1.5 kg of gas flows through gas turbine unit from its initial pressure and temperature 600 kN/m2 and 1300 K respectively and exhausts at a pressure of 102 kN/m2

m2 and a temperature of 600 k to the atmosphere. The atmospheric pressure and temperature are 100 kN/m2 and 298K. Calculate availability at the entrance to the gas turbine and exhaust of the gas turbine.

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