Cantilever Beam Deflection Calculator
Calculate maximum deflection and slope for cantilever beams under point, uniform, or moment loads.
Cantilever Deflection Is Highly Sensitive to Length and Section Depth
A cantilever is fixed at one end and free at the other, so bending moment and deflection build toward the fixed support under transverse loading. For an end point load P, the free-end deflection is δ=PL³/(3EI) and slope is θ=PL²/(2EI). For a uniform load w over the entire beam, free-end deflection is wL⁴/(8EI).
Flexural rigidity EI combines material stiffness E with geometric stiffness I. The strong L³ or L⁴ dependence means a modest increase in span can cause a large deflection increase. The formulas assume small deflection, linear elasticity, and Euler-Bernoulli beam behavior.
| Symbol | Meaning | Why it appears / units |
|---|---|---|
| P | End point load | N. |
| w | Uniform load intensity | N/m. |
| L | Cantilever length | m. |
| EI | Flexural rigidity | N·m². |
The fixed end usually carries the largest bending moment, while the free end has the largest deflection in these simple load cases. Stress and deflection should both be checked because serviceability can govern before material yield.
Use scaling to test a cantilever result. Increasing E or I must reduce deflection, while increasing the applied load must increase it. For an end-load case, doubling L should multiply δ by eight. If the calculator trend violates one of those relationships, recheck the selected load case, support condition, and units.
Worked Examples
Common Mistakes
Support conditions change moment distribution and deflection coefficients dramatically.
Because I contains length to the fourth power, mm⁴-to-m⁴ conversion errors are severe.
Euler-Bernoulli theory can underestimate deflection when shear deformation is important.
Frequently Asked Questions
Formula Explorer connections
Interpretation: This engineering-physics relationship connects load, material property, geometry, deformation or system response. Assumption: Confirm material linearity, geometry, support conditions and safety convention. Small deformation, elastic behavior and ideal loading are common assumptions.