Fundamentals of Aerodynamics
Fundamentals of Aerodynamics
6th Edition
ISBN: 9781259129919
Author: John D. Anderson Jr.
Publisher: McGraw-Hill Education
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Chapter 14, Problem 14.3P

Consider a hypersonic vehicle with a spherical nose flying at Mach 20 at a standard altitude of 150,000 ft. where the ambient temperature and pressure are 5 00 ° R and 3 .0 6 lb / ft 2 , respectively. At the point on the surface of the nose located 200 away from the stagnation point, estimate the: (a) pressure, (b) temperature. (c) Mach number, and (d) velocity of the flow.

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