How It Works

Euler-Bernoulli Beam Theory

The Euler-Bernoulli beam equation describes the relationship between a beam's deflection and the applied load. It assumes that plane sections remain plane and perpendicular to the neutral axis after bending.

EI * d4y/dx4 = w(x)

Where E = elastic modulus, I = moment of inertia, y = deflection, and w(x) = distributed load.

  • Assumptions: Linear elastic material, small deflections, no shear deformation
  • Validity: Best for slender beams where length > 10x depth
  • Limitations: Does not account for shear deformation (use Timoshenko theory for short beams)

Support Conditions

The boundary conditions at beam supports determine the deflection behavior:

  • Simply Supported (Pinned-Roller): Zero deflection at both ends, free rotation. Most common for floor joists and bridge spans.
  • Cantilever (Fixed-Free): One end rigidly fixed (zero deflection and slope), other end free. Used for balconies, brackets, and overhangs.
  • Fixed-Fixed (Built-in): Both ends rigidly fixed. Results in lower deflection but higher end moments. Common in continuous beams.

Load Types

  • Point Load (P): Concentrated force at a specific location. Units: N, kN, lbf
  • Distributed Load (w): Load spread over length. Units: N/m, kN/m, lb/ft
  • Moment (M): Applied torque/couple at a point. Units: N-m, kN-m, lb-ft

Moment of Inertia and Section Modulus

The moment of inertia (I) measures a cross-section's resistance to bending:

I = integral(y^2 dA)

  • Rectangle: I = bh^3/12 (b = width, h = height)
  • I-Beam: I = (BH^3 - bh^3)/12 (optimized for bending)
  • Circular: I = pi*d^4/64
  • Hollow Tube: I = pi*(D^4 - d^4)/64

Section Modulus (S = I/c) relates to maximum bending stress: sigma = M/S = Mc/I

Deflection Limits by Code

Building codes specify maximum allowable deflections for serviceability:

  • L/360: Floor beams supporting plaster ceilings (IBC)
  • L/240: Floor beams, general (most common)
  • L/180: Roof beams, not supporting ceilings
  • L/600: Crane runway beams (AISC)
  • L/1000: Precision machinery bases
Simply Supported Beam - Center Point Load P R1 = P/2 R2 = P/2 delta_max L (span length) Key Formulas (Simply Supported, Center Load): Maximum Deflection: delta = PL^3 / 48EI Maximum Moment: M = PL / 4 (at center) Maximum Shear: V = P / 2 (at supports) Bending Stress: sigma = Mc / I Shear Stress: tau = VQ / Ib Deflection Ratio: L/delta

Stress Distribution in Beams

Bending Stress Distribution (Cross-Section View) Neutral Axis Compression (-sigma) Tension (+sigma) c Stress Formulas: sigma = M * c / I sigma = M / S (where S = I/c) c = distance to outer fiber I = moment of inertia

Beam Deflection Calculator

Calculate maximum deflection, bending stress, shear force, and reactions for beams with various support and loading conditions.

Same length unit as beam - for stress calculation
Calculating...
Deflection Ratio: --

Beam Diagram

Results

Maximum Deflection --
Maximum Bending Moment --
Maximum Shear Force --
Maximum Bending Stress --
Reactions --
Deflection Ratio (L/delta) --

Code Compliance Check

L/360
Floor (IBC)
L/240
General
L/180
Roof
L/600
Crane (AISC)

Deflection Formulas

CaseMax DeflectionMax Moment
SS - Center LoadPL^3 / 48EIPL/4
SS - Uniform Load5wL^4 / 384EIwL^2/8
Cantilever - End LoadPL^3 / 3EIPL
Cantilever - UniformwL^4 / 8EIwL^2/2
Fixed - Center LoadPL^3 / 192EIPL/8
Fixed - UniformwL^4 / 384EIwL^2/12

Common Material Properties

MaterialE (GPa)Yield (MPa)
Steel (A36)200250
Steel (A992)200345
Aluminum 6061-T669276
Wood (SPF)12.4~10
Stainless 304193215