Fox and McDonald's Introduction to Fluid Mechanics
9th Edition
ISBN: 9781118912652
Author: Philip J. Pritchard, John W. Mitchell
Publisher: WILEY
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Textbook Question
Chapter 12, Problem 87P
Air undergoes a normal shock. Upstream, T1 = 35°C, p1 = 229 kPa absolute, and V1 = 704 m/s. Determine the temperature and stagnation pressure of the air stream leaving the shock.
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Chapter 12 Solutions
Fox and McDonald's Introduction to Fluid Mechanics
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