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Air enters a 3600-kW turbine operating at steady state with a mass flow rate of 18 kg/s at 800 C, 3 bar and a velocity of 100 m/s. The air expands adiabatically through the turbine and exits at a velocity of 150 m/s. The air then enters a diffuser where it is decelerated isentropically to a velocity of 10 m/s and a pressure of 1 bar. Employing the ideal gas model, determine

(a) the pressure and temperature of the air at the turbine exit, in bar and C, respectively.

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(b) the rate of entropy production in the turbine, in kW/K.

(c) Show the processes on a T–s diagram.

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