$5\mathrm{.}34$ Use the PARA computer program to determine and plot the thrust specific fuel consumption vs specific thrust for the turboprop engine of Example $5\mathrm{.}7$ for $T_{t4}=1750K$ over the same range of compressor pressure ratios for turbine temperature ratios of $0\mathrm{.}8,0\mathrm{.}7,0\mathrm{.}6,0\mathrm{.}5,0\mathrm{.}4,$ and optimum.