Advanced Thermodynamics (MCE753) Brayton Cycle write a working EES code for the following problem: A gas-turbine power plant operates on the regenerative Brayton cycle, and the pressure ratio across the compressor varies between 5 to 9. 12.6 kg/s of air enters the compressor at 100 kPa and 30C, whose isentropic efficiency is 80 percent. The hot combustion gases leaving the turbine are used to increase the air temperature that leaves the compressor by 150C. A 0.2 kg/s of diesel fuel with a heating value of 42,000 kJ/kg is burned in the combustion chamber with a combustion efficiency of 97 percent. The combustion gases enter the turbine, whose isentropic efficiency is 85 percent. Determine (a) the effectiveness of the regenerator, (b) the net power output and the back-work ratio, (c) the thermal efficiency, (d) the second-law efficiency of the plant, and also determine (e) the second-law efficiencies of the compressor, the turbine, and the regenerator, and (f) the rate of the energy flow with the combustion gases at the regenerator exit.