EBK FUNDAMENTALS OF AERODYNAMICS
EBK FUNDAMENTALS OF AERODYNAMICS
6th Edition
ISBN: 9781259681486
Author: Anderson
Publisher: MCGRAW HILL BOOK COMPANY
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Chapter 9, Problem 9.3P

Equation ( 8 . 8 0 ) does not hold for an oblique shock wave, and hence the column in Appendix B labeled p 0 , 2 / p 1 cannot be used, in conjunction with the normal component of the upstream Mach number, to obtain the total pressure behind an oblique shock wave. On the other hand, the column labeled p 0 , 2 / p 0 , 1 can be used for an oblique shock wave, using M n , 1 . Explain why all this is so.

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