Solved: Air flowing at 60 kPa, 240 K, and a Mach number of
Chapter 12, Problem 79P(choose chapter or problem)
Problem 79P
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 , 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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