Knowing that beam AB is in equilibrium under the loading shown,

a$)$ The value of the shearing force at x$=0\mathrm{.}05$m is $\_\_\_\_\_$kN$.$

b$)$ The value of the moment at x$=0\mathrm{.}05$m is $\_\_\_\_\_$kN$-$m$.$

c$)$ The value of the shearing force at x$=0\mathrm{.}35$m is $\_\_\_\_\_$kN$.$

d$)$ The value of the moment at x$=0\mathrm{.}35$m is $\_\_\_\_\_$kN$-$m$.$

e$)$ The value of the shearing force at x$=0\mathrm{.}55$m is $\_\_\_\_\_$kN$.$

f$)$ The value of the moment at x$=0\mathrm{.}55$m is $\_\_\_\_\_$kN$-$m$.$

g$)$ The magnitude of the flexural stress on the top of the beam at x$=0\mathrm{.}55$m is $\_\_\_\_\_$MPa.

h$)$ The magnitude of the flexural stress at the centroid of the beam at x$=0\mathrm{.}55$m is $\_\_\_\_\_$MPa.

i$)$ The magnitude of the flexural stress on the bottom of the beam at x$=0\mathrm{.}55$m is $\_\_\_\_\_$MPa.

j$)$ In the original overall problem statement, the beam is oriented such that it is loaded along its "strong axis".

$$For this problem, load the beam along its "weak axis".

$($Simply rotate the cross$-$section $90$ degrees$).$

The magnitude of the flexural stress on the top of the beam at x$=0\mathrm{.}55$m is $\_\_\_\_\_$MPa.

k$)$ The maximum flexural stress in the beam is $\_\_\_\_\_$MPa.

l$)$ The maximum flexural stress in the beam occurs at x$=\_\_\_\_\_$m$.$