Air enters the compressor of a simple gas turbine at 95 kPa, 310 K, where it is

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Air enters the compressor of a simple gas turbine at 95 kPa, 310 K, where it is compressed to 800 kPa. Heat is transferred to air in the amount of 1000 kJ/kg before it enters the turbine. For a turbine efficiency of 90%, determine
The thermal efficiency (ηth) of the cycle, and
The fraction of turbine work output used to drive the compressor. Use the PG model for air.
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