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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
  • *Corresponding author for this work
  • Beihang University

Research output: Contribution to journalArticlepeer-review

Abstract

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.

Original languageEnglish
Pages (from-to)313-319
Number of pages7
JournalChinese Journal of Aeronautics
Volume21
Issue number4
DOIs
StatePublished - Aug 2008

Keywords

  • Composite laminate
  • Delamination
  • Low-velocity impact
  • Self-adapting delamination element method

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