🏗️ Civil & Structural

Beam Deflection Calculator

Calculate max deflection and bending moments for simply supported and cantilever beams instantly.

Point Loads
Uniform Distributed Loads
Solid Mechanics

🏗️ Quick Beam Deflection Estimator

Max Deflection (δ max)
Max Bending Moment (M)

Beam Deflection Formulas

Beam deflection is a measure of the displacement of a structural element under a load. The calculation varies depending on the beam's supports and the type of load applied.

Simply Supported, Center Point Load (P)
δ = (P × L³) / (48 × E × I)
Simply Supported, Uniform Load (w)
δ = (5 × w × L⁴) / (384 × E × I)
Cantilever, End Point Load (P)
δ = (P × L³) / (3 × E × I)

Frequently Asked Questions

How is beam deflection calculated for a simply supported beam with a center point load?

The maximum deflection occurs at the center and is calculated as: delta = (P * L^3) / (48 * E * I).

What is beam deflection?

Beam deflection is the vertical displacement of a structural beam from its unloaded position under applied loads. Excessive deflection causes serviceability issues (cracking in finishes, door binding) even if the beam is structurally adequate. Most codes limit deflection to L/360 for live loads and L/240 for total loads, where L is the span length.

What factors affect beam deflection?

Beam deflection depends on: applied load type and magnitude; span length (deflection increases with the cube of span — doubling span increases deflection 8×); moment of inertia (I) of the cross-section (larger I = less deflection); modulus of elasticity (E) of the material (steel deflects less than timber); and support conditions (cantilever deflects 4× more than simply supported for the same loading).

What is the deflection formula for a cantilever beam with point load at the tip?

For a cantilever beam with a point load P at the free end: maximum deflection δ = PL³ / (3EI), occurring at the free end. For a uniformly distributed load w (N/m): δ = wL⁴ / (8EI). Cantilever beams deflect 4 to 5 times more than simply supported beams of the same span and loading — this is a critical design consideration.

What is the modulus of elasticity (E) for common structural materials?

Modulus of elasticity (Young's Modulus): Structural Steel — 200 GPa; Aluminium alloy — 69 GPa; Concrete — 20–30 GPa (varies with grade); Timber along grain — 8–15 GPa (species dependent); Carbon fibre composite — 70–300 GPa. Steel is 3–10× stiffer than timber, which is why steel beams deflect far less for the same cross-section.

What is the moment of inertia and why does it matter for beam design?

The second moment of area (I), or moment of inertia, measures a cross-section's resistance to bending. For a rectangular section: I = b×h³/12, where b is width and h is depth. Doubling the depth increases I by 8×, reducing deflection 8×. This is why I-beams (wide flange sections) are efficient — most material is placed far from the neutral axis where it contributes most to stiffness.

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