A concise guide to designing steel sections to Eurocode 3 (EN 1993-1-1): what each cross-section property means, how sections are classified, and how bending, lateral-torsional buckling, compression buckling and shear resistances are calculated - the theory behind this tool's capacity checks.
This is a concise theory reference for the design of steel sections to Eurocode 3 (EN 1993-1-1), covering the cross-section properties tabulated in this tool and the resistance checks the Capacity tab computes. It explains what each property means and how the key ultimate-limit-state (ULS) resistances are derived.
Section properties - what they mean
Every tabulated section carries the geometric properties below. They are the inputs to all strength and stability checks.
Area (A, cm²) - the cross-sectional area, used for axial (tension/compression) resistance and self-weight.
Second moment of area (Iy, Iz, cm⁴) - resistance to bending about the major (y-y) and minor (z-z) axes; governs deflection and buckling. Larger I = stiffer.
Radius of gyration (iy, iz, cm) - i=I/A; sets the slenderness for buckling. The minor-axis iz usually governs column buckling.
Elastic modulus (Wel, cm³) - Wel=I/c (c = distance to extreme fibre); gives the elastic bending resistance (Class 3 sections).
Plastic modulus (Wpl, cm³) - the first moment of area about the plastic neutral axis; gives the plastic bending resistance (Class 1 and 2 sections), which exceeds the elastic value.
Torsion constant (It, cm⁴) and warping constant (Iw) - control torsional and lateral-torsional buckling behaviour.
Cross-section classification (EN 1993-1-1 §5.5)
Before any resistance is calculated, the section is classified 1–4 by the slenderness of its compression parts (flange outstand c/tf, web c/tw), scaled by the material factor:
ε=fy235
Class 1 - can form a plastic hinge with rotation capacity; full plastic resistance and plastic analysis allowed.
Class 2 - can reach the plastic moment but with limited rotation; plastic resistance, elastic analysis.
Class 3 - can reach the yield (elastic) moment but local buckling prevents the plastic moment; elastic resistance.
Class 4 - local buckling occurs before yield; an effective (reduced) cross-section is used.
Bending resistance - Mc,Rd (§6.2.5)
The cross-section bending resistance depends on class. For Class 1 and 2 it uses the plastic modulus; for Class 3 the elastic modulus:
where fy is the yield strength (e.g. 275 MPa for S275, 355 MPa for S355) and γM0=1.0 (UK National Annex).
Lateral-torsional buckling - Mb,Rd (§6.3.2)
An unrestrained beam in bending can buckle sideways and twist before reaching Mc,Rd. The buckling resistance applies a reduction factor χLT to the cross-section resistance:
Mb,Rd=χLTγM1Wyfy
The reduction factor χLT depends on the non-dimensional LTB slenderness:
λˉLT=Wyfy/Mcr
where:
Mcr - the elastic critical moment for lateral-torsional buckling.
Lcr - the unrestrained (buckling) length of the compression flange.
C1 - the moment-distribution factor (1.0 for uniform moment, higher for a more favourable shape).
Mcralso depends on the section's torsional and warping stiffness. Shorter spans, more lateral restraint and a more uniform moment all raise Mb,Rd.
Compression / flexural buckling - Nb,Rd (§6.3.1)
A column's resistance is the squash load Npl,Rd=Afy/γM0 reduced for buckling by the factor χ:
Nb,Rd=χγM1Afy
The reduction χ follows the relevant buckling curve (a₀–d, Table 6.2) as a function of the non-dimensional slenderness:
λˉ=iλ1Lcr
Because iz<iy for most I-sections, minor-axis buckling usually governs unless the column is braced about the weak axis.
Shear resistance - Vpl,Rd (§6.2.6)
Vpl,Rd=γM0Av(fy/3)
where Avis the shear area (the web for I-sections). Shear and bending are checked together; high coexistent shear (>50% of Vpl,Rd) reduces the bending resistance.
Combined bending + axial - interaction checks
A member rarely carries pure bending or pure axial load - usually both, often biaxial. Two interaction checks apply, exactly as the Capacity tab computes them.
Cross-section interaction - Expr (6.41) §6.2.9
For Class 1/2 sections the plastic non-linear interaction governs:
(MN,y,RdMy,Ed)α+(MN,z,RdMz,Ed)β≤1.0
where:
MN,y,Rd,MN,z,Rd - axial-reduced moment resistances (the cross-section moment capacity after allowing for the coexistent axial force NEd).
n=NEd/Npl,Rd - the axial utilisation ratio (clamped to 0–1).
α,β - interaction exponents: for I/H sections α=2, β=max(5n,1); for CHS α=β=2; for solid/other shapes α=β=1 (linear). Class 3 sections use the linear elastic form.
Member stability - Expr (6.61) & (6.62) §6.3.3
When the member is also unrestrained (can buckle), both expressions must be satisfied - they combine column buckling with lateral-torsional buckling:
The interaction factors kyy,kyz,kzy,kzzcan be taken from either of two methods in EN 1993-1-1, presented in the standard's order below. This tool implements Annex B (Method 2), which is valid for all section types.
Annex A (Method 1)
Method 1 is only valid for doubly-symmetric sections. It splits each k-factor into auxiliary terms (it is not used by this tool):
Factor
Method 1 form
kyy
CmyCmLT1−NEd/Ncr,yμy
kzz
Cmz1−NEd/Ncr,zμz
kyz
kzzwy0.6wz
kzy
kyywz0.6wy
Annex B (Method 2) - the factors this tool computes
For members not susceptible to torsional deformation (Table B.1), with the axial ratios ny=NEd/Nb,y,Rd and nz=NEd/Nb,z,Rd:
Factor
λˉ≤1.0
λˉ>1.0
kyy
Cmy[1+(λˉy−0.2)ny]
Cmy[1+0.8ny]
kzz (I/H)
Cmz[1+(2λˉz−0.6)nz]
Cmz[1+1.4nz]
kzz (RHS)
Cmz[1+(λˉz−0.2)nz]
Cmz[1+0.8nz]
kyz
0.6kzz
kzy
0.6kyy (not susceptible to torsion; a three-branch form applies if susceptible - Table B.2)
Cmy,Cmz are the equivalent-uniform-moment factors (Table B.3) - they depend on the moment shape over the member; a uniform moment gives the conservative value, a more favourable moment diagram a lower one.
Method 1 generally gives marginally higher capacity for doubly-symmetric members but is more involved; Method 2 is simpler and broadly applicable, which is why it is implemented here.
Section families compared
UB / IPE (I-beams) - deep, efficient in major-axis bending; the workhorse beam. IPE is the European series (EN 10365); UB is the UK Blue Book.
UC / HE (H-sections / wide-flange) - wider flanges, better minor-axis and axial performance; used as columns.
Channels (PFC / UPN) - single-symmetric; common for purlins, bracing, and built-up members. The shear centre lies outside the web, so loading can induce torsion.
Angles (EA / UA) - designed about principal axes (u-u, v-v); used in trusses and bracing.
Hollow sections (CHS / SHS / RHS) - closed, high torsional stiffness, good in compression and architecturally clean.
Cold-formed (Z-purlins, lipped channels) - thin-walled, light secondary members for roofs and cladding.
This is a summary for orientation; always design to the full provisions of EN 1993-1-1 and the relevant National Annex. Use the Capacity tab to compute section-specific resistances.
Frequently asked questions
Lateral-torsional buckling is the tendency of an unrestrained steel beam in bending to suddenly deflect sideways and twist before reaching its full bending strength. It is to a beam what flexural (Euler) buckling is to a column. It happens because the compression flange, like a column, wants to buckle sideways but is connected to the tension flange, so the section twists. Restraining the compression flange - for example with a floor slab or roof purlins - largely eliminates it.
Eurocode 3 classifies cross-sections by how their compression parts behave: Class 1 (plastic) can form a plastic hinge with full rotation capacity; Class 2 (compact) reaches the plastic moment but with limited rotation; Class 3 (semi-compact) reaches only the elastic (yield) moment because local buckling prevents the plastic moment; and Class 4 (slender) buckles locally before yield, so a reduced effective section is used. The class is set by the slenderness (width-to-thickness ratio) of the most critical compression part - a section takes the least favourable class of its parts.
UB (Universal Beams) are the UK/British series to BS EN 10365, while IPE are the European series to EN 10365. Both are I-beams used mainly in bending, but they come in different size steps with different flange tapers and dimensions. IPE and HE (HEA/HEB/HEM) dominate continental Europe, the Middle East and much of Asia; UB and UC dominate the UK and Commonwealth. The Eurocode 3 design method is identical for both - only the section geometry differs.
The section modulus relates a section's bending resistance to the stress in its extreme fibre. The elastic modulus (Wel = I/c) gives the moment at first yield and is used for Class 3 sections. The plastic modulus (Wpl) gives the moment when the whole section has yielded and is used for Class 1 and 2 sections; it is larger than the elastic value (about 10–15% more for a typical I-section), so compact sections carry more moment.
A channel is symmetric about only one axis, and its shear centre lies outside the web on the opposite side from the flanges. If a load is applied through the web rather than through the shear centre, it creates a torque, so a channel used as a simple beam tends to twist as well as bend. In practice channels are used where this torsion is restrained - fixed to roof sheeting, paired back-to-back, or used in bracing.
For an equal angle the principal axes lie at 45° to the legs (skewed for unequal angles), and the minimum radius of gyration about the weak principal v-v axis governs buckling - not the axes parallel to the legs. Designing an angle as if it bent about the leg directions over-estimates its buckling strength. Angles are also usually connected through one leg only, so Eurocode rules account for the resulting load eccentricity.
Hot-finished hollow sections (EN 10210) are formed at high temperature, giving uniform material properties and sharper corners. Cold-formed hollow sections (EN 10219) are shaped at ambient temperature, producing work-hardened, more rounded corners and slightly different design parameters. Both come as CHS, SHS and RHS; the choice depends on the project specification and availability.
For Class 1 and 2 sections the cross-section bending resistance is M_c,Rd = Wpl·fy/γM0 (plastic modulus); for Class 3 it is M_c,Rd = Wel·fy/γM0 (elastic modulus). Here fy is the yield strength (275 MPa for S275, 355 MPa for S355) and γM0 = 1.0 in the UK National Annex. If the beam is unrestrained, the lower lateral-torsional buckling resistance M_b,Rd governs instead.