Air at 0.9 MPa and 400 K enters a converging nozzle with a
Chapter 17, Problem 17131(choose chapter or problem)
Air at 0.9 MPa and 400 K enters a converging nozzle with a velocity of 180 m/s. The throat area is 10 cm2 . Assuming isentropic flow, calculate and plot the mass flow rate through the nozzle, the exit velocity, the exit Mach number, and the exit pressurestagnation pressure ratio versus the back pressurestagnation pressure ratio for a back pressure range of 0.9 $ Pb $ 0.1 MPa.
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