Given,
Pressure at the inlet turbine "(P_1)=1MPa=10^6 Pa"
Temperature "(T_1)=500^o C"
Outlet pressure "(P_2)=5KPa =5000Pa"
Flow rate "=20kg\/s"
"\\eta =\\frac{h_i -h_f}{h_i - h_f'}"
"=\\frac{3479.1-2560.7}{3479.1-137.75}"
"=0.274"
Output energy "=m(h_1-h_o)"
"=20(3479.1-2560.7) =18368kw"
Output shaft "=18368\\times \\eta"
"=18368\\times 0.274"
"=5032.05 kW"
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