Beam load calculator

Maximum bending moment, shear and mid-span deflection for a simply-supported beam under uniformly distributed load (UDL). For preliminary checks — not a substitute for code-compliant design.

Beam inputs

m
kN/m
N/mm²
mm⁴
Max bending moment (mid-span)
90.0 kN·m
Max shear (at supports)
60.0 kN
Reaction at each support
60.0 kN
Mid-span deflection
5.4 mm
L / deflection
L / 1,111
Total UDL load
120 kN
Deflection well within typical L/360 serviceability limit.

Formulas (simply-supported beam, UDL)

Reactions: R = wL ÷ 2
Max bending moment: M = wL² ÷ 8
Max shear: V = wL ÷ 2
Mid-span deflection: δ = 5wL⁴ ÷ (384 × E × I)

All formulas assume a prismatic beam with constant EI, an evenly-distributed load along the full span, and small deflections. For point loads, partial UDLs, or continuous beams, the formulas change — use a structural analysis tool.

Typical input values

MaterialYoung's modulus E (N/mm²)
Concrete (M20)22,360
Concrete (M25)25,000
Concrete (M30)27,386
Structural steel200,000
Aluminium69,000
Timber (softwood)9,000 – 12,000

For RCC, IS 456 specifies E = 5000 × √fck (in N/mm²). For a 230×450 mm rectangular beam, I = bd³/12 = 230 × 450³ ÷ 12 ≈ 1.75 × 10⁹ mm⁴.

FAQ

What is the L / 360 rule?

It's a serviceability limit: deflection should be less than span ÷ 360 to avoid visible sag and damage to finishes. For floors with brittle finishes use L/480; for roofs without ceilings, L/240 is often acceptable.

How do I get the moment of inertia?

Rectangular section: I = b × d³ ÷ 12, where b is width and d is depth (both in mm). Standard rolled steel sections (ISMB, ISLB, etc.) have I tabulated in IS 808 / SP 6. For composite sections, compute the equivalent transformed section.

What about self-weight?

Add the beam's self-weight to your UDL. For a 230×450 mm RCC beam: 0.23 × 0.45 × 25 ≈ 2.6 kN/m of self-weight, on top of any imposed load.

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