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ONLY DO PART B: Gas A expands through an adiabatic turbine. The inlet stream flows in at 1 0 0 bar and 6 0 0

ONLY DO PART B: Gas A expands through an adiabatic turbine. The inlet stream flows in at 100 bar and 600 K while the outlet is at 20 bar and 445 K.(Part A) Calculate the work produced by the turbine. The following data are available for gas A: The ideal gas heat capacity for this process: Cp=30.0+0.02T where Cp is in J/mol*K and T is in K. PvT data have been fit to the following equation P(v-b)=RT+(a*P^{2})/T Wherea=0.001(m^{3}*K)/(bar*mol)andb=8*10^{-5}(m^{3}/mol)(Part B) Redo part A with a different EOS (eg. cubic EOS with different attributes...)

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