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SUPPORT SITE |
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Path: ACPro/ACEngine
% Computes temperature ratio
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Form:
tau = TempRatioFromPressure( pi, eta, gamma )
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Inputs
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pi (1,n) Pressure ratio
eta (1,n) Efficiency
gamma (1,n) Gamma
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Outputs
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tau (1,n) Temperature ratio
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Reference: Mattingly, "Elements of Gas Turbine Propulsion,"
McGraw-Hill, 1996.
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Common: Graphics/Plot2D
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