RHSAerodynamicHeating:

Path: Thermal/ThermalAnalysis

% Compute aerodynamic heating.
   This is a flat plate model.

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   Form:
   qDot = RHSAerodynamicHeating( d )
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   Inputs
   ------
   d       (1,1)   Data structure
                   .rho (1,1) Density (kg/m^3)
                   .v   (1,1) Velocity (m/s)
                   .s   (1,1) Surface area (m^2)
                   .cH  (1,1) Heat transfer coefficient

   -------
   Outputs
   -------
   qDot    (1,1)   Heating rate

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   Reference: http://worldofaerospace.googlepages.com/Calculate-
              Aerodynamic-Heating-Rate.htm
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