Hot combustion gases enter a gas turbine at 0.8 MPa and 0.538 m3/kg at a rate...

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Mechanical Engineering

Hot combustion gases enter a gas turbine at 0.8 MPa and 0.538m3/kg at a rate of 2.1 kg/s, and exit at 0.1 MPa and2.29 m3/kg. Heat is lost from the turbine to thesurroundings at a rate of 150 kW and the internal energy decreases904 kW in the process. What is the power output of the gas turbine?(Assume no change in velocity or elevation across the turbine.)

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4.2 Ratings (552 Votes)
In above problem all the values are given in SI unitsie massflow rate in kgs m Internal energy in Js u Pressure in Pa p Specific volume m3kg v Heat lost    See Answer
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