Column Buckling Calculator
Euler buckling analysis for columns: critical load, slenderness, and safety check
Critical Load (P_cr)
Slenderness (λ)
Required I
Safety Factor
End Condition (Effective Length Factor K)
K=1.0 (P-P)
K=0.5 (F-F)
K=0.7 (F-P)
K=2.0 (F-Free)
Current: Pinned-Pinned (K=1.0)
Pa GPa ksi
m⁴ mm⁴ in⁴
m mm ft
m² mm² in²
m mm ft
m mm in
Pa GPa
N kN lbf
Pa GPa
m mm
N kN
N kN
Pa MPa
Material Preset (fills E and yield)
Preset sets E and yield strength for applicable modes.
Euler Critical Load (P_cr)
54.38 kN
E=200 GPa, I=8.33e-8 m⁴, L=3 m, K=1.0
Slenderness Ratio λ = 103.9
ShortIntermediateSlender
Euler buckling governs
Formula
π²EI/(KL)²
Buckling Stress
54.4 MPa
Safety Status
Safe
Key Buckling Formulas
Pcr = π²EI / (KL)²
σcr = Pcr / A = π²E / λ²
λ = KL / r , r = √(I/A)
K – effective length factor (end conditions)
λ – slenderness ratio
r – radius of gyration
λ – slenderness ratio
r – radius of gyration
People Also Ask
📌 What is Euler buckling and when does it occur?
📏 How do I choose the effective length factor K?
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⚙️ Johnson vs Euler: which formula to use?
🔧 How does lateral bracing affect buckling?
📐 Typical moment of inertia for steel sections?
Understanding Column Buckling
Euler buckling is a sudden lateral deflection that occurs in slender columns under axial compression when the load reaches a critical value. The critical load depends on:
- Material stiffness (Young's modulus E)
- Cross‑section geometry (moment of inertia I, area A)
- Column length (L) and end restraints (K)
Buckling is a stability failure, not a material strength failure. Even a very strong material can buckle if the column is slender enough.
Typical Material Properties
| Material | E (GPa) | σ_y (MPa) | Typical λ_transition |
|---|---|---|---|
| Structural Steel | 200 | 250 | 125 |
| Aluminum 6061-T6 | 69 | 276 | 70 |
| Timber (Pine) | 9 | 30 | 77 |
| Concrete C30 | 25 | 30 | 128 |
Detailed FAQs
What is the difference between Euler and Johnson buckling?
Euler applies to slender columns where buckling occurs elastically. For intermediate columns, inelastic buckling (Johnson formula) is used: σ_cr = σ_y - (σ_y/(2π))²·(λ²/E). The transition slenderness λ_t = π√(2E/σ_y).
How do I find the radius of gyration for a section?
r = √(I/A). For standard sections (W‑shapes, tubes), values are tabulated. For a rectangle b×h, r_min = h/√12 (bending about weak axis).
Column Buckling Calculator – For educational and preliminary design purposes. Always verify with applicable codes (AISC, Eurocode, etc.).