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Column Buckling Calculator – Euler Critical Load & Slenderness

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
mm² in²
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
People Also Ask
📌 What is Euler buckling and when does it occur?
📏 How do I choose the effective length factor K?
📊 Slenderness ratio limits for columns?
⚙️ 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
MaterialE (GPa)σ_y (MPa)Typical λ_transition
Structural Steel200250125
Aluminum 6061-T66927670
Timber (Pine)93077
Concrete C302530128
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).
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