A cantilever beam of length, L, and flexural rigidity, EI, is subjected to an end moment, M, as shown in the figure. The deflection of the beam at x = L/2

1
\(\frac{ML^2}{16EI}\)
2
\(\frac{ML^2}{4EI}\)
3
\(\frac{ML^2}{8EI}\)
4
\(\frac{ML^2}{2EI}\)

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