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Air flows steadily through an adiabatic turbine, entering at 1.4 MPa, 600°C, and 178 m/s and...

Air flows steadily through an adiabatic turbine, entering at 1.4 MPa, 600°C, and 178 m/s and leaving at 150 kPa, 200°C, and 210 m/s. The inlet of the turbine is 105 cm2 . Assume that air is an ideal gas with constant specific heat. Given CP = 1.013 kJ/kgK. Estimate: i) the mass flow rate of the air ii) the power output of the turbine, in kW

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