Question: Consider an ideal gas-turbine cycle with two stages of compression and two stages of expansion. The pressure ratio across each compressor stage and each turbine

Consider an ideal gas-turbine cycle with two stages of compression and two stages of expansion. The pressure ratio across each compressor stage and each turbine stage is 8 to 1. The pressure at the entrance to the first compressor is 100 kPa, the temperature entering each compressor is 20C, and the temperature entering each turbine is 1100C. An ideal regenerator is also incorporated into the cycle. Determine the compressor work, the turbine work, and the thermal efficiency of the cycle.

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of COMP IC www T T T COMP PP PP3 P6PPgP 80 P 100 kPa 1 10 TT3 20 C T6 Tg 1100C Assume const spec... View full answer

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