Detail Categories (EN 1993-1-9 Tables 8.1-8.10)
| Category | Description | Typical Application |
|---|---|---|
| 160 | Base metal, rolled sections away from welds | Plain girder |
| 140 | Base metal with welded attachments, short | Beam with short stiffeners |
| 125 | Full penetration butt weld, ground flush | Welded splices ground smooth |
| 112 | Full penetration butt weld, NDT checked | Welded splices |
| 100 | Fillet welded attachment | Cross-beam connections |
| 90 | Fillet welded cover plate end | Cover plate termination |
| 80 | Longitudinal weld of stiffener | Stiffener-to-web weld |
| 71 | Fillet weld, transverse load, K-joint | Truss K-joints, crane girders |
| 63 | Cruciform joint with partial penetration | Heavy welded sections |
| 56 | Transverse butt weld on backing bar | Site welds |
| 50 | Base metal at weld toe of stiffener | Fillet welded stiffener toe |
| 45 | Base metal at end of welded cover plate | Cover plate end on flange |
| 40 | Base metal at fillet weld on edge plate | Edge beam weld termination |
| 36 | Non-load-carrying longitudinal fillet weld | Longitudinal attachments |
S-N Curves (EN 1993-1-9 Table 8.1)
| Category | Delta_sigma_C (MPa) at 2M cycles | Delta_sigma_D (MPa) at 5M cycles | Delta_sigma_L (MPa) at 100M cycles |
|---|---|---|---|
| 160 | 160 | 118 | 65 |
| 140 | 140 | 103 | 57 |
| 125 | 125 | 92 | 51 |
| 112 | 112 | 83 | 46 |
| 100 | 100 | 74 | 40 |
| 90 | 90 | 66 | 36 |
| 80 | 80 | 59 | 32 |
| 71 | 71 | 52 | 29 |
| 63 | 63 | 46 | 26 |
| 56 | 56 | 41 | 23 |
| 50 | 50 | 37 | 20 |
| 45 | 45 | 33 | 18 |
| 40 | 40 | 29 | 16 |
| 36 | 36 | 26 | 15 |
For constant amplitude stress ranges above Delta_sigma_D, slope m = 3. Below Delta_sigma_D, slope m = 5. Stress ranges below Delta_sigma_L do not contribute to fatigue damage.
Partial Factors (EN 1993-1-9 Table 3.1)
| Assessment Method | gamma_Ff | gamma_Mf |
|---|---|---|
| Damage tolerant (low consequence) | 1.00 | 1.00 |
| Safe life (medium consequence) | 1.00 | 1.15 |
| Fail safe — non-welded details | 1.00 | 1.15 |
| Fail safe — welded details | 1.00 | 1.25 |
Worked Example — Crane Runway Girder
Welded plate girder, 12 m span. Detail category at web-to-flange weld: Category 71. Crane: 100 kN capacity, 5000 cycles/day, 50 year design life (approx 1.25M cycles).
Stress range at weld: Delta_sigma = 90 MPa (tension to near-zero)
| Parameter | Value |
|---|---|
| Category | 71 |
| Delta_sigma_C | 71 MPa |
| Applied Delta_sigma | 90 MPa |
| gamma_Ff | 1.00 |
| gamma_Mf | 1.25 |
Fatigue resistance: Delta_sigma_C / gamma_Mf = 71 / 1.25 = 56.8 MPa Applied: gamma_Ff x Delta_sigma = 1.00 x 90 = 90 MPa > 56.8 MPa
Fatigue life: N_Rd = 2E6 x (71 / 90)^3 = 2E6 x 0.491 = 982,000 cycles Design life: 1.25M cycles > 982k cycles — detail does NOT achieve design life.
Option: Upgrade to Category 100 (ground butt weld): N_Rd = 2E6 x (100 / 90)^3 = 2E6 x 1.372 = 2.74M cycles > 1.25M cycles OK
Design Applications
Common Design Scenarios
This reference covers structural design scenarios commonly encountered in structural steel design practice:
- Strength verification: Check member or connection capacity against factored loads per the applicable design code
- Serviceability checks: Verify deflections, vibrations, and other serviceability criteria
- Code compliance: Ensure design meets all provisions of the governing standard
- Connection detailing: Verify weld sizes, bolt quantities, and edge distances
Related Design Considerations
- System behavior: consider the interaction between members and connections
- Load paths: verify that forces can be transferred through the structure to the foundations
- Constructability: check that the design can be fabricated and erected practically
- Cost optimisation: evaluate alternative sections or connection types for economy
Worked Example
Problem: Verify a typical steel member for the following conditions:
Typical span: 6.0 m | Load: service loads per applicable code | Section: common section in this category
Design Check:
- Determine governing load combination (ULS or SLS per EN 1990)
- Calculate maximum internal forces (moment, shear, axial)
- Compute nominal capacity per code provisions
- Apply resistance/safety factors
- Verify interaction if combined forces exist
Result: Use the results from the Steel Calculator tool to verify design adequacy.
Frequently Asked Questions
What European Standard governs structural steel design?
EN 1993 (Eurocode 3: Design of Steel Structures) is the primary standard for structural steel design in Europe. EN 1993-1-1 covers general rules for buildings, EN 1993-1-8 addresses connection design, and EN 1993-1-2 covers fire design. The standard uses limit state design with partial safety factors (ÃÂóM). National Annexes adapt parameters to each member state. Companion standards include EN 10025 for hot-rolled products, EN 1090 for execution, and EN 1994 for composite design.
What are the common steel grades used in European construction?
The most common steel grades for European construction are S235, S275, S355, S420, and S460 per EN 10025-2. S355 (minimum yield 355 MPa for t âÃÂä 16 mm) is the most widely used for structural applications. S275 is used for secondary members. S420 and S460 are quenched and tempered high-strength steels for weight-critical applications. Weathering steel (S355J2W) and fine-grain structural steels (EN 10025-3 and -4) are also available.
How does EN 1993 compare to other international steel design codes?
EN 1993, AISC 360 (US), AS 4100 (Australia), and CSA S16 (Canada) all use limit states design principles but differ in key details. EN 1993 uses partial safety factors (ÃÂóM0 = 1.00, ÃÂóM1 = 1.00, ÃÂóM2 = 1.25) rather than resistance factors (ÃÂÃÂ). Buckling curves in EN 1993 follow the European Column Curve system (a0 to d) with 5 distinct curves, compared to AISC's single curve. EN 1993-1-8 has comprehensive connection design provisions including the component method for moment connections.
Frequently Asked Questions
What do the detail categories in EN 1993-1-9 represent?
Detail categories (Delta_sigma_C) represent the fatigue strength at 2 million cycles. Higher numbers (160 for plain rolled sections) indicate better fatigue performance. Lower numbers (36 for longitudinal fillet welds) indicate fatigue-sensitive details. The category depends on geometry, loading direction, weld type, and fabrication quality.
How does the Palmgren-Miner rule apply?
The Palmgren-Miner rule (Clause 8.3) sums fatigue damage: D = sum(n_i / N_Ri) where n_i is cycle count at stress range Delta_sigma_i and N_Ri is the endurance from the S-N curve. Failure when D >= 1.0. For variable amplitude loading, the stress spectrum is binned and damage accumulated. EN 1993-1-9 permits using equivalent constant amplitude stress range for simplified assessment.
Related Pages
Educational reference only. Fatigue design per EN 1993-1-9:2005. Detail categories from Tables 8.1-8.10. Verify fatigue load models with EN 1991 parts. Results are PRELIMINARY - NOT FOR CONSTRUCTION without independent verification.
Design Resources
Reference pages