Calculate the entropy change of air across the normal shock

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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