An exhaust gas at 1.2 MPa and 660 K is expanded in an adiabatic turbine to a final pressure of 161 kPa producing 1,559 k

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An Exhaust Gas At 1 2 Mpa And 660 K Is Expanded In An Adiabatic Turbine To A Final Pressure Of 161 Kpa Producing 1 559 K 1 (23.75 KiB) Viewed 39 times

An exhaust gas at 1.2 MPa and 660 K is expanded in an adiabatic turbine to a final pressure of 161 kPa producing 1,559 kW. The inlet area of the device is 0.2 m2 and the gas velocity at inlet is 38 m/s and at outlet is 25 m/s. Determine the specific volume at outlet in m3/kg to 2 decimal places. Assume the gas constant to be 0.26 (kPa m3)/(kg K) and constant specific heats cp-1,01 kJ/(kg K) and C+0.75 kJ/(kg K).