Abstract
Transform of six-fatigue damage parameters with the location of plane in uni-axial, multi-axial proportional, multi-axial non-proportional loading using the finite element method is studied. Then the damage parameter and critical plane are found. Based on this, a damage parameter which combines shear stress work and micro-mechanism is provided.
| Original language | English |
|---|---|
| Pages (from-to) | 606-609 |
| Number of pages | 4 |
| Journal | Harbin Gongye Daxue Xuebao/Journal of Harbin Institute of Technology |
| Volume | 36 |
| Issue number | 5 |
| State | Published - May 2004 |
Keywords
- Critical plane
- Fatigue damage parameter
- Non-proportional loading
- Shear stress work
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