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SUPPORT SITE |
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Path: AerospaceUtils/AtmosphericCalculations
% Compute the stagnation temperature in the earth's atmosphere. The the altitude is greater than 80 km it uses values at 80 km. -------------------------------------------------------------------------- Form: t0 = TemperatureStagnation( v, h, r ) -------------------------------------------------------------------------- ------ Inputs ------ v (1,:) Velocity (m/s) h (1,:) Altitude (m) r (1,1) Recovery factor (0.88 turbulent, 0.85 laminar) ------- Outputs ------- t0 (1,1) Stagnation temperature -------------------------------------------------------------------------- References: http://en.wikipedia.org/wiki/Stagnation_temperature --------------------------------------------------------------------------
AerospaceUtils: AtmosphericCalculations/AtmGamma Common: Atmosphere/StdAtm Common: Graphics/Plot2D
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