Hot combustion gases enter the nozzle of a turbojet engine at 260 kPa, 747°C, and 80...

Hot combustion gases enter the nozzle of a turbojet engine at 260 kPa, 747°C, and 80 m/s, and they exit at a pressure of 85 kPa. Assuming an isentropic efficiency of 92 percent and treating the combustion gases as air, determine (a) the exit velocity and (b) the exit temperature. Answers: (a) 728 m/s, (b) 786 K

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genius_generous answered 1 year ago

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