For the turbocharged engine operating steadily under the condition specified in Fig. 2, answer the following questions by assuming that there are no frictional losses, turbine and compressor are the adiabatic kind, and the exhaust gas from the engine cylinder is simply composed of carbon dioxide. (c) What is the fuel flow rate in the engine cylinder? (d) What is the mass flow rate of the fluid at station (d)? (e) What is the power output from the turbine? (f) What is the temperature of the air at the compressor exit (station (b))? (g) What is the density ratio of air across the compressor? Figure 2: A turbocharged engine with specified flow conditions (not to scale)