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Compressor and turbine efficiencies

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Reference no: EM131044608

1 A simple cycle stationary gas turbine has compressor and turbine efficiencies of 0.85 and 0.9, respectively, and a compressor pressure ratio of 20. Determine the work of the compressor and the turbine, the net work, the turbine exit temperature, and the thermal efficiency for 20 °C ambient and 1200 00 turbine inlet temperatures.

Reference no: EM131044608

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