界面粘合对黄麻纤维/环氧聚合物复合材料低速冲击性能的影响

IF 3.2 3区 材料科学 Q2 ENGINEERING, CHEMICAL
M. Manoj Prabhakar , N. Rajini , K. Mayandi , Nadir Ayrilmis , Mahmood M.S. Abdullah , Faruq Mohammad , Kumar Krishnan , Ahmed A. Soleiman
{"title":"界面粘合对黄麻纤维/环氧聚合物复合材料低速冲击性能的影响","authors":"M. Manoj Prabhakar ,&nbsp;N. Rajini ,&nbsp;K. Mayandi ,&nbsp;Nadir Ayrilmis ,&nbsp;Mahmood M.S. Abdullah ,&nbsp;Faruq Mohammad ,&nbsp;Kumar Krishnan ,&nbsp;Ahmed A. Soleiman","doi":"10.1016/j.ijadhadh.2024.103833","DOIUrl":null,"url":null,"abstract":"<div><p>This research aimed to analyze the low-velocity impact on jute/epoxy polymer samples and used their fractured samples for computer tomographic (CT) analysis for predicting the impact damage areas developed on jute/epoxy polymer by using its impact images. The computer tomography analysis was performed with two different thicknesses of natural fabric composites. Initially, this developed the jute/epoxy polymer composites using Compression molding techniques with different thickness and these fabricated samples undergoes to analyzed the low-velocity impact strength with an automated data acquisition system on different thicknesses of jute fabric-reinforced polymer composite materials. The fabricated composite plates were tested under the low-velocity impact testing method with different loading conditions. The higher impact strength was observed on the 6 mm thickness of the plate. The impact analysis on laminate materials is performed with different energy levels on the same thickness of the plate individually. Among various energy absorption tests, the 10 J created more damage on the 3 mm thick plate and 15 J created more damage on the 6 mm thick plate. After the impact testing, the samples were analyzed in the damaged areas using CT scanning systems. Based on this analysis, the fabricated materials were best-suited for lightweight application areas.</p></div>","PeriodicalId":13732,"journal":{"name":"International Journal of Adhesion and Adhesives","volume":"135 ","pages":"Article 103833"},"PeriodicalIF":3.2000,"publicationDate":"2024-09-05","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Effect of interfacial bonding on the low velocity impact performance of jute fibre/epoxy polymer composites\",\"authors\":\"M. Manoj Prabhakar ,&nbsp;N. Rajini ,&nbsp;K. Mayandi ,&nbsp;Nadir Ayrilmis ,&nbsp;Mahmood M.S. Abdullah ,&nbsp;Faruq Mohammad ,&nbsp;Kumar Krishnan ,&nbsp;Ahmed A. Soleiman\",\"doi\":\"10.1016/j.ijadhadh.2024.103833\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"<div><p>This research aimed to analyze the low-velocity impact on jute/epoxy polymer samples and used their fractured samples for computer tomographic (CT) analysis for predicting the impact damage areas developed on jute/epoxy polymer by using its impact images. The computer tomography analysis was performed with two different thicknesses of natural fabric composites. Initially, this developed the jute/epoxy polymer composites using Compression molding techniques with different thickness and these fabricated samples undergoes to analyzed the low-velocity impact strength with an automated data acquisition system on different thicknesses of jute fabric-reinforced polymer composite materials. The fabricated composite plates were tested under the low-velocity impact testing method with different loading conditions. The higher impact strength was observed on the 6 mm thickness of the plate. The impact analysis on laminate materials is performed with different energy levels on the same thickness of the plate individually. Among various energy absorption tests, the 10 J created more damage on the 3 mm thick plate and 15 J created more damage on the 6 mm thick plate. After the impact testing, the samples were analyzed in the damaged areas using CT scanning systems. Based on this analysis, the fabricated materials were best-suited for lightweight application areas.</p></div>\",\"PeriodicalId\":13732,\"journal\":{\"name\":\"International Journal of Adhesion and Adhesives\",\"volume\":\"135 \",\"pages\":\"Article 103833\"},\"PeriodicalIF\":3.2000,\"publicationDate\":\"2024-09-05\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"International Journal of Adhesion and Adhesives\",\"FirstCategoryId\":\"88\",\"ListUrlMain\":\"https://www.sciencedirect.com/science/article/pii/S014374962400215X\",\"RegionNum\":3,\"RegionCategory\":\"材料科学\",\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"Q2\",\"JCRName\":\"ENGINEERING, CHEMICAL\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"International Journal of Adhesion and Adhesives","FirstCategoryId":"88","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S014374962400215X","RegionNum":3,"RegionCategory":"材料科学","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q2","JCRName":"ENGINEERING, CHEMICAL","Score":null,"Total":0}
引用次数: 0

摘要

本研究旨在分析黄麻/环氧聚合物样品受到的低速冲击,并利用其断裂样品进行计算机断层扫描(CT)分析,通过其冲击图像预测黄麻/环氧聚合物上形成的冲击损伤区域。计算机断层扫描分析使用了两种不同厚度的天然织物复合材料。最初,研究人员利用压缩成型技术开发了不同厚度的黄麻/环氧聚合物复合材料,并利用自动数据采集系统对这些制成的样品进行了低速冲击强度分析,分析了不同厚度的黄麻织物增强聚合物复合材料。在不同的加载条件下,采用低速冲击试验方法对制作的复合材料板进行了测试。在厚度为 6 毫米的板材上观察到了较高的冲击强度。对层压材料的冲击分析是在相同厚度的板材上以不同的能量水平单独进行的。在各种能量吸收测试中,10 焦耳的能量对 3 毫米厚的板材造成的破坏更大,而 15 焦耳的能量对 6 毫米厚的板材造成的破坏更大。冲击测试结束后,使用 CT 扫描系统对样品的受损区域进行了分析。根据分析结果,制造的材料最适合用于轻质应用领域。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Effect of interfacial bonding on the low velocity impact performance of jute fibre/epoxy polymer composites

This research aimed to analyze the low-velocity impact on jute/epoxy polymer samples and used their fractured samples for computer tomographic (CT) analysis for predicting the impact damage areas developed on jute/epoxy polymer by using its impact images. The computer tomography analysis was performed with two different thicknesses of natural fabric composites. Initially, this developed the jute/epoxy polymer composites using Compression molding techniques with different thickness and these fabricated samples undergoes to analyzed the low-velocity impact strength with an automated data acquisition system on different thicknesses of jute fabric-reinforced polymer composite materials. The fabricated composite plates were tested under the low-velocity impact testing method with different loading conditions. The higher impact strength was observed on the 6 mm thickness of the plate. The impact analysis on laminate materials is performed with different energy levels on the same thickness of the plate individually. Among various energy absorption tests, the 10 J created more damage on the 3 mm thick plate and 15 J created more damage on the 6 mm thick plate. After the impact testing, the samples were analyzed in the damaged areas using CT scanning systems. Based on this analysis, the fabricated materials were best-suited for lightweight application areas.

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
International Journal of Adhesion and Adhesives
International Journal of Adhesion and Adhesives 工程技术-材料科学:综合
CiteScore
6.90
自引率
8.80%
发文量
200
审稿时长
8.3 months
期刊介绍: The International Journal of Adhesion and Adhesives draws together the many aspects of the science and technology of adhesive materials, from fundamental research and development work to industrial applications. Subject areas covered include: interfacial interactions, surface chemistry, methods of testing, accumulation of test data on physical and mechanical properties, environmental effects, new adhesive materials, sealants, design of bonded joints, and manufacturing technology.
×
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