12.29 A normal shock wave exists in an airflow. The absolute pressure, velocity, and temperature just upstream
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12.29 A normal shock wave exists in an airflow. The absolute pressure, velocity, and temperature just upstream from the wave are 207 kPa, 610 m s, and −17 8 C, respectively. Calculate the pressure, velocity, temperature, and sonic velocity just downstream from the shock wave.
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Related Book For 
Fox And McDonald S Introduction To Fluid Mechanics
ISBN: 9781119721024
10th Edition
Authors: Robert W. Fox, Alan T. McDonald, John W. Mitchell
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