Quick Reference: Beam Deflection & Stress
These are the formulas you’ll use most often in mechanical and structural design. Memorize the first two (center-loaded simply supported and end-loaded cantilever) — every other case is a variation.
Simply Supported Beam
Case 1: Center Point Load
| Parameter |
Formula |
| Max Deflection (at center) |
δ = PL³ / 48EI |
| Max Moment (at center) |
M = PL / 4 |
| Reactions (each support) |
R = P / 2 |
Case 2: Uniform Distributed Load
| Parameter |
Formula |
| Max Deflection (at center) |
δ = 5wL⁴ / 384EI |
| Max Moment (at center) |
M = wL² / 8 |
| Reactions (each support) |
R = wL / 2 |
Case 3: Off-Center Point Load (at distance a from left)
| Parameter |
Formula |
| Max Deflection |
δ = Pa²b² / 3EIL (at load point, approx) |
| Moment at load |
M = Pab / L |
| Left reaction |
R₁ = Pb / L |
| Right reaction |
R₂ = Pa / L |
where b = L – a
Cantilever Beam (Fixed-Free)
Case 4: End Point Load
| Parameter |
Formula |
| Max Deflection (at free end) |
δ = PL³ / 3EI |
| Max Moment (at fixed end) |
M = PL |
| Reaction (at fixed end) |
R = P |
Case 5: Uniform Distributed Load
| Parameter |
Formula |
| Max Deflection (at free end) |
δ = wL⁴ / 8EI |
| Max Moment (at fixed end) |
M = wL² / 2 |
| Reaction (at fixed end) |
R = wL |
Fixed-Fixed Beam
Case 6: Center Point Load
| Parameter |
Formula |
| Max Deflection (at center) |
δ = PL³ / 192EI |
| Max Moment (at ends) |
M = PL / 8 |
| Moment at center |
M = PL / 8 |
Case 7: Uniform Distributed Load
| Parameter |
Formula |
| Max Deflection (at center) |
δ = wL⁴ / 384EI |
| Max Moment (at ends) |
M = wL² / 12 |
| Moment at center |
M = wL² / 24 |
Variable Definitions
| Variable |
Description |
Common Units |
| P |
Point load (force) |
lbs or N |
| w |
Distributed load (force per unit length) |
lbs/in or N/m |
| L |
Beam span length |
in or m |
| E |
Young’s Modulus (see chart) |
psi or Pa |
| I |
Area moment of inertia |
in⁴ or m⁴ |
| δ |
Maximum deflection |
in or m |
| M |
Bending moment |
in-lbs or N-m |
Comparison: How Support Conditions Affect Stiffness
For the same beam, load, and cross-section:
| Support |
Center Point Load Deflection |
Relative Stiffness |
| Cantilever (end load) |
PL³/3EI |
1× (baseline) |
| Simply Supported |
PL³/48EI |
16× stiffer |
| Fixed-Fixed |
PL³/192EI |
64× stiffer |
Key insight: Fixing both ends of a beam makes it 4× stiffer than simply supported and 64× stiffer than a cantilever of the same length. Support conditions matter enormously.
Related: Young’s Modulus Chart | Tolerance Stack-Up Analysis
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