A gas-turbine power plant operating on an ideal brayton


A gas-turbine power plant operating on an ideal Brayton cycle has a pressure ratio of 6. The gas temperature is 350 K at the compressor inlet and 1450 K at the turbine inlet. Utilizing the air­ standard assumptions, 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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Mechanical Engineering: A gas-turbine power plant operating on an ideal brayton
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