Determine the deflection curve and the mid-span deflection of the simply supported beam shown in Fig. 15.18(a); the beam has a doubly symmetrical cross-section.
Determine the deflection curve and the mid-span deflection of the simply supported beam shown in Fig. 15.18(a); the beam has a doubly symmetrical cross-section.
The support reactions are each wL/2 and the bending moment, M, at any section Z, a distance z from the lefthand support is
M=-\frac{w L}{2} z+\frac{w z^{2}}{2} (i)
Substituting for M in the second of Eqs. (15.31), we obtain
u^{\prime \prime}=-\frac{M_{y}}{E I_{y y}}, \quad v^{\prime \prime}=-\frac{M_{x}}{E I_{x x}} (15.31)
E I v^{\prime \prime}=\frac{w}{2}\left(L z-z^{2}\right) (ii)
Integrating, we have
E I v^{\prime}=\frac{w}{2}\left(\frac{L z^{2}}{2}-\frac{z^{3}}{3}\right)+C_{1}
From symmetry, it is clear that, at the mid-span section, the gradient v^{\prime}=0. Hence,
0=\frac{w}{2}\left(\frac{L^{3}}{8}-\frac{L^{3}}{24}\right)+C_{1}
which gives
C_{1}=-\frac{w L^{3}}{24}
Therefore,
E I v^{\prime}=\frac{w}{24}\left(6 L z^{2}-4 z^{3}-L^{3}\right) (iii)
Integrating again gives
E I v=\frac{w}{24}\left(2 L z^{3}-z^{4}-L^{3} z\right)+C_{2}
Since v=0 when z=0 (or since v=0 when z=L), it follows that C_{2}=0 and the deflected shape of the beam has the equation
v=\frac{w}{24 E I}\left(2 L z^{3}-z^{4}-L^{3} z\right) (iv)
The maximum deflection occurs at mid-span, where z=L/2 and is
v_{\text {mid-span }}=-\frac{5 w L^{4}}{384 E I} (v)