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2. Cross-section classification

The idea

A thin plate in compression can buckle locally before the steel yields. The more slender the plate, the earlier this happens. Design standards therefore sort cross-sections into four classes, according to how they behave in bending and compression.

Class Behaviour Consequence for the design
1 Reaches the plastic moment and can rotate a lot Plastic global analysis is allowed
2 Reaches the plastic moment, rotation is limited Plastic moment resistance can be used
3 Yields at the extreme fibre, local buckling stops it there Elastic resistance (or an elasto-plastic method) is used
4 Local buckling happens before yield Effective cross-section is needed

Slenderness of a plate

The slenderness of a plate part is the ratio of its width \(c\) to its thickness \(t\). It is compared with limits that depend on the yield strength through the factor

\[ \varepsilon = \sqrt{\frac{235}{f_y}} \]

with \(f_y\) in N/mm². A higher steel grade gives a smaller \(\varepsilon\), so the limits become stricter.

Steel grade \(f_y\) [N/mm²] \(\varepsilon\)
S235 235 1.000
S275 275 0.924
S355 355 0.814
S420 420 0.748
S460 460 0.715

Where are the limits?

The limits of \(c/t\) for each class are given in the tables of the design standard. They depend on the loading (bending, compression or both) and are not repeated here. Read them from the edition of the standard you use.

Worked example: IPE 330

The dimensions of the IPE 330 are \(h = 330\) mm, \(b = 160\) mm, \(t_w = 7.5\) mm, \(t_f = 11.5\) mm and \(r = 18\) mm.

Web (internal part, between the fillets):

\[ c_w = h - 2\,t_f - 2\,r = 330 - 2(11.5) - 2(18) = 271\ \text{mm} \qquad \frac{c_w}{t_w} = \frac{271}{7.5} = 36.1 \]

Flange (outstand):

\[ c_f = \frac{b - t_w - 2\,r}{2} = \frac{160 - 7.5 - 2(18)}{2} = 58.25\ \text{mm} \qquad \frac{c_f}{t_f} = \frac{58.25}{11.5} = 5.07 \]

The web is the slender part of this section: its \(c/t\) is much larger than that of the flange, so the web decides the class under compression.

Next step

Compare \(c_w/t_w\) and \(c_f/t_f\) with the limits of the standard for your load case. The chapter Flexural buckling continues with a section that is not limited by local buckling.