If, through a normal shock wave in air, the absolute pressure rises from 275 to (410 mathrm{kPa})

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If, through a normal shock wave in air, the absolute pressure rises from 275 to \(410 \mathrm{kPa}\) and the velocity diminishes from 460 to \(346 \mathrm{~m} / \mathrm{s}\), what temperatures are to be expected upstream and downstream from the 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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