Air flows in a converging-diverging nozzle. The nozzle throat area is 50 cm2. The total pressure...

Air flows in a converging-diverging nozzle. The nozzle throat area is 50 cm2. The total pressure at the nozzle inlet is 1 MPa. The total pressure at the nozzle exit is 650 kPa. The Mach number at the nozzle exit is 0.70. Find the nozzle exit area.

51.7 cm2

84.2 cm2

35.6 cm2

54.7 cm2

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Expert Solution

samet mamat answered 4 weeks ago

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