Nitrogen enters a converging-diverging nozzle at 620 kPa
Chapter 17, Problem 134P(choose chapter or problem)
Problem 134P
Nitrogen enters a converging-diverging nozzle at 620 kPa and 310 K with a negligible velocity, and it experi-ences a normal shock at a location where the Mach number is Ma = 3.0. Calculate the pressure, temperature, velocity, Mach number, and stagnation pressure downstream of the shock. Compare these results to those of air undergoing a normal shock at the same conditions.
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