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Hot combustion gases enter a gas turbine at 8mpa and 1500 k

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Reference no: EM13625331

Hot combustion gases enter a gas turbine at .8Mpa and 1500 K at a rate of 2.1 kg/s and exit at .1 Mpa and 800 K. If heat lost from the turbine to the surroundings at a rate of 150 kj/s find the power output of the gas turbine using constant and variable specific heat. (assume exhaust gases are the same as properties of air.

Reference no: EM13625331

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