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Beam Load Calculator

Enter your beam span, support condition, load type, and cross-section dimensions to instantly find the support reactions, maximum bending moment, maximum shear force, mid-span deflection, and maximum bending stress. Choose between metric and imperial units and switch between a simply-supported beam and a cantilever at any time.

Your details

Simply supported: pinned at both ends (equal reactions for symmetric loads). Cantilever: one end fixed, the other free.
Point load is applied at the midspan of a simply-supported beam or at the free end of a cantilever. UDL is spread evenly over the full span.
Clear span between supports (or fixed wall to free end for a cantilever).
m
Point load in kN (or kip), or total UDL intensity in kN/m (or kip/ft).
kN
Selects the elastic modulus E used for deflection. Override with a custom value if your material differs.
Width b of the rectangular cross-section (b x d).
mm
Depth d of the rectangular cross-section (b x d). The neutral axis is at d/2.
mm
Max shear forceDeflection OK (L/360+)
5

Largest internal shear force anywhere along the beam.

Reaction at A5
Reaction at B5
Max bending moment12.5
Max deflection0.3858
Max bending stress5.556
Second moment of area (I)337,500,000
Span/deflection ratio12,960
Reaction A5
Reaction B5
Max shear5
Max moment12.5
12,960 L/d
Excessive<240Borderline240-360OK360+
06.2512.5035
Position along beam (m)
  • Bending moment (kN-m)
  • Deflection (mm)

Simply-supported beam with central point load: results calculated.

  • Max shear force: 5.000 kN. Max bending moment: 12.500 kN-m.
  • Maximum deflection at the critical point: 0.386 mm.
  • The span-to-deflection ratio is L/12960, which is within the typical L/360 serviceability limit.
  • Maximum bending stress in the outer fibre: 5.56 MPa. Compare this to the material allowable stress.

Next stepThese results assume elastic, isotropic behaviour and a rectangular cross-section. For I-beams, T-beams, or composite sections, use the actual second moment of area (I) and section modulus (Z = I / y_max) in the formulas shown in the steps panel.

How the beam load calculator works

This calculator applies classical elastic beam theory (Euler-Bernoulli) to find the support reactions, internal forces, and deflection of two common structural configurations. For a simply-supported beam, equilibrium of vertical forces and moments at the supports gives the reactions; for a cantilever, the fixed end must resist both the full shear and the full moment. Internal shear and bending moment are then found from equilibrium at every cross-section. Deflections use the closed-form integration of the bending moment equation (the double-integration or moment-area methods), which assume the beam is linearly elastic and that cross-sections remain plane. The bending stress at the outer fibre is found from the flexure formula: sigma = M * y / I, where y = d/2 for a rectangular section.

Simply supported vs cantilever: what changes

A simply-supported beam (pinned at A, roller at B) develops equal reactions of P/2 for a central point load, or wL/2 for a UDL. The maximum moment is at midspan. A cantilever (fixed at A, free at B) resists the entire load at the fixed end: the full force P or wL as a shear reaction, plus a moment equal to P*L (point) or wL^2/2 (UDL). Because the cantilever is only supported at one end, it deflects far more for the same span, load, and stiffness: P*L^3/(3EI) vs P*L^3/(48EI) for a central point load, a 16-fold difference. This is why cantilevered elements such as balconies and overhangs require deeper or heavier sections than equivalent simply-supported spans.

Point load vs uniform distributed load (UDL)

A point load concentrates all the force at one location, creating an abrupt change in the shear force diagram and a triangular bending moment diagram that peaks at the load. A UDL spreads the load evenly along the span, producing a parabolic bending moment diagram with a lower peak for the same total force. For example, a simply-supported 5 m beam carrying 10 kN as a central point load has a maximum moment of 12.5 kN-m, while the same 10 kN spread as a 2 kN/m UDL gives only 6.25 kN-m at midspan. Choosing the right load model matters: distributed self-weight and floor loads are best represented as UDLs, while columns, wall loads, and machinery footings are modelled as point loads.

Checking your results: deflection limits and stress

Two checks govern most beam designs. The strength check compares the calculated maximum bending stress (sigma = M*y/I) against the material allowable bending stress: 165 MPa for common structural steel (A36/S275), 138 MPa for 6061-T6 aluminium, and typically 7-15 MPa for structural timber depending on grade. The serviceability check compares L/delta_max against the code limit: L/360 for floors under live load and L/240 under total load are the most widely used thresholds. If either check fails, you need a deeper section (larger I), a shorter span, a different material, or a change in support condition. The steps panel shows the exact numbers substituted into each formula.

Typical beam deflection limits (serviceability)

ApplicationDeflection limitSpan/delta ratioNotes
Floor beams (live load)L/360360 Typical residential and commercial floors
Floor beams (total load)L/240240 Total dead + live load
Roof beams (live load)L/360360 Sloped roofs
Roof beams (total, no ceiling)L/180180 Flat or low-slope roofs without plaster
Roof beams (total, plaster ceil.)L/240240 Ceilings susceptible to cracking
Cantilever beams (live load)L/180180 Half of simply-supported limit by convention
Lintels and headersL/600600 To protect brittle masonry above

Common span-to-deflection limits from building codes and structural engineering practice. L is the beam span.

Frequently asked questions

What is a beam support reaction?

A support reaction is the upward force (and, for a fixed support, the moment) that a support must provide to keep the beam in static equilibrium. For a simply-supported beam with a central load P, each support provides P/2. For a cantilever, the fixed wall provides the entire load as a shear force plus a bending moment equal to P times the span.

What is the deflection limit for a floor beam?

Most building codes specify L/360 for live load deflection and L/240 for total (dead plus live) load deflection in floor beams, where L is the beam span. These limits prevent cracking in non-structural finishes and ensure the floor does not feel bouncy. Cantilevers use L/180 for live load by convention. This calculator shows the span/deflection ratio so you can compare it directly against whichever limit applies.

How do I calculate the bending moment in a beam?

For the standard cases covered here: simply-supported beam with a central point load, M_max = P*L/4; with a UDL, M_max = w*L^2/8. For a cantilever with a point load at the free end, M_max = P*L; with a UDL, M_max = w*L^2/2. For other load positions or multiple loads, use the principle of superposition or free-body diagrams at successive cross-sections.

What is the second moment of area and why does it matter?

The second moment of area (also called moment of inertia) I quantifies how a cross-section resists bending. For a solid rectangle, I = b*d^3/12. Doubling the depth d quadruples I, which halves the bending stress and reduces deflection by a factor of four. This is why beams are almost always oriented with the larger dimension vertical, and why I-beams and H-sections are so efficient: they place the most material as far from the neutral axis as possible.

Can I use this calculator for steel I-beams?

Yes, but you need to use the actual I value for the section (from a steel section tables, not the rectangular formula). Look up your section (e.g., W8x31 or UB203x102) in the manufacturer or code section tables to get the strong-axis I and the elastic section modulus Z = I/y_max. Then cross-check the deflection formula manually using those values. The reference table in this calculator shows the most common allowable deflection limits.

What does L/360 mean?

L/360 means the maximum allowable deflection is the beam span divided by 360. For a 5 m beam, that is 5000/360 = 13.9 mm. The ratio is a practical limit developed from observation: when deflections exceed L/360 under live load, many floor finishes crack and occupants notice the movement. Tighter limits (L/480 or L/600) apply where very stiff surfaces such as stone tile or brittle masonry are present.

Sources

Written by Aisha Rahman, PEng Structural Engineer · Toronto, Canada

Structural Engineer and PEng with 16 years designing and verifying load-bearing systems across Canada's most demanding construction environments.

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