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.

F13.16
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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}

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