Ballistic impact behavior of hybrid composites

被引:129
|
作者
Pandya, Kedar S. [1 ]
Pothnis, Jayaram R. [1 ]
Ravikumar, G. [1 ]
Naik, N. K. [1 ]
机构
[1] Indian Inst Technol, Dept Aerosp Engn, Bombay 400076, Maharashtra, India
来源
MATERIALS & DESIGN | 2013年 / 44卷
关键词
HIGH-VELOCITY IMPACT; WOVEN FABRIC COMPOSITES; THICK COMPOSITES; SANDWICH PANELS; PERFORMANCE; PLATES; PERFORATION; FORMULATION; CORE;
D O I
10.1016/j.matdes.2012.07.044
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Experimental studies are presented on ballistic impact behavior of hybrid composites. The materials considered for the studies are four types of symmetric hybrid composites made using plain weave E-glass fabric and 8H satin weave T300 carbon fabric with epoxy resin. Studies are also carried out on plain weave E-glass/epoxy and 8H satin weave T300 carbon/epoxy for comparison. It is observed that ballistic limit velocity, V-50 can be increased for the composites by adding E-glass layers to T300 carbon layers compared with only carbon composites for the same laminate thickness. Placing E-glass layers in the exterior and carbon layers in the interior provides higher ballistic limit velocity than placing carbon layers in the exterior and E-glass layers in the interior. Experimental damage patterns during ballistic impact have been obtained for the materials considered. (C) 2012 Elsevier Ltd. All rights reserved.
引用
收藏
页码:128 / 135
页数:8
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