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Engineering, 24.11.2021 17:00 bgallman153p71edg

Question 6: Isentropic efficiency of turbine (ideal gas) Air enters the adiabatic turbine with temperature 383 K, pressure 4 bar and exits with temperature 328.1 K, pressure 2 bar. Treat the gas as ideal with 1.008 kJ/kg-K. Determine the isentropic efficiency of the turbine, .

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