Throttle:

Path: ACPro/ACEngine

% Computes the value of the burner temperature given the throttle ratio
   and the burner value at sea level static conditions.
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   Form:
   pT = PressureTotal( p, gamma, machNo )
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   ------
   Inputs
   ------
   tT4SLS          (1,1)   Burner temperature at sea level static
   throttleRatio   (1,1)   Throttle ratio

   -------
   Outputs
   -------
   tT4             (1,1)   Burner temperature

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Children:

ACPro: ACEngine/Theta0
Common: Atmosphere/StdAtm
Common: Graphics/Plot2D

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