Engineering
Beam Deflection Calculator
Calculates maximum deflection and bending moment for a simply supported beam with a single center point load — the most common textbook case.
Modulus of Elasticity, E (GPa)
Enter I in m⁴ (e.g. a typical steel I-beam is around 1×10⁻⁵ to 1×10⁻⁴ m⁴). Convert from mm⁴ by dividing by 1×10¹².
Results
Max Deflection
—
Max Bending Moment
—
Formulas
Max Deflection (δ)
δ = PL³ / (48EI)
Maximum downward deflection at midspan
Max Bending Moment (M)
M = PL / 4
Peak internal bending moment, occurring under the load
Load (P)
Applied force in N
Single concentrated point load at the beam center
Length (L)
Span in m
Distance between the two supports
Modulus of Elasticity (E)
Material stiffness in Pa
Converted internally from GPa: 1 GPa = 1×10⁹ Pa
Moment of Inertia (I)
Cross-section property in m⁴
Resistance of the cross-section to bending
Assumptions
Simply supported
The beam rests on two supports that allow free rotation — a pin at one end, a roller at the other.
Center point load
A single concentrated load is applied at the exact midpoint of the span.
Linear elastic material
The material obeys Hooke's law — stress is proportional to strain, with no permanent deformation.
Small deflections: the formulas assume deflection is small relative to span length, so beam curvature does not change the geometry of the load path.
FAQ
Frequently asked questions.
How do you calculate beam deflection for a simply supported beam with a center point load?
For a simply supported beam carrying a single point load P at its midspan, the maximum deflection occurs at the center and is given by δ = PL³ / (48EI), where P is the load in newtons, L is the span length in meters, E is the modulus of elasticity in pascals, and I is the moment of inertia of the beam's cross-section in meters to the fourth power. For example, a 1000 N load on a 2 m steel beam (E = 200 GPa) with I = 1×10⁻⁵ m⁴ produces a deflection of about 0.0833 mm — small because steel is stiff and the moment of inertia is large relative to the load.
What is the formula for maximum bending moment in a center-loaded simply supported beam?
The maximum bending moment for a simply supported beam with a single point load P at midspan is M = PL/4, and it occurs directly under the load at the center of the span. This is the highest internal bending stress point along the beam, so it is the location engineers check first when verifying a beam won't yield or fail under the applied load.
What is modulus of elasticity (E) and why does it matter for deflection?
Modulus of elasticity (also called Young's modulus) measures a material's stiffness — how much it resists elastic (non-permanent) deformation under load. It appears in the denominator of the deflection formula, so a stiffer material (higher E) produces less deflection for the same load and geometry. Typical values are about 200 GPa for structural steel, 69 GPa for aluminum, and roughly 11 GPa for wood, which is why a wood beam deflects far more than a steel beam of identical dimensions under the same load.
What is moment of inertia (I) and how does cross-section shape affect it?
Moment of inertia (technically the second moment of area) describes how a beam's cross-sectional area is distributed relative to its neutral bending axis — the further material is placed from that axis, the higher I becomes and the stiffer the beam is against bending. This is why I-beams and hollow tubes resist bending so efficiently: they concentrate material away from the center. I is usually expressed in m⁴ or mm⁴, and because it is raised to the first power in the denominator of δ = PL³/(48EI), doubling I halves the deflection.
What does 'simply supported' mean, and how is it different from a cantilever or fixed beam?
A simply supported beam rests on two supports — typically a pin support at one end (resists vertical and horizontal movement) and a roller support at the other (resists only vertical movement) — allowing the beam ends to rotate freely under load. This is the most common textbook and real-world case for bridges, floor joists, and shelving. It differs from a cantilever beam (fixed at only one end, free at the other) or a fixed-fixed beam (both ends rigidly clamped), both of which have different deflection and moment formulas because rotation at the supports is restrained.
Why does beam length have such a large effect on deflection?
Deflection is proportional to the cube of the span length (L³) in the formula δ = PL³/(48EI), so even a modest increase in span causes a dramatic rise in deflection. Doubling the length of a beam while keeping the load, material, and cross-section the same increases the deflection eightfold (2³ = 8). This is why longer spans require disproportionately deeper or stiffer beams to keep deflection within safe, serviceable limits.
Last updated: August 17, 2026