A large stationary Brayton cycle gas turbine power plant deliver output of 100 MW to an electric generator, minimum temperature in the cycle is 300 K and maximum temperature in the cycle is 1600 K, minimum pressure is 100 KPa and compressor pressure ratio is 14:1, calculate power output of turbine, and what portion of turbine output is required to drive the compressor. What is thermal efficiency of the cycle?
Repeat the above problem, when the isentropic efficiencies of compressor and turbine are 85% and 88% respectively.
Repeat the above problem with the use of regenerator having efficiency of 75%.
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