A gas turbine cycle has a single compression with pressure ratio of 18, and has isentropic efficiency of 80%. The air en

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A gas turbine cycle has a single compression with pressure ratio of 18, and has isentropic efficiency of 80%. The air en

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A gas turbine cycle has a single compression with pressure ratio of 18, and has isentropic efficiency of 80%. The air enters the compressor at 95 kPa, 27°C. The cycle has two stages of expansion, with a reheat between the stages. Air enters the first stage at 1300°C and exits the reheat at 1050°C. The cycle also includes a regenerator with an effectiveness of 76%.Calculate the compressor work,turbine work and the thermal efficiency
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