TemperatureStagnation:

moved to AeroUtils/

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   Compute the stagnation temperature in the earth's atmosphere.
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   Form:
   t0 = TemperatureStagnation( v, h )
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   ------
   Inputs
   ------
   v               (1,:) Velocity (m/s)
   h               (1,:) Altitude (m)

   -------
   Outputs
   -------
   t0              (1,1) Stagnation temperature

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	References:	http://en.wikipedia.org/wiki/Stagnation_temperature
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Children:

Common: AtmosphericCalculations/AtmGamma
Common: AtmosphericCalculations/StdAtm
Common: Graphics/Plot2D