Engineering, 14.04.2020 17:21 danetth18

A gas turbine operating on a real Brayton cycle has inlet air at 300 K and 100 kPa. The compressor operates at 20:1 pressure ratio and has an isentropic efficiency of 81%. The turbine inlet is at 1700 K and the turbine has an isentropic efficiency of 93%. If the mass flowrate of air through the turbine is 6 kg/s, find the net output power, the thermal efficiency, and the turbine exhaust temperature.

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A gas turbine operating on a real Brayton cycle has inlet air at 300 K and 100 kPa. The compressor o...