Repeat Problem 9.63 assuming a turbine isentropic efficiency of 96% and a compressor efficiency of 95%. Compare your results with those from Problem 9.63.

Problem 9.63

Consider a gas-turbine engine operating with 30 kg/s of air entering at 300 K and a pressure ratio of 12.5. Using an ideal air-standard cycle as a model of this engine, determine the ideal thermal efficiency and the net shaft power delivered to the load. Assume the turbine inlet temperature is 1050 k.

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Oin Qout W out