One simple gas turbine cycle Air enters the cycle at 1 bar and 27 C and is boosted to 6 bar with an isenthro-wing efficiency of 85%. The air flows through the combustion chamber and enters the turbine at 360 °C. The hot air expands through the turbine. up to pressure I but with an isenthro-wing efficiency of 80% assume no change in flow rate. Mass due to fuel Calculate the air flow rate at the net power output of 1500kW. The pressure loss at the combustion chamber is 0.08 bar. Answer 42.67