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| <html lang="en"><head><meta charset="UTF-8"/><meta name="viewport" content="width=device-width, initial-scale=1.0"/><title>DFDC Airfoil Type · DuctAPE.jl</title><meta name="title" content="DFDC Airfoil Type · DuctAPE.jl"/><meta property="og:title" content="DFDC Airfoil Type · DuctAPE.jl"/><meta property="twitter:title" content="DFDC Airfoil Type · DuctAPE.jl"/><meta name="description" content="Documentation for DuctAPE.jl."/><meta property="og:description" content="Documentation for DuctAPE.jl."/><meta property="twitter:description" content="Documentation for DuctAPE.jl."/><script data-outdated-warner src="../../../assets/warner.js"></script><link href="https://cdnjs.cloudflare.com/ajax/libs/lato-font/3.0.0/css/lato-font.min.css" rel="stylesheet" type="text/css"/><link href="https://cdnjs.cloudflare.com/ajax/libs/juliamono/0.050/juliamono.min.css" rel="stylesheet" type="text/css"/><link href="https://cdnjs.cloudflare.com/ajax/libs/font-awesome/6.4.2/css/fontawesome.min.css" 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href="../../../DuctAPE/theory/">Theory</a></li></ul></li><li><span class="tocitem">C<span>$^4$</span>Blade</span><ul><li><a class="tocitem" href="../../intro/">Intro</a></li><li><input class="collapse-toggle" id="menuitem-3-2" type="checkbox" checked/><label class="tocitem" for="menuitem-3-2"><span class="docs-label">Blade Element Types</span><i class="docs-chevron"></i></label><ul class="collapsed"><li class="is-active"><a class="tocitem" href>DFDC Airfoil Type</a></li><li><a class="tocitem" href="../CCBlade/">CCBlade Airfoil Types</a></li><li><a class="tocitem" href="../actuator_disk/">Actuator Disk Type</a></li><li><a class="tocitem" href="../cascade/">Cascade Types</a></li></ul></li><li><a class="tocitem" href="../../corrections/">Polar Modification</a></li><li><a class="tocitem" href="../../api/">API Reference</a></li></ul></li></ul><div class="docs-version-selector field has-addons"><div class="control"><span class="docs-label button is-static is-size-7">Version</span></div><div class="docs-selector control is-expanded"><div class="select is-fullwidth is-size-7"><select id="documenter-version-selector"></select></div></div></div></nav><div class="docs-main"><header class="docs-navbar"><a class="docs-sidebar-button docs-navbar-link fa-solid fa-bars is-hidden-desktop" id="documenter-sidebar-button" href="#"></a><nav class="breadcrumb"><ul class="is-hidden-mobile"><li><a class="is-disabled">C<span>$^4$</span>Blade</a></li><li><a class="is-disabled">Blade Element Types</a></li><li class="is-active"><a href>DFDC Airfoil Type</a></li></ul><ul class="is-hidden-tablet"><li class="is-active"><a href>DFDC Airfoil Type</a></li></ul></nav><div class="docs-right"><a class="docs-navbar-link" href="https://github.com/byuflowlab/DuctAPE.jl/blob/{commit}{path}#L{line}" title="View the repository on GitHub"><span class="docs-icon fa-brands"></span><span class="docs-label is-hidden-touch">GitHub</span></a><a class="docs-navbar-link" href="https://github.com/byuflowlab/DuctAPE.jl/blob/main/docs/src/C4Blade/airfoil_types/DFDC.md" title="Edit source on GitHub"><span class="docs-icon fa-solid"></span></a><a class="docs-settings-button docs-navbar-link fa-solid fa-gear" id="documenter-settings-button" href="#" title="Settings"></a><a class="docs-article-toggle-button fa-solid fa-chevron-up" id="documenter-article-toggle-button" href="javascript:;" title="Collapse all docstrings"></a></div></header><article class="content" id="documenter-page"><h1 id="DFDC-Airfoil-Type"><a class="docs-heading-anchor" href="#DFDC-Airfoil-Type">DFDC Airfoil Type</a><a id="DFDC-Airfoil-Type-1"></a><a class="docs-heading-anchor-permalink" href="#DFDC-Airfoil-Type" title="Permalink"></a></h1><p>The DFDC Airfoil type is very similar to the <a href="https://web.mit.edu/drela/Public/web/xrotor/">XROTOR</a> airfoil type, but includes additions for cascade corrections based on stagger and solidity. The cascade corrections aren't particularly accurate, but they do apply ballpark effects resulting from high solidity blade sections. The main benefit to this airfoil type is its simplicity and that the post-stall behavior is already in a format allowing more robust convergence of the DuctAPE solvers.</p><article class="docstring"><header><a class="docstring-article-toggle-button fa-solid fa-chevron-down" href="javascript:;" title="Collapse docstring"></a><a class="docstring-binding" id="DuctAPE.C4Blade.DFDCairfoil" href="#DuctAPE.C4Blade.DFDCairfoil"><code>DuctAPE.C4Blade.DFDCairfoil</code></a> — <span class="docstring-category">Type</span><span class="is-flex-grow-1 docstring-article-toggle-button" title="Collapse docstring"></span></header><section><div><p><strong>Fields:</strong></p><ul><li><code>alpha0::Float</code> : zero lift angle of attack</li><li><code>clmax::Float</code> : maximum cl</li><li><code>clmin::Float</code> : minimum cl</li><li><code>dclda::Float</code> : lift curve slope (1/radians)</li><li><code>dclda_stall::Float</code> : lift curve slope post-stall (1/radians)</li><li><code>dcl_stall::Float</code> : cl increment from initial to total stall.</li><li><code>cdmin::Float</code> : minimum cd</li><li><code>cldmin::Float</code> : cl at cdmin</li><li><code>dcddcl2::Float</code> : quadratic curve factor for cl vs cd curve <span>$\left(\frac{d(c_d)}{d(c_l^2)}\right)$</span></li><li><code>cmcon::Float</code> : pitching moment constant (unused right now)</li><li><code>Re_ref::Float</code> : reference Reynolds number at which cd values apply</li><li><code>Re_exp::Float</code> : Reynolds number exponent scaling <span>$\left( c_d = c_d(Re/Re_{ref})^{Re_{exp}}\right)$</span> should be 0.2 for fully laminar and 0.5 for fully turbulent</li><li><code>mcrit::Float</code> : critical Mach number</li><li><code>correct_for_mach::Bool</code> : flag to add Prandtl-Glauert correction</li><li><code>correct_for_cascade::Bool</code> : flag to add cascade corrections</li><li><code>correct_for_reynolds::Bool</code> : flag to add reynolds drag correction</li><li><code>correct_for_transonic::Bool</code> : flag to add drag correction above critical mach number</li></ul></div><a class="docs-sourcelink" target="_blank" href="https://github.com/byuflowlab/DuctAPE.jl/blob/ed6dd796b897430aad2bd361fc28ead611dbd3d0/src/C4Blade/dfdc_polars.jl#L1-L20">source</a></section></article></article><nav class="docs-footer"><a class="docs-footer-prevpage" href="../../intro/">« Intro</a><a class="docs-footer-nextpage" href="../CCBlade/">CCBlade Airfoil Types »</a><div class="flexbox-break"></div><p class="footer-message">Powered by <a href="https://github.com/JuliaDocs/Documenter.jl">Documenter.jl</a> and the <a href="https://julialang.org/">Julia Programming Language</a>.</p></nav></div><div class="modal" id="documenter-settings"><div class="modal-background"></div><div class="modal-card"><header class="modal-card-head"><p class="modal-card-title">Settings</p><button class="delete"></button></header><section class="modal-card-body"><p><label class="label">Theme</label><div class="select"><select id="documenter-themepicker"><option value="auto">Automatic (OS)</option><option value="documenter-light">documenter-light</option><option value="documenter-dark">documenter-dark</option><option value="catppuccin-latte">catppuccin-latte</option><option value="catppuccin-frappe">catppuccin-frappe</option><option value="catppuccin-macchiato">catppuccin-macchiato</option><option value="catppuccin-mocha">catppuccin-mocha</option></select></div></p><hr/><p>This document was generated with <a href="https://github.com/JuliaDocs/Documenter.jl">Documenter.jl</a> version 1.7.0 on <span class="colophon-date" title="Saturday 21 September 2024 17:38">Saturday 21 September 2024</span>. 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