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A gas-turbine power plant operating on an ideal Brayton cycle has a pressure ratio of 9....

A gas-turbine power plant operating on an ideal Brayton cycle has a pressure ratio of 9. The gas temperature is 438 K at the compressor inlet and 1582 K at the turbine inlet. Utilizing the air-standard assumptions (A-17 tables), determine (1) The gas temperature at the exit of the compressor K (2) The gas temperature at the exit of the turbine K (3) Work input to the compressor kJ/kg (4) Work output of the turbine kJ/kg (5) Total heat input kJ/kg (6) Net power output kJ/kg (7) The thermal efficiency %

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