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Finite element analysis of stiffened composite panels subjected by low-velocity impact

  • Wen Chao Zhang*
  • , Yuan Guo
  • , Zhi Dong Guan
  • , Xia Guo
  • , Wei He
  • , Ri Ming Tan
  • *此作品的通讯作者
  • Beihang University
  • Aerospace Technology Institute of Specialty Materials and Processes

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 low-velocity performance of stiffened composite panels is investigated experimentally and numerically. In order to illustrate the effect of the stiffener, a number of plain laminates with same lay-up of the skin were impacted in various energies. Progressive damage models based on continuum damage mechanics (CDM) were used in combination with cohesive interface elements to predict the structural response and fracture mechanics of stiffened composite panels. The constitutive mode was implemented into the ABAQUS/Explicit FE code by user-defined material subroutines (VUMAT). The developed FE model made a good prediction about the structural impact response of stiffened panels over the rang of impact energies examined. Very good agreement was achieved between the extent of damage predicted around the impact site and the damage detected by non-destructive technique (NDT) ultrasonic C-scan of the panels.

源语言英语
主期刊名Machine Tool Technology, Mechatronics and Information Engineering
编辑Zhongmin Wang, Liangyu Guo, Jianming Tan, Dongfang Yang, Dongfang Yang, Kun Yang, Dongfang Yang, Dongfang Yang, Dongfang Yang
出版商Trans Tech Publications Ltd
4726-4730
页数5
ISBN(电子版)9783038352464
DOI
出版状态已出版 - 2014
活动International Conference on Machine Tool Technology and Mechatronics Engineering, ICMTTME 2014 - Guilin, 中国
期限: 22 6月 201423 6月 2014

出版系列

姓名Applied Mechanics and Materials
644-650
ISSN(印刷版)1660-9336
ISSN(电子版)1662-7482

会议

会议International Conference on Machine Tool Technology and Mechatronics Engineering, ICMTTME 2014
国家/地区中国
Guilin
时期22/06/1423/06/14

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