Abaqus Fatigue Analysis Skill
SkillAI & modelsOnce this skill is added, your AI can predict how long a part will last under repeated loading before fatigue becomes a problem. It is a skill for fatigue and durability analysis built around Abaqus. It covers the full workflow: counting load cycles, tracking how damage builds up, and estimating fatigue life.
Available today. Use it from your connected AI after setup.
No other account needed.
After adding the skill, ask your AI to run a fatigue or durability analysis and provide the loading information it should work from.
Then ask your AI: use the Abaqus Fatigue Analysis Skill skill
What your AI can do with it
- Count load cycles from repeated loading
- Calculate how damage accumulates over time
- Predict the fatigue life of a part
- Run a complete durability analysis from start to finish
What this skill tells your AI
The instructions your AI receives, as published by cai-aa/cae-agent-hub in Skill/abaqus/analysis/abaqus-fatigue-analysis/SKILL.md and read by ahel’s review.
Predict fatigue life from FEA stress results using S-N curves and damage accumulation.
When to Use This Skill
Route here when user mentions:
- "fatigue", "how many cycles", "fatigue life"
- "durability", "S-N curve", "cycles to failure"
- "rainflow counting", "Miner's rule"
- "high-cycle fatigue", "low-cycle fatigue"
Route elsewhere:
- Just stress analysis →
/abaqus-static-analysis - Crack propagation → specialized fracture tools
- Static strength check →
/abaqus-static-analysis
Important: Abaqus Fatigue Limitations
Abaqus has limited native fatigue capabilities. The typical workflow is:
- Run structural analysis in Abaqus (stress/strain results)
- Extract stress history from ODB
- Apply fatigue criteria externally (Basquin, Miner's rule)
For full fatigue analysis, consider external tools: fe-safe, nCode, FEMFAT.
Prerequisites
Before fatigue analysis:
- ✅ Completed static or dynamic analysis with converged results
- ✅ Material fatigue data (S-N curve or Coffin-Manson parameters)
- ✅ Stress output at critical locations
Workflow Steps
Step 1: Run Stress Analysis
Use /abaqus-static-analysis for constant loads or /abaqus-dynamic-analysis for time-varying.
Ensure output requests include:
S- Stress components (principal, Mises)E- Strain componentsPEEQ- Equivalent plastic strain (for low-cycle)
Step 2: Identify Critical Location
Find the maximum stress location:
- Use
/abaqus-odbto extract peak stress - Check stress concentrations (fillets, holes, notches)
- Consider fatigue notch factor (Kf) vs stress concentration (Kt)
Step 3: Extract Stress History
For constant amplitude: single max/min stress values. For variable amplitude: full stress-time history for rainflow counting.
Step 4: Apply Fatigue Criteria
Use appropriate method based on loading and life regime.
Step 5: Calculate Life and Damage
Apply Basquin equation for life, Miner's rule for cumulative damage.
Key Decisions
Fatigue Approach
| Approach | When to Use | Data Needed |
|---|---|---|
| Stress-life (S-N) | High-cycle (N > 10^4) | S-N curve |
| Strain-life (e-N) | Low-cycle (N < 10^4) | Coffin-Manson params |
| Fracture mechanics | Crack growth | da/dN curve |
Loading Type
| Loading | Analysis Method |
|---|---|
| Constant amplitude | Single static analysis |
| Variable amplitude | Multiple loads + rainflow |
| Proportional | Single load case |
| Non-proportional | Critical plane method |
Mean Stress Correction
| Method | Use Case |
|---|---|
| Goodman | Conservative, tensile mean |
| Gerber | Less conservative |
| Soderberg | Very conservative |
| SWT | Strain-life with mean stress |
What to Ask the User
If unclear, ask:
- Material fatigue properties? S-N curve coefficients or test data?
- Loading type? Constant amplitude or variable (spectrum)?
- Mean stress? Fully reversed (R=-1) or with mean stress (R=0)?
- Critical location known? Or need to find max stress?
- Life target? What's the required number of cycles?
Key Parameters
| Parameter | Typical Values | Notes |
|---|---|---|
| S-N slope (b) | 0.08-0.15 | Lower = longer life |
| Endurance limit | 40-50% UTS (steel) | Stress below which infinite life |
| Fatigue notch factor (Kf) | 1.0-3.0 | Kf = 1 + q(Kt-1) |
| Notch sensitivity (q) | 0.7-0.95 | Higher for stronger steels |
Troubleshooting
| Problem | Cause | Solution |
|---|---|---|
| Unrealistically short life | Stress singularity | Use Kf correction, refine mesh away from singularity |
| Wrong units | MPa vs Pa mismatch | Verify stress units match S-N data |
| Unconservative prediction | Missing mean stress | Apply Goodman/Gerber correction |
| Very long calculated life | Stress below endurance limit | Check if stress > endurance limit |
Related Skills
/abaqus-static-analysis- Base stress analysis/abaqus-dynamic-analysis- Time-varying loading/abaqus-amplitude- Cyclic loading definition/abaqus-odb- Extract stress history from results
Code Patterns
For API syntax, equations, and code examples, see:
Signals
- GitHub stars
- 891
- Forks
- 115
- Last commit
- Sep 2026
Advanced
- Catalog kind
- skill
- Gateway key
abaqus-fatigue-analysis- Source
- github.com/cai-aa/cae-agent-hub