Why steel beams twist
Load a steel beam and watch it swing sideways and twist: lateral-torsional buckling in 3D, with the critical moment and the Eurocode resistance.
Try the steps, or set the beam below.
Your browser can’t show the 3D view; the numbers and the cross-section still work.
Press Load it to see the buckled shape.
- The elastic critical moment: the largest moment at which the perfect, elastic beam stays straight. A stability threshold, not a resistance.
- 102 kNm
- Equivalent ratio divided by under uniform moment for the same beam. Only with the load at the shear center and no restraints is it comparable with the factors of SN003, which assume ; it is not a general factor.
- 1.13
- 1.48
- CurveBuckling curve for rolled sections: b for , c above (EN 1993-1-1, Table 6.5).
- b
- 0.44
- The design buckling resistance moment, .
- 97.5 kNm
- The resistance of the cross-section, , with for class 1 and 2 and for class 3.
- 223 kNm
- Section classIn bending, EN 1993-1-1, Table 5.2: the flange outstand and the web.
- 1
What twisting costs you: is 44 % of .
Method
The beam is divided into 40 finite elements. Each node carries the sideways displacement and the twist of the shear center, and their slopes (cubic Hermite functions). The elastic critical moment is the lowest eigenvalue of the stability problem, including the height of the load above or below the shear center (after Trahair 1993). Fork supports and restraints are exact constraints.
Section properties come from the nominal dimensions (EN 10365), root fillets included, and agree with the ArcelorMittal catalog within its rounding.
The design resistance follows EN 1993-1-1:2005, 6.3.2.3, for rolled sections with the recommended values: , , curve b for and c above, .
Checked against the closed form under uniform moment, the factors of NCCI SN003 in their limit (1.127 and 1.348), an independent Ritz sine series, and a hand calculation of the resistance.
Assumptions and limits
Doubly symmetric rolled sections on fork supports (free warping), elastic, with prebuckling deflections ignored. No local or distortional buckling, no web openings, no post-buckling.
Restraints are discrete and rigid. “Top flange” holds the top flange sideways; “Full” holds the sideways movement and the twist. Loads act downwards, so the top flange is in compression.
The drawn shape is the buckling mode, enlarged: an eigenvalue analysis gives its shape, not its size. is a stability threshold, not a resistance.
Recommended values of the 2005 edition, not a National Annex; the factor f of 6.3.2.3(2) is not used, which is conservative. The second-generation Eurocodes replace this edition nationally by 2028. For design, check with software such as LTBeam (CTICM).
Cite
@software{guven_beam_twist,
author = {Güven, Murat},
title = {Why steel beams twist},
year = {2026},
url = {https://likemaestro.github.io/tools/beam-twist}
}References
- Access Steel (2006). NCCI: Elastic critical moment for lateral torsional buckling (SN003a-EN-EU). eurocodes.jrc.ec.europa.eu/sites/default/files/2022-06/SN003a-EN-EU.pdf
- CEN (2005). EN 1993-1-1: Eurocode 3: Design of steel structures – Part 1-1: General rules and rules for buildings. European Committee for Standardization.
- CEN (2017). EN 10365: Hot rolled steel channels, I and H sections – Dimensions and masses. European Committee for Standardization.
- Trahair, N. S. (1993). Flexural-Torsional Buckling of Structures. CRC Press. doi:10.1201/9781482271218