Air flows into a convergent-divergent nozzle with an exit area of1.59 times the throat area of 0.005

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Air flows into a convergent-divergent nozzle with an exit area of1.59 times the throat area of 0.005 m. The inlet stagnation state is 1 MPa, 600 K. Find the backpressure that will cause subsonic flow throughout the entire nozzle with M = 1 at the throat. What is the mass flow rate?
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Fundamentals of Thermodynamics

ISBN: 978-0471152323

6th edition

Authors: Richard E. Sonntag, Claus Borgnakke, Gordon J. Van Wylen

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