A nozzle is designed assuming reversible adiabatic flow with an exit Mach number of2.6 while flowing air

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A nozzle is designed assuming reversible adiabatic flow with an exit Mach number of2.6 while flowing air with a stagnation pressure and temperature of 2 MPa and 150°C, respectively. The mass flow rate is 5 kg/s, and k may be assumed to be 1.40 and constant. Determine the exit pressure, temperature, exit area, and the throat area.
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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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