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 85P
Air approaches a normal shock at V1 = 900 m/s, p1 = 50 kPa absolute, and T1 = 220 K. What are the velocity and pressure after the shock? What would the velocity and pressure be if the flow were decelerated isentropically to the same Mach number?
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Chapter 12 Solutions
Fox and McDonald's Introduction to Fluid Mechanics
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