DynamicPressureAndHeat:

Path: ACPro/ACThermal

------------------------------------------------------------------------
   Heat, velocity and temperature at a fixed dynamic pressure.

   Type DynamicPressureAndHeat for a demo at the Space Shuttle maximum
   dynamic pressure.

   Since version 2014.1
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   Form:
   [v, t, qDot] = DynamicPressureAndHeat( h, l, qMax )
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   ------
   Inputs
   ------
   h               (1,:)     Altitude (km)
   l               (1,1)     Initial flight path angle at h0 (rad)
   qMax            (1,1)     Maximum dynamic pressure

   -------
   Outputs
   -------
   v               (1,:)     Velocity (m/s)
   t               (1,:)     Temperature stagnation (deg-K)
   qDot            (1,:)     Heat flux (W/m^2)

------------------------------------------------------------------------

Children:

AeroUtils: AtmosphericCalculations/TemperatureStagnation
Common: Atmosphere/StdAtm
Common: Graphics/Plot2D

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