Path: ACPro/ACEngine
% Computes the value of the burner temperature given the throttle ratio and the burner value at sea level static conditions. -------------------------------------------------------------------------- Form: tT4 = Throttle( tT4SLS, throttleRatio, t0, machNo, units ) -------------------------------------------------------------------------- ------ Inputs ------ tT4SLS (1,1) Burner temperature at sea level static t0 (1,1) Ambient temperature m0 (1,1) Mach number units (1,1) Unit type ------- Outputs ------- tT4 (1,1) Burner temperature --------------------------------------------------------------------------
ACPro: ACEngine/Theta0 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 Math: Linear/DupVect
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