Figure Q6 illustrates a turbocharger system of an internal combustion engine. Note that, for turbocharger system, the turbine drives the compressor. If thirteen percent (13%) of turbine work is lost during its transmission to the compressor, determine; a) the turbine power output, W+= 2.46 [kW] b) The compressor power output, Wc = 2.14 [kW] c) The temperature at the exit of compressor, Tac 443.397 [K] d) the isentropic efficiency of the compressor. = 45.55 [%] Treat exhaust gas and air as ideal gas and take specific heat at constant pressure and specific heat at constant volume as 1.005 kJ/kg.K and 0.718 kJ/kg.K, respectively. Plot T-s diagram for both turbine and compressor for this thermodynamics process. Air 395 C 69C 95 kPa 0.021 kg/s Turbine Compressor Exhaust gas 148 kPa 465 C 0.035 kg/s Figure Q6: Turbocharger system.