Beam Deflection Calculator - Supported Beams

Parameters

Calculate beam deflection, bending moment, and reaction forces for simply supported, cantilever, and fixed beams. Includes shear and moment diagrams.

Select beam type

Choose load type

Enter beam dimensions

Input load value

Deflection here follows Euler-Bernoulli beam theory for the support type and load you selected. It does not include the beam's own weight unless you add it as a load, shear deformation, buckling, material defects, connection stiffness or dynamic loading, so have a licensed structural engineer check any design before it is built.

Formulas and sources

Each formula this calculator uses, where it comes from, and what it leaves out. "How it works" shows the same formula with your own numbers.

Simply supported, point load at midspan

Simply supported, point load at midspan

δ = (P × L³) / (48 × E × I)
δ
maximum deflection
P
point load
L
span between supports
E
Young's modulus
I
moment of inertia (second moment of area)

Source: Uses the formula in American Wood Council Design Aid No. 6, Figure 7 [1].

Simply supported, point load off center

Simply supported, point load off center

δ = (P × b × (L² − b²)^(3/2)) / (9√3 × E × I × L), b = the shorter segment

The largest deflection is not under the load but toward the middle of the longer segment.

Source: Uses the formula in American Wood Council Design Aid No. 6, Figure 8, written with the shorter segment [1].

Simply supported, uniform load

Simply supported, uniform load over the whole span

δ = (5 × w × L⁴) / (384 × E × I)
δ
maximum deflection
w
load per unit length (the peak, for a triangular load)
L
span, or the cantilever length
E
Young's modulus
I
moment of inertia (second moment of area)

Source: Uses the formula in American Wood Council Design Aid No. 6, Figure 1 [1].

Simply supported, triangular load

Simply supported, triangular load over the whole span

δ = 0.00652 × w × L⁴ / (E × I)

The coefficient is rounded: the solver gives 0.0065222, so the number shown comes from the solver, not the rounded line.

Source: Based on American Wood Council Design Aid No. 6, Figure 5, with its total load W = w × L ÷ 2 [1].

Simply supported, moment at an end

Simply supported, moment at an end

δ = (M₀ × L²) / (9√3 × E × I)
δ
maximum deflection
M₀
applied moment

Source: Based on American Wood Council Design Aid No. 6, Figure 20: an overhang load applies the same end moment [1].

Cantilever, point load at the tip

Cantilever, point load at the tip

δ = (P × L³) / (3 × E × I)

Source: Uses the formula in American Wood Council Design Aid No. 6, Figure 13 [1].

Cantilever, point load short of the tip

Cantilever, point load short of the tip

δ = (P × a² × (3L − a)) / (6 × E × I)
δ
tip deflection
a
distance from the fixed end to the load

δ is at the tip; a is measured from the fixed end.

Source: Uses the formula in American Wood Council Design Aid No. 6, Figure 14, whose b is the a here [1].

Cantilever, uniform load

Cantilever, uniform load over the whole length

δ = (w × L⁴) / (8 × E × I)

Source: Uses the formula in American Wood Council Design Aid No. 6, Figure 12 [1].

Cantilever, triangular load

Cantilever, triangular load rising to the tip

δ = (11 × w × L⁴) / (120 × E × I)

Zero at the fixed end, w at the free end.

Source: Standard formula; no single publisher.

Cantilever, moment at the tip

Cantilever, moment at the tip

δ = (M₀ × L²) / (2 × E × I)

Source: Standard formula; no single publisher.

Fixed both ends, point load at midspan

Fixed both ends, point load at midspan

δ = (P × L³) / (192 × E × I)

Source: Uses the formula in American Wood Council Design Aid No. 6, Figure 24 [1].

Fixed both ends, uniform load

Fixed both ends, uniform load over the whole span

δ = (w × L⁴) / (384 × E × I)

Source: Uses the formula in American Wood Council Design Aid No. 6, Figure 23 [1].

Any other beam and load

Any other beam and load

E × I × y″ = M(x), integrated twice with the support conditions

Overhanging beams, partial loads, off-center loads on a fixed beam and moments away from an end have no single closed form. Every case, textbook ones included, is solved this way.

Source: Standard method; no single publisher. It reproduces American Wood Council Design Aid No. 6, Figures 20 and 25, for an overhang and an off-center load on a fixed beam [1].

Bending stress

With a section depth

σ = M × (h / 2) / I
σ
bending stress at the outer fiber, in MPa
M
the largest bending moment
h
the section depth
I
moment of inertia (second moment of area)

For a section symmetric about its neutral axis; otherwise enter twice the distance to the outer fiber. The moment, shear and reactions come from the same solution as the deflection.

Source: Standard formula; no single publisher.

Deflection limit

Span ratio = L ÷ δ
L
the span, or twice a cantilever's length
δ
the largest deflection, up or down
L/180
roof member with no ceiling (IBC)
L/240
roof member over a nonplaster ceiling (IBC)
L/360
floor member under live load, or roof over a plaster ceiling (IBC)
L/480, L/600, L/1000
tighter limits set by your design standard

The check passes when δ is at most L ÷ n for the limit you pick. For a cantilever, L is twice its length. The ratio is rounded down, so a beam just over a limit never reads as passing. The IBC limits are for live load.

Source: The three code limits and the cantilever rule are those of the International Building Code's Table 1604.3, live load, and its footnote i (2012 edition read) [2]. The tighter limits name no code; no publisher.

Material moduli

With a material chosen

Steel
200 GPa
Aluminum
70 GPa
Concrete
30 GPa, about M35 concrete by IS 456; an M20 concrete is about 22 GPa
Wood (pine)
10 GPa, clear wood at 12% moisture; pines run 8.2 to 13.7 GPa

Representative values. A typed modulus is used only with Custom.

Source: Steel's 200 kN/mm² and concrete's E = 5,000 √fck are IS 456's [3]. Aluminum is within 3% of MIL-HDBK-5J's 6061-T6 and 7075-T6 [4], and pine is mid-range in the USDA Wood Handbook's Table 5-3a [5].

Sources

  1. American Wood Council (American Forest & Paper Association). Beam Design Formulas with Shear and Moment Diagrams, Design Aid No. 6, Figures 1, 5, 7, 8, 12, 13, 14, 20, 23, 24 and 25. 2007.
  2. International Code Council (ICC). International Building Code, section 1604.3, Serviceability, and Table 1604.3, Deflection limits, with footnote i. 2012 edition.
  3. Bureau of Indian Standards (BIS). IS 456:2000, Plain and Reinforced Concrete, Code of Practice, clauses 5.6.3, 6.2.3.1 and 9.3; Tables 2, 5 and 9. Fourth revision, July 2000.
  4. US Department of Defense. MIL-HDBK-5J, Metallic Materials and Elements for Aerospace Vehicle Structures, Tables 2.3.1.0(c2), 3.6.2.0(b1), 3.7.6.0(b1) and 5.4.1.0(b). January 31, 2003.
  5. USDA Forest Service, Forest Products Laboratory. Wood Handbook: Wood as an Engineering Material (FPL-GTR-282), Table 5-3a, modulus of elasticity. 2021.

What this calculator does not cover

  • This solves a straight, uniform, linear-elastic beam under one static load at a time. It does not include its own weight unless you enter it, shear deformation, lateral-torsional or local buckling, moving or dynamic loads, or support settlement.
  • An overhanging beam is checked against the span between its supports, not the overhang.
  • Deflection limits for later IBC editions, ACI 318, TMS 402 or crane runways were not read; set the limit your work is held to.

Sources checked on .

Help

Quick Start Guide

  1. Select beam type: Choose from simply supported, cantilever, fixed-fixed, or overhanging.
  2. Choose load type: Select point load, uniform distributed load, triangular, or moment.
  3. Enter beam dimensions: Input length and specify the unit (meters, feet, inches, or millimeters).
  4. Input load value: Enter the magnitude and unit of the applied load.
  5. Specify material properties: Enter Young's modulus and moment of inertia, or select a predefined material.
  6. View results: See the maximum deflection, its span ratio and whether it passes your deflection limit, plus the bending moment, the reactions and, with a section depth, the bending stress.

Frequently Asked Questions

Excessive deflection can crack finishes, jam doors, or be visually unsettling. Building codes limit deflection (e.g., L/360) to keep floors and finishes serviceable; strength is checked separately.

Related Calculators

Last updated