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).