Learning topic
Bending
Learn beam bending from Q–M diagrams to flexural and shear stress, neutral axis, flexural rigidity EI, slope, deflection, and strength and stiffness checks.
Bending is a deformation mode in which the longitudinal axis of a member becomes curved under transverse loads or applied moments. A typical structural member working in bending is a beam.
Internal force resultants
In transverse bending, the beam sections carry a bending moment $M$ and a shear force $Q$. They are determined by the method of sections and represented by diagrams along the beam axis. Detailed construction of $Q$ and $M$ diagrams is covered in the corresponding child topic.
Normal stresses
The bending moment produces normal stresses: part of the cross-section is in tension and another part is in compression. Between them lies the neutral axis, where normal stress is zero in the classical simple-bending model.
For simple bending of a beam within the linear-elastic model, normal stress varies linearly with distance from the neutral axis:
$$\sigma_x(y)=-\frac{My}{I}.$$
The maximum absolute stress at an extreme fiber is:
$$|\sigma_{\max}|=\frac{|M|y_{\max}}{I}=\frac{|M|}{W},\qquad W=\frac{I}{y_{\max}}.$$
- $M$ — bending moment;
- $I$ — second moment of area about the neutral axis;
- $y$ — distance from the neutral axis;
- $y_{\max}$ — distance to the relevant extreme fiber;
- $W$ — section modulus.
The sign of $\sigma_x$ depends on the sign convention for $M$ and $y$; one side of the section is in tension and the other in compression.
Shear stresses
The shear force $Q$ produces shear stresses whose distribution depends on the cross-sectional shape. In classical beam theory, they are evaluated using the Zhuravsky formula.
For transverse bending, the shear stress at a point of the cross-section is determined by the Zhuravsky formula:
$$\tau=\frac{QS}{Ib}.$$
- $Q$ — shear force at the section;
- $S$ — first moment of the cut-off part of the area about the neutral axis;
- $I$ — second moment of area of the entire section about the neutral axis;
- $b$ — local section width at the level where $\tau$ is evaluated.
At a free upper or lower boundary of a solid section, $S$ tends to zero and therefore $\tau$ is zero. For a rectangular section, the maximum shear stress occurs at the neutral axis.
Beam deformation
Under load, the beam axis becomes an elastic curve. The main kinematic quantities are transverse deflection $w$ and cross-section rotation $\theta$. Resistance to curvature is characterized by the flexural rigidity $EI$.
In classical linear-elastic bending theory, curvature of the deflected beam axis is related to bending moment by:
$$\kappa=\frac{1}{\rho}=\frac{M}{EI},$$
where the sign of the right-hand side depends on the adopted conventions for bending moment and deflection.
For small rotations, curvature is approximately:
$$\kappa\approx w''(x).$$
Therefore, the differential equation of the elastic curve is often written as:
$$EI\,w''(x)=M(x),$$
or with a minus sign according to the chosen sign convention.
- $E$ — Young's modulus;
- $I$ — second moment of area;
- $EI$ — flexural rigidity;
- $w$ — transverse deflection;
- $\rho$ — radius of curvature.
The calculator below uses the equivalent relation $M=EI/\rho$.
Strength and stiffness
Beam design normally includes a stress check at critical sections and a check of deflections or rotations. Excessive deflection may make a structure unserviceable even when the stresses remain within safe limits.
Section structure
The child topics successively cover internal forces and $Q$–$M$ diagrams, normal and shear stresses, deflections and rotations, the differential equation of the elastic curve, and the initial-parameter method. The geometric properties $I$ and $W$ are treated in a separate section on plane cross-sections.
About this topic
Bending is a deformation mode characterized by the curvature of a beam's longitudinal axis under transverse loading. This section covers pure bending, transverse bending, and direct bending in symmetric cross-sections. Learn the internal force generation theory for shear force Q and bending moment M, along with differential relationships between load intensity, shear force, and bending moment.