Strength of Materials · Combined Loading and Stability

Buckling of columns (Euler)

Predict the buckling load of slender columns with Euler's formula and see how end conditions and slenderness matter.

By the end of this topic you will be able to

  • Explain buckling as a stability failure rather than a strength failure.
  • Calculate the Euler critical load for different end conditions using the effective length.
  • Use the slenderness ratio to decide whether Euler's formula or yielding governs.

A different kind of failure

A short, stocky column fails by crushing: the material yields. A long, slender column fails much earlier, by buckling: it suddenly bows sideways, often with a stress far below the yield stress. Buckling is a failure of stability, not of material strength. Think of pressing on the ends of a plastic ruler.

Euler's formula

For an ideal, straight, pin-ended column loaded exactly along its axis, the load at which it buckles is

Pcr=π2EIL2P_{\text{cr}} = \frac{\pi^2 EI}{L^2}

where II is the smaller second moment of area of the section (the column buckles about its weakest axis).

End conditions: effective length

Other supports change the buckled shape. We account for them with an effective-length factor KK:

Pcr=π2EI(KL)2P_{\text{cr}} = \frac{\pi^2 EI}{(KL)^2}
Ends KK
Pinned – pinned 1.0
Fixed – free (flagpole) 2.0
Fixed – fixed 0.5
Fixed – pinned 0.7

A column fixed at both ends carries four times the load of a pinned one; a flagpole carries only a quarter.

Slenderness

With the radius of gyration r=I/Ar = \sqrt{I/A}, the slenderness ratio λ=KL/r\lambda = KL/r and the critical stress are

λ=KLr,σcr=π2Eλ2\lambda = \frac{KL}{r}, \qquad \sigma_{\text{cr}} = \frac{\pi^2 E}{\lambda^2}

Euler's curve is valid only while σcr\sigma_{\text{cr}} is below the yield stress. For stockier columns (small λ\lambda) the column yields before it buckles, and the load is limited by σyA\sigma_y A.

Interactive modelVary length, section and end conditions. The curve shows critical stress against slenderness.

This interactive model needs JavaScript. The theory, worked example and problems on this page work without it.

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Practice problems

  1. The column in the worked example is fixed at both ends. What is its critical load?
    Show answer
    K=0.5K = 0.5, so PcrP_{\text{cr}} is four times as large: 4×182.8=7314\times182.8 = 731 kN (the stress, 183 MPa, is still below yield).
  2. The same column is used as a flagpole (fixed at the bottom, free at the top). Find PcrP_{\text{cr}}.
    Show answer
    K=2K = 2, so Pcr=182.8/4=45.7P_{\text{cr}} = 182.8/4 = 45.7 kN.
  3. A pinned column's length is increased from 3 m to 4 m. How does the buckling load change?
    Show answer
    Pcr∝1/L2P_{\text{cr}} \propto 1/L^2: (3/4)2=0.5625(3/4)^2 = 0.5625, so it falls to 56% of the previous value.
  4. Why is a circular tube a better column than a solid bar of the same area?
    Show answer
    For the same area, a tube has a larger II (the material is further from the centroid), so a bigger rr and smaller λ\lambda, hence a higher PcrP_{\text{cr}}.

Key formulae

Euler critical load
Pcr=π2EI(KL)2P_{\text{cr}} = \frac{\pi^2 EI}{(KL)^2}
Radius of gyration
r=IAr = \sqrt{\frac{I}{A}}
Slenderness ratio
λ=KLr\lambda = \frac{KL}{r}
Critical stress
σcr=π2Eλ2\sigma_{\text{cr}} = \frac{\pi^2 E}{\lambda^2}
Lecturer notes: suggested plan, activity and assessment

Suggested plan (45 min). 5 min: students push on a plastic ruler to feel buckling; 15 min: Euler's idea and KK; 10 min: worked example; 15 min: model, slenderness curve and Euler validity.

Activity. Find the shortest length at which the modelled steel column switches from yielding to buckling.

Discussion. Why do scaffolding and bracing add bars at mid-height?

Assessment idea. Compare three end conditions for one section and rank the results.