Using the following tabulated data plot the stress$-$strain curve $($use Excel$)$ and determine the elastic modulus $($E$),0\mathrm{.}2\%$ offset YS$,\%$elongation, $\%$RA and the tensile strength. $D_0=0\mathrm{.}505-$inches, $D$ at max. load $=0\mathrm{.}454-$inches, final diameter $=0\mathrm{.}284-$inches. Calculate the true stress at fracture.

$\backslash$table$[[$Gage Length, inches,Load, lbs$,],[2,0],[2\mathrm{.}00167,5000],[2\mathrm{.}0034,10,000],[2\mathrm{.}00425,12,000],[2\mathrm{.}0047,13,000],[2\mathrm{.}0052,14,000],[2\mathrm{.}0065,13,900],[2\mathrm{.}0079,15,000],[2\mathrm{.}0118,18,000],[2\mathrm{.}0156,20,000],[2\mathrm{.}056,26,000],[2\mathrm{.}472,39,000],[2\mathrm{.}82,32,000]]$

Table $1.$ Tensile Test Results