Question

Ex. 8.12.3 : A gas turbine of 800 kW capacities takes the
air at 1.01 bar and 15°C. The pressure ratio of the cycle
is 6 and marimum temperature is limited to 700 °C. A
regenerator of 75 % effectiveness is added in the plant
to increase the overall efficiency of the plant. The
pressure drop in the combustion chamber is 0.15 bars as
well as in the regenerator is also 0.15 bars. Assuming
the isentropic efficiency of the compressor 80 % and the
turbine 85 % determine the plant thermal efficiency.
Neglect the mass of the fuel.​

Answer 1

Answer:

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Explanation: