A normal shock wave exists in an airflow. The absolute pressure, velocity, and temperature just upstream from

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A normal shock wave exists in an airflow. The absolute pressure, velocity, and temperature just upstream from the wave are \(207 \mathrm{kPa}, 610 \mathrm{~m} / \mathrm{s}\), and \(-17.8^{\circ} \mathrm{C}\), respectively. Calculate the pressure, velocity, temperature, and sonic velocity just downstream from the shock wave.

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Fox And McDonald's Introduction To Fluid Mechanics

ISBN: 9781118912652

9th Edition

Authors: Philip J. Pritchard, John W. Mitchell

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