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Shear failure mechanisms and influences of overlaminate configuration on the failure of composite π joints

  • Kangkang Wang
  • , Fengrui Liu*
  • , Haiming Hong
  • *此作品的通讯作者
  • Beihang University
  • Xi'an Jiaotong University
  • China Aviation Industry Corporation

科研成果: 期刊稿件 › 文章 › 同行评审

摘要

All-composite adhesively bonded π-shaped joints, designed for integrated composite structures, have attracted increasing attention on account of their excellent mechanical behaviors. In this study, shear behaviors and failure mechanisms of two types of composite π joints made up of different overlaminates and configurations have been studied by static experiments accompanying with numerical progressive damage analyses. Good agreements between the numerical and experimental results validate the effectiveness of the numerical models and also give convincing proof of the predicted shear behaviors as well as failure mechanisms. Further the influences of overlaminate configurations on the failure of π joints were also investigated to improve their shearing load bearing capacity. It follows that the overlaminates and configurations have remarkable influences on the damage onset, propagation, and ultimate collapse patterns of the composite π joints. The adoption of the base laminate and enlargement of the filler radius and horizontal length of the L laminate in some extent could help to improve the load bearing capacity of the composite π joints.

源语言英语
页(从-至)934-942
页数9
期刊Results in Physics
卷12
DOI
出版状态已出版 - 3月 2019

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