A convergent–divergent nozzle with an exit area to throat area
ratio of 3 is supplied with...
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Mechanical Engineering
A convergent–divergent nozzle with an exit area to throat arearatio of 3 is supplied with air from a reservoir in which thepressure is 350 kPa. The air from the nozzle is discharged intoanother large reservoir. It is found that the flow leaving thenozzle exit is directed inward at an angle of 4° to the nozzlecenterline. The velocity on the nozzle exit plane is supersonic.What is the pressure in the second reservoir?
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