Your selection was a gas-turbine power plant operating on an ideal Brayton cycle and according to the manufacturing datasheets it has the following specifications: pressure ratio of 14.77. The gas temperature is 350K at the compressor inlet and 1500 K at the turbine inlet. A Under the assumption of standard air, perform the following: 1. Gas temperature of the compressor and the turbine exits, 2. Back-work ratio, 3. Thermal efficiency using the formula Nth = Wnet and by formula nth = 1 - din 1 discuss any (k-1)/k > differences and explain it.

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