Solved: Thermal efficiency of gas-turbine cycle, Mechanical Engineering

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Thermal efficiency of gas-turbine cycle

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Q: An ideal gas turbine cycle with many stages of compression and expansion and a regenerator of 100 percent effectiveness has an overall pressure ratio of 10. Air enters every stage of compressor at 290 K, and every stage of turbine at 1200 K. The thermal efficiency of this gas-turbine cycle is.

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Mechanical Engineering: Thermal efficiency of gas-turbine cycle

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Mechanical Engineering: Thermal efficiency of gas-turbine cycle

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