Find the back pressure that will cause subsonic flow

Reference no: EM131238500

Air flows into a convergent-divergent nozzle with an exit area of 1.59 times the throat area of 0.005 m². The inlet stagnation state is 1 MPa, 600 K. Find the back pressure that will cause subsonic flow throughout the entire nozzle with M = 1 at the throat. What is the mass flow rate?

Reference no: EM131238500

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