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Combustor Gas turbine :Compressor- Turbine Air inlet- 7 Heat-recovery steam generator Turbine Vapor cycle W) Pump Condenser C

Consider Figure 1 above. The following information is given a. p- 14.7 psia, T 540 °R b. P/p1 12.0 С. Т,-2500,R d, P,-14.7 p

please solve the problem, it is thermo-design problem, please do in details, thank you

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Combustoy Am Exhadst ST 6 Ston qurton 2- apouh PuMN o ccoli iven P,.Up7 psia=1.0135 BanNo T) T 0.338 baona haat excharen 1- QSStura. 居こ 0,067947 SS 8639 0, gSㅈ (2571-6-16332) 、NO Wo dora T.-T,006.48 3 138 not fansabl 9- Heat ooded Net Heat oddud * Cu3-2u -|99 と 396489ナ125No Net p pod Ca foton on pin be poblen

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