Euler Column Buckling Calculator

Choose the end conditions and enter E, the smallest moment of inertia I and the length. The calculator returns the Euler critical load. Add the area and yield strength to get the slenderness ratio and check whether the column is long enough for Euler’s formula to apply, or whether the Johnson parabola governs.

Last updated

Euler column buckling

Units
Steel is about 200 GPa (29 000 ksi).
The smaller of Ix and Iy. Scientific notation works, e.g. 1e6.
Between end restraints.
For slenderness ratio and critical stress.
Needs A. Checks whether Euler applies.
Euler critical load Pcr
219.3 kN
Effective length K·L
3 m (K = 1)
Slenderness ratio K·L/r
134.2
Euler critical stress
109.7 MPa
Governing critical load
219.3 kN

λ = 134.2 is at or above the transition slenderness λc = 125.7, so the column is long and Euler governs.

P
First buckling mode, Pinned–pinned (K = 1)
Intermediate steps
StepFormulaValue
Effective lengthLe = K·L = 1 × 3 m3 m
Euler critical loadPcr = π²·E·I / Le² = π² × 200 GPa × 1.000e+6 mm⁴ / Le²219.3 kN
Radius of gyrationr = √(I / A)22.36 mm
Slenderness ratioλ = K·L / r134.2
Euler critical stressσcr = Pcr / A = π²E / λ²109.7 MPa
Transition slendernessλc = √(2π²E / Sy)125.7

Inputs

Key formulas

Formulas used on this page, with the textbook each is cited from
FormulaExpressionWhereCited from
Euler critical loadPcr = π²·E·I / (K·L)²K·L = effective lengthGere & Goodno, Mechanics of Materials
Effective-length factors (ideal ends)K = 1 (pinned–pinned), 2 (fixed–free), 0.699 (fixed–pinned), 0.5 (fixed–fixed)theoretical values from the buckled mode shapesTimoshenko & Gere, Theory of Elastic Stability
Slenderness and critical stressr = √(I / A), λ = K·L / r, σcr = π²·E / λ²r = radius of gyrationHibbeler, Mechanics of Materials
Transition slendernessλc = √(2π²·E / Sy)Euler applies for λ ≥ λcShigley’s Mechanical Engineering Design
J. B. Johnson parabolaσcr = Sy − (Sy·λ / 2π)² / Efor intermediate columns, λ < λcShigley’s Mechanical Engineering Design

Assumptions

Worked example

Example: A pinned steel strut

Given

  • A steel strut 3 m long, pinned at both ends (K = 1).
  • E = 200 GPa (typical for carbon steel), minimum I = 1.0 × 10⁶ mm⁴, A = 2000 mm².
  • Yield strength Sy = 250 MPa, an assumed value for a mild steel grade.

Find

  • The Euler critical load.
  • Whether Euler’s formula is valid for this strut.

Solution

  1. Convert I to m⁴ and apply Euler’s formula with an effective length of 1 × 3 m.Pcr = π² × 200 × 10⁹ × 1.0 × 10⁻⁶ / 3² = 219 300 N = 219.3 kN
  2. Find the radius of gyration and the slenderness ratio.r = √(1.0 × 10⁶ / 2000) = 22.36 mm, λ = 3000 / 22.36 = 134.2
  3. Find the transition slenderness for this steel.λc = √(2π² × 200 000 / 250) = 125.7
  4. λ = 134.2 is above λc = 125.7, so the strut is long and Euler governs. Check the critical stress against yield.σcr = 219 300 / 2000 = 109.7 MPa < Sy = 250 MPa
  5. For comparison, fixing one end and freeing the other (K = 2) divides the load by K² = 4.Pcr = 219.3 / 4 = 54.8 kN

Answer: Pcr = 219.3 kN. λ = 134.2 exceeds λc = 125.7, so Euler’s formula applies, with σcr = 109.7 MPa.

Common mistakes

Frequently asked questions

What is the effective length factor K?

K scales the actual length to the length of an equivalent pinned–pinned column that buckles at the same load. It comes from the shape of the buckled column for each pair of end restraints.

When is Euler’s formula valid?

When the column is slender enough to buckle elastically, before any part of it yields. In practice that means a slenderness ratio above the transition value √(2π²E/Sy). Shorter columns fail by a mix of yielding and buckling.

Why does doubling the length cut the load to a quarter?

Pcr is proportional to 1/(K·L)². Twice the effective length gives one quarter of the critical load.

Does a stronger steel buckle at a higher load?

Not for a slender column. Euler’s load depends on E and I, not on strength, and E is nearly the same for all steels. A higher yield strength only helps short and intermediate columns.

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See also

Sources

  1. J. M. Gere, B. J. Goodno, Mechanics of Materials, Cengage
  2. R. C. Hibbeler, Mechanics of Materials, Pearson
  3. S. P. Timoshenko, J. M. Gere, Theory of Elastic Stability, McGraw Hill (reprinted by Dover)
  4. R. G. Budynas, J. K. Nisbett, Shigley’s Mechanical Engineering Design, McGraw Hill
  5. NIST Special Publication 811, Guide for the Use of the International System of Units (conversion factors), NIST

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