Experimental Investigation of Impacted and Non-impacted Composite Laminates under Compressive Loading

被引：0
|
作者：
Ruan, Jiangtao [1 ]
Shen, Min [1 ]
Tong, Jingwei [1 ]
Wang, Shibin [1 ]
Aymerich, F. [2 ]
Priolo, P. [2 ]
机构：
[1] Tianjin Univ, Dept Mech, Tianjin 300072, Peoples R China
[2] Univ Cagliari, Dept Mech Engn, I-09123 Cagliari, Italy
来源：
MATERIALS AND DESIGN, PTS 1-3 | 2011年 / 284-286卷
基金：
中国国家自然科学基金;
关键词：
Composite laminate; Deformation; Delamination; Compression; ESPI; BUCKLING BEHAVIOR; DELAMINATIONS;
D O I：
10.4028/www.scientific.net/AMR.284-286.607
中图分类号：
TB3 [工程材料学];
学科分类号：
0805 ; 080502 ;
摘要：
In this paper, the deformation measurements of impacted and non-impacted composite laminates under compressive loading are taken. [0(3)/90(3)]s orientated cross-ply laminated plates with impact delamination and without delamination are tested using an anti-buckling testing device in compression experiment. The delamination is induced by low-velocity impact test at the impact energy level of 3.105J For both impacted and non-impacted specimens, the compressive deformation is measured by a carrier electronic speckle pattern interferometry (CESPI) optical measurement technique. It is found that the deformation behavior of the two specimens presents a mixed deformation mode. However, the delamination has significant effect on the compressive deformation of composite laminates.
引用
收藏
页码：607 / +
页数：2
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