Path: Airships/Modeling
% The drag coefficient of airship as a function of angle of attack. -------------------------------------------------------------------------- Form: cD = CMAirship( alpha, delta ) -------------------------------------------------------------------------- ------ Inputs ------ alpha (:) Angle of attack (deg) delta (:) Elevator angle (deg) ------- Outputs ------- cD (:) Drag coefficient --------------------------------------------------------------------------
Common: CommonData/SwooshWatermark Common: General/CellToMat Common: General/MatToCell Common: General/Watermark Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle
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