Using $"$ K $"$ and $"$ n $"$ from Table $2\mathrm{.}2$ and Equation $2\mathrm{.}11,$ make a table of the stress $($MPa$)$ for the given strains for the following materials. The columns should be "Material", $"lon=0\mathrm{.}05","lon=0\mathrm{.}1","lon=0\mathrm{.}2","lon=0\mathrm{.}4",$ and $"lon=0\mathrm{.}8".$ The rows should be: $1112$ CR$,1045$ HR$,4135$ CR$,4340$ annealed, $304$ annealed, Ti$-6$Al$4$ V annealed $20,$ Ti$-6$Al$-4$V annealed $800,6061-O,6061-T6,$ and $7075-$O$.$