Path: ACPro/ACProAerodynamics
% Compute the drag polar from data lift and drag coefficient data. The drag polar is cD = cD0 + k*cL^2 Does a least squares curve fit. Type DragPolarFromData for a demo. -------------------------------------------------------------------------- Form: [cD0, k] = DragPolarFromData( cD, cL ) -------------------------------------------------------------------------- ------ Inputs ------ cD (1,:) Drag coefficients cL (1,:) Lift coefficients ------- Outputs ------- cD0 (1,1) Drag at zero lift k (1,1) Induced drag coefficient --------------------------------------------------------------------------
Common: CommonData/SwooshWatermark Common: General/CellToMat Common: General/MatToCell Common: General/Watermark Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle Math: Linear/LeastSq
Back to the ACPro Module page