Beam Deflection Calculator

Calculate maximum deflection of a beam under load.

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Beam Deflection

Euler-Bernoulli · 3 beam types · 2 load types

Instructions — Beam Deflection Calculator

1

Pick beam and load type

Choose between simply supported, cantilever, or fixed-fixed beam. Select point load (center) or uniform distributed load (UDL).

2

Enter load and span

Point load in kN or distributed load in kN/m. Span length in meters between supports (or from fixed end to free end for cantilevers).

3

Pick material and section

Select material (steel, aluminum, concrete, wood) — sets E automatically. Enter moment of inertia I in cm⁴ from the manufacturer\'s section table or your own calculation.

Code limit warning: if deflection exceeds L/360 (floor) or L/180 (cantilever), a warning appears. Real designs go to a structural engineer.
Disclaimer: this is an estimate using simple Euler-Bernoulli theory. Production design needs full code-compliant analysis.
Disclaimer: This calculator provides estimates only and does not replace structural engineering analysis. Building code compliance (IBC, Eurocode, NDS) requires checks for moment, shear, bearing, deflection, and lateral stability under all load combinations. Always consult a licensed structural engineer for real construction.

Formulas

Beam deflection follows from Euler-Bernoulli theory: the bending moment along the beam is related to curvature via M = EI(d²y/dx²). Solving for boundary conditions gives closed-form expressions for maximum deflection in each common case.

Simply Supported + Point Load
$$ \delta_{max} = \frac{PL^3}{48EI} $$
Maximum at center of span. P at midspan, L is full span.
Simply Supported + UDL
$$ \delta_{max} = \frac{5wL^4}{384EI} $$
Uniform load w (per unit length). The L⁴ dependence means doubling span gives 16× deflection.
Cantilever + Point Load
$$ \delta_{max} = \frac{PL^3}{3EI} $$
P at free end. 16× more deflection than simply supported with the same P, L, E, I.
Cantilever + UDL
$$ \delta_{max} = \frac{wL^4}{8EI} $$
Uniform load along the cantilever length. Used for balcony floor loading, eaves.
Fixed-Fixed + Point Load
$$ \delta_{max} = \frac{PL^3}{192EI} $$
Both ends fixed (no rotation). Four times stiffer than simply supported.
Code Limits
$$ \delta_{allow} = \frac{L}{360}\,(\text{floor}) \;\;\; \frac{L}{240}\,(\text{roof}) \;\;\; \frac{L}{180}\,(\text{cant}) $$
IBC and ACI deflection limits for serviceability — prevents plaster cracks, ponding, and occupant discomfort.

Reference

Young\'s modulus by material
MaterialE (GPa)E (Mpsi)Typical use
Steel (mild)200–21029.0I-beams, columns, joists
Stainless steel19328.0Corrosive environments
Aluminum 6061-T66910.0Light framing, aerospace
Concrete (normal)20–403.0–5.8Slabs, beams
Concrete (high-strength)40–505.8–7.2Towers, bridges
Wood (pine)9–141.3–2.0Joists, rafters
Wood (Douglas fir)11–131.6–1.9Structural lumber
Wood (oak)12–141.7–2.0Beams, flooring

Common section properties

Standard structural sections come with published I values. For custom rectangles, use I = bh³/12.

Steel I-beams (W shapes)
SectionI (cm⁴)
W6×12972
W8×243373
W10×337035
W12×268783
W14×3414609
W18×5033710
Lumber (S4S, US)
SectionI (cm⁴)
2×6 (1.5"×5.5")879
2×8 (1.5"×7.25")2018
2×10 (1.5"×9.25")4173
2×12 (1.5"×11.25")7503
4×6 (3.5"×5.5")2050

Note: nominal lumber sizes (2"×6") are 1.5"×5.5" actual. I-beam data from AISC tables. Always confirm from current section property tables for design work.

Article — Beam Deflection Calculator

Beam Deflection: Theory, Formulas, and Code Limits

Beam deflection is the vertical displacement of a loaded beam from its straight position, calculated as δ = PL³/(48EI) for a simply supported beam with a point load at center. The deflection depends strongly on span (L³ or L⁴), modestly on load (P), and inversely on material stiffness (E) times the section's moment of inertia (I). Building codes typically limit deflection to L/360 for floors and L/240 for roofs to prevent cracking and discomfort.

Beam deflection is one of the oldest problems in engineering. Galileo first attempted it in 1638, Bernoulli and Euler solved it analytically in the 18th century, and the resulting Euler-Bernoulli beam theory remains the working foundation of structural design. Modern finite element methods refine the answers for complex cases, but the closed-form solutions still cover the common ones — and they live inside this calculator.

What is beam deflection?

When a beam supports a load, internal stresses develop that bend the beam from straight to curved. The maximum vertical displacement is the deflection, measured perpendicular to the original beam axis. For typical structures, deflections are small — millimeters or fractions of an inch — but they grow rapidly with longer spans or weaker sections.

Deflection matters for three reasons. First, excessive deflection cracks finishes: drywall, plaster, tile, and brick veneer all fail well before structural collapse. Second, deflection affects function: sagging floors feel uncomfortable, doors stick, and sloping floors collect water. Third, deflection is a stiffness check — a beam that bends too easily under service load may also vibrate excessively or fail under sudden impact loads.

Did you know

The Tacoma Narrows Bridge collapse (1940) was not primarily a deflection failure — it was an aeroelastic flutter problem. But every modern long-span bridge now uses deflection and oscillation studies that trace directly back to Euler-Bernoulli theory and its successor methods.

The beam deflection formula

The fundamental Euler-Bernoulli beam equation is:

Beam deflection formulas
δ = PL³/(48EI) simply supp. + point
δ = 5wL⁴/(384EI) simply supp. + UDL
δ = PL³/(3EI) cantilever + point
δ = wL⁴/(8EI) cantilever + UDL

The L³ and L⁴ terms dominate. Doubling the span gives 8× more deflection for a point load and 16× more for a uniform load, holding everything else constant. This is why beam tables are organized around span — most structural design starts there.

E (Young's modulus) and I (second moment of inertia) appear as the product EI, called flexural rigidity. Doubling either halves deflection. In practice, designers usually adjust I (by picking a deeper section) because changing material rarely makes economic sense.

Beam types and supports

The boundary conditions at the ends of a beam determine which formula applies. The three most common in residential and light commercial construction:

  1. Simply supported. Two supports, both allowing rotation. The standard residential floor joist sitting on two walls. Maximum deflection occurs at midspan.
  2. Cantilever. One end fixed, the other end free. Balconies, eaves, overhanging decks. Cantilevers deflect 16× more than simply supported beams with the same load and span — they are structurally inefficient but architecturally necessary.
  3. Fixed-fixed. Both ends restrained against rotation. Achieves a quarter of the simply-supported deflection. Hard to build truly fixed connections — most real beams are somewhere between simply supported and fixed.
Simply supported
δ = PL³/48EI
baseline reference
┃═
Cantilever
δ = PL³/3EI
16× the deflection

Beam deflection limits in building codes

International Building Code (IBC), ACI 318 for concrete, and the National Design Specification (NDS) for wood all specify deflection limits as a fraction of span:

  • L/360 = floor beams with plaster or drywall finish
  • L/240 = roof beams without plaster ceiling
  • L/480 = floor beams with stiff finishes (tile, stone)
  • L/180 = cantilevers
  • L/600 = some glass-walled facades
  • H/400 = wind-loaded building lateral drift

For a 4 m floor beam (L = 4000 mm), the L/360 limit is 11.1 mm — slightly less than half an inch. A 6 m span allows 16.7 mm. Cantilevers, with their L/180 limit, allow twice the deflection of a similar simply-supported beam but are still tightly controlled.

Tip

Deflection is a serviceability limit, not a strength limit. A beam can meet code for moment, shear, and bearing while still deflecting excessively under service loads. Both checks are required, and deflection often governs long-span beams of light material.

Young's modulus by material

E is a material property, measured by tensile testing. It does not depend on cross-section, only on the substance. Typical values for structural materials:

  • Steel (A36/A992) = 200–210 GPa (29 Mpsi)
  • Stainless steel = 193 GPa (28 Mpsi)
  • Aluminum 6061-T6 = 69 GPa (10 Mpsi)
  • Concrete (normal) = 20–40 GPa (varies with mix)
  • Wood (softwood) = 9–14 GPa (varies with species, moisture)
  • Wood (hardwood) = 11–18 GPa

Concrete and wood have wide ranges because their stiffness depends on factors that vary in practice. Concrete E grows with age, compressive strength, and density. Wood E depends on species, moisture content, grain direction, and grade. Building codes give modulus values matched to material grades, which engineers must use rather than averages.

Moment of inertia for common sections

I (the second moment of inertia, or second moment of area) measures a section's geometric resistance to bending. For a rectangular cross-section with width b and depth h in the bending direction:

I = bh³ / 12

The h³ dependence is the key insight. A 2×8 lumber (1.5" × 7.25" actual) has I = 1.5 × 7.25³ / 12 = 47.6 in⁴ in strong-axis bending. A 2×10 (1.5" × 9.25") has I = 99.0 in⁴ — more than double, just from depth. Steel I-beams put as much material as possible at the top and bottom (the flanges) where the bending stresses are highest, giving them excellent I-to-weight ratios.

Reducing beam deflection in design

If a beam deflects too much, designers have a hierarchy of fixes, ordered roughly from cheapest to most expensive:

Shortening span is dramatic

Halving the span reduces deflection by a factor of 8 (point load) or 16 (UDL). Adding one intermediate support to a 12-foot beam usually cuts deflection more than going up two lumber sizes — and it costs less.

  1. Add intermediate supports. Cuts span, drops deflection dramatically.
  2. Increase section depth. Doubling h gives 8× the I.
  3. Switch to a stiffer section type. I-beam, glulam, LVL, steel.
  4. Composite construction. Bonding a steel beam to a concrete slab makes the slab structurally active, doubling effective I.
  5. Camber. Build the beam with an initial upward curve that flattens under load. Common in long-span steel.
  6. Stiffer material. Hardly ever the right answer — switching from wood to steel is a 14–22× E increase but a major cost change.

Beam deflection calculation pitfalls

  1. Wrong E value. Wood E depends on species, moisture, and grade. Concrete E grows with time. Always use a code-published value matched to the actual material.
  2. Wrong I orientation. A 2×10 joist on its side (1.5" deep) has I = 9.25 × 1.5³ / 12 = 2.6 in⁴ — about 1/40 of its strong-axis I. Orientation matters.
  3. Ignoring composite effects. A steel beam with concrete topping is much stiffer than the bare beam. Standard formulas understate stiffness in these cases.
  4. Skipping load combinations. Real beams must satisfy deflection limits under several load combinations (dead, live, snow, wind). The worst case is not always the largest single load.
  5. Assuming Euler-Bernoulli holds. Short, deep beams (depth/span > 1/10) develop significant shear deformation that the standard formulas miss. Use Timoshenko theory or finite elements for those.
  6. Forgetting long-term deflection. Concrete and wood creep — deflections grow with time under sustained load by 50–300%. Long-term limits are tighter than instantaneous limits.

FAQ

Beam deflection is the displacement of a beam from its straight position under load. The amount depends on load magnitude, span length, material stiffness (E), and the section's moment of inertia (I). Building codes limit deflection to prevent cracks, sagging, and discomfort, typically to L/360 for floors and L/240 for roofs.
Use the formula matched to your boundary conditions. For a simply supported beam with a point load at center: δ = PL³/(48EI). For a uniform load: δ = 5wL⁴/(384EI). For a cantilever with end load: δ = PL³/(3EI). E is Young's modulus (in Pa), I is the second moment of inertia (in m⁴), L is span (m), P is point load (N) or w is distributed load (N/m).
International Building Code limits: L/360 for floors, L/240 for roofs without plaster ceiling, L/480 for floors with plaster, L/180 for cantilevers. For a 4 m floor beam, the limit is 4000/360 = 11.1 mm. These prevent cracks in drywall, water ponding on roofs, and human discomfort.
Young's modulus E is a material's stiffness — stress per unit strain. Steel: ~200 GPa, aluminum: ~70 GPa, concrete: 20–40 GPa, wood: 9–14 GPa. Higher E means less deflection for the same load and geometry. Doubling E halves deflection — but you can't simply pick stiffer material; you usually change the cross-section instead.
Moment of inertia I describes a cross-section's resistance to bending. For a rectangle: I = bh³/12, with h in the bending plane. A deep beam (large h) is far stiffer than a wide one. Steel sections (W10, I-beams) have published I values; for lumber, calculate from actual dimensions (not nominal).
Four options, in order of effectiveness: (1) increase depth h — deflection drops as h³; (2) shorten span L — deflection drops as L³ or L⁴; (3) reduce load; (4) use stiffer material. Adding intermediate supports is usually the cheapest fix; doubling the section depth is the next-best.
Deflection refers specifically to a beam's lateral movement under transverse load. Deformation is the general term — any change in shape under stress (compression, tension, bending, twisting). Beam deflection is one type of bending deformation; axial stretching and shear distortion are others.
It uses Euler-Bernoulli beam theory, which assumes small deflections, linear-elastic material, no shear deformation, and constant cross-section. Real engineering must also check moment capacity, shear, lateral-torsional buckling, bearing stresses, vibration, fatigue, and code-required load combinations. Always consult a licensed structural engineer for real construction.