Beam Deflection — Simply Supported, Uniform Load
Worked example: 10 kN/m over 5 m → 4.069 mm sag — press Try an example to run it live, then adjust anything.
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Beam Deflection — Simply Supported, Uniform Load explained
The odd-looking 5/384 comes straight from integrating the parabolic moment diagram of a uniformly loaded simply supported beam twice; it works out to 0.013021. A 10 kN/m load on a 5 m span with E = 200 GPa and I = 10⁻⁴ m⁴ sags δ = 5 × 10 000 × 5⁴ ÷ (384 × 200 × 10⁹ × 10⁻⁴) = 0.00407 m, about 4 mm, or L/1230 — a comfortably stiff floor.
Now the fourth power. Going from a 4 m to a 5 m span with everything else unchanged multiplies the deflection by (5/4)⁴ = 2.44, and it is this exponent, not stress, that governs most residential floor framing: the joists are almost always chosen for bounce, not for strength. A useful shortcut is that the uniform-load deflection is 5/8 of the deflection a single mid-span point load of the same total magnitude would cause, so wL total spread out sags less than the same weight concentrated at the middle. Enter w in force per unit length (N/m, kN/m, lbf/ft) and I as a plain number in m⁴; forgetting the tributary width when turning a floor pressure into w is the classic mistake here.
Beam Deflection — Simply Supported, Uniform Load formula
- = Maximum deflection (m)
- = Uniform load per unit length (N/m)
- = Span (m)
- = Young's modulus (kPa)
- = Area moment of inertia (mm⁴)
Missing one of these? Work it out first, then come back
- Maximum deflection — Beam Deflection — Simply Supported, Centre Load
- Uniform load per unit length — Max Bending Moment — Uniform Load, Cantilever Deflection — Uniform Load
- Span — Max Bending Moment — Centre Point Load, Max Bending Moment — Uniform Load
- Young's modulus — Young's Modulus (E = σ/ε), Axial Deformation (δ = PL/AE)
- Area moment of inertia — Bending Stress (σ = Mc/I), Beam Deflection — Simply Supported, Centre Load