Fatigue damage prediction under a general multiaxial service loading consists of three main steps: multiaxial cycle counting, damage evaluation for an identified cycle (or reversal), and damage accumulations. The accuracy of fatigue life predictions depends on all the above steps. This paper reviews
A unified multiaxial fatigue damage model for isotropic and anisotropic materials
โ Scribed by Yongming Liu; Sankaran Mahadevan
- Publisher
- Elsevier Science
- Year
- 2007
- Tongue
- English
- Weight
- 362 KB
- Volume
- 29
- Category
- Article
- ISSN
- 0142-1123
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โฆ Synopsis
A unified multiaxial fatigue damage model based on a characteristic plane approach is proposed in this paper, integrating both isotropic and anisotropic materials into one framework. Compared with most available critical plane-based models for multiaxial fatigue problem, the physical basis of the characteristic plane does not rely on the observations of the fatigue crack in the proposed model. The cracking information is not required for multiaxial fatigue analysis and the proposed model can automatically adapt for very different materials experiencing different failure modes. The effect of the mean normal stress is also included in the proposed model. The results of the proposed fatigue life prediction model are validated using experimental results of metals as well as unidirectional and multidirectional composite laminates.
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