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
--------------------------------------------------------------------------
Reference: Mattingly, "Elements of Gas Turbine Propulsion,"
McGraw-Hill, 1996, p. 479.
--------------------------------------------------------------------------
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
Back to the ACPro Module page