Understanding effectiveness of stitching in suppression of impact damage: An empirical delamination reduction trend for stitched composites

被引:36
作者
Tan, K. T. [1 ]
Watanabe, N. [2 ]
Iwahori, Y. [3 ]
Ishikawa, T. [4 ]
机构
[1] Purdue Univ, Sch Aeronaut & Astronaut, W Lafayette, IN 47907 USA
[2] Tokyo Metropolitan Univ, Dept Aerosp Engn, Hino, Tokyo 1910065, Japan
[3] Japan Aerosp Explorat Agcy, Adv Composite Technol Ctr, Mitaka, Tokyo 1810015, Japan
[4] Japan Aerosp Explorat Agcy, Aviat Program Grp, Aerosp Res & Dev Directorate, Chofu, Tokyo 1828522, Japan
关键词
Stitching; Impact behavior; Damage tolerance; Delamination; LOW-VELOCITY IMPACT; INTERLAMINAR FRACTURE-TOUGHNESS; MIXED-MODE DELAMINATION; LAMINATED COMPOSITES; LAP JOINTS; T-JOINTS; BEHAVIOR; WOVEN; RESISTANCE; SINGLE;
D O I
10.1016/j.compositesa.2011.12.022
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
In this paper, a novel empirical trend has been identified to understand the delamination reduction in stitched composites subjected to impact loading. This empirical-based Delamination Reduction Trend (DRT) is developed based on an extensive series of low-velocity impact tests using specimens of different laminate thicknesses, stitch densities and stitch thread linear (mass) densities, subjected over a range of impact energy levels. The DRT simply relates two parameters: normalized delamination area (Delam(Norm)) and stitch fiber volume fraction (V-ft), to characterize the effectiveness of stitching in impact damage suppression. DRT evidently shows a bi-linear behavior: first, an initial linearly decreasing relationship of Delam(Norm) with V-ft; and second, a plateau which indicates maximum delamination area reduction limit of 40% by stitching. Experimentally observed mechanisms are presented and discussed with the aim to justify and explain the bi-linear behavior of DRT. The DRT is further validated with numerous published literature results and has demonstrated excellent agreement. (C) 2011 Elsevier Ltd. All rights reserved.
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页码:823 / 832
页数:10
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