Show that Eq. 7.68 gives the rate of heating in terms of the surface pressure change for
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Show that Eq. 7.68 gives the rate of heating in terms of the surface pressure change for the shock boundary layer interaction.
Eq. 7.68
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Related Book For
Fundamentals Of Modern Unsteady Aerodynamics
ISBN: 9783030607760,9783030607777
3rd Edition
Authors: Ülgen Gülçat
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