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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
written 5.5 years ago by
teamques10
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• modified 2.3 years ago |
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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