A gas turbine cycle has one- stage of compression, with pres sure ratio 25 and isentropic 10 marks efficiency of 82%. The cycle has a two-stages turbine with reheat between the stages and isentropic efficiency of 80% for each stage. Air enters the compressor at 100 kPa, 296 K. The maximum cycle temperature is 1210 °C. The cycle also includes a regenerator with an effectiveness of 75%. C= 1.004 kJ/kg. K . Draw the cycle and the T-s diagram. 2- Find all temperatures in the cycle 3. Calculate the cycle thermal efficiency

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A gas turbine cycle has one- stage of compression, with pres sure ratio 25 and isentropic 10 marks efficiency of 82%. The cycle has a two-stages turbine with reheat between the stages and isentropic efficiency of 80% for each stage. Air enters the compressor at 100 kPa, 296 K. The maximum cycle temperature is 1210 °C. The cycle also includes a regenerator with an effectiveness of 75%. C= 1.004 kJ/kg. K . Draw the cycle and the T-s diagram. 2- Find all temperatures in the cycle 3. Calculate the cycle thermal efficiency

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Anonymous 2025-03-23T20:39:14+05:00 1 Answer 13 views
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    2025-03-24T00:13:24+05:00
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