Consider the isentropic flow through a supersonic wind-tunnel nozzle. The reservoir properties are T0 = 500 K

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Consider the isentropic flow through a supersonic wind-tunnel nozzle. The reservoir properties are T0 = 500 K and p0 = 10atm. If p = 1atm at the nozzle exit, calculate the exit temperature and density.

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Fundamentals of Aerodynamics

ISBN: 978-0070016798

2nd Edition

Authors: J. Anderson

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Question Posted: Dec 09, 2010 03:24 AM

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Consider the isentropic flow through a supersonic wind-tunnel nozzle. The reservoir properties are T0 = 500 K

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Fundamentals of Aerodynamics

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