Failure configuration and evaluation of hybrid CFRP-GFRP laminates using innovative Arcan fixture: Experimental and simulation approach

IF 5.3 Q2 MATERIALS SCIENCE, COMPOSITES
Ariyana Dwiputra Nugraha , Daffa Alandro , Kevin Gausultan Hadith Mangunkusumo , Muhammad Kusni , Yi Chieh Wu , Muhammad Akhsin Muflikhun
{"title":"Failure configuration and evaluation of hybrid CFRP-GFRP laminates using innovative Arcan fixture: Experimental and simulation approach","authors":"Ariyana Dwiputra Nugraha ,&nbsp;Daffa Alandro ,&nbsp;Kevin Gausultan Hadith Mangunkusumo ,&nbsp;Muhammad Kusni ,&nbsp;Yi Chieh Wu ,&nbsp;Muhammad Akhsin Muflikhun","doi":"10.1016/j.jcomc.2024.100452","DOIUrl":null,"url":null,"abstract":"<div><p>This study successfully explored and evaluated the impact of notches modification in U, V, and square shapes on both tensile and shear strength using Arcan fixture. ASTM <span>D</span><svg><path></path></svg> 5379 was incorporated to evaluate the model then compared with FEA simulation. Composite material featuring a U-shaped notch possesses a notable advantage in terms of its tensile strength and shear strength values, which measure at 276.3 MPa and 14.9 MPa, respectively. 3D Hashin's damage model also employed to compare and validate the shear damage resulting from each notch of the experimental work. The composite with a U-shaped notch demonstrates excellent capacity for withstanding both tensile and shear loading without compromising its strength and fracture resistance in shear. the failure mode analysis was showed that the matrix failure tent to make weaker of the specimen, although the fiber still stands and kinked. The present study can be used as the leading method to evaluate the hybrid laminates applied in wind turbines, automotives body structures, and aircraft structures.</p></div>","PeriodicalId":34525,"journal":{"name":"Composites Part C Open Access","volume":"14 ","pages":"Article 100452"},"PeriodicalIF":5.3000,"publicationDate":"2024-03-15","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"https://www.sciencedirect.com/science/article/pii/S2666682024000239/pdfft?md5=0e0e56a85a9f3acb8e98053483f06c60&pid=1-s2.0-S2666682024000239-main.pdf","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Composites Part C Open Access","FirstCategoryId":"1085","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S2666682024000239","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q2","JCRName":"MATERIALS SCIENCE, COMPOSITES","Score":null,"Total":0}
引用次数: 0

Abstract

This study successfully explored and evaluated the impact of notches modification in U, V, and square shapes on both tensile and shear strength using Arcan fixture. ASTM D 5379 was incorporated to evaluate the model then compared with FEA simulation. Composite material featuring a U-shaped notch possesses a notable advantage in terms of its tensile strength and shear strength values, which measure at 276.3 MPa and 14.9 MPa, respectively. 3D Hashin's damage model also employed to compare and validate the shear damage resulting from each notch of the experimental work. The composite with a U-shaped notch demonstrates excellent capacity for withstanding both tensile and shear loading without compromising its strength and fracture resistance in shear. the failure mode analysis was showed that the matrix failure tent to make weaker of the specimen, although the fiber still stands and kinked. The present study can be used as the leading method to evaluate the hybrid laminates applied in wind turbines, automotives body structures, and aircraft structures.

Abstract Image

使用创新型 Arcan 夹具对 CFRP-GFRP 混合层压板进行失效配置和评估:实验和模拟方法
这项研究使用 Arcan 夹具成功地探索和评估了 U 形、V 形和方形凹槽对拉伸和剪切强度的影响。研究采用 ASTM D 5379 标准对模型进行评估,然后与有限元分析模拟进行比较。具有 U 形缺口的复合材料在拉伸强度和剪切强度值方面具有明显优势,分别达到 276.3 兆帕和 14.9 兆帕。此外,还采用了三维 Hashin 损伤模型来比较和验证实验工作中每个缺口造成的剪切损伤。失效模式分析显示,虽然纤维仍然存在并扭结,但基体失效帐篷使试样变得更脆弱。本研究可作为评估应用于风力涡轮机、汽车车身结构和飞机结构的混合层压板的主要方法。
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
Composites Part C Open Access
Composites Part C Open Access Engineering-Mechanical Engineering
CiteScore
8.60
自引率
2.40%
发文量
96
审稿时长
55 days
×
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