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Civil

Euler buckling load

Compressive load at which a slender column bows sideways.

Ref
CIV-05
Rev
v1
Field
Civil
Result
Pcr [kN]

Pcr in newtons (shown in kN), E Young’s modulus, Imin the smaller second moment of area of the section, L the length and K the effective-length factor: 1 for pin–pin, 0.5 for fixed–fixed, 0.7 for fixed–pinned and 2 for fixed–free.

A long thin column loaded in compression suddenly bows sideways at a critical load, often long before the material would crush. Longer, more slender, or more weakly restrained columns buckle at lower loads.

Calculator

Solve for
kN
GPa
10210
cm⁴
1020,000
m
0.510
0.52
  • Effective length KL3 m
  • Critical load as a mass178.9 tonne

What drives the result

Each variable is moved across its typical range while the others stay at the values above. The longest bar is the key driver.

Critical buckling load (kN) current value 1,755 kN
LColumn lengthKey driver
15863,200
IminSecond moment of area
21.943,900
KEffective-length factor
4397,020
EYoung’s modulus
87.71,840
  • Length enters squared (and with K, so does end restraint). Restraining the middle of a column halves its effective length and quadruples the capacity.
  • Buckling is governed by stiffness EI, not strength. A high-strength steel buckles at the same load as a mild steel of the same size.
  • Always use the weaker axis. A tall, narrow column buckles about its thin direction.
Chart data as tables

Ranked variables

VariableTypical rangeLowest resultHighest resultSwing (kN)Local stepChange in result
L Column length0.5 to 10 m157.963,17063,010+10%−17.4 %
Imin Second moment of area10 to 20,000 cm⁴21.9343,86043,840+10%+10 %
K Effective-length factor0.5 to 2 438.67,0186,580+undefined%—
E Young’s modulus10 to 210 GPa87.731,8421,755+10%+10 %

Sweep of Column length

Column length (m)Critical buckling load (kN)
0.563,170
0.727129,870
1.05714,120
1.5386,679
2.2363,158
3.2521,493
4.729706.2
6.877333.9
10157.9

Sweep one variable

Critical buckling load (kN)Hover, touch, or use the arrow keys on the chart
010k20k30k40k50k60k 0.512510 Column length (m), log scale now 1,755

Variables and how each one contributes

Pcr

Critical buckling load

Result · kN

What the equation gives you. Everything else feeds it.

E

Young’s modulus

GPa · typical 10 to 210

Material stiffness. Directly proportional.

Imin

Second moment of area

cm⁴ · typical 10 to 20,000

About the weaker axis of the cross-section. Directly proportional.

L

Column length

m · typical 0.5 to 10

Unsupported length. The dominant driver: inversely proportional to L², so +10% length cuts the load by about 17%.

K

Effective-length factor

· typical 0.5 to 2

Set by end restraint: 0.5 fixed–fixed, 0.7 fixed–pinned, 1 pin–pin, 2 fixed–free. Inversely proportional to K²: a fixed–free column (2) carries one quarter of a pin–pin column (1).

Worked example with the values above

  1. EI = 2×1011 Pa × 8×10−6 m⁴ = 1,600,000 N·m². Effective length KL = 3 m.
  2. Pcr = π²EI/(KL)² = 9.8696 × 1,600,000 / 9.
  3. Pcr = 1,755,000 N = 1,755 kN.

Assumptions and limits

  • Ideal straight, slender, elastic column under concentric load.
  • Pure elastic buckling (slenderness high enough that stress stays below yield).
  • Constant section.

Common mistakes

  • Using the strong axis I instead of Imin.
  • Assuming Euler applies to short, stocky columns; those fail by crushing.
  • Using the wrong K for the support conditions.

Statistics and uncertainty

Real columns have initial crookedness, load eccentricity and residual stress, so test loads fall below Euler by 10–30%. Design codes apply a safety factor or reduction curve. The squared effective length amplifies errors: a 5% error in K or L becomes 10% in Pcr.

Where it is used

  • Struts, masts, tripod legs and ramp supports.
  • Frame bracing and trusses.
  • Pushrods and actuator rods.

Maths you need

  • Second moment of area: I measures section stiffness
  • Support conditions: pinned or fixed ends set K

Related formulas

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