Amogh N P
 In loving memory of Amogh N P — Architect · Designer · Visionary 
Steel columns rising on a building site — slender compression members whose strength is set by buckling.
Unit IIIDesign of Structures - II

Compression Members

Columns don't crush — they buckle. Slenderness is everything.

≈ 40 min + worked example

A column rarely fails by crushing — it fails by buckling, bowing sideways long before the steel reaches its yield stress. So the whole of compression design turns on one idea: slenderness. Fix the effective length from the end conditions, find the slenderness ratio about the weak axis, read the design stress off a buckling curve, and the capacity follows.

Learning objectives

By the end of this lesson, you will be able to — mapped to the course outcomes for Design of Structures I:

1
CO3 · Understand

Distinguish short and slender columns and the way each fails.

2
CO3 · Apply

Find the effective length from the end conditions (K) and the slenderness ratio λ = KL/r about the weak axis.

3
CO3 · Apply

Compute the design compressive stress fcd from the buckling curve and the capacity Pd = Ae·fcd.

4
CO6 · Apply

Describe single, laced and battened built-up columns and their slenderness penalties.

Crush vs buckle

Short, slender, and the effective length

Short columns crush; slender ones buckle. The effective length KL = K·L, where K depends on the end restraints (0.65 fixed–fixed to 2.0 for a cantilever), and the slenderness λ = KL/r uses the minimum radius of gyration — buckling picks the weak axis.[1]

Short crushes, slender buckles short — crushes at fy load it bows out slender — buckles below fy slenderness λ = KL/r decides the mode and the strength.
DiagramA short stocky column crushing at the yield stress beside a slender column bowing sideways and buckling at a lower stress
Effective length — K from the end conditions fixed–fixed K = 0.65 pin–pin K = 1.0 fixed–pin K = 0.80 cantilever K = 2.0
DiagramFour column end conditions and their effective length factors K: fixed-fixed 0.65, pin-pin 1.0, fixed-pin 0.80 and cantilever 2.0

Crushing vs buckling

A short (stocky) column fails by yielding/crushing at about fy/γm0; a slender (long) column buckles sideways at a stress well below fy. Slenderness decides which — and almost all real columns are slender enough that buckling governs.[1, 3]

fcd → Pd

The buckling curve and the capacity

The design compressive stress fcd is read from one of four buckling curves (classes a–d), falling steeply as slenderness rises and never exceeding fy/γm0. The capacity is Pd = Ae·fcd.[1]

The buckling curves — fcd falls with slenderness KL/r → fcd fy/γm0 class a (strongest) class d (weakest) stocky → plateau slender → buckling
DiagramThe design compressive stress plotted against slenderness — a plateau near the yield stress falling steeply with slenderness, with separate lines for buckling classes a to d

fcd from the column curve

The design compressive stress fcd is not a single number — it is read from one of four buckling curves (classes a/b/c/d) by the section's shape and axis (Table 10). Class a is the strongest (least imperfection), class d the weakest. fcd ≤ fy/γm0 always.[1]

Drive the numbers

Column capacity calculator

Enter the area, radius of gyration, length, end condition and buckling class; the tool computes the slenderness, the design stress and the axial capacity, and plots fcd against slenderness. An ISHB 250 over 3.5 m carries about 1114 kN.[1]

Compression member · axial capacity (IS 800 cl. 7)

λ = KL/r; fcd from the buckling curve; Pd = A·fcd. Fe410, E = 200 GPa.

0.0 kN

Axial capacity Pd

0.0

Slenderness λ = KL/r

0.0 MPa

Design stress fcd

fcd falls as slenderness rises — buckling class c.

The contrasts

At a glance

AspectOneThe other
Failure modeShort column: crushing / yielding (~fy/γm0)Slender column: buckling (fcd ≪ fy)
End conditionsBoth fixed: K = 0.65 (shorter KL, stronger)Cantilever (fixed–free): K = 2.0 (longest, weakest)
Which radiusUse r_min (weak axis)Never r_max — buckling picks the weak axis
Single vs built-upSingle rolled: simple, limited rBuilt-up laced/battened: larger r, longer reach
Lacing vs battensLacing: stiffer in shearBattens: simpler, +10% slenderness penalty
A built-up laced steel column — two sections tied by diagonal lacing to spread the area and resist buckling.
PhotoA built-up laced steel column — two sections tied by diagonal lacing to spread the area and resist buckling.HighVoltage 5576 · CC0 · via Wikimedia Commons
Vocabulary

Key terms

Slenderness ratio (λ)

KL/r — the key measure of buckling-proneness; higher means weaker.

Radius of gyration (r)

√(I/A); design uses r_min, the value about the weak axis.

Effective length (KL)

K·L — equivalent pinned-pinned length; K from end conditions (Table 11).

Buckling class (a/b/c/d)

Table 10 category fixing the column curve and imperfection factor α.

Imperfection factor (α)

0.21 / 0.34 / 0.49 / 0.76 for classes a/b/c/d — models residual stress and crookedness.

Design compressive stress (fcd)

Reduced stress from the buckling curve; fcd ≤ fy/γm0.

Euler buckling stress (fcc)

π²E/λ² — the elastic critical stress of an ideal slender column.

Short vs slender column

Short crushes near fy; slender buckles at fcd well below fy.

Apply it

Worked example

An ISHB 250 column (A = 6971 mm², r = 53.6 mm), pinned–pinned, 3.5 m, Fe410, buckling class c. λ = 3500/53.6 = 65.3; fcc = π²·E/λ² = 462.9 MPa; λ̄ = √(250/462.9) = 0.735; with α = 0.49, φ = 0.901, so fcd = 159.8 MPa and Pd = 6971×159.8 ≈ 1114 kN. Fix the ends (K = 0.65) in the calculator and watch the capacity climb.

Check your understanding

Self-assessment

1. The imperfection factor α for buckling class c is —

2. For a column fixed at one end and free at the other (a cantilever/flagpole), the effective length factor K is —

3. In computing slenderness, the radius of gyration to use is —

In a nutshell

Recap

Slender columns buckle before they crush; slenderness λ = KL/r (about the weak axis, r_min) decides the strength.
Effective length KL = K·L; K runs from 0.65 (both fixed) to 2.0 (cantilever); fixing ends makes a column stronger.
The design compressive stress fcd comes from one of four buckling curves (α = 0.21/0.34/0.49/0.76) and never exceeds fy/γm0.
Capacity Pd = Ae·fcd; built-up laced/battened columns extend reach, with a 10% slenderness penalty for battens.
The evidence

References & further reading

  1. [1]IS 800:2007 — General Construction in Steel, Code of Practice (Section 7: compression members; cl. 7.1; Tables 3, 7, 9, 10, 11). Bureau of Indian Standards.
  2. [2]SP 6 (Part 1) — ISI Handbook for Structural Engineers: Structural Steel Sections. Bureau of Indian Standards.
  3. [3]N. Subramanian, Design of Steel Structures (2nd ed.). Oxford University Press, 2016.
  4. [4]S.K. Duggal, Limit State Design of Steel Structures (2nd ed.). McGraw-Hill Education, 2014.

Further reading

  • N. Subramanian, Design of Steel Structures — compression-member chapters.
  • S.K. Duggal, Limit State Design of Steel Structures.
  • S.S. Bhavikatti, Design of Steel Structures by Limit State Method as per IS 800-2007.

Sources gathered and fact-checked June 2026. Published values vary by source, sample and method — treat as indicative and confirm against the cited standard before structural use.