摘要
On the basis of a 2D 4-node Mindlin shell element method, a novel self-adapting delamination finite element method is presented, which is developed to model the delamination damage of composite laminates. In the method, the sublaminate elements are generated automatically when the delamination damage occurs or extends. Thus, the complex process and state of delamination damage can be simulated practically with high efficiency for both analysis and modeling. Based on the self-adapting delamination method, linear dynamic finite element damage analysis is performed to simulate the low-velocity impact damage process of three types of mixed woven composite laminates. Taking the frictional force among sublaminations during delaminating and the transverse normal stress into account, the analytical results are consistent with those of the experimental data.
| 源语言 | 英语 |
|---|---|
| 页(从-至) | 313-319 |
| 页数 | 7 |
| 期刊 | Chinese Journal of Aeronautics |
| 卷 | 21 |
| 期 | 4 |
| DOI | |
| 出版状态 | 已出版 - 8月 2008 |
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