Path: Airships/Modeling
% Compute the approximate drag on an airship. -------------------------------------------------------------------------- Form: D = AirshipDrag( h, u, A, Cd ); -------------------------------------------------------------------------- ------ Inputs ------ h (1) Altitude [m] u (1) Velocity [m/s] A (1) Reference Aera [m^2] Cd (1) Zero-incidence drag coeffcient ------- Outputs ------- D (1) Total drag force [N] --------------------------------------------------------------------------
AerospaceUtils: AeroData/AtmData Common: Atmosphere/StdAtm Common: CommonData/SwooshWatermark Common: General/CellToMat Common: General/MatToCell Common: General/Watermark Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle
Back to the Airships Module page