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Engineering, 26.07.2019 20:10 ayoismeisalex

Agas turbine cycle using brayton cycle with both intercooler and regenerators air and split ideal compressor and turbine, enters in the compressor at 14.7 psia and 80 f the pressure ration is 6: 1 and air leaves the combustion chamber at 1540 f. draw ts diagram and cycle sketch and compute the compressor work, turbine work, and thermal efficiency and state of each point of the cycle.

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