Slenderness Ratio Calculator — Column Buckling (KL/r)
The slenderness ratio λ = KL/r governs whether a column buckles elastically (Euler), inelastically, or fails by crushing. Enter the end conditions, unsupported length and cross-section to get λ and a classification per AISC guidance.
End condition (effective length factor K)
mm
Cross-section type
mm
Long column — elastic (Euler) buckling governs
- 1
Effective length KL
1 × 4,000 mm = 4,000 mm - 2
Radius of gyration r
25 mmr = √(I/A) about the weak axis, computed from the cross-section dimensions. - 3
Slenderness ratio λ = KL / r
4,000 ÷ 25 = 160
How does this calculator work?
Slenderness ratio λ = KL/r, where K is the effective-length factor (0.5 for fixed-fixed to 2.0 for cantilever), L is the unsupported length, and r = √(I/A) is the weak-axis radius of gyration. AISC limits λ ≤ 200 for compression members. Higher λ means lower buckling capacity.
Formula
How this is calculated
The slenderness ratio λ = KL/r compares a column's effective length KL to its least radius of gyration r. A larger λ means the column is more slender and therefore more susceptible to buckling at a lower load. The effective length KL accounts for the end conditions: a fixed-fixed column (K = 0.5) is much stiffer than a cantilever (K = 2.0) of the same physical length. The radius of gyration r = √(I/A) is computed from the section's second moment of area I and cross-sectional area A about its weak axis.
The AISC Steel Construction Manual (latest edition) sets a recommended maximum slenderness ratio of 200 for compression members. Below λ ≈ 50, a column is considered short and fails primarily by material yielding or crushing; between 50 and ~120 the failure mode is inelastic buckling (Johnson parabola range); above ~120 the column is long enough that elastic Euler buckling dominates, and critical stress drops with λ². This calculator computes λ only — critical buckling stress additionally depends on material yield strength (F_y), Young's modulus (E) and the applicable code equation.
Note: all dimensions are entered in millimetres and all results are in consistent SI units. The effective length factor K values listed follow AISC theoretical and recommended design values; actual K may differ if the assumption of perfectly rigid or perfectly pinned connections is not met in practice.
Frequently asked questions
AISC recommends λ ≤ 200 for compression members. For main structural members most designers target λ ≤ 120–150; bracing and secondary members may go up to 200. Below 50 buckling rarely governs.
K squares into the critical buckling load (P_cr ∝ 1/λ²), so doubling K from 1 to 2 (pinned-pinned to cantilever) reduces the critical load by a factor of four for the same physical column.
Buckling always occurs about the axis with the smallest radius of gyration (the weak axis), because that is the direction the column is least stiff. This calculator uses r_min; if your section is braced at different heights in each plane, compute KL/r separately for each axis.
Also known as
TG we-Calculate Editorial Team. (2026). Slenderness Ratio Calculator — Column Buckling (KL/r) [Online calculator]. TG we-Calculate. https://we-calculate.com/calculator/slenderness-ratio-calculator
TG we-Calculate Editorial Team. "Slenderness Ratio Calculator — Column Buckling (KL/r)." TG we-Calculate. 2026. https://we-calculate.com/calculator/slenderness-ratio-calculator.
TG we-Calculate Editorial Team, "Slenderness Ratio Calculator — Column Buckling (KL/r)," TG we-Calculate, 2026. [Online]. Available: https://we-calculate.com/calculator/slenderness-ratio-calculator
@misc{wecalculate_slenderness_ratio_calculator, title = {Slenderness Ratio Calculator — Column Buckling (KL/r)}, author = {{TG we-Calculate Editorial Team}}, howpublished = {\url{https://we-calculate.com/calculator/slenderness-ratio-calculator}}, year = {2026}, note = {TG we-Calculate} }
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