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 89P
The stagnation temperature in an airflow is 149°C upstream and downstream from a normal shock wave. The absolute stagnation pressure downstream from the shock wave is 229.5 kPa. Through the wave the absolute pressure rises from 103.4 to 138 kPa. Determine the velocities upstream and downstream from the wave.
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Chapter 12 Solutions
Fox and McDonald's Introduction to Fluid Mechanics
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