(1) Calculate the partial pressures of A and B in the gas phase.

Problem 2 A turbine operating on compressed air in a steady state produces 1 kW of work. The inlet and exit conditions are 300 kPa, 300 K and 200 kPa, 250K, respectively. Find the required mass flow rate of air. Assuming the process is adiabatic and the changes of kinetic and potential energy are ignored.