Tensile test and simulation of woven composite laminates after high velocity impact

doi:10.4028/www.scientific.net/AMR.971-973.232

科研成果详情

题名	Tensile test and simulation of woven composite laminates after high velocity impact
作者	Ge，Ming Ming; Cheng，Xiao Quan; Zhang，Qian; Xu，Yunyan
发表日期	2014
会议录名称	Advanced Materials Research
ISSN	1022-6680
卷号	971-973
页码	232-235
摘要	Tensile mechanical behaviors of two kinds composite laminates G803/5224 and G827/5224 specimen after high-speed impact were investigated separately. The influences of open-hole on the specimen's net tensile strength were analyzed by comparing with standard specimen's experimental results. An FEM model was established to simulate the damage growth in the laminates. Different equivalent zones were applied to model different velocity impact damages, and different damage criteria and modulus attenuation rules were used for two different ply forms. © (2014) Trans Tech Publications, Switzerland.
关键词	Composite laminates Impact failure Simulation analysis Tensile test
DOI	10.4028/www.scientific.net/AMR.971-973.232
URL	查看来源
语种	英语English
Scopus入藏号	2-s2.0-84904194806
引用统计
文献类型	会议论文
条目标识符	https://repository.uic.edu.cn/handle/39GCC9TT/12314
专题	个人在本单位外知识产出
作者单位	School of Aeronautic Science and Engineering, BEIHANG UNIV.,Beijing, 100191,China
推荐引用方式 GB/T 7714	Ge，Ming Ming,Cheng，Xiao Quan,Zhang，Qianet al. Tensile test and simulation of woven composite laminates after high velocity impact[C], 2014: 232-235.