Calculate the velocity of the air at exit from the nozzle

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Reference no: EM131171578

Air at 6.9 bar, 260°C is throtded to 5.5 bar before expanding through a nozzle to a pressure of 1.1 bar. Assuming that the air flows reversibly in steady flow through the nozzle. and that no heat is rejected, calculate the velocity of the air at exit from the nozzle when the inlet velocity is 100 m/s.

Reference no: EM131171578

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Calculate the velocity of the air at exit from the nozzle : Air at 6.9 bar, 260°C is throtded to 5.5 bar before expanding through a nozzle to a pressure of 1.1 bar. Assuming that the air flows reversibly in steady flow through the nozzle. and that no heat is rejected, calculate the velocity of the air at e..

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