The compressor turbine of a simple gas turbine each have

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Reference no: EM13629200

The compressor turbine of a simple gas turbine each have isentopic efficiencies of 90%. The compressor pressure ratio is 12. The minimum and maximum temperatures are 290K and 1400K, respectively. Determine:

(a) the net work per unit mass of air flowing in kJ/kg
(b) the heat rejected per unit mass of air flowing in kJ/kg
(c) the thermal efficiency of the same quantities evaluated for an ideal cycle

Reference no: EM13629200

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