带有表面玻璃纤维的碳纤维复合材料层压板的低速冲击响应

IF 2.3 4区 材料科学 Q3 MATERIALS SCIENCE, COMPOSITES
Longquan Xue, Songze Yang, Zhiquan He, Rong Wang, Yangyan Zheng, Nian Li, Kai Zheng, Yi Ren
{"title":"带有表面玻璃纤维的碳纤维复合材料层压板的低速冲击响应","authors":"Longquan Xue, Songze Yang, Zhiquan He, Rong Wang, Yangyan Zheng, Nian Li, Kai Zheng, Yi Ren","doi":"10.1007/s10443-024-10259-4","DOIUrl":null,"url":null,"abstract":"<p>The sensitivity of carbon fiber composite laminate to impact damage makes impact damage a significant cause of composite material performance degradation. This study aims to investigate the influence of surface glass fibers on carbon fiber composite laminates under low-velocity impact. A user-defined VUMAT subroutine based on the Puck criterion was employed to implement an intralaminar damage model, while a bilinear cohesive model based on quadratic criterion in Abaqus was used to simulate interlaminar damage. By simulating the low-velocity impact behavior of carbon fiber laminates under three energy levels (2 J, 4 J, and 8 J), the predicted mechanical response results were compared with the experimental results from the literature to validate the rationality of the model. The mechanical response and damage evolution under impact loading were studied by adding glass fibers of different angles and thicknesses on the surface layer of carbon fiber laminate. The results show that increasing the thickness of surface glass fibers can effectively enhance the impact resistance of carbon fiber composite laminates, and a single layer glass fibers at 90° provides better protection than at 45°. The results of this study are instructive for the selection of the thickness as well as the angle of the glass fibers on the surface of carbon fiber composite laminates.</p>","PeriodicalId":468,"journal":{"name":"Applied Composite Materials","volume":"109 1","pages":""},"PeriodicalIF":2.3000,"publicationDate":"2024-08-29","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Low Velocity Impact Response of Carbon Fiber Composite Laminates with Surface Glass Fibers\",\"authors\":\"Longquan Xue, Songze Yang, Zhiquan He, Rong Wang, Yangyan Zheng, Nian Li, Kai Zheng, Yi Ren\",\"doi\":\"10.1007/s10443-024-10259-4\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"<p>The sensitivity of carbon fiber composite laminate to impact damage makes impact damage a significant cause of composite material performance degradation. This study aims to investigate the influence of surface glass fibers on carbon fiber composite laminates under low-velocity impact. A user-defined VUMAT subroutine based on the Puck criterion was employed to implement an intralaminar damage model, while a bilinear cohesive model based on quadratic criterion in Abaqus was used to simulate interlaminar damage. By simulating the low-velocity impact behavior of carbon fiber laminates under three energy levels (2 J, 4 J, and 8 J), the predicted mechanical response results were compared with the experimental results from the literature to validate the rationality of the model. The mechanical response and damage evolution under impact loading were studied by adding glass fibers of different angles and thicknesses on the surface layer of carbon fiber laminate. The results show that increasing the thickness of surface glass fibers can effectively enhance the impact resistance of carbon fiber composite laminates, and a single layer glass fibers at 90° provides better protection than at 45°. The results of this study are instructive for the selection of the thickness as well as the angle of the glass fibers on the surface of carbon fiber composite laminates.</p>\",\"PeriodicalId\":468,\"journal\":{\"name\":\"Applied Composite Materials\",\"volume\":\"109 1\",\"pages\":\"\"},\"PeriodicalIF\":2.3000,\"publicationDate\":\"2024-08-29\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Applied Composite Materials\",\"FirstCategoryId\":\"88\",\"ListUrlMain\":\"https://doi.org/10.1007/s10443-024-10259-4\",\"RegionNum\":4,\"RegionCategory\":\"材料科学\",\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"Q3\",\"JCRName\":\"MATERIALS SCIENCE, COMPOSITES\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Applied Composite Materials","FirstCategoryId":"88","ListUrlMain":"https://doi.org/10.1007/s10443-024-10259-4","RegionNum":4,"RegionCategory":"材料科学","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q3","JCRName":"MATERIALS SCIENCE, COMPOSITES","Score":null,"Total":0}
引用次数: 0

摘要

碳纤维复合材料层压板对冲击损伤的敏感性使冲击损伤成为复合材料性能退化的重要原因。本研究旨在探讨低速冲击下表面玻璃纤维对碳纤维复合材料层压板的影响。研究采用了基于帕克准则的用户自定义 VUMAT 子程序来实现层内损伤模型,同时使用 Abaqus 中基于二次准则的双线性内聚模型来模拟层间损伤。通过模拟碳纤维层板在三种能量水平(2 J、4 J 和 8 J)下的低速冲击行为,将预测的力学响应结果与文献中的实验结果进行比较,以验证模型的合理性。通过在碳纤维层压板表层添加不同角度和厚度的玻璃纤维,研究了冲击载荷下的机械响应和损伤演变。结果表明,增加表层玻璃纤维的厚度可有效提高碳纤维复合材料层压板的抗冲击性能,而单层 90° 玻璃纤维比 45° 玻璃纤维能提供更好的保护。该研究结果对选择碳纤维复合材料层压板表面玻璃纤维的厚度和角度具有指导意义。
本文章由计算机程序翻译,如有差异,请以英文原文为准。

Low Velocity Impact Response of Carbon Fiber Composite Laminates with Surface Glass Fibers

Low Velocity Impact Response of Carbon Fiber Composite Laminates with Surface Glass Fibers

The sensitivity of carbon fiber composite laminate to impact damage makes impact damage a significant cause of composite material performance degradation. This study aims to investigate the influence of surface glass fibers on carbon fiber composite laminates under low-velocity impact. A user-defined VUMAT subroutine based on the Puck criterion was employed to implement an intralaminar damage model, while a bilinear cohesive model based on quadratic criterion in Abaqus was used to simulate interlaminar damage. By simulating the low-velocity impact behavior of carbon fiber laminates under three energy levels (2 J, 4 J, and 8 J), the predicted mechanical response results were compared with the experimental results from the literature to validate the rationality of the model. The mechanical response and damage evolution under impact loading were studied by adding glass fibers of different angles and thicknesses on the surface layer of carbon fiber laminate. The results show that increasing the thickness of surface glass fibers can effectively enhance the impact resistance of carbon fiber composite laminates, and a single layer glass fibers at 90° provides better protection than at 45°. The results of this study are instructive for the selection of the thickness as well as the angle of the glass fibers on the surface of carbon fiber composite laminates.

求助全文
通过发布文献求助,成功后即可免费获取论文全文。 去求助
来源期刊
Applied Composite Materials
Applied Composite Materials 工程技术-材料科学:复合
CiteScore
4.20
自引率
4.30%
发文量
81
审稿时长
1.6 months
期刊介绍: Applied Composite Materials is an international journal dedicated to the publication of original full-length papers, review articles and short communications of the highest quality that advance the development and application of engineering composite materials. Its articles identify problems that limit the performance and reliability of the composite material and composite part; and propose solutions that lead to innovation in design and the successful exploitation and commercialization of composite materials across the widest spectrum of engineering uses. The main focus is on the quantitative descriptions of material systems and processing routes. Coverage includes management of time-dependent changes in microscopic and macroscopic structure and its exploitation from the material''s conception through to its eventual obsolescence.
×
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:481959085
Book学术官方微信