Part geometry has a significant effect upon the overall safety of components.

Both plates are $60mm$ wide $($dimension $"$b$")$ and $5mm$ thick, but the hole $"d"$ is $12mm,$ the radius $"R"$ is $6mm,$ and the dimension $"c"$ is $40mm.$

With an applied load of $P=2500+xYZ$ Newtons:

Determine the maximum stress for each plate. $(5$ marks$)$

Determine the Factor of Safety for each ALUMINUM plate for the following tempers:

$1100-07075-02024-$T$4(3)$

Neatly summarize your findings in a concise table. $(4)$