Eurocode 3 (EN 1993-1-1)
The EC3 engine implements EN 1993-1-1:2005/A1:2014 - Design of Steel Structures, Part 1-1: General Rules and Rules for Buildings. It supports the default Recommended Values and the UK National Annex for partial factor overrides.
Standard Reference
| Standard | EN 1993-1-1:2005/A1:2014 (Eurocode 3, Part 1-1) |
| Effective Widths | EN 1993-1-5:2006 (Plated Structural Elements) |
| Design Method | Limit State Design with partial safety factors (γM0, γM1, γM2) |
| Units | Metric (kN, kN·m, MPa, mm) |
| Verification Sources | SCI P364, Designers' Guide to EN 1993-1-1, Worked Examples in EC3 & EC4 |
| Benchmark Results | 126 test cases, 0.43% average difference |
Supported Section Types
- I-Shapes (UKB, UKC, IPE, HEB, HEA - rolled and welded including plate girders)
- Channels (PFC/UPN/UAP where available from the section library or imported section data)
- Tees (cut from UKB/UKC parents - beam tees and column tees)
- Rectangular Hollow Sections (SHS and RHS - hot-finished and cold-formed)
- Circular Hollow Sections (CHS)
- Angles (equal and unequal leg)
Checks Performed
The design-check table shows the specific row and clause used for each member result. The documentation keeps the same clause groups at a summary level:
- Section classification (5.5 / Table 5.2): Class 1-4 section classes are assigned by section family and active stress state.
- Class 4 effective sections (EN 1993-1-5): Supported flat-plate Class 4 paths use effective properties; CHS shell buckling is outside scope.
- Section resistance (6.2.3-6.2.10): Tension, compression, bending, shear, shear-bending, and N+M section checks use the reported clause row.
- Member buckling (6.3.1 / 6.3.1.4): Flexural and supported torsional or flexural-torsional compression buckling checks are reported separately.
- LTB (6.3.2.1(3) / 6.3.2.2 / 6.3.2.3): LTB resistance uses the general or modified I/H reduction method according to the section family.
- Combined stability and torsion (6.3.3 / 6.2.6(4) / 6.2.7): Annex B stability interaction and closed-hollow-section torsion rows are reported where applicable.
Calculator Inputs
The standalone EC3 calculator accepts the following inputs. All values are in metric units.
Fabrication Type
Select the fabrication method. This affects buckling curves, section classification limits, and the applicable shear-area path under 6.2.6:
- Rolled - standard hot-rolled sections (IPE, HEB, HEA, UKB, UKC)
- Welded / Built-up - fabricated plate girders and welded sections
- Cold Formed - cold-formed hollow sections
Section Geometry
Select a shape group, then enter dimensions or pick from the built-in section library (European/UK shapes).
| Shape | Dimensions |
|---|---|
| I/H Section | h (total height), b (flange width), tw (web thickness), tf (flange thickness) - mm |
| Channel (U) | h, b, tw, tf - mm |
| Tee (T) | h, b, tw, tf - mm |
| RHS / SHS | h (height), b (width), t (wall thickness) - mm |
| CHS / Pipe | d (diameter), t (wall thickness) - mm |
| Angle (L) | h (leg 1), b (leg 2), t (thickness) - mm |
Material Properties
| Symbol | Description | Unit |
|---|---|---|
fy | Yield strength | MPa |
fu | Ultimate tensile strength | MPa |
Partial Safety Factors (γ)
These can be adjusted to match national annex requirements:
| Symbol | Description | Recommended | UK NA |
|---|---|---|---|
γM0 | Cross-section resistance | 1.00 | 1.00 |
γM1 | Member instability (buckling) resistance | 1.00 | 1.00 |
γM2 | Net section tension resistance | 1.25 | 1.10 |
η | Shear area factor for rolled I/H sections (fy ≤ 460 MPa) | 1.20 | 1.00 |
Member Lengths & Bracing
| Symbol | Description | Unit |
|---|---|---|
L | System member length | m |
Lcr,z | Effective buckling length for the strong/major-axis slot. This maps to the FEA design tab's Kz major-axis factor. | m |
Lcr,y | Effective buckling length for the weak/minor-axis slot. This maps to the FEA design tab's Ky minor-axis factor. | m |
Lb | Unbraced length for lateral-torsional buckling - distance between points of lateral restraint | m |
C1 | Moment distribution factor for LTB (default 1.0 = uniform moment). Auto-computed in FEA tool. | - |
Mcr | Optional elastic critical moment override for EC3 lateral-torsional buckling. Empty = engine computes Mcr. | kN·m |
kc,LT | Optional Table 6.6 correction factor for the 6.3.2.3 modified I/H LTB method only. Empty = computed from the moment diagram. | - |
Cmy | Equivalent uniform moment factor about the major axis (y-y) for the 6.3.3 interaction check (Annex B, Table B.3). Default 1.0 = uniform moment (conservative). Reduce for non-uniform moment diagrams. | - |
Cmz | Equivalent uniform moment factor about the minor axis (z-z) for the 6.3.3 interaction check (Annex B, Table B.3). Default 1.0 = uniform moment (conservative). | - |
CmLT | Equivalent uniform moment factor for LTB interaction (Eq 6.62). Default = same as Cmy. Affects the kzy interaction factor. | - |
A Continuously Restrained checkbox sets Lb = 0, bypassing the LTB check.
For EC3 cantilever LTB cases, verify C1, Lb/KLT, and load-height assumptions from a suitable NCCI/SCI reference or elastic buckling calculation. The engine does not automatically infer fixed-free cantilever boundary conditions from the model.
Design Actions
| Symbol | Description | Unit | Sign Convention |
|---|---|---|---|
NEd | Design axial force | kN | Positive = compression |
My,Ed | Design bending moment about major axis (y-y) | kN·m | - |
Mz,Ed | Design bending moment about minor axis (z-z) | kN·m | - |
Vz,Ed | Design shear force (z-z direction) | kN | - |
Vy,Ed | Design shear force (y-y direction) | kN | - |
Partial Safety Factors
| Factor | Recommended | UK NA | Usage |
|---|---|---|---|
| γM0 | 1.00 | 1.00 | Cross-section resistance |
| γM1 | 1.00 | 1.00 | Member stability (buckling) |
| γM2 | 1.25 | 1.10 | Net section tension rupture |
| η | 1.20 | 1.00 | Shear area factor for rolled I-shapes |
Partial factors can be adjusted in the calculator via the advanced settings panel.
Limitations & Notes
- Custom-section axis convention: The section-library convention uses
Izzas the strong-axis inertia andIyyas the weak-axis inertia. Raw section-librarySzz/Syyfields are plastic section modulus values; the loader may expose those plastic values internally asPzz/Pyybefore EC3 reportsWpl,y/Wpl,z. Displayed/reportWel,y/Wel,zelastic values are derived separately. EC3 results are labelled in Eurocode notation, so the library strong axis is reported asy-yand the library weak axis asz-z. Custom or imported sections with these axes swapped can produce incorrect bending, buckling, and LTB axis assignments. - Net section: Tension rupture under 6.2.3 uses gross section area because bolt-hole deductions are not inferred. Check connection-region net sections separately.
- Torsional-flexural buckling (compression): Clause 6.3.1.4 torsional or flexural-torsional buckling is checked for supported open-section families. Angles are excluded because the doubly-asymmetric formulation is outside this engine scope.
- CHS Class 4: Not supported. EN 1993-1-6 (shell buckling) is required for CHS with D/t exceeding Class 3 limits. The engine issues a warning if this limit is exceeded.
- Tee stem classification: Tee classification follows the active stress state and Table 5.2 Sheet 2 limits for the reported station.
- Cm factors: Moment-gradient factors for 6.3.3 are computed from the moment diagram where available and can be overridden in the standalone calculator.
- Tee shear: Tee shear follows the relevant EC3 6.2.6 path for rolled or welded tees, with shear routed to the active stem or flange direction based on member orientation.
- Mcr methodology: Uses a supplied Mcr when present; otherwise uses the project analytical LTB method. Some benchmark discrepancies can arise where a reference uses a numerical eigenvalue model.
- Cantilever LTB: C1 is auto-computed from the moment diagram or can be manually overridden. Fixed-free/cantilever LTB boundary conditions are not auto-detected, so confirm the C1 and effective length assumptions for EC3 cantilevers separately.
- Local transverse forces and reactions: The EC3 member engine does not perform EN 1993-1-5 local transverse force, patch loading, web bearing, web buckling, end-post, or transverse-stiffener checks, and it does not derive these checks from FEA reactions, point loads, or connection forces. Check support bearing and concentrated load introduction regions separately from the member-strength result.
- National Annex: Default values follow the EN 1993-1-1 Recommended Values used by most European countries. The UK National Annex (γM2 = 1.10, η = 1.0) is auto-applied when a UK section is selected from the library. Other national annexes can be matched by adjusting γM and η in the advanced settings.
- Torsion (6.2.6(4)): Not an input in the standalone calculator. In the FEA tool, closed hollow sections (RHS/SHS/CHS) use a torsional shear stress check when a torsional section modulus is supplied or derivable. Warping torsion for open sections (I-beams, channels, angles, tees) is not performed.
- Serviceability and special design states: Structural analysis results may report displacements separately, but the EC3 design engine does not perform serviceability limit comparisons, vibration checks, fatigue, fire, corrosion/durability, connection detailing, or execution checks unless handled by a separate workflow.
Verification
The engine is benchmarked against 126 independent test cases from SCI P364, the Designers' Guide to EN 1993-1-1, EUR 22898 EN, and Worked Examples in Eurocode 3 & 4, with an average difference of 0.43%. The higher average compared to other engines reflects differences in Mcr computation methodology (analytical vs. numerical), which are documented in individual benchmark notes.