A convergent-divergent nozzle with an exit area to throat, Mechanical Engineering

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A convergent-divergent nozzle with an exit area to throat

Question: A convergent-divergent nozzle with an exit area to throat area ratio of 3 is supplied with air from a reservoir in which the pressure is 350 kPa. The air from the nozzle is discharged into another large reservoir. It is found that the flow leaving the nozzle exit is directed inward at an angle of 4° to the nozzle centerline. The velocity on the nozzle exit plane is supersonic. What is the pressure in the second reservoir?

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Mechanical Engineering: A convergent-divergent nozzle with an exit area to throat

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Mechanical Engineering: A convergent-divergent nozzle with an exit area to throat

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