Failure of Stitched Composite L-Joints Under Tensile Loading - Experiment and Simulation

被引:19
作者
Wood, Michael D. K. [1 ,2 ]
Tong, Liyong [1 ]
Luo, Quantian [1 ]
Sun, Xiannian [1 ,3 ]
Katzos, Anthony [4 ]
Rispler, Adrian R. [4 ]
机构
[1] Univ Sydney, Sch Aerosp Mech & Mechatron Engn, Sydney, NSW 2006, Australia
[2] Univ S Pacific, Sch Phys & Engn, Suva, Fiji
[3] Dalian Maritime Univ, Coll Electromech & Mat Engn, Dalian 116026, Peoples R China
[4] Hawker Havilland Aerosp Pty Ltd, Port Melbourne, Vic, Australia
基金
澳大利亚研究理事会;
关键词
stitched CFRP; delamination; finite element analysis; L-joint testing; I DELAMINATION TOUGHNESS; INTERLOCKED FABRIC COMPOSITES; SINGLE-LAP JOINTS; LAMINATED COMPOSITES; COMPRESSION; BEHAVIOR; FRACTURE; DAMAGE;
D O I
10.1177/0731684407086969
中图分类号
TB33 [复合材料];
学科分类号
摘要
This article presents an experimental and numerical investigation into the influence of transverse stitching on failure of composite L-joints under tensile loading. Six unstitched and six stitched L-joint specimens were manufactured and tested under quasi static tensile loading. It was observed that the average measured failure load and the associated crosshead displacement for the stitched L-joint specimens are increased significantly compared to those for the unstitched specimens. Full 3D and 2D plane strain finite element (FE) models were developed to simulate both stitched and unstitched L-joints with an implemented stitch element. The load-displacement curves and results predicted via FE models compare favorably with the experimental results. For the stitched L-joints, it is shown that the observed delamination in the elbow region of the flange can be modeled by using a softening model for epoxy layer.
引用
收藏
页码:715 / 742
页数:28
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