Question: Nitrogen enters a convergingdiverging nozzle at 700 kPa and 300 K with a negligible velocity, and it experiences a normal shock at a location where

Nitrogen enters a converging–diverging nozzle at 700 kPa and 300 K with a negligible velocity, and it experiences 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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