Path: ACPro/ACEngine
% Computes the value of the burner temperature given the throttle ratio and the burner value at sea level static conditions. -------------------------------------------------------------------------- Form: pT = PressureTotal( p, gamma, machNo ) -------------------------------------------------------------------------- ------ Inputs ------ tT4SLS (1,1) Burner temperature at sea level static throttleRatio (1,1) Throttle ratio ------- Outputs ------- tT4 (1,1) Burner temperature --------------------------------------------------------------------------
ACPro: ACEngine/Theta0 Common: Atmosphere/StdAtm Common: Graphics/Plot2D
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