Path: ACPro/ACPerformance
% Angle of attack for maximum L/D. This assumes cD = cD0 + k*cL^2 cL = cLA*alpha Since version 4 (ACT). -------------------------------------------------------------------------- Form: [alpha, lD] = AngleOfAttackMaxLD( cD0, k, cLA ) -------------------------------------------------------------------------- ------ Inputs ------ cD0 (1,1) Zero angle of attack drag k (1,1) Induced drag coefficient cLA (1,1) Lift curve slope ------- Outputs ------- alpha (1,1) Angle of attack (rad) lD (1,1) Maximum lift over drag --------------------------------------------------------------------------
Common: Graphics/Plot2D
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