Path: ACPro/ACEngine
% Static pumping of air. -------------------------------------------------------------------------- Form: [mDot, v] = StaticPumping( cP, altitude, pR, g ) -------------------------------------------------------------------------- ------ Inputs ------ cP (1,1) Specific heat altitude (1,1) Altitude (m) (Unused if g entered) pR (1,:) Pressure ratio g (1,1) Standard atmosphere ------- Outputs ------- mDot (1,:) Mass (kg/m^2) v (1,:) Velocity --------------------------------------------------------------------------
AerospaceUtils: AtmosphericCalculations/AtmGamma Common: Atmosphere/StdAtm Common: Graphics/Plot2D
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