The flow just upstream of a normal shock wave is given by p1 = 1800 lb/ft2, T,

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The flow just upstream of a normal shock wave is given by p1 = 1800 lb/ft2, T, =480°R, and M1 = 3.1. Calculate the velocity and M* behind the shock.

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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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The flow just upstream of a normal shock wave is given by p1 = 1800 lb/ft2, T,

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From Table A2 Hence T2 7723 1 1 22 V M a2 04695 17966 84...View the full answer

Fundamentals of Aerodynamics

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