At some point for air flow in a duct, (p=20 mathrm{psia}, T=500^{circ} mathrm{R}), and (V=500 mathrm{ft} /
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At some point for air flow in a duct, \(p=20 \mathrm{psia}, T=500^{\circ} \mathrm{R}\), and \(V=500 \mathrm{ft} / \mathrm{s}\). Can a normal shock occur at this point?
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Related Book For
Munson Young And Okiishi's Fundamentals Of Fluid Mechanics
ISBN: 9781119080701
8th Edition
Authors: Philip M. Gerhart, Andrew L. Gerhart, John I. Hochstein
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