Path: ACPro/ACEngine
% Computes the dimensionless total temperature. -------------------------------------------------------------------------- Form: theta0 = Theta0( gamma, t0, machNo, units ) -------------------------------------------------------------------------- ------ Inputs ------ gamma (1,n) Burner temperature at sea level static t0 (1,n) Temperature machNo (1,m) Mach number units (1,:) 'mks' or 'eng' ------- Outputs ------- theta0 (n,m) Dimensionless total temperature --------------------------------------------------------------------------
AerospaceUtils: AtmosphericCalculations/AtmGamma Common: Atmosphere/StdAtm Common: Graphics/Plot2D Math: Linear/DupVect
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