Fluid Mechanics: Fundamentals and Applications
4th Edition
ISBN: 9781259696534
Author: Yunus A. Cengel Dr., John M. Cimbala
Publisher: McGraw-Hill Education
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Question
Chapter 12, Problem 73P
To determine
Two possible oblique shock angles
To calculate:
The pressure and Mach number downstream of the oblique shock.
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The Mach number behind a normal shock wave is 0.4752. What is the Mach number in front of the wave? What are the density, pressure, and temperature ratios across the shock?
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Chapter 12 Solutions
Fluid Mechanics: Fundamentals and Applications
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