Thermodynamic problem. I am using the book of Cengel, Y.A., and Boles, M.A. (2008). Thermodynamics: An Engineering Approach. 6th ed. McGraw Hill. Chapter 9 and 10. Analyze Brayton (gas-turbine) cycle problems for simple cycles as well as for cycles including intercooling, reheating, and regeneration. I need to complete the following table. The analysis of the compressors is with direct method and turbines with constant specific heat.

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Using the next diagram answer the following table with the given constants and for the Compressors use the exact method formulas that use enthalpy and Reduced pressures and for the Turbines use specific heat and CP formulas. 9intercool Ireheat lin Estates T1 350 K rp 5 P1 200 kPa cp 1.4 T2s K Wneto 2 MW P2 kPa eff. Reger 0.9 kJ/kg K h2s nc 0.9 T2r nt 0.9 kJ/kg |kJ/kg w comp1 T1 350 K 200 kPa 1300 K h2real P1 T3 K T6 kJ/kg kPa |kJ/kg h3 P3 q intercool T4s K P4 kPa |kJ/kg |kJ/kg h4s wcomp2 T4r K h4r |kJ/kg T5 K h5 kJ/kg Using the next diagram answer the following table with the given constants and for the Compressors use the exact method formulas that use enthalpy and Reduced pressures and for the Turbines use specific heat and CP formulas. 9intercool Ireheat lin Estates T1 350 K rp 5 P1 200 kPa cp 1.4 T2s K Wneto 2 MW P2 kPa eff. Reger 0.9 kJ/kg K h2s nc 0.9 T2r nt 0.9 kJ/kg |kJ/kg w comp1 T1 350 K 200 kPa 1300 K h2real P1 T3 K T6 kJ/kg kPa |kJ/kg h3 P3 q intercool T4s K P4 kPa |kJ/kg |kJ/kg h4s wcomp2 T4r K h4r |kJ/kg T5 K h5 kJ/kg