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Engineering, 08.04.2020 01:13 J3ak06

Consider a gas turbine with air entering the compressor under the same conditions as in P1 and leaving at a pressure of 1.0 MPa. The maximum temperature is 1100oC. Assume a compressor efficiency of 80%, a turbine efficiency of 85%, and a pressure drop between the compressor and turbine of 15 kPa. Determine the compressor work, turbine work, and cycle efficiency

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Consider a gas turbine with air entering the compressor under the same conditions as in P1 and leavi...
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