Delamination Behavior of L-Shaped Laminated Composites

被引:22
|
作者
Geleta, Tsinuel N. [1 ]
Woo, Kyeongsik [2 ]
Lee, Bongho [3 ]
机构
[1] Western Univ, Dept Civil & Environm Engn, London, ON N6A 3K7, Canada
[2] Chungbuk Natl Univ, Sch Civil Engn, Chungbuk 28644, South Korea
[3] Nextcoms Co LTD, Daejeon 34037, South Korea
关键词
Delamination; Curved laminate; Cohesive zone modeling; Multiple delamination; CRACK-GROWTH; FRACTURE-TOUGHNESS; SIMULATION; POLYMERS; FAILURE; SOLIDS; MODELS;
D O I
10.1007/s42405-018-0038-y
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
We studied the delamination behavior of L-shaped laminated composites numerically and experimentally. In finite-element modeling, cohesive zone modeling was used to simulate the delamination of plies. Cohesive elements were inserted between bulk elements at each interlayer to represent the occurrence of multiple delaminations. The laminated composite models were subjected to several types of loading inducing opening and shearing types of delamination. Numerical results were compared to those in the literature and of experiments conducted in this study. The results were carefully examined to investigate diverse delamination initiation and propagation behaviors. The effect of varying presence and location of pre-crack was also studied.
引用
收藏
页码:363 / 374
页数:12
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