Physics, 18.12.2019 06:31 bellajuliet13

5. combustion gases enter a gas turbine at 627 c and 1.2 mpa at a rate of 2.5 kg/s and leave at 527 c and 500 kpa. it is estimated that heat is lost from the turbine at a rate of 20 kw. using air properties for the combustion gases and assuming the surroundings to be at 25 c and 100 kpa, determine

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5. combustion gases enter a gas turbine at 627 c and 1.2 mpa at a rate of 2.5 kg/s and leave at 527...

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