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Path: ACPro/ACThermal
------------------------------------------------------------------------ Heat flux as a function of mach number. Type AerodynamicHeatFlux for a demo. Since version 2014.1 ------------------------------------------------------------------------ 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) ------------------------------------------------------------------------
Common: Atmosphere/StdAtm Common: Graphics/Plot2D
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