MachNumber:

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
  
--------------------------------------------------------------------------

Children:

Propulsion: Gas/SpeedSnd
Common: Graphics/Mesh2

Back to the Propulsion Module page