A normal shock in air has an upstream total pressure of 75 psia, a stagnation temperature of

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A normal shock in air has an upstream total pressure of 75 psia, a stagnation temperature of 900 R, and Mx = 1.4. Find the downstream stagnation pressure.

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Fundamentals Of Thermodynamics

ISBN: 9781118131992

8th Edition

Authors: Claus Borgnakke, Richard E. Sonntag

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