Air flowing at 60 kPa, 240 K, and a Mach number of 3.4
Chapter 17, Problem 95P(choose chapter or problem)
Problem 95P
Air flowing at 60 kPa, 240 K, and a Mach number of 3.4 impinges on a two-dimensional wedge of half-angle 8°. Determine the two possible oblique shock angles, βweak and βstrong, that could be formed by this wedge. For each case, calculate the pressure, temperature, and Mach number downstream of the oblique shock.
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