Path: ACPro/ACPerformance
% Generates vertices and faces for a wing based on the wing parameters. Produces a symmetric airfoil. Since version 4 (ACT). -------------------------------------------------------------------------- Form: [v, f] = WingFromParameters( c, s, b, sweep, t ) -------------------------------------------------------------------------- ------ Inputs ------ c (1,1) Root chord length (m) s (1,1) Wing area (m^2) b (1,1) Wing span (m) sweep (1,1) Sweep angle (rad) t (1,1) Thickness ratio ------- Outputs ------- v (:,3) Vertices f (:,3) Faces --------------------------------------------------------------------------
Common: Graphics/NewFig Common: Graphics/XLabelS Common: Graphics/YLabelS Common: Graphics/ZLabelS
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