9.3 A turbine unit receives air at I bar and gas 300K and compresses it adia batically at to 6.2 issor efficiency is bar. The compressor e has a 88% The fuel and the fuel -*3/kg and heating valve of 44186 kJ/kg air ratio is internal 0.017 kJ/kg of air. The turbine efficiency is 90% Calculate the work of turbine and compressor per kg of air Compressed and thermal e fficiency.