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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Fundamentals Of Gas Dynamics

ISBN: 9781119481690

3rd Edition

Authors: Robert D Zucker, Oscar Biblarz

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