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
Stress Distribution in Beams
Beam Deflection Calculator
Calculate maximum deflection, bending stress, shear force, and reactions for beams with various support and loading conditions.
Beam Diagram
Results
Code Compliance Check
Deflection Formulas
| Case | Max Deflection | Max Moment |
|---|---|---|
| SS - Center Load | PL^3 / 48EI | PL/4 |
| SS - Uniform Load | 5wL^4 / 384EI | wL^2/8 |
| Cantilever - End Load | PL^3 / 3EI | PL |
| Cantilever - Uniform | wL^4 / 8EI | wL^2/2 |
| Fixed - Center Load | PL^3 / 192EI | PL/8 |
| Fixed - Uniform | wL^4 / 384EI | wL^2/12 |
Common Material Properties
| Material | E (GPa) | Yield (MPa) |
|---|---|---|
| Steel (A36) | 200 | 250 |
| Steel (A992) | 200 | 345 |
| Aluminum 6061-T6 | 69 | 276 |
| Wood (SPF) | 12.4 | ~10 |
| Stainless 304 | 193 | 215 |