Air at V1 = 800 m/s, p1 = 100 kPa, and T1 = 300 K passesthrough a normal shock
Chapter 11, Problem 11.34(choose chapter or problem)
Air at V1 = 800 m/s, p1 = 100 kPa, and T1 = 300 K passesthrough a normal shock. Calculate the velocity V2, temperature T2,and pressure p2 after the shock. What would be the values of T2 andp2 if the same velocity change were accomplished isentropically?
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