The temperature in the reservoir of a supersonic wind tunnel is 519R. In the test section, the

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The temperature in the reservoir of a supersonic wind tunnel is 519°R. In the test section, the flow velocity is 1385 ft/s. Calculate the test-section Mach number. Assume the tunnel flow is adiabatic.

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Fundamentals of Aerodynamics

ISBN: 978-0070016798

2nd Edition

Authors: J. Anderson

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Question Posted: Dec 09, 2010 03:24 AM

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The temperature in the reservoir of a supersonic wind tunnel is 519R. In the test section, the

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Fundamentals of Aerodynamics

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