Abstract
The effect of stacking sequence on the failure process of hybrid composite laminates under quasi-static loading and impact loading is investigated. The results reveal that stacking sequence affects the appearance or non-appearance of delamination and thus affects the failure process. The best stacking sequence which reduces the tensile stress concentration fact around failure link by approximately 10-20% is then obtained.
| Original language | English |
|---|---|
| Pages (from-to) | 243-250 |
| Number of pages | 8 |
| Journal | Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University |
| Volume | 10 |
| Issue number | 2 |
| State | Published - Apr 1992 |
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