A normal shock is traveling into still air ( (14.7 mathrm{psia}) and (520^{circ} mathrm{R}) ) at a
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A normal shock is traveling into still air ( \(14.7 \mathrm{psia}\) and \(520^{\circ} \mathrm{R}\) ) at a velocity of 1800 \(\mathrm{ft} / \mathrm{sec}\).
(a) Determine the temperature, pressure, and velocity that exist after passage of the shock wave.
(b) What is the entropy change experienced by the air?
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Related Book For
Fundamentals Of Gas Dynamics
ISBN: 9781119481690
3rd Edition
Authors: Robert D Zucker, Oscar Biblarz
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