|
SUPPORT SITE |
|
|
|
SUPPORT SITE |
|
Path: ACPro/ACEngine
% Computes the total temperature ratio from Mach number and gamma.
--------------------------------------------------------------------------
Form:
tR = TempRatioFromMachAndGamma( cP, gamma )
--------------------------------------------------------------------------
------
Inputs
------
m (1,n) Specific heat
gamma (1,1) Gamma
-------
Outputs
-------
tR (1,n) Temperature ratio
--------------------------------------------------------------------------
Reference: Mattingly, "Elements of Gas Turbine Propulsion,"
McGraw-Hill, 1996.
--------------------------------------------------------------------------
Common: Graphics/Plot2D
Back to the ACPro Module page