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Experiment and modeling of repaired composite lamina under compression

  • Zhengzhou University of Aeronautics
  • Northwestern Polytechnical University Xian

Research output: Contribution to journalArticlepeer-review

2 Scopus citations

Abstract

The finite element modeling under compressive static load of repaired composite lamina is reported, and two methods: geometry non-linear method, linear method are applied to compute the stress-strain response of the repaired laminate. Then finite element models are analyzed with the ABAQUS package two-dimensional S8R shell elements. Non-linear geometry effects are taken into account in the presented model. The predicted strain distribution, damage evolution and strength of the laminate are compared with experimental results.

Original languageEnglish
Pages (from-to)869-873
Number of pages5
JournalJixie Qiangdu/Journal of Mechanical Strength
Volume28
Issue number6
StatePublished - Dec 2006

Keywords

  • Damage
  • Finite element method
  • Laminate
  • Mechanical properties

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