Path: ACPro/ACProAerodynamics
% Hypersonic coefficient of pressure. Type CPHypersonic for a demo. -------------------------------------------------------------------------- Form: cP = CPHypersonic( m, gamma ) -------------------------------------------------------------------------- ------ Inputs ------ m (1,:) Freestream Mach number gamma (1,1) Ratio of specific heats (Default = 1.4) ------- Outputs ------- cP (1,:) Pressure coefficient --------------------------------------------------------------------------
AC: Aero/RayleighPitotTube AerospaceUtils: AeroData/AtmData AerospaceUtils: AtmosphericCalculations/AtmGamma Common: Atmosphere/StdAtm 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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