Studies on impact damage resistance of affordable stitched woven carbon/epoxy composite laminates

被引:37
作者
Hosur, MV [1 ]
Adya, M
Alexander, J
Jeelani, S
Vaidya, U
Mayer, A
机构
[1] Tuskegee Univ, Ctr Adv Mat, Tuskegee, AL 36088 USA
[2] Univ Alabama Birmingham, Dept Mech & Mat Engn, Birmingham, AL 35294 USA
[3] USAF, Struct Design & Dev Branch VASD, Res Lab, Wright Patterson AFB, OH 45433 USA
关键词
affordable manufacturing; woven fabric composites; low-velocity impact; damage resistance; stitching; ultrasonics;
D O I
10.1177/0731684403022010005
中图分类号
TB33 [复合材料];
学科分类号
摘要
This paper discusses the response of seven layer plain and satin weave carbon fabric reinforced composites fabricated using low-cost Vacuum Assisted Resin Infusion Molding (VARIM) process under low-velocity impact loading. Both stitched and unstitched laminates were tested at energy levels ranging 5-50 J using an instrumented drop-weight machine. A 3-cord Kevlar thread was used to stitch the laminate in two orthogonal grid patterns each at a 6 mm pitch: one with 25.4 mm and the other with 12.7 mm grid. Damage due to impact loading was evaluated through ultrasonic nondestructive evaluation (NDE). Results of the study showed the effectiveness of stitching in containing the damage size with 12.7 mm grid stitch samples exhibiting the least damage. Further, satin weave fabric composites exhibit better impact resistance as compared to plain weave fabric composites.
引用
收藏
页码:927 / 952
页数:26
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