Path: ACPro/ACThermal
% Heat flux as a function of mach number. Type AerodynamicHeatFlux for a demo. ------------------------------------------------------------------------ Form: qDot = AerodynamicHeatFlux( m, l, p ) ------------------------------------------------------------------------ ------ Inputs ------ m (1,:) Mach number l (1,1) Characteristic length (m) p (.) Standard atmosphere ------- Outputs ------- qDot (1,:) Heat flux (W/m^2) ------------------------------------------------------------------------
AerospaceUtils: AeroData/AtmData 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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