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Unformatted text preview: a. The compressor work b. The turbine work c. The thermal efficiency d. The thermal efficiency if an ideal regenerator was incorporated 3) A gasturbine power plant operating on an ideal Brayton cycle has a pressure ratio of 8. The gas temperature is 300 K at the compressor inlet and 1300 K at the turbine inlet. Assuming a compressor efficiency of 80% and a turbine efficiency 85% determine: a. The back work ratio b. The thermal efficiency c. The turbine exit temperature...
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This note was uploaded on 01/03/2011 for the course MEEN 315 taught by Professor Ramussen during the Fall '07 term at Texas A&M.
 Fall '07
 RAMUSSEN
 Combustion

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