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Treating the combustion gases as air

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Reference no: EM13874690

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.

2091_treating the combustion gases.jpg

Reference no: EM13874690

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