A standing normal shock occurs in air that is flowing at a Mach number of 1.8. (a)
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A standing normal shock occurs in air that is flowing at a Mach number of 1.8.
(a) What are the pressure, temperature, and density ratios across the shock?
(b) Compute the entropy change for the air as it passes through the shock.
(c) Repeat part (b) for flows at \(M=2.8\) and What pattern do you see?
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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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