Tell me which table to use for every part $.$Problem $2(50$ points$)$: Air enters an adiabatic turbine at $\backslash (\backslash$mathbf$\{850\}\backslash$mathbf$\{$~ k P a$\},1200^\{\backslash$circ$\}\backslash$mathrm$\{$C$\}\backslash ),$ with a rate of $\backslash (\backslash$mathbf$\{7$ k g$\}/\backslash$mathrm$\{$s$\}\backslash ),$ and leaves at $\backslash (\backslash$mathbf$\{150$ ~$\}\backslash$mathbf$\{$~ k P a$\}\backslash )$ and $\backslash (\backslash$mathbf$\{700\}\{\}^\{\backslash$circ$\}\backslash$mathrm$\{$C$\}\backslash )$

Part $1)$ Sketch the schematic of this problem; show the boundary of the system and all types of energy crossing the boundary. Write all known values.

Part $2)$ Determine the specific enthalpy at the inlet.

Part $3)$ Determine the specific enthalpy at the exit.

Part $4)$ Determine the change in specific entropy.

Part $5)$ Write the complete form of the entropy balance, and simplify it for this problem. List the assumptions. Obtain the rate of entropy generation during the process. Is this process reversible, irreversible or impossible?