Path: AerospaceUtils/AtmosphericCalculations
% Computes air data based on a simplified standard atmosphere model. If no arguments are specified it will plot m and q versus v and h. Type AirData for demo. -------------------------------------------------------------------------- Form: [m, q, rho, pS] = AirData( v, altitude, AtmData, units ) -------------------------------------------------------------------------- ------ Inputs ------ v (1,:) Velocity (m/sec) altitude (1,:) Altitude (m) AtmData (:,6) Standard atmosphere data units (1,:) 'si' or 'eng' i.e. m & kg or lb & ft ------- Outputs ------- m (v,h) Mach number q (v,h) Dynamic Pressure rho h Density pS h Static Pressure --------------------------------------------------------------------------
AerospaceUtils: AeroData/AtmData Common: Atmosphere/StdAtm Common: CommonData/SwooshWatermark Common: General/CellToMat Common: General/DeBlankLT Common: General/MatToCell Common: General/Watermark Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle Common: Graphics/XLabelS Common: Graphics/YLabelS Common: Graphics/ZLabelS
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