Physics, asked by tarun4496, 1 year ago

A gas-turbine 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. determine (a) the gas temperature at the exits of the compressor and the turbine, (b) the back work ratio, and (c) the thermal efficiency

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Answered by nitesh2k2

0

b number is the answer

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