Calculate the mass flow rate, nozzle diameter and velocity


Air flows from a reservoir ( ) 2 0 0 1 , 40 p MN m T C = = ° through a Laval nozzle with a throat diameter of 0.1 m and a maximum Mach number of 0.75.

Calculate the mass flow rate, nozzle diameter, velocity, pressure and temperature at the exit where M = 0.5.

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Physics: Calculate the mass flow rate, nozzle diameter and velocity
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