Compression After Impact Testing of Carbon Fiber Reinforced Plastic Laminates

M. Hosur, C. Murthy, T. S. Ramurthy
{"title":"Compression After Impact Testing of Carbon Fiber Reinforced Plastic Laminates","authors":"M. Hosur, C. Murthy, T. S. Ramurthy","doi":"10.1520/CTR10947J","DOIUrl":null,"url":null,"abstract":"Carbon fiber reinforced plastic (CFRP) composite laminates are susceptible for multiple delaminations, which reduce the compressive strength significantly even when the impact load is insufficient to cause visible damage. The post-impact compression test is used widely to assess the relative performance of different composite laminates with different fiber matrix combinations. In the present work, CFRP (T300/914) laminates were subjected to low-velocity impact loading simulating tool drops and runway debris. Compression after impact (CAI) tests were performed using fixtures as per NASA specifications. Results obtained indicate definite correlation between impact energy, failure strain, and residual compressive strength.","PeriodicalId":15514,"journal":{"name":"Journal of Composites Technology & Research","volume":"67 1","pages":"51-64"},"PeriodicalIF":0.0000,"publicationDate":"1999-04-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"11","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Journal of Composites Technology & Research","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1520/CTR10947J","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 11

Abstract

Carbon fiber reinforced plastic (CFRP) composite laminates are susceptible for multiple delaminations, which reduce the compressive strength significantly even when the impact load is insufficient to cause visible damage. The post-impact compression test is used widely to assess the relative performance of different composite laminates with different fiber matrix combinations. In the present work, CFRP (T300/914) laminates were subjected to low-velocity impact loading simulating tool drops and runway debris. Compression after impact (CAI) tests were performed using fixtures as per NASA specifications. Results obtained indicate definite correlation between impact energy, failure strain, and residual compressive strength.
碳纤维增强塑料层压板冲击后压缩性能试验
碳纤维增强塑料(CFRP)复合材料层合板易发生多次分层,即使在冲击载荷不足以造成可见损伤的情况下,也会显著降低其抗压强度。冲击后压缩试验被广泛用于评价不同纤维基组合的复合材料层合板的相对性能。在本工作中,CFRP (T300/914)层压板进行了低速冲击加载模拟工具掉落和跑道碎片。撞击后压缩(CAI)测试使用夹具按照NASA规范进行。结果表明,冲击能、破坏应变和残余抗压强度之间存在一定的相关性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
求助全文
约1分钟内获得全文 求助全文
来源期刊
自引率
0.00%
发文量
0
×
引用
GB/T 7714-2015
复制
MLA
复制
APA
复制
导出至
BibTeX EndNote RefMan NoteFirst NoteExpress
×
提示
您的信息不完整,为了账户安全,请先补充。
现在去补充
×
提示
您因"违规操作"
具体请查看互助需知
我知道了
×
提示
确定
请完成安全验证×
copy
已复制链接
快去分享给好友吧!
我知道了
右上角分享
点击右上角分享
0
联系我们:info@booksci.cn Book学术提供免费学术资源搜索服务,方便国内外学者检索中英文文献。致力于提供最便捷和优质的服务体验。 Copyright © 2023 布克学术 All rights reserved.
京ICP备2023020795号-1
ghs 京公网安备 11010802042870号
Book学术文献互助
Book学术文献互助群
群 号:604180095
Book学术官方微信