Flambement de poteau
Estimate Charge critique d'Euler, effective length, et slenderness pour compression members avec courant end conditions.
Enter length in meters, E in GPa, inertia in cm^4, area in cm^2, et applied axial charge 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 et slenderness.
Applied charge is compared directly avec the ideal Charge critique d'Euler.
| End condition | Pinned-Pinned |
| Longueur efficace factor K | 1,000 |
| Radius of gyration r | 13,87 cm |
| Euler stress Fe | 3 892,38 MPa |
| Reserve de charge Pcr - P | 12 470,25 kN |
Longueur efficace
L_e = K L
L_e = 1.000 * 3.20
L_e = 3.20 m
Charge critique d'Euler
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
Rapport de slenderness
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 et is most reliable pour slender columns before inelastic or code-specific checks.
- The column is straight, prismatic, et loaded concentrically.
- Material behavior is linear elastic up to the predicted buckling charge.
- Only ideal Euler global buckling is screened here; local buckling et imperfections are excluded.
Assumptions & Limits
- The model screens ideal global Euler buckling only et does not include local buckling or material nonlinearity.
- Imperfections, eccentricity, et frame sway effects need separate ingenierie revue.
- K-factors are modeling hypotheses about end restraint et 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 Materiaux references
- Euler buckling et column-stability references