EBK FUNDAMENTALS OF AERODYNAMICS
EBK FUNDAMENTALS OF AERODYNAMICS
6th Edition
ISBN: 9781259681486
Author: Anderson
Publisher: MCGRAW HILL BOOK COMPANY
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Chapter 8, Problem 8.6P

Consider the isentropic flow over an airfoil. The freestream conditions correspond to a standard altitude of 10.000 ft and M = 0. 82 . At a given point on the airfoil, M = .0 . Calculate p and T at this point. (Note: You will have to use the standard atmosphere table in Appendix E for this problem.)

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