Steel Section Design Theory - Eurocode 3

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.

I-SectionUB · UC · UBP · UJ📖 Theory📐 Worked example
Channel SectionPFC · PFC-BTB · PFC-LACED · UPN📖 Theory📐 Worked example
Angle SectionEA · UA · EA-BTB · UA-BTB📖 Theory📐 Worked example
Hollow SectionCHS · SHS · RHS · EHS📖 Theory📐 Worked example
Cold-Formed SectionZPURLIN · LIPPED-CHANNEL · PLAIN-CHANNEL📖 Theory📐 Worked example (soon)

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 (AA, cm²) - the cross-sectional area, used for axial (tension/compression) resistance and self-weight.
  • Second moment of area (IyI_y, IzI_z, cm⁴) - resistance to bending about the major (y-y) and minor (z-z) axes; governs deflection and buckling. Larger II = stiffer.
  • Radius of gyration (iyi_y, izi_z, cm) - i=I/Ai = \sqrt{I/A}; sets the slenderness for buckling. The minor-axis izi_z usually governs column buckling.
  • Elastic modulus (WelW_{el}, cm³) - Wel=I/cW_{el} = I / c (c = distance to extreme fibre); gives the elastic bending resistance (Class 3 sections).
  • Plastic modulus (WplW_{pl}, 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 (ItI_t, cm⁴) and warping constant (IwI_w) - 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/tfc/t_f, web c/twc/t_w), scaled by the material factor:

ε=235fy\varepsilon = \sqrt{\frac{235}{f_y}}
  • 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,RdM_{c,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:

Mc,Rd=WplfyγM0(Class 1, 2);Mc,Rd=WelfyγM0(Class 3)M_{c,Rd} = \frac{W_{pl}\, f_y}{\gamma_{M0}} \quad (\text{Class 1, 2}); \qquad M_{c,Rd} = \frac{W_{el}\, f_y}{\gamma_{M0}} \quad (\text{Class 3})

where fyf_y is the yield strength (e.g. 275 MPa for S275, 355 MPa for S355) and γM0=1.0\gamma_{M0} = 1.0 (UK National Annex).

Lateral-torsional buckling - Mb,RdM_{b,Rd} (§6.3.2)

An unrestrained beam in bending can buckle sideways and twist before reaching Mc,RdM_{c,Rd}. The buckling resistance applies a reduction factor χLT\chi_{LT} to the cross-section resistance:

Mb,Rd=χLTWyfyγM1M_{b,Rd} = \chi_{LT}\, \frac{W_y\, f_y}{\gamma_{M1}}

The reduction factor χLT\chi_{LT} depends on the non-dimensional LTB slenderness:

λˉLT=Wyfy/Mcr\bar{\lambda}_{LT} = \sqrt{W_y\, f_y / M_{cr}}

where:

  • McrM_{cr} - the elastic critical moment for lateral-torsional buckling.
  • LcrL_{cr} - the unrestrained (buckling) length of the compression flange.
  • C1C_1 - the moment-distribution factor (1.0 for uniform moment, higher for a more favourable shape).

McrM_{cr}also depends on the section's torsional and warping stiffness. Shorter spans, more lateral restraint and a more uniform moment all raise Mb,RdM_{b,Rd}.

Compression / flexural buckling - Nb,RdN_{b,Rd} (§6.3.1)

A column's resistance is the squash load Npl,Rd=Afy/γM0N_{pl,Rd} = A\, f_y / \gamma_{M0} reduced for buckling by the factor χ\chi:

Nb,Rd=χAfyγM1N_{b,Rd} = \chi\, \frac{A\, f_y}{\gamma_{M1}}

The reduction χ\chi follows the relevant buckling curve (a₀–d, Table 6.2) as a function of the non-dimensional slenderness:

λˉ=Lcriλ1\bar{\lambda} = \frac{L_{cr}}{i\,\lambda_1}

Because iz<iyi_z < i_y for most I-sections, minor-axis buckling usually governs unless the column is braced about the weak axis.

Shear resistance - Vpl,RdV_{pl,Rd} (§6.2.6)

Vpl,Rd=Av(fy/3)γM0V_{pl,Rd} = \frac{A_v\, (f_y/\sqrt{3})}{\gamma_{M0}}

where AvA_vis the shear area (the web for I-sections). Shear and bending are checked together; high coexistent shear (>50% of Vpl,RdV_{pl,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:

(My,EdMN,y,Rd) ⁣α+(Mz,EdMN,z,Rd) ⁣β1.0\left(\frac{M_{y,Ed}}{M_{N,y,Rd}}\right)^{\!\alpha} + \left(\frac{M_{z,Ed}}{M_{N,z,Rd}}\right)^{\!\beta} \le 1.0

where:

  • MN,y,Rd, MN,z,RdM_{N,y,Rd},\ M_{N,z,Rd} - axial-reduced moment resistances (the cross-section moment capacity after allowing for the coexistent axial force NEdN_{Ed}).
  • n=NEd/Npl,Rdn = N_{Ed}/N_{pl,Rd} - the axial utilisation ratio (clamped to 0–1).
  • α, β\alpha,\ \beta - interaction exponents: for I/H sections α=2\alpha = 2, β=max(5n,1)\beta = \max(5n,\,1); for CHS α=β=2\alpha = \beta = 2; for solid/other shapes α=β=1\alpha = \beta = 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:

NEdNb,y,Rd+kyyMy,EdMb,Rd+kyzMz,EdMc,z,Rd1.0(6.61)\frac{N_{Ed}}{N_{b,y,Rd}} + k_{yy}\frac{M_{y,Ed}}{M_{b,Rd}} + k_{yz}\frac{M_{z,Ed}}{M_{c,z,Rd}} \le 1.0 \quad (6.61)
NEdNb,z,Rd+kzyMy,EdMb,Rd+kzzMz,EdMc,z,Rd1.0(6.62)\frac{N_{Ed}}{N_{b,z,Rd}} + k_{zy}\frac{M_{y,Ed}}{M_{b,Rd}} + k_{zz}\frac{M_{z,Ed}}{M_{c,z,Rd}} \le 1.0 \quad (6.62)

The interaction factors kyy, kyz, kzy, kzzk_{yy},\ k_{yz},\ k_{zy},\ k_{zz}can 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):

FactorMethod 1 form
kyyk_{yy}CmyCmLTμy1NEd/Ncr,yC_{my}\,C_{mLT}\,\dfrac{\mu_y}{1 - N_{Ed}/N_{cr,y}}
kzzk_{zz}Cmzμz1NEd/Ncr,zC_{mz}\,\dfrac{\mu_z}{1 - N_{Ed}/N_{cr,z}}
kyzk_{yz}kzz0.6wzwyk_{zz}\,\dfrac{0.6\,w_z}{w_y}
kzyk_{zy}kyy0.6wywzk_{yy}\,\dfrac{0.6\,w_y}{w_z}

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,Rdn_y = N_{Ed}/N_{b,y,Rd} and nz=NEd/Nb,z,Rdn_z = N_{Ed}/N_{b,z,Rd}:

Factorλˉ1.0\bar\lambda \le 1.0λˉ>1.0\bar\lambda > 1.0
kyyk_{yy}Cmy[1+(λˉy0.2)ny]C_{my}\,[1+(\bar\lambda_y-0.2)\,n_y]Cmy[1+0.8ny]C_{my}\,[1+0.8\,n_y]
kzzk_{zz} (I/H)Cmz[1+(2λˉz0.6)nz]C_{mz}\,[1+(2\bar\lambda_z-0.6)\,n_z]Cmz[1+1.4nz]C_{mz}\,[1+1.4\,n_z]
kzzk_{zz} (RHS)Cmz[1+(λˉz0.2)nz]C_{mz}\,[1+(\bar\lambda_z-0.2)\,n_z]Cmz[1+0.8nz]C_{mz}\,[1+0.8\,n_z]
kyzk_{yz}0.6kzz0.6\,k_{zz}
kzyk_{zy}0.6kyy0.6\,k_{yy}  (not susceptible to torsion; a three-branch form applies if susceptible - Table B.2)

Cmy, CmzC_{my},\ C_{mz} 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.

Browse the section property tables or open the interactive tool to run EC3 capacity checks.

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