLOPS", "group__Methods-Weights-Correlations-FLOPS.html#ga8292d50e76d24702d6f860574685a7de", null ], + [ "nacelle_FLOPS", "group__Methods-Weights-Correlations-FLOPS.html#ga9997a6596142a993040d6c075d69cf2e", null ], + [ "operating_items_FLOPS", "group__Methods-Weights-Correlations-FLOPS.html#ga5971789103f9526da2292712e9a96041", null ], + [ "payload_FLOPS", "group__Methods-Weights-Correlations-FLOPS.html#gaac8657c6b2302d63271f4343e1785e48", null ], + [ "systems_FLOPS", "group__Methods-Weights-Correlations-FLOPS.html#ga6bd0b3e7be259c0d569ead086a28530f", null ], + [ "tail_vertical_FLOPS", "group__Methods-Weights-Correlations-FLOPS.html#ga875d7b8cdc23ab9fffb346b818a16b25", null ], + [ "thrust_reverser_FLOPS", "group__Methods-Weights-Correlations-FLOPS.html#ga8f6207eea61c7a97d0117219c518432d", null ], + [ "total_prop_flops", "group__Methods-Weights-Correlations-FLOPS.html#gad144579be3a369ae5428260c806efefe", null ], + [ "wing_weight_constants_FLOPS", "group__Methods-Weights-Correlations-FLOPS.html#gaf1316a510353f1a424dddfe49596df34", null ], + [ "wing_weight_FLOPS", "group__Methods-Weights-Correlations-FLOPS.html#gaa9d2a982638ffa982e761a86295ad4ca", null ] +]; \ No newline at end of file diff --git a/doxygen/group__Methods-Weights-Correlations-General__Aviation.html b/doxygen/group__Methods-Weights-Correlations-General__Aviation.html index 747522b4..df4f5c69 100644 --- a/doxygen/group__Methods-Weights-Correlations-General__Aviation.html +++ b/doxygen/group__Methods-Weights-Correlations-General__Aviation.html @@ -1,9 +1,9 @@ - + - + SUAVE: Generational @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@

- +
@@ -73,7 +78,9 @@

@@ -161,14 +168,14 @@

Generated by - doxygen 1.8.14 + doxygen 1.8.15

diff --git a/doxygen/group__Methods-Weights-Correlations-Human__Powered.html b/doxygen/group__Methods-Weights-Correlations-Human__Powered.html index 5eb38cd3..593dabe5 100644 --- a/doxygen/group__Methods-Weights-Correlations-Human__Powered.html +++ b/doxygen/group__Methods-Weights-Correlations-Human__Powered.html @@ -1,9 +1,9 @@ - + - + SUAVE: Human_Powered @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@
- +
@@ -73,7 +78,9 @@

@@ -103,8 +110,8 @@ - - + + @@ -118,8 +125,8 @@

Detailed Description

Provides structural weight correlations for a human-powered aircraft; applicable to solar-UAVs.

Function Documentation

- -

◆ empty()

+ +

◆ empty()

- + + + + + + + + + + +

Functions

def SUAVE.Methods.Weights.Correlations.Human_Powered.empty.empty (vehicle)
 
def SUAVE.Methods.Weights.Correlations.Human_Powered.empty.empty (vehicle, settings=None)
 
def SUAVE.Methods.Weights.Correlations.Human_Powered.fuselage.fuselage (Sts, qm, Ltb)
 fuselage.py More...
 
(  vehicle)vehicle,
 settings = None 
)
diff --git a/doxygen/group__Methods-Weights-Correlations-Human__Powered.js b/doxygen/group__Methods-Weights-Correlations-Human__Powered.js index 5ec660ac..51ee3d12 100644 --- a/doxygen/group__Methods-Weights-Correlations-Human__Powered.js +++ b/doxygen/group__Methods-Weights-Correlations-Human__Powered.js @@ -1,6 +1,6 @@ var group__Methods_Weights_Correlations_Human__Powered = [ - [ "empty", "group__Methods-Weights-Correlations-Human__Powered.html#gaaecbf938c83082c10701c8c5b358d9f3", null ], + [ "empty", "group__Methods-Weights-Correlations-Human__Powered.html#ga1015918f8151416814ce2ea6cd7a9a60", null ], [ "fuselage", "group__Methods-Weights-Correlations-Human__Powered.html#gaeec5ba9b1b81becbceda022ba62a5439", null ], [ "tail", "group__Methods-Weights-Correlations-Human__Powered.html#gac77c04f3e7f673c8dcb0414cdf63a415", null ], [ "wing", "group__Methods-Weights-Correlations-Human__Powered.html#ga44dc2d0fd1cde113b20de336869fd6c7", null ] diff --git a/doxygen/group__Methods-Weights-Correlations-Propulsion.html b/doxygen/group__Methods-Weights-Correlations-Propulsion.html index 2ff7e50f..3ecb5590 100644 --- a/doxygen/group__Methods-Weights-Correlations-Propulsion.html +++ b/doxygen/group__Methods-Weights-Correlations-Propulsion.html @@ -1,9 +1,9 @@ - + - + SUAVE: Propulsion @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@
- +

@@ -73,7 +78,9 @@
@@ -110,13 +117,14 @@ def SUAVE.Methods.Weights.Correlations.Propulsion.engine_piston.engine_piston (max_power, kwt2=5.22, xwt=.780)   def SUAVE.Methods.Weights.Correlations.Propulsion.hts_motor.hts_motor (max_power) - hts_motor.py More...
  def SUAVE.Methods.Weights.Correlations.Propulsion.integrated_propulsion.integrated_propulsion (engine_jet, num_eng, engine_wt_factor=1.6)  integrated_propulsion.py More...
  def SUAVE.Methods.Weights.Correlations.Propulsion.integrated_propulsion_general_aviation.integrated_propulsion_general_aviation (engine_piston, num_eng, engine_wt_factor=2.575, engine_wt_exp=.922)   +def SUAVE.Methods.Weights.Correlations.Propulsion.nasa_motor.nasa_motor (torque, kwt2=.3928, xwt=.8587) + 

Detailed Description

Contains some methods for calculating different propulsion system weights.

@@ -169,7 +177,7 @@

- -

hts_motor.py

-

Created: Jan 2014, M. Vegh, Modified: Feb 2014, A. Wendorff Feb 2016, E. Botero

Calculate the weight of a high temperature superconducting motor
+
Calculate the weight of a high temperature superconducting motor
 
    Assumptions:
        calculated from fit of commercial available motors
        
    Source: [10] Snyder, C., Berton, J., Brown, G. et all
        'Propulsion Investigation for Zero and Near-Zero Emissions Aircraft,' NASA STI Program,
-       NASA Glenn,  2009.012
+       NASA Glenn,  2009.012. page 12
        
    Inputs:
        max_power- maximum power the motor can deliver safely   [Watts]
@@ -400,6 +406,59 @@ 

+

◆ nasa_motor()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Weights.Correlations.Propulsion.nasa_motor.nasa_motor ( torque,
 kwt2 = .3928,
 xwt = .8587 
)
+
+
Calculate the weight of an air-cooled motor    
+weight correlation; weight=kwt2*(max_power**xwt)
+    
+Assumptions:
+        calculated from fit of high power-to-weight motors
+        
+Source: NDARC Theory Manual, Page 213
+https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20170011656.pdf
+
+Inputs:
+        torque- maximum torque the motor can deliver safely      [N-m]
+        kwt2
+        xwt
+        
+Outputs:
+        mass- mass of the motor                                [kilograms]
+    
+Properties Used:
+        N/A
+
+
+

@@ -407,7 +466,7 @@

Generated by - doxygen 1.8.14 + doxygen 1.8.15

diff --git a/doxygen/group__Methods-Weights-Correlations-Propulsion.js b/doxygen/group__Methods-Weights-Correlations-Propulsion.js index 889fb4fa..0d549b57 100644 --- a/doxygen/group__Methods-Weights-Correlations-Propulsion.js +++ b/doxygen/group__Methods-Weights-Correlations-Propulsion.js @@ -5,5 +5,6 @@ var group__Methods_Weights_Correlations_Propulsion = [ "engine_piston", "group__Methods-Weights-Correlations-Propulsion.html#ga219a67f302a34af561324cdb77799c7d", null ], [ "hts_motor", "group__Methods-Weights-Correlations-Propulsion.html#ga4910a296a5c344da2cae7b81c05895c1", null ], [ "integrated_propulsion", "group__Methods-Weights-Correlations-Propulsion.html#gaa6dd0b5a3adb2b4948101434f55a197a", null ], - [ "integrated_propulsion_general_aviation", "group__Methods-Weights-Correlations-Propulsion.html#gaec6d717c50436eda2cf455782f446a9f", null ] + [ "integrated_propulsion_general_aviation", "group__Methods-Weights-Correlations-Propulsion.html#gaec6d717c50436eda2cf455782f446a9f", null ], + [ "nasa_motor", "group__Methods-Weights-Correlations-Propulsion.html#gacfa3e8be417d0f1bd08a7c9e52c8aa60", null ] ]; \ No newline at end of file diff --git a/doxygen/group__Methods-Weights-Correlations-Raymer.html b/doxygen/group__Methods-Weights-Correlations-Raymer.html new file mode 100644 index 00000000..34a74f5c --- /dev/null +++ b/doxygen/group__Methods-Weights-Correlations-Raymer.html @@ -0,0 +1,698 @@ + + + + + + + +SUAVE: Methods-Weights-Correlations-Raymer + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
Methods-Weights-Correlations-Raymer
+
+
+ +

Provides structural weight correlations for aircraft components based on the Raymer method. +More...

+ + + + + + + + + + + + + + + + + + + + + + +

+Functions

def SUAVE.Methods.Weights.Correlations.Raymer.fuselage.fuselage_weight_Raymer (vehicle, fuse, settings)
 
def SUAVE.Methods.Weights.Correlations.Raymer.landing_gear.landing_gear_Raymer (vehicle)
 
def SUAVE.Methods.Weights.Correlations.Raymer.prop_system.total_prop_Raymer (vehicle, prop)
 
def SUAVE.Methods.Weights.Correlations.Raymer.prop_system.nacelle_Raymer (vehicle, WENG)
 
def SUAVE.Methods.Weights.Correlations.Raymer.prop_system.misc_engine_Raymer (vehicle, prop, WENG)
 
def SUAVE.Methods.Weights.Correlations.Raymer.prop_system.fuel_system_Raymer (vehicle, NENG)
 
def SUAVE.Methods.Weights.Correlations.Raymer.systems.systems_Raymer (vehicle)
 
def SUAVE.Methods.Weights.Correlations.Raymer.tail.tail_vertical_Raymer (vehicle, wing)
 
def SUAVE.Methods.Weights.Correlations.Raymer.tail.tail_horizontal_Raymer (vehicle, wing, elevator_fraction=0.4)
 
def SUAVE.Methods.Weights.Correlations.Raymer.wing_main_raymer.wing_main_raymer (vehicle, wing)
 
+

Detailed Description

+

Provides structural weight correlations for aircraft components based on the Raymer method.

+

Function Documentation

+ +

◆ fuel_system_Raymer()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Weights.Correlations.Raymer.prop_system.fuel_system_Raymer ( vehicle,
 NENG 
)
+
+
Calculates the weight of the fuel system based on the Raymer method
+    Assumptions:
+
+    Source:
+        Aircraft Design: A Conceptual Approach
+
+    Inputs:
+        vehicle - data dictionary with vehicle properties                   [dimensionless]
+            -.design_mach_number: design mach number
+            -.mass_properties.max_zero_fuel: maximum zero fuel weight   [kg]
+
+    Outputs:
+        WFSYS: Fuel system weight                                       [kg]
+
+    Properties Used:
+        N/A
+
+
+
+ +

◆ fuselage_weight_Raymer()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Weights.Correlations.Raymer.fuselage.fuselage_weight_Raymer ( vehicle,
 fuse,
 settings 
)
+
+
Calculate the weight of the fuselage of a transport aircraft based on the Raymer method
+
+    Assumptions:
+        No fuselage mounted landing gear
+        1 cargo door
+
+    Source:
+        Aircraft Design: A Conceptual Approach (2nd edition)
+
+    Inputs:
+        vehicle - data dictionary with vehicle properties                   [dimensionless]
+            -.mass_properties.max_takeoff: MTOW                             [kg]
+            -.envelope.ultimate_load: ultimate load factor (default: 3.75)
+            -.wings['main_wing']: data dictionary with main wing properties
+                -.taper: wing taper ratio
+                -.sweeps.quarter_chord: quarter chord sweep                 [rad]
+        fuse - data dictionary with specific fuselage properties            [dimensionless]
+            -.lenghts.total: total length                                   [m]
+            -.width: fuselage width                                         [m]
+            -.heights.maximum: maximum height of the fuselage               [m]
+
+    Outputs:
+        weight_fuse - weight of the fuselage                                [kilograms]
+
+    Properties Used:
+        N/A
+
+
+
+ +

◆ landing_gear_Raymer()

+ +
+
+ + + + + + + + +
def SUAVE.Methods.Weights.Correlations.Raymer.landing_gear.landing_gear_Raymer ( vehicle)
+
+
Calculate the weight of the landing gear of a transport aircraft based on the Raymer method
+
+    Assumptions:
+        No fuselage mounted landing gear
+        1 cargo door
+        gear load factor = 3
+        number of main gear shock struts = 2
+        stall speed = 51 kts as defined by FAA
+        Not a reciprocating engine
+
+    Source:
+        Aircraft Design: A Conceptual Approach (2nd edition)
+
+    Inputs:
+        vehicle - data dictionary with vehicle properties                   [dimensionless]
+            -.design_range: design range of aircraft                        [m]
+            -.mass_properties.max_takeoff: MTOW                             [kg]
+            -.systems.accessories: type of aircraft (short-range, commuter
+                                                    medium-range, long-range,
+                                                    sst, cargo)
+            -.landing_gear.main_strut_length: main strut length              [m]
+            -.landing_gear.main_wheels: number of wheels on main landing gear
+            -.landing_gear.nose_strut_length: nose strut length              [m]
+            -.landing_gear.nose_wheels: number of wheels on nose landing gear
+
+        fuse - data dictionary with specific fuselage properties            [dimensionless]
+
+    Outputs:
+        weight_fuse - weight of the fuselage                                [kilograms]
+
+    Properties Used:
+        N/A
+
+
+
+ +

◆ misc_engine_Raymer()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Weights.Correlations.Raymer.prop_system.misc_engine_Raymer ( vehicle,
 prop,
 WENG 
)
+
+
Calculates the miscellaneous engine weight based on the Raymer method, electrical control system weight
+    and starter engine weight
+    Assumptions:
+
+    Source:
+        Aircraft Design: A Conceptual Approach
+
+    Inputs:
+        vehicle - data dictionary with vehicle properties                   [dimensionless]
+            -.fuselages['fuselage'].lengths.total: length of fuselage   [m]
+        prop    - data dictionary for the specific network that is being estimated [dimensionless]
+            -.number_of_engines: number of engines
+
+    Outputs:
+        WEC: electrical engine control system weight                    [kg]
+        WSTART: starter engine weight                                   [kg]
+
+    Properties Used:
+        N/A
+
+
+
+ +

◆ nacelle_Raymer()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Weights.Correlations.Raymer.prop_system.nacelle_Raymer ( vehicle,
 WENG 
)
+
+
Calculates the nacelle weight based on the Raymer method
+    Assumptions:
+        1) All nacelles are identical
+        2) The number of nacelles is the same as the number of engines 
+    Source:
+        Aircraft Design: A Conceptual Approach (2nd edition)
+
+    Inputs:
+        vehicle - data dictionary with vehicle properties                           [dimensionless]
+            -.ultimate_load: ultimate load factor of aircraft
+        nacelle  - data dictionary for the specific nacelle that is being estimated [dimensionless]
+            -lenght: total length of engine                                         [m]
+            -diameter: diameter of nacelle                                          [m]
+        WENG    - dry engine weight                                                 [kg]
+
+
+    Outputs:
+        WNAC: nacelle weight                                                        [kg]
+
+    Properties Used:
+        N/A
+
+
+
+ +

◆ systems_Raymer()

+ +
+
+ + + + + + + + +
def SUAVE.Methods.Weights.Correlations.Raymer.systems.systems_Raymer ( vehicle)
+
+
Calculates the system weight based on the Raymer method
+
+    Assumptions:
+        Number of flight control systems = 4
+        Max APU weight = 70 lbs
+        Assuming not a reciprocating engine and not a turboprop
+        System Electrical Rating: 60 kv · A (typically 40-60 for transports, 110-160 for fighters & bombers)
+        Uninstalled Avionics weight: 1400 lb (typically= 800-1400 lb)
+
+    Source:
+        Aircraft Design: A Conceptual Approach (2nd edition)
+
+    Inputs:
+        vehicle - data dictionary with vehicle properties                   [dimensionless]
+            -.networks: data dictionary containing all propulsion properties
+            -.number_of_engines: number of engines
+            -.sealevel_static_thrust: thrust at sea level               [N]
+            -.fuselages['fuselage'].lengths.total: fuselage total length    [meters]
+            -.fuselages['fuselage'].width: fuselage width                   [meters]
+            -.fuselages['fuselage'].heights.maximum: fuselage maximum height[meters]
+            -.mass_properties.max_takeoff: MTOW                             [kilograms]
+            -.design_mach_number: design mach number for cruise flight
+            -.design_range: design range of aircraft                        [nmi]
+            -.passengers: number of passengers in aircraft
+            -.wings['main_wing']: data dictionary with main wing properties
+                -.sweeps.quarter_chord: quarter chord sweep                 [deg]
+                -.areas.reference: wing surface area                        [m^2]
+                -.spans.projected: projected span of wing                   [m]
+                -.flap_ratio: flap surface area over wing surface area
+            -.payload: payload weight of aircraft                           [kg]
+
+    Outputs:
+        output - a data dictionary with fields:
+           wt_flt_ctrl - weight of the flight control system                                [kilograms]
+           wt_apu - weight of the apu                                                       [kilograms]
+           wt_hyd_pnu - weight of the hydraulics and pneumatics                             [kilograms]
+           wt_instruments - weight of the instruments and navigational equipment            [kilograms]
+           wt_avionics - weight of the avionics                                             [kilograms]
+           wt_elec - weight of the electrical items                                         [kilograms]
+           wt_ac - weight of the air conditioning and anti-ice system                       [kilograms]
+           wt_furnish - weight of the furnishings in the fuselage                           [kilograms]
+           wt_anti_ice - weight of anti-ice system                                          [kilograms]
+
+    Properties Used:
+        N/A
+
+
+
+ +

◆ tail_horizontal_Raymer()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Weights.Correlations.Raymer.tail.tail_horizontal_Raymer ( vehicle,
 wing,
 elevator_fraction = 0.4 
)
+
+
Calculates horizontal tail weight based on Raymer method
+
+    Assumptions:
+        If all-moving horizontal tail, change Kuht to 1.143
+    Source:
+        Aircraft Design: A Conceptual Approach
+
+    Inputs:
+        vehicle - data dictionary with vehicle properties                    [dimensionless]
+            -.mass_properties.max_takeoff: MTOW                             [kilograms]
+            -.envelope.ultimate_load: ultimate load factor (default: 3.75)
+            -.wings['main_wing']: data dictionary with properties of main wing
+                -.aerodynamic_center: aerodynamic center as measured from root leading edge
+                -.origin: root of main wing as measured from nose of aircraft
+            -.fuselages['fuselage'].width: width of the fuselage
+        wing    - data dictionary with specific tail properties              [dimensionless]
+            -.areas.reference: tail surface area                            [m^2}
+            -.origin: location of tail measured from nose
+            -.aerodynamic_center: location of ac measured from leading edge
+            -.sweeps.quarter_chord: quarter chord sweep of tail             [rad]
+            -.thickness_to_chord: t/c of tail
+            -.span.projected: project span of tail                          [m]
+            -.aspect_ratio: aspect ratio of wing
+        elevator_fraction - fraction of horizontal tail for elevator = 0.4
+
+    Outputs:
+        tail_weight: horizontal tail weight                                [kilograms]
+
+    Properties Used:
+        N/A
+
+
+
+ +

◆ tail_vertical_Raymer()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Weights.Correlations.Raymer.tail.tail_vertical_Raymer ( vehicle,
 wing 
)
+
+
Calculates vertical tail weight based on Raymer method
+
+    Assumptions:
+
+    Source:
+        Aircraft Design: A Conceptual Approach (2nd edition)
+
+    Inputs:
+        vehicle - data dictionary with vehicle properties                    [dimensionless]
+            -.mass_properties.max_takeoff: MTOW                             [kilograms]
+            -.envelope.ultimate_load: ultimate load factor (default: 3.75)
+            -.wings['main_wing']: data dictionary with properties of main wing
+                -.aerodynamic_center: aerodynamic center as measured from root leading edge
+                -.origin: root of main wing as measured from nose of aircraft
+        wing    - data dictionary with specific tail properties              [dimensionless]
+            -.areas.reference: tail surface area                            [m^2}
+            -.origin: location of tail measured from nose
+            -.aerodynamic_center: location of ac measured from leading edge
+            -.sweeps.quarter_chord: quarter chord sweep of tail             [rad]
+            -.thickness_to_chord: t/c of tail
+
+    Outputs:
+          tail_weight: vertical tail weight                                [kilograms]
+
+    Properties Used:
+        N/A
+
+
+
+ +

◆ total_prop_Raymer()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Weights.Correlations.Raymer.prop_system.total_prop_Raymer ( vehicle,
 prop 
)
+
+
Calculate the weight of propulsion system using Raymer method, including:
+    - fuel system weight
+    - thurst reversers weight
+    - electrical system weight
+    - starter engine weight
+    - nacelle weight
+    - cargo containers
+    The dry engine weight comes from the FLOPS relations since it is not listed in Raymer
+
+    Assumptions:
+
+    Source:
+        Aircraft Design: A Conceptual Approach
+
+    Inputs:
+        vehicle - data dictionary with vehicle properties                   [dimensionless]
+        prop    - data dictionary for the specific network that is being estimated [dimensionless]
+
+    Outputs:
+        output - data dictionary with weights                               [kilograms]
+                - output.wt_prop: total propulsive system weight
+                - output.wt_thrust_reverser: thurst reverser weight
+                - output.starter: starter engine weight
+                - output.wt_engine_controls: engine controls weight
+                - output.fuel_system: fuel system weight
+                - output.nacelle: nacelle weight
+                - output.wt_eng: dry engine weight
+
+    Properties Used:
+        N/A
+
+
+
+ +

◆ wing_main_raymer()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Methods.Weights.Correlations.Raymer.wing_main_raymer.wing_main_raymer ( vehicle,
 wing 
)
+
+
Calculate the wing weight of the aircraft based the Raymer method
+
+Assumptions:
+
+Source:
+    Aircraft Design: A Conceptual Approach (2nd edition)
+
+Inputs:
+    vehicle - data dictionary with vehicle properties                   [dimensionless]
+            -.mass_properties.max_takeoff: MTOW                         [kg]
+            -.envelope.ultimate_load: ultimate loading factor
+            -.systems.accessories: type of aircraft (short-range, commuter
+                                                    medium-range, long-range,
+                                                    sst, cargo)
+    wing    - data dictionary with specific wing properties             [dimensionless]
+            -.taper: taper ratio
+            -.sweeps.quarter_chord: quarter chord sweep angle           [deg]
+            -.thickness_to_chord: thickness to chord
+            -.aspect_ratio: aspect ratio of wing
+            -.areas.reference: wing surface area                        [m^2]
+
+Outputs:
+    weight - weight of the wing                  [kilograms]
+
+
+Properties Used:
+    N/A
+
+
+
+
+
+ + + + diff --git a/doxygen/group__Methods-Weights-Correlations-Raymer.js b/doxygen/group__Methods-Weights-Correlations-Raymer.js new file mode 100644 index 00000000..122297b3 --- /dev/null +++ b/doxygen/group__Methods-Weights-Correlations-Raymer.js @@ -0,0 +1,13 @@ +var group__Methods_Weights_Correlations_Raymer = +[ + [ "fuel_system_Raymer", "group__Methods-Weights-Correlations-Raymer.html#ga053885dd30aef586ce7af90ca67b7b51", null ], + [ "fuselage_weight_Raymer", "group__Methods-Weights-Correlations-Raymer.html#gaf37972a0ce6855b3d1243b9443025c85", null ], + [ "landing_gear_Raymer", "group__Methods-Weights-Correlations-Raymer.html#ga0319d2ceae77def47cc5a4f49d83521c", null ], + [ "misc_engine_Raymer", "group__Methods-Weights-Correlations-Raymer.html#ga14180f091ee265a9c967eeeaf8b28787", null ], + [ "nacelle_Raymer", "group__Methods-Weights-Correlations-Raymer.html#gaddfbc8ef52245b3332f4459387c889d6", null ], + [ "systems_Raymer", "group__Methods-Weights-Correlations-Raymer.html#ga06ff7c62ead0f5be90c48474ab21b548", null ], + [ "tail_horizontal_Raymer", "group__Methods-Weights-Correlations-Raymer.html#ga2c8d274dc8ba663bd2f317fd61e3ee2d", null ], + [ "tail_vertical_Raymer", "group__Methods-Weights-Correlations-Raymer.html#ga43a3a37ad92a5ef4a6839ff34f7b818e", null ], + [ "total_prop_Raymer", "group__Methods-Weights-Correlations-Raymer.html#ga32f664d11dc37db355fee9f37d74d9f7", null ], + [ "wing_main_raymer", "group__Methods-Weights-Correlations-Raymer.html#ga445963c5573f2957112c9d5a1c49b7ce", null ] +]; \ No newline at end of file diff --git a/doxygen/group__Methods-Weights-Correlations-Tube__Wing.html b/doxygen/group__Methods-Weights-Correlations-Tube__Wing.html index fcbcbf67..1ab8b2f1 100644 --- a/doxygen/group__Methods-Weights-Correlations-Tube__Wing.html +++ b/doxygen/group__Methods-Weights-Correlations-Tube__Wing.html @@ -1,9 +1,9 @@ - + - + SUAVE: Tube_Wing @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@

- +
@@ -73,7 +78,9 @@

@@ -103,252 +110,33 @@ - - - - - - - - - - + + + + + +

Functions

def SUAVE.Methods.Weights.Correlations.Tube_Wing.empty.empty (vehicle)
 
def SUAVE.Methods.Weights.Correlations.Tube_Wing.systems.systems (num_seats, ctrl_type, S_h, S_v, S_gross_w, ac_type)
 
def SUAVE.Methods.Weights.Correlations.Tube_Wing.tail_horizontal.tail_horizontal (b_h, sweep_h, Nult, S_h, TOW, mac_w, mac_h, l_w2h, t_c_h, exposed)
 
def SUAVE.Methods.Weights.Correlations.Tube_Wing.tail_vertical.tail_vertical (S_v, Nult, b_v, TOW, t_c_v, sweep_v, S_gross_w, t_tail, rudder_fraction=0.25)
 
def SUAVE.Methods.Weights.Correlations.Tube_Wing.tube.tube (S_fus, diff_p_fus, w_fus, h_fus, l_fus, Nlim, wt_zf, wt_wing, wt_propulsion, wing_c_r)
 
def SUAVE.Methods.Weights.Correlations.Transport.tail_horizontal.tail_horizontal (vehicle, wing)
 
def SUAVE.Methods.Weights.Correlations.Transport.tail_vertical.tail_vertical (vehicle, wing, rudder_fraction=0.25)
 
def SUAVE.Methods.Weights.Correlations.Transport.tube.tube (vehicle, fuse, wt_wing, wt_propulsion)
 

Detailed Description

Provides structural weight correlations for a tube and wing aircraft.

Function Documentation

- -

◆ empty()

- -
-
- - - - - - - - -
def SUAVE.Methods.Weights.Correlations.Tube_Wing.empty.empty ( vehicle)
-
-
This is for a standard Tube and Wing aircraft configuration.        
-
-Assumptions:
-    calculated aircraft weight from correlations created per component of historical aircraft
-
-Source:
-    N/A
-    
-Inputs:
-  engine - a data dictionary with the fields:                    
-      thrust_sls - sea level static thrust of a single engine                [Newtons]
-
-  wing - a data dictionary with the fields:
-      gross_area - wing gross area                                           [meters**2]
-      span - span of the wing                                                [meters]
-      taper - taper ratio of the wing                                        [dimensionless]
-      t_c - thickness-to-chord ratio of the wing                             [dimensionless]
-      sweep - sweep angle of the wing                                        [radians]
-      mac - mean aerodynamic chord of the wing                               [meters]
-      r_c - wing root chord                                                  [meters]
-
-  aircraft - a data dictionary with the fields:                    
-      Nult - ultimate load of the aircraft                                   [dimensionless]
-      Nlim - limit load factor at zero fuel weight of the aircraft           [dimensionless]
-      TOW - maximum takeoff weight of the aircraft                           [kilograms]
-      zfw - maximum zero fuel weight of the aircraft                         [kilograms]
-      num_eng - number of engines on the aircraft                            [dimensionless]
-      num_pax - number of passengers on the aircraft                         [dimensionless]
-      wt_cargo - weight of the bulk cargo being carried on the aircraft      [kilograms]
-      num_seats - number of seats installed on the aircraft                  [dimensionless]
-      ctrl - specifies if the control system is "fully powered", "partially powered", or not powered [dimensionless]
-      ac - determines type of instruments, electronics, and operating items based on types: 
-          "short-range", "medium-range", "long-range", "business", "cargo", "commuter", "sst"        [dimensionless]
-      w2h - tail length (distance from the airplane c.g. to the horizontal tail aerodynamic center)  [meters]
-
-  fuselage - a data dictionary with the fields:
-      area - fuselage wetted area                                            [meters**2]
-      diff_p - Maximum fuselage pressure differential                        [Pascal]
-      width - width of the fuselage                                          [meters]
-      height - height of the fuselage                                        [meters]
-      length - length of the fuselage                                        [meters]                     
-
-  horizontal
-      area - area of the horizontal tail                                     [meters**2]
-      span - span of the horizontal tail                                     [meters]
-      sweep - sweep of the horizontal tail                                   [radians]
-      mac - mean aerodynamic chord of the horizontal tail                    [meters]
-      t_c - thickness-to-chord ratio of the horizontal tail                  [dimensionless]
-      exposed - exposed area ratio for the horizontal tail                   [dimensionless]
-
-  vertical
-      area - area of the vertical tail                                       [meters**2]
-      span - sweight = weight * Units.lbpan of the vertical                  [meters]
-      t_c - thickness-to-chord ratio of the vertical tail                    [dimensionless]
-      sweep - sweep angle of the vertical tail                               [radians]
-      t_tail - factor to determine if aircraft has a t-tail, "yes"           [dimensionless]
-
-Outputs:
-    output - a data dictionary with fields:
-        wt_payload - weight of the passengers plus baggage and paid cargo    [kilograms]
-        wt_pax - weight of all the passengers                                [kilogram]
-        wt_bag - weight of all the baggage                                   [kilogram]
-        wt_fuel - weight of the fuel carried                                 [kilogram]
-        wt_empty - operating empty weight of the aircraft                    [kilograms]
- 
-Properties Used:
-    N/A
-
-
-
- -

◆ systems()

+ +

◆ tail_horizontal()

- + - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
def SUAVE.Methods.Weights.Correlations.Tube_Wing.systems.systems def SUAVE.Methods.Weights.Correlations.Transport.tail_horizontal.tail_horizontal (  num_seats,
 ctrl_type,
 S_h,
 S_v,
 S_gross_w,
 ac_type 
)
-
-
Calculate the weight of the different engine systems on the aircraft
-
-Assumptions:
-    numbers based on FAA regulations and correlations from previous aircraft 
-
-Source: 
-    N/A
-            
-   Inputs:
-   num_seats - total number of seats on the aircraft                                                   [dimensionless]
-   ctrl_type - specifies if the control system is fully power, partially powered, or not powered       [dimensionless]
-   S_h - area of the horizontal tail                                                                   [meters**2]
-   S_v - area of the vertical tail                                                                     [meters**2]
-   S_gross_w - area of the wing                                                                        [meters**2]
-   ac_type - determines type of instruments, electronics, and operating items based on type of vehicle [dimensionless]
-   
-   Outputs:
-   output - a data dictionary with fields:
-       wt_flt_ctrl - weight of the flight control system                                               [kilograms]
-       wt_apu - weight of the apu                                                                      [kilograms]
-       wt_hyd_pnu - weight of the hydraulics and pneumatics                                            [kilograms]
-       wt_instruments - weight of the instruments and navigational equipment                           [kilograms]
-       wt_avionics - weight of the avionics                                                            [kilograms]
-       wt_opitems - weight of the optional items based on the type of aircraft                         [kilograms]
-       wt_elec - weight of the electrical items                                                        [kilograms]
-       wt_ac - weight of the air conditioning and anti-ice system                                      [kilograms]
-       wt_furnish - weight of the furnishings in the fuselage                                          [kilograms]
-   
-Properties Used:
-    N/A
-
-
-
- -

◆ tail_horizontal()

- -
-
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - + - + @@ -367,16 +155,16 @@

-

◆ tail_vertical()

+ +

◆ tail_vertical()

def SUAVE.Methods.Weights.Correlations.Tube_Wing.tail_horizontal.tail_horizontal ( b_h,
 sweep_h,
 Nult,
 S_h,
 TOW,
 mac_w,
 mac_h,
 l_w2h,
 t_c_h, vehicle,
 exposed wing 
- + - - - - - - - - - - - - - - - - - - - + - - - - - - - - - - - - - - - - - - - + @@ -465,13 +217,13 @@

-

◆ tube()

+ +

◆ tube()

def SUAVE.Methods.Weights.Correlations.Tube_Wing.tail_vertical.tail_vertical def SUAVE.Methods.Weights.Correlations.Transport.tail_vertical.tail_vertical (  S_v,
 Nult,
 b_v,
 TOW, vehicle,
 t_c_v,
 sweep_v,
 S_gross_w,
 t_tail, wing,
- + - + - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - + @@ -542,13 +264,7 @@

- - - - - - - + @@ -566,19 +282,19 @@

Generated by - doxygen 1.8.14 + doxygen 1.8.15 diff --git a/doxygen/group__Methods-Weights-Correlations-Tube__Wing.js b/doxygen/group__Methods-Weights-Correlations-Tube__Wing.js index 4f17b1db..47e36991 100644 --- a/doxygen/group__Methods-Weights-Correlations-Tube__Wing.js +++ b/doxygen/group__Methods-Weights-Correlations-Tube__Wing.js @@ -1,8 +1,6 @@ var group__Methods_Weights_Correlations_Tube__Wing = [ - [ "empty", "group__Methods-Weights-Correlations-Tube__Wing.html#ga88d820445757e8a0b404bd4a927987af", null ], - [ "systems", "group__Methods-Weights-Correlations-Tube__Wing.html#ga30ab082cdcf65e2353337185bf791f18", null ], - [ "tail_horizontal", "group__Methods-Weights-Correlations-Tube__Wing.html#ga01911fdc8a489264f6085fc867f64a85", null ], - [ "tail_vertical", "group__Methods-Weights-Correlations-Tube__Wing.html#ga76320919117c9debed0edc4395fe7e9b", null ], - [ "tube", "group__Methods-Weights-Correlations-Tube__Wing.html#gafd8256895c20e1a5343c362d922aa8c1", null ] + [ "tail_horizontal", "group__Methods-Weights-Correlations-Tube__Wing.html#ga3e66149cee2665f85796c901f2c557ae", null ], + [ "tail_vertical", "group__Methods-Weights-Correlations-Tube__Wing.html#ga5be3497f4f2be96f18482d4ce35ea3db", null ], + [ "tube", "group__Methods-Weights-Correlations-Tube__Wing.html#gacf1fd2ea10ed5077247c579b0ad2a7de", null ] ]; \ No newline at end of file diff --git a/doxygen/group__Methods-Weights-Correlations-UAV.html b/doxygen/group__Methods-Weights-Correlations-UAV.html index 9df03b3e..cda1af28 100644 --- a/doxygen/group__Methods-Weights-Correlations-UAV.html +++ b/doxygen/group__Methods-Weights-Correlations-UAV.html @@ -1,9 +1,9 @@ - + - + SUAVE: UAV @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@
def SUAVE.Methods.Weights.Correlations.Tube_Wing.tube.tube def SUAVE.Methods.Weights.Correlations.Transport.tube.tube (  S_fus, vehicle,
 diff_p_fus,
 w_fus,
 h_fus,
 l_fus,
 Nlim,
 wt_zf, fuse,
 wt_propulsion,
 wing_c_r wt_propulsion 
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -103,14 +110,14 @@ - - + +

Functions

def SUAVE.Methods.Weights.Correlations.UAV.empty.empty (vehicle)
 
def SUAVE.Methods.Weights.Correlations.UAV.empty.empty (vehicle, settings=None)
 

Detailed Description

Provides structural weight correlations for UAVs.

Function Documentation

- -

◆ empty()

+ +

◆ empty()

diff --git a/doxygen/group__Methods-Weights-Correlations-UAV.js b/doxygen/group__Methods-Weights-Correlations-UAV.js index 3cd6894a..37e99e9c 100644 --- a/doxygen/group__Methods-Weights-Correlations-UAV.js +++ b/doxygen/group__Methods-Weights-Correlations-UAV.js @@ -1,4 +1,4 @@ var group__Methods_Weights_Correlations_UAV = [ - [ "empty", "group__Methods-Weights-Correlations-UAV.html#gacdd594163b3b6ae3e879aa060413000e", null ] + [ "empty", "group__Methods-Weights-Correlations-UAV.html#ga40ad328bc90982de90fe65fd9778b1a9", null ] ]; \ No newline at end of file diff --git a/doxygen/group__Methods-Weights-Correlations.html b/doxygen/group__Methods-Weights-Correlations.html index 617a25d0..6d9c92dc 100644 --- a/doxygen/group__Methods-Weights-Correlations.html +++ b/doxygen/group__Methods-Weights-Correlations.html @@ -1,9 +1,9 @@ - + - + SUAVE: Correlations @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@
- +
@@ -73,7 +78,9 @@
@@ -109,6 +116,9 @@  Common  Provides structural weight correlations for aircraft components applicable to all aircraft configurations.
  + Methods-Weights-Correlations-FLOPS + Provides structural weight correlations for aircraft components based on the FLOPS method.
+   Generational  Provides structural and component weight correlations for general aviation aircraft.
  @@ -118,6 +128,9 @@  Propulsion  Contains some methods for calculating different propulsion system weights.
  + Methods-Weights-Correlations-Raymer + Provides structural weight correlations for aircraft components based on the Raymer method.
+   Tube_Wing  Provides structural weight correlations for a tube and wing aircraft.
  @@ -134,7 +147,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/group__Methods-Weights-Correlations.js b/doxygen/group__Methods-Weights-Correlations.js index 9aa9347e..28eeb92d 100644 --- a/doxygen/group__Methods-Weights-Correlations.js +++ b/doxygen/group__Methods-Weights-Correlations.js @@ -2,9 +2,11 @@ var group__Methods_Weights_Correlations = [ [ "BWB", "group__Methods-Weights-Correlations-BWB.html", "group__Methods-Weights-Correlations-BWB" ], [ "Common", "group__Methods-Weights-Correlations-Common.html", "group__Methods-Weights-Correlations-Common" ], + [ "Methods-Weights-Correlations-FLOPS", "group__Methods-Weights-Correlations-FLOPS.html", "group__Methods-Weights-Correlations-FLOPS" ], [ "Generational", "group__Methods-Weights-Correlations-General__Aviation.html", "group__Methods-Weights-Correlations-General__Aviation" ], [ "Human_Powered", "group__Methods-Weights-Correlations-Human__Powered.html", "group__Methods-Weights-Correlations-Human__Powered" ], [ "Propulsion", "group__Methods-Weights-Correlations-Propulsion.html", "group__Methods-Weights-Correlations-Propulsion" ], + [ "Methods-Weights-Correlations-Raymer", "group__Methods-Weights-Correlations-Raymer.html", "group__Methods-Weights-Correlations-Raymer" ], [ "Tube_Wing", "group__Methods-Weights-Correlations-Tube__Wing.html", "group__Methods-Weights-Correlations-Tube__Wing" ], [ "UAV", "group__Methods-Weights-Correlations-UAV.html", "group__Methods-Weights-Correlations-UAV" ] ]; \ No newline at end of file diff --git a/doxygen/group__Methods-Weights.html b/doxygen/group__Methods-Weights.html index 2661d12d..03eb74ed 100644 --- a/doxygen/group__Methods-Weights.html +++ b/doxygen/group__Methods-Weights.html @@ -1,9 +1,9 @@ - + - + SUAVE: Weights @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@

- +
@@ -73,7 +78,9 @@
@@ -103,6 +110,9 @@ + + + @@ -116,7 +126,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/group__Methods-Weights.js b/doxygen/group__Methods-Weights.js index 37ef2471..d197bc14 100644 --- a/doxygen/group__Methods-Weights.js +++ b/doxygen/group__Methods-Weights.js @@ -1,4 +1,5 @@ var group__Methods_Weights = [ + [ "Buildups", "group__Methods-Weights-Buildups.html", "group__Methods-Weights-Buildups" ], [ "Correlations", "group__Methods-Weights-Correlations.html", "group__Methods-Weights-Correlations" ] ]; \ No newline at end of file diff --git a/doxygen/group__Methods.html b/doxygen/group__Methods.html index 8b5e1573..588c5543 100644 --- a/doxygen/group__Methods.html +++ b/doxygen/group__Methods.html @@ -1,9 +1,9 @@ - + - +SUAVE: Methods @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ @@ -57,9 +60,11 @@

Modules

 Buildups
 Buildup weight methods provide weight breakdowns for vehicles based on part-by-part sizing.
 
 Correlations
 Correlation methods provide component weight breakdowns for different vehicle configurations based on regressed data.
 
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +

@@ -73,7 +78,9 @@
@@ -110,6 +117,9 @@  Center_of_Gravity  Description.
  + Cooling + Cooling methods contain the functions for cryogenic systems such as Cryocoolers and cryogen cooling.
+   Costs  This contains functions that can compute costs associated with building and operating an aircraft.
  @@ -143,15 +153,15 @@ - - + +

Functions

def SUAVE.Methods.skip.skip (args, kwarg)
 
def SUAVE.Methods.skip.skip (*args, **kwarg)
 

Detailed Description

Methods provide the functions needed to perform analyses.

These are generally not classes.

Function Documentation

- -

◆ skip()

+ +

◆ skip()

diff --git a/doxygen/group__Methods.js b/doxygen/group__Methods.js index 9dbde42f..68df2cc7 100644 --- a/doxygen/group__Methods.js +++ b/doxygen/group__Methods.js @@ -2,6 +2,7 @@ var group__Methods = [ [ "Aerodynamics", "group__Methods-Aerodynamics.html", "group__Methods-Aerodynamics" ], [ "Center_of_Gravity", "group__Methods-Center__of__Gravity.html", "group__Methods-Center__of__Gravity" ], + [ "Cooling", "group__Methods-Cooling.html", "group__Methods-Cooling" ], [ "Costs", "group__Methods-Costs.html", "group__Methods-Costs" ], [ "Flight_Dynamics", "group__Methods-Flight__Dynamics.html", "group__Methods-Flight__Dynamics" ], [ "Geometry", "group__Methods-Geometry.html", "group__Methods-Geometry" ], @@ -12,5 +13,5 @@ var group__Methods = [ "Propulsion", "group__Methods-Propulsion.html", "group__Methods-Propulsion" ], [ "Utilities", "group__Methods-Utilities.html", "group__Methods-Utilities" ], [ "Weights", "group__Methods-Weights.html", "group__Methods-Weights" ], - [ "skip", "group__Methods.html#gaf0740dc1eaaae86e6127b7eebc718d8f", null ] + [ "skip", "group__Methods.html#ga058685b28af299d20f492e1984fdc40b", null ] ]; \ No newline at end of file diff --git a/doxygen/group__Optimization-Package__Setups-TRMM.html b/doxygen/group__Optimization-Package__Setups-TRMM.html index 7e80f875..39790899 100644 --- a/doxygen/group__Optimization-Package__Setups-TRMM.html +++ b/doxygen/group__Optimization-Package__Setups-TRMM.html @@ -1,9 +1,9 @@ - + - + SUAVE: TRMM @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@
- +
@@ -73,7 +78,9 @@

@@ -182,7 +189,7 @@

Generated by - doxygen 1.8.14 + doxygen 1.8.15

diff --git a/doxygen/group__Optimization-Package__Setups-TRMM.js b/doxygen/group__Optimization-Package__Setups-TRMM.js index f9962c96..6842ca18 100644 --- a/doxygen/group__Optimization-Package__Setups-TRMM.js +++ b/doxygen/group__Optimization-Package__Setups-TRMM.js @@ -17,10 +17,12 @@ var group__Optimization_Package__Setups_TRMM = [ "calculate_constraint_violation", "classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region__Optimization_1_1Trust__Region__Optimization.html#ae762fcbbe9ff61309c645680cf7ac24b", null ], [ "calculate_correction", "classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region__Optimization_1_1Trust__Region__Optimization.html#a8acaabb3bd8cb0d67d6d33dd69f4cb2f", null ], [ "evaluate_constraints", "classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region__Optimization_1_1Trust__Region__Optimization.html#acba95060955b293232cd7215397584c4", null ], - [ "evaluate_corrected_model", "classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region__Optimization_1_1Trust__Region__Optimization.html#a4714077a34faa3add6305b6aa14bd62c", null ], + [ "evaluate_corrected_model", "classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region__Optimization_1_1Trust__Region__Optimization.html#a8fe6735c35a588f86fd7326acd12ebaa", null ], [ "evaluate_model", "classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region__Optimization_1_1Trust__Region__Optimization.html#ac182b46b7d513c7745520f5421cc4cd4", null ], + [ "initialize_SLSQP_constraints", "classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region__Optimization_1_1Trust__Region__Optimization.html#af674f5240a676b1ce0b7bfd06458ff31", null ], [ "optimize", "classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region__Optimization_1_1Trust__Region__Optimization.html#a41444575f97d7ce4a60ab05e25d4c39f", null ], [ "scale_vals", "classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region__Optimization_1_1Trust__Region__Optimization.html#a9a074a8e7cf8603b560333fd309fd8d3", null ], + [ "unpack_constraints_slsqp", "classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region__Optimization_1_1Trust__Region__Optimization.html#a01877d2aec26bbe67846e72c0fcd2d1b", null ], [ "update_tr_size", "classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region__Optimization_1_1Trust__Region__Optimization.html#a8b053bf1bf439b9e0a7c152b8b1b7faf", null ], [ "convergence_tolerance", "classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region__Optimization_1_1Trust__Region__Optimization.html#ace708c4c014c74e98e33a590a280b661", null ], [ "difference_interval", "classSUAVE_1_1Optimization_1_1Package__Setups_1_1TRMM_1_1Trust__Region__Optimization_1_1Trust__Region__Optimization.html#ad3226034b0686052ff6e865e19443e73", null ], diff --git a/doxygen/group__Optimization-Package__Setups.html b/doxygen/group__Optimization-Package__Setups.html index ee907143..2ba88569 100644 --- a/doxygen/group__Optimization-Package__Setups.html +++ b/doxygen/group__Optimization-Package__Setups.html @@ -1,9 +1,9 @@ - + - + SUAVE: Package_Setups @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@
- +
@@ -73,7 +78,9 @@
@@ -110,22 +117,22 @@ - - - - - - - - - - - - - - - - + + + + + + + + + + + + + + + + @@ -138,30 +145,42 @@ + + - - + + + + + +

Functions

def SUAVE.Optimization.Package_Setups.additive_setup.Additive_Solve (problem, num_fidelity_levels=2, num_samples=10, max_iterations=10, tolerance=1e-6, opt_type='basic', num_starts=3, print_output=True)
 
def SUAVE.Optimization.Package_Setups.additive_setup.evaluate_model (problem, x, cons)
 
def SUAVE.Optimization.Package_Setups.additive_setup.evaluate_corrected_model (x, problem=None, obj_surrogate=None, cons_surrogate=None)
 
def SUAVE.Optimization.Package_Setups.additive_setup.evaluate_expected_improvement (x, problem=None, obj_surrogate=None, cons_surrogate=None, fstar=np.inf, cons=None)
 
def SUAVE.Optimization.Package_Setups.additive_setup.expected_improvement_carpet (lbs, ubs, problem, obj_surrogate, cons_surrogate, fstar, show_log_improvement=False)
 
def SUAVE.Optimization.Package_Setups.additive_setup.scale_vals (inp, con, ini, bnd, scl)
 
def SUAVE.Optimization.Package_Setups.additive_setup.initialize_opt_vals (opt_prob, obj, inp, x_low_bound, x_up_bound, con_low_edge, con_up_edge, nam, con, x_eval)
 
def SUAVE.Optimization.Package_Setups.additive_setup.run_objective_optimization (opt_prob, problem, f_additive_surrogate, g_additive_surrogate)
 
def SUAVE.Optimization.Package_Setups.additive_setup.Additive_Solver.Additive_Solve (self, problem, num_fidelity_levels=2, num_samples=10, max_iterations=10, tolerance=1e-6, opt_type='basic', num_starts=3, print_output=True)
 
def SUAVE.Optimization.Package_Setups.additive_setup.Additive_Solver.evaluate_model (self, problem, x, cons)
 
def SUAVE.Optimization.Package_Setups.additive_setup.Additive_Solver.evaluate_corrected_model (self, x, problem=None, obj_surrogate=None, cons_surrogate=None)
 
def SUAVE.Optimization.Package_Setups.additive_setup.Additive_Solver.evaluate_expected_improvement (self, x, problem=None, obj_surrogate=None, cons_surrogate=None, fstar=np.inf, cons=None)
 
def SUAVE.Optimization.Package_Setups.additive_setup.Additive_Solver.expected_improvement_carpet (self, lbs, ubs, problem, obj_surrogate, cons_surrogate, fstar, show_log_improvement=False)
 
def SUAVE.Optimization.Package_Setups.additive_setup.Additive_Solver.scale_vals (self, inp, con, ini, bnd, scl)
 
def SUAVE.Optimization.Package_Setups.additive_setup.Additive_Solver.initialize_opt_vals (self, opt_prob, obj, inp, x_low_bound, x_up_bound, con_low_edge, con_up_edge, nam, con, x_eval)
 
def SUAVE.Optimization.Package_Setups.additive_setup.Additive_Solver.run_objective_optimization (self, opt_prob, problem, f_additive_surrogate, g_additive_surrogate)
 
def SUAVE.Optimization.Package_Setups.ipopt_setup.Ipopt_Solve (problem)
 
def SUAVE.Optimization.Package_Setups.ipopt_setup.eval_grad_f (x, problem)
 
def SUAVE.Optimization.Package_Setups.ipopt_setup.make_structure (problem)
 
def SUAVE.Optimization.Package_Setups.particle_swarm_optimization.particle_swarm_optimization (func, lb, ub, ieqcons=[], f_ieqcons=None, args=(), kwargs={}, swarmsize=100, omega=0.5, phip=0.5, phig=0.5, maxiter=100, minstep=1e-8, minfunc=1e-8, debug=False)
 
def SUAVE.Optimization.Package_Setups.pyopt_setup.Pyopt_Solve (problem, solver='SNOPT', FD='single', sense_step=1.0E-6, nonderivative_line_search=False)
 
def SUAVE.Optimization.Package_Setups.pyopt_setup.PyOpt_Problem (problem, x)
 
def SUAVE.Optimization.Package_Setups.pyopt_surrogate_setup.pyopt_surrogate_setup (surrogate_function, inputs, constraints)
 
def SUAVE.Optimization.Package_Setups.scipy_setup.SciPy_Solve (problem, solver='SLSQP', sense_step=1.4901161193847656e-08)
 
def SUAVE.Optimization.Package_Setups.pyoptsparse_setup.Pyoptsparse_Solve (problem, solver='SNOPT', FD='single', sense_step=1.0E-6, nonderivative_line_search=False)
 
def SUAVE.Optimization.Package_Setups.pyoptsparse_setup.PyOpt_Problem (problem, xdict)
 
def SUAVE.Optimization.Package_Setups.scipy_setup.SciPy_Solve (problem, solver='SLSQP', sense_step=1.4901161193847656e-08, tolerance=1e-6, pop_size=10, prob_seed=None)
 
def SUAVE.Optimization.Package_Setups.scipy_setup.SciPy_Problem (problem, x)
 

Detailed Description

Individual package setups that help you interface with other codes.

Function Documentation

- -

◆ Additive_Solve()

+ +

◆ Additive_Solve()

- + + + + + + + @@ -214,13 +233,13 @@

Solves a multifidelity problem using an additive corrections
-
+    
 Assumptions:
 N/A
-
+    
 Source:
 N/A
-
+    
 Inputs:
 problem             [nexus()]
 num_fidelity_levels [int]
@@ -233,7 +252,7 @@ 

-

◆ evaluate_corrected_model()

+ +

◆ evaluate_corrected_model()

def SUAVE.Optimization.Package_Setups.additive_setup.Additive_Solve def SUAVE.Optimization.Package_Setups.additive_setup.Additive_Solver.Additive_Solve (  self,
  problem,
- + + + + + + + @@ -465,13 +490,13 @@

Evaluates the corrected model with the low fidelity plus the corrections
-
+    
 Assumptions:
 N/A
-
+    
 Source:
 N/A
-
+    
 Inputs:
 x              [array]
 problem        [nexus()]
@@ -482,21 +507,27 @@ 

-

◆ evaluate_expected_improvement()

+ +

◆ evaluate_expected_improvement()

def SUAVE.Optimization.Package_Setups.additive_setup.evaluate_corrected_model def SUAVE.Optimization.Package_Setups.additive_setup.Additive_Solver.evaluate_corrected_model (  self,
  x,
- + + + + + + + @@ -537,13 +568,13 @@

Evaluates the expected improvement of the point x
-
+    
 Assumptions:
 N/A
-
+    
 Source:
 N/A
-
+    
 Inputs:
 x              [array]
 problem        [nexus()]
@@ -556,21 +587,27 @@ 

-

◆ evaluate_model()

+ +

◆ evaluate_model()

def SUAVE.Optimization.Package_Setups.additive_setup.evaluate_expected_improvement def SUAVE.Optimization.Package_Setups.additive_setup.Additive_Solver.evaluate_expected_improvement (  self,
  x,
- + + + + + + + @@ -593,13 +630,13 @@

Solves the optimization problem to get the objective and constraints
-
+    
 Assumptions:
 N/A
-
+    
 Source:
 N/A
-
+    
 Inputs:
 problem   [nexus()]
 x         [array]
@@ -608,22 +645,28 @@ 

-

◆ expected_improvement_carpet()

+ +

◆ expected_improvement_carpet()

def SUAVE.Optimization.Package_Setups.additive_setup.evaluate_model def SUAVE.Optimization.Package_Setups.additive_setup.Additive_Solver.evaluate_model (  self,
  problem,
- + + + + + + + @@ -670,13 +713,13 @@

Makes a carpet plot of the expected improvement
-
+    
 Assumptions:
 N/A
-
+    
 Source:
 N/A
-
+    
 Inputs:
 lbs                  [array]
 lbs                  [array]
@@ -688,21 +731,27 @@ 

-

◆ initialize_opt_vals()

+ +

◆ initialize_opt_vals()

def SUAVE.Optimization.Package_Setups.additive_setup.expected_improvement_carpet def SUAVE.Optimization.Package_Setups.additive_setup.Additive_Solver.expected_improvement_carpet (  self,
  lbs,
- + + + + + + + @@ -767,13 +816,13 @@

Sets up the optimization values 
-
+    
 Assumptions:
 N/A
-
+    
 Source:
 N/A
-
+    
 Inputs:
 opt_prob         [pyopt_problem()]
 obj              [float]
@@ -861,8 +910,220 @@ 

+

◆ particle_swarm_optimization()

+ +
+
+

def SUAVE.Optimization.Package_Setups.additive_setup.initialize_opt_vals def SUAVE.Optimization.Package_Setups.additive_setup.Additive_Solver.initialize_opt_vals (  self,
  opt_prob,
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Optimization.Package_Setups.particle_swarm_optimization.particle_swarm_optimization ( func,
 lb,
 ub,
 ieqcons = [],
 f_ieqcons = None,
 args = (),
 kwargs = {},
 swarmsize = 100,
 omega = 0.5,
 phip = 0.5,
 phig = 0.5,
 maxiter = 100,
 minstep = 1e-8,
 minfunc = 1e-8,
 debug = False 
)
+
+
This function perform a particle swarm optimization (PSO)
+
+Source:
+    Pyswarm: https://github.com/tisimst/pyswarm
+      
+Inputs: 
+    func      : The function to be minimized                                                                    [function] 
+    lb        : The lower bounds of the design variable(s)                                                      [array] 
+    ub        :  The upper bounds of the design variable(s)                                                     [array]
+                                                                                                                
+    ieqcons   : A list of functions of length n such that ieqcons[j](x,*args)                                   
+                >= 0.0 in a successfully optimized problem (Default: [])                                        [list]
+    f_ieqcons : Returns a 1-D array in which each element must be greater or equal                              
+                to 0.0 in a successfully optimized problem. If f_ieqcons is specified,                          
+                ieqcons is ignored (Default: None)                                                              [function]
+    args      : Additional arguments passed to objective and constraint functions                               [tuple]                       
+    kwargs    : Additional keyword arguments passed to objective and constraint functions                       [dict] 
+    swarmsize : The number of particles in the swarm (Default: 100)                                             [int] 
+    omega     : Particle velocity scaling factor (Default: 0.5)                                                 [float] 
+    phip      : Scaling factor to search away from the particle's best known position (Default: 0.5)            [scalar] 
+    phig      : Scaling factor to search away from the swarm's best known position (Default: 0.5)               [scalar]
+    maxiter   : The maximum number of iterations for the swarm to search (Default: 100) [int]                   
+    minstep   : The minimum stepsize of swarm's best position before the search terminates (Default: 1e-8)      [scalar]
+    minfunc   : The minimum change of swarm's best objective value before the search terminates (Default: 1e-8) [scalar]
+    debug     : If True, progress statements will be displayed every iteration (Default: False)                 [boolean]
+   
+Outputs:
+    g         : The swarm's best known position (optimal design)                                                [list] 
+    f         : The objective value at ``g``                                                                    [float]
+     
+Properties Used:
+    None
Copyright (c) 2015, Sebastian M. Castillo Hair
+All rights reserved.
+
+Redistribution and use in source and binary forms, with or without
+modification, are permitted provided that the following conditions are met:
+1. Redistributions of source code must retain the above copyright
+    notice, this list of conditions and the following disclaimer.
+2. Redistributions in binary form must reproduce the above copyright
+    notice, this list of conditions and the following disclaimer in the
+    documentation and/or other materials provided with the distribution.
+3. All advertising materials mentioning features or use of this software
+    must display the following acknowledgement:
+    This product includes software developed by Sebastian M. Castillo Hair.
+4. Neither the name of Sebastian M. Castillo Hair nor the
+    names of its contributors may be used to endorse or promote products
+    derived from this software without specific prior written permission.
+
+THIS SOFTWARE IS PROVIDED BY SEBASTIAN M. CASTILLO HAIR ''AS IS'' AND ANY
+EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT LIMITED TO, THE IMPLIED
+WARRANTIES OF MERCHANTABILITY AND FITNESS FOR A PARTICULAR PURPOSE ARE
+DISCLAIMED. IN NO EVENT SHALL SEBASTIAN M. CASTILLO HAIR BE LIABLE FOR ANY
+DIRECT, INDIRECT, INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES
+(INCLUDING, BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES;
+LOSS OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED AND
+ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT LIABILITY, OR TORT
+(INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN ANY WAY OUT OF THE USE OF THIS
+SOFTWARE, EVEN IF ADVISED OF THE POSSIBILITY OF SUCH DAMAGE.
+
+
+ +

◆ PyOpt_Problem() [1/2]

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Optimization.Package_Setups.pyoptsparse_setup.PyOpt_Problem ( problem,
 xdict 
)
+
+
This wrapper runs the SUAVE problem and is called by the PyOpt solver.
+    Prints the inputs (x) as well as the objective values and constraints.
+    If any values produce NaN then a fail flag is thrown.
+
+    Assumptions:
+    None
+
+    Source:
+    N/A
+
+    Inputs:
+    problem   [nexus()]
+    x         [array]
+
+    Outputs:
+    obj       [float]
+    cons      [array]
+    fail      [bool]
+
+    Properties Used:
+    None
+
+
+
-

◆ PyOpt_Problem()

+

◆ PyOpt_Problem() [2/2]

@@ -1029,16 +1290,89 @@

-

◆ run_objective_optimization()

+ +

◆ Pyoptsparse_Solve()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Optimization.Package_Setups.pyoptsparse_setup.Pyoptsparse_Solve ( problem,
 solver = 'SNOPT',
 FD = 'single',
 sense_step = 1.0E-6,
 nonderivative_line_search = False 
)
+
+
This converts your SUAVE Nexus problem into a PyOptsparse optimization problem and solves it.
+    Pyoptsparse has many algorithms, they can be switched out by using the solver input. 
+
+    Assumptions:
+    None
+
+    Source:
+    N/A
+
+    Inputs:
+    problem                   [nexus()]
+    solver                    [str]
+    FD (parallel or single)   [str]
+    sense_step                [float]
+    nonderivative_line_search [bool]
+
+    Outputs:
+    outputs                   [list]
+
+    Properties Used:
+    None
+
+
+
+ +

◆ run_objective_optimization()

- + + + + + + + @@ -1067,13 +1401,13 @@

Runs SNOPT to optimize
-
+    
 Assumptions:
 N/A
-
+    
 Source:
 N/A
-
+    
 Inputs:
 opt_prob             [pyopt_problem()]
 problem              [nexus()]
@@ -1088,16 +1422,22 @@ 

-

◆ scale_vals()

+ +

◆ scale_vals()

def SUAVE.Optimization.Package_Setups.additive_setup.run_objective_optimization def SUAVE.Optimization.Package_Setups.additive_setup.Additive_Solver.run_objective_optimization (  self,
  opt_prob,
- + + + + + + + @@ -1132,13 +1472,13 @@

Scales values to help setup the problem
-
+    
 Assumptions:
 N/A
-
+    
 Source:
 N/A
-
+    
 Inputs:
 inp                         [array]
 con                         [array]
@@ -1148,13 +1488,13 @@ 

-

◆ SciPy_Solve()

+ +

◆ SciPy_Solve()

@@ -1227,7 +1567,25 @@

- + + + + + + + + + + + + + + + + + + + @@ -1265,7 +1623,7 @@

Generated by - doxygen 1.8.14 + doxygen 1.8.15 diff --git a/doxygen/group__Optimization-Package__Setups.js b/doxygen/group__Optimization-Package__Setups.js index eb403f78..8e7c2560 100644 --- a/doxygen/group__Optimization-Package__Setups.js +++ b/doxygen/group__Optimization-Package__Setups.js @@ -1,23 +1,26 @@ var group__Optimization_Package__Setups = [ [ "TRMM", "group__Optimization-Package__Setups-TRMM.html", "group__Optimization-Package__Setups-TRMM" ], - [ "Additive_Solve", "group__Optimization-Package__Setups.html#gabb534dc553c269c0b883908092d6f2ed", null ], + [ "Additive_Solve", "group__Optimization-Package__Setups.html#ga8f9c498581a443c5b268bc995f4771d7", null ], [ "eval_f", "group__Optimization-Package__Setups.html#ga98973b9e47004f10152a0cf6ecec5594", null ], [ "eval_g", "group__Optimization-Package__Setups.html#ga7199ae6dab817398c93252096797a1c4", null ], [ "eval_grad_f", "group__Optimization-Package__Setups.html#gaec2e3de7f3b64d10edfe40b91cd6b5ab", null ], [ "eval_jac_g", "group__Optimization-Package__Setups.html#ga2b96466343bf8317ec428d7b851f8d41", null ], - [ "evaluate_corrected_model", "group__Optimization-Package__Setups.html#ga9b73c8d202a3e4c4bad264c7137b7e02", null ], - [ "evaluate_expected_improvement", "group__Optimization-Package__Setups.html#gaa37f71305979147550b800385506b273", null ], - [ "evaluate_model", "group__Optimization-Package__Setups.html#ga391d6c55cf2297cfc0c2582db19676e6", null ], - [ "expected_improvement_carpet", "group__Optimization-Package__Setups.html#ga595a0239c702615e76556141cbdc235a", null ], - [ "initialize_opt_vals", "group__Optimization-Package__Setups.html#ga55bbd6058098de65ac5e59c10c7f90bb", null ], + [ "evaluate_corrected_model", "group__Optimization-Package__Setups.html#ga9fd8c25ffe84afec24ae5842fd01bc59", null ], + [ "evaluate_expected_improvement", "group__Optimization-Package__Setups.html#ga2fce77878956493ab46ed6d86b7c7028", null ], + [ "evaluate_model", "group__Optimization-Package__Setups.html#ga1aa96d868702f99a0b15f58bf5eca0ce", null ], + [ "expected_improvement_carpet", "group__Optimization-Package__Setups.html#ga75d4008576d2b1539a517bdde5147089", null ], + [ "initialize_opt_vals", "group__Optimization-Package__Setups.html#gaa25a2e15b4183507a2a1ec0725bfe9ce", null ], [ "Ipopt_Solve", "group__Optimization-Package__Setups.html#ga9b30cb43a55ff698b8f6d2e6b0d01272", null ], [ "make_structure", "group__Optimization-Package__Setups.html#gaea0f7002ef7f26f7ace5bc50bf7b869b", null ], + [ "particle_swarm_optimization", "group__Optimization-Package__Setups.html#ga9731806102b0917cad52cd899f1638ac", null ], + [ "PyOpt_Problem", "group__Optimization-Package__Setups.html#ga9a9401838b0af9f0893b6681bd41360b", null ], [ "PyOpt_Problem", "group__Optimization-Package__Setups.html#ga5c240bcf69db9bdb19e34bf3b8934518", null ], [ "Pyopt_Solve", "group__Optimization-Package__Setups.html#ga15bf2d97e59321d406a21617f5140576", null ], [ "pyopt_surrogate_setup", "group__Optimization-Package__Setups.html#ga9a79b2d8360c0ccdffaa4ee2a0a5c785", null ], - [ "run_objective_optimization", "group__Optimization-Package__Setups.html#ga00b222e15be6c8f9bf756a669dda63c2", null ], - [ "scale_vals", "group__Optimization-Package__Setups.html#ga3404bfd5a112bd1528b155f0886a7eb5", null ], + [ "Pyoptsparse_Solve", "group__Optimization-Package__Setups.html#ga9c398886e9ce01725cafbf0e1f29dd16", null ], + [ "run_objective_optimization", "group__Optimization-Package__Setups.html#ga4977676388001bfa1045dd9ed14448a1", null ], + [ "scale_vals", "group__Optimization-Package__Setups.html#ga9466bd27f5f4934f91f5f60643747db3", null ], [ "SciPy_Problem", "group__Optimization-Package__Setups.html#gaf64bbbdea4a28ea4184ce286e99fc22d", null ], - [ "SciPy_Solve", "group__Optimization-Package__Setups.html#ga455ed3db18d3969bc8541ad9ef033897", null ] + [ "SciPy_Solve", "group__Optimization-Package__Setups.html#ga1abbb2ae55d17dcae7a01c42d8f87396", null ] ]; \ No newline at end of file diff --git a/doxygen/group__Optimization.html b/doxygen/group__Optimization.html index c3a09c10..0afb8d49 100644 --- a/doxygen/group__Optimization.html +++ b/doxygen/group__Optimization.html @@ -1,9 +1,9 @@ - + - + SUAVE: Optimization @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@

@@ -57,9 +60,11 @@
def SUAVE.Optimization.Package_Setups.additive_setup.scale_vals def SUAVE.Optimization.Package_Setups.additive_setup.Additive_Solver.scale_vals (  self,
  inp,
 sense_step = 1.4901161193847656e-08 sense_step = 1.4901161193847656e-08,
 tolerance = 1e-6,
 pop_size = 10,
 prob_seed = None 
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@

diff --git a/doxygen/group__Optimization.js b/doxygen/group__Optimization.js index 40cd8832..e79ac0c4 100644 --- a/doxygen/group__Optimization.js +++ b/doxygen/group__Optimization.js @@ -15,6 +15,8 @@ var group__Optimization = [ "analyses", "classSUAVE_1_1Optimization_1_1Nexus_1_1Nexus.html#a7540bae0fa705aedd67732e6a4f2fd03", null ], [ "evaluation_count", "classSUAVE_1_1Optimization_1_1Nexus_1_1Nexus.html#a0e0a0b0d2ba3e3cd1381569156f1f2ff", null ], [ "fidelity_level", "classSUAVE_1_1Optimization_1_1Nexus_1_1Nexus.html#aea9b128c29d6dc551ac15263d0e2267c", null ], + [ "force_evaluate", "classSUAVE_1_1Optimization_1_1Nexus_1_1Nexus.html#a1b71ecd9205cdee6e020beb50922e180", null ], + [ "hard_bounded_inputs", "classSUAVE_1_1Optimization_1_1Nexus_1_1Nexus.html#a9b62669b43a4ee0837fb3c0b689b4baa", null ], [ "last_fidelity", "classSUAVE_1_1Optimization_1_1Nexus_1_1Nexus.html#ac4c2045d9bc469e48c23a7b5f96ecb84", null ], [ "last_inputs", "classSUAVE_1_1Optimization_1_1Nexus_1_1Nexus.html#a4a62b5f7d690c3b4390ccd4f54fd6a45", null ], [ "missions", "classSUAVE_1_1Optimization_1_1Nexus_1_1Nexus.html#a3b13fe94b3835bb58af3aca92ec95a16", null ], diff --git a/doxygen/group__Plots-Geometry.html b/doxygen/group__Plots-Geometry.html new file mode 100644 index 00000000..ca4adae4 --- /dev/null +++ b/doxygen/group__Plots-Geometry.html @@ -0,0 +1,364 @@ + + + + + + + +SUAVE: Geometry + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
Geometry
+
+
+ +

Description. +More...

+ + + + + + + + +

+Functions

def SUAVE.Plots.Geometry.plot_propeller.plot_propeller (prop, face_color='red', edge_color='black', save_figure=False, save_filename="Propeller_Geometry", file_type=".png")
 
def SUAVE.Plots.Geometry.plot_vehicle.plot_vehicle (vehicle, elevation_angle=30, azimuthal_angle=210, axis_limits=10, plot_axis=False, save_figure=False, plot_control_points=True, save_filename="Vehicle_Geometry")
 
def SUAVE.Plots.Geometry.plot_vehicle_vlm_panelization.plot_vehicle_vlm_panelization (vehicle, elevation_angle=30, azimuthal_angle=210, axis_limits=10, plot_axis=False, save_figure=False, plot_control_points=True, save_filename="VLM_Panelization")
 
+

Detailed Description

+

Description.

+

Function Documentation

+ +

◆ plot_propeller()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Plots.Geometry.plot_propeller.plot_propeller ( prop,
 face_color = 'red',
 edge_color = 'black',
 save_figure = False,
 save_filename = "Propeller_Geometry",
 file_type = ".png" 
)
+
+
This plots the geometry of a propeller or rotor
+
+Assumptions:
+None
+
+Source:
+None
+
+Inputs:
+SUAVE.Components.Energy.Converters.Propeller()
+
+Outputs: 
+Plots
+
+Properties Used:
+N/A 
+
+
+
+ +

◆ plot_vehicle()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Plots.Geometry.plot_vehicle.plot_vehicle ( vehicle,
 elevation_angle = 30,
 azimuthal_angle = 210,
 axis_limits = 10,
 plot_axis = False,
 save_figure = False,
 plot_control_points = True,
 save_filename = "Vehicle_Geometry" 
)
+
+
This plots vortex lattice panels created when Fidelity Zero  Aerodynamics
+Routine is initialized
+
+Assumptions:
+None
+
+Source:
+None
+
+Inputs:
+vehicle
+
+Outputs:
+Plots
+
+Properties Used:
+N/A
+
+
+
+ +

◆ plot_vehicle_vlm_panelization()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Plots.Geometry.plot_vehicle_vlm_panelization.plot_vehicle_vlm_panelization ( vehicle,
 elevation_angle = 30,
 azimuthal_angle = 210,
 axis_limits = 10,
 plot_axis = False,
 save_figure = False,
 plot_control_points = True,
 save_filename = "VLM_Panelization" 
)
+
+
This plots vortex lattice panels created when Fidelity Zero  Aerodynamics 
+Routine is initialized
+
+Assumptions:
+None
+
+Source:
+None
+
+Inputs:
+vehicle.vortex_distribution
+
+Outputs: 
+Plots
+
+Properties Used:
+N/A 
+
+
+
+
+
+ + + + diff --git a/doxygen/group__Plots-Geometry.js b/doxygen/group__Plots-Geometry.js new file mode 100644 index 00000000..bc434aee --- /dev/null +++ b/doxygen/group__Plots-Geometry.js @@ -0,0 +1,6 @@ +var group__Plots_Geometry = +[ + [ "plot_propeller", "group__Plots-Geometry.html#gadcaa63b02fc213afa83f948fe550a792", null ], + [ "plot_vehicle", "group__Plots-Geometry.html#ga65e8ca683569ece05ac1c071022b57db", null ], + [ "plot_vehicle_vlm_panelization", "group__Plots-Geometry.html#ga6306902bdaed7a8dded178df78a7ecc4", null ] +]; \ No newline at end of file diff --git a/doxygen/group__Plots-Geometry__Plots.html b/doxygen/group__Plots-Geometry__Plots.html new file mode 100644 index 00000000..79edf61b --- /dev/null +++ b/doxygen/group__Plots-Geometry__Plots.html @@ -0,0 +1,380 @@ + + + + + + + +SUAVE: Geometry_Plots + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.4.0 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
Geometry_Plots
+
+
+ +

Description. +More...

+ + + + + + + + + + +

+Functions

def SUAVE.Plots.Geometry_Plots.plot_airfoil.plot_airfoil (airfoil_names, line_color='k-', overlay=False, save_figure=False, save_filename="Airfoil_Geometry", file_type=".png")
 
def SUAVE.Plots.Geometry_Plots.plot_propeller.plot_propeller (prop, face_color='red', edge_color='black', save_figure=False, save_filename="Propeller_Geometry", file_type=".png")
 
def SUAVE.Plots.Geometry_Plots.plot_vehicle.plot_vehicle (vehicle, save_figure=False, plot_control_points=True, save_filename="Vehicle_Geometry")
 
def SUAVE.Plots.Geometry_Plots.plot_vehicle_vlm_panelization.plot_vehicle_vlm_panelization (vehicle, save_figure=False, plot_control_points=True, save_filename="VLM_Panelization")
 
+

Detailed Description

+

Description.

+

Function Documentation

+ +

◆ plot_airfoil()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Plots.Geometry_Plots.plot_airfoil.plot_airfoil ( airfoil_names,
 line_color = 'k-',
 overlay = False,
 save_figure = False,
 save_filename = "Airfoil_Geometry",
 file_type = ".png" 
)
+
+
This plots all airfoil defined in the list "airfoil_names" 
+
+Assumptions:
+None
+
+Source:
+None
+
+Inputs:
+airfoil_geometry_files   <list of strings>
+
+Outputs: 
+Plots
+
+Properties Used:
+N/A 
+
+
+
+ +

◆ plot_propeller()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Plots.Geometry_Plots.plot_propeller.plot_propeller ( prop,
 face_color = 'red',
 edge_color = 'black',
 save_figure = False,
 save_filename = "Propeller_Geometry",
 file_type = ".png" 
)
+
+
This plots the geometry of a propeller or rotor
+
+Assumptions:
+None
+
+Source:
+None
+
+Inputs:
+SUAVE.Components.Energy.Converters.Propeller()
+
+Outputs: 
+Plots
+
+Properties Used:
+N/A 
+
+
+
+ +

◆ plot_vehicle()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Plots.Geometry_Plots.plot_vehicle.plot_vehicle ( vehicle,
 save_figure = False,
 plot_control_points = True,
 save_filename = "Vehicle_Geometry" 
)
+
+
This plots vortex lattice panels created when Fidelity Zero  Aerodynamics 
+Routine is initialized
+
+Assumptions:
+None
+
+Source:
+None
+
+Inputs:
+vehicle 
+
+Outputs: 
+Plots
+
+Properties Used:
+N/A 
+
+
+
+ +

◆ plot_vehicle_vlm_panelization()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Plots.Geometry_Plots.plot_vehicle_vlm_panelization.plot_vehicle_vlm_panelization ( vehicle,
 save_figure = False,
 plot_control_points = True,
 save_filename = "VLM_Panelization" 
)
+
+
This plots vortex lattice panels created when Fidelity Zero  Aerodynamics 
+Routine is initialized
+
+Assumptions:
+None
+
+Source:
+None
+
+Inputs:
+vehicle.vortex_distribution
+
+Outputs: 
+Plots
+
+Properties Used:
+N/A 
+
+
+
+
+
+ + + + diff --git a/doxygen/group__Plots-Geometry__Plots.js b/doxygen/group__Plots-Geometry__Plots.js new file mode 100644 index 00000000..07662174 --- /dev/null +++ b/doxygen/group__Plots-Geometry__Plots.js @@ -0,0 +1,7 @@ +var group__Plots_Geometry__Plots = +[ + [ "plot_airfoil", "group__Plots-Geometry__Plots.html#gad182dd558d863e732b9a6df731af8163", null ], + [ "plot_propeller", "group__Plots-Geometry__Plots.html#gac775361103187f6fe93e84d946b34d02", null ], + [ "plot_vehicle", "group__Plots-Geometry__Plots.html#gaa29969c039277747cc6d0f527b1247bc", null ], + [ "plot_vehicle_vlm_panelization", "group__Plots-Geometry__Plots.html#ga2ee7f404e72440da48677856f25f7fe0", null ] +]; \ No newline at end of file diff --git a/doxygen/group__Plots-Performance.html b/doxygen/group__Plots-Performance.html new file mode 100644 index 00000000..0fc1a451 --- /dev/null +++ b/doxygen/group__Plots-Performance.html @@ -0,0 +1,124 @@ + + + + + + + +SUAVE: Performance + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
Performance
+
+
+ +

Plots contains functions for generating common figures. +More...

+

Plots contains functions for generating common figures.

+

Propeller_Plots.py.

+

Mission_Plots.py.

+

Created: Mar 2020, M. Clarke Apr 2020, M. Clarke Sep 2020, M. Clarke Apr 2021, M. Clarke Dec 2021, S. Claridge

+

Created: Mar 2021, R. Erhard Modified: Feb 2022, R. Erhard

+
+
+ + + + diff --git a/doxygen/group__Plots.html b/doxygen/group__Plots.html new file mode 100644 index 00000000..44299668 --- /dev/null +++ b/doxygen/group__Plots.html @@ -0,0 +1,340 @@ + + + + + + + +SUAVE: Plots + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+ +
+
Plots
+
+
+ +

Plots contains functions for generating common figures. +More...

+ + + + + + + + +

+Modules

 Geometry
 Description.
 
 Performance
 Plots contains functions for generating common figures.
 
+ + + + + + + + + +

+Functions

def SUAVE.Plots.Performance.Airfoil_Plots.plot_airfoil_analysis_boundary_layer_properties (ap, show_legend=True)
 
def SUAVE.Plots.Performance.Airfoil_Plots.plot_airfoil_analysis_polars (ap, show_legend=True)
 
def SUAVE.Plots.Performance.Airfoil_Plots.plot_airfoil_analysis_surface_forces (ap, show_legend=True, arrow_color='r')
 
def SUAVE.Plots.Performance.Mission_Plots.plot_stability_coefficients (results, line_color='bo-', save_figure=False, save_filename="Stability_Coefficients", file_type=".png")
 
+

Detailed Description

+

Plots contains functions for generating common figures.

+

Function Documentation

+ +

◆ plot_airfoil_analysis_boundary_layer_properties()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Plots.Performance.Airfoil_Plots.plot_airfoil_analysis_boundary_layer_properties ( ap,
 show_legend = True 
)
+
+
This plots the boundary layer properties of an airfoil
+    or group of airfoils
+
+    Assumptions:
+    None
+    
+    Inputs: 
+    ap       - data stucture of airfoil boundary layer properties  
+    
+    Outputs: 
+    None 
+    
+    Properties Used:
+    N/A
+
+
+ +

◆ plot_airfoil_analysis_polars()

+ +
+
+ + + + + + + + + + + + + + + + + + +
def SUAVE.Plots.Performance.Airfoil_Plots.plot_airfoil_analysis_polars ( ap,
 show_legend = True 
)
+
+
This plots the polars of an airfoil or group of airfoils
+
+    Assumptions:
+    None
+    
+    Inputs: 
+    ap       - data stucture of airfoil boundary layer properties and polars 
+     
+    Outputs: 
+    None 
+    
+    Properties Used:
+    N/A
+
+
+ +

◆ plot_airfoil_analysis_surface_forces()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Plots.Performance.Airfoil_Plots.plot_airfoil_analysis_surface_forces ( ap,
 show_legend = True,
 arrow_color = 'r' 
)
+
+
This plots the forces on an airfoil surface
+
+    Assumptions:
+    None
+    
+    Inputs: 
+    ap       - data stucture of airfoil boundary layer properties and polars 
+     
+    Outputs: 
+    None 
+    
+    Properties Used:
+    N/A
+
+
+ +

◆ plot_stability_coefficients()

+ +
+
+ + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
def SUAVE.Plots.Performance.Mission_Plots.plot_stability_coefficients ( results,
 line_color = 'bo-',
 save_figure = False,
 save_filename = "Stability_Coefficients",
 file_type = ".png" 
)
+
+
This plots the static stability characteristics of an aircraft
+
+Assumptions:
+None
+
+Source:
+None
+
+Inputs:
+results.segments.conditions.stability.
+   static
+       CM 
+       Cm_alpha 
+       static_margin 
+   aerodynamics.
+       angle_of_attack
+Outputs: 
+Plots
+
+Properties Used:
+N/A 
+
+
+
+
+
+ + + + diff --git a/doxygen/group__Plots.js b/doxygen/group__Plots.js new file mode 100644 index 00000000..3ebc8f58 --- /dev/null +++ b/doxygen/group__Plots.js @@ -0,0 +1,9 @@ +var group__Plots = +[ + [ "Geometry", "group__Plots-Geometry.html", "group__Plots-Geometry" ], + [ "Performance", "group__Plots-Performance.html", null ], + [ "plot_airfoil_analysis_boundary_layer_properties", "group__Plots.html#ga00f9d3f1a1fc18ffd492dc1b18919c7a", null ], + [ "plot_airfoil_analysis_polars", "group__Plots.html#ga6b38742f54467ce7e5bc33a1368f3db3", null ], + [ "plot_airfoil_analysis_surface_forces", "group__Plots.html#gaaa6e3b5c7bbfd96ccc2c13363a7fb6fe", null ], + [ "plot_stability_coefficients", "group__Plots.html#ga67cd2f6e4859529ad880f4feb9320164", null ] +]; \ No newline at end of file diff --git a/doxygen/group__Plugins.html b/doxygen/group__Plugins.html index 48c0a81f..ae9f0773 100644 --- a/doxygen/group__Plugins.html +++ b/doxygen/group__Plugins.html @@ -1,9 +1,9 @@ - + - + SUAVE: Plugins @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@
- +
@@ -73,7 +78,9 @@

@@ -152,7 +159,7 @@

Generated by - doxygen 1.8.14 + doxygen 1.8.15

diff --git a/doxygen/group__Sizing.html b/doxygen/group__Sizing.html deleted file mode 100644 index 8ea8fedf..00000000 --- a/doxygen/group__Sizing.html +++ /dev/null @@ -1,265 +0,0 @@ - - - - - - - -SUAVE: Sizing - - - - - - - - - - - - - - - -
-
- - - - - - - - -
-
SUAVE -  1.1.0 -
-
An Aerospace Vehicle Environment for Designing Future Aircraft
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Sizing
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Sizing provides methods to size a vehicle's mass, battery energy(s), and power based on its geometric properties and mission. -More...

- - - - -

-Classes

class  SUAVE.Sizing.Sizing_Loop.Sizing_Loop
 
- - - - - - - -

-Functions

def SUAVE.Sizing.read_sizing_inputs.read_sizing_inputs (sizing_loop, opt_inputs)
 
def SUAVE.Sizing.read_sizing_inputs.format_input_data (data)
 
def SUAVE.Sizing.Sizing_Loop.Finite_Difference_Gradient (x, f, my_function, inputs, scaling, iter, h)
 
-

Detailed Description

-

Sizing provides methods to size a vehicle's mass, battery energy(s), and power based on its geometric properties and mission.

-

Function Documentation

- -

◆ Finite_Difference_Gradient()

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def SUAVE.Sizing.Sizing_Loop.Finite_Difference_Gradient ( x,
 f,
 my_function,
 inputs,
 scaling,
 iter,
 h 
)
-
-
Uses a first-order finite difference step to calculate the Jacobian
-
-Inputs:
-x               [array]
-f               [array]
-my_function     function that returns the residual f and sizing variable y-y_save
-inputs          ordered dict that is unpacked within my_function
-scaling         [array]
-iter            [int]
-h               [float]
-
-
- -

◆ format_input_data()

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-
- - - - - - - - -
def SUAVE.Sizing.read_sizing_inputs.format_input_data ( data)
-
-
Properly formats an input data structure so it can be read as an array
-of floats
-
-Inputs:
-data
-
-Outputs:
-data_out
-
-
- -

◆ read_sizing_inputs()

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def SUAVE.Sizing.read_sizing_inputs.read_sizing_inputs ( sizing_loop,
 opt_inputs 
)
-
-
This function reads a sizing loop outputs file and returns an array 
-of design variables, an array of sizing variables, and an output 
-flag to indicate whether the file was successfully read.
-
-Inputs:
-sizing_loop.
-    output_filename
-opt_inputs
-
-Outputs:
-data_inputs
-data_outputs
-read_success
-
-
-
-
- - - - diff --git a/doxygen/group__Sizing.js b/doxygen/group__Sizing.js deleted file mode 100644 index 8134bcd4..00000000 --- a/doxygen/group__Sizing.js +++ /dev/null @@ -1,24 +0,0 @@ -var group__Sizing = -[ - [ "Sizing_Loop", "classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.html", [ - [ "__defaults__", "classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.html#a178ec5c05131960d4fa8d5ad6e3c3e11", null ], - [ "broyden_update", "classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.html#a52d275bd606778420dde57df5c710ced", null ], - [ "damped_newton_update", "classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.html#a5942e4cd16b9a18ed372e79d4e8dbd70", null ], - [ "evaluate", "classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.html#a153a6ac6de2d18f130320b5e871756de", null ], - [ "newton_raphson_update", "classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.html#afee06f0c84b5023393a68b8163024939", null ], - [ "successive_substitution_update", "classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.html#a4222e0b4efa8045836ef6fb1ba94a6f3", null ], - [ "default_scaling", "classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.html#addd0442dc00517c1db5c0de356e75e68", null ], - [ "default_y", "classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.html#ac3d271509f69df8f90e10e2bf709413e", null ], - [ "initial_step", "classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.html#a5afe4453cdff685473f8f94cb6f054df", null ], - [ "iteration_options", "classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.html#af4d73d77d7b7748b08cd8e5f6cedf4fd", null ], - [ "maximum_iterations", "classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.html#a880e2af1ba6856fd9ba640aaa2b78136", null ], - [ "output_filename", "classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.html#a8bd8cbf5a638d448371e44a2f59fb4bd", null ], - [ "sizing_evaluation", "classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.html#aa9f5e946792b134387052287be34a531", null ], - [ "tolerance", "classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.html#ab945e6e09e3783f41580e291da29559f", null ], - [ "update_method", "classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.html#a82aceccafa7e1f519154a06057f02fe9", null ], - [ "write_threshhold", "classSUAVE_1_1Sizing_1_1Sizing__Loop_1_1Sizing__Loop.html#afb271146361bd7c3157ded88876df9e9", null ] - ] ], - [ "Finite_Difference_Gradient", "group__Sizing.html#gacb282e3da193d9ca04443b8303bd76d2", null ], - [ "format_input_data", "group__Sizing.html#ga473313e047f6db43c1fc004366311cae", null ], - [ "read_sizing_inputs", "group__Sizing.html#ga5080520bcc9bf040df348fb54023e7fa", null ] -]; \ No newline at end of file diff --git a/doxygen/group__Surrogate.html b/doxygen/group__Surrogate.html index 71c89b04..0e8d2cfd 100644 --- a/doxygen/group__Surrogate.html +++ b/doxygen/group__Surrogate.html @@ -1,9 +1,9 @@ - + - + SUAVE: Surrogate @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@
- +

@@ -73,7 +78,9 @@
@@ -338,7 +345,7 @@

Generated by - doxygen 1.8.14 + doxygen 1.8.15

diff --git a/doxygen/group__Vehicle.html b/doxygen/group__Vehicle.html index 7b4c9395..ef3846fb 100644 --- a/doxygen/group__Vehicle.html +++ b/doxygen/group__Vehicle.html @@ -1,9 +1,9 @@ - + - + SUAVE: Vehicle @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@
- +
@@ -73,7 +78,9 @@
@@ -112,7 +119,7 @@

Detailed Description

Vehicle.py.

-

Created: ### 2013, SUAVE Team Modified: ### ####, M. Vegh Feb 2016, E. Botero Apr 2017, M. Clarke

+

Created: ### 2013, SUAVE Team Modified: ### ####, M. Vegh Feb 2016, E. Botero Apr 2017, M. Clarke Apr 2020, E. Botero

@@ -120,7 +127,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/group__Vehicle.js b/doxygen/group__Vehicle.js index 792d0705..89fc2f90 100644 --- a/doxygen/group__Vehicle.js +++ b/doxygen/group__Vehicle.js @@ -1,18 +1,22 @@ var group__Vehicle = [ [ "Vehicle", "classSUAVE_1_1Vehicle_1_1Vehicle.html", [ - [ "__init__", "classSUAVE_1_1Vehicle_1_1Vehicle.html#ae6908bd99e7d8f4708f4fbcf64ec821d", null ], + [ "__init__", "classSUAVE_1_1Vehicle_1_1Vehicle.html#a25c012a6150c6702a2d850eed55b1964", null ], [ "__defaults__", "classSUAVE_1_1Vehicle_1_1Vehicle.html#ab279ed6a6b71a4a34fd5e07595b5d640", null ], [ "append_component", "classSUAVE_1_1Vehicle_1_1Vehicle.html#a33e2631545860ec0f2d89affae0569e7", null ], + [ "center_of_gravity", "classSUAVE_1_1Vehicle_1_1Vehicle.html#ad24633dacee7e977358e0cd7a76e6f89", null ], [ "find_component_root", "classSUAVE_1_1Vehicle_1_1Vehicle.html#aa5f8c6794e64be4f87f2fc5848d1c5bf", null ], + [ "sum_mass", "classSUAVE_1_1Vehicle_1_1Vehicle.html#ac95d257d25ef319a1812d1dfb8030ace", null ], [ "costs", "classSUAVE_1_1Vehicle_1_1Vehicle.html#a5a86ec750966687ee01ecd04f18f9b61", null ], - [ "energy", "classSUAVE_1_1Vehicle_1_1Vehicle.html#a8dd71874edebf03de72c240406ef6fed", null ], [ "envelope", "classSUAVE_1_1Vehicle_1_1Vehicle.html#af627044c07d1d292a963abafad9ad4f8", null ], [ "fuselages", "classSUAVE_1_1Vehicle_1_1Vehicle.html#aa5a1c52d2f0be67663a3a84b5f918182", null ], + [ "landing_gear", "classSUAVE_1_1Vehicle_1_1Vehicle.html#a0f7d7dd2ed5b6bf65ac9ec88c971d53f", null ], [ "mass_properties", "classSUAVE_1_1Vehicle_1_1Vehicle.html#aa8694bc77300ae2ff815e9d59f3775e3", null ], - [ "max_lift_coefficient_factor", "classSUAVE_1_1Vehicle_1_1Vehicle.html#a763d9473ea2c6f89f8da5f07a8521adc", null ], + [ "nacelles", "classSUAVE_1_1Vehicle_1_1Vehicle.html#ae4704f435e56947b2a7ce0eea7621023", null ], + [ "networks", "classSUAVE_1_1Vehicle_1_1Vehicle.html#aeae8e8827bbba3e52d519cbf140a3ebf", null ], [ "passengers", "classSUAVE_1_1Vehicle_1_1Vehicle.html#afc67cdf2695b8ecc92f5f067639c3ada", null ], - [ "propulsors", "classSUAVE_1_1Vehicle_1_1Vehicle.html#a50c78d84e282ec3b88d50d5596cdba2c", null ], + [ "payload", "classSUAVE_1_1Vehicle_1_1Vehicle.html#afebfa5278a827144682c786b58939be9", null ], + [ "performance", "classSUAVE_1_1Vehicle_1_1Vehicle.html#a2de4d7b944e7b6b9561afa7018e77e1e", null ], [ "reference_area", "classSUAVE_1_1Vehicle_1_1Vehicle.html#a60668c7b9710b4df0a667ec8e9c0d7dd", null ], [ "systems", "classSUAVE_1_1Vehicle_1_1Vehicle.html#ab8b0b39ab3b930928b161151cacfdc59", null ], [ "tag", "classSUAVE_1_1Vehicle_1_1Vehicle.html#a91d0af7fac13cf22c95a7d085ec96dbf", null ], @@ -24,6 +28,12 @@ var group__Vehicle = [ "center_of_gravity", "classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties.html#ad36a0a734f8ae4b41f05e283661c586f", null ], [ "crew", "classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties.html#a39046a61d2b3ed8b384979511664d599", null ], [ "fuel", "classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties.html#affb84ea67f2a0b653e28e89508600ecb", null ], + [ "generative_design_char_max_bounds", "classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties.html#adc0bef021dc3d87224247bc59763d6e5", null ], + [ "generative_design_char_min_bounds", "classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties.html#a7b2f4e790b10f791ca74b82cf64f8f24", null ], + [ "generative_design_characteristics", "classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties.html#ad0344e991b9ede653865ac7b9ca9e356", null ], + [ "generative_design_max_per_vehicle", "classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties.html#aa3c8f7e9eb55d9d96916a7d8d166fd7c", null ], + [ "generative_design_minimum", "classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties.html#a191eaacd413eff5750357aa1b4f1e51c", null ], + [ "generative_design_special_parent", "classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties.html#aaa9c637e89cbe7a255894b91ce81d938", null ], [ "landing", "classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties.html#a07f79f8b79143a05e0b7ca66682064cf", null ], [ "max_cargo", "classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties.html#af57c262dd32191437d3ee529406e17e9", null ], [ "max_fuel", "classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties.html#ad32f98f3ed16911912400e1b7e24140e", null ], @@ -34,6 +44,7 @@ var group__Vehicle = [ "operating_empty", "classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties.html#ac40e731a21e2e1bb5184af4cdd318b94", null ], [ "passenger", "classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties.html#a68699c58cb0d984fd6d59abb422c659e", null ], [ "payload", "classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties.html#a7626274633166b37c23dd5236ec70925", null ], + [ "tag", "classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties.html#ac4d3be566140d1dceac66e0e54b2f6cd", null ], [ "takeoff", "classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties.html#a5c8f0a58b0892e19cae442c9630423d9", null ], [ "zero_fuel_center_of_gravity", "classSUAVE_1_1Vehicle_1_1Vehicle__Mass__Properties.html#afb63d59caed1c5937f3596caa7feec43", null ] ] ], diff --git a/doxygen/group__components-Lofted__Body__Segment.html b/doxygen/group__components-Lofted__Body__Segment.html new file mode 100644 index 00000000..dad9d3b9 --- /dev/null +++ b/doxygen/group__components-Lofted__Body__Segment.html @@ -0,0 +1,121 @@ + + + + + + + +SUAVE: Lofted_Body_Segment + + + + + + + + + + + + + + + +
+
+ + + + + + + + +
+
SUAVE +  2.5.2 +
+
An Aerospace Vehicle Environment for Designing Future Aircraft
+
+ + + + + + +
+
+
+ + + +
+
+ +
+
+
+ +
+ +
+
+ + +
+ +
+ +
+
+
Lofted_Body_Segment
+
+
+ +

Components traditionally considered to be the fuselage of a vehicle. +More...

+

Components traditionally considered to be the fuselage of a vehicle.

+

These typically contain the primary payload of the vehicle.

+
+
+ + + + diff --git a/doxygen/group__components-fuselages.html b/doxygen/group__components-fuselages.html index c3f20a40..51ef6b6f 100644 --- a/doxygen/group__components-fuselages.html +++ b/doxygen/group__components-fuselages.html @@ -1,9 +1,9 @@ - + - + SUAVE: Fuselages @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@
- +
@@ -73,7 +78,9 @@
@@ -116,7 +123,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/group__components-fuselages.js b/doxygen/group__components-fuselages.js index 46f40db8..93ba1230 100644 --- a/doxygen/group__components-fuselages.js +++ b/doxygen/group__components-fuselages.js @@ -2,6 +2,8 @@ var group__components_fuselages = [ [ "Fuselage", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html", [ [ "__defaults__", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#a13a4cd81f10d72cd1bbfbc756d69ca25", null ], + [ "append_fuel_tank", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#a615394f9cefa0cb72b775efa71dde7b3", null ], + [ "append_segment", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#a71849cc67e000a19806a3a134c8de503", null ], [ "aerodynamic_center", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#a804b9a97a7090359a6ba48d636714e1f", null ], [ "aft_centerbody_area", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#ae569f01643b85dfeb3da55275897144d", null ], [ "aft_centerbody_taper", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#a928c49bd07c05f4e278827f08b0a976f", null ], @@ -10,14 +12,28 @@ var group__components_fuselages = [ "differential_pressure", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#a60e74147869ccd496f8c8185c5d07c09", null ], [ "effective_diameter", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#a79f6884ddd6e0ca4241194b4966d8cf1", null ], [ "fineness", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#afb50945499974ff3306d15d9715bc8f7", null ], + [ "Fuel_Tanks", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#a2b3df4dc373a45db0faa78838b5b39c9", null ], + [ "generative_design_char_max_bounds", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#a786bd2bf623a59a48b6531abcc41f93e", null ], + [ "generative_design_char_min_bounds", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#a012c0557881ba9cb1f9a62c53a77c766", null ], + [ "generative_design_characteristics", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#a8a3e4d4c290d3bd24f6e5ae920dbb72a", null ], + [ "generative_design_max_per_vehicle", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#aab41dc0f6471d0439b4743a509b618ad", null ], + [ "generative_design_minimum", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#a190c2fdb02c38a02cc6bda829401ddd4", null ], [ "heights", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#ae46d1a31c166bca78400a194d3ef3686", null ], [ "lengths", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#acc972f58e4a9f7d1632271f0ed24e1df", null ], + [ "max_per_vehicle", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#a3f3d52098dc33a3f7ce0784c8883cbf5", null ], + [ "non_dimensional_origin", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#a8b7a4f557fcb3743696dd568b15a2b1a", null ], + [ "nose_curvature", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#a2d506f5051ed8803337809e76699aef9", null ], [ "number_coach_seats", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#acc6f517eb0fdec2c551169210492af0c", null ], + [ "origin", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#a2315530edda0fe1b2e9a93f793e50c4b", null ], [ "seat_pitch", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#ab06ac6ecf14ab5ce6b3346d05d2e284d", null ], [ "seats_abreast", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#a779b05b88a125d4ea57d480112384c9f", null ], - [ "Sections", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#a6214ee66b1f87414bc095f9f2587ada7", null ], [ "Segments", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#a60d47dc740536a8703505ce95da44bb3", null ], [ "tag", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#aeb1aab02a525f21939d7b5e5b11375f3", null ], - [ "width", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#a2d18b6bcb752bfb5d39974806c0079e8", null ] + [ "tail_curvature", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#aaef82973d65dfb24addce41293e02253", null ], + [ "vsp_data", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#ac17ea88a9708643456699bf3a980c5fd", null ], + [ "width", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#a2d18b6bcb752bfb5d39974806c0079e8", null ], + [ "x_rotation", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#a9e7dfc07cbbd08d981d59eed910052a4", null ], + [ "y_rotation", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#a57bae7168626693898f7e40286b7fdc9", null ], + [ "z_rotation", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Fuselage.html#af2c1b6de77d2a27de9a07555f29c9f39", null ] ] ] ]; \ No newline at end of file diff --git a/doxygen/group__components-landing__gear.html b/doxygen/group__components-landing__gear.html index bbce636b..dc9adcfd 100644 --- a/doxygen/group__components-landing__gear.html +++ b/doxygen/group__components-landing__gear.html @@ -1,9 +1,9 @@ - + - + SUAVE: Landing Gear @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -91,6 +98,8 @@
+
Landing Gear
@@ -98,6 +107,17 @@

Components considered are the Main and Nose Landing Gear. More...

+ + + + + + + + +

+Classes

class  SUAVE.Components.Landing_Gear.Landing_Gear.Landing_Gear
 
class  SUAVE.Components.Landing_Gear.Main_Landing_Gear.Main_Landing_Gear
 
class  SUAVE.Components.Landing_Gear.Nose_Landing_Gear.Nose_Landing_Gear
 
+

Detailed Description

Components considered are the Main and Nose Landing Gear.

@@ -106,7 +126,7 @@
    + doxygen 1.8.15
diff --git a/doxygen/hierarchy.html b/doxygen/hierarchy.html index 73a34c83..9c982eb5 100644 --- a/doxygen/hierarchy.html +++ b/doxygen/hierarchy.html @@ -1,9 +1,9 @@ - + - + SUAVE: Class Hierarchy @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -97,296 +104,354 @@
This inheritance list is sorted roughly, but not completely, alphabetically:
[detail level 1234567]
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +
 CContainer
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 CSUAVE.Analyses.Process.Process
 CSUAVE.Components.Wings.Main_Wing.Segment_Container
 CSUAVE.Components.Wings.Segment.Segment_Container
 CData
 CSUAVE.Analyses.Analysis.Analysis
 CSUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
 CSUAVE.Analyses.Mission.Segments.Conditions.Conditions.expanded_array
 CSUAVE.Analyses.Settings.Settings
 CSUAVE.Attributes.Airports.Airport.Airport
 CSUAVE.Attributes.Constants.Constant.Constant
 CSUAVE.Attributes.Cryogens.Cryogen.Cryogen
 CSUAVE.Attributes.Gases.Gas.Gas
 CSUAVE.Attributes.Propellants.Propellant.Propellant
 CSUAVE.Attributes.Solids.Solid.Solid
 CSUAVE.Components.Component.Component
 CSUAVE.Components.Costs.Costs.Industrial_Costs
 CSUAVE.Components.Costs.Costs.Operating_Costs
 CSUAVE.Components.Mass_Properties.Mass_Properties
 CDiffed_Data
 CSUAVE.Components.Configs.Config.Config
 CMutableMapping
 CSUAVE.Plugins.pint.compat.ChainMap
 COrderedDict
 CSUAVE.Core.DataOrdered.DataOrdered
@@ -396,7 +461,7 @@

Generated by - doxygen 1.8.14 + doxygen 1.8.15

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"classSUAVE_1_1Components_1_1Component_1_1Container.html", [ - [ "SUAVE.Components.Lofted_Body.CurveContainer", "classSUAVE_1_1Components_1_1Lofted__Body_1_1CurveContainer.html", null ], - [ "SUAVE.Components.Lofted_Body.SectionContainer", "classSUAVE_1_1Components_1_1Lofted__Body_1_1SectionContainer.html", null ], + [ "SUAVE.Components.Lofted_Body.Section_Container", "classSUAVE_1_1Components_1_1Lofted__Body_1_1Section__Container.html", null ], [ "SUAVE.Components.Physical_Component.Container", "classSUAVE_1_1Components_1_1Physical__Component_1_1Container.html", [ + [ "SUAVE.Components.Energy.Networks.Network.Container", "classSUAVE_1_1Components_1_1Energy_1_1Networks_1_1Network_1_1Container.html", null ], [ "SUAVE.Components.Fuselages.Fuselage.Container", "classSUAVE_1_1Components_1_1Fuselages_1_1Fuselage_1_1Container.html", null ], [ "SUAVE.Components.Payloads.Payload.Container", "classSUAVE_1_1Components_1_1Payloads_1_1Payload_1_1Container.html", null ], - [ 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null ], [ "SUAVE.Vehicle.Costs", "classSUAVE_1_1Vehicle_1_1Costs.html", null ], - [ "SUAVE.Vehicle.Vehicle", "classSUAVE_1_1Vehicle_1_1Vehicle.html", null ] + [ "SUAVE.Vehicle.Vehicle", "classSUAVE_1_1Vehicle_1_1Vehicle.html", [ + [ "SUAVE.Components.Configs.Config.Config", "classSUAVE_1_1Components_1_1Configs_1_1Config_1_1Config.html", null ] + ] ] ] ], [ "SUAVE.Plugins.pint.unit.UnitsContainer", "classSUAVE_1_1Plugins_1_1pint_1_1unit_1_1UnitsContainer.html", null ], [ "SUAVE.Plugins.pint.util.ParserHelper", "classSUAVE_1_1Plugins_1_1pint_1_1util_1_1ParserHelper.html", null ] @@ -125,10 +132,11 @@ var hierarchy = [ "ContainerOrdered", null, [ [ "SUAVE.Analyses.Process.Process", "classSUAVE_1_1Analyses_1_1Process_1_1Process.html", [ [ "SUAVE.Analyses.Aerodynamics.Process_Geometry.Process_Geometry", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Process__Geometry_1_1Process__Geometry.html", null ] - ] ] + ] ], + [ "SUAVE.Components.Wings.Main_Wing.Segment_Container", "classSUAVE_1_1Components_1_1Wings_1_1Main__Wing_1_1Segment__Container.html", null ], + [ "SUAVE.Components.Wings.Segment.Segment_Container", "classSUAVE_1_1Components_1_1Wings_1_1Segment_1_1Segment__Container.html", null ] ] ], [ "Data", null, [ - [ "SUAVE.Analyses.Aerodynamics.Results.Results", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Results_1_1Results.html", null ], [ "SUAVE.Analyses.Analysis.Analysis", "classSUAVE_1_1Analyses_1_1Analysis_1_1Analysis.html", [ [ "SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Aerodynamics_1_1Aerodynamics.html", [ [ "SUAVE.Analyses.Aerodynamics.Lifting_Line.Lifting_Line", "classSUAVE_1_1Analyses_1_1Aerodynamics_1_1Lifting__Line_1_1Lifting__Line.html", null ], @@ -151,8 +159,6 @@ var hierarchy = ] ], [ "SUAVE.Analyses.Costs.Costs.Costs", "classSUAVE_1_1Analyses_1_1Costs_1_1Costs_1_1Costs.html", null ], [ "SUAVE.Analyses.Energy.Energy.Energy", "classSUAVE_1_1Analyses_1_1Energy_1_1Energy_1_1Energy.html", null ], - [ "SUAVE.Analyses.Geometry.Geometry.Geometry", "classSUAVE_1_1Analyses_1_1Geometry_1_1Geometry_1_1Geometry.html", null ], - [ "SUAVE.Analyses.Loads.Loads.Loads", "classSUAVE_1_1Analyses_1_1Loads_1_1Loads_1_1Loads.html", null ], [ "SUAVE.Analyses.Mission.Segments.Segment.Segment", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Segment.html", [ [ "SUAVE.Analyses.Mission.Segments.Segment.Container", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Segment_1_1Container.html", null ], [ "SUAVE.Analyses.Mission.Segments.Simple.Simple", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Simple_1_1Simple.html", [ @@ -163,6 +169,7 @@ var hierarchy = [ "SUAVE.Analyses.Mission.Segments.Climb.Constant_Throttle_Constant_Speed.Constant_Throttle_Constant_Speed", "classSUAVE_1_1Analyses_1_1Mission_1_1Segments_1_1Climb_1_1Constant__Throttle__Constant__Speed_1_02b90ea2f234e748373e0a5403527689.html", null ], [ 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SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -112,7 +119,7 @@
    + doxygen 1.8.15
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@@ -57,9 +60,11 @@
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
- +
@@ -73,7 +78,9 @@
@@ -90,20 +97,21 @@
-
+
SUAVE: An Aerospace Vehicle Environment for Designing Future Aircraft

This is the documentation page for SUAVE. For more information on general capabilities, current development efforts, and code/documentation style, please check the main website.

-
+
+ diff --git a/doxygen/md_PULL_REQUEST_TEMPLATE.html b/doxygen/md_PULL_REQUEST_TEMPLATE.html index 7198242a..89ff21bf 100644 --- a/doxygen/md_PULL_REQUEST_TEMPLATE.html +++ b/doxygen/md_PULL_REQUEST_TEMPLATE.html @@ -1,9 +1,9 @@ - + - + SUAVE: # Pull Request Checklist @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
SUAVE -  1.1.0 +  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
@@ -57,9 +60,11 @@ - +
@@ -73,7 +78,9 @@
@@ -90,7 +97,7 @@
-
+
# Pull Request Checklist
@@ -114,14 +121,15 @@
  • Did you update your headers to include your name and date?
  • Do a final compare with the Develop branch to be sure what you're changing
  • -
    + + diff --git a/doxygen/modules.html b/doxygen/modules.html index 2ad60a61..6de40d46 100644 --- a/doxygen/modules.html +++ b/doxygen/modules.html @@ -1,9 +1,9 @@ - + - + SUAVE: Modules @@ -14,13 +14,16 @@ +/* @license-end */ @@ -33,7 +36,7 @@ Logo
    SUAVE -  1.1.0 +  2.5.2
    An Aerospace Vehicle Environment for Designing Future Aircraft
    @@ -57,9 +60,11 @@ - +
    @@ -73,7 +78,9 @@
    @@ -102,144 +109,168 @@  AtmosphericClasses that represent the different types of atmospheres that may be used for analysis  CostsCost Analysis  EnergyThis is the analysis that controls energy network evaluations - GeometryThis is the analysis that controls vehicle geometry evaluations - LoadsThis is the analysis that controls vehicle load evaluations - MissionMission Analyses to setup each part of a mission to fly - SegmentSegment analyses to setup each part of a mission to fly - ClimbSegments for climbing flight - ConditionsThese are analyses files that help setup a mission - CruiseSegments for cruise flight - DescentSegments for descending flight - GroundSegments for ground operations - HoverSegments for VTOL aircraft - Single_PointSingle point segments - Vary_CruiseVariable cruise mission setups - NoiseThese are the analyses that control noise evaluations - SizingThis is the analysis that controls vehicle sizing evaluations - Stability - StructuresThis is the analysis that controls vehicle structure evaluations - WeightsClasses that represent the types of aircraft configuration weight computations + MissionMission Analyses to setup each part of a mission to fly + SegmentSegment analyses to setup each part of a mission to fly + ClimbSegments for climbing flight + ConditionsThese are analyses files that help setup a mission + CruiseSegments for cruise flight + DescentSegments for descending flight + GroundSegments for ground operations + HoverSegments for VTOL aircraft + Single_PointSingle point segments + TransitionSegments for transition flight + Vary_Range_CruiseVariable cruise mission setups + NoiseThese are the analyses that control noise evaluations + PropulsionThese are the analyses that control aerodynamic evaluations + SizingThis is the analysis that controls vehicle sizing evaluations + Stability + WeightsClasses that represent the types of aircraft configuration weight computations  AttributesAttributes provide objects that can be attached to various analyses  AirportsThese are airport related classes - AtmospheresContains basic data for atmospheres - EarthContains basic data for specific Earth atmosphere types - ConstantsContains basic data for atmospheres - GasesCommon gasesclasses - LiquidsCommon liquidsclasses - PlanetsAvailable planetsclasses - PropellantsCommon propellantsclasses - ComponentsComponents are classes that represent objects that are put together to form a vehicle - ConfigsThis is the component that defines the template for vehicle configurations - CostsCost component - EnergyComponents used in energy networks - ConvertersEnergy components meant to be used within an energy network - DistributorsComponents that move energy/control energy/power in a network - NetworksComponents used in energy networks - PeripheralsThese are components that use energy but are otherwise not part of a network - ProcessesThese are components that use energy to perform a process - StoragesEnergy components that store energy (such as batteries) - BatteriesContains different battery types, separated into variable mass (metal-air) and constant mass batteries - Constant_MassContains different battery types that don't change mass, such as lithium-ion and lithium-sulfur batteries - Variable_MassContains different battery types that don't change mass, such as lithium-air and aluminum-air batteries - FuselagesComponents traditionally considered to be the fuselage of a vehicle - Landing GearComponents considered are the Main and Nose Landing Gear - PayloadsAvailable payload componentsinit.py - PropulsorsThese are the components used to provide thrust to a vehicle - SystemsThese are the components which define a vehicle's onboard systems - Wingsinit.py - Airfoilsinit.py - CoreCore is all the under the hood magic that makes SUAVE work - Input_OutputThese functions provide SUAVE data storage capabilities and capabilities to work with files for other programs - D3JSFiles to handle D3JS output - FreeMindFunction to save FreeMind output - GMSHFunctions needed to work with GMSH - OpenVSPFunctions needed to work with OpenVSP - ResultsMiscellaneous functions to print results - SU2Functions needed to interface with SU2 - SUAVEFunctions needed to save SUAVE data structures in JSON form - XMLFiles to handle XML input and output - MethodsMethods provide the functions needed to perform analyses - AerodynamicsAerodynamic methods contain the functions for the aerodynamic analyses - AERODASFunctions to perform calculations according to AERODAS models - AVLFunctions to AVL calculations - Data - CommonThese are methods that are used by several analyses - Fidelity_ZeroLow-fidelity methods that are used by many analyses - DragDrag methods that are directly specified by analyses - Helper_FunctionsFunctions that are needed by aerodynamics methods - LiftLift methods that are directly specified by analyses - Fidelity_ZeroFunctions to perform low-fidelity calculations - LiftFunctions to perform low-fidelity lift calculations - Lifting_LineFunctions to perform lifting line calculations - OpenVSP_Wave_DragFunctions to perform wave drag calculations using OpenVSP - Supersonic_ZeroFunctions to perform low-fidelity calculations including supersonics - DragFunctions to perform low-fidelity drag calculations including supersonic - LiftFunctions to perform low-fidelity lift calculations for supersonics - Center_of_GravityDescription - CostsThis contains functions that can compute costs associated with building and operating an aircraft - Industrial CostsThese functions provide cost estimates for an aircraft program - Operating CostsThis is a stub for computing operating costs - Flight_DynamicsDescription - Dynamic_Stability - Approximations - Full_Linearized_Equations - Supporting_Functions - Static_Stability - Approximations - Supporting_Functions - Tube_Wing - GeometryThese methods are primarily used for sizing - Three DimensionalGeometry functions for three dimensions - Two DimensionalGeometry functions for two dimensions - Cross SectionGeometry functions for two dimensional cross sections - AirfoilGeometry functions for two dimensional airfoils - PropulsionGeometry functions for two dimensional propulsion measurements - PlanformGeometry functions for two dimensional planforms - MissionsMission methods contain the functions for setting up and solving a mission - SegmentsMission Segment folders containing the functions for setting up and solving a mission - ClimbClimb mission methods containing the functions for setting up and solving a mission - CommonClimb mission methods containing the functions for setting up and solving a mission - CruiseCruise mission methods containing the functions for setting up and solving a mission - DescentDescent mission methods containing the functions for setting up and solving a mission - GroundDescent mission methods containing the functions for setting up and solving a mission - HoverHover mission methods containing the functions for setting up and solving a mission - Single_PointSingle Point mission methods containing the functions for setting up and solving a mission - NoiseDescription - CorrelationsCorrelation type methods for calculating noise - Fidelity_OneDescription - AirframeFidelity One level noise calculations for the airframe components - EngineFidelity One level noise calculations for the engine - Noise ToolsVarious functions that are used to calculate noise using the fidelity one level - PerformanceThis is a set of basic aircraft performance estimation functions - PowerPower methods contain the functions for electric systems such as batteries and fuel cells - BatteryFunctions pertaining to battery discharge and sizing - DischargeFunctions to evaluate battery discharge losses and voltage requirements - RagoneFunctions to evaluate a Ragone of the battery - SizingFunctions to size battery from mass, specific energy, and specific power - Variable_MassFunctions pertaining to variable mass batteries (such as metal air) - Fuel_CellFuel_Cell methods contain the functions for the fuel cell analyses - ChemistryFuel_Cell methods contain the functions for the fuel cell analyses - DischargeFunctions to evaluate fuel cell discharge losses and voltage requirements - SizingFuel_Cell methods contain the functions for the fuel cell analyses - PropulsionDescription - UtilitiesThese provide functionality that is not easily grouped into another set - ChebyshevThese functions provide methods for discrete derivative and integral calculations - WeightsWeights methods provide different means of estimating vehicle weight breakdowns - CorrelationsCorrelation methods provide component weight breakdowns for different vehicle configurations based on regressed data - BWBProvides structural weight correlations for a BWB concept - CommonProvides structural weight correlations for aircraft components applicable to all aircraft configurations - GenerationalProvides structural and component weight correlations for general aviation aircraft - Human_PoweredProvides structural weight correlations for a human-powered aircraft; applicable to solar-UAVs - PropulsionContains some methods for calculating different propulsion system weights - Tube_WingProvides structural weight correlations for a tube and wing aircraft - UAVProvides structural weight correlations for UAVs - OptimizationThe files that help you setup an optimization problem - Package_SetupsIndividual package setups that help you interface with other codes - TRMMTrust Region Model Management Scripts live here - PluginsThese are external packages that have been incorporated into SUAVE - SizingSizing provides methods to size a vehicle's mass, battery energy(s), and power based on its geometric properties and mission - SurrogateSurrogate provides methods for different surrogate formulations of the original problem - VehicleVehicle.py + AtmospheresContains basic data for atmospheres + EarthContains basic data for specific Earth atmosphere types + ConstantsContains basic data for atmospheres + CryogensCommon Cryogensclasses + GasesCommon gasesclasses + PlanetsAvailable planetsclasses + PropellantsCommon propellantsclasses + Solids + ComponentsComponents are classes that represent objects that are put together to form a vehicle + Airfoils + ConfigsThis is the component that defines the template for vehicle configurations + CostsCost component + EnergyComponents used in energy networks + Charging + ConvertersEnergy components meant to be used within an energy network + CoolingComponents that cryogenically cool others + DistributorsComponents that move energy/control energy/power in a network + NetworksComponents used in energy networks + PeripheralsThese are components that use energy but are otherwise not part of a network + ProcessesThese are components that use energy to perform a process + StoragesEnergy components that store energy (such as batteries) + BatteriesContains different battery types, separated into variable mass (metal-air) and constant mass batteries + Constant_MassContains different battery types that don't change mass, such as lithium-ion and lithium-sulfur batteries + Variable_MassContains different battery types that don't change mass, such as lithium-air and aluminum-air batteries + Fuel_TanksContains different fuel tank types + FuselagesComponents traditionally considered to be the fuselage of a vehicle + Landing GearComponents considered are the Main and Nose Landing Gear + Lofted_Body_SegmentComponents traditionally considered to be the fuselage of a vehicle + NacellesThese typically contain the primary payload of the vehicle + PayloadsAvailable payload componentsinit.py + SystemsThese are the components which define a vehicle's onboard systems + Wingsinit.py + Control_Surfacesinit.py + CoreCore is all the under the hood magic that makes SUAVE work + Input_OutputThese functions provide SUAVE data storage capabilities and capabilities to work with files for other programs + D3JSFiles to handle D3JS output + FreeMindFunction to save FreeMind output + GMSHFunctions needed to work with GMSH + OpenVSPFunctions needed to work with OpenVSP + ResultsMiscellaneous functions to print results + SU2Functions needed to interface with SU2 + SUAVEFunctions needed to save SUAVE data structures in JSON form + XMLFiles to handle XML input and output + MethodsMethods provide the functions needed to perform analyses + AerodynamicsAerodynamic methods contain the functions for the aerodynamic analyses + AERODASFunctions to perform calculations according to AERODAS models + Airfoil_Panel_Method + AVLFunctions to AVL calculations + Data + CommonThese are methods that are used by several analyses + Fidelity_ZeroLow-fidelity methods that are used by many analyses + DragDrag methods that are directly specified by analyses + Helper_FunctionsFunctions that are needed by aerodynamics methods + LiftLift methods that are directly specified by analyses + Gas_DymamicsGas Dynamics methods that are directly specified by analyses + Fidelity_ZeroFunctions to perform low-fidelity calculations + LiftFunctions to perform low-fidelity lift calculations + Lifting_LineFunctions to perform lifting line calculations + OpenVSP_Wave_DragFunctions to perform wave drag calculations using OpenVSP + Supersonic_ZeroFunctions to perform low-fidelity calculations including supersonics + DragFunctions to perform low-fidelity drag calculations including supersonic + Center_of_GravityDescription + CoolingCooling methods contain the functions for cryogenic systems such as Cryocoolers and cryogen cooling + CryogenCooling by liquid (or gaseous) cryogen + ConsumptionFunctions to evaluate the use of cryogen to provide cooling power + CostsThis contains functions that can compute costs associated with building and operating an aircraft + Industrial CostsThese functions provide cost estimates for an aircraft program + Operating CostsThis is a stub for computing operating costs + Flight_DynamicsDescription + Dynamic_Stability + Approximations + Full_Linearized_Equations + Supporting_Functions + Static_Stability + Approximations + Supporting_Functions + Tube_Wing + GeometryThese methods are primarily used for sizing + Three DimensionalGeometry functions for three dimensions + Two DimensionalGeometry functions for two dimensions + Cross SectionGeometry functions for two dimensional cross sections + AirfoilGeometry functions for two dimensional airfoils + PropulsionGeometry functions for two dimensional propulsion measurements + PlanformGeometry functions for two dimensional planforms + MissionsMission methods contain the functions for setting up and solving a mission + SegmentsMission Segment folders containing the functions for setting up and solving a mission + ClimbClimb mission methods containing the functions for setting up and solving a mission + CommonClimb mission methods containing the functions for setting up and solving a mission + CruiseCruise mission methods containing the functions for setting up and solving a mission + DescentDescent mission methods containing the functions for setting up and solving a mission + GroundDescent mission methods containing the functions for setting up and solving a mission + HoverHover mission methods containing the functions for setting up and solving a mission + Single_PointSingle Point mission methods containing the functions for setting up and solving a mission + TransitionTransition mission methods containing the functions for setting up and solving a mission + NoiseDescription + Certification + Fidelity_OneDescription + AirframeFidelity One level noise calculations for the airframe components + EngineFidelity One level noise calculations for the engine + Noise ToolsVarious functions that are used to calculate noise using the fidelity one level + Zero Fidelity ZeroCorrelation type methods for calculating noise + Fidelity_ZeroCorrelation type methods for calculating noise + PerformanceThis is a set of basic aircraft performance estimation functions + PowerPower methods contain the functions for electric systems such as batteries and fuel cells + BatteryFunctions pertaining to battery discharge and sizing + State_Estimation_ModelsFunctions to evaluate battery state variables + RagoneFunctions to evaluate a Ragone of the battery + SizingFunctions to size battery from mass, specific energy, and specific power + Variable_MassFunctions pertaining to variable mass batteries (such as metal air) + Fuel_CellFuel_Cell methods contain the functions for the fuel cell analyses + DischargeFunctions to evaluate fuel cell discharge losses and voltage requirements + SizingFuel_Cell methods contain the functions for the fuel cell analyses + TurboelectricTurboelectric methods contain the functions for investigating vehicle electric power supplied by a turboelectric powertrain + DischargeFunctions to evaluate the use of a turboelectric powertrain to provide electric power + SizingTurboelectric methods contain the functions for analyses where a turboelectric powertrain provieds the required electric power + PropulsionDescription + Rotor_WakeRotor_Wake provides the functions needed to perform analyses + Fidelity_OneRotor wake methods that are directly specified by analyses + Fidelity_ZeroRotor wake methods that are directly specified by analyses + UtilitiesThese provide functionality that is not easily grouped into another set + ChebyshevThese functions provide methods for discrete derivative and integral calculations + WeightsWeights methods provide different means of estimating vehicle weight breakdowns + BuildupsBuildup weight methods provide weight breakdowns for vehicles based on part-by-part sizing + CommonThe Common buildup methods are those which are shared between vehicle types utilizing buildup weight methods + EVTOLThe empty method that is called by the analysis + CorrelationsCorrelation methods provide component weight breakdowns for different vehicle configurations based on regressed data + BWBProvides structural weight correlations for a BWB concept + CommonProvides structural weight correlations for aircraft components applicable to all aircraft configurations + Methods-Weights-Correlations-FLOPSProvides structural weight correlations for aircraft components based on the FLOPS method + GenerationalProvides structural and component weight correlations for general aviation aircraft + Human_PoweredProvides structural weight correlations for a human-powered aircraft; applicable to solar-UAVs + PropulsionContains some methods for calculating different propulsion system weights + Methods-Weights-Correlations-RaymerProvides structural weight correlations for aircraft components based on the Raymer method + Tube_WingProvides structural weight correlations for a tube and wing aircraft + UAVProvides structural weight correlations for UAVs + OptimizationThe files that help you setup an optimization problem + Package_SetupsIndividual package setups that help you interface with other codes + TRMMTrust Region Model Management Scripts live here + PlotsPlots contains functions for generating common figures + GeometryDescription + PerformancePlots contains functions for generating common figures + PluginsThese are external packages that have been incorporated into SUAVE + SurrogateSurrogate provides methods for different surrogate formulations of the original problem + VehicleVehicle.py
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a:hover,.sm-dox.sm-vertical ul a:focus,.sm-dox.sm-vertical ul a:active,.sm-dox.sm-vertical ul a.highlighted{background:#eee}.sm-dox.sm-vertical ul a.disabled{background:#fff}} \ No newline at end of file diff --git a/email/.DS_Store b/email/.DS_Store new file mode 100644 index 00000000..5008ddfc Binary files /dev/null and b/email/.DS_Store differ diff --git a/email/email_v03.html b/email/email_v03.html index 388721c7..d6a9eb2a 100644 --- a/email/email_v03.html +++ b/email/email_v03.html @@ -190,7 +190,7 @@
    -
    +

    To all of our SUAVE friends,

    @@ -229,7 +229,7 @@

    - Download the latest release here + Download the latest release here
    @@ -272,7 +272,7 @@

    The SUAVE Team

    -

    Having trouble viewing this email? View it as a webpage.

    +

    Having trouble viewing this email? View it as a webpage.

    SUAVE is maintained by the Aerospace Design Lab in the Department of Aeronautics and Astronautics at Stanford University and is released under an open-source license (CC BY-NC-SA 4.0). This list is only used to disseminate important information and updates regarding our software. The development team respects your privacy, and should you wish, you can unsubscribe from our email list. diff --git a/email/email_v09.html b/email/email_v09.html index c1e91ff0..6ab87952 100644 --- a/email/email_v09.html +++ b/email/email_v09.html @@ -190,7 +190,7 @@
    -
    +

    To all of our SUAVE friends,

    @@ -221,7 +221,7 @@

    The big improvements for version 0.9 are:

    - Download the latest release here + Download the latest release here
    @@ -264,7 +264,7 @@

    The SUAVE Team

    -

    Having trouble viewing this email? View it as a webpage.

    +

    Having trouble viewing this email? View it as a webpage.

    SUAVE is maintained by the Aerospace Design Lab in the Department of Aeronautics and Astronautics at Stanford University and is released under an open-source license (LGPL v2.1). This list is only used to disseminate important information and updates regarding our software. The development team respects your privacy, and should you wish, you can unsubscribe from our email list. diff --git a/email/email_v100.html b/email/email_v100.html index 5e5f2c8b..62533c46 100644 --- a/email/email_v100.html +++ b/email/email_v100.html @@ -190,7 +190,7 @@
    -
    +

    To the SUAVE aerospace designers,

    @@ -221,7 +221,7 @@

    The big new features for version 1.0.0 are:

    - Download SUAVE 1.0.0 + Download SUAVE 1.0.0
    @@ -264,7 +264,7 @@

    The SUAVE Team

    -

    Having trouble viewing this email? View it as a webpage.

    +

    Having trouble viewing this email? View it as a webpage.

    SUAVE is maintained by the Aerospace Design Lab in the Department of Aeronautics and Astronautics at Stanford University and is released under an open-source license (LGPL v2.1). This list is only used to disseminate important information and updates regarding our software. The development team respects your privacy, and should you wish, you can unsubscribe from our email list. diff --git a/email/email_v200.html b/email/email_v200.html new file mode 100644 index 00000000..cc658496 --- /dev/null +++ b/email/email_v200.html @@ -0,0 +1,288 @@ + + + + +SUAVE v2.0.0 Release + + + + + + + + + + + + +
    + + +
    + + + + +
    +
    +

    +

    +

    To the SUAVE community,

    + +

    Our Valentine’s Gift to you is SUAVE 2! The development team has lovingly coded this latest release of SUAVE in Python 3. This represents months of hard work and over 500 commits since the last release. We suggest you upgrade to take advantage of these changes.

    +

    The big new features for version 2.0 are:

    + +
      +
    • Python 3
    • +
    • Better integration with OpenVSP
    • +
    • More flexible AVL integration
    • +
    • Under the hood speed improvements
    • +
    • Ramjets, Scramjets, and Rockets
    • +
    • Weight methodologies for eVTOL
    • +
    • Fuel Tank CGs
    • +
    • Supersonic upgrades
    • +
    • Better Fuselage Segmentation
    • +
    • PyOptSparse interface
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    + + + + + + + + + + + + + + \ No newline at end of file diff --git a/forum.md b/forum.md deleted file mode 100644 index 3ace76af..00000000 --- a/forum.md +++ /dev/null @@ -1,23 +0,0 @@ ---- -layout: page -title: Forum -subtitle: Together we design exotic aerospace configurations - -permalink: /forum/ ---- - - - - - diff --git a/guides/.DS_Store b/guides/.DS_Store new file mode 100644 index 00000000..d0607452 Binary files /dev/null and b/guides/.DS_Store differ diff --git a/guides/_posts/2014-03-15-AVL_Tutorial.md b/guides/_posts/2014-03-15-AVL_Tutorial.md deleted file mode 100644 index bb2d7ce3..00000000 --- a/guides/_posts/2014-03-15-AVL_Tutorial.md +++ /dev/null @@ -1,98 +0,0 @@ ---- -layout: post -title: AVL - Boeing 737-800 -date: 2014-03-14 13:25:00 -categories: blog -description: Setup and analyze an aircraft using Athena Vortex Lattice (AVL) - -permalink: /guides/AVL_Tutorial.html ---- - - - - - -## Boeing 737 Using AVL - -SUAVE was built upon the philosophy of creating a conceptualizing space that enables the user to have maximum design, -analysis and optimization flexibility. In SUAVE, the aerodynamics and stability module is set up to permit multiple fidelity -levels of analysis. The addition of Athena Vortex Lattice (AVL), a vortex lattice method (VLM) code developed by Professor -Mark Drela at MIT, extends SUAVE aerodynamic and stability analysis of aircraft configurations whose geometry have prior -posed difficulty in obtaining accurate results. Examples include oblique wings, joined wings, canard configurations and -blended-wing-bodies (BWB). For this example we use the Boeing 737-800 used in the Boeing 737-800 Tutorial. - -### Downloading AVL -The tutorial assumes that AVL is available on your machine and can be called using just “avl” in the command line. AVL can be downloaded [here](http://web.mit.edu/drela/Public/web/avl/) for all platforms. - -### Steps to simulate the aircraft's performance over a mission -1. Locate the folder where you have the tutorial repository. If using the command line, cd to this directory. -2. Open the tut_mission_B737_AVL.py script in your favorite editor or IDE. The script is setup to run the B737 on its design -mission. Run it in your IDE. If using the command line use the command. - -
     python tut_mission_B737_800_AVL.py  
    - -It is very simple to interchange analysis tools in SUAVE. AVL is no exception. To study an aircraft in SUAVE using AVL, simply change the two lines in the analysis_set up shown below form Fidelity_Zero (SUAVE’s first order approximation method) to AVL. - -Replace line 109 -
     aerodynamics = SUAVE.Analyses.Aerodynamics.Fidelity_Zero() 
    -with -
      aerodynamics = SUAVE.Analyses.Aerodynamics.AVL() 
    - -SUAVE launches AVL from the command line, runs analyses and then reads in the files. This process is done automatically. All -subroutines described later in this tutorial are done in the background. Since running a full stability analysis at each -point in the mission can be extremely expensive, a surrogate model is built for the aerodynamic coefficients, stability -derivatives, and neutral point locations by running through a set of representative angles of attack and mach numbers. - -3. A few plots depicting the variation of the different aircraft performance parameters over the course of the mission are shown. - -### Important Functions: -The important functions used in this tutorial are exactly the same as the ones used in the Boeing Boeing 737-800 Analysis -Tutorial. Refer to this section in this tutorial [here](http://suave.stanford.edu/guides/boeing_737-800.html). -### Subroutines Unique to SUAVE-AVL -*Excluding the functions **tut_mission_B737_AVL.py** script, all of the subroutine python scripts described below are located -in the SUAVE/Methods/Aerodynamics/AVL repository*. -#### Geometry Creation - Wing -Parameters defining the aircraft geometry in the in the vehicle_setup() are translated to an AVL file format using embedded -subroutines. Shown below is an example of the translation of the wing geometry from the vehicle-setup() function to AVL file -format. -1. Firstly, if the wing defined by segments, a data structure is created to store the geometry parameters (chord length,twist,span location) of the beginning and end of each segment. For example the 737-800 wing below will be divided into three segments - yehudi, inboard and outboard wing). -2. Secondly, if control surfaces are defined either the full wing or its segments, the data structure created in step 1 is -further divided into sections at instances where the control surfaces begin and end. This is shown images below. - - - -The above steps describing wing geometry parameterization are found in **create_avl_datasturcture.py** script. Along with -the creation of wing geometry, the SAUVE-AVL wrapper allows the user to refine the accuracy of the analysis by modifying the -vortex spacing placed on the wings. The number of chordwise/spanwise horseshoe vertices can also be modified. This is located in the Analyses/Aerodynamics/**AVL_Inviscid.py** (for Aerodynamics) and Analyses/Stability/**AVL.py** (for Stability) scripts below. -
      # Default spanwise vortex density 
    -  self.settings.spanwise_vortex_density  = 1.5
    -
    - -#### Geometry Creation - Fuselage -Despite AVL having the capability of modelling bodies, a decision was made to model the fuselage as a wake-producing, lifting surface. The entire body is defined by a series of vertical and horizontal chords that create a cross when viewed from the front. - -#### Defining Flight Conditions -This is done in the **translate_data.py** script which translates flight conditions parameters defined in the -**mission_setup()** to an AVL data structure to be used in run cases. This script also stores AVL results into SUAVE’s -results data structures. -#### Writing Run Cases -Uses information in the AVL run case data structure created in **translate_data.py** to write an AVL format run case to be -used by the AVL executable. This is done in **write_run_cases.py** script. -#### Writing Commend Instructions for AVL executable -This is a sequence of commands used to load AVL files into the executable, perform aerodynamic and stability analyses, and -save results. This is done in **write_input_deck.py** script. -#### Reading Results -Opens saved AVL result files and stores data in a data structure used to create aerodynamic and stability surrogate models. -This is done in **read_results.py** script. - -### Results -The plots shown below should be generated if the mission analysis executes correctly. The results show the aerodynamic, propulsion and mission properties of the B737-800 for the defined mission. - - -![B737 mission](/images/B737_AVL_Altitude_sfc_weight.png) - -![B737 Aerodynamics](/images/B737_AVL_Aerodynamic_Coefficients.png) - -![B737 Propulsion](/images/B737_AVL_Aerodynamic_Forces.png) - -![B737 Drag](/images/B737_AVL_Drag_Components.png) diff --git a/guides/_posts/2015-01-01-BWB_tutorial.md b/guides/_posts/2015-01-01-BWB_tutorial.md deleted file mode 100644 index 98897dab..00000000 --- a/guides/_posts/2015-01-01-BWB_tutorial.md +++ /dev/null @@ -1,224 +0,0 @@ ---- -layout: post -title: Blended Wing Body with CFD -date: 2015-06-13 23:22:21 -categories: blog -description: Run an unconventional configuration with SU2! - -permalink: /guides/BWB.html ---- - - - - - -## Blended Wing Body using CFD - -The purpose of this tutorial is to show the analysis settings used to generate geometry, a mesh, and run CFD via SU2 from SUAVE. It will also show how to add individual wing segments. We assume you are familiar with SUAVE and have some CFD experience already. For this example we use a Blended Wing Body (BWB). The BWB used here is similar to the Boeing BWB-450 by Liebeck. - -# Other Software You need - -For the full tool chain 3 additional pieces of software are needed. These are OpenVSP, Gmsh, and SU2. These are all open source and freely available online. - -First, you will need [OpenVSP](http://openvsp.org) compiled with Python support. Unfortunately, you cannot use the precompiled binary versions of OpenVSP. You must compile it from scratch. This tutorial was tested with version 3.15.0. - -Second, you must install [Gmsh](http://gmsh.info). In this case you can use the precompiled binaries. Make sure to add Gmsh to your command line path so it can be called from the terminal. This tutorial was tested with version 3.0.6. - -Finally, you need to install [SU2](https://su2code.github.io/). If you want parallel support then you must also compile the code. Otherwise, you can the precompiled versions. This tutorial was tested with version 6.0.0. - -# Vehicle Setup - -Here we see how to construct multi-segment wings. With multiple segments we can build more complex shapes such as cranks, yehudis, and winglets. We also show how to specify an airfoil on the wing or on a wing segment. If an airfoil is not specified, it will default to a symmertic airfoil. - -This BWB is broken down into 7 segments. We first specify the top level parameters of the wing and then add each segment sequentially as shown below. - -
    
    -
    -
    -    # ------------------------------------------------------------------        
    -    #   Main Wing
    -    # ------------------------------------------------------------------        
    -
    -    wing = SUAVE.Components.Wings.Main_Wing()
    -    wing.tag = 'main_wing'
    -
    -    wing.aspect_ratio            = 289.**2 / (7840. * 2)
    -    wing.thickness_to_chord      = 0.15
    -    wing.taper                   = 0.0138
    -    wing.span_efficiency         = 0.95
    -    wing.spans.projected         = 289.0 * Units.feet    
    -    wing.chords.root             = 145.0 * Units.feet
    -    wing.chords.tip              = 3.5   * Units.feet
    -    wing.chords.mean_aerodynamic = 86.   * Units.feet
    -    wing.areas.reference         = 15680. * Units.feet**2   
    -    wing.sweeps.quarter_chord    = 33. * Units.degrees
    -    wing.twists.root             = 0.0 * Units.degrees
    -    wing.twists.tip              = 0.0 * Units.degrees
    -    wing.dihedral                = 2.5 * Units.degrees
    -    wing.origin                  = [0.,0.,0]
    -    wing.aerodynamic_center      = [0,0,0] 
    -    wing.vertical                = False
    -    wing.symmetric               = True
    -    wing.high_lift               = True
    -    wing.dynamic_pressure_ratio  = 1.0
    -
    -    segment = SUAVE.Components.Wings.Segment()
    -    segment.tag                   = 'section_1'
    -    segment.percent_span_location = 0.0
    -    segment.twist                 = 0. * Units.deg
    -    segment.root_chord_percent    = 1.
    -    segment.dihedral_outboard     = 0. * Units.degrees
    -    segment.sweeps.quarter_chord  = 30.0 * Units.degrees
    -    segment.thickness_to_chord    = 0.165 
    -    wing.Segments.append(segment)    
    -    
    -    segment = SUAVE.Components.Wings.Segment()
    -    segment.tag                   = 'section_2'
    -    segment.percent_span_location = 0.052
    -    segment.twist                 = 0. * Units.deg
    -    segment.root_chord_percent    = 0.921
    -    segment.dihedral_outboard     = 0.   * Units.degrees
    -    segment.sweeps.quarter_chord  = 52.5 * Units.degrees
    -    segment.thickness_to_chord    = 0.167    
    -    wing.Segments.append(segment)   
    -
    -    segment = SUAVE.Components.Wings.Segment()
    -    segment.tag                   = 'section_3'
    -    segment.percent_span_location = 0.138
    -    segment.twist                 = 0. * Units.deg
    -    segment.root_chord_percent    = 0.76
    -    segment.dihedral_outboard     = 1.85 * Units.degrees
    -    segment.sweeps.quarter_chord  = 36.9 * Units.degrees  
    -    segment.thickness_to_chord    = 0.171    
    -    wing.Segments.append(segment)   
    -    
    -    segment = SUAVE.Components.Wings.Segment()
    -    segment.tag                   = 'section_4'
    -    segment.percent_span_location = 0.221
    -    segment.twist                 = 0. * Units.deg
    -    segment.root_chord_percent    = 0.624
    -    segment.dihedral_outboard     = 1.85 * Units.degrees
    -    segment.sweeps.quarter_chord  = 30.4 * Units.degrees    
    -    segment.thickness_to_chord    = 0.175
    -    wing.Segments.append(segment)       
    -    
    -    segment = SUAVE.Components.Wings.Segment()
    -    segment.tag                   = 'section_5'
    -    segment.percent_span_location = 0.457
    -    segment.twist                 = 0. * Units.deg
    -    segment.root_chord_percent    = 0.313
    -    segment.dihedral_outboard     = 1.85  * Units.degrees
    -    segment.sweeps.quarter_chord  = 30.85 * Units.degrees
    -    segment.thickness_to_chord    = 0.118
    -    wing.Segments.append(segment)       
    -    
    -    segment = SUAVE.Components.Wings.Segment()
    -    segment.tag                   = 'section_6'
    -    segment.percent_span_location = 0.568
    -    segment.twist                 = 0. * Units.deg
    -    segment.root_chord_percent    = 0.197
    -    segment.dihedral_outboard     = 1.85 * Units.degrees
    -    segment.sweeps.quarter_chord  = 34.3 * Units.degrees
    -    segment.thickness_to_chord    = 0.10
    -    wing.Segments.append(segment)     
    -    
    -    segment = SUAVE.Components.Wings.Segment()
    -    segment.tag                   = 'section_7'
    -    segment.percent_span_location = 0.97
    -    segment.twist                 = 0. * Units.deg
    -    segment.root_chord_percent    = 0.086
    -    segment.dihedral_outboard     = 73. * Units.degrees
    -    segment.sweeps.quarter_chord  = 55. * Units.degrees
    -    segment.thickness_to_chord    = 0.10
    -    wing.Segments.append(segment)      
    -
    -    # add to vehicle
    -    vehicle.append_component(wing)
    -
    -
    - -Once we build the vehicle we can write the OpenVSP file. If there are multiple configurations then you will need multiple writes to OpenVSP. We highly suggest you only have one configuration when possible to minimize computational costs. Also note that while the tip section was not defined here (meaning the top level tip values were used), it can also be added with `segment.percent_span_location = 1.`. - -
    
    -# ----------------------------------------------------------------------
    -#   Define the Configurations
    -# ---------------------------------------------------------------------
    -
    -def configs_setup(vehicle):
    -
    -    # ------------------------------------------------------------------
    -    #   Initialize Configurations
    -    # ------------------------------------------------------------------
    -
    -    configs = SUAVE.Components.Configs.Config.Container()
    -
    -    base_config = SUAVE.Components.Configs.Config(vehicle)
    -    base_config.tag = 'base'
    -    configs.append(base_config)
    -    
    -    write(vehicle,base_config.tag) 
    -
    -
    -    # done!
    -    return configs
    -
    -
    - -# Analyses Setup - -Here we setup the SU2 analysis. We commented out the parallel setting but you may use these if you want to parallelize the computation. - -The next setting which is commented out is the input file for pregenerated CFD data. We have included an example of this, so even if you don't have SU2 and Gmsh installed you can still run this file to generate the surrogate and run the mission. A 10 iteration limit is used so that the tutorial can be run in a reasonable amount of time (~15 min). Data for runs with the 10 iteration limit and 1500 iteration limit are provided. - -After that we specify the points we want to use to generate the SU2-based lift surrogate. SUAVE has default values for these, but we suggest the user specify their own Mach numbers and angles of attack. - -Next we set up a bit of mesh refinement by modifying the source parameters at specific segments. Here we reduce the source length in the root area which refines the mesh there. This is optional as sources will also be added by default if these options are not specified. - -
    
    -
    -    # ------------------------------------------------------------------
    -    #  Aerodynamics Analysis
    -    aerodynamics = SUAVE.Analyses.Aerodynamics.SU2_Euler()
    -    aerodynamics.geometry = vehicle
    -    
    -    #aerodynamics.process.compute.lift.inviscid.settings.parallel   = True
    -    #aerodynamics.process.compute.lift.inviscid.settings.processors = 12  
    -    #aerodynamics.process.compute.lift.inviscid.training_file       = 'base_data_1500.txt'
    -    aerodynamics.process.compute.lift.inviscid.settings.maximum_iterations = 10
    -    aerodynamics.settings.drag_coefficient_increment = 0.0000
    -    
    -    aerodynamics.process.compute.lift.inviscid.training.Mach             = np.array([.3, .5, .7, .85]) 
    -    aerodynamics.process.compute.lift.inviscid.training.angle_of_attack  = np.array([0.,3.,6.]) * Units.deg    
    -    
    -    wing_segments = vehicle.wings.main_wing.Segments
    -    wing_segments.section_1.vsp_mesh = Data()
    -    wing_segments.section_1.vsp_mesh.inner_radius  = 4.
    -    wing_segments.section_1.vsp_mesh.outer_radius  = 4.
    -    wing_segments.section_1.vsp_mesh.inner_length  = .14
    -    wing_segments.section_1.vsp_mesh.outer_length  = .14
    -    
    -    wing_segments.section_2.vsp_mesh = Data()
    -    wing_segments.section_2.vsp_mesh.inner_radius  = 4.
    -    wing_segments.section_2.vsp_mesh.outer_radius  = 4.
    -    wing_segments.section_2.vsp_mesh.inner_length  = .14
    -    wing_segments.section_2.vsp_mesh.outer_length  = .14
    -    
    -    wing_segments.section_3.vsp_mesh = Data()
    -    wing_segments.section_3.vsp_mesh.inner_radius  = 4.
    -    wing_segments.section_3.vsp_mesh.outer_radius  = 4.
    -    wing_segments.section_3.vsp_mesh.inner_length  = .14
    -    wing_segments.section_3.vsp_mesh.outer_length  = .14
    -    
    -    wing_segments.section_4.vsp_mesh = Data()
    -    wing_segments.section_4.vsp_mesh.inner_radius  = 4.
    -    wing_segments.section_4.vsp_mesh.outer_radius  = 2.8
    -    wing_segments.section_4.vsp_mesh.inner_length  = .14
    -    wing_segments.section_4.vsp_mesh.outer_length  = .14      
    -    
    -    analyses.append(aerodynamics)
    -
    -
    -
    - - -The rest of the code runs as usual. However, we add in an extra plot which shows the surrogate and the points that were used to build it. diff --git a/guides/_posts/2015-06-14-Boeing_737-800.md b/guides/_posts/2015-06-14-Boeing_737-800.md deleted file mode 100644 index 5a1cb823..00000000 --- a/guides/_posts/2015-06-14-Boeing_737-800.md +++ /dev/null @@ -1,300 +0,0 @@ ---- -layout: post -title: Boeing 737-800 -date: 2016-02-14 13:25:00 -categories: blog -description: Setup and analyze a conventional aircraft configuration - -permalink: /guides/boeing_737-800.html ---- - - - - - -## Boeing 737-800 Analysis Tutorial - -This tutorial shows how the user can setup a conventional configuration aircraft, a mission the aircraft is to fly, and then simulate the aircraft's performance over the defined mission. The code is divided into a number of functions that are called from the main function. - -### Steps to simulate the aircraft's performance over a mission : - -1) Locate the folder where you have the tutorial repository. If using the command line, cd to this directory. - -2) Open the tut_mission_B737.py script in your favorite editor or IDE. The script is setup to run the B737 on its design mission. Run it in your IDE. If using the command line use the command - -
     python tut_mission_B737_800.py  
    - -3) A few plots depicting the variation of the different aircraft performance parameters over the course of the mission are shown. - -### Important Functions : - -The script is divided into a set of functions that setup different aspects of the modeling process. The important functions are: - -#### vehicle_setup() -function is where the aircraft's geometry is specified. - -##### Setting up a wing -The code below shows how the main wing of the aircraft is set up. The basic geometric inputs that define the wing are specified. Then the wing is then appended to the vehicle, which is an instance of the aircraft class. - -In SUAVE units are identified through the use of a units package called Pint. Notice, that for the wing sweep that the units are specified in degrees through *Units.deg. To get results into a desired unit use /Units.deg. - -The wing sweep is defined as the sweep of the quarter chord. Additionally, a symmetric wing means that it is symmetric about the root, i.e. there is right and left side. - - -
    
    -    wing = SUAVE.Components.Wings.Main_Wing()
    -    wing.tag = 'main_wing'
    -    
    -    wing.aspect_ratio            = 10.18
    -    wing.sweeps.quarter_chord    = 25 * Units.deg
    -    wing.thickness_to_chord      = 0.1
    -    wing.taper                   = 0.1
    -    wing.span_efficiency         = 0.9
    -    wing.spans.projected         = 34.32 * Units.meter
    -    wing.chords.root             = 7.760 * Units.meter
    -    wing.chords.tip              = 0.782 * Units.meter
    -    wing.chords.mean_aerodynamic = 4.235 * Units.meter
    -    wing.areas.reference         = 124.862 * Units['meters**2']  
    -    wing.twists.root             = 4.0 * Units.degrees
    -    wing.twists.tip              = 0.0 * Units.degrees
    -    wing.origin                  = [13.61,0,-1.27] # meters
    -    wing.vertical                = False
    -    wing.symmetric               = True
    -    wing.high_lift               = True
    -    wing.dynamic_pressure_ratio  = 1.0
    -
    -
    - -##### Setting up the fuselage -Similar to the wing above, the code below illustrates how a fuselage can be added to the vehicle. Again the user is required to specify the basic fuselage geometric parameters and then add the fuselage object to the vehicle. - -
      
    -    fuselage = SUAVE.Components.Fuselages.Fuselage()
    -    fuselage.tag = 'fuselage'
    -    
    -    fuselage.number_coach_seats    = vehicle.passengers
    -    fuselage.seats_abreast         = 6
    -    fuselage.seat_pitch            = 1     * Units.meter
    -    fuselage.fineness.nose         = 1.6
    -    fuselage.fineness.tail         = 2.
    -    fuselage.lengths.nose          = 6.4   * Units.meter
    -    fuselage.lengths.tail          = 8.0   * Units.meter
    -    fuselage.lengths.cabin         = 28.85 * Units.meter
    -    fuselage.lengths.total         = 38.02 * Units.meter
    -    fuselage.lengths.fore_space    = 6.    * Units.meter
    -    fuselage.lengths.aft_space     = 5.    * Units.meter
    -    fuselage.width                 = 3.74  * Units.meter
    -    fuselage.heights.maximum       = 3.74  * Units.meter
    -    fuselage.effective_diameter    = 3.74     * Units.meter
    -    fuselage.areas.side_projected  = 142.1948 * Units['meters**2'] 
    -    fuselage.areas.wetted          = 446.718  * Units['meters**2'] 
    -    fuselage.areas.front_projected = 12.57    * Units['meters**2'] 
    -    fuselage.differential_pressure = 5.0e4 * Units.pascal # Maximum differential pressure
    -    
    -    fuselage.heights.at_quarter_length          = 3.74 * Units.meter
    -    fuselage.heights.at_three_quarters_length   = 3.65 * Units.meter
    -    fuselage.heights.at_wing_root_quarter_chord = 3.74 * Units.meter
    -    
    -    # add to vehicle
    -    vehicle.append_component(fuselage)
    -
    - -##### Setting up the propulsion system - -The aircraft uses a turbofan engine. This engine can be constructed piece by piece using the energy network framework. We instantiate the network as shown below. - -
    
    -    # ------------------------------------------------------------------
    -    #   Turbofan Network
    -    # ------------------------------------------------------------------    
    -    
    -    #instantiate the gas turbine network
    -    turbofan = SUAVE.Components.Energy.Networks.Turbofan()
    -    turbofan.tag = 'turbofan'
    -    
    -    # setup
    -    turbofan.number_of_engines = 2
    -    turbofan.bypass_ratio      = 5.4
    -    turbofan.engine_length     = 2.71 * Units.meter
    -    turbofan.nacelle_diameter  = 2.05 * Units.meter
    -    turbofan.origin            = [[13.72, 4.86,-1.9],[13.72, -4.86,-1.9]] # meters
    -    
    -    #compute engine areas
    -    turbofan.areas.wetted      = 1.1*np.pi*turbofan.nacelle_diameter*turbofan.engine_length
    -    
    -    # working fluid
    -    turbofan.working_fluid = SUAVE.Attributes.Gases.Air()
    -
    -
    - -Next the components of the turbofan are initialized and added to the engine as shown in the energy networks section. The turbofan is composed of an inlet diffuser (nozzle), low and high pressure compressors, a combustor, a fan, a high and low pressure turbine, and exit nozzles for the core and the fan. - -Finally the network is added to the aircraft as shown below. - -
    
    -#size the turbofan
    -turbofan_sizing(turbofan,mach_number,altitude)   
    -    
    -# add  gas turbine network turbofan to the vehicle 
    -vehicle.append_component(turbofan)  
    -
    -# add  gas turbine network gt_engine to the vehicle
    -vehicle.append_component(turbofan)  
    -
    - -#### Data Structure Visualization -The data structure associated with the Boeing 737-800 can be visualized [here](/guides/data_structures/B737.html). - -[![Boeing 737 Data Structure](../images/b737_datastructure_preview.png)](/guides/data_structures/B737.html) - -This visualization shows the hierarchy of data in a SUAVE vehicle. Some of the values are defaulted, for example costs. This is because we are not performing cost analysis on the Boeing 737-800. Additionally, this snapshot of the data structure was taken prior to analysis. Therefore weights have not been calculated and are not part of the data. During the mission analysis component weights will be determined and weights will be populated. - -#### configs_setup() -The aircraft geometry created is converted into configurations that can be used to make simple modifications to the geometric parameters while not modifying the aircraft geometry completely. An example of the use of this feature is when high-lift devices need to be deployed during landing and takeoff. Thus a landing and takeoff configuration can be added as shown below and then during say the flaps and slats settings can be set differently for each of the configurations. - -
    
    -    # ------------------------------------------------------------------
    -    #   Cruise Configuration
    -    # ------------------------------------------------------------------
    -    config = SUAVE.Components.Configs.Config(base_config)
    -    config.tag = 'cruise'
    -    configs.append(config)
    -
    -    # ------------------------------------------------------------------
    -    #   Takeoff Configuration
    -    # ------------------------------------------------------------------
    -    config = SUAVE.Components.Configs.Config(base_config)
    -    config.tag = 'takeoff'
    -    config.wings['main_wing'].flaps.angle = 20. * Units.deg
    -    config.wings['main_wing'].slats.angle = 25. * Units.deg
    -    config.max_lift_coefficient_factor    = 1.
    -
    -    configs.append(config)
    -
    - -#### mission_setup() -To modify the baseline mission that the aircraft flies, go to the mission_setup() function and add or delete segments of the mission - -
    
    -    segment = Segments.Cruise.Constant_Speed_Constant_Altitude(base_segment)
    -    segment.tag = "cruise"
    -
    -    segment.analyses.extend( analyses.cruise )
    -
    -    segment.air_speed  = 230.412 * Units['m/s']
    -    segment.distance   = 2490. * Units.nautical_miles
    -
    -    # add to mission
    -    mission.append_segment(segment)
    -
    - - -#### base_analysis() -Also to leverage SUAVE's multifidelity capability and use a different fidelity analysis for any of the disciplines (aerodynamics,propulsion, stability, etc), the base_analysis function can be modified by switching out an analysis module for a different one. - - - - -### Other Functions : - -#### main() - -The main function is the driver function for the mission simulation. It calls the various routines in the appropriate order in order to set up the geometry and the mission, evaluate the performance of the aircraft over the mission and return the results. - -#### full_setup() - -This function (called from the main() function) sets up the aircraft geometry, configs and the missions the aircraft is to be analysed for by calling the vehicle_setup, configs_setup, analyses_setup, mission_setup and missions_setup functions. - - -#### simple_sizing() - -The simple sizing function sizes the aircraft's geometric components based on the geometric inputs specified by the user in the vehicle_setup() function. - -#### base_analysis() - -The method takes in the vehicle and assigns different analysis methods (for aero, propulsion, weights, stability) to the analyses object. - -#### analyses_setup() - -This functions takes in the base analysis and sets up different analysis methods for different configurations. - -#### missions_setup() - -This method allows the user to set up a variety of missions that need to be evaluated for an aircraft. - -#### plot_mission() - -This is a post processing function that takes in the results data structure and generates the necessary plots. - -### RESULTS - -The plots shown below should be generated if the mission analysis executes correctly. The results show the aerodynamic, propulsion and mission properties of the B737-800 for the defined mission. - -![B737 mission](/images/B737_mission.png) - -![B737 Aerodynamics](/images/B737_aero.png) - -![B737 Propulsion](/images/B737_engine.png) - -![B737 Drag](/images/B737_drag.png) - - -### Modifying the Aircraft's Geometry or Mission : - -Suppose we want to simulate a high span variant of the B737-800. The span is increased to 40.0 m. We assume the wing chords, sweep, taper ratio, thickness to chord ratio remain the same. Thus changing the span only changes the aspect ratio and the wing area. - -Now we try to fly the aircraft at a lower cruise speed of 200m/s at a cruise altitude of 25000 ft - -1) To update the geometry, scroll to the vehicle_setup() function - -2) Modify the parameters of the main wing - -
    
    -wing.aspect_ratio            = 10.12      
    -wing.spans.projected         = 40.0  * Units.meter
    -wing.areas.reference         = 158.0 * Units['meters**2'] 
    -
    - -You may also need to update the reference area for the aircraft. - -
    vehicle.reference_area         =     158.0
    -
    - -3) Update the mission parameters by moving to the mission_setup() function - -4) First update the end altitude of the final climb segment. Although the original script has the altitude stated in m, courtesy of the Units package it is easy to modify the altitude to 25,000ft without worrying about the units conversion as shown below. - - -
    segment = Segments.Climb.Constant_Speed_Constant_Rate(base_segment)
    -segment.tag = "climb_3"
    -
    -segment.analyses.extend( analyses.cruise )
    -
    -segment.altitude_end = 25000 * Units.ft  
    -segment.air_speed    = 226.0  * Units['m/s']
    -segment.climb_rate   = 3.0    * Units['m/s']
    -
    -mission.append_segment(segment)
    -
    - - - -5) Next update the cruise segment velocity to the new speed value - -
    segment = Segments.Cruise.Constant_Speed_Constant_Altitude(base_segment)
    -segment.tag = "cruise"
    -
    -segment.analyses.extend( analyses.cruise )
    -
    -segment.air_speed  = 200.0 * Units['m/s']
    -segment.distance   = 2490. * Units.nautical_miles
    -
    -# add to mission
    -mission.append_segment(segment)
    -
    - -6) Now go back and run the mission for the updated geometry and mission using the steps specified in 'Steps to run the aircraft on a mission' - - - - diff --git a/guides/_posts/2015-06-15-Turbofan_Network.md b/guides/_posts/2015-06-15-Turbofan_Network.md deleted file mode 100644 index ac5822d1..00000000 --- a/guides/_posts/2015-06-15-Turbofan_Network.md +++ /dev/null @@ -1,274 +0,0 @@ ---- -layout: post -title: Turbofan Network -date: 2015-06-15 14:20:03 -categories: blog -description: Get familiar with SUAVE’s energy and propulsion network - -permalink: /guides/turbofan_network.html ---- - - - - - -## Turbofan Modeling Tutorial - -This tutorial describes how the energy network framework in SUAVE can be used to build a model of a turbofan engine. Once this is clear to the user, understanding the setup of the other gasturbine models, the ducted fan and the turbojet will be much easier. The turbofan model is built with several turbofan components as its building blocks. These are then linked together through their inputs and outputs. The script to follow is the tut_mission_B737.py script that was used in the [Boeing 737-800 Analysis Tutorial](/guides/boeing_737-800.html) - - -### Setting up the Turbofan model - -First the turbofan energy network is instantiated. The parameters associated with the network as a whole are assigned. - -
    # ------------------------------------------------------------------
    -#   Turbofan Network
    -# ------------------------------------------------------------------    
    -
    -#instantiate the gas turbine network
    -turbofan = SUAVE.Components.Energy.Networks.Turbofan()
    -turbofan.tag = 'turbofan'
    -
    -# setup
    -turbofan.bypass_ratio      = 5.4
    -turbofan.number_of_engines = 2.0
    -turbofan.engine_length     = 2.5
    -turbofan.nacelle_diameter  = 1.580
    -
    -# working fluid
    -turbofan.working_fluid = SUAVE.Attributes.Gases.Air()
    -
    - -Then the different components are added - - -### Components - -The basic components used to model the turbofan are described below. - - -#### Ram - -The 'Ram' component is used to convert the freestream quantities that are passed into the turbofan network into stagnation quantities. As the turbofan network is based on a 1D gasdynamic analysis, most of the energy transfer across the different components are modelled as changes in the stagnation quantities. Thus the Ram component acts as a preprocessor converting the input conditions into quantities required by the network. - -
    # ------------------------------------------------------------------
    -#   Component 1 - Ram
    -
    -# to convert freestream static to stagnation quantities
    -
    -# instantiate
    -ram = SUAVE.Components.Energy.Converters.Ram()
    -ram.tag = 'ram'
    -
    -# add to the network
    -turbofan.append(ram)
    -
    - -#### Nozzle - -The 'Nozzle' component is used to model the inlet diffuser, the outlet fan, and the compressor nozzles as shown below. - - -
    # ------------------------------------------------------------------
    -#  Component 2 - Inlet Nozzle
    -
    -# instantiate
    -inlet_nozzle = SUAVE.Components.Energy.Converters.Compression_Nozzle()
    -inlet_nozzle.tag = 'inlet_nozzle'
    -
    -# setup
    -inlet_nozzle.polytropic_efficiency = 0.98
    -inlet_nozzle.pressure_ratio        = 0.98
    -
    -# add to network
    -turbofan.append(inlet_nozzle)
    -
    -# ------------------------------------------------------------------
    -#  Component 8 - Core Nozzle
    -
    -# instantiate
    -nozzle = SUAVE.Components.Energy.Converters.Expansion_Nozzle()   
    -nozzle.tag = 'core_nozzle'
    -
    -# setup
    -nozzle.polytropic_efficiency = 0.95
    -nozzle.pressure_ratio        = 0.99    
    -
    -# add to network
    -turbofan.append(nozzle)
    -
    -# ------------------------------------------------------------------
    -#  Component 9 - Fan Nozzle
    -
    -# instantiate
    -nozzle = SUAVE.Components.Energy.Converters.Expansion_Nozzle()   
    -nozzle.tag = 'fan_nozzle'
    -
    -# setup
    -nozzle.polytropic_efficiency = 0.95
    -nozzle.pressure_ratio        = 0.99    
    -
    -# add to network
    -turbofan.append(nozzle)
    -
    - -#### Compressor - -Two compressors are used in the turbofan model, a low and a high pressure compressor. - -
    # ------------------------------------------------------------------
    -#  Component 3 - Low Pressure Compressor
    -
    -# instantiate 
    -compressor = SUAVE.Components.Energy.Converters.Compressor()    
    -compressor.tag = 'low_pressure_compressor'
    -
    -# setup
    -compressor.polytropic_efficiency = 0.91
    -compressor.pressure_ratio        = 1.14    
    -
    -# add to network
    -turbofan.append(compressor)
    -
    -# ------------------------------------------------------------------
    -#  Component 4 - High Pressure Compressor
    -
    -# instantiate
    -compressor = SUAVE.Components.Energy.Converters.Compressor()    
    -compressor.tag = 'high_pressure_compressor'
    -
    -# setup
    -compressor.polytropic_efficiency = 0.91
    -compressor.pressure_ratio        = 13.415    
    -
    -# add to network
    -turbofan.append(compressor)
    -
    - -#### Fan - -A fan component is also added to the network. If you were to model a turbojet, the fan component and the fan nozzle would not be added but all the other components would remain the same. - -
    # ------------------------------------------------------------------
    -#  Component 10 - Fan
    -
    -# instantiate
    -fan = SUAVE.Components.Energy.Converters.Fan()   
    -fan.tag = 'fan'
    -
    -# setup
    -fan.polytropic_efficiency = 0.93
    -fan.pressure_ratio        = 1.7    
    -
    -# add to network
    -turbofan.append(fan)
    -
    - - -#### Combustor - -The combustor component is where the the fuel to air ratio is computed. It is also used to compute the sfc and the thrust later in the network. - -
    # ------------------------------------------------------------------
    -#  Component 7 - Combustor
    -
    -# instantiate    
    -combustor = SUAVE.Components.Energy.Converters.Combustor()   
    -combustor.tag = 'combustor'
    -
    -# setup
    -combustor.efficiency                = 0.99 
    -combustor.turbine_inlet_temperature = 1450
    -combustor.pressure_ratio            = 0.95
    -combustor.fuel_data                 = SUAVE.Attributes.Propellants.Jet_A()    
    -
    -# add to network
    -turbofan.append(combustor)
    -
    - -#### Turbine - -The work done by the fan and the compressors is used to compute the turbine work required. This is used to compute the change in the stagnation quantities across the turbine. - -
    # ------------------------------------------------------------------
    -#  Component 5 - Low Pressure Turbine
    -
    -# instantiate
    -turbine = SUAVE.Components.Energy.Converters.Turbine()   
    -turbine.tag='low_pressure_turbine'
    -
    -# setup
    -turbine.mechanical_efficiency = 0.99
    -turbine.polytropic_efficiency = 0.93     
    -
    -# add to network
    -turbofan.append(turbine)
    -
    -# ------------------------------------------------------------------
    -#  Component 6 - High Pressure Turbine
    -
    -# instantiate
    -turbine = SUAVE.Components.Energy.Converters.Turbine()   
    -turbine.tag='high_pressure_turbine'
    -
    -# setup
    -turbine.mechanical_efficiency = 0.99
    -turbine.polytropic_efficiency = 0.93     
    -
    -# add to network
    -turbofan.append(turbine)
    -
    - - - -#### Thrust - -The thrust component takes in the initial (inputs of the inlet nozzle) and final (exit of the fan and core exirt nozzles) stagnation quantities of the network and the fuel to air ratio and computes the specific fuel conspumption (sfc) and thrust generated by the network (turbofan engine). - -
    # ------------------------------------------------------------------
    -#  Component 10 - Thrust
    -
    -# to compute thrust
    -
    -# instantiate
    -thrust = SUAVE.Components.Energy.Processes.Thrust()       
    -thrust.tag ='thrust'
    -
    -# setup
    -thrust.total_design =42383.01
    -
    -# add to network
    -turbofan.thrust = thrust   
    -
    - - - -### Sizing the Turbofan - -Once the network is built, it is essential to size the engine with a set of sizing conditions. The sizing function 'turbofan_sizing' takes in the model of the turbofan and the mach number and the altitude for which the turbofan is sized. The sizing thrust is an engine/network property (defined in the 'Setting up the Turbofan model' section above). The function takes these quantities and computes the design mass flow rate through the components. Once sized, the network/engine can be added to the vehicle as shown in the B737 tutorial. - -
    #bypass ratio  closer to fan
    -
    -#design sizing conditions
    -altitude      = 35000.0*Units.ft
    -mach_number   = 0.78 
    -isa_deviation = 0.
    -
    -# add to network
    -turbofan.thrust = thrust
    -
    -#size the turbofan (for thrust)
    -turbofan_sizing(turbofan,mach_number,altitude)   
    -
    -#compute the turbofan diameter and engine length
    -#note that the second input is to maintain a common interface with other sizing methods
    -compute_turbofan_geometry(turbofan,None)
    -
    - - - - - - - - diff --git a/guides/_posts/2015-06-17-Payload_Range_Diagram.md b/guides/_posts/2015-06-17-Payload_Range_Diagram.md deleted file mode 100644 index 9fa34b3b..00000000 --- a/guides/_posts/2015-06-17-Payload_Range_Diagram.md +++ /dev/null @@ -1,44 +0,0 @@ ---- -layout: post -title: Payload Range Diagram -date: 2015-06-17 23:22:21 -categories: blog -description: Learn how to use SUAVE for creating a payload-range diagram - -permalink: /guides/payload_range_diagram.html ---- - -### Embraer E-190 Payload Range Diagram Tutorial -1) Locate the tutorial script folder. - -2) Open the test_payload_range.py script in your favorite editor or IDE. - -3) Similar to the B737-800 Tutorial, the setup is divided into steps. - -4) For the Payload Range Diagram, besides the vehicle and mission, the user must provide the following inputs: - -* **cruise_segment_tag**: You must enter the tag of the segment which will have its length modified in order to comply with required fuel burn for each one of the payload range diagram points. -* **reserves**: This will be considered as a fixed fuel reserve for all the diagram points. - -5) The tutorial presents the following definition: - -~~~ -# run payload diagram -cruise_segment_tag = "Cruise" -reserves = 1750. -payload_range_results = payload_range(vehicle,mission,cruise_segment_tag,reserves) -~~~ - -6) First, let's just run it as it is for now. Run the script in either the IDE or in a terminal as `python tut_payload_range.py` - -7) After the calculations are completed, the payload diagram will be plotted and the data will be stored in a file named 'PayloadRangeDiagram.dat'. This is in the folder where you run the script. - -8) You can try to modify vehicle and/or mission parameters and see how the payload range diagram is affected. For now, let's add some drag counts to the airplane: - -* Locate and open the script test_mission_Embraer_E190_constThr.py, in the tutorial folder (this is the script that contains the vehicle and mission setups) -* Locate ``` base_analysis() ``` and then the Aerodynamics Analysis text block (line 113) -* Add 50 drag counts to the vehicle (line 115): `aerodynamics.settings.drag_coefficient_increment = 0.0050 ` -* Rerun the script as before and notice the changes in the results. - -9) Similarly the mission parameters can be changed. Again, this lets the user decide what changes they want to explore. - diff --git a/guides/_posts/2015-06-18-Solar_UAV.md b/guides/_posts/2015-06-18-Solar_UAV.md deleted file mode 100644 index a10ac5db..00000000 --- a/guides/_posts/2015-06-18-Solar_UAV.md +++ /dev/null @@ -1,149 +0,0 @@ ---- -layout: post -title: Solar UAV -date: 2015-06-18 23:22:20 -categories: blog -description: Analyze an unconventional aircraft and energy network - -permalink: /guides/solar_uav.html ---- - - - - - -## Introduction - -The purpose of this tutorial is to educate users on how to setup a preconfigured solar energy network to work with a high altitude solar UAV. In this tutorial it is assumed that the user has some familiarity with SUAVE having completed the fundamental tutorial for the Boeing 737-800. You will learn about setting up the following: - -* Solar missions, -* Human powered/solar weight estimation, -* Boundary layer transition -* Solar panels, -* Batteries, -* Electric motors, -* Propellers, -* Electric network integration in a solar UAV - -Because of the flexible nature of SUAVE, the approach shown is just one way to setup the UAV for analysis. By experimenting and eventually developing your own code you will be able to do far more than what is shown in this tutorial. The original script can be found in the tutorial repository as tut_solar_uav.py. - -## Vehicle and Mission - -The vehicle is similar to the Qinetiq Zephyr but far larger at 40 meters in wing span and a weight of 200 kg. However, it does carry double the payload of the Zephyr at 5 kg and accounts for constant payload power usage. The battery energy density is set to an optimistic estimate of 450 Watt-hours per kg. Additionally, 90 percent of the wings are covered with solar panels that have a 25 percent efficiency. - -This mission exercises the methods developed for solar radiation estimation, propeller and motor integration, as well as the human powered aircraft weight estimation. The mission setup is a constant altitude cruise at 15 km at Mach 0.12 for about 24 hours. The location is over the California Bay Area during the summer solstice. - -## Setup - -This tutorial highlights the differences between setting up a typical aircraft like a Boeing 737 and a solar UAV. - -### Mission Setup - -For a solar UAV, the starting location as well as the day and time are critical. So the first segment must be modified to include this information. It is important to note that the start times provided are in "Zulu" time or Greenwich Mean Time. This is typical for aircraft navigation to prevent time zone errors and ambiguity. - -
    segment.state.numerics.number_control_points = 64
    -segment.start_time                           = time.strptime("Tue, Jun 21 11:30:00  2015", "%a, %b %d %H:%M:%S %Y",)
    -segment.altitude                             = 15.0  * Units.km 
    -segment.mach                                 = 0.12
    -segment.distance                             = 3050.0 * Units.km
    -segment.battery_energy                       = vehicle.propulsors.network.battery.max_energy*0.2 #Set the battery charge to start
    -segment.latitude                             = 37.4300
    -segment.longitude                            = -122.1700
    -
    - -Additionally, this mission is highly simplified. It consists of only one mission segment. To provide ample resolution the number of control points have been increased to 64. - -### Structural Weight Sizing - -The vehicle sizing of the human powered aircraft or solar UAV requires the dimensions of the vehicle like in other weight estimation methods. However, it also requires information about the number of wing ribs and the number of end ribs. The end ribs are relevant for wing designs where the sections can come apart for transportation. - -
    wing.number_ribs             = 26.
    -wing.number_end_ribs         = 2.
    -
    - -### Wing Boundary Layer Transition - -The transition location of the boundary layer can have a great impact on the drag of the wing. This is especially important in properly designed low Reynolds number flows when laminar flow can be extended for larger percentages of the surface. The code snippet below is how surfaces have transition points set. These are estimates provided from the designer based on experience. - -
    wing.transition_x_upper      = 0.6
    -wing.transition_x_lower      = 1.0
    -
    - -### Solar Panels - -The solar panel model is quite simple and only requires a capture area, an efficiency, and mass. In this case we assume that 90% of the wing area is covered in solar panels. - -
    panel.area                 = vehicle.reference_area * 0.9
    -panel.efficiency           = 0.25
    -panel.mass_properties.mass = panel.area*(0.60 * Units.kg)
    -
    - - -### Batteries - -The batteries are set up with knowledge of the mass of the battery and the specific energy. In this case a futuristic specific energy of 450 Watt-hr/kg is set for lithium ion type batteries. The resistance of the batteries is another important input to determine charging and discharging losses. - -
    bat = SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion()
    -bat.mass_properties.mass = 55.0 * Units.kg
    -bat.specific_energy      = 450.*Units.Wh/Units.kg
    -bat.resistance           = 0.05
    -initialize_from_mass(bat,bat.mass_properties.mass)
    -net.battery              = bat
    -
    - - -### Propeller - -To setup the propeller we will actually design an optimized propeller. This is done through the methods provided by Adkins and Liebeck. The attributes of the propeller design are then seeded to the motor and network to accelerate convergence of the propeller and motor models. - -
    prop_attributes = Data()
    -prop_attributes.number_blades       = 2.0
    -prop_attributes.freestream_velocity = 40.0 # freestream m/s
    -prop_attributes.angular_velocity    = 150. * Units['rpm']
    -prop_attributes.tip_radius          = 4.25
    -prop_attributes.hub_radius          = 0.05
    -prop_attributes.design_Cl           = 0.7
    -prop_attributes.design_altitude     = 14.0 * Units.km
    -prop_attributes.design_thrust       = 0.0
    -prop_attributes.design_power        = 3500.0
    -prop_attributes                     = propeller_design(prop_attributes)
    -
    -prop = SUAVE.Components.Energy.Converters.Propeller()
    -prop.prop_attributes = prop_attributes
    -net.propeller        = prop
    -
    - -### Motor - -This motor model relies on data that is generally available from motor manufacturers. This includes the resistance, no load current, and the speed constant. Additionally, any gearbox is specified here and basic information about the propeller is entered here to help inform the solver when converging the motor and propeller analyses. - -
    motor = SUAVE.Components.Energy.Converters.Motor()
    -motor.resistance           = 0.008
    -motor.no_load_current      = 4.5
    -motor.speed_constant       = 120. * Units['rpm'] # RPM/volt converted to (rad/s)/volt      
    -motor.propeller_radius     = prop.prop_attributes.tip_radius
    -motor.propeller_Cp         = prop.prop_attributes.Cp
    -motor.gear_ratio           = 12. # Gear ratio
    -motor.gearbox_efficiency   = .98 # Gear box efficiency
    -motor.expected_current     = 160. # Expected current
    -motor.mass_properties.mass = 2.0
    -net.motor                  = motor   
    -
    - - -## Running - -As you should be familiar with by now, running this script is just like any other. -
    python tut_solar_uav.py
    -
    - -## Results - -If all went well the script ran and it provided you with more plots than you ever wanted. Here are some of the plots that were generated when we ran it: - -![solar_flux](/images/solar_flux.png) - -![battery charging](/images/battery_charging.png) - -![battery energy](/images/battery_energy.png) - diff --git a/guides/_posts/2015-07-15-Concorde.md b/guides/_posts/2015-07-15-Concorde.md deleted file mode 100644 index cd1d2cd2..00000000 --- a/guides/_posts/2015-07-15-Concorde.md +++ /dev/null @@ -1,83 +0,0 @@ ---- -layout: post -title: Concorde -date: 2015-07-15 14:25:00 -categories: blog -description: Go Supersonic ! - -permalink: /guides/concorde.html ---- - - - - - -## Concorde Tutorial - - -This tutorial gives an overview of changes made to the setup to evaluate a supersonic mission. - -### Aerodynamics Module: - -To allow aerodynamic calculations in supersonic flight, we use the zero fidelity supersonic module. This is quite easy to swap with the subsonic zero fidelity model. This model and the zero fidelity subsonic module are in the same directory, so they can be switched by changing a single line in the analysis section: - -``` -aerodynamics = SUAVE.Analyses.Aerodynamics.Fidelity_Zero() -``` - -to - -``` -aerodynamics = SUAVE.Analyses.Aerodynamics.Supersonic_Zero() -``` -The supersonic aerodynamics module can still handle the subsonic portions of the flight. - -### Wing Additions: - -Some of the calculations are changed to account for different properties that are not automatically captured in the model. - -* Vortex lift is set to true. This causes the vortex lift module to add a CL increment to the aircraft. -* High Mach is set to true. This changes the way that high subsonic compressibility drag is calculated and brings it more in line with Concorde behavior. - -``` - wing.vortex_lift = True -``` - -``` - wing.high_mach = True -``` - -Note also that Concorde does not have a horizontal tail, so this is not included in the vehicle setup. - -### Turbojet Module: - -Since Concorde has a diverging nozzle that allows for supersonic outflow, a modified turbojet is used that can account for this. This turbojet component is again switched out with a single line. - -``` -nozzle = SUAVE.Components.Energy.Converters.Supersonic_Nozzle() -``` - -instead of - -``` -nozzle = SUAVE.Components.Energy.Converters.Expansion_Nozzle() -``` - -### Mission Segments: - -The mission typically flown by Concorde calls for mission segments that are not utilized in the Boeing 737 case. These are Mach number dependent, and require different inputs from the segments previously given. The new mission segments are linear Mach constant rate (climb and descent). Both require a starting and ending Mach number, which will vary linearly in time over the descent. For an example, check the third climb segment: - - - segment = Segments.Climb.Linear_Mach_Constant_Rate(base_segment) - segment.tag = "climb_3" - - segment.analyses.extend( analyses.cruise ) - - segment.altitude_end = 7.60 * Units.km - segment.mach_start = 0.64 - segment.mach_end = 1.0 - segment.climb_rate = 5.05 * Units['m/s'] - -### Takeoff and Landing Configuration - -Since Concorde does not have flaps or slats, specific takeoff and landing configurations are not used. diff --git a/guides/_posts/2016-02-11-Regional_Jet_Optimization.md b/guides/_posts/2016-02-11-Regional_Jet_Optimization.md deleted file mode 100644 index 51eb4662..00000000 --- a/guides/_posts/2016-02-11-Regional_Jet_Optimization.md +++ /dev/null @@ -1,155 +0,0 @@ ---- -layout: post -title: Regional Jet Optimization -date: 2015-06-14 23:22:25 -categories: blog -description: Learn the optimization framework within SUAVE - -permalink: /guides/regional_jet_optimization.html ---- - - - - - -### Regional Jet Optimization Tutorial -This tutorial assumes familiarity with SUAVE and knowledge of the information in the Boeing 737-800 analysis tutorial. It provides a specific case of the more general information provided in the optimization structure tutorial, and some more information on how to modify the code for different uses. - -Some important files for the optimization problem can be seen below - - -### Important Files : - -#### Optimize.py: -Defines the optimization framework of the problem, wherein one minimizes an assigned objective, subject to certain constraints, by altering some design variables. - - In order to ensure that the subfunctions can communicate with eachother, and that SUAVE can communicate with the external optimizer, a special data object called the "Nexus" is used. The nexus object contains all of the vehicles, missions, results, and other important information. It alters these values at each optimizer iteration, depending on the input parameters defined in Optimize.py. - -In this particular setup, there are two design variables: wing area and cruise altitude. The objective is fuel burn, and there is only one constraint: fuel margin. The default inputs are defined in the following lines. - - - # [ tag, initial, (lb,ub), scaling, units] - problem.inputs = np.array([ - [ 'wing_area' , 95., ( 90., 130.), 100., Units.meter**2], - [ 'cruise_altitude', 11., ( 9., 14.), 10., Units.km ], - ]) - -Each input parameter takes in 5 values; a tag (an identification to communicate between the optimizer and SUAVE), an initial value, set of bounds, a scale factor (many optimizers tend to be more effective when the input values are of order 1), as well as the units used. - -The objective and constraints are defined in the lines below. - - # [ tag, scaling, units ] - problem.objective = np.array([ - [ 'fuel_burn', 10000, Units.kg ] - ]) - - # [ tag, sense, edge, scaling, units ] - problem.constraints = np.array([ - [ 'design_range_fuel_margin' , '>', 0., 1E-1, Units.less], - ]) - -Note that in this case, only a single constraint is used; Multiple constraints may be used using a list format, similar to the input variables. - - - -This file also defines the "aliasing," i.e. how the design variables, constraints, and objective map to the variables used in Procedure.py (which is where the problem is evaluated). The aliases for this problem are defined in the lines below. Note that the first entry refers to the tag defined in either problem.inputs, problem.objective, or problem.constraints. - - problem.aliases = [ - [ 'wing_area' , ['vehicle_configurations.*.wings.main_wing.areas.reference', - 'vehicle_configurations.*.reference_area' ]], - [ 'cruise_altitude' , 'missions.base.segments.climb_5.altitude_end' ], - [ 'fuel_burn' , 'summary.base_mission_fuelburn' ], - [ 'design_range_fuel_margin' , 'summary.max_zero_fuel_margin' ], - ] - -Note that, sometimes, a single input can map to multiple outputs, such as the "wing_area" design variable; in this case, use a list for the outputs, as seen above. The use of a wild card "*", can also allow values to map to multiple outputs. Values to be outputted cannot contain wild cards as that would be ambiguous to an optimizer. - -#### Procedure.py: -This links everything together by defining the steps you would use to size and analyze the aircraft at each optimizer iteration. - -This file contains a number of subfunctions to alter the vehicle and mission. The function setup() instantiates the procedure, defining the functions that are called at each step of the optimizer in their order of execution. - -1. simple_sizing() defines the geometry of the aircraft based on the input parameters (in this case, wing area and cruise altitude). - -2. weights() determines the weight breakdown of the aircraft - -3. mission() decides which missions are run at each step, as well as the design mission of the aircraft - -4. post_process() handles the results from the missions, saving the constraints and objective value - -Each step of the procedure takes the nexus object as an input, and returns the object as an output, ensuring that the data is available for handling. - -#### Vehicles.py: - Initializes the vehicle (or vehicles if desired) used in the optimization problem. This includes two subfunctions: base_setup(), where the vehicle structure is itself defined, including the fuselage, wing, vertical and horizontal tails, and the propulsion system. - -configs_setup() takes in the vehicle that was defined in base_setup() and defines other configurations (such as takeoff and landing, which include different flap settings). This may be used to define other parameters, such as changing the sweep angle of a variable-sweep-wing at higher Mach Numbers, or changing a propulsion component. - -#### Missions.py: - Initializes the missions that are run at each iteration. In this case, only a single mission is run. - -#### Analyses.py: - Defines the set of features that are used in this particular problem (e.g. weights correlations, aerodynamics correlations, etc.). - -#### Plot_Mission.py: -Plots the mission outputs. - -### Running the Problem: -1. Locate the tutorial script folder "Regional_Jet_Optimization." - -2. Open the Optimize.py script in a text editor or IDE. You will see this line near the top of main(): - - `output = problem.objective()` - -3. This runs the problem with the default inputs. Run the file using an IDE or type `python Optimize.py` in the command line. You should see a set of output plots. - - -### Running a Sweep of the Inputs -Now try running a 2D sweep of the problem to observe the shape of the design space: comment `output = problem.objective` then uncomment the following (the next line down in the code). - - variable_sweep(problem) - -Then run the program again. This could take a few minutes. The results should look like the plot below. - -![2D Sweep](/images/wing_area_v_cruise_altitude_v_fuel_burn_5_steps.png) - -The labeled lines depict the fuel margin (i.e. fraction of the aircraft remaining weight that can be loaded with fuel). Positive values indicate a feasible design. Fuel burn is shown in the colored contours. Note that a smoother plot may be created by changing the number of points in the sweep function, but this will take more time. A carpet plot run using 400 points on can be seen below. A local minimum is now visible. - -![2D Sweep_20](/images/wing_area_v_cruise_altitude_v_fuel_burn.png) - -Note: If you run this 400 point case yourself you may see messages indicating that a segment did not converge. This is normal and can happen when a mission is run far from a feasible point. In this case, it does not have a negative impact on the results. - -### Optimizing: - - Now try running an Optimization. Recomment `variable_sweep(problem)` then uncomment the lines below: - - output = scipy_setup.SciPy_Solve(problem,solver='SLSQP') - print output - -and run the file again. - -From the default inputs, the terminal (or IDE output) should display an optimum of [ 1.08980937 1.02089232], which corresponds to a wing area of 109 m^2, and 10.2 km. It appears to have found the local minimum. - -Now try starting the optimization from a different initial guess. You can either modify the input parameters in the initial formulation (the relevant lines are repeated below with the modification) - - # [ tag , initial, (lb,ub) , scaling , units ] - problem.inputs = np.array([ - [ 'wing_area' , 128 , ( 90. , 130. ) , 100. , Units.meter**2], - [ 'cruise_altitude' , 13.8 , ( 9 , 14. ) , 10. , Units.km], - ]) - - -or set up the optimization problem and change the inputs manually by uncommenting the following lines. - - - inputs = [1.28, 1.38] - scaling = problem.optimization_problem.inputs[:,3] # have to - rescale inputs to start problem from here - scaled_inputs = np.multiply(inputs,scaling) - problem.optimization_problem.inputs[:,1] = scaled_inputs - output = scipy_setup.SciPy_Solve(problem,solver='SLSQP') - print output - - - This starts the optimization problem above the feasible region (wing area = 128 m^2, altitude = 13.8 km), and results in a fuel burn that is 30 kg lower than the result using the initial guess. This illustrates the important of choosing a starting point when running optimization problem. Additionally, this demonstrates SUAVE's ability to handle infeasible cases, showing that it can converge to a feasible case even when starting from an infeasible set of initial inputs. - -At this point, you can explore other starting points, or alter the vehicle or mission properties in Vehicles.py or Missions.py. Additionally, feel free to start using this as the basis for creating custom optimization scripts. \ No newline at end of file diff --git a/guides/_posts/2016-05-11-solar_uav_optimization_tutorial.md b/guides/_posts/2016-05-11-solar_uav_optimization_tutorial.md deleted file mode 100644 index 6d8829a9..00000000 --- a/guides/_posts/2016-05-11-solar_uav_optimization_tutorial.md +++ /dev/null @@ -1,255 +0,0 @@ ---- -layout: post -title: Solar UAV Optimization -date: 2015-06-14 23:22:21 -categories: blog -description: Use SUAVE’s optimization for unconventional configurations - -permalink: /guides/solar_uav_optimization.html ---- - -## Solar UAV Optimization Tutorial - -The purpose of this tutorial is to illustrate a different type of problem. We assume you have gone through the first optimization tutorial: Regional Jet Optimization. This tutorial will illustrate a little more complex setup that modifies a mission parameter. - -Your objective is simple: get a small UAV to fly from San Francisco to San Diego. In fact you can pose that as an optimization problem, with some constraints that govern how it works. There is no requirement to minimize this or maximize that. Of course you could try to minimize something, but you just want something that works for now. Later iterations can do fancier things. - -Next we will go into detail about some of the required files. *Analyses.py* and *Plot_mission.py* are straightforward from prior tutorials. So we will not go into those in detail, except to say that we are using a UAV weight model in *Analyses.py*. - -### Optimize.py: - -Let’s pose the optimization problem first and then setup the rest. We start with the *Nexus* first as usual. With this design problem there are things you are uncertain of and want to solve for. - -You're not sure if you really need any solar panels on the airplane, so to start there will be none. The solar ratio is the ratio of wing area to solar area. A value of 1 would the whole top of the wing covered with solar panels. - -
    
    -	  # [ tag , initial, [lb,ub], scaling, units ]
    -    problem.inputs = np.array([
    -        [ 'wing_area'       ,   0.5, (  0.1,    1.5 ),    0.5, Units.meter      ],
    -        [ 'aspect_ratio'    ,  10.0, (  5.0,   20.0 ),   10.0, Units.less       ], 
    -        [ 'dynamic_pressure', 125.0, (  1.0, 2000.0 ),  125.0, Units.pascals    ], 
    -        [ 'solar_ratio'     ,   0.0, (  0.0,    0.97),    1.0, Units.less       ], 
    -        [ 'kv'              , 800.0, ( 10.0, 1500.0 ),  800.0, Units['rpm/volt']], 
    -    ])
    -
    - -Next come the constraints. The first constraint is that the battery energy can never go negative, the math behind this will be elaborated on later. The next constraint is that the plane must have a battery. Finally there are limits to coefficients of lift and throttle settings. - -
    
    -      # [ tag, sense, edge, scaling, units ]
    -    problem.constraints = np.array([
    -        [ 'energy_constraint', '=', 0.0, 1.0, Units.less],
    -        [ 'battery_mass'     , '>', 0.0, 1.0, Units.kg  ],       
    -        [ 'CL'               , '>', 0.0, 1.0, Units.less],
    -        [ 'Throttle_min'     , '>', 0.0, 1.0, Units.less],
    -        [ 'Throttle_max'     , '>', 0.0, 1.0, Units.less],
    -    ])
    -
    - -Notice here that all constraints are greater than zero. This is because SciPy’s SLSQP optimization algorithm assumes this form. To correct for these, the values are adjusted in Procedure.py. Other optimization packages such as PyOpt don’t require this strict form. - -Finally, the objective. It’s nothing of course! As long as the constraints are met, the goal of the design is satisfied. - -
    
    -    # [ tag, scaling, units ]
    -    problem.objective = np.array([
    -         [ 'Nothing', 1. , Units.kg],
    -    ])
    -
    - -### Vehicles.py: - -Next, you will setup the vehicle. This is very similar to the prior Solar UAV tutorial. So we will gloss over this, the one noticeable difference is that a lower fidelity energy network is used. This means that most components operate with prescribed efficiencies. For example: - -
    
    -    # Component 4 the Motor
    -    motor = SUAVE.Components.Energy.Converters.Motor_Lo_Fid()
    -    kv                         = 800. * Units['rpm/volt'] # RPM/volt is standard
    -    motor                      = size_from_kv(motor, kv)    
    -    motor.gear_ratio           = 1. # Gear ratio, no gearbox
    -    motor.gearbox_efficiency   = 1. # Gear box efficiency, no gearbox
    -    motor.motor_efficiency     = 0.825;
    -    net.motor                  = motor  
    -    ])
    -
    - -### Missions.py: - -Now for the mission setup. Here we assume it will take 1000 km and the plane will cruise off the coast at 1000 feet in altitude. The distance is a bit longer than the straight line distance, but we're not going to fly through populated areas. The heading, or body rotation, must be set to account for the changes in latitude and longitude to accurately calculate the solar radiation. We will cruise at a constant altitude and assume it takes no time to climb and descend compared to the cruise time. - -
    
    -    segment.state.numerics.number_control_points = 50
    -    segment.dynamic_pressure = 115.0 * Units.pascals
    -    segment.start_time       = time.strptime("Tue, Jun 21  11:00:00  2016", "%a, %b %d %H:%M:%S %Y",)
    -    segment.altitude         = 1000.0 * Units.feet
    -    segment.distance         = 1000.0 * Units.km
    -    segment.charge_ratio     = 1.0
    -    segment.latitude         = 37.4
    -    segment.longitude        = -122.15
    -    segment.state.conditions.frames.wind.body_rotations[:,2] = 125.* Units.degrees 
    -
    - -### Procedure.py: - -Finally we have the procedure setup. In the procedure, we resize the vehicle, calculate weights, finalize the analyses, solve the mission, and post process. - -Some notes about sizing. Each wing component (main wing, horizontal tail, and vertical tail) needs the surfaces sized based on its area and aspect ratio. Next the solar panels are sized based on the wing area and solar_ratio. Finally the motor is resized based on correlations for the speed constant of the motor. - -
    
    -def simple_sizing(nexus):
    -    
    -    # Pull out the vehicle
    -    vec = nexus.vehicle_configurations.base
    -    
    -    # Change the dynamic pressure based on the, add a factor of safety   
    -    vec.envelope.maximum_dynamic_pressure = nexus.missions.mission.segments.cruise.dynamic_pressure*1.2
    -    
    -    # Scale the horizontal and vertical tails based on the main wing area
    -    vec.wings.horizontal_stabilizer.areas.reference = 0.15 * vec.reference_area
    -    vec.wings.vertical_stabilizer.areas.reference   = 0.08 * vec.reference_area
    -
    -    # wing spans,areas, and chords
    -    for wing in vec.wings:
    -        
    -        # Unpack
    -        AR = wing.aspect_ratio
    -        S  = wing.areas.reference
    -        
    -        # Set the spans
    -        wing.spans.projected = np.sqrt(AR*S)
    -        
    -        # Set all of the areas for the surfaces
    -        wing.areas.wetted   = 2.0 * S
    -        wing.areas.exposed  = 1.0 * wing.areas.wetted
    -        wing.areas.affected = 1.0 * wing.areas.wetted   
    -        
    -        # Set all of the chord lengths
    -        chord = wing.areas.reference/wing.spans.projected
    -        wing.chords.mean_aerodynamic = chord
    -        wing.chords.mean_geometric   = chord
    -        wing.chords.root             = chord
    -        wing.chords.tip              = chord
    -
    -    # Size solar panel area
    -    wing_area                   = vec.reference_area
    -    spanel                      = vec.propulsors.network.solar_panel
    -    sratio                      = spanel.ratio
    -    solar_area                  = wing_area*sratio
    -    spanel.area                 = solar_area
    -    spanel.mass_properties.mass = solar_area*(0.60 * Units.kg)    
    -    
    -    # Resize the motor
    -    motor = vec.propulsors.network.motor
    -    kv    = motor.speed_constant
    -    motor = size_from_kv(motor, kv)    
    -    
    -    # diff the new data
    -    vec.store_diff()
    -
    -    return nexus
    -
    - -Here the battery is sized and charged. The battery weight consists of everything that is left over from sizing. - -
    
    -def weights_battery(nexus):
    -
    -    # Evaluate weights for all of the configurations
    -    config = nexus.analyses.base
    -    config.weights.evaluate() 
    -    
    -    vec     = nexus.vehicle_configurations.base
    -    payload = vec.propulsors.network.payload.mass_properties.mass  
    -    msolar  = vec.propulsors.network.solar_panel.mass_properties.mass
    -    MTOW    = vec.mass_properties.max_takeoff
    -    empty   = vec.weight_breakdown.empty
    -    mmotor  = vec.propulsors.network.motor.mass_properties.mass
    -    
    -    # Calculate battery mass
    -    batmass = MTOW - empty - payload - msolar -mmotor
    -    bat     = vec.propulsors.network.battery
    -    initialize_from_mass(bat,batmass)
    -    vec.propulsors.network.battery.mass_properties.mass = batmass
    -        
    -    # Set Battery Charge
    -    maxcharge = nexus.vehicle_configurations.base.propulsors.network.battery.max_energy
    -    charge    = maxcharge
    -    
    -    nexus.missions.mission.segments.cruise.battery_energy = charge 
    -
    -    return nexus
    -
    - -The next we run the mission and post process the results. The post_process function will setup the information of importance for the user. The energy constraint is a way of ensuring that nowhere in the mission the battery energy goes negative. The coefficient of lift is limited to 1.2. The throttle is limited to 0.9, to make sure there is excess throttle to climb. Throttle is also limited from going negative. Finally, the objective, nothing is specified to be zero. - -
    
    -def post_process(nexus):
    -    
    -    # Unpack
    -    mis = nexus.missions.mission.segments.cruise
    -    vec = nexus.vehicle_configurations.base
    -    res = nexus.results.mission.segments.cruise.conditions
    -    
    -    # Final Energy
    -    maxcharge    = vec.propulsors.network.battery.max_energy
    -    
    -    # Energy constraints, the battery doesn't go to zero anywhere, using a P norm
    -    p                    = 8.    
    -    energies             = res.propulsion.battery_energy[:,0]/np.abs(maxcharge)
    -    energies[energies>0] = 0.0 # Exclude the values greater than zero
    -    energy_constraint    = np.sum((np.abs(energies)**p))**(1/p) 
    -
    -    # CL max constraint, it is the same throughout the mission
    -    CL = res.aerodynamics.lift_coefficient[0]
    -    
    -    # Pack up
    -    summary = nexus.summary
    -    summary.CL                = 1.2 - CL
    -    summary.energy_constraint = energy_constraint
    -    summary.throttle_min      = res.propulsion.throttle[0]
    -    summary.throttle_max      = 0.9 - res.propulsion.throttle[0]
    -    summary.nothing           = 0.0
    -    
    -    return nexus    
    -
    - -### Results -Let’s look at the results: - -
    
    -Optimization terminated successfully.    (Exit mode 0)
    -            Current function value: [0.0]
    -            Iterations: 4
    -            Function evaluations: 29
    -            Gradient evaluations: 4
    -[ 1.12963146  1.43880081  1.39329626  0.65589785  0.97171879]
    -Design Variable Table:
    -
    -[['wing_area' 0.5648157324099996 (0.1, 1.5) 0.5 1.0]
    - ['aspect_ratio' 14.388008119672202 (5.0, 20.0) 10.0 1.0]
    - ['dynamic_pressure' 174.16203234031317 (1.0, 2000.0) 125.0 1.0]
    - ['solar_ratio' 0.6558978486767236 (0.0, 0.97) 1.0 1.0]
    - ['kv' 777.3750338508712 (10.0, 1500.0) 800.0 0.10471975511965977]]
    -
    -Constraint Table:
    -
    -[['energy_constraint' 0.0 '=' 0.0 1.0 ]
    - ['battery_mass' 4.939962596982861 '>' 0.0 1.0 ]
    - ['CL' 0.5309682332699428 '>' 0.0 1.0 ]
    - ['Throttle_min' 0.7319219623084848 '>' 0.0 1.0 ]
    - ['Throttle_max' 0.1680780376915152 '>' 0.0 1.0 ]]
    -
    - -Okay looks like SciPy found a feasible solution without too much time. Now let’s review the plots. - -![battery_energy](/images/opt_battery_energy.png) - -So we can tell now that the battery energy doesn't go all the way to zero. Let's look at how the solar flux varies throughout the day and how that affects the draw from the battery. - -![solar flux](/images/opt_solar_flux.png) - -![battery draw](/images/opt_battery_draw.png) - -So maybe those solar panels actually are worth it. They seem to decrease the load on the battery considerably during the daytime. - - diff --git a/guides/data_structures/.DS_Store b/guides/data_structures/.DS_Store new file mode 100644 index 00000000..5008ddfc Binary files /dev/null and b/guides/data_structures/.DS_Store differ diff --git a/guides/data_structures/B737.html b/guides/data_structures/B737.html index 32d03a46..09ba195c 100644 --- a/guides/data_structures/B737.html +++ b/guides/data_structures/B737.html @@ -49,8 +49,8 @@ } - - + +
    diff --git a/guides/data_structures/B737.js b/guides/data_structures/B737.js index 7400b601..cc0189b5 100644 --- a/guides/data_structures/B737.js +++ b/guides/data_structures/B737.js @@ -334,7 +334,7 @@ treeJSON = d3.json("B737.json", function(error, treeData) { } }); - // Update the nodes + // Update the nodes� node = svgGroup.selectAll("g.node") .data(nodes, function(d) { return d.id || (d.id = ++i); @@ -433,7 +433,7 @@ treeJSON = d3.json("B737.json", function(error, treeData) { nodeExit.select("text") .style("fill-opacity", 0); - // Update the links + // Update the links� var link = svgGroup.selectAll("path.link") .data(links, function(d) { return d.target.id; diff --git a/guides/index.html b/guides/index.html deleted file mode 100644 index 4adbe6f8..00000000 --- a/guides/index.html +++ /dev/null @@ -1,49 +0,0 @@ ---- -layout: awesome ---- - -
    - -
    - -
    -
    -

    Tutorials

    -

    Examples for Getting Started

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    - - -
    -

    These are tutorials for SUAVE. The tutorials will then help you get started with SUAVE. We recommend starting with the Boeing 737-800 tutorial and then moving to the Transport Optimization or the Turbofan Network tutorial. These will allow you to explore the capabilities of SUAVE. If you haven't already downloaded the latest accompanying tutorial scripts you can find them here.

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    + + + + SUAVE + + + + -
    + + + -
    -
    -

    SUAVE

    -

    An Aerospace Vehicle Environment for Designing Future Aircraft

    -
    -
    -
    -

    SUAVE is a conceptual level aircraft design environment built with the ability to analyze and optimize both conventional and unconventional designs. This capability is achieved in part by allowing analysis information for aircraft to be drawn from multiple sources. Many other software tools for aircraft conceptual design rely on fixed empirical correlations and other handbook approximation. SUAVE instead provides a framework that can be used to design aircraft featuring advanced technologies by augmenting relevant correlations with physics-based methods.

    + + + + +
    -

    Blended Wing Body

    + + -

    -T. MacDonald, E. Botero, J. M. Vegh, A. Variyar, J. J. Alonso, T. Orra, C. Ilario da Silva. "SUAVE: An Open-Source Environment Enabling Unconventional Designs through Higher Fidelity", 55th AIAA Aerospace Sciences Meeting, Grapevine, TX, January 2017. -

    + + + +
    +
    + +

    SUAVE is a conceptual level aircraft design environment built with the ability to analyze and optimize both conventional and unconventional designs. + This capability is achieved in part by allowing analysis information for aircraft to be drawn from multiple sources. + Many other software tools for aircraft conceptual design rely on fixed empirical correlations and other handbook approximation. + SUAVE instead provides a framework that can be used to design aircraft featuring advanced technologies by augmenting relevant correlations with physics-based methods. +

    +
    + +
    +
    + +
    +
    +
    +
    +
    + +

    Open Source

    +

    Released in LGPL 2.1. This open source license + enables commercial industry and academia to collaborate together.

    +
    -

    -T. MacDonald, M. Clarke, E. Botero, J. M. Vegh, J. J. Alonso. "SUAVE: An Open-Source Environment Enabling Multi-fidelity Vehicle Optimization", 16th AIAA Multidisciplinary Analysis and Optimization Conference, Denver, CO, June 2017. -

    - -

    Partners

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    Python 3

    +

    Built on the latest versions of SciPy, NumPy, and scikit-learn for maximum portability and flexibility.

    +
    +
    +
    +
    + +

    Conceptual Design

    +

    Physics based analysis combined with proven + correlations allows SUAVE to perform multifidelity optimization.

    +
    +
    +
    +
    +
    - - + +
    +
    +
    +

    Supersonics, eVTOLs, Solar UAVs, Airliners, MultiCopters...

    +

    SUAVE: Aerospace Conceptual Design Environment

    +
    +
    +
    + + +
    +
    +
    +

    Are you ready to design the future of aerospace?

    + Download +
    +
    +
    + + + + + + + + + + + + + + diff --git a/js/main.js b/js/main.js deleted file mode 100644 index 39c373e7..00000000 --- a/js/main.js +++ /dev/null @@ -1,23 +0,0 @@ -(function () { - 'use strict'; - /*globals moment*/ - - window.onload = function () { - if (document.readyState === 'complete') { - init(); - } - }; - - function init() { - // Do something awesome here... - var datesElement = document.querySelectorAll('.post-date'); - - for (var i = 0, l = datesElement.length; i < l; i ++) { - var de = datesElement[i]; - var date = de.getAttribute('post-date'); - - de.textContent = moment(date).fromNow(); - } - } - -})(); diff --git a/js/print-email.js b/js/print-email.js deleted file mode 100644 index 1bd6b161..00000000 --- a/js/print-email.js +++ /dev/null @@ -1,8 +0,0 @@ -//outputs a mailto link in the form: -//[addr]@[domain] -function printEmailLink(addr, domain, link) -{ - //var domain = 'stanford.edu'; - document.write(''); - document.write(link + ''); -} \ No newline at end of file diff --git a/latest_release.html b/latest_release.html new file mode 100644 index 00000000..555c7eed --- /dev/null +++ b/latest_release.html @@ -0,0 +1,168 @@ + + + + + Latest + + + + + + + + + + +
    + + + + + +
    +
    +
    + + + +
    +
    +

    SUAVE 2.5.0

    +

    The Latest in Aerospace Design

    +
    + +

    This release has numerous changes. Unfortunately, some interfaces have been altered to support all these changes. We tried to make these interface alterations as user friendly and intuitive as possible. The next major release will be a 3.0 with significant changes.

    + + +
      +
    • VLM: Control surfaces, sideslip, rotation rate effects, and arbitrary discretization.
    • +
    • Nacelles are now independent geometric objects from networks
    • +
    • Energy networks: fewer networks, propellers and motors can be appended arbitrarily, networks are no longer referred as propulsors, and integrating a mission with a network is much easier.
    • +
    • Battery model rewrite
    • +
    • New airfoil panel method
    • +
    • Momentum wake effects from rotors
    • +
    • Updates for both import and export of vehicles to OpenVSP (propellers/rotors are now seamless)
    • +
    • New Noise models
    • +
    • Stability derivatives from VLM including with respect to control surface deflections
    • +
    • VTK file outputs for rotor wake simulations
    • +
    • New plotting functions
    • +
    • Under the hood fixes: hover corrections, FLOPS, CG, fineness ratio, propellers/rotors are merged, removed duplicated iterations, addressed many known issues
    • +
    + + +
  • We have also made a tutorial on using 2.5 for basic eVTOL analysis.
  • + +
    + + +
    + +
    +
    +
    + +
    +
    +
    +

    Are you ready to design the future of aerospace?

    + Download +
    +
    +
    + + + + + + + + + + + + + + + diff --git a/publications.html b/publications.html new file mode 100644 index 00000000..783ea482 --- /dev/null +++ b/publications.html @@ -0,0 +1,182 @@ + + + + + Publications + + + + + + + + + + +
    + + + + + +
    +
    +
    + +
    +
    + +

    Aerodynamic Verification and Validation of SUAVE

    +
    +
    + +

    Forecasting the Operational Lifetime of Electric Aircraft Through Battery Degradation Modeling

    +
    +
    + +

    Evaluating the Performance and Acoustic Footprint of Aircraft for Regional and Urban Air Mobility

    +
    +
    + +

    Lithium–Ion Battery Modeling for Aerospace Applications

    +
    +
    + +

    Aerodynamic Optimization of Wing-Mounted Propeller Configurations for Distributed Electric Propulsion Architectures

    +
    +
    + +

    A Low-Cost Aero-Propulsive Analysis of Distributed Electric Propulsion Aircraft

    +
    +
    + +

    Current Capabilities and Challenges of NDARC and SUAVE for eVTOL Aircraft Design and Analysis

    +
    +
    + +

    Strategies for Posing a Well-Defined Problem for Urban Air Mobility Vehicles

    +
    +
    + +

    Conceptual Design and Optimization of Small Transitioning UAVs using SUAVE

    +
    +
    + +

    SUAVE: An Open-Source Environment Enabling Multi-Fidelity Vehicle Optimization

    +
    +
    + +

    SUAVE: An Open-Source Environment Enabling Unconventional Vehicle Designs through Higher Fidelity

    +
    +
    + +

    Comparing Different Off-the-Shelf Optimizers’ Performance in Conceptual Aircraft Design

    +
    +
    + +

    SUAVE: An Open-Source Environment for Conceptual Vehicle Design and Optimization

    +
    +
    + +

    SUAVE: An Open-Source Environment for Multi-Fidelity Conceptual Vehicle Design

    +
    +
    +
    +
    +
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b/publications/uav_transition.pdf differ diff --git a/register.md b/register.md deleted file mode 100644 index e8e05b39..00000000 --- a/register.md +++ /dev/null @@ -1,10 +0,0 @@ ---- -layout: page -title: Register -subtitle: Together we design exotic aerospace configurations - -permalink: /register/ ---- - - - diff --git a/registration.html b/registration.html new file mode 100644 index 00000000..f9bad517 --- /dev/null +++ b/registration.html @@ -0,0 +1,131 @@ + + + + + SUAVE Registration + + + + + + + + + +
    + + + + + +
    +
    +
    + + + +
    +

    Registration

    +
    + + + +
    +
    +
    + + + + + + + + + + + + + + \ No newline at end of file diff --git a/tutorials.html b/tutorials.html new file mode 100644 index 00000000..cbcc15c5 --- /dev/null +++ b/tutorials.html @@ -0,0 +1,162 @@ + + + + + Tutorials + + + + + + + + + + +
    + + + + +
    +
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    + +
    +
    + + + +
    +
    +

    Tutorials

    +

    These are tutorials for SUAVE. The tutorials will then help you get started with SUAVE. We recommend starting with the Boeing 737-800 tutorial and then moving to the Regional Jet Optimization or the Turbofan Network tutorial. These will allow you to explore the capabilities of SUAVE. If you haven't already downloaded the latest accompanying tutorial scripts you can find them here.

    +
    + + +
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    + + + + + + + + + + + + + + \ No newline at end of file diff --git a/tutorials/B737.html b/tutorials/B737.html new file mode 100644 index 00000000..02d7b658 --- /dev/null +++ b/tutorials/B737.html @@ -0,0 +1,743 @@ + + + + + Boeing 737-800 - SUAVE Tutorial + + + + + + + + + + +
    + + + + + +
    +
    +
    + + + +
    +
    +

    Boeing 737-800

    +
    + +

    This tutorial shows how the user can build a conventional aircraft and analyze its performance over the course of a mission. The focus is on providing general information that can apply to setup for a variety of vehicles.

    + +

    Running the Tutorial File:

    + +

    Before jumping into the code, it is important to make sure that your installation is working properly. To do this, we start by running the tutorial file.

    + +
      +
    1. Locate the tutorial file, titled "tut_mission_B737_800.py". If you are using an IDE, open the file there. Otherwise, navigate to the containing folder in the command line.
    2. +
    3. Run the file in your IDE or if in the command line use the command
      python tut_mission_B737_800.py
      Note that depending on your system settings you may need to use "python3" or another command instead. Remember that SUAVE is only compatible with Python 3.
    4. +
    5. Review the plots that are generated. If everything is running properly, you should have several performance plots and matching .pdf and .png files in your tutorial directory. If you have trouble with this step, first check the installation instructions and then refer to the forum with any questions.
    6. +
    + +

    Collecting Information on the Chosen Vehicle:

    + +

    For this tutorial, we will be analyzing a Boeing 737-800. The values shown come from a variety of sources. For most common aircraft, parameters can be found online or extracted from available three views. For Boeing aircraft, much of this information can be found in their airport planning documentation.

    + +

    Using the Code:

    +

    Now we will step through the code to explain how it works and where changes can be made to create a different vehicle.

    + +

    Header and Imports

    +

    The header contains the file name and information on who created it and when it was last modified. If you plan to add your other files to the main SUAVE repository, a similar header should be created with matching style. A line only needs to be added to the modified section when significant changes are made. This would be to identify you as a key person to check with if someone has questions about the file.

    + +
    # tut_mission_B737.py
    +# 
    +# Created:  Aug 2014, SUAVE Team
    +# Modified: Aug 2017, SUAVE Team
    +#           Mar 2020, E. Botero
    +

    +

    The imports contain two sections. The first is generally used Python libraries, which are not specific to SUAVE. Two are imported here. The first is numpy, which is a common numerical programming package used in scientific computing. The second is matplotlib, which allows plotting of the results.

    + +
    # General Python Imports
    +import numpy as np
    +# Numpy is a commonly used mathematically computing package. It contains many frequently used
    +# mathematical functions and is faster than native Python, especially when using vectorized
    +# quantities.
    +import matplotlib.pyplot as plt
    +# Matplotlib's pyplot can be used to generate a large variety of plots. Here it is used to create
    +# visualizations of the aircraft's performance throughout the mission.
    +

    +

    Next is the SUAVE imports. SUAVE is imported directly first, which allows us to grab individual SUAVE classes later on without importing each one at the top. Next, the Data and Units modules are imported. Data is a SUAVE-specific data structure that operates much like a dictionary but has some special features as described in the comments. The Units module is a standardized way to do unit conversions, also further described in the comments. After that is the turbofan sizing method. This method is used to size the design mass flow, and does not specify any geometric properties.

    + + + +
    # SUAVE Imports
    +import SUAVE
    +from SUAVE.Core import Data, Units 
    +# The Data import here is a native SUAVE data structure that functions similarly to a dictionary.
    +#   However, iteration directly returns values, and values can be retrieved either with the 
    +#   typical dictionary syntax of "entry['key']" or the more class-like "entry.key". For this to work
    +#   properly, all keys must be strings.
    +# The Units import is used to allow units to be specified in the vehicle setup (or elsewhere).
    +#   This is because SUAVE functions generally operate using metric units, so inputs must be 
    +#   converted. To use a length of 20 feet, set l = 20 * Units.ft . Additionally, to convert to SUAVE
    +#   output back to a desired units, use l_ft = l_m / Units.ft
    +from SUAVE.Plots.Mission_Plots import *
    +# These are a variety of plotting routines that simplify the plotting process for commonly 
    +# requested metrics. Plots of specifically desired metrics can also be manually created.
    +from SUAVE.Methods.Propulsion.turbofan_sizing import turbofan_sizing
    +# Rather than conventional sizing, this script builds the turbofan energy network. This process is
    +# covered in more detail in a separate tutorial. It does not size the turbofan geometry.
    +

    + +

    main

    +

    The main function builds the vehicle, runs the mission, and plots the results by calling the required functions in sequence. The details of each call can be seen in the comments.

    +
    def main():
    +    """This function gets the vehicle configuration, analysis settings, and then runs the mission.
    +    Once the mission is complete, the results are plotted."""
    +    
    +    # Extract vehicle configurations and the analysis settings that go with them
    +    configs, analyses = full_setup()
    +
    +    # Size each of the configurations according to a given set of geometry relations
    +    simple_sizing(configs)
    +
    +    # Perform operations needed to make the configurations and analyses usable in the mission
    +    configs.finalize()
    +    analyses.finalize()
    +
    +    # Determine the vehicle weight breakdown (independent of mission fuel usage)
    +    weights = analyses.configs.base.weights
    +    breakdown = weights.evaluate()      
    +
    +    # Performance a mission analysis
    +    mission = analyses.missions.base
    +    results = mission.evaluate()
    +
    +    # Plot all mission results, including items such as altitude profile and L/D
    +    plot_mission(results)
    +
    +    return
    +

    + +

    full_setup

    +

    This function builds the vehicle configurations, their analyses, and the mission. The mission is built here because the missions are attached to the analyses. In the context of SUAVE, configurations refer to changes in the vehicle in relation to its baseline setup. These can range for flap deflections to a different number of engines (something which may be more relevant for eVTOL concepts).

    +
    def full_setup():
    +    """This function gets the baseline vehicle and creates modifications for different 
    +    configurations, as well as the mission and analyses to go with those configurations."""
    +
    +    # Collect baseline vehicle data and changes when using different configuration settings
    +    vehicle  = vehicle_setup()
    +    configs  = configs_setup(vehicle)
    +
    +    # Get the analyses to be used when different configurations are evaluated
    +    configs_analyses = analyses_setup(configs)
    +
    +    # Create the mission that will be flown
    +    mission  = mission_setup(configs_analyses)
    +    missions_analyses = missions_setup(mission)
    +
    +    # Add the analyses to the proper containers
    +    analyses = SUAVE.Analyses.Analysis.Container()
    +    analyses.configs  = configs_analyses
    +    analyses.missions = missions_analyses
    +
    +    return configs, analyses

    + +

    analyses_setup

    +

    This function assigns a set of analyses to each configuration. In this tutorial, all configurations have the same analyses set. If you would like a different analyses set to be used for a particular configuration, this is the place to call that function.

    +
    def analyses_setup(configs):
    +    """Set up analyses for each of the different configurations."""
    +
    +    analyses = SUAVE.Analyses.Analysis.Container()
    +
    +    # Build a base analysis for each configuration. Here the base analysis is always used, but
    +    # this can be modified if desired for other cases.
    +    for tag,config in configs.items():
    +        analysis = base_analysis(config)
    +        analyses[tag] = analysis
    +
    +    return analyses

    + +

    base_analysis

    +

    This is the function that sets each individual analysis. Here are considerations for each of the analyses shown:

    +
      +
    1. Weights - the weights method here is based on empirical correlations for tube and wing transport configurations. It will give a breakdown of the various components in the aircraft. The weights method is not directly used in the performance analysis.
    2. +
    3. Aerodynamics - the aerodynamics method is labeled here as "fidelity zero," which indicates that it is SUAVE's baseline analysis method. This method is designed for subsonic transport aircraft and is similar to what can be found in many conceptual design texts. Other methods are available for different purposes.
    4. +
    5. Stability - the stability method is not used in the current mission, but can be used for checks afterwards. This one is also labeled as fidelity zero and has similar applicability.
    6. +
    7. Energy - the energy analysis will run any energy network that is attached to the vehicle. For this vehicle it will include only the turbofan.
    8. +
    9. Planet - this is needed so that we can attach an atmosphere.
    10. +
    11. Atmosphere - this sets the atmospheric conditions that the aircraft will fly through. The US 1976 standard atmosphere is a common choice for performance analysis.
    12. +
    +
    def base_analysis(vehicle):
    +    """This is the baseline set of analyses to be used with this vehicle. Of these, the most
    +    commonly changed are the weights and aerodynamics methods."""
    +
    +    # ------------------------------------------------------------------
    +    #   Initialize the Analyses
    +    # ------------------------------------------------------------------     
    +    analyses = SUAVE.Analyses.Vehicle()
    +
    +    # ------------------------------------------------------------------
    +    #  Weights
    +    weights = SUAVE.Analyses.Weights.Weights_Tube_Wing()
    +    weights.vehicle = vehicle
    +    analyses.append(weights)
    +
    +    # ------------------------------------------------------------------
    +    #  Aerodynamics Analysis
    +    aerodynamics = SUAVE.Analyses.Aerodynamics.Fidelity_Zero()
    +    aerodynamics.geometry = vehicle
    +    analyses.append(aerodynamics)
    +
    +    # ------------------------------------------------------------------
    +    #  Stability Analysis
    +    stability = SUAVE.Analyses.Stability.Fidelity_Zero()
    +    stability.geometry = vehicle
    +    analyses.append(stability)
    +
    +    # ------------------------------------------------------------------
    +    #  Energy
    +    energy= SUAVE.Analyses.Energy.Energy()
    +    energy.network = vehicle.propulsors 
    +    analyses.append(energy)
    +
    +    # ------------------------------------------------------------------
    +    #  Planet Analysis
    +    planet = SUAVE.Analyses.Planets.Planet()
    +    analyses.append(planet)
    +
    +    # ------------------------------------------------------------------
    +    #  Atmosphere Analysis
    +    atmosphere = SUAVE.Analyses.Atmospheric.US_Standard_1976()
    +    atmosphere.features.planet = planet.features
    +    analyses.append(atmosphere)   
    +
    +    return analyses    

    + +

    vehicle_setup

    +

    This function is where the baseline vehicle is defined. The order of the components added in this section is arbitrary. To start, we create a vehicle instance and add a tag. This tag can be any string.

    +
        vehicle = SUAVE.Vehicle()
    +    vehicle.tag = 'Boeing_737-800'  

    + +

    The next step is to define the high-level vehicle parameters. This consists of the items shown below. Units.lb could be used here to automatically convert values from pounds to kilograms. If a conversion from pounds to Newtons is desired in another context, Units.lbf can be used.

    +
        # Vehicle level mass properties
    +    # The maximum takeoff gross weight is used by a number of methods, most notably the weight
    +    # method. However, it does not directly inform mission analysis.
    +    vehicle.mass_properties.max_takeoff               = 79015.8 * Units.kilogram 
    +    # The takeoff weight is used to determine the weight of the vehicle at the start of the mission
    +    vehicle.mass_properties.takeoff                   = 79015.8 * Units.kilogram   
    +    # Operating empty may be used by various weight methods or other methods. Importantly, it does
    +    # not constrain the mission analysis directly, meaning that the vehicle weight in a mission
    +    # can drop below this value if more fuel is needed than is available.
    +    vehicle.mass_properties.operating_empty           = 62746.4 * Units.kilogram 
    +    # The maximum zero fuel weight is also used by methods such as weights
    +    vehicle.mass_properties.max_zero_fuel             = 62732.0 * Units.kilogram
    +    # Cargo weight typically feeds directly into weights output and does not affect the mission
    +    vehicle.mass_properties.cargo                     = 10000.  * Units.kilogram   
    +    
    +    # Envelope properties
    +    # These values are typical FAR values for a transport of this type
    +    vehicle.envelope.ultimate_load = 3.75
    +    vehicle.envelope.limit_load    = 2.5
    +
    +    # Vehicle level parameters
    +    # The vehicle reference area typically matches the main wing reference area 
    +    vehicle.reference_area         = 124.862 * Units['meters**2']  
    +    # Number of passengers, control settings, and accessories settings are used by the weights
    +    # methods
    +    vehicle.passengers             = 170
    +    vehicle.systems.control        = "fully powered" 
    +    vehicle.systems.accessories    = "medium range"

    + +

    Next the landing gear are defined. The values shown here are not actually used in the calculation performed by this tutorial script, but may be used for noise analysis.

    +
        # The settings here can be used for noise analysis, but are not used in this tutorial
    +    landing_gear = SUAVE.Components.Landing_Gear.Landing_Gear()
    +    landing_gear.tag = "main_landing_gear"
    +    
    +    landing_gear.main_tire_diameter = 1.12000 * Units.m
    +    landing_gear.nose_tire_diameter = 0.6858 * Units.m
    +    landing_gear.main_strut_length  = 1.8 * Units.m
    +    landing_gear.nose_strut_length  = 1.3 * Units.m
    +    landing_gear.main_units  = 2    # Number of main landing gear
    +    landing_gear.nose_units  = 1    # Number of nose landing gear
    +    landing_gear.main_wheels = 2    # Number of wheels on the main landing gear
    +    landing_gear.nose_wheels = 2    # Number of wheels on the nose landing gear      
    +    vehicle.landing_gear = landing_gear

    + +

    The main wing is now defined. Note that the Main_Wing class is used. This will automatically let certain analyses know that this is the main wing (or potentially one of them). The tag 'main_wing' may still be in use with some older analysis, but efforts are being made to remove dependence of analyses on this tag. Other notes on this setup can be seen in the comments.

    +
        # This main wing is approximated as a simple trapezoid. A segmented wing can also be created if
    +    # desired. Segmented wings appear in later tutorials, and a version of the 737 with segmented
    +    # wings can be found in the SUAVE testing scripts.
    +    
    +    # SUAVE allows conflicting geometric values to be set in terms of items such as aspect ratio
    +    # when compared with span and reference area. Sizing scripts may be used to enforce 
    +    # consistency if desired.
    +    
    +    wing = SUAVE.Components.Wings.Main_Wing()
    +    wing.tag = 'main_wing'
    +    
    +    wing.aspect_ratio            = 10.18
    +    # Quarter chord sweep is used as the driving sweep in most of the low fidelity analysis methods.
    +    # If a different known value (such as leading edge sweep) is given, it should be converted to
    +    # quarter chord sweep and added here. In some cases leading edge sweep will be used directly as
    +    # well, and can be entered here too.
    +    wing.sweeps.quarter_chord    = 25 * Units.deg
    +    wing.thickness_to_chord      = 0.1
    +    wing.taper                   = 0.1
    +    wing.spans.projected         = 34.32 * Units.meter
    +    wing.chords.root             = 7.760 * Units.meter
    +    wing.chords.tip              = 0.782 * Units.meter
    +    wing.chords.mean_aerodynamic = 4.235 * Units.meter
    +    wing.areas.reference         = 124.862 * Units['meters**2']  
    +    wing.twists.root             = 4.0 * Units.degrees
    +    wing.twists.tip              = 0.0 * Units.degrees
    +    wing.origin                  = [[13.61, 0, -1.27]] * Units.meter
    +    wing.vertical                = False
    +    wing.symmetric               = True
    +    # The high lift flag controls aspects of maximum lift coefficient calculations
    +    wing.high_lift               = True
    +    # The dynamic pressure ratio is used in stability calculations
    +    wing.dynamic_pressure_ratio  = 1.0

    + +

    The control surfaces follow the general geometric definition. For the main wing, these are used in high lift calculations and if export to AVL is desired. Span fractions include the centerbody.

    +
        # Information in this section is used for high lift calculations and when conversion to AVL
    +    # is desired.
    +    
    +    # Deflections will typically be specified separately in individual vehicle configurations.
    +    
    +    flap                       = SUAVE.Components.Wings.Control_Surfaces.Flap() 
    +    flap.tag                   = 'flap' 
    +    flap.span_fraction_start   = 0.20 
    +    flap.span_fraction_end     = 0.70   
    +    flap.deflection            = 0.0 * Units.degrees
    +    # Flap configuration types are used in computing maximum CL and noise
    +    flap.configuration_type    = 'double_slotted'
    +    flap.chord_fraction        = 0.30   
    +    wing.append_control_surface(flap)   
    +        
    +    slat                       = SUAVE.Components.Wings.Control_Surfaces.Slat() 
    +    slat.tag                   = 'slat' 
    +    slat.span_fraction_start   = 0.324 
    +    slat.span_fraction_end     = 0.963     
    +    slat.deflection            = 0.0 * Units.degrees
    +    slat.chord_fraction        = 0.1  	 
    +    wing.append_control_surface(slat)  
    +        
    +    aileron                       = SUAVE.Components.Wings.Control_Surfaces.Aileron() 
    +    aileron.tag                   = 'aileron' 
    +    aileron.span_fraction_start   = 0.7 
    +    aileron.span_fraction_end     = 0.963 
    +    aileron.deflection            = 0.0 * Units.degrees
    +    aileron.chord_fraction        = 0.16    
    +    wing.append_control_surface(aileron)    
    +    
    +    # Add to vehicle
    +    vehicle.append_component(wing)

    + +

    Next is the horizontal stabilizer. This is built in nearly the same way as the main wing, but now uses the Horizontal_Tail class.

    +
        wing = SUAVE.Components.Wings.Horizontal_Tail()
    +    wing.tag = 'horizontal_stabilizer'

    + +

    The vertical stabilizer also uses a different class, and otherwise has one additional field to designate it as a t-tail or not. This difference is used in the weight calculation.

    +
        wing = SUAVE.Components.Wings.Vertical_Tail()

    +
        wing.t_tail                  = False

    + +

    With the wings complete, we now move to the fuselage. A number of geometric parameters are defined here, with unusual ones described in the comments.

    +
        fuselage = SUAVE.Components.Fuselages.Fuselage()
    +    fuselage.tag = 'fuselage'
    +    
    +    # Number of coach seats is used in some weights methods
    +    fuselage.number_coach_seats    = vehicle.passengers
    +    # The seats abreast can be used along with seat pitch and the number of coach seats to
    +    # determine the length of the cabin if desired.
    +    fuselage.seats_abreast         = 6
    +    fuselage.seat_pitch            = 1     * Units.meter
    +    # Fineness ratios are used to determine VLM fuselage shape and sections to use in OpenVSP
    +    # output
    +    fuselage.fineness.nose         = 1.6
    +    fuselage.fineness.tail         = 2.
    +    # Nose and tail lengths are used in the VLM setup
    +    fuselage.lengths.nose          = 6.4   * Units.meter
    +    fuselage.lengths.tail          = 8.0   * Units.meter
    +    fuselage.lengths.total         = 38.02 * Units.meter
    +    # Fore and aft space are added to the cabin length if the fuselage is sized based on
    +    # number of seats
    +    fuselage.lengths.fore_space    = 6.    * Units.meter
    +    fuselage.lengths.aft_space     = 5.    * Units.meter
    +    fuselage.width                 = 3.74  * Units.meter
    +    fuselage.heights.maximum       = 3.74  * Units.meter
    +    fuselage.effective_diameter    = 3.74     * Units.meter
    +    fuselage.areas.side_projected  = 142.1948 * Units['meters**2'] 
    +    fuselage.areas.wetted          = 446.718  * Units['meters**2'] 
    +    fuselage.areas.front_projected = 12.57    * Units['meters**2'] 
    +    # Maximum differential pressure between the cabin and the atmosphere
    +    fuselage.differential_pressure = 5.0e4 * Units.pascal
    +    
    +    # Heights at different longitudinal locations are used in stability calculations and
    +    # in output to OpenVSP
    +    fuselage.heights.at_quarter_length          = 3.74 * Units.meter
    +    fuselage.heights.at_three_quarters_length   = 3.65 * Units.meter
    +    fuselage.heights.at_wing_root_quarter_chord = 3.74 * Units.meter
    +    
    +    # add to vehicle
    +    vehicle.append_component(fuselage)

    + +

    Next is the turbofan. It is created as a Turbofan energy network, which determines its behavior. More details on the turbofan are provided in the Turbofan Modeling Tutorial, and more information on energy networks in general can be found in the documentation section. The high-level parameters are reproduced here.

    +
        turbofan = SUAVE.Components.Energy.Networks.Turbofan()
    +    # For some methods, the 'turbofan' tag is still necessary. This will be changed in the
    +    # future to allow arbitrary tags.
    +    turbofan.tag = 'turbofan'
    +    
    +    # High-level setup
    +    turbofan.number_of_engines = 2
    +    turbofan.bypass_ratio      = 5.4
    +    turbofan.engine_length     = 2.71 * Units.meter
    +    turbofan.nacelle_diameter  = 2.05 * Units.meter
    +    turbofan.origin            = [[13.72, 4.86,-1.9],[13.72, -4.86,-1.9]] * Units.meter
    +    
    +    # Approximate the wetted area
    +    turbofan.areas.wetted      = 1.1*np.pi*turbofan.nacelle_diameter*turbofan.engine_length
    +    
    +    # Establish the correct working fluid
    +    turbofan.working_fluid = SUAVE.Attributes.Gases.Air()

    + +

    One component of particular interest is the thrust component. This is a bit different than the other components in the list since it is not a physical item. It is used to size the design mass flow of the engine, which determines what throttle is needed for a particular thrust. For this network, the thrust and mass flow scale linearly with throttle at given conditions.

    +
    
    +# ------------------------------------------------------------------
    +#  Component 11 - thrust (to compute the thrust)
    +
    +thrust = SUAVE.Components.Energy.Processes.Thrust()       
    +thrust.tag ='compute_thrust'
    +
    +# Design thrust is used to determine mass flow at full throttle
    +thrust.total_design             = 2*24000. * Units.N #Newtons
    +
    +# Design sizing conditions are also used to determine mass flow
    +altitude      = 35000.0*Units.ft
    +mach_number   = 0.78 
    +
    +# Add to network
    +turbofan.thrust = thrust

    + +

    configs_setup

    +

    This function is where the different vehicle configurations (labeled configs here) are defined. In this case, these configs only change flap and slat settings. To start, the base configuration is defined as simply matching the baseline vehicle. The configs are defined as containers, which are SUAVE Data classes with a few extra features such as append. The cruise config is created in almost the same way, but demonstrates that configs can be used to create a new config as well. The first config to include changes is then the takeoff config. This shows how vehicle parameters can be changed. The remaining configs follow a similar pattern.

    +
    def configs_setup(vehicle):
    +    """This function sets up vehicle configurations for use in different parts of the mission.
    +    Here, this is mostly in terms of high lift settings."""
    +    
    +    # ------------------------------------------------------------------
    +    #   Initialize Configurations
    +    # ------------------------------------------------------------------
    +    configs = SUAVE.Components.Configs.Config.Container()
    +
    +    base_config = SUAVE.Components.Configs.Config(vehicle)
    +    base_config.tag = 'base'
    +    configs.append(base_config)
    +
    +    # ------------------------------------------------------------------
    +    #   Cruise Configuration
    +    # ------------------------------------------------------------------
    +    config = SUAVE.Components.Configs.Config(base_config)
    +    config.tag = 'cruise'
    +    configs.append(config)
    +
    +    # ------------------------------------------------------------------
    +    #   Takeoff Configuration
    +    # ------------------------------------------------------------------
    +    config = SUAVE.Components.Configs.Config(base_config)
    +    config.tag = 'takeoff'
    +    config.wings['main_wing'].control_surfaces.flap.deflection = 20. * Units.deg
    +    config.wings['main_wing'].control_surfaces.slat.deflection = 25. * Units.deg
    +    # A max lift coefficient factor of 1 is the default, but it is highlighted here as an option
    +    config.max_lift_coefficient_factor    = 1.
    +
    +    configs.append(config)

    + +

    simple_sizing

    +

    This function modifies the base and landing configurations according to a few sizing relations. These relationships could be replaced with others depending on your needs. Additionally, a few functions exist to more fully size the wing and fuselage based on a smaller number of inputs. They exist here.

    +
    def simple_sizing(configs):
    +    """This function applies a few basic geometric sizing relations and modifies the landing
    +    configuration."""
    +
    +    base = configs.base
    +    # Update the baseline data structure to prepare for changes
    +    base.pull_base()
    +
    +    # Revise the zero fuel weight. This will only affect the base configuration. To do all
    +    # configurations, this should be specified in the top level vehicle definition.
    +    base.mass_properties.max_zero_fuel = 0.9 * base.mass_properties.max_takeoff 
    +
    +    # Estimate wing areas
    +    for wing in base.wings:
    +        wing.areas.wetted   = 2.0 * wing.areas.reference
    +        wing.areas.exposed  = 0.8 * wing.areas.wetted
    +        wing.areas.affected = 0.6 * wing.areas.wetted
    +
    +    # Store how the changes compare to the baseline configuration
    +    base.store_diff()
    +
    +    # ------------------------------------------------------------------
    +    #   Landing Configuration
    +    # ------------------------------------------------------------------
    +    landing = configs.landing
    +
    +    # Make sure base data is current
    +    landing.pull_base()
    +
    +    # Add a landing weight parameter. This is used in field length estimation and in
    +    # initially the landing mission segment type.
    +    landing.mass_properties.landing = 0.85 * base.mass_properties.takeoff
    +
    +    # Store how the changes compare to the baseline configuration
    +    landing.store_diff()
    +
    +    return

    + +

    mission_setup

    +

    The mission setup describes the mission profile that is used for computing aircraft performance. It consists of a series of segments that are then simulated sequentially. More information on the details of the mission solver can be found here. This also contains a starting airport, which may be used with other types of analysis but does not affect to flown mission by default.

    +
    def mission_setup(analyses):
    +    """This function defines the baseline mission that will be flown by the aircraft in order
    +    to compute performance."""
    +
    +    # ------------------------------------------------------------------
    +    #   Initialize the Mission
    +    # ------------------------------------------------------------------
    +
    +    mission = SUAVE.Analyses.Mission.Sequential_Segments()
    +    mission.tag = 'the_mission'
    +
    +    # Airport
    +    # The airport parameters are used in calculating field length and noise. They are not
    +    # directly used in mission performance estimation
    +    airport = SUAVE.Attributes.Airports.Airport()
    +    airport.altitude   =  0.0  * Units.ft
    +    airport.delta_isa  =  0.0
    +    airport.atmosphere = SUAVE.Attributes.Atmospheres.Earth.US_Standard_1976()
    +
    +    mission.airport = airport    
    +
    +    # Unpack Segments module
    +    Segments = SUAVE.Analyses.Mission.Segments
    +
    +    # Base segment 
    +    base_segment = Segments.Segment()
    +
    +    # ------------------------------------------------------------------
    +    #   First Climb Segment: Constant Speed, Constant Rate
    +    # ------------------------------------------------------------------
    +
    +    # A constant speed, constant rate climb segment is used first. This means that the aircraft
    +    # will maintain a constant airspeed and constant climb rate until it hits the end altitude.
    +    # For this type of segment, the throttle is allowed to vary as needed to match required
    +    # performance.
    +    segment = Segments.Climb.Constant_Speed_Constant_Rate(base_segment)
    +    # It is important that all segment tags must be unique for proper evaluation. At the moment 
    +    # this is not automatically enforced. 
    +    segment.tag = "climb_1"
    +
    +    # The analysis settings for mission segment are chosen here. These analyses include information
    +    # on the vehicle configuration.
    +    segment.analyses.extend( analyses.takeoff )
    +
    +    segment.altitude_start = 0.0   * Units.km
    +    segment.altitude_end   = 3.0   * Units.km
    +    segment.air_speed      = 125.0 * Units['m/s']
    +    segment.climb_rate     = 6.0   * Units['m/s']
    +
    +    # Add to misison
    +    mission.append_segment(segment)

    + +

    missions_setup

    +

    This function allows the bundling of multiple missions into a missions container, but only contains the base mission in this tutorial. If multiple missions are added here, they still must be called individually for evaluation.

    +
    def missions_setup(base_mission):
    +    """This allows multiple missions to be incorporated if desired, but only one is used here."""
    +
    +    # Setup the mission container
    +    missions = SUAVE.Analyses.Mission.Mission.Container()
    +
    +    # ------------------------------------------------------------------
    +    #   Base Mission
    +    # ------------------------------------------------------------------
    +
    +    # Only one mission (the base mission) is defined in this case
    +    missions.base = base_mission
    +
    +    return missions  

    + +

    plot_mission

    +

    The last function in this file is used to plot the performance results from the mission evaluation. The results shown are not an exhaustive list of SUAVE outputs, and custom plotting routines can be created.

    +
    def plot_mission(results,line_style='bo-'):
    +    """This function plots the results of the mission analysis and saves those results to 
    +    png files."""
    +
    +    # Plot Flight Conditions 
    +    plot_flight_conditions(results, line_style)

    + +

    This section should generate the plots below if the mission analysis executes correctly. The results show the aerodynamic, propulsion, and mission properties of the B737-800 for the defined mission.

    + +

    B737 Conditions

    + +

    B737 Mission

    + +

    B737 Aerodynamic Coefficients

    + +

    B737 Aerodynamic Forces

    + +

    B737 Drag

    + +

    Modifying the Aircraft's Geometry or Mission:

    + +

    Suppose we want to simulate a high span variant of the B737-800. The span is increased to 40.0 m. We assume the wing chords, sweep, taper ratio, thickness to chord ratio remain the same. Thus changing the span only changes the aspect ratio and the wing area.

    + +

    Now we try to fly the aircraft at a lower cruise speed of 200 m/s at a cruise altitude of 25000 ft

    + +

    1) To update the geometry, scroll to the vehicle_setup() function

    + +

    2) Modify the parameters of the main wing

    + +
    wing.aspect_ratio            = 10.12      
    +wing.spans.projected         = 40.0  * Units.meter
    +wing.areas.reference         = 158.0 * Units['meters**2']

    + +

    You may also need to update the reference area for the aircraft.

    + +
    vehicle.reference_area         =     158.0

    + +

    3) Update the mission parameters by moving to the mission_setup function

    + +

    4) First update the end altitude of the final climb segment. Although the original script has the altitude stated in m, courtesy of the Units package it is easy to modify the altitude to 25,000 ft without worrying about the units conversion as shown below.

    + +
    segment = Segments.Climb.Constant_Speed_Constant_Rate(base_segment)
    +segment.tag = "climb_3"
    +
    +segment.analyses.extend( analyses.cruise )
    +
    +segment.altitude_end = 25000  * Units.ft  
    +segment.air_speed    = 226.0  * Units['m/s']
    +segment.climb_rate   = 3.0    * Units['m/s']
    +
    +mission.append_segment(segment)

    + +

    5) Next update the cruise segment velocity to the new speed value

    + +
    segment = Segments.Cruise.Constant_Speed_Constant_Altitude(base_segment)
    +segment.tag = "cruise"
    +
    +segment.analyses.extend( analyses.cruise )
    +
    +segment.air_speed  = 200.0 * Units['m/s']
    +segment.distance   = 2490. * Units.nautical_miles
    +
    +# add to mission
    +mission.append_segment(segment)

    + +

    6) Now go back and run the mission for the updated geometry and mission.

    + +

    What's Next?

    +

    This tutorial has shown the basic building blocks of a SUAVE vehicle and mission analysis. Remaining tutorials cover different ways that you may wish to use the code, including new analysis definitions and optimization. Check out the remaining tutorials to learn about these topics and more. If there is something you would like to do that you do not see covered in the tutorials, feel free to ask about it on our forum.

    + +
    +
    + +
    +
    +
    + + + + + + + + + + + + + + \ No newline at end of file diff --git a/tutorials/Concorde.html b/tutorials/Concorde.html new file mode 100644 index 00000000..ba007602 --- /dev/null +++ b/tutorials/Concorde.html @@ -0,0 +1,232 @@ + + + + + Creating and Using a New Analysis + + + + + + + + + + +
    + + + + + +
    +
    +
    + + + +
    +
    +

    Creating and Using a New Analysis

    +
    + +

    This tutorial is designed to provide the information needed to modify a SUAVE aerodynamic analysis and create new ones. Many of the items discussed here also apply to other analysis types within SUAVE. For this tutorial, the Concorde is used to demonstrate switching the aerodynamic analysis to one that can handle supersonic conditions.

    + +

    Baseline Aerodynamic Analysis

    + +

    The basic aerodynamic analysis used in SUAVE is called Fidelity_Zero. It is based on a mix of low fidelity physical and empirical methods, similar to what you might find in a typical conceptual design textbook. This is what is used for the 737 in the previous tutorial, and is specified in the analysis settings:

    + +
    def base_analysis(vehicle):
    +...
    +    # ------------------------------------------------------------------
    +    #  Aerodynamics Analysis
    +    aerodynamics = SUAVE.Analyses.Aerodynamics.Fidelity_Zero()
    +    aerodynamics.geometry = vehicle
    +    analyses.append(aerodynamics)
    +...
    +

    +

    In the SUAVE code structure, the analysis is broken into two sections. One is what you see above, which is the analysis class. The other is the individual methods that are used in the analysis class, which are stored in separate Methods folders. The purpose of splitting them is to make it easier for the different analysis classes to share methods. We will start with an explanation of the individual bits of the analysis class in the file trunk/Analyses/Aerodynamics/Fidelity_Zero.py.

    + +

    The first section is the imports. These are mix of standard imports and a few specific items needed for the analysis. They are described individually as they appear in the body of the class. The first function in the fidelity zero class is __defaults__. This contains the primary functionality, as it sets the default settings and the methods that will be used to compute aerodynamics.

    + +

    The settings begin as below:

    + +
    # correction factors
    +settings = self.settings
    +settings.fuselage_lift_correction           = 1.14
    +settings.trim_drag_correction_factor        = 1.02
    +settings.wing_parasite_drag_form_factor     = 1.1
    +

    +

    self.settings is inherited from the base Markup class and therefore is not redefined. Instead, these values and several more are added. Items in this group control how the aerodynamic methods operate. Variables that are set to None typically mean that a method specific default will be used instead. For example, span efficiency controls whether or not a blanket span efficiency is used to override the drag output for the vortex lattice method.

    + +

    The next group builds the evaluation procedure. It is constructed as a set of processes which include a number of functions from the methods group. The Process class is essentially a container for all the functions added to it, and will evaluate those functions in the order they are added. Another process can also be added instead of a function, as is initially done with compute.drag.parasite. There is also a special type of process class called Process_Geometry, which will iterate through the vehicle geometry and apply the submethod to all components in the specified group. Altogether, this code block creates a process for lift and drag and sets up the analysis to run the relevant methods in the order shown (however they are not run as we step through this code block). self.process.compute is a process itself as well.

    + +
    # build the evaluation process
    +compute = self.process.compute
    +
    +compute.lift = Process()
    +
    +compute.lift.inviscid_wings                = Vortex_Lattice()
    +compute.lift.vortex                        = SUAVE.Methods.skip
    +compute.lift.fuselage                      = Common.Lift.fuselage_correction
    +compute.lift.total                         = Common.Lift.aircraft_total
    +
    +compute.drag = Process()
    +compute.drag.parasite                      = Process()
    +compute.drag.parasite.wings                = Process_Geometry('wings')
    +compute.drag.parasite.wings.wing           = Common.Drag.parasite_drag_wing 
    +compute.drag.parasite.fuselages            = Process_Geometry('fuselages')
    +compute.drag.parasite.fuselages.fuselage   = Common.Drag.parasite_drag_fuselage
    +compute.drag.parasite.propulsors           = Process_Geometry('propulsors')
    +

    + +

    The other function in this class is the initialize function. This allows a surrogate of the lift model to be built. A surrogate is often used here in order to avoid the time required to evaluate the vortex lattice every time the aerodynamic analysis is called.

    + +

    Changes for Supersonic Analysis

    +

    The next question is how to change this analysis class to allow for calculations in supersonic conditions. For this, we switch over to the Supersonic_Zero class and examine the differences. Generally, changes that are required are updates to the settings and changes in which methods are used. The primary settings additions that are needed for this analysis type are those that control the transonic drag rise and wave drag scaling.

    +
    # this multiplier is used to determine the volume wave drag at the peak Mach number
    +# by multiplying the volume wave drag at the end drag rise Mach number
    +settings.peak_mach_number                      = 1.04
    +settings.cross_sectional_area_calculation_type = 'Fixed'
    +# 'Fixed' means that the area is not able to vary with Mach number, so the number at the desired cruise condition should
    +# be used
    +# 'OpenVSP' is a desired future possibility. This would allow the cross sectional area to vary with Mach number, but is 
    +# much more computationally intensive.        
    +settings.volume_wave_drag_scaling    = 3.7 # 1.8-2.2 are given as typical for an SST, but 3.7 was found to be more accurate 
    +# This may be due to added propulsion effects
    +settings.fuselage_parasite_drag_begin_blend_mach = 0.91
    +settings.fuselage_parasite_drag_end_blend_mach   = 0.99
    +

    + +

    For the methods, a subset must be swapped. Two groups of methods are imported this time. The first is designated as Common, which is the same group as was used in Fidelity_Zero. The second is designated as Methods, and contains methods specific to the supersonic case. These new methods replace their subsonic-only variants. Once all of these methods have been replaced, the new analysis class is ready.

    + +

    In order for the new analysis class and any new methods created to function properly, they must also be added to the relevant __init__.py files that link together SUAVE as a library. This requires adding a line to trunk/Analyses/Aerodynamics/__init__.py:

    + +
    from .Supersonic_Zero              import Supersonic_Zero
    +

    + +

    and to trunk/Methods/Aerodynamics/__init__.py:

    + +
    from . import Supersonic_Zero

    + +

    New files must also be created for the supersonic methods folder structure, which can be found as trunk/Methods/Aerodynamics/Supersonic_Zero/__init__.py, trunk/Methods/Aerodynamics/Supersonic_Zero/Lift/__init__.py, and trunk/Methods/Aerodynamics/Supersonic_Zero/Lift/__init__.py.

    + +

    Once all of the files are ready, a couple of modifications are needed in the vehicle and analysis setup. These can be seen the tut_concorde.py tutorial file. First, to switch the analysis type used, we replace

    + +
    aerodynamics = SUAVE.Analyses.Aerodynamics.Fidelity_Zero()

    + +

    with

    + +
    aerodynamics = SUAVE.Analyses.Aerodynamics.Supersonic_Zero()

    + +

    Then, to use the special analysis capabilities, a couple settings are added to the main wing:

    + +
    wing.vortex_lift             = True
    +wing.high_mach               = True
    +

    + +

    This turns on the vortex lift correction at low speeds and changes the compressibility equations at high subsonic speeds to better match Concorde-type behavior.

    + +

    You can run the tut_concorde.py tutorial file to see the results of these changes. If you have any more questions on how to modify the aerodynamic analyses or any other types of analyses, please let us know on our forum.

    +
    +
    + +
    +
    +
    + + + + + + + + + + + + + + \ No newline at end of file diff --git a/tutorials/Files/eVTOL_tutorial.py b/tutorials/Files/eVTOL_tutorial.py new file mode 100644 index 00000000..61f1213b --- /dev/null +++ b/tutorials/Files/eVTOL_tutorial.py @@ -0,0 +1,592 @@ +# eVTOL_tutorial.py +# +# Created: Nov 2021, E. Botero +# + +# ---------------------------------------------------------------------------------------------------------------------- +# Imports +# ---------------------------------------------------------------------------------------------------------------------- + +# pacakgee imports +import SUAVE +import numpy as np + +# module imports +from SUAVE.Core import Units +from SUAVE.Attributes.Gases import Air +from SUAVE.Plots.Performance.Mission_Plots import * +from SUAVE.Input_Output.OpenVSP import write +from SUAVE.Methods.Geometry.Two_Dimensional.Planform import segment_properties, wing_segmented_planform, wing_planform +from SUAVE.Methods.Propulsion import propeller_design +from SUAVE.Methods.Propulsion.electric_motor_sizing import size_optimal_motor +from SUAVE.Methods.Power.Battery.Sizing import initialize_from_mass + + +from copy import deepcopy + +# ---------------------------------------------------------------------------------------------------------------------- +# Main +# ---------------------------------------------------------------------------------------------------------------------- + +def main(): + + # Setup a vehicle + vehicle = setup_vehicle() + + # export the vehicle + #write(vehicle, 'our_eVTOL') + + # Setup analyses + analyses = setup_analyses(vehicle) + analyses.finalize() #<- this builds surrogate models! + + # Setup a mission + mission = setup_mission(vehicle, analyses) + + # Evaluate the mission + results = mission.evaluate() + + # plot the mission + make_plots(results) + + return + + +# ---------------------------------------------------------------------------------------------------------------------- +# Vehicle +# ---------------------------------------------------------------------------------------------------------------------- + +def setup_vehicle(): + + # ------------------------------------------------------------------ + # Initialize the Vehicle + # ------------------------------------------------------------------ + + # Create a vehicle and set level properties + vehicle = SUAVE.Vehicle() + vehicle.tag = 'eVTOL' + + # ------------------------------------------------------------------ + # Vehicle-level Properties + # ------------------------------------------------------------------ + # mass properties + vehicle.mass_properties.takeoff = 2500. * Units.lb + vehicle.mass_properties.operating_empty = 2150. * Units.lb + vehicle.mass_properties.max_takeoff = 2500. * Units.lb + vehicle.mass_properties.max_payload = 100. * Units.lb + vehicle.mass_properties.center_of_gravity = [[2.0, 0. , 0. ]] # I made this up + + # basic parameters + vehicle.envelope.ultimate_load = 5.7 + vehicle.envelope.limit_load = 3. + + # ------------------------------------------------------------------ + # WINGS + # ------------------------------------------------------------------ + # WING PROPERTIES + wing = SUAVE.Components.Wings.Main_Wing() + wing.tag = 'main_wing' + wing.origin = [[1.5, 0., -0.5 ]] + wing.spans.projected = 35.0 * Units.feet + wing.chords.root = 3.25 * Units.feet + + # Segment + segment = SUAVE.Components.Wings.Segment() + segment.tag = 'Root' + segment.percent_span_location = 0. + segment.twist = 0. + segment.root_chord_percent = 1.5 + segment.dihedral_outboard = 1.0 * Units.degrees + segment.sweeps.quarter_chord = 8.5 * Units.degrees + segment.thickness_to_chord = 0.18 + wing.Segments.append(segment) + + # Segment + segment = SUAVE.Components.Wings.Segment() + segment.tag = 'Section_2' + segment.percent_span_location = 0.227 + segment.twist = 0. + segment.root_chord_percent = 1. + segment.dihedral_outboard = 1.0 * Units.degrees + segment.sweeps.quarter_chord = 0.0 * Units.degrees + segment.thickness_to_chord = 0.12 + wing.Segments.append(segment) + + # Segment + segment = SUAVE.Components.Wings.Segment() + segment.tag = 'Tip' + segment.percent_span_location = 1.0 + segment.twist = 0. + segment.root_chord_percent = 1.0 + segment.dihedral_outboard = 0.0 * Units.degrees + segment.sweeps.quarter_chord = 0.0 * Units.degrees + segment.thickness_to_chord = 0.12 + wing.Segments.append(segment) + + # Fill out more segment properties automatically + wing = segment_properties(wing) + wing = wing_segmented_planform(wing) + + + ## ALSO SET THE VEHICLE REFERENCE AREA + vehicle.reference_area = wing.areas.reference + + # add to vehicle + vehicle.append_component(wing) + + # Add a horizontal tail + # WING PROPERTIES + wing = SUAVE.Components.Wings.Horizontal_Tail() + wing.tag = 'horizontal_tail' + wing.areas.reference = 2.0 + wing.taper = 0.5 + wing.sweeps.quarter_chord = 20. * Units.degrees + wing.aspect_ratio = 5.0 + wing.thickness_to_chord = 0.12 + wing.dihedral = 5. * Units.degrees + wing.origin = [[5.5 , 0.0 , 0.65 ]] + + # Fill out more segment properties automatically + wing = wing_planform(wing) + + # add to vehicle + vehicle.append_component(wing) + + # Add a vertical tail + wing = SUAVE.Components.Wings.Vertical_Tail() + wing.tag = 'vertical_tail' + wing.areas.reference = 1.0 + wing.taper = 0.5 + wing.sweeps.quarter_chord = 30 * Units.degrees + wing.aspect_ratio = 2.5 + wing.thickness_to_chord = 0.12 + wing.origin = [[5.5 , 0.0 , 0.65 ]] + + # Fill out more segment properties automatically + wing = wing_planform(wing) + + # add to vehicle + vehicle.append_component(wing) + + # Add a fuseelage + + # --------------------------------------------------------------- + # FUSELAGE + # --------------------------------------------------------------- + # FUSELAGE PROPERTIES + fuselage = SUAVE.Components.Fuselages.Fuselage() + fuselage.tag = 'fuselage' + fuselage.seats_abreast = 2. + fuselage.fineness.nose = 0.88 + fuselage.fineness.tail = 1.13 + fuselage.lengths.nose = 3.2 * Units.feet + fuselage.lengths.tail = 6.4 * Units.feet + fuselage.lengths.cabin = 6.4 * Units.feet + fuselage.lengths.total = 6.0 + fuselage.width = 5.85 * Units.feet + fuselage.heights.maximum = 4.65 * Units.feet + fuselage.heights.at_quarter_length = 3.75 * Units.feet + fuselage.heights.at_wing_root_quarter_chord = 4.65 * Units.feet + fuselage.heights.at_three_quarters_length = 4.26 * Units.feet + fuselage.areas.wetted = 236. * Units.feet**2 + fuselage.areas.front_projected = 0.14 * Units.feet**2 + fuselage.effective_diameter = 5.85 * Units.feet + fuselage.differential_pressure = 0. + + # Segment + segment = SUAVE.Components.Lofted_Body_Segment.Segment() + segment.tag = 'segment_0' + segment.percent_x_location = 0. + segment.percent_z_location = -0.05 + segment.height = 0.1 + segment.width = 0.1 + fuselage.Segments.append(segment) + + # Segment + segment = SUAVE.Components.Lofted_Body_Segment.Segment() + segment.tag = 'segment_1' + segment.percent_x_location = 0.06 + segment.percent_z_location = -0.05 + segment.height = 0.52 + segment.width = 0.75 + fuselage.Segments.append(segment) + + # Segment + segment = SUAVE.Components.Lofted_Body_Segment.Segment() + segment.tag = 'segment_2' + segment.percent_x_location = 0.25 + segment.percent_z_location = -.01 + segment.height = 1.2 + segment.width = 1.43 + fuselage.Segments.append(segment) + + # Segment + segment = SUAVE.Components.Lofted_Body_Segment.Segment() + segment.tag = 'segment_3' + segment.percent_x_location = 0.475 + segment.percent_z_location = 0 + segment.height = 1.4 + segment.width = 1.4 + fuselage.Segments.append(segment) + + # Segment + segment = SUAVE.Components.Lofted_Body_Segment.Segment() + segment.tag = 'segment_4' + segment.percent_x_location = 0.75 + segment.percent_z_location = 0.06 + segment.height = 0.6 + segment.width = 0.4 + fuselage.Segments.append(segment) + + # Segment + segment = SUAVE.Components.Lofted_Body_Segment.Segment() + segment.tag = 'segment_5' + segment.percent_x_location = 1. + segment.percent_z_location = 0.1 + segment.height = 0.05 + segment.width = 0.05 + fuselage.Segments.append(segment) + + # add to vehicle + vehicle.append_component(fuselage) + + + #------------------------------------------------------------------- + # Booms + #------------------------------------------------------------------- + # Add booms for the motors + boom = SUAVE.Components.Fuselages.Fuselage() + boom.tag = 'boom_R' + boom.origin = [[0.525, 3.0, -0.35]] + boom.lengths.nose = 0.2 + boom.lengths.tail = 0.2 + boom.lengths.total = 4 + boom.width = 0.15 + boom.heights.maximum = 0.15 + boom.heights.at_quarter_length = 0.15 + boom.heights.at_three_quarters_length = 0.15 + boom.heights.at_wing_root_quarter_chord = 0.15 + boom.effective_diameter = 0.15 + boom.areas.wetted = 2*np.pi*(0.075)*3.5 + boom.areas.front_projected = np.pi*0.15 + boom.fineness.nose = 0.15/0.2 + boom.fineness.tail = 0.15/0.2 + + vehicle.append_component(boom) + + # Now attach the mirrored boom + other_boom = deepcopy(boom) + other_boom.origin[0][1] = -boom.origin[0][1] + other_boom.tag = 'boom_L' + vehicle.append_component(other_boom) + + + #------------------------------------------------------------------ + # Network + #------------------------------------------------------------------ + net = SUAVE.Components.Energy.Networks.Lift_Cruise() + net.number_of_lift_rotor_engines = 4 + net.number_of_propeller_engines = 1 + net.identical_propellers = True + net.identical_lift_rotors = True + net.voltage = 400. + + #------------------------------------------------------------------ + # Electronic Speed Controller + #------------------------------------------------------------------ + lift_rotor_esc = SUAVE.Components.Energy.Distributors.Electronic_Speed_Controller() + lift_rotor_esc.efficiency = 0.95 + net.lift_rotor_esc = lift_rotor_esc + + propeller_esc = SUAVE.Components.Energy.Distributors.Electronic_Speed_Controller() + propeller_esc.efficiency = 0.95 + net.propeller_esc = propeller_esc + + #------------------------------------------------------------------ + # Payload + #------------------------------------------------------------------ + payload = SUAVE.Components.Energy.Peripherals.Avionics() + payload.power_draw = 0. + net.payload = payload + + #------------------------------------------------------------------ + # Avionics + #------------------------------------------------------------------ + avionics = SUAVE.Components.Energy.Peripherals.Avionics() + avionics.power_draw = 300. * Units.watts + net.avionics = avionics + + #------------------------------------------------------------------ + # Design Battery + #------------------------------------------------------------------ + bat = SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion_LiNiMnCoO2_18650() + bat.mass_properties.mass = 1000. * Units.lb + bat.max_voltage = net.voltage + initialize_from_mass(bat) + net.battery = bat + + #------------------------------------------------------------------ + # Design Rotors and Propellers + #------------------------------------------------------------------ + + # The tractor propeller + propeller = SUAVE.Components.Energy.Converters.Propeller() + propeller.origin = [[0,0,-0.325]] + propeller.number_of_blades = 3 + propeller.tip_radius = 0.9 + propeller.hub_radius = 0.1 + propeller.angular_velocity = 2200 * Units.rpm + propeller.freestream_velocity = 100. * Units.knots + propeller.design_Cl = 0.7 + propeller.design_altitude = 5000. * Units.feet + propeller.design_thrust = 500. * Units.lbf + propeller.airfoil_geometry = ['./Airfoils/NACA_4412.txt'] + propeller.airfoil_polars = [['./Airfoils/Polars/NACA_4412_polar_Re_50000.txt' , + './Airfoils/Polars/NACA_4412_polar_Re_100000.txt' , + './Airfoils/Polars/NACA_4412_polar_Re_200000.txt' , + './Airfoils/Polars/NACA_4412_polar_Re_500000.txt' , + './Airfoils/Polars/NACA_4412_polar_Re_1000000.txt' ]] + propeller.airfoil_polar_stations = np.zeros((20),dtype=np.int8).tolist() + propeller = propeller_design(propeller) + net.propellers.append(propeller) + + # The lift rotors + lift_rotor = SUAVE.Components.Energy.Converters.Lift_Rotor() + lift_rotor.tip_radius = 1.5 + lift_rotor.hub_radius = 0.15 + lift_rotor.number_of_blades = 4 + lift_rotor.design_tip_mach = 0.65 + lift_rotor.freestream_velocity = 500. * Units['ft/min'] + lift_rotor.angular_velocity = lift_rotor.design_tip_mach* Air().compute_speed_of_sound()/lift_rotor.tip_radius + lift_rotor.design_Cl = 0.7 + lift_rotor.design_altitude = 3000. * Units.feet + lift_rotor.design_thrust = 2500*Units.lbf/4 + lift_rotor.variable_pitch = False + lift_rotor.airfoil_geometry = ['./Airfoils/NACA_4412.txt'] + lift_rotor.airfoil_polars = [['./Airfoils/Polars/NACA_4412_polar_Re_50000.txt' , + './Airfoils/Polars/NACA_4412_polar_Re_100000.txt' , + './Airfoils/Polars/NACA_4412_polar_Re_200000.txt' , + './Airfoils/Polars/NACA_4412_polar_Re_500000.txt' , + './Airfoils/Polars/NACA_4412_polar_Re_1000000.txt' ]] + + lift_rotor.airfoil_polar_stations = np.zeros((20),dtype=np.int8).tolist() + lift_rotor = propeller_design(lift_rotor) + + # Appending rotors with different origins + rotations = [1,-1,-1,1] + origins = [[0.6, 3., -0.125] ,[4.5, 3., -0.125], + [0.6, -3., -0.125] ,[4.5, -3., -0.125]] + + for ii in range(4): + lift_rotor = deepcopy(lift_rotor) + lift_rotor.tag = 'lift_rotor' + lift_rotor.rotation = rotations[ii] + lift_rotor.origin = [origins[ii]] + net.lift_rotors.append(lift_rotor) + + + + #------------------------------------------------------------------ + # Design Motors + #------------------------------------------------------------------ + # Propeller (Thrust) motor + propeller_motor = SUAVE.Components.Energy.Converters.Motor() + propeller_motor.efficiency = 0.95 + propeller_motor.nominal_voltage = bat.max_voltage + propeller_motor.mass_properties.mass = 2.0 * Units.kg + propeller_motor.origin = propeller.origin + propeller_motor.propeller_radius = propeller.tip_radius + propeller_motor.no_load_current = 2.0 + propeller_motor = size_optimal_motor(propeller_motor,propeller) + net.propeller_motors.append(propeller_motor) + + # Rotor (Lift) Motor + lift_rotor_motor = SUAVE.Components.Energy.Converters.Motor() + lift_rotor_motor.efficiency = 0.85 + lift_rotor_motor.nominal_voltage = bat.max_voltage*3/4 + lift_rotor_motor.mass_properties.mass = 3. * Units.kg + lift_rotor_motor.origin = lift_rotor.origin + lift_rotor_motor.propeller_radius = lift_rotor.tip_radius + lift_rotor_motor.gearbox_efficiency = 1.0 + lift_rotor_motor.no_load_current = 4.0 + lift_rotor_motor = size_optimal_motor(lift_rotor_motor,lift_rotor) + + for _ in range(4): + lift_rotor_motor = deepcopy(lift_rotor_motor) + lift_rotor_motor.tag = 'motor' + net.lift_rotor_motors.append(lift_rotor_motor) + + + vehicle.append_component(net) + + + # Now account for things that have been overlooked for now: + vehicle.excrescence_area = 0.1 + + return vehicle + + +# ---------------------------------------------------------------------------------------------------------------------- +# Analyses +# ---------------------------------------------------------------------------------------------------------------------- + + +def setup_analyses(vehicle): + # ------------------------------------------------------------------ + # Initialize the Analyses + # ------------------------------------------------------------------ + analyses = SUAVE.Analyses.Vehicle() + + # ------------------------------------------------------------------ + # Weights + weights = SUAVE.Analyses.Weights.Weights_eVTOL() + weights.vehicle = vehicle + analyses.append(weights) + + # ------------------------------------------------------------------ + # Aerodynamics Analysis + aerodynamics = SUAVE.Analyses.Aerodynamics.Fidelity_Zero() + aerodynamics.geometry = vehicle + aerodynamics.settings.drag_coefficient_increment = 0.4 * vehicle.excrescence_area/vehicle.reference_area + analyses.append(aerodynamics) + + # ------------------------------------------------------------------ + # Energy + energy= SUAVE.Analyses.Energy.Energy() + energy.network = vehicle.networks + analyses.append(energy) + + # ------------------------------------------------------------------ + # Noise Analysis + noise = SUAVE.Analyses.Noise.Fidelity_One() + noise.geometry = vehicle + analyses.append(noise) + + # ------------------------------------------------------------------ + # Planet Analysis + planet = SUAVE.Analyses.Planets.Planet() + analyses.append(planet) + + # ------------------------------------------------------------------ + # Atmosphere Analysis + atmosphere = SUAVE.Analyses.Atmospheric.US_Standard_1976() + atmosphere.features.planet = planet.features + analyses.append(atmosphere) + + return analyses + + +# ---------------------------------------------------------------------------------------------------------------------- +# Mission +# ---------------------------------------------------------------------------------------------------------------------- + +def setup_mission(vehicle,analyses): + + # ------------------------------------------------------------------ + # Initialize the Mission + # ------------------------------------------------------------------ + mission = SUAVE.Analyses.Mission.Sequential_Segments() + mission.tag = 'the_mission' + + # unpack Segments module + Segments = SUAVE.Analyses.Mission.Segments + + # base segment + base_segment = Segments.Segment() + base_segment.state.numerics.number_control_points = 8 + base_segment.process.initialize.initialize_battery = SUAVE.Methods.Missions.Segments.Common.Energy.initialize_battery + base_segment.process.iterate.conditions.planet_position = SUAVE.Methods.skip + base_segment.process.iterate.conditions.stability = SUAVE.Methods.skip + base_segment.process.finalize.post_process.stability = SUAVE.Methods.skip + ones_row = base_segment.state.ones_row + + # ------------------------------------------------------------------ + # Hover Climb Segment + # ------------------------------------------------------------------ + segment = Segments.Hover.Climb(base_segment) + segment.tag = "hover_climb" + segment.analyses.extend(analyses) + segment.altitude_start = 0.0 * Units.ft + segment.altitude_end = 100. * Units.ft + segment.climb_rate = 200. * Units['ft/min'] + segment.battery_energy = vehicle.networks.lift_cruise.battery.max_energy*0.95 + segment.process.iterate.unknowns.mission = SUAVE.Methods.skip + segment = vehicle.networks.lift_cruise.add_lift_unknowns_and_residuals_to_segment(segment) + + # add to misison + mission.append_segment(segment) + + # ------------------------------------------------------------------ + # Second Climb Segment: Constant Speed, Constant Rate + # ------------------------------------------------------------------ + segment = Segments.Climb.Constant_Speed_Constant_Rate(base_segment) + segment.tag = 'wing_climb' + segment.analyses.extend(analyses) + segment.air_speed = 70. * Units.knots + segment.altitude_end = 3000. * Units.ft + segment.climb_rate = 500. * Units['ft/min'] + segment = vehicle.networks.lift_cruise.add_cruise_unknowns_and_residuals_to_segment(segment) + + # add to misison + mission.append_segment(segment) + + # ------------------------------------------------------------------ + # Cruise + # ------------------------------------------------------------------ + segment = Segments.Cruise.Constant_Speed_Constant_Altitude(base_segment) + segment.tag = "Cruise" + segment.analyses.extend(analyses) + segment.distance = 50. * Units.nautical_miles + segment.air_speed = 100. * Units.knots + segment = vehicle.networks.lift_cruise.add_cruise_unknowns_and_residuals_to_segment(segment) + + # add to misison + mission.append_segment(segment) + + # ------------------------------------------------------------------ + # Descent + # ------------------------------------------------------------------ + segment = Segments.Descent.Constant_Speed_Constant_Rate(base_segment) + segment.tag = "wing_descent" + segment.analyses.extend(analyses) + segment.air_speed = 100. * Units.knots + segment.altitude_end = 100 * Units.ft + segment.descent_rate = 300. * Units['ft/min'] + segment = vehicle.networks.lift_cruise.add_cruise_unknowns_and_residuals_to_segment(segment) + + # add to misison + mission.append_segment(segment) + + # ------------------------------------------------------------------ + # Hover Descent + # ------------------------------------------------------------------ + segment = Segments.Hover.Descent(base_segment) + segment.tag = "hover_descent" + segment.analyses.extend(analyses) + segment.altitude_end = 0. + segment.descent_rate = 100 * Units['ft/min'] + segment.process.iterate.unknowns.mission = SUAVE.Methods.skip + segment = vehicle.networks.lift_cruise.add_lift_unknowns_and_residuals_to_segment(segment) + + # add to misison + mission.append_segment(segment) + + return mission + +# ---------------------------------------------------------------------------------------------------------------------- +# Plots +# ---------------------------------------------------------------------------------------------------------------------- + +def make_plots(results): + + plot_flight_conditions(results) + + plot_aerodynamic_coefficients(results) + + plot_battery_pack_conditions(results) + + plot_lift_cruise_network(results) + +if __name__ == '__main__': + main() + plt.show() \ No newline at end of file diff --git a/tutorials/PRD.html b/tutorials/PRD.html new file mode 100644 index 00000000..9195ab4e --- /dev/null +++ b/tutorials/PRD.html @@ -0,0 +1,166 @@ + + + + + Payload Range Diagram - SUAVE Tutorial + + + + + + + + + +
    + + + + + +
    +
    +
    + + + +
    +

    Embraer E-190 Payload Range Diagram Tutorial

    +

    1) Locate the tutorial script folder.

    + +

    2) Open the tut_payload_range.py script in your favorite editor or IDE.

    + +

    3) Similar to the B737-800 Tutorial, the setup is divided into steps.

    + +

    4) For the Payload Range Diagram, besides the vehicle and mission, the user must provide the following inputs:

    + +
      +
    • cruise_segment_tag: You must enter the tag of the segment which will have its length modified in order to comply with required fuel burn for each one of the payload range diagram points.
    • +
    • reserves: This will be considered as a fixed fuel reserve for all the diagram points.
    • +
    + +

    5) The tutorial presents the following definition:

    + +
    # run payload diagram	
    +cruise_segment_tag = "Cruise"
    +reserves = 1750.
    +payload_range_results = payload_range(vehicle,mission,cruise_segment_tag,reserves)
    +
    + +

    6) First, let’s just run it as it is for now. Run the script in either the IDE or in a terminal as

    python tut_payload_range.py

    + +

    7) After the calculations are completed, the payload diagram will be plotted and the data will be stored in a file named ‘PayloadRangeDiagram.dat’. This is located in the folder with the script that you just ran.

    + +

    8) You can try to modify vehicle and/or mission parameters and see how the payload range diagram is affected. For now, let’s add some drag counts to the airplane:

    + +
      +
    • Locate
      base_analysis()
      and then the Aerodynamics Analysis text block (line 114)
    • +
    • Add 50 drag counts to the vehicle (line 116):
      aerodynamics.settings.drag_coefficient_increment = 0.0050 
    • +
    • Rerun the script as before and notice the changes in the results.
    • +
    + +

    9) Similarly the mission parameters can be changed. Again, this lets the user decide what changes they want to explore.

    + +
    + + +
    + +
    +
    +
    + + + + + + + + + + + + + + \ No newline at end of file diff --git a/tutorials/Solar.html b/tutorials/Solar.html new file mode 100644 index 00000000..7ec6d769 --- /dev/null +++ b/tutorials/Solar.html @@ -0,0 +1,260 @@ + + + + + Solar UAV - SUAVE Tutorial + + + + + + + + + +
    + + + + + +
    +
    +
    + + + +
    + +

    Introduction

    + +

    The purpose of this tutorial is to educate users on how to setup a preconfigured solar energy network to work with a high altitude solar UAV. In this tutorial it is assumed that the user has some familiarity with SUAVE having completed the fundamental tutorial for the Boeing 737-800. You will learn about setting up the following:

    + +
      +
    • Solar missions,
    • +
    • Human powered/solar weight estimation,
    • +
    • Boundary layer transition,
    • +
    • Solar panels,
    • +
    • Batteries,
    • +
    • Electric motors,
    • +
    • Propellers,
    • +
    • Electric network integration in a solar UAV
    • +
    + +

    Because of the flexible nature of SUAVE, the approach shown is just one way to setup the UAV for analysis. By experimenting and eventually developing your own code you will be able to do far more than what is shown in this tutorial. The original script can be found in the tutorial repository as tut_solar_uav.py.

    + +

    Vehicle and Mission

    + +

    The vehicle is similar to the Qinetiq Zephyr but far larger at 40 meters in wing span and a weight of 200 kg. However, it does carry double the payload of the Zephyr at 5 kg and accounts for constant payload power usage. The battery energy density is set to an optimistic estimate of 450 Watt-hours per kg. Additionally, 90 percent of the wings are covered with solar panels that have a 25 percent efficiency.

    + +

    This mission exercises the methods developed for solar radiation estimation, propeller and motor integration, as well as the human powered aircraft weight estimation. The mission setup is a constant altitude cruise at 15 km at Mach 0.12 for about 24 hours. The location is over the California Bay Area during the summer solstice.

    + +

    Setup

    + +

    This tutorial highlights the differences between setting up a typical commercial aircraft like a Boeing 737 and a solar UAV.

    + +

    Mission Setup

    + +

    For a solar UAV, the starting location as well as the day and time are critical. So the first segment must be modified to include this information. It is important to note that the start times provided are in “Zulu” time or Greenwich Mean Time. This is typical for aircraft navigation to prevent time zone errors and ambiguity.

    + +
    segment.state.numerics.number_control_points = 64
    +segment.start_time                           = time.strptime("Tue, Jun 21 11:30:00  2020", "%a, %b %d %H:%M:%S %Y",)
    +segment.altitude                             = 15.0  * Units.km 
    +segment.mach                                 = 0.12
    +segment.distance                             = 3050.0 * Units.km
    +segment.battery_energy                       = vehicle.propulsors.solar.battery.max_energy*0.2 #Charge the battery to start
    +segment.latitude                             = 37.4300   # this defaults to degrees (do not use Units.degrees)
    +segment.longitude                            = -122.1700 # this defaults to degrees
    +
    + +

    Additionally, this mission is highly simplified. It consists of only one mission segment. To provide ample resolution, the number of control points has been increased to 64.

    + +

    Structural Weight Sizing

    + +

    The vehicle sizing of the human powered aircraft or solar UAV requires the dimensions of the vehicle like in other weight estimation methods. However, it also requires information about the number of wing ribs and the number of end ribs. The end ribs are relevant for wing designs where the sections can come apart for transportation.

    + +
    wing.number_ribs             = 26.
    +wing.number_end_ribs         = 2.
    +
    + +

    Wing Boundary Layer Transition

    + +

    The transition location of the boundary layer can have a great impact on the drag of the wing. This is especially important in properly designed, low Reynolds number flows, where laminar flow can be extended for larger regions of the surface. The code snippet below is how surfaces have transition points set. These are estimates provided from the designer based on experience.

    + +
    wing.transition_x_upper      = 0.6
    +wing.transition_x_lower      = 1.0
    +
    + +

    Solar Panels

    + +

    The solar panel model is quite simple and only requires a capture area, an efficiency, and mass. In this case we assume that 90% of the wing area is covered in solar panels.

    + +
    panel.area                 = vehicle.reference_area * 0.9
    +panel.efficiency           = 0.25
    +panel.mass_properties.mass = panel.area*(0.60 * Units.kg)
    +
    + +

    Batteries

    + +

    The batteries are set up with knowledge of the mass of the battery and the specific energy. In this case a futuristic specific energy of 600 Watt-hr/kg is set for lithium ion type batteries. The resistance of the batteries is another important input to determine charging and discharging losses.

    + +
    bat = SUAVE.Components.Energy.Storages.Batteries.Constant_Mass.Lithium_Ion()
    +bat.mass_properties.mass = 90.0 * Units.kg
    +bat.specific_energy      = 800. * Units.Wh/Units.kg
    +bat.resistance           = 0.05
    +bat.max_voltage          = 45.0
    +initialize_from_mass(bat,bat.mass_properties.mass)
    +net.battery              = bat
    +
    + +

    Propeller

    + +

    To setup the propeller we will actually design an optimized propeller. This is done through the methods provided by Adkins and Liebeck. The attributes of the propeller design are then seeded to the motor and network to accelerate convergence of the propeller and motor models.

    + +
    prop = SUAVE.Components.Energy.Converters.Propeller()
    +prop.number_blades       = 2.0
    +prop.freestream_velocity = 40.0 * Units['m/s']# freestream
    +prop.angular_velocity    = 150. * Units['rpm']
    +prop.tip_radius          = 4.25 * Units.meters
    +prop.hub_radius          = 0.05 * Units.meters
    +prop.design_Cl           = 0.7
    +prop.design_altitude     = 14.0 * Units.km
    +prop.design_thrust       = None
    +prop.design_power        = 3500.0 * Units.watts
    +prop                     = propeller_design(prop)
    +
    +net.propeller            = prop
    +
    + +

    Motor

    + +

    This motor model relies on data that is generally available from motor manufacturers. This includes the resistance, no load current, and the speed constant. Additionally, any gearbox is specified here and basic information about the propeller is entered here to help inform the solver when converging the motor and propeller analyses.

    + +
    motor = SUAVE.Components.Energy.Converters.Motor()
    +motor.resistance           = 0.008
    +motor.no_load_current      = 4.5  * Units.ampere
    +motor.speed_constant       = 120. * Units['rpm'] # RPM/volt converted to (rad/s)/volt    
    +motor.propeller_radius     = prop.tip_radius
    +motor.propeller_Cp         = prop.power_coefficient
    +motor.gear_ratio           = 12. # Gear ratio
    +motor.gearbox_efficiency   = .98 # Gear box efficiency
    +motor.expected_current     = 160. # Expected current
    +motor.mass_properties.mass = 2.0  * Units.kg
    +net.motor                  = motor    
    +
    + +

    Running

    + +

    As you should be familiar with by now, running this script is just like any other.

    +
    python tut_solar_uav.py
    +
    + +

    Results

    + +

    If all went well the script ran and it provided you with more plots than you ever wanted. Here are some of the plots that were generated when we ran it:

    + +

    solar_flux

    + + +
    +
    + +
    +
    +
    + + + + + + + + + + + + + + \ No newline at end of file diff --git a/tutorials/avl.html b/tutorials/avl.html new file mode 100644 index 00000000..f3eb1dcb --- /dev/null +++ b/tutorials/avl.html @@ -0,0 +1,218 @@ + + + + + Boeing 737-800 with AVL - SUAVE Tutorial + + + + + + + + + +
    + + + + + +
    +
    +
    + + + +
    +

    Boeing 737 Using AVL

    + +

    SUAVE was built upon the philosophy of creating a conceptualizing space that enables the user to have maximum design, +analysis and optimization flexibility. In SUAVE, the aerodynamics and stability module is set up to permit multiple fidelity +levels of analysis. The addition of Athena Vortex Lattice (AVL), a vortex lattice method (VLM) code developed by Professor +Mark Drela at MIT, extends SUAVE aerodynamic and stability analysis of aircraft configurations whose geometry have prior +posed difficulty in obtaining accurate results. Examples include oblique wings, joined wings, canard configurations and +blended-wing-bodies (BWB). For this example we use the Boeing 737-800 used in the Boeing 737-800 Tutorial.

    + +

    Downloading AVL

    +

    The tutorial assumes that AVL is available on your machine and can be called using just “avl” in the command line. AVL can be downloaded here for all platforms.

    + +

    Steps to simulate the aircraft’s performance over a mission

    +
      +
    1. Locate the folder where you have the tutorial repository. If using the command line, cd to this directory.
    2. +
    3. Open the tut_mission_B737_AVL.py script in your favorite editor or IDE. The script is setup to run the B737 on its design +mission. Run it in your IDE. If using the command line use the command.
    4. +
    + +
     python tut_mission_B737_800_AVL.py  
    + +

    It is very simple to interchange analysis tools in SUAVE. AVL is no exception. To study an aircraft in SUAVE using AVL, simply change the two lines in the analysis_set up shown below from Fidelity_Zero (SUAVE’s first order approximation method) to AVL.

    + +

    Replace line 109

    +
     aerodynamics = SUAVE.Analyses.Aerodynamics.Fidelity_Zero() 
    +

    with

    +
      aerodynamics = SUAVE.Analyses.Aerodynamics.AVL() 
    + +

    SUAVE launches AVL from the command line, runs analyses and then reads in the files. This process is done automatically. All +subroutines described later in this tutorial are done in the background. Since running a full stability analysis at each +point in the mission can be extremely expensive, a surrogate model is built for the aerodynamic coefficients, stability +derivatives, and neutral point locations by running through a set of representative angles of attack and mach numbers.

    + +
      +
    1. A few plots depicting the variation of the different aircraft performance parameters over the course of the mission are shown.
    2. +
    + +

    Important Functions:

    +

    The important functions used in this tutorial are exactly the same as the ones used in the Boeing Boeing 737-800 Analysis +Tutorial. Refer to this section in this tutorial here.

    +

    Subroutines Unique to SUAVE-AVL

    +

    Excluding the functions tut_mission_B737_AVL.py script, all of the subroutine python scripts described below are located +in the SUAVE/Methods/Aerodynamics/AVL repository.

    +

    Geometry Creation - Wing

    +

    Parameters defining the aircraft geometry in the in the vehicle_setup() are translated to an AVL file format using embedded +subroutines. Shown below is an example of the translation of the wing geometry from the vehicle-setup() function to AVL file +format.

    +
      +
    1. Firstly, if the wing defined by segments, a data structure is created to store the geometry parameters (chord length,twist,span location) of the beginning and end of each segment. For example the 737-800 wing below will be divided into three segments - yehudi, inboard and outboard wing).
    2. +
    3. Secondly, if control surfaces are defined either the full wing or its segments, the data structure created in step 1 is +further divided into sections at instances where the control surfaces begin and end. This is shown images below.
    4. +
    + +

    + +

    The above steps describing wing geometry parameterization are found in create_avl_datasturcture.py script. Along with +the creation of wing geometry, the SAUVE-AVL wrapper allows the user to refine the accuracy of the analysis by modifying the +vortex spacing placed on the wings. The number of chordwise/spanwise horseshoe vertices can also be modified. This is located in the Analyses/Aerodynamics/AVL_Inviscid.py (for Aerodynamics) and Analyses/Stability/AVL.py (for Stability) scripts below.

    +
      aerodynamics.settings.number_spanwise_vortices  = 5
    +
    + +

    Geometry Creation - Fuselage

    +

    Despite AVL having the capability of modelling bodies, a decision was made to model the fuselage as a wake-producing, lifting surface. The entire body is defined by a series of vertical and horizontal chords that create a cross when viewed from the front.

    + +

    Defining Flight Conditions

    +

    This is done in the translate_data.py script which translates flight conditions parameters defined in the +mission_setup() to an AVL data structure to be used in run cases. This script also stores AVL results into SUAVE’s +results data structures.

    +

    Writing Run Cases

    +

    Uses information in the AVL run case data structure created in translate_data.py to write an AVL format run case to be +used by the AVL executable. This is done in write_run_cases.py script.

    +

    Writing Commend Instructions for AVL executable

    +

    This is a sequence of commands used to load AVL files into the executable, perform aerodynamic and stability analyses, and +save results. This is done in write_input_deck.py script.

    +

    Reading Results

    +

    Opens saved AVL result files and stores data in a data structure used to create aerodynamic and stability surrogate models. +This is done in read_results.py script.

    + +

    Results

    +

    The plots shown below should be generated if the mission analysis executes correctly. The results show the aerodynamic, propulsion and mission properties of the B737-800 for the defined mission.

    + +

    B737 mission

    + +

    B737 Aerodynamics

    + +

    B737 Propulsion

    + +

    B737 Drag

    + +
    +
    + +
    +
    +
    + + + + + + + + + + + + + + diff --git a/tutorials/basic_eVTOL.html b/tutorials/basic_eVTOL.html new file mode 100644 index 00000000..8a3c95d2 --- /dev/null +++ b/tutorials/basic_eVTOL.html @@ -0,0 +1,143 @@ + + + + + Basic eVTOL- SUAVE Tutorial + + + + + + + + + + +
    + + + + + +
    +
    +
    + + + +
    +
    +

    Basic eVTOL Analysis

    +
    + +

    This video shows one way to setup an eVTOL aircraft for basic analysis. This configuration was chosen to be dissimilar to existing eVTOL models, yet be able to highlight how to use SUAVE.

    + +
    + + + + +
    + +
    +
    + +
    +
    +
    + + + + + + + + + + + + + + \ No newline at end of file diff --git a/tutorials/bwb.html b/tutorials/bwb.html new file mode 100644 index 00000000..31680c3b --- /dev/null +++ b/tutorials/bwb.html @@ -0,0 +1,350 @@ + + + + + Blended Wing Body with CFD - SUAVE Tutorial + + + + + + + + + +
    + + + + + +
    +
    +
    + + + +
    +

    Blended Wing Body using CFD

    + +

    The purpose of this tutorial is to show the analysis settings used to generate geometry, a mesh, and run CFD via SU2 from SUAVE. It will also show how to add individual wing segments. We assume you are familiar with SUAVE and have some CFD experience already. For this example we use a Blended Wing Body (BWB). The BWB used here is similar to the Boeing BWB-450 by Liebeck.

    + +

    Other Software You need

    + +

    For the full tool chain 3 additional pieces of software are needed. These are OpenVSP, Gmsh, and SU2. These are all open source and freely available online.

    + +

    First, you will need OpenVSP compiled with Python support. Unfortunately, you cannot use the precompiled binary versions of OpenVSP. You must compile it from scratch. This tutorial was tested with version 3.15.0.

    + +

    Second, you must install Gmsh. In this case you can use the precompiled binaries. Make sure to add Gmsh to your command line path so it can be called from the terminal. This tutorial was tested with version 3.0.6.

    + +

    Finally, you need to install SU2. If you want parallel support then you must also compile the code. Otherwise, you can use the precompiled versions. This tutorial was tested with version 6.0.0.

    + +

    Vehicle Setup

    + +

    Here we see how to construct multi-segment wings. With multiple segments we can build more complex shapes such as cranks, yehudis, and winglets. We also show how to specify an airfoil on the wing or on a wing segment. If an airfoil is not specified, it will default to a symmertic airfoil.

    + +

    This BWB is broken down into 7 segments. We first specify the top level parameters of the wing and then add each segment sequentially as shown below. This is also done for the tip section.

    + +
    
    +
    +
    +    # ------------------------------------------------------------------        
    +    #   Main Wing
    +    # ------------------------------------------------------------------        
    +
    +    wing = SUAVE.Components.Wings.Main_Wing()
    +    wing.tag = 'main_wing'
    +
    +    wing.aspect_ratio            = 289.**2 / (7840. * 2)
    +    wing.thickness_to_chord      = 0.15
    +    wing.taper                   = 0.0138
    +    wing.span_efficiency         = 0.95
    +    wing.spans.projected         = 289.0 * Units.feet    
    +    wing.chords.root             = 145.0 * Units.feet
    +    wing.chords.tip              = 3.5   * Units.feet
    +    wing.chords.mean_aerodynamic = 80. * Units.feet
    +    wing.areas.reference         = 7840. * 2 * Units.feet**2
    +    wing.sweeps.quarter_chord    = 33. * Units.degrees
    +    wing.twists.root             = 0.0 * Units.degrees
    +    wing.twists.tip              = 0.0 * Units.degrees
    +    wing.dihedral                = 2.5 * Units.degrees
    +    wing.origin                  = [[0.,0.,0]]
    +    wing.aerodynamic_center      = [0,0,0] 
    +    wing.vertical                = False
    +    wing.symmetric               = True
    +    wing.high_lift               = True
    +    wing.dynamic_pressure_ratio  = 1.0
    +
    +    segment = SUAVE.Components.Wings.Segment()
    +    segment.tag                   = 'section_1'
    +    segment.percent_span_location = 0.0
    +    segment.twist                 = 0. * Units.deg
    +    segment.root_chord_percent    = 1.
    +    segment.dihedral_outboard     = 0. * Units.degrees
    +    segment.sweeps.quarter_chord  = 40.0 * Units.degrees
    +    segment.thickness_to_chord    = 0.165 
    +    wing.Segments.append(segment)    
    +    
    +    segment = SUAVE.Components.Wings.Segment()
    +    segment.tag                   = 'section_2'
    +    segment.percent_span_location = 0.052
    +    segment.twist                 = 0. * Units.deg
    +    segment.root_chord_percent    = 0.921
    +    segment.dihedral_outboard     = 0.   * Units.degrees
    +    segment.sweeps.quarter_chord  = 52.5 * Units.degrees
    +    segment.thickness_to_chord    = 0.167    
    +    wing.Segments.append(segment)   
    +
    +    segment = SUAVE.Components.Wings.Segment()
    +    segment.tag                   = 'section_3'
    +    segment.percent_span_location = 0.138
    +    segment.twist                 = 0. * Units.deg
    +    segment.root_chord_percent    = 0.76
    +    segment.dihedral_outboard     = 1.85 * Units.degrees
    +    segment.sweeps.quarter_chord  = 36.9 * Units.degrees  
    +    segment.thickness_to_chord    = 0.171    
    +    wing.Segments.append(segment)   
    +    
    +    segment = SUAVE.Components.Wings.Segment()
    +    segment.tag                   = 'section_4'
    +    segment.percent_span_location = 0.221
    +    segment.twist                 = 0. * Units.deg
    +    segment.root_chord_percent    = 0.624
    +    segment.dihedral_outboard     = 1.85 * Units.degrees
    +    segment.sweeps.quarter_chord  = 30.4 * Units.degrees    
    +    segment.thickness_to_chord    = 0.175
    +    wing.Segments.append(segment)       
    +    
    +    segment = SUAVE.Components.Wings.Segment()
    +    segment.tag                   = 'section_5'
    +    segment.percent_span_location = 0.457
    +    segment.twist                 = 0. * Units.deg
    +    segment.root_chord_percent    = 0.313
    +    segment.dihedral_outboard     = 1.85  * Units.degrees
    +    segment.sweeps.quarter_chord  = 30.85 * Units.degrees
    +    segment.thickness_to_chord    = 0.118
    +    wing.Segments.append(segment)       
    +    
    +    segment = SUAVE.Components.Wings.Segment()
    +    segment.tag                   = 'section_6'
    +    segment.percent_span_location = 0.568
    +    segment.twist                 = 0. * Units.deg
    +    segment.root_chord_percent    = 0.197
    +    segment.dihedral_outboard     = 1.85 * Units.degrees
    +    segment.sweeps.quarter_chord  = 34.3 * Units.degrees
    +    segment.thickness_to_chord    = 0.10
    +    wing.Segments.append(segment)     
    +    
    +    segment = SUAVE.Components.Wings.Segment()
    +    segment.tag                   = 'section_7'
    +    segment.percent_span_location = 0.97
    +    segment.twist                 = 0. * Units.deg
    +    segment.root_chord_percent    = 0.086
    +    segment.dihedral_outboard     = 73. * Units.degrees
    +    segment.sweeps.quarter_chord  = 55. * Units.degrees
    +    segment.thickness_to_chord    = 0.10
    +    wing.Segments.append(segment)      
    +	
    +	segment = SUAVE.Components.Wings.Segment()
    +    segment.tag                   = 'tip'
    +    segment.percent_span_location = 1
    +    segment.twist                 = 0. * Units.deg
    +    segment.root_chord_percent    = 0.0241
    +    segment.dihedral_outboard     = 0. * Units.degrees
    +    segment.sweeps.quarter_chord  = 0. * Units.degrees
    +    segment.thickness_to_chord    = 0.10
    +    wing.Segments.append(segment)  
    +	
    +	# add to vehicle
    +    vehicle.append_component(wing)
    +
    +
    + +

    Once we build the vehicle we can write the OpenVSP file. If there are multiple configurations then you will need multiple writes to OpenVSP. We highly suggest you only have one configuration when possible to minimize computational costs..

    + +
    
    +# ----------------------------------------------------------------------
    +#   Define the Configurations
    +# ---------------------------------------------------------------------
    +
    +def configs_setup(vehicle):
    +
    +    # ------------------------------------------------------------------
    +    #   Initialize Configurations
    +    # ------------------------------------------------------------------
    +
    +    configs = SUAVE.Components.Configs.Config.Container()
    +
    +    base_config = SUAVE.Components.Configs.Config(vehicle)
    +    base_config.tag = 'base'
    +    configs.append(base_config)
    +    
    +    write(vehicle,base_config.tag) 
    +
    +    return configs
    +
    +
    + +

    Analyses Setup

    + +

    Here we setup the SU2 analysis. We commented out the parallel setting but you may use these if you want to parallelize the computation.

    + +

    The next setting which is commented out is the input file for pregenerated CFD data. We have included an example of this, so even if you don’t have SU2 and Gmsh installed you can still run this file to generate the surrogate and run the mission. A 10 iteration limit is used so that the tutorial can be run in a reasonable amount of time (~15 min). Data for runs with the 10 iteration limit and 1500 iteration limit are provided.

    + +

    After that we specify the points we want to use to generate the SU2-based lift surrogate. SUAVE has default values for these, but we suggest the user specify their own Mach numbers and angles of attack.

    + +

    Next we set up a bit of mesh refinement by modifying the source parameters at specific segments. Here we reduce the source length in the root area which refines the mesh there. This is optional as sources will also be added by default if these options are not specified.

    + +
    
    +
    +    # ------------------------------------------------------------------
    +    #  Aerodynamics Analysis
    +    aerodynamics = SUAVE.Analyses.Aerodynamics.SU2_Euler()
    +    aerodynamics.geometry = vehicle
    +    
    +    #aerodynamics.process.compute.lift.inviscid.settings.parallel   = True
    +    #aerodynamics.process.compute.lift.inviscid.settings.processors = 12  
    +    #aerodynamics.process.compute.lift.inviscid.training_file       = 'base_data_1500.txt'
    +    aerodynamics.process.compute.lift.inviscid.settings.maximum_iterations = 10
    +    
    +	aerodynamics.settings.drag_coefficient_increment = 0.0000
    +	aerodynamics.settings.half_mesh_flag             = False
    +    aerodynamics.settings.span_efficiency            = 0.85
    +    
    +    aerodynamics.process.compute.lift.inviscid.training.Mach             = np.array([.3, .5, .7, .85]) 
    +    aerodynamics.process.compute.lift.inviscid.training.angle_of_attack  = np.array([0.,3.,6.]) * Units.deg    
    +    
    +    wing_segments = vehicle.wings.main_wing.Segments
    +    wing_segments.section_1.vsp_mesh = Data()
    +    wing_segments.section_1.vsp_mesh.inner_radius  = 4.
    +    wing_segments.section_1.vsp_mesh.outer_radius  = 4.
    +    wing_segments.section_1.vsp_mesh.inner_length  = .14
    +    wing_segments.section_1.vsp_mesh.outer_length  = .14
    +    
    +    wing_segments.section_2.vsp_mesh = Data()
    +    wing_segments.section_2.vsp_mesh.inner_radius  = 4.
    +    wing_segments.section_2.vsp_mesh.outer_radius  = 4.
    +    wing_segments.section_2.vsp_mesh.inner_length  = .14
    +    wing_segments.section_2.vsp_mesh.outer_length  = .14
    +    
    +    wing_segments.section_3.vsp_mesh = Data()
    +    wing_segments.section_3.vsp_mesh.inner_radius  = 4.
    +    wing_segments.section_3.vsp_mesh.outer_radius  = 4.
    +    wing_segments.section_3.vsp_mesh.inner_length  = .14
    +    wing_segments.section_3.vsp_mesh.outer_length  = .14
    +    
    +    wing_segments.section_4.vsp_mesh = Data()
    +    wing_segments.section_4.vsp_mesh.inner_radius  = 4.
    +    wing_segments.section_4.vsp_mesh.outer_radius  = 2.8
    +    wing_segments.section_4.vsp_mesh.inner_length  = .14
    +    wing_segments.section_4.vsp_mesh.outer_length  = .14      
    +    
    +    analyses.append(aerodynamics)
    +
    +
    +
    + +

    The rest of the code runs as usual. However, we add in an extra plot which shows the surrogate and the points that were used to build it.

    + +
    +
    + +
    +
    +
    + + + + + + + + + + + + + + diff --git a/tutorials/general_aviation.html b/tutorials/general_aviation.html new file mode 100644 index 00000000..6643e359 --- /dev/null +++ b/tutorials/general_aviation.html @@ -0,0 +1,143 @@ + + + + + Basic eVTOL- SUAVE Tutorial + + + + + + + + + + +
    + + + + + +
    +
    +
    + + + +
    +
    +

    General Aviation Analysis

    +
    + +

    This video shows one way to setup a GA aircraft for basic analysis.

    + +
    + + + + +
    + +
    +
    + +
    +
    +
    + + + + + + + + + + + + + + \ No newline at end of file diff --git a/tutorials/jet_optimization.html b/tutorials/jet_optimization.html new file mode 100644 index 00000000..4edc8e24 --- /dev/null +++ b/tutorials/jet_optimization.html @@ -0,0 +1,269 @@ + + + + + Regional Jet Optimization - SUAVE Tutorial + + + + + + + + + +
    + + + + + +
    +
    +
    + + + +
    +

    Regional Jet Optimization Tutorial

    +

    This tutorial assumes familiarity with SUAVE and knowledge of the information in the Boeing 737-800 analysis tutorial. It provides a specific case of the more general optimization capabilities in SUAVE, and provides more information on how to modify the code for different uses.

    + +

    Some important files for the optimization problem can be seen below

    + +

    Important Files :

    + +

    Optimize.py:

    +

    Defines the optimization framework of the problem, wherein one minimizes an assigned objective, subject to certain constraints, by altering some design variables.

    + +

    In order to ensure that the subfunctions can communicate with eachother, and that SUAVE can communicate with the external optimizer, a special data object called the “Nexus” is used. The nexus object contains all of the vehicles, missions, results, and other important information. It alters these values at each optimizer iteration, depending on the input parameters defined in Optimize.py.

    + +

    In this particular setup, there are two design variables: wing area and cruise altitude. The objective is to minimize fuel burn, and there is only one constraint: fuel margin. The default inputs are defined in the following lines.

    + +
    
    +    #   [ tag                   , initial,     (lb , ub)        , scaling , units ]
    +    problem.inputs = np.array([
    +	[ 'wing_area'           ,  80    , (   50. ,   130.   ) ,   100.  , Units.meter**2],
    +	[ 'cruise_altitude'     ,   8    , (    6. ,    12.   ) ,   10.   , Units.km],
    +    ])
    +
    +
    +
    + +

    Each input parameter takes in 5 values; a tag (an identification to communicate between the optimizer and SUAVE), an initial value, set of bounds, a scale factor (many optimizers tend to be more effective when the input values are of order 1), as well as the units used.

    + +

    The objective and constraints are defined in the lines below.

    + +
    
    +	# [ tag, scaling, units ]
    +	problem.objective = np.array([
    +		[ 'fuel_burn', 10000, Units.kg ]
    +	])
    +	
    +	# [ tag, sense, edge, scaling, units ]
    +	problem.constraints = np.array([
    +		[ 'design_range_fuel_margin' , '>', 0., 1E-1, Units.less],
    +	])
    +	
    +
    + +

    Note that in this case, only a single constraint is used. Multiple constraints may be used using a list format, similar to the input variables.

    + +

    This file also defines the “aliasing,” i.e. how the design variables, constraints, and objective map to the variables used in Procedure.py (which is where the problem is evaluated). The aliases for this problem are defined in the lines below. Note that the first entry refers to the tag defined in either problem.inputs, problem.objective, or problem.constraints.

    + +
    
    +	problem.aliases = [
    +		[ 'wing_area'                        ,   ['vehicle_configurations.*.wings.main_wing.areas.reference',
    +							  'vehicle_configurations.*.reference_area'                    ]],  
    +		[ 'cruise_altitude'                  ,    'missions.base.segments.climb_5.altitude_end'                 ],
    +		[ 'fuel_burn'                        ,    'summary.base_mission_fuelburn'                               ],
    +		[ 'design_range_fuel_margin'         ,    'summary.max_zero_fuel_margin'                                ],
    +	]    
    +
    + +

    Note that, sometimes, a single input can map to multiple outputs, such as the “wing_area” design variable; in this case, use a list for the outputs, as seen above. The use of a wild card “*”, can also allow values to map to multiple outputs. Values to be outputted cannot contain wild cards as that would be ambiguous to an optimizer.

    + +

    Procedure.py:

    +

    This links everything together by defining the steps you would use to size and analyze the aircraft at each optimizer iteration.

    + +

    This file contains a number of subfunctions to alter the vehicle and mission. The function setup() instantiates the procedure, defining the functions that are called at each step of the optimizer in their order of execution.

    + +
      +
    1. +

      simple_sizing() defines the geometry of the aircraft based on the input parameters (in this case, wing area and cruise altitude).

      +
    2. +
    3. +

      weights() determines the weight breakdown of the aircraft

      +
    4. +
    5. +

      mission() decides which missions are run at each step, as well as the design mission of the aircraft

      +
    6. +
    7. +

      post_process() handles the results from the missions, saving the constraints and objective value

      +
    8. +
    + +

    Each step of the procedure takes the nexus object as an input, and returns the object as an output, ensuring that the data is available for handling.

    + +

    Vehicles.py:

    +

    Initializes the vehicle (or vehicles if desired) used in the optimization problem. This includes two subfunctions: base_setup(), where the vehicle structure is itself defined, including the fuselage, wing, vertical and horizontal tails, and the propulsion system.

    + +

    configs_setup() takes in the vehicle that was defined in base_setup() and defines other configurations (such as takeoff and landing, which include different flap settings). This may be used to define other parameters, such as changing the sweep angle of a variable-sweep-wing at higher Mach Numbers, or changing a propulsion component.

    + +

    Missions.py:

    +

    Initializes the missions that are run at each iteration. In this case, only a single mission is run.

    + +

    Analyses.py:

    +

    Defines the set of features that are used in this particular problem (e.g. weights correlations, aerodynamics correlations, etc.).

    + +

    Plot_Mission.py:

    +

    Plots the mission outputs.

    + +

    Running the Problem:

    +
      +
    1. +

      Locate the tutorial script folder “Regional_Jet_Optimization.”

      +
    2. +
    3. +

      Open the Optimize.py script in a text editor or IDE. You will see this line near the top of main():

      + +

      output = problem.objective()

      +
    4. +
    5. +

      This runs the problem with the default inputs. Run the file using an IDE or type python Optimize.py in the command line. You should see a set of output plots.

      +
    6. +
    + +

    Running a Sweep of the Inputs

    +

    Now try running a 2D sweep of the problem to observe the shape of the design space: comment output = problem.objective then uncomment the following (the next line down in the code).

    + +
    
    +	variable_sweep(problem)
    +
    + +

    Then run the program again. This could take a few minutes. The results should look like the plot below.

    + +

    2D Sweep

    + +

    The labeled lines depict the fuel margin (i.e. fraction of the aircraft remaining weight that can be loaded with fuel). Positive values indicate a feasible design. Fuel burn is shown in the colored contours. Note that a smoother plot may be created by changing the number of points in the sweep function, but this will take more time. A carpet plot run using 400 points on can be seen below. A local minimum is now visible.

    + +

    2D Sweep_20

    + +

    Note: If you run this 400 point case yourself you may see messages indicating that a segment did not converge. This is normal and can happen when a mission is run far from a feasible point. In this case, it does not have a negative impact on the results.

    + +

    Optimizing:

    + +

    Now try running an Optimization. Recomment variable_sweep(problem) then uncomment the lines below:

    + +
    
    +	output = scipy_setup.SciPy_Solve(problem,solver='SLSQP')
    +	print output
    +
    + +

    and run the file again.

    + +

    From the default inputs, the terminal (or IDE output) should display an optimum of [0.57213139 0.75471681] which corresponds to a wing area of 58 m^2, and 7.5 km. It appears to have found a minima. Keep in mind that in designing a real regional jet the desingers would incorporate additional constraints and analyses. These additional constraints change the final design considerably

    + +

    At this point, you can explore other starting points, or alter the vehicle or mission properties in Vehicles.py or Missions.py. Additionally, feel free to start using this as the basis for creating custom optimization scripts.

    + +
    +
    + +
    +
    +
    + + + + + + + + + + + + + + \ No newline at end of file diff --git a/tutorials/solar_optimization.html b/tutorials/solar_optimization.html new file mode 100644 index 00000000..68c307b1 --- /dev/null +++ b/tutorials/solar_optimization.html @@ -0,0 +1,378 @@ + + + + + Solar UAV Optimization - SUAVE Tutorial + + + + + + + + + +
    + + + + + +
    +
    +
    + + + +
    +

    Solar UAV Optimization Tutorial

    + +

    The purpose of this tutorial is to illustrate a different type of problem. We assume you have gone through the first optimization tutorial: Regional Jet Optimization. This tutorial will illustrate a little more complex setup that modifies a mission parameter.

    + +

    Your objective is simple: get a small UAV to fly from San Francisco to San Diego. In fact you can pose that as an optimization problem, with some constraints that govern how it works. There is no requirement to minimize this or maximize that. Of course you could try to minimize something, but you just want something that works for now. Later iterations can do fancier things.

    + +

    Next we will go into detail about some of the required files. Analyses.py and Plot_mission.py are straightforward from prior tutorials. So we will not go into those in detail, except to say that we are using a UAV weight model in Analyses.py.

    + +

    Optimize.py:

    + +

    Let’s pose the optimization problem first and then setup the rest. We start with the Nexus first as usual. With this design problem there are things you are uncertain of and want to solve for.

    + +

    You’re not sure if you really need any solar panels on the airplane, so to start there will be none. The solar ratio is the ratio of wing area to solar area. A value of 1 would indicate that the entire top of the wing is covered with solar panels.

    + +
    
    +    # [ tag , initial, [lb,ub], scaling, units ]
    +    problem.inputs = np.array([
    +	[ 'wing_area'       ,    0.5, (  0.1,      1.5 ),    0.5, Units.meter      ],
    +	[ 'aspect_ratio'    ,   10.0, (  5.0,     20.0 ),   10.0, Units.less       ], 
    +	[ 'dynamic_pressure',  125.0, (  1.0,   2000.0 ),  125.0, Units.pascals    ], 
    +	[ 'solar_ratio'     ,    0.0, (  0.0,      0.97),    1.0, Units.less       ], 
    +	[ 'kv'              ,  800.0, ( 10.0,  10000.0 ),  800.0, Units['rpm/volt']], 
    +    ])
    +
    + +

    Next come the constraints. The first constraint is that the battery energy can never go negative; the math behind this will be elaborated on later. The next constraint is that the plane must have a battery. Finally there are limits to coefficients of lift and throttle settings.

    + +
    
    +      # [ tag, sense, edge, scaling, units ]
    +    problem.constraints = np.array([
    +        [ 'energy_constraint', '=', 0.0, 1.0, Units.less],
    +        [ 'battery_mass'     , '>', 0.0, 1.0, Units.kg  ],       
    +        [ 'CL'               , '>', 0.0, 1.0, Units.less],
    +        [ 'Throttle_min'     , '>', 0.0, 1.0, Units.less],
    +        [ 'Throttle_max'     , '>', 0.0, 1.0, Units.less],
    +    ])
    +
    + +

    Notice here that all constraints are greater than zero. This is because SciPy’s SLSQP optimization algorithm assumes this form. To correct for these, the values are adjusted in Procedure.py. Other optimization packages such as PyOpt don’t require this strict form.

    + +

    Finally, the objective. It’s nothing of course! As long as the constraints are met, the goal of the design is satisfied.

    + +
    
    +    # [ tag, scaling, units ]
    +    problem.objective = np.array([
    +         [ 'Nothing', 1. , Units.kg],
    +    ])
    +
    + +

    Vehicles.py:

    + +

    Next, you will setup the vehicle. This is very similar to the prior Solar UAV tutorial, so we will gloss over this. The one noticeable difference is that a lower fidelity energy network is used. This means that most components operate with prescribed efficiencies. For example:

    + +
    
    +   # Component 5 the Motor
    +    motor = SUAVE.Components.Energy.Converters.Motor_Lo_Fid()
    +    motor.speed_constant       = 900. * Units['rpm/volt'] # RPM/volt is standard
    +    motor                      = size_from_kv(motor)    
    +    motor.gear_ratio           = 1. # Gear ratio, no gearbox
    +    motor.gearbox_efficiency   = 1. # Gear box efficiency, no gearbox
    +    motor.motor_efficiency     = 0.8;
    +    net.motor                  = motor   
    +
    + +

    Missions.py:

    + +

    Now for the mission setup. Here we assume it will take 1000 km and the plane will cruise off the coast at 1000 feet in altitude. The distance is a bit longer than the straight line distance, but we’re not going to fly through populated areas. The heading, or body rotation, must be set to account for the changes in latitude and longitude to accurately calculate the solar radiation. We will cruise at a constant altitude and assume it takes no time to climb and descend compared to the cruise time.

    + +
    
    +    segment.state.numerics.number_control_points = 50
    +    segment.dynamic_pressure = 115.0 * Units.pascals
    +    segment.start_time       = time.strptime("Tue, Jun 21  11:00:00  2020", "%a, %b %d %H:%M:%S %Y",)
    +    segment.altitude         = 1000.0 * Units.feet
    +    segment.distance         = 1000.0 * Units.km
    +    segment.charge_ratio     = 1.0
    +    segment.latitude         = 37.4
    +    segment.longitude        = -122.15
    +    segment.state.conditions.frames.wind.body_rotations[:,2] = 125.* Units.degrees 
    +
    + +

    Procedure.py:

    + +

    Finally we have the procedure setup. In the procedure, we resize the vehicle, calculate weights, finalize the analyses, solve the mission, and post process.

    + +

    Some notes about sizing. Each wing component (main wing, horizontal tail, and vertical tail) needs the surfaces sized based on its area and aspect ratio. Next the solar panels are sized based on the wing area and solar_ratio. Finally the motor is resized based on correlations for the speed constant of the motor.

    + +
    
    +def simple_sizing(nexus):
    +    
    +    # Pull out the vehicle
    +    vec = nexus.vehicle_configurations.base
    +    
    +    # Change the dynamic pressure based on the, add a factor of safety   
    +    vec.envelope.maximum_dynamic_pressure = nexus.missions.mission.segments.cruise.dynamic_pressure*1.2
    +    
    +    # Scale the horizontal and vertical tails based on the main wing area
    +    vec.wings.horizontal_stabilizer.areas.reference = 0.15 * vec.reference_area
    +    vec.wings.vertical_stabilizer.areas.reference   = 0.08 * vec.reference_area
    +
    +    # wing spans,areas, and chords
    +    for wing in vec.wings:
    +        
    +        # Unpack
    +        AR = wing.aspect_ratio
    +        S  = wing.areas.reference
    +        
    +        # Set the spans
    +        wing.spans.projected = np.sqrt(AR*S)
    +        
    +        # Set all of the areas for the surfaces
    +        wing.areas.wetted   = 2.0 * S
    +        wing.areas.exposed  = 1.0 * wing.areas.wetted
    +        wing.areas.affected = 1.0 * wing.areas.wetted   
    +        
    +        # Set all of the chord lengths
    +        chord = wing.areas.reference/wing.spans.projected
    +        wing.chords.mean_aerodynamic = chord
    +        wing.chords.mean_geometric   = chord
    +        wing.chords.root             = chord
    +        wing.chords.tip              = chord
    +
    +    # Size solar panel area
    +    wing_area                   = vec.reference_area
    +    spanel                      = vec.propulsors.network.solar_panel
    +    sratio                      = spanel.ratio
    +    solar_area                  = wing_area*sratio
    +    spanel.area                 = solar_area
    +    spanel.mass_properties.mass = solar_area*(0.60 * Units.kg)    
    +    
    +    # Resize the motor
    +    motor = vec.propulsors.network.motor
    +    kv    = motor.speed_constant
    +    motor = size_from_kv(motor, kv)    
    +    
    +    # diff the new data
    +    vec.store_diff()
    +
    +    return nexus
    +
    + +

    Here the battery is sized and charged. The battery weight consists of everything that is left over from sizing.

    + +
    
    +def weights_battery(nexus):
    +
    +    # Evaluate weights for all of the configurations
    +    config = nexus.analyses.base
    +    config.weights.evaluate() 
    +    
    +    vec     = nexus.vehicle_configurations.base
    +    payload = vec.propulsors.network.payload.mass_properties.mass  
    +    msolar  = vec.propulsors.network.solar_panel.mass_properties.mass
    +    MTOW    = vec.mass_properties.max_takeoff
    +    empty   = vec.weight_breakdown.empty
    +    mmotor  = vec.propulsors.network.motor.mass_properties.mass
    +    
    +    # Calculate battery mass
    +    batmass = MTOW - empty - payload - msolar -mmotor
    +    bat     = vec.propulsors.network.battery
    +    initialize_from_mass(bat,batmass)
    +    vec.propulsors.network.battery.mass_properties.mass = batmass
    +        
    +    # Set Battery Charge
    +    maxcharge = nexus.vehicle_configurations.base.propulsors.network.battery.max_energy
    +    charge    = maxcharge
    +    
    +    nexus.missions.mission.segments.cruise.battery_energy = charge 
    +
    +    return nexus
    +
    + +

    The next we run the mission and post process the results. The post_process function will setup the information of importance for the user. The energy constraint is a way of ensuring that nowhere in the mission the battery energy goes negative. The coefficient of lift is limited to 1.2. The throttle is limited to 0.9, to make sure there is excess throttle to climb. Throttle is also limited from going negative. Finally, the objective, nothing is specified to be zero.

    + +
    
    +def post_process(nexus):
    +    
    +    # Unpack
    +    mis = nexus.missions.mission.segments.cruise
    +    vec = nexus.vehicle_configurations.base
    +    res = nexus.results.mission.segments.cruise.conditions
    +    
    +    # Final Energy
    +    maxcharge    = vec.propulsors.network.battery.max_energy
    +    
    +    # Energy constraints, the battery doesn't go to zero anywhere, using a P norm
    +    p                    = 8.    
    +    energies             = res.propulsion.battery_energy[:,0]/np.abs(maxcharge)
    +    energies[energies>0] = 0.0 # Exclude the values greater than zero
    +    energy_constraint    = np.sum((np.abs(energies)**p))**(1/p) 
    +
    +    # CL max constraint, it is the same throughout the mission
    +    CL = res.aerodynamics.lift_coefficient[0]
    +    
    +    # Pack up
    +    summary = nexus.summary
    +    summary.CL                = 1.2 - CL
    +    summary.energy_constraint = energy_constraint
    +    summary.throttle_min      = res.propulsion.throttle[0]
    +    summary.throttle_max      = 0.9 - res.propulsion.throttle[0]
    +    summary.nothing           = 0.0
    +    
    +    return nexus    
    +
    + +

    Results

    +

    Let’s look at the results:

    + +
    
    +	
    +	Optimization terminated successfully    (Exit mode 0)
    +		    Current function value: 0.0
    +		    Iterations: 11
    +		    Function evaluations: 87
    +		    Gradient evaluations: 11
    +	Design Variable Table:
    +	
    +	[['wing_area' 0.5752006084860377 0.1 1.5 0.5 1.0]
    +	 ['aspect_ratio' 8.565954690253863 5.0 20.0 10.0 1.0]
    +	 ['dynamic_pressure' 55.97515712027977 1.0 2000.0 125.0 1.0]
    +	 ['solar_ratio' 0.8312208823908036 0.0 0.97 1.0 1.0]
    +	 ['kv' 1492.0665786572088 10.0 10000.0 800.0 0.10471975511965977]]
    +	
    +	Objective Table:
    +	
    +	['Nothing' 0.0 1.0 1.0]
    +	
    +	Constraint Table:
    +	
    +	[['energy_constraint' 0.0 '=' 0.0 1.0 1]
    +	 ['battery_mass' 1.5944499541683659 '>' 0.0 1.0 1]
    +	 ['CL' 0.00866061116778094 '>' 0.0 1.0 1]
    +	 ['Throttle_min' 0.3067756978833726 '>' 0.0 1.0 1]
    +	 ['Throttle_max' 0.5932243021166275 '>' 0.0 1.0 1]]
    +
    +
    + +

    Okay looks like SciPy found a feasible solution without too much time. Now let’s review the plots.

    + +

    Electronics

    + +

    So we can tell now that the battery energy doesn’t go all the way to zero. One thing to note, because we have a solar UAV the voltage is regulated differently and the C-rate doesn't apply in the same way. + +Let’s look at how the solar flux varies throughout the day and how that affects the draw from the battery.

    + +

    Solar Flux

    + + +

    So maybe those solar panels actually are worth it. They seem to decrease the load on the battery considerably during the daytime.

    + +
    +
    + +
    +
    +
    + + + + + + + + + + + + + + \ No newline at end of file diff --git a/tutorials/tail-sitter_UAV.html b/tutorials/tail-sitter_UAV.html new file mode 100644 index 00000000..994d31c0 --- /dev/null +++ b/tutorials/tail-sitter_UAV.html @@ -0,0 +1,143 @@ + + + + + Basic eVTOL- SUAVE Tutorial + + + + + + + + + + +
    + + + + + +
    +
    +
    + + + +
    +
    +

    Tail-sitter UAV Analysis

    +
    + +

    This video shows one way to setup a small tail-sitter UAV for basic analysis.

    + +
    + + + + +
    + +
    +
    + +
    +
    +
    + + + + + + + + + + + + + + \ No newline at end of file diff --git a/tutorials/turbofan.html b/tutorials/turbofan.html new file mode 100644 index 00000000..f8cdbef9 --- /dev/null +++ b/tutorials/turbofan.html @@ -0,0 +1,375 @@ + + + + + Turbofan Network - SUAVE Tutorial + + + + + + + + + +
    + + + + + +
    +
    +
    + + + +
    +

    Turbofan Modeling Tutorial

    + +

    This tutorial describes how the energy network framework in SUAVE can be used to build a model of a turbofan engine. Once this is clear to the user, understanding the setup of the other gasturbine models, the ducted fan and the turbojet will be much easier. The turbofan model is built with several turbofan components as its building blocks. These are then linked together through their inputs and outputs. The script to follow is the tut_mission_B737.py script that was used in the Boeing 737-800 Analysis Tutorial

    + +

    Setting up the Turbofan model

    + +

    First the turbofan energy network is instantiated. The parameters associated with the network as a whole are assigned.

    + +
    # ------------------------------------------------------------------
    +#   Turbofan Network
    +# ------------------------------------------------------------------    
    +
    +turbofan = SUAVE.Components.Energy.Networks.Turbofan()
    +# For some methods, the 'turbofan' tag is still necessary. This will be changed in the
    +# future to allow arbitrary tags.
    +turbofan.tag = 'turbofan'
    +
    +# High-level setup
    +turbofan.number_of_engines = 2
    +turbofan.bypass_ratio      = 5.4
    +turbofan.engine_length     = 2.71 * Units.meter
    +turbofan.nacelle_diameter  = 2.05 * Units.meter
    +turbofan.origin            = [[13.72, 4.86,-1.9],[13.72, -4.86,-1.9]] * Units.meter
    +
    +# Approximate the wetted area
    +turbofan.areas.wetted      = 1.1*np.pi*turbofan.nacelle_diameter*turbofan.engine_length
    +
    +# Establish the correct working fluid
    +turbofan.working_fluid = SUAVE.Attributes.Gases.Air()
    +
    + +

    Then the different components are added

    + +

    Components

    + +

    The basic components used to model the turbofan are described below.

    + +

    Ram

    + +

    The ‘Ram’ component is used to convert the freestream quantities that are passed into the turbofan network into stagnation quantities. As the turbofan network is based on a 1D gasdynamic analysis, most of the energy transfer across the different components are modelled as changes in the stagnation quantities. Thus the Ram component acts as a preprocessor, converting the input conditions into quantities required by the network.

    + +
    # ------------------------------------------------------------------
    +#   Component 1 - Ram
    +
    +# Converts freestream static to stagnation quantities
    +ram = SUAVE.Components.Energy.Converters.Ram()
    +ram.tag = 'ram'
    +
    +# add to the network
    +turbofan.append(ram)
    +
    + +

    Nozzle

    + +

    The ‘Nozzle’ component is used to model the inlet diffuser, the outlet fan, and the compressor nozzles as shown below.

    + +
    # ------------------------------------------------------------------
    +# ------------------------------------------------------------------
    +#  Component 2 - Inlet Nozzle
    +
    +# Create component
    +inlet_nozzle = SUAVE.Components.Energy.Converters.Compression_Nozzle()
    +inlet_nozzle.tag = 'inlet_nozzle'
    +
    +# Specify performance
    +inlet_nozzle.polytropic_efficiency = 0.98
    +inlet_nozzle.pressure_ratio        = 0.98
    +
    +# Add to network
    +turbofan.append(inlet_nozzle)
    +
    +
    +# ------------------------------------------------------------------
    +#  Component 8 - Core Nozzle
    +
    +# Create component
    +nozzle = SUAVE.Components.Energy.Converters.Expansion_Nozzle()   
    +nozzle.tag = 'core_nozzle'
    +
    +# Specify performance
    +nozzle.polytropic_efficiency = 0.95
    +nozzle.pressure_ratio        = 0.99    
    +
    +# Add to network
    +turbofan.append(nozzle)
    +
    +
    +# ------------------------------------------------------------------
    +#  Component 9 - Fan Nozzle
    +
    +# Create component
    +nozzle = SUAVE.Components.Energy.Converters.Expansion_Nozzle()   
    +nozzle.tag = 'fan_nozzle'
    +
    +# Specify performance
    +nozzle.polytropic_efficiency = 0.95
    +nozzle.pressure_ratio        = 0.99    
    +
    +# Add to network
    +turbofan.append(nozzle)
    +
    + +

    Compressor

    + +

    Two compressors are used in the turbofan model, a low and a high pressure compressor.

    + +
    # ------------------------------------------------------------------
    +# ------------------------------------------------------------------
    +#  Component 3 - Low Pressure Compressor
    +
    +# Create component
    +compressor = SUAVE.Components.Energy.Converters.Compressor()    
    +compressor.tag = 'low_pressure_compressor'
    +
    +# Specify performance
    +compressor.polytropic_efficiency = 0.91
    +compressor.pressure_ratio        = 1.14    
    +
    +# Add to network
    +turbofan.append(compressor)
    +    
    +
    +# ------------------------------------------------------------------
    +#  Component 4 - High Pressure Compressor
    +
    +# Create component
    +compressor = SUAVE.Components.Energy.Converters.Compressor()    
    +compressor.tag = 'high_pressure_compressor'
    +
    +# Specify performance
    +compressor.polytropic_efficiency = 0.91
    +compressor.pressure_ratio        = 13.415    
    +
    +# Add to network
    +turbofan.append(compressor)
    +
    + +

    Fan

    + +

    A fan component is also added to the network. If you were to model a turbojet, the fan component and the fan nozzle would not be added but all the other components would remain the same.

    + +
    # ------------------------------------------------------------------
    +#  Component 10 - Fan
    +
    +# Create component
    +fan = SUAVE.Components.Energy.Converters.Fan()   
    +fan.tag = 'fan'
    +
    +# Specify performance
    +fan.polytropic_efficiency = 0.93
    +fan.pressure_ratio        = 1.7    
    +
    +# Add to network
    +turbofan.append(fan)
    +
    + +

    Combustor

    + +

    The combustor component is where the fuel-to-air ratio is computed. It is also used to compute the sfc and the thrust later in the network.

    + +
    
    +# ------------------------------------------------------------------
    +#  Component 7 - Combustor
    +
    +# Create component    
    +combustor = SUAVE.Components.Energy.Converters.Combustor()   
    +combustor.tag = 'combustor'
    +
    +# Specify performance
    +combustor.efficiency                = 0.99 
    +combustor.alphac                    = 1.0   
    +combustor.turbine_inlet_temperature = 1450 # K
    +combustor.pressure_ratio            = 0.95
    +combustor.fuel_data                 = SUAVE.Attributes.Propellants.Jet_A()    
    +
    +# Add to network
    +turbofan.append(combustor)
    +
    + +

    Turbine

    + +

    The work done by the fan and the compressors is used to compute the turbine work required. This is used to compute the change in the stagnation quantities across the turbine.

    + +
        # ------------------------------------------------------------------
    +    #  Component 5 - Low Pressure Turbine
    +    
    +    # Create component
    +    turbine = SUAVE.Components.Energy.Converters.Turbine()   
    +    turbine.tag='low_pressure_turbine'
    +    
    +    # Specify performance
    +    turbine.mechanical_efficiency = 0.99
    +    turbine.polytropic_efficiency = 0.93     
    +    
    +    # Add to network
    +    turbofan.append(turbine)
    +      
    +    # ------------------------------------------------------------------
    +    #  Component 6 - High Pressure Turbine
    +    
    +    # Create component
    +    turbine = SUAVE.Components.Energy.Converters.Turbine()   
    +    turbine.tag='high_pressure_turbine'
    +
    +    # Specify performance
    +    turbine.mechanical_efficiency = 0.99
    +    turbine.polytropic_efficiency = 0.93     
    +    
    +    # Add to network
    +    turbofan.append(turbine)  
    +    
    +
    + +

    Thrust

    + +

    The thrust component takes in the initial (inputs of the inlet nozzle) and final (exit of the fan and core exirt nozzles) stagnation quantities of the network and the fuel to air ratio and computes the specific fuel conspumption (sfc) and thrust generated by the network (turbofan engine).

    + +
    
    +# ------------------------------------------------------------------
    +#  Component 11 - thrust (to compute the thrust)
    +
    +thrust = SUAVE.Components.Energy.Processes.Thrust()       
    +thrust.tag ='compute_thrust'
    +
    +# Design thrust is used to determine mass flow at full throttle
    +thrust.total_design             = 2*24000. * Units.N #Newtons
    +
    +# Add to network
    +turbofan.thrust = thrust   
    +
    + +

    Sizing the Turbofan

    + +

    Once the network is built, it is essential to size the engine with a set of sizing conditions. The sizing function ‘turbofan_sizing’ takes in the model of the turbofan, the mach number, and the altitude for which the turbofan is sized. The sizing thrust is an engine/network property (defined in the ‘Setting up the Turbofan model’ section above). The function takes these quantities and computes the design mass flow rate through the components. Once sized, the network/engine can be added to the vehicle as shown in the B737 tutorial.

    + +
    
    +# Design sizing conditions are also used to determine mass flow
    +altitude      = 35000.0*Units.ft
    +mach_number   = 0.78     
    +
    +# Determine turbofan behavior at the design condition
    +turbofan_sizing(turbofan,mach_number,altitude)   
    +
    +# Add turbofan network to the vehicle 
    +vehicle.append_component(turbofan) 
    +
    +
    +
    + +
    +
    +
    + + + + + + + + + + + + + + \ No newline at end of file