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Mathematics, 04.03.2020 03:13 rayraye

Air at 3.4 bar, 530 K, and a Mach number of 0.4 enters a converging–diverging nozzle operating at steady state. A normal shock stands in the diverging section at a location where the Mach number is Mx=1.8. The flow is isentropic, except where the shock stands. The air behaves as an ideal gas with k=1.4

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Air at 3.4 bar, 530 K, and a Mach number of 0.4 enters a converging–diverging nozzle operating at st...

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