A beam carrying a uniform load is simply supported with the supports set back a distance a from the ends as shown in the figure. The bending moment at x can be found from summing moments to zero at section x :
\sum M=M+\frac{1}{2} w(a+x)^{2}-\frac{1}{2} w l x=0
or
M=\frac{w}{2}\left[l x-(a+x)^{2}\right]
where w is the loading intensity in \mathrm{lbf} / \mathrm{in} . The designer wishes to minimize the necessary weight of the supporting beam by choosing a setback resulting in the smallest possible maximum bending stress
(a) If the beam is configured with a=2.25 in, l=10 in, and w=100 \mathrm{lbf} / in, find the magnitude of the severest bending moment in the beam.
( b ) Since the configuration in part ( a ) is not optimal, find the optimal setback a that will result in the lightest-weight beam.