Why is the ratio of the velocity at any point downstream of the throat of a supersonic
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Why is the ratio of the velocity at any point downstream of the throat of a supersonic nozzle to the velocity at the throat (where it equals the speed of sound), though dimensionless, not a Mach number?
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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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