o Air enters the compressor of a stationary gas turbine engine steady at 100kPa and 5...

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o Air enters the compressor of a stationary gas turbine engine steady at 100kPa and 5 m/s. The engine features a pressure ratio of 10:1, and is designed to induce a maximum temperature of 1400K. assuming the cold air - standard, determine the following; (a) The temperature and pressure at all state points (T=300.15K, T2-579.5K, T3-1400K, T=725.1K) (b) The net power output (2307.2kW) (c) The required mass flow rate of the fuel (Assuming the engine runs on pure ethanol) (0.173kg of fuel per sec). (d) The thermal efficiency of the engine (efficiency=48.2% o Air enters the compressor of a stationary gas turbine engine steady at 100kPa and 5 m/s. The engine features a pressure ratio of 10:1, and is designed to induce a maximum temperature of 1400K. assuming the cold air - standard, determine the following; (a) The temperature and pressure at all state points (T=300.15K, T2-579.5K, T3-1400K, T=725.1K) (b) The net power output (2307.2kW) (c) The required mass flow rate of the fuel (Assuming the engine runs on pure ethanol) (0.173kg of fuel per sec). (d) The thermal efficiency of the engine (efficiency=48.2%