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
- Select Circular column or S-shaped beam.
- Enter outer diameter D and inner diameter d in mm, requiring 0 ≤ d < D.
- Enter length L in m and Young’s modulus E in GPa; both must be positive.
- For a circular column, choose mode I–IV matching the intended idealized coefficient.
- For an S-shaped beam, choose type I or II and enter non-negative deflection z in m; z changes bending stress only.
- Select Calculate to update the result. Select Reset to restore the active example.
- Read critical load first, then section and stiffness metrics. Correct any red warning before use.
- 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.
I = π(D⁴ − d⁴)/64
Circular column
Fcr = C E I/L²
C = π (mode I), π²/4 (mode II), 4π² (mode III), or 2.046π² (mode IV).
S-shaped beam
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.
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.

