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. Type TemperatureStagnation for a demo. -------------------------------------------------------------------------- Form: t0 = TemperatureStagnation( v, h, r ) -------------------------------------------------------------------------- ------ Inputs ------ v (1,:) Velocity (m/s) h (1,:) Altitude (m) r (1,1) Recovery factor (0.88 turbulent, default; 0.85 laminar) ------- Outputs ------- t0 (1,1) Stagnation temperature -------------------------------------------------------------------------- References: http://en.wikipedia.org/wiki/Stagnation_temperature --------------------------------------------------------------------------
AerospaceUtils: AeroData/AtmData AerospaceUtils: AtmosphericCalculations/AtmGamma Common: Atmosphere/StdAtm Common: CommonData/SwooshWatermark Common: General/CellToMat Common: General/MatToCell Common: General/Watermark Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle
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