Determination of Interfacial Fracture Toughness in High Temperature Composites

V. T. Bechel, N. Sottos
{"title":"Determination of Interfacial Fracture Toughness in High Temperature Composites","authors":"V. T. Bechel, N. Sottos","doi":"10.1115/imece1996-0475","DOIUrl":null,"url":null,"abstract":"\n Understanding the behavior of the fiber/matrix interface region over a range of temperatures is essential for designing composites that will have a high service temperature. In the current work, the interface failure sequence was observed during fiber pushout tests on two model composites (steel/epoxy and polyester/epoxy) with different Young’s moduli ratio and residual stress values. Novel photoelastic experiments were conducted on the model composites to measure the interfacial crack length versus load during the fiber push-out test. The data were used to better understand the failure mechanisms during the test and to determine the range of applicability of analytical and computational models of the test. Debonding was observed to occur from either the top or the bottom of the sample depending on the ratio of the elastic moduli of the fiber and matrix and the residual stress state. The pushout data from a polyester/epoxy system which debonded from the top was fit to a shear lag solution to obtain the fiber-matrix interfacial toughness (GIIc). The resulting interfacial toughness was then used to check the predicted debond length as a function of pushout force. The debond length calculated from the shear lag model was less than the measured debond length by a nearly constant 1.5 fiber radii which may correspond to the thickness of the surface effects region for polyester/epoxy.\n In the future, the results of the model experiments will be used to understand the interfacial properties of two representative high temperature composites, SiC/Ti-Al-V and Al2O3/Ti-Al-V. A special high temperature apparatus was constructed for performing the push-out test at temperatures ranging from room temperature to 1000°C under vacuum. Performing interfacial measurements at elevated temperatures can be used to optimize interfacial performance at service temperatures and to better evaluate the effects of residual stresses and matrix ductility on fiber debonding and sliding.","PeriodicalId":326220,"journal":{"name":"Aerospace and Materials","volume":null,"pages":null},"PeriodicalIF":0.0000,"publicationDate":"1996-11-17","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Aerospace and Materials","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1115/imece1996-0475","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

Understanding the behavior of the fiber/matrix interface region over a range of temperatures is essential for designing composites that will have a high service temperature. In the current work, the interface failure sequence was observed during fiber pushout tests on two model composites (steel/epoxy and polyester/epoxy) with different Young’s moduli ratio and residual stress values. Novel photoelastic experiments were conducted on the model composites to measure the interfacial crack length versus load during the fiber push-out test. The data were used to better understand the failure mechanisms during the test and to determine the range of applicability of analytical and computational models of the test. Debonding was observed to occur from either the top or the bottom of the sample depending on the ratio of the elastic moduli of the fiber and matrix and the residual stress state. The pushout data from a polyester/epoxy system which debonded from the top was fit to a shear lag solution to obtain the fiber-matrix interfacial toughness (GIIc). The resulting interfacial toughness was then used to check the predicted debond length as a function of pushout force. The debond length calculated from the shear lag model was less than the measured debond length by a nearly constant 1.5 fiber radii which may correspond to the thickness of the surface effects region for polyester/epoxy. In the future, the results of the model experiments will be used to understand the interfacial properties of two representative high temperature composites, SiC/Ti-Al-V and Al2O3/Ti-Al-V. A special high temperature apparatus was constructed for performing the push-out test at temperatures ranging from room temperature to 1000°C under vacuum. Performing interfacial measurements at elevated temperatures can be used to optimize interfacial performance at service temperatures and to better evaluate the effects of residual stresses and matrix ductility on fiber debonding and sliding.
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
高温复合材料界面断裂韧性的测定
了解纤维/基体界面区域在一定温度范围内的行为对于设计具有高使用温度的复合材料至关重要。本研究对不同杨氏模量比和残余应力值的两种模型复合材料(钢/环氧树脂和聚酯/环氧树脂)进行纤维推出试验,观察其界面破坏顺序。在模型复合材料上进行了新型的光弹性实验,以测量纤维推出试验过程中界面裂纹长度与载荷的关系。这些数据用于更好地了解试验过程中的破坏机制,并确定试验分析和计算模型的适用范围。根据纤维和基体的弹性模量和残余应力状态的比值,观察到从样品的顶部或底部发生脱粘。将从顶部剥离的聚酯/环氧树脂体系的推出数据与剪切滞后溶液相匹配,以获得纤维-基体界面韧性(GIIc)。然后用所得的界面韧性来检验预测的脱粘长度作为推力的函数。根据剪切滞后模型计算得到的脱粘长度比实测的脱粘长度小1.5个纤维半径,这可能与聚酯/环氧树脂表面效应区的厚度相对应。在未来,模型实验的结果将用于了解两种具有代表性的高温复合材料,SiC/Ti-Al-V和Al2O3/Ti-Al-V的界面性能。建造了一个特殊的高温装置,用于在室温至1000°C的真空条件下进行推出试验。在高温下进行界面测量可用于优化界面在使用温度下的性能,并更好地评估残余应力和基体延展性对纤维脱粘和滑动的影响。
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
Determination of Interfacial Fracture Toughness in High Temperature Composites Fatigue Damage Evolution in a Short Fiber Reinforced Metal Matrix Composite Modeling of Porosity Effects in Gas-Filled Composites Using Biot’s Parameter A Systematic Shear-Lag Approach for Analyzing the Failure Mechanisms in Ceramic Matrix Composites Dislocation Punching in Functionally-Graded Materials
×
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