Micromechanical Analysis of Nonlinear Response of Unidirectional Composites: A Fundamental Approach

V. Jadhav, S. Sridharan
{"title":"Micromechanical Analysis of Nonlinear Response of Unidirectional Composites: A Fundamental Approach","authors":"V. Jadhav, S. Sridharan","doi":"10.1115/imece2001/ad-25315","DOIUrl":null,"url":null,"abstract":"\n Micromechanical models with different representative volume elements have been developed to study their ability to predict nonlinear response of unidirectional composites. A simple, square cells type micro-mechanical model similar to those widely used by other researchers is compared with a more advanced 3-phase finite element based micro-mechanical model. The models utilize the “bulk” properties of the matrix without attempting to “tune” the model to fit with experimental response of laminae. This is a more fundamental approach and constitutes a departure from current practice. The models account for shear softening, matrix cracking and the presence of residual stresses. A smeared cracking approach was used to characterize the micro-cracking in matrix. Experimental studies were performed on laminae, laminates and cylinders made from carbon epoxy composites. Experimental comparisons show that the more accurate micro-mechanical model with proper partial cracking options provides good bounds on experimental response with consistent accuracy. A square cells type model however is not consistent in its predictions, thus raising questions about its applicability in any general micro-mechanics based analysis.","PeriodicalId":442756,"journal":{"name":"Damage Initiation and Prediction in Composites, Sandwich Structures and Thermal Barrier Coatings","volume":"8 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2001-11-11","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Damage Initiation and Prediction in Composites, Sandwich Structures and Thermal Barrier Coatings","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1115/imece2001/ad-25315","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 0

Abstract

Micromechanical models with different representative volume elements have been developed to study their ability to predict nonlinear response of unidirectional composites. A simple, square cells type micro-mechanical model similar to those widely used by other researchers is compared with a more advanced 3-phase finite element based micro-mechanical model. The models utilize the “bulk” properties of the matrix without attempting to “tune” the model to fit with experimental response of laminae. This is a more fundamental approach and constitutes a departure from current practice. The models account for shear softening, matrix cracking and the presence of residual stresses. A smeared cracking approach was used to characterize the micro-cracking in matrix. Experimental studies were performed on laminae, laminates and cylinders made from carbon epoxy composites. Experimental comparisons show that the more accurate micro-mechanical model with proper partial cracking options provides good bounds on experimental response with consistent accuracy. A square cells type model however is not consistent in its predictions, thus raising questions about its applicability in any general micro-mechanics based analysis.
查看原文
分享 分享
微信好友 朋友圈 QQ好友 复制链接
本刊更多论文
单向复合材料非线性响应的微观力学分析:一种基本方法
建立了具有不同代表性体积元的微力学模型,研究了其预测单向复合材料非线性响应的能力。将其他研究人员广泛使用的简单的方形单元微力学模型与更先进的基于三相有限元的微力学模型进行了比较。该模型利用了基体的“体积”特性,而没有试图“调整”模型以适应层状材料的实验响应。这是一种更基本的办法,背离了目前的做法。这些模型考虑了剪切软化、基体开裂和残余应力的存在。采用涂抹裂纹法对基体微裂纹进行表征。对碳-环氧复合材料的层板、层压板和圆柱体进行了实验研究。实验结果表明,在适当的局部开裂选项下,更精确的微力学模型提供了良好的实验响应边界,且精度一致。然而,方形单元格类型模型在其预测中并不一致,因此提出了关于其在任何一般微观力学分析中的适用性的问题。
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 去求助
来源期刊
自引率
0.00%
发文量
0
期刊最新文献
Photo-Stimulated Luminescence Piezo-Spectroscopy Measurement on a EB-PVD 7YSZ/(Ni, Pt)Al/CMSX-4 TBC System Dynamic Response of Sandwich Anisotropic Flat Panels to Explosive Pressure Pulses Novel Concept of Advanced Thermal Protection Coating Based on Fullerenes Micromechanical Analysis of Nonlinear Response of Unidirectional Composites: A Fundamental Approach Failure of Composites Under Combined Loading
×
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
现在去查看 取消
×
提示
确定
0
微信
客服QQ
Book学术公众号 扫码关注我们
反馈
×
意见反馈
请填写您的意见或建议
请填写您的手机或邮箱
已复制链接
已复制链接
快去分享给好友吧!
我知道了
×
扫码分享
扫码分享
Book学术官方微信
Book学术文献互助
Book学术文献互助群
群 号:481959085
Book学术
文献互助 智能选刊 最新文献 互助须知 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 Book学术 All rights reserved.
ghs 京公网安备 11010802042870号 京ICP备2023020795号-1