Air enters a converging-diverging nozzle with a low velocity at 1.5 MPa and 120oC. If the exit

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Air enters a converging-diverging nozzle with a low velocity at 1.5 MPa and 120oC. If the exit area of the nozzle is 3 times the throat area, determine
The back pressure to produce a normal shock at the exit plane of the nozzle.
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