Comparing Weld Fatigue Standards: FEM 1.001 vs. Eurocode 3 Using SDC Verifier

Last Updated on March 19th, 2025 by
Evaluating Weld Fatigue Standards

Weld fatigue plays a critical role in the structural integrity of cranes and general steel structures. Selecting the appropriate fatigue assessment standard directly impacts design safety, operational efficiency, and compliance. FEM 1.001 and Eurocode 3 are two commonly applied fatigue standards, each with a distinct methodology for evaluating weld strength and fatigue resistance.

FE-Tech conducted a study using structural design and analysis software SDC Verifier to compare FEM 1.001 and Eurocode 3 in assessing weld fatigue. This article presents a detailed breakdown of the study, explaining how each standard approaches fatigue evaluation and what engineers need to consider when selecting between them.

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FEM 1.001

Stress Fatigue depends on:

  • Weld Type (W0-W2, K0-K4);
  • Element Group / Loading Group (E1-E8);
  • Material Type ( St360/St37, St510/St52).

How to select weld type in SDC Verifier?

How to select weld type in SDC verifier?

Weld Type – also called Notch Case, defines which elements belong to what weld type (K0-K4 – joints affected by welding, W0-W2 – elements and joints, not affected by welding). Weld Type depends on shape, structural design, whole pattern or type and quality of welds.

While 𝜎𝑤 is the allowable stress limit and κ is th stress ratio (Kappa Factor).

To determine 𝜎𝑤, you can use two approaches:

1. Using the MJK Diagram (Graphical Approach)

The diagram on the right side provides permissible stress values as a function of the ratio between extreme stresses κ. The steps are:

  • Figure 1. Permissible Stress vs. Stress Ratio κ ChartIdentify the given κ value (x-axis).
  • Locate the corresponding curve based on the material type and construction case (e.g., W0, W1, K0, etc.).
  • Read the permissible stress 𝜎𝑡 from the y-axis.
  • Use the relationship between 𝜎𝑡 and 𝜎𝑤 to compute 𝜎𝑤 if needed.

2. Using Equations (Analytical Approach)

a) κ ≤ 0

  • For tension: 𝜎𝑡 = 5 . 𝜎𝑤 / (3 – 2 . κ)    
  • For compression: 𝜎𝑐=2 . 𝜎𝑤/(1- κ)      

b) κ > 0

  • For tension: 𝜎𝑡 = 𝜎0/[1- κ . (1 – 𝜎0/𝜎+1)] 
  • For compression: 𝜎𝑐 = 1.2 . 𝜎𝑡 

𝝈𝟎=1.66 . 𝝈𝒘(for κ = 0).
𝝈+𝟏=0.75 . 𝜎𝑅 (for κ = +1).
𝝈𝑹 ultimate strength.

𝜎𝑡 is limited in every case to 0.75 . 𝜎𝑅.

By way of illustration, Figure 1. shows curves giving the permissible stress as a function of the ratio κ for the following cases:

  • steel A.52;
  • predominant tensile stress;
  • group E6;
  • construction cases W0, W1, W2 for unwelded components and cases of construction for joints K0 to K4.

The permissible stresses have been limited to 240 N/mm², to the permissible stress adopted for checking ultimate strength.

Utilization Factor Combined (calculated stresses devided by the allowable stress)
(𝜎𝑥 𝑚𝑎𝑥/ 𝜎𝑥𝑎)2 + (𝜎𝑦 𝑚𝑎𝑥 / 𝜎𝑦𝑎 )2 – 𝜎𝑥 𝑚𝑎𝑥 .𝜎𝑦 𝑚𝑎𝑥 / (| 𝜎𝑥𝑎 | . | 𝜎𝑦𝑎 |) + (𝜏𝑥𝑦 𝑚𝑎𝑥/𝜏𝑥𝑦𝑎 )2 ≤ 1

where the stress values 𝜎𝑥𝑎, 𝜎𝑦𝑎 and 𝜏𝑥𝑦𝑎 are those resulting from the application of formulae (1), (2), (3) and (4) limited to 0.75 ⋅ 𝜎𝑅

Stress Fatigue is used in Fatigue Allowable Stress calculations.

Tablo 1. Values of 𝜎𝑤 depending on the component group and construction caseN 𝑚𝑚2

How to select element group in SDC Verifier?

How to select element group in SDC Verifier?

Need to select load spectrum, which means according to the standard, the structure is repeatedly loaded with the work load but the average load is between A and B of the working load, by selecting a load spectrum of 𝑃𝑖.

Symbol Spectrum Factor (𝑘𝑠𝑝)
P1 𝑘𝑠𝑝 ≤ 0.125
P2 0.125 < 𝑘𝑠𝑝 ≤ 0.250
P3 0.250 < 𝑘𝑠𝑝 ≤ 0.500
P4 0.500 < 𝑘𝑠𝑝 ≤ 1.000

Screenshot 2025 03 18 160047

 

Load Spectrum Remarks
P0 Very light P=0 Crane by exception loaded with the working load, and as a rule, with very light loads
P1 Light P=1/3 Crane sometimes loaded with the working load, and as a rule with loads of about 1/3 of the working load
P2 Moderate P=2/3 Crane repeatedly loaded with the working load, and as a rule with loads between 1/3 and 2/3 of the working load
P3 Heavy P=1 Crane frequently loaded with the working load

And maximum number of load cases of B, Class of Utilization B7 (1.8 million < 2 x 106).

Figure 2. classes of utilization

which gives utilisation class E we end up with element group of 𝐸𝑖.

Figure 3. Components Groups

We need to select the type of welding or notch group, and in our model we keep it simple out of 7 possible classifications we only use 3 of them, we have parts where there are no welding at all, which is W0 which is the best category, and have stress along the weld defined as notch group K1, and for stress perpendicular to the weld we use a slightly heavier notch group K2.

Screenshot 2025 03 18 165202

Screenshot 2025 03 18 165244

Eurocode 03

FAT Class – the fatigue strength for nominal stress ranges is represented by a series of (𝑙𝑜𝑔Δ𝜎𝑅)-(𝑙𝑜𝑔 𝑁) curves and (𝑙𝑜𝑔Δ𝜏𝑅)-(𝑙𝑜𝑔 𝑁) curves (S-N-curves), which correspond to typical detail categories. Each detail category is designated by a number which represents, in N/mm2, the reference value Δ𝜎𝐶 and Δ𝜏𝐶 for the fatigue strength at 2 million cycles.

How to select FAT class in SDC Verifier?

How to select FAT class in SDC verifier?

Table 1. FAT Classes

Figure 4. Endurance, Number of cycles N

Table 2. FAT Classes Description

Safety Factor Low consequence High consequence
Damage Tolerant 1.0 1.15
Safe Life 1.15 1.35


Example

This crane model was subjected to mechanical loadings as shown below, and SDC Verifier was used to evaluate weld fatigue according to FEM 1.001 and Eurocode 3. The obtained results were then compared.

Figure 5. Crane ModelWeld Type:

  Perpendicular to weld Parallel with weld Shear
Weld K1 K2 K0
No Weld W0 𝜏𝐷(-1) = 𝜎𝐷(-1) / sqrt(3)

 

Steel Grade 𝜎𝐷(-1) for κ=-1s element group 5 St 52-3
Notch Group W0 W1 W2 K0 K1 K2 K3 K4
Stress Amplitude 163.8 130.3 104.2 118.8 106.1 89.1 63.6 38.2


Screenshot 2025 03 19 080651
Boundary conditions:

Screenshot 2025 03 19 080842

Screenshot 2025 03 19 080933

Results
Max Displacement(mm):

Max Displacement(mm)

Max Stress(Mpa):

Max Stress(Mpa)

FEM 1.001 Utilization Factor Results

Table:

FEM 1.001 Utilization Factor Results

Plot (over All elements):

Plot(over All elements):

Screenshot 2025 03 19 081609

Plot (Over Weld Elements):

Plot(Over Weld Elements):

Screenshot 2025 03 19 081811

EUROCODE 03 Summed Dammage Results:

EUROCODE_03 Summed Dammage Results

Conclusion

The study conducted by FE Tech highlights the differences between FEM 1.001 and Eurocode 3 in fatigue assessment. FEM 1.001 proves to be the superior choice for crane fatigue evaluation, offering more precise classifications and stress criteria. However, Eurocode 3 remains a valid option for general steel structures, where a more conservative approach is necessary.

Screenshot 2025 03 19 082238

By using SDC Verifier, engineers can seamlessly compare both standards, automating fatigue calculations and enhancing structural decision-making. Whether optimizing crane design or evaluating structural components, SDC Verifier provides a comprehensive toolset for fatigue verification.

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