Beam Deflection: Simply Supported, Uniform Load

δ=5wL4384EI\delta = \frac{5 w L^{4}}{384 E I}
sig figs

Worked example: 10 kN/m over 5 m → 4.069 mm sag. Press Try an example to run it live, then adjust anything.

Enter your known values, leave one input blank, and solves for the missing one. Tap a variable’s symbol to see what it means, with a typical value. Change any unit and the answer follows.

Where Beam Deflection: Simply Supported, Uniform Load fits

Missing an input?
In this toolkit

See also

Beam Deflection: Simply Supported, Centre Load: Both use maximum deflection and beam span.Cantilever Deflection: End Load: Both use maximum deflection and Young's modulus.Cantilever Deflection: Uniform Load: Both use uniform load per unit length and Young's modulus.Fixed-End Moment: Fixed-Fixed Beam, Uniform Load: Both use uniform load per unit length and beam span.Max Bending Moment: Uniform Load: Both use uniform load per unit length and beam span.Support Reaction: Simple Beam, Uniform Load (R = wL/2): Both use uniform load per unit length and beam span.
3 more relatedMax Bending Moment: Centre Point Load: Both use beam span.Max Moment: Simple Beam, Off-Centre Point Load: Both use beam span.Support Reaction: Simple Beam, Off-Centre Point Load: Both use beam span.
Here the solver did the work. Could you?

Deflection limits →

UniversityMechanics of Materials

Test your skills in the Exam Room: new numbers every attempt. Free lessons for students, no sign-up, just pure learning.

See your Report Card
Learning zone

Beam Deflection: Simply Supported, Uniform Load explained

wδEIL

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

δ=5wL4384EI\delta = \frac{5 w L^{4}}{384 E I}
Where
  • δ\delta= Maximum deflection (m)
  • ww= Uniform load per unit length (N/m)
  • LL= Span (m)
  • EE= Young's modulus (kPa)
  • II= Area moment of inertia (mm⁴)
Revised 16 October 2026
Cite this page

formula.expert. (2026, October 16). Beam Deflection: Simply Supported, Uniform Load Calculator. https://formula.expert/solvers/beam-deflection-uniform-load