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The compressor pressure ratio is 10 and the turbine inlet

Air enters the compressor of an ideal cold air-standard Brayton cycle at 100 kPa, 300K, with a mass flow rate of 6 kg/s. The compressor pressure ratio is 10, and the turbine inlet temperature is 1400K. For k=1.4, calculate: (a) the thermal efficiency of the cycle (b) the back work ratio (c) the net power developed, in kW

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Mechanical Engineering: The compressor pressure ratio is 10 and the turbine inlet

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