Path: ACPro/ACPerformance
% Generates the taper and trailing edge angle for a wing. s and b are for the entire wing (both sides of the fuselage). WingAreaToTaper( c, s, b, sweep ), with no outputs, will generate a picture of the wing. -------------------------------------------------------------------------- Form: [f, omegaT] = WingAreaToTaper( c, s, b, sweep ) -------------------------------------------------------------------------- ------ 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) ------- Outputs ------- f (1,1) Taper omegaT (1,1) Trailing edge angle (rad) --------------------------------------------------------------------------
Common: General/DeBlankLT Common: Graphics/NewFig Common: Graphics/PltStyle Common: Graphics/TitleS Common: Graphics/XLabelS Common: Graphics/YLabelS Common: Graphics/ZLabelS
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