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Low-velocity impact damage analysis of composite laminates using self-adapting delamination element method

  • Lipeng Wang
  • , Ying Yan*
  • , Dafang Wu
  • , Hao Wu
  • *此作品的通讯作者
  • Beihang University

科研成果: 期刊稿件文章同行评审

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
21
4
DOI
出版状态已出版 - 8月 2008

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