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Column Stability

Column Buckling

Estimate Euler critical load, effective length, and slenderness for compression members with common end conditions.

Enter length in meters, E in GPa, inertia in cm^4, area in cm^2, and applied axial load in kN.

Buckling Inputs

End condition

Member data

Use the end condition that best matches the expected rotational restraint.

Use the weaker-axis inertia when buckling can occur about multiple axes.

Area is used to calculate the radius of gyration and slenderness.

Applied load is compared directly with the ideal Euler critical load.

Buckling Diagram
Effective length3.20 mOriginal axisBuckled shape
Euler critical load12,650.25 kN
Load ratio P / Pcr0.014
Slenderness ratio23.08
Effective length3.20 m
Stability Summary
End conditionPinned-Pinned
Effective length factor K1.000
Radius of gyration r13.87 cm
Euler stress Fe3,892.38 MPa
Load margin Pcr - P12,470.25 kN
Buckling Formula

Effective length

General form

L_e = K L

With current values

L_e = 1.000 * 3.20

Calculated result

L_e = 3.20 m

Euler critical load

General form

P_cr = pi^2 E I / L_e^2

With current values

P_cr = pi^2 * 210 * 6,250 / 3.20^2

Calculated result

P_cr = 12,650.25 kN

Slenderness ratio

General form

lambda = L_e / r, r = sqrt(I / A)

With current values

lambda = 3.20 / sqrt(6,250 / 33)

Calculated result

lambda = 23.08

This screen applies classical Euler elastic buckling and is most reliable for slender columns before inelastic or code-specific checks.

Model Assumptions
  • The column is straight, prismatic, and loaded concentrically.
  • Material behavior is linear elastic up to the predicted buckling load.
  • Only ideal Euler global buckling is screened here; local buckling and imperfections are excluded.
Engineering Reading
This column is relatively stocky; elastic Euler buckling is only a screening check.
Calculation Basis
MethodEuler buckling theory with effective-length-factor method
ScopeColumn Buckling for elastic preliminary compression-member review
ReviewTechnically reviewed: 2026-04-15

Assumptions & Limits

  • The model screens ideal global Euler buckling only and does not include local buckling or material nonlinearity.
  • Imperfections, eccentricity, and frame sway effects need separate engineering review.
  • K-factors are modeling assumptions about end restraint and should be treated as a sensitivity study when restraint is uncertain.

Reference Basis