Path: Propulsion/Gas
% Compute the Mach number -------------------------------------------------------------------------- Form: m = MachNumber( u, gamma, molWt, T ) -------------------------------------------------------------------------- ------ Inputs ------ u (n) Velocity (m/sec) gamma (1,1) Ratio of specific heats molWt (1,1) Average molecular weight of the gas (kg/mole) T (m) Temperature (deg-K) ------- Outputs ------- m (n,m) Mach number --------------------------------------------------------------------------
Propulsion: Gas/SpeedSnd Common: Graphics/Mesh2
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