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Air enters the compressor of an ideal air-standard Brayton cycle at 100kPa, 300 K, with a volumetric flow rate of 7.5 m³/s. The compressor pressure ratio is 10. The turbine inlet temperature is 1400 K. Determine the following: [MO1. MO2. M041 a. The thermal efficiency of the cycle b. The back work ratio c. The net power developed in kW

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