Air enters the compressor of a gas turbine at 100 kpa 300 k

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Reference no: EM13625014

Air enters the compressor of a gas turbine at 100 kPa, 300 K, and a volumetric flow rate of 5.0 m3/s. The air is compressed in two stages to 1200 kPa, with intercooling to 300 K between the stages at a pressure of 350 kPa. The turbine inlet temperature is 1400 K and the expansion occurs in two stages, with reheat to 1340 K between the stages at a pressure of 350 kPa. The compressor and turbine stage efficiencies are 87% and 85%
respectively. Determine:

a) the thermal efficiency of the cycle,

b) the back work ratio,

c) the net power developed, in kW.

Reference no: EM13625014

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