Compressible Flow
A converging–diverging nozzle operates at steady state. Air as an ideal gas with k = 1.4 enters the nozzle at 500 K, 6 bar, and a Mach number of 0.3. The air flows isentropically to the exit plane, where a normal shock stands. The temperature just upstream of the shock is 380.416 K. Determine the back pressure, in bar.
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