An open cycle gas turbine has a single stage compressor and a single stage expander incorporating a heat exchanger. The air suction temperature is 17 degree Celsius and the pressure1 bar. For an overall pressure ratio o f 4.5 and the shaft output of 4000kW the mass flow is 40kg/s. if the thermal ratio of the heat exchanger is 0.6 and the isentropic efficiency of the compressor is 0.84 calculate the isentropic efficiency of the gas turbine for a plant thermal efficiency of 0.29. Take for air y=14, Cpa=1.005 kJ/kg K for gas y=1.365, Cpg=1.07 kJ/kg K
An open cycle gas turbine has a single stage compressor and a single stage expander incorporating a heat exchanger. The air suction temperature is 17 degree Celsius and the pressurel bar. For an overall pressure ratio of 4.5 and the shaft output of 4000kW the mass flow is 40kg/s. if the thermal ratio of the heat exchanger is 0.6 and the isentropic efficiency of the compressor is 0.84 calculate the isentropic efficiency of the gas turbine for a plant thermal efficiency of 0.29. Take for air y=1.4, Cpa=1.005 kJ/kg K for gas y=1.365, Cpg=1.07 kJ/kg K
An open cycle gas turbine has a single stage compressor and a single stage expander incorporating a heat exchanger. The
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An open cycle gas turbine has a single stage compressor and a single stage expander incorporating a heat exchanger. The
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