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.
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.
| End condition | Pinned-Pinned |
| Effective length factor K | 1.000 |
| Radius of gyration r | 13.87 cm |
| Euler stress Fe | 3,892.38 MPa |
| Load margin Pcr - P | 12,470.25 kN |
Effective length
L_e = K L
L_e = 1.000 * 3.20
L_e = 3.20 m
Euler critical load
P_cr = pi^2 E I / L_e^2
P_cr = pi^2 * 210 * 6,250 / 3.20^2
P_cr = 12,650.25 kN
Slenderness ratio
lambda = L_e / r, r = sqrt(I / A)
lambda = 3.20 / sqrt(6,250 / 33)
lambda = 23.08
This screen applies classical Euler elastic buckling and is most reliable for slender columns before inelastic or code-specific checks.
- 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.
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
- Documentation: Methodology
- Documentation: Engineering Review
- Roark's Formulas for Stress and Strain
- Mechanics of Materials references
- Euler buckling and column-stability references