Column and S-Beam Buckling Calculator

Estimate elastic buckling loads, section properties, and stiffness for circular columns and two S-shaped beam configurations.

How to use

  1. Select Circular column or S-shaped beam.
  2. Enter outer diameter D and inner diameter d in mm, requiring 0 ≤ d < D.
  3. Enter length L in m and Young’s modulus E in GPa; both must be positive.
  4. For a circular column, choose mode I–IV matching the intended idealized coefficient.
  5. For an S-shaped beam, choose type I or II and enter non-negative deflection z in m; z changes bending stress only.
  6. Select Calculate to update the result. Select Reset to restore the active example.
  7. Read critical load first, then section and stiffness metrics. Correct any red warning before use.
  8. Do not use this screening model for short or inelastic columns, local shell buckling, imperfect/eccentric members, unsupported beam geometries, safety certification, or final code compliance.

Equations used

SI is used internally: D is outer diameter (m), d is inner diameter (m), L is unsupported or member length (m), z is non-negative transverse deflection (m), and E is Young’s modulus (Pa).

Calculated quantities are cross-sectional area A (m²), second moment of area I (m⁴), axial stiffness S (N/m), critical compressive load Fcr (N), longitudinal stiffness Sx (N/m), lateral stiffness Sz (N/m), and bending-stress magnitude σb (Pa). Coefficients are the dimensionless column coefficient C, dimensionless S-beam stiffness coefficients cxx and czz, and dimensionless S-beam buckling coefficient fk.

Falex
A = π(D² − d²)/4
I = π(D⁴ − d⁴)/64

Circular column

S = AE/L
Fcr = C E I/L²

C = π (mode I), π²/4 (mode II), 4π² (mode III), or 2.046π² (mode IV).

S-shaped beam

Sx = cxxEA/L
Sz = czzEI/L³
σb = 3EDz/L²
Fcr = fkEI/L²

Type I: (cxx, czz, fk) = (1, 12, 4π²). Type II: (3, 72/5, 36π²). Positive Fcr is compression capacity; positive z gives the reported positive stress magnitude. S-beam stiffness and buckling load are independent of z. Type II gives 9× the type-I load and 1.2× the lateral stiffness for equal inputs.

Rheologylab

Assumptions and limits: straight homogeneous linear-elastic members, annular circular section, idealized coefficients, and small deformation. Yielding, local buckling, imperfections, eccentricity, residual stress, connection flexibility, and post-buckling are excluded.

References: Anton van Beek, Tribology-ABC formula pages “Buckling of a round column” and “S-shaped beam”; Euler critical load and effective-length idealization.

Method note

Use the result as an elastic stability screen. Confirm end conditions, slenderness, material behavior, geometric applicability, safety factors, and governing design-code requirements with a qualified engineer.