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Compressive behavior of composite laminate with delamination and a quick mechanical repair

  • Beihang University
  • Shenyang Aerospace University

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

In this paper, the compressive behavior of the ZT7H/QY9611 composite laminates containing single delamination and a corresponding quick mechanical repair method for field repairing have been investigated both experimentally and by numerical calculation method. After the conduct of the test, the buckling mode and load as well as the failure mode and load were obtained. A parametric analysis was implemented using the finite element method (FEM) models. The results show that the delamination size and though thickness position have an influence on the buckling load and mode, and a mixed buckling mode composed of sub-laminate buckling and global buckling occurs with a delamination size of Ф60mm located in the 1/4 thickness position. It is concluded that the buckling load decreases with the increase of the delamination size and the decrease of the delamination position in the thickness direction, and the quick mechanical repair method has an obvious restraining effect on the sub-laminate buckling.

源语言英语
主期刊名ECCM 2018 - 18th European Conference on Composite Materials
出版商Applied Mechanics Laboratory
ISBN(电子版)9781510896932
出版状态已出版 - 2020
活动18th European Conference on Composite Materials, ECCM 2018 - Athens, 希腊
期限: 24 6月 201828 6月 2018

出版系列

姓名ECCM 2018 - 18th European Conference on Composite Materials

会议

会议18th European Conference on Composite Materials, ECCM 2018
国家/地区希腊
Athens
时期24/06/1828/06/18

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