Effect of a gap on the open hole tension strength of carbon fiber reinforced plastic laminates

被引:0
|
作者
Suemasu, Hiroshi [1 ,3 ]
Aoki, Yuichiro [1 ]
Tateishi, Yasutomo [2 ]
Sugimoto, Sunao [1 ]
Nakamura, Toshiya [1 ]
机构
[1] Japan Aerosp Explorat Agcy, Aeronaut Technol Directorate, Tokyo, Japan
[2] Nihon Emsco Co Ltd, Tokyo branch Off, Tokyo, Japan
[3] Japan Aerosp Explorat Agcy, Aeronaut Technol Directorate, 6-13-1 Osawa, Mitaka, Tokyo 1810015, Japan
关键词
Structural composites; automated fiber placement technique; defects; stress concentrations; complex variable method; finite element method; PLACEMENT; MICROSTRUCTURE; DEFECTS;
D O I
10.1177/00219983231184590
中图分类号
TB33 [复合材料];
学科分类号
摘要
Tensile tests of quasi-isotropic laminates with a circular open hole, which include a gap in the hole area, were conducted to demonstrate the effect of the gap on the strength. The test showed that the reduction in the open-hole strength owing to the gap was less significant than that in the no-hole tensile strength. A two-dimensional mechanical model of quasi-isotropic laminates with an arbitrary inclined gap was proposed and analytically solved to obtain a closed-form expression for the stress concentration. An approximate expression was provided as the sum of the global uniform stress field and the local stress field near the open hole, which was solved based on a complex variable method. The present analytical solution agrees well with the corresponding two-dimensional finite element solutions. The solution indicated that the stress increase owing to the gap is limited at the stress concentration area. The analytical results were consistent with the experimental results.
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页码:3377 / 3391
页数:15
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