For Nos, $36-38$: The $6-$meter cantilever beam shown in the figure is loaded with a uniform load of $4k\frac{N}{m}$ and s end with a point load of $10kN.$

The maximum tensile flexural stress for the cantilever beam is $q,$ MPa.

$($a$)16\mathrm{.}25$

$($b$)24$

$($c$)25$

The maximum compressive flexural stress for the cantilever beam is $q,$ MPa.

$16\mathrm{.}25$

$($b$)24$

$($c$)25$

where is the location of the maximum compressive flexural stress?

$($a$)$ Free End

$($b$)$ Fixed End

$($C$)2\mathrm{.}5m$ from the free end

$($d$)2\mathrm{.}5m$ from the fixed end