AtmGamma:

Path: AerospaceUtils/AtmosphericCalculations

% Computes the ratio of specific heats for air.

 The ratio is a function of temperature of the atmosphere.

 Type AtmGamma for demo showing gamma from 0 to 80 km altitude.

 Since version 1.
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   Form:
   gamma = AtmGamma( T )
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   ------
   Inputs
   ------
   T       (1,:)   Temperature (deg-K)

   -------
   Outputs
   -------
   gamma   (1,:)   Ratio of specific heats

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   References:	Hill, P.G., C. R. Peterson, Mechanics and Thermodynamics
               of Propulsion, Addison-Wesley, Reading, MA, 1970, p. 541.
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Children:

Common: Atmosphere/StdAtm
Common: Graphics/Plot2D

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