Question 13.14: The cantilever beam shown in Fig. 13.16 tapers along its len...
The cantilever beam shown in Fig. 13.16 tapers along its length so that the second moment of area of its cross section varies linearly from its value I_0 at the free end to 2I_0 at the built-in end. Determine the deflection at the free end when the cantilever carries a concentrated load W.

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Choosing the origin of axes at the free end B we have, from Eq. (13.10)
x_B\left(\frac{dv}{dx} \right) _B – x_A\left(\frac{dv}{dx} \right) _A – (v_B-v_A) = \int_{A}^{B}{\frac{M}{EI}x } \ dx (13.10)
x_A\left(\frac{dv}{dx} \right) _A – x_B\left(\frac{dv}{dx} \right) _B – (v_A-v_B) = \int_{B}^{A}{\frac{M}{EI_X}x } \ dx (i)
in which I_x , the second moment of area at any section X, is given by
I_X = I_0\left(1+\frac{x}{L} \right)
Also (dv/dx)_A = 0, x_B = 0, v_A = 0 so that Eq. (i) reduces to
v_B = \int_{0}^{L}{\frac{M_x}{EI_0 (1+\frac{x}{L} )} } dx (ii)
The geometry of the M/EI diagram in this case will be complicated so that the analytical approach is most suitable. Therefore since M = −Wx, Eq. (ii) becomes
v_B = – \int_{0}^{L}{\frac{Wx^2}{EI_0 (1+\frac{x}{L} )} } dx
or
v_B = – \frac{WL}{EI_0} \int_{0}^{L}{\frac{x^2}{L+x} } dx (iii)
Rearranging Eq. (iii) we have
v_B = – \frac{WL}{EI_0} \left[\int_{0}^{L}{(x-L) \ dx } + \int_{0}^{L}{\frac{L^2}{L+x} \ dx } \right]
Hence
v_B = – \frac{WL}{EI_0} \left[\left(\frac{x^2}{2} – Lx \right) + L^2 \log_e(L-x) \right] _0^L
so that
v_B = – \frac{WL^3}{EI_0} \left(-\frac{1}{2} + \log_e 2 \right)
i.e.
v_B = -\frac{0.19WL^3}{EI_0}