$8.$ Combustion gases enter a gas turbine at $627^{\circ} \mathrm{C}$ and $1.2 \mathrm{MPa}$ at a rate of $2.5 \mathrm{~kg} / \mathrm{s}$ and leave at $527^{\circ} \mathrm{C}$ and $500 \mathrm{kPa}$. It is estimated that heat is lost from the turbine at a rate of $20 \mathrm{~kW}$. Using air properties for the combustion gases and assuming the surroundings to be at $25^{\circ} \mathrm{C}$ and $100 \mathrm{kPa}$, determine $(a)$ the actual and reversible power outputs of the turbine, $(b)$ the exergy destroyed within the turbine, and $(c)$ the second-law efficiency of the turbine