Air enters the compressor of a simple gas turbine at 100 kPa, 25oC, with a volumetric flow rate of 6 m3/s. The compressor pressure ratio is 10 and its isentropic efficiency is 80%. The turbine inlet the pressure is 100 kPa temperature is 1000oC. The turbine has an isentropic efficiency of 88% and the exit pressure is 100 kPa. On the basis of air standard analysis using the PG model, determine
(a) Net power developed, in kW.
(b) The thermal efficiency (ηth) of the cycle,