Abstract
Evaluation of low fatigue life was studied under multi-axial non-proportional loading using critical plane, element and experimental method. The maximum and critical planes of six-fatigue damage parameters under uni-axial, multi-axial proportional and multi-axial non-proportional were determined. Based on this the fatigue life is calculated and the damage models are evaluated.
| Original language | English |
|---|---|
| Pages (from-to) | 95-98 |
| Number of pages | 4 |
| Journal | Zhongguo Jixie Gongcheng/China Mechanical Engineering |
| Volume | 17 |
| Issue number | 1 |
| State | Published - 10 Jan 2006 |
Keywords
- Critical plane method
- Damage parameter
- Evaluation method of life
- Multi-axial non-proportional loading
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