For the supersonic flow, show that the area of the integration over the surface is hyperbola. The
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For the supersonic flow, show that the area of the integration over the surface is hyperbola. The chordwise integration process has the upper surface denoted by \(-\mathrm{z}\), and the lower surface by \(+\mathrm{z}\) in 5.64.
Eq 5.64
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Fundamentals Of Modern Unsteady Aerodynamics
ISBN: 9783030607760,9783030607777
3rd Edition
Authors: Ülgen Gülçat
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