Path: ACPro/ACEngine
% Computes the total temperature ratio from Mach number and gamma.
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Form:
tR = TempRatioFromMachAndGamma( cP, gamma )
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Inputs
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m (1,n) Specific heat
gamma (1,1) Gamma
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Outputs
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tR (1,n) Temperature ratio
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Reference: Mattingly, "Elements of Gas Turbine Propulsion,"
McGraw-Hill, 1996.
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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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