Calculate the entropy change of air across the normal
Chapter 17, Problem 81P(choose chapter or problem)
Problem 81P
Calculate the entropy change of air across the normal shock wave in Problem 17–80.
Problem 17–80
Air enters a normal shock at 26 kPa, 230 K, and 815 m/s. Calculate the stagnation pressure and Mach number upstream of the shock, as well as pressure, temperature, velocity, Mach number, and stagnation pressure downstream of the shock.
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