A gas turbine air- standard cycle operates between a lowpressure of 14.7 Psia and a high pressure of 60 Psia. Thetemperature of the gas at the inlet to the compressor and turbineare 60 and 1000 respectively. If 40,000 ft3 /min. of air enter thecompressor and assuming k=1.41, compute:
a) The theoretical net power output, and
b) The air – standard thermal efficiency
