Beam Handbook

Simply supported beam with symmetric overhangs

Reactions

F_1 = F_2 = \Large \frac{qL}{2}

Shear Force

V(x) = \begin{cases} -qx & \text{for}   x \le \large \frac{L-s}{2} \\ -q(x-\Large \frac{L}{2}\normalsize) & \text{for}   \large \frac{L-s}{2} \normalsize < x \le \small L-\large \frac{L-s}{2} \\ -q(x+L) & \text{for}   x > \small L-\large \frac{L-s}{2} \end{cases}

-V_A = V_D = \Large \frac{q (L-s)}{2}

V_B = -V_C = \Large \frac{qs}{2}

Bending Moments

M(x) = \begin{cases} -\large \frac{1}{2} \normalsize qx^2 & \text{for}   x \le \large \frac{L-s}{2} \\ -\large \frac{1}{2} \normalsize q(x^2-Lx+L\Large\frac{L-s}{2}\normalsize) & \text{for}   \large \frac{L-s}{2} \normalsize < x \le \small L-\large \frac{L-s}{2} \\ -\large \frac{1}{2} \normalsize q(x^2-2Lx+L^2) & \text{for}   x > \small L-\large \frac{L-s}{2} \end{cases}

M_E = M_I = -\Large \frac{1}{8}\normalsize qL(L-s);  \text{for}  x = \large \frac{L-s}{2} \normalsize = \small L- \large \frac{L-s}{2}

M_G = \Large \frac{1}{2} \normalsize qL \Large (\frac{Ls}{2} \normalsize - \Large \frac{L^2}{4}) \normalsize;  \text{for}  x = \large \frac{L}{2}

Diagramas-1c
Shear and bending moment diagrams

It can be shown that the relationship between L and s that minimizes bending moments, i.e., -M_E = M_G , is:

s =f(L) : -M_E = M_G

s = \Large \frac{2}{2+\sqrt{2}} \normalsize L

The distance e that marks the separation between zero moments at points F and H of the central span is:

e = \sqrt{2Ls-L^2}

Where:

M_F = M_H = 0

x_F = \Large \frac{L-e}{2}

x_H = \Large \frac{L+e}{2}

Continuous beam with overhangs

Characterization of a continuous beam under a distributed load with n sections, 2 symmetric overhangs, n-2 interior spans, and n-1 reactions.

L = d_n = \sum_{i=0}^{n} s_i

d_k = \sum_{i=0}^{k} s_i

Reactions

Since this is a statically indeterminate problem, as an approximation, it is assumed that each reaction supports half the load of each adjacent span, except for the reactions next to the overhangs, which will support the total overhang load plus half of the adjacent span load.

R_i(x) = \begin{cases} q(s_0+ \Large \frac{s_1}{2}\normalsize) & \text{for}   i = 0 \\ q(\Large \frac{s_i+s_{i+1}}{2}\normalsize)  & \text{for}   i \in [1, n-2] \in \mathbb{N} \\ q(\Large \frac{s_{n-1}}{2}\normalsize +s_n) & \text{for}   i = n-1 \end{cases}

Shear Force

The subscript k denotes the calculation section.

k = \begin{cases} 0 & \text{for left overhang}   \\ \in [1, n-1] \in \mathbb{N} & \text{for interior spans}   \\ n & \text{for right overhang}   \end{cases}

V_k(x) = \begin{cases} -qx & \text{for}   k = 0 \\ -qx+\sum_{i=0}^{k-1} R_i & \text{for}   k \in [1, n-1] \in \mathbb{N} \\ -q(x+L) & \text{for}   k = n \end{cases}

Bending Moments

M_k(x) = \begin{cases} -\large \frac{1}{2} \normalsize qx^2 & \text{for}   k = 0 \\ -\large \frac{1}{2} \normalsize qx^2+x\sum_{i=0}^{k-1} R_i - \sum_{i=0}^{k-1} R_i d_i  & \text{for}   k \in [1, n-1] \in \mathbb{N} \\ -\large \frac{1}{2} \normalsize q(x^2-2Lx+L^2) & \text{for}   k = n \end{cases}

The maximum moment occurring at the center of each span can be calculated as:

M_k(x_k) = -\large \frac{1}{2} \normalsize qx_k^2+x_k\sum_{i=0}^{k-1} R_i - \sum_{i=0}^{k-1} R_i d_i 

Where:

x_k = d_k - \Large \frac{s_k}{2}

Diagramas multi
Shear and bending moment diagrams

Does your structure have complex geometries or dynamic loads?

These simplified formulas are valid for pre-sizing and standard cases; they have limits.

At Atreydes Engineering, we validate non-linear cases in critical structures, complex joints, or fatigue using Finite Element Analysis (FEA) to ensure optimization and safety.

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