Please answer the first 3 parts. ASAP mm-mTUma34.LP FOMHPm.3,M*CKK OcondHLConsider a cogenerative GT/ST combined power plant (e g., see the figure above). The following data are provided:Steam turbine plant internal power PST-60 MW, Qond97 MW, Q-65 MW, organic efficiency n.=0.95, heat recovery steamgenerator. T,-423.15KGas turbine plant compressor p, = 1 bar, T, = 293 K, B,-10, polytropic exponent m=1.473; turbine: polytropic exponentm=1.279, T,=1325.15K, burner. n=0.97,n=0.97, fuel. H-42500 kJ/kg,Fluids air (k = 1.4, R= 287 J/kgK, c = 1004.5J/kgK), burned gas (k' = 1.335, R'=293 J/kgK, c=1168 J/kgK)iST190801) The specific work of the compressor and the temperature T,Evaluate:2) The specific work of the gas turbine and the temperature T,3) The heat power Q, provided by the gases to the steam in the heat recovery steam generator, as well as the mass flow rate ofburned gases4) The air-to-fuel ratio 'a' and the mass flow rates of air and fuel in the gas turbine plant5) The net output power of the plant and the overall efficiency of the plant (assume, for the cogenerative steam turbine plant, anequivalent burner efficiency ne0.9)

Combined cogeneration gas turbine and steam turbine plant In this plant gas turbine and steam…

Eluids air (k = 1.4, R = 287 J/kgK, C, = 1004.5J/kgK), burned gas (K' = 1.335. * K,1168 J/kgK) ms m-mTu m. 3 LP FG HP m. 8, M* MTU IK Ocond C T HL Consider a cogenerative GT/ST combined power plant (eg., see the figure above). The following data are provided. Steam turbine plant internal power P generator. T,-423.15K Gas turbine plant compressor m-1.279, T,-1325.15K, burner n,=0.97.nm0.97 , fuel. H,-42500 kJ/kg, (ST 60 MW, Qond=97 MW, Q65 MW, organic efficiency n.=0.95, heat recovery steam = 1 bar, T, = 293 K. B-10, polytropic exponent m=1.473; turbine: polytropic exponent %3! Evaluate: 1) The specific work of the compressor and the temperature T, 2) The specific work of the gas turbine and the temperature T, 1904 3) The heat power Q, provided by the gases to the steam in the heat recovery steam generator, as well as the mass flow rate of burned gases 4) The air-to-fuel ratio 'a' and the mass flow rates of air and fuel in the gas turbine plant 5) The net output power of the plant and the overall efficiency of the plant (assume, for the cogenerative steam turbine plant, an equivalent burner efficiency ne0.9)