European Beam Capacity Calculator — EN 1993-1-1
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Design per EN 1993-1-1 Clause 6.2
Calculate the bending and shear resistance of European hot-rolled steel sections per Eurocode 3. The calculator supports IPE, HEA, HEB, and HEM sections with S235, S275, S355, and S460 steel grades.
Supported Sections and Grades
- IPE sections — IPE 80 to IPE 750, the standard European I-section for beams
- HEA sections — HEA 100 to HEA 1000, wide flange with light flange thickness
- HEB sections — HEB 100 to HEB 1000, wide flange with medium flange thickness
- HEM sections — HEM 100 to HEM 1000, wide flange with heavy flange thickness
- Steel grades — S235 (EN 10025-2), S275, S355 (most common), S460
Design Checks Performed
- Section classification — Class 1, 2, 3, or 4 per EN 1993-1-1 Table 5.2
- Bending moment resistance — Mc,Rd = Wpl × fy / ÃÂóM0 for Class 1-2 sections
- Lateral-torsional buckling — Mb,Rd = ÃÂÃÂLT × Wy × fy / ÃÂóM1 per Clause 6.3.2
- Shear resistance — Vc,Rd = Av × (fy/âÃÂÃÂ3) / ÃÂóM0 per Clause 6.2.6
- Shear buckling — Checked when hw/tw > 72ÃÂõ/ÃÂ÷ per Clause 6.2.6(6)
- Deflection — Serviceability limits per EN 1990 Annex A1.4.3
Worked Example
Problem: Check an IPE 400 beam in S355 steel for a 6.0 m simply supported span with a factored UDL of 30 kN/m.
Solution:
- Section: IPE 400, S355 (fy = 355 MPa)
- Section class: Class 1 (compact)
- Plastic modulus Wpl,y = 1307 cm³
- Design moment: MEd = 30 × 6.0² / 8 = 135 kNm
- Moment resistance: Mc,Rd = 1307 × 10³ × 355 / 1.0 = 464 kNm
- Utilisation: 135/464 = 0.29 (29%) — OK
- Design shear: VEd = 30 × 6.0 / 2 = 90 kN
- Shear resistance: Vc,Rd = 4268 × (355/âÃÂÃÂ3) / 1.0 = 874 kN
- Utilisation: 90/874 = 0.10 (10%) — OK
Result: IPE 400 in S355 is adequate. Moment governs at 29% utilisation.
Second Worked Example — Laterally Unrestrained HEA Beam
Problem: Check an HEA 280 beam in S275 steel for an 8.0 m simply supported span with a factored UDL of 15 kN/m. Assume no intermediate lateral restraint. Load applied to top flange.
Solution:
- Section properties: HEA 280, S275 (fy = 275 MPa, tf = 13 mm) Wpl,y = 1110 cm³, Iy = 13700 cm⁴, Iz = 4760 cm⁴ It = 62 cm⁴ (torsion constant), Iw = 785000 cm⁶ (warping constant)
- Class check: Class 1 for both flange and web
- Design moment: MEd = 15 × 8.0²/8 = 120 kNm
- Cross-section resistance: Mc,Rd = 1110 × 10³ × 275 / 1.0 = 305 kNm
- Elastic critical moment Mcr (LTB, Clause 6.3.2.2): For simply-supported beam with UDL on top flange, C1 = 1.13, kz = kw = 1.0 Mcr = C1 × (ÃÂò × E × Iz / L²) × Ã¢ÃÂÃÂ[Iw/Iz + (L² × G × It)/(ÃÂò × E × Iz)] Mcr = 1.13 × (ÃÂò × 210000 × 4760 × 10⁴ / 8000²) × Ã¢ÃÂÃÂ[785000/4760 + (8000² × 81000 × 62 × 10⁴)/(ÃÂò × 210000 × 4760 × 10⁴)] × 10âÃÂû⁶ Mcr = 218 kNm
- Non-dimensional slenderness: ÃÂûÃÂÃÂLT = âÃÂÃÂ(Wy × fy / Mcr) = âÃÂÃÂ(1110 × 10³ × 275 / 218 × 10⁶) = âÃÂÃÂ(1.40) = 1.18
- Reduction factor ÃÂÃÂLT (Clause 6.3.2.3, curve 'b' for HEA with h/b ≤ 2): ÃÂñLT = 0.34, ÃÂûÃÂÃÂLT,0 = 0.4 ÃÂæLT = 0.5 × [1 + 0.34 × (1.18 - 0.4) + 1.18²] = 0.5 × [1 + 0.265 + 1.392] = 1.329 ÃÂÃÂLT = 1 / (1.329 + âÃÂÃÂ(1.329² - 1.18²)) = 1 / (1.329 + âÃÂÃÂ(1.766 - 1.392)) = 1 / (1.329 + 0.612) = 0.515
- LTB resistance: Mb,Rd = 0.515 × 1110 × 10³ × 275 / 1.0 = 157.3 kNm
- Check: 120 ≤ 157.3 → OK (usage: 76%)
Result: HEA 280 in S275 is adequate for the 8.0 m span. LTB governs at 76% utilisation — significantly higher than the fully restrained case. For longer spans or heavier loads, consider a deeper section (HEA 300+) or provide intermediate lateral restraint.
EN 1993-1-1 Clause Reference
| Design Check | EN 1993-1-1 Clause | Key Parameters |
|---|---|---|
| Section classification | Table 5.2 (Sheet 1 of 3) | ÃÂõ = âÃÂÃÂ(235/fy), flange c/tf, web c/tw |
| Bending resistance Mc,Rd | Clause 6.2.5 | Wpl for Class 1-2, Wel for Class 3, Weff for Class 4 |
| Shear resistance Vc,Rd | Clause 6.2.6 | Av shear area, fy/âÃÂÃÂ3 |
| Shear buckling | Clause 6.2.6(6) | hw/tw > 72ÃÂõ/ÃÂ÷ requires check |
| Bending + shear interaction | Clause 6.2.8 | Reduced My,V,Rd when VEd > 0.5Vpl,Rd |
| LTB — General method | Clause 6.3.2.2 | ÃÂÃÂLT from curve a-d per Table 6.4, ÃÂñLT imperfection factor |
| LTB — Simplified method | Clause 6.3.2.3 | For restrained tension flange |
| Deflection | EN 1990 Annex A1.4.3 | L/250 for floor with finishes, L/200 for roof |
Serviceability and Deflection — Eurocode Approach
EN 1990 Annex A1.4.3 defines characteristic load combinations for serviceability:
- Characteristic combination (irreversible limit states): Gk + Qk,1 + ÃÂã ÃÂÃÂ0,i Qk,i
- Frequent combination (reversible): Gk + ÃÂÃÂ1,1 Qk,1 + ÃÂã ÃÂÃÂ2,i Qk,i
- Quasi-permanent combination (long-term): Gk + ÃÂã ÃÂÃÂ2,i Qk,i
Typical deflection limits per EN 1993-1-1:
- Floors with brittle finishes: ÃÂômax ≤ L/250 for characteristic combination
- Roofs: ÃÂômax ≤ L/200 for characteristic combination
- Camber: Pre-camber ≤ L/300 to offset dead load deflection
For the IPE 400 example under service loads (unfactored UDL = 21.4 kN/m): Δ = 5 × 21.4 × 6000⁴ / (384 × 210000 × 231 × 10⁶) = 10.5 mm < 6000/250 = 24 mm → OK.
Related Resources
- European Beam Design Guide
- European Steel Grades
- European Column Buckling Guide
- Section Properties Calculator
FAQ
What steel grades does the calculator support? S235, S275, S355, and S460 per EN 10025-2. S355 is the default and most commonly used grade for structural steel in Europe.
Does it check lateral-torsional buckling? Yes. The calculator determines the reduction factor ÃÂÃÂLT based on the non-dimensional slenderness ÃÂûLT and the appropriate buckling curve per EN 1993-1-1 Clause 6.3.2.
What is the difference between EN 1993-1-1 and EN 1993-1-5 for beams? Clause 6.2 of EN 1993-1-1 covers the basic cross-section resistance. EN 1993-1-5 covers plate buckling for slender webs (Class 4 sections) — the calculator flags when this is required.
Can I use UK National Annex values? The calculator uses the recommended values from EN 1993-1-1 (ÃÂóM0 = 1.0, ÃÂóM1 = 1.0). For UK NA modifications, refer to the UK-specific guidance page.
How are the buckling curves selected for LTB? Per EN 1993-1-1 Table 6.4, the LTB buckling curve depends on the cross-section type and h/b ratio. For rolled I-sections with h/b ≤ 2: curve 'b' (ÃÂñLT = 0.34). For h/b > 2: curve 'c' (ÃÂñLT = 0.49). For welded sections, curve 'd' (ÃÂñLT = 0.76) may apply. More severe curves produce lower ÃÂÃÂLT values.
How does the bending and shear interaction work? Per EN 1993-1-1 Clause 6.2.8, when VEd exceeds 50% of Vpl,Rd, the moment resistance is reduced to My,V,Rd using a reduced yield strength for the shear area: (1 - ÃÂÃÂ) × fy where ÃÂà= (2VEd/Vpl,Rd - 1)². For hot-rolled I-sections with equal flanges bending about the major axis, the simplified formula My,V,Rd = (Wpl,y - ÃÂÃÂ × Aw²/4tw) × fy / ÃÂóM0 may be used.
What about plate girders and Class 4 sections? For slender webs (hw/tw > 72ÃÂõ/ÃÂ÷), the calculator flags that EN 1993-1-5 (plated structural elements) considerations apply. Class 4 sections use effective widths beff from EN 1993-1-5 Clause 4.4, with the reduction factor ÃÂàbased on plate slenderness ÃÂûÃÂÃÂp. Effective section properties (Weff, Aeff) replace gross properties for all resistance checks.
Which partial factors apply to beam design? Per EN 1993-1-1 Clause 6.1: ÃÂóM0 = 1.00 for cross-section resistance (all classes), ÃÂóM1 = 1.00 for member buckling resistance, and ÃÂóM2 = 1.25 for fracture resistance at bolt holes (tension). The same factors apply across Eurocode-participating countries unless modified by the National Annex.
Disclaimer: This content is for educational purposes only. Results must be verified by a licensed professional engineer. Steel Calculator provides preliminary design tools — NOT a substitute for professional engineering judgment.