STRUCTURAL
Load Capacity Calculator
Beam · Column · Bending · Buckling · Safety factor
σ = M/Z
Pcr = π²EI/(KL)²
Beam parameters
—
shape
mm
mm
m
—
—
×
Max allowable load
—
kN
Bending stress
—
MPa
Max deflection
—
mm
Section modulus (Z)
—
cm³
σ = M / Z | P = 4·M / L (simple point)
Load vs span
Load capacity decreases with span
Beam diagram
Simply supported beam with center point load
Column parameters
—
shape
mm
mm
m
—
×
Critical load (Pcr)
—
kN
Allowable load
—
kN
Slenderness ratio (λ)
—
—
Radius of gyration (r)
—
mm
Pcr = π² × E × I / (K × L)²
Critical load vs height
Buckling load decreases with height²
Buckling modes
Euler buckling — first mode
Material properties
| Material | Yield strength (MPa) | E modulus (GPa) | Density (kg/m³) | Typical use |
|---|---|---|---|---|
| Steel (A36) | 250 | 200 | 7850 | Structural beams |
| Aluminum (6061) | 240 | 69 | 2700 | Lightweight structures |
| Wood (Douglas Fir) | 55 | 13 | 550 | Timber framing |
| Concrete (C30) | 30 | 30 | 2400 | Compression members |
| Stainless Steel | 310 | 193 | 8000 | Corrosion-resistant |
| Brass (C260) | 200 | 110 | 8500 | Machined parts |
σallow = σyield / SF | I = ∫ y² dA