对II型疲劳裂纹扩展的认识

IF 0.2 4区 工程技术 Q4 NUCLEAR SCIENCE & TECHNOLOGY
Michael C. Smith, Roderick A. Smith
{"title":"对II型疲劳裂纹扩展的认识","authors":"Michael C. Smith, Roderick A. Smith","doi":"10.1520/STP23220S","DOIUrl":null,"url":null,"abstract":"The Mode II crack flank displacement and crack growth responses of three precracked specimens made from structural steel were measured, using plastic replicas and a crack-tip compliance gage. Crack surface interaction wasfound to dominate behavior: at low stress intensity range (ΔK I I n o m = 9 MPa √m) the precracks did not suffer reversed slip to their tips and no crack growth occurred, while at high stress intensity range (ΔK I I n o m = 19 MPa √m) the effective stress intensity range was less than half that nominally applied. Three sources of crack flank frictional attenuation were identified: compressive residual stresses due to precracking, Mode I wedging over asperities, and gross plastic deformation of interlocking asperities. The measured unlocking response was modeled successfully by assuming that crack flank frictional stresses obeyed a constant interfacial shear stress friction law.","PeriodicalId":55585,"journal":{"name":"Atw-International Journal for Nuclear Power","volume":"33 1","pages":"260-280"},"PeriodicalIF":0.2000,"publicationDate":"1988-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"43","resultStr":"{\"title\":\"Toward an understanding of Mode II fatigue crack growth\",\"authors\":\"Michael C. Smith, Roderick A. Smith\",\"doi\":\"10.1520/STP23220S\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"The Mode II crack flank displacement and crack growth responses of three precracked specimens made from structural steel were measured, using plastic replicas and a crack-tip compliance gage. Crack surface interaction wasfound to dominate behavior: at low stress intensity range (ΔK I I n o m = 9 MPa √m) the precracks did not suffer reversed slip to their tips and no crack growth occurred, while at high stress intensity range (ΔK I I n o m = 19 MPa √m) the effective stress intensity range was less than half that nominally applied. Three sources of crack flank frictional attenuation were identified: compressive residual stresses due to precracking, Mode I wedging over asperities, and gross plastic deformation of interlocking asperities. The measured unlocking response was modeled successfully by assuming that crack flank frictional stresses obeyed a constant interfacial shear stress friction law.\",\"PeriodicalId\":55585,\"journal\":{\"name\":\"Atw-International Journal for Nuclear Power\",\"volume\":\"33 1\",\"pages\":\"260-280\"},\"PeriodicalIF\":0.2000,\"publicationDate\":\"1988-01-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"43\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Atw-International Journal for Nuclear Power\",\"FirstCategoryId\":\"5\",\"ListUrlMain\":\"https://doi.org/10.1520/STP23220S\",\"RegionNum\":4,\"RegionCategory\":\"工程技术\",\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"Q4\",\"JCRName\":\"NUCLEAR SCIENCE & TECHNOLOGY\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Atw-International Journal for Nuclear Power","FirstCategoryId":"5","ListUrlMain":"https://doi.org/10.1520/STP23220S","RegionNum":4,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q4","JCRName":"NUCLEAR SCIENCE & TECHNOLOGY","Score":null,"Total":0}
引用次数: 43

摘要

采用塑性模型和裂纹尖端柔度仪测量了3个结构钢预制裂纹试件的II型裂纹侧面位移和裂纹扩展响应。在低应力强度范围内(ΔK I I I I nom = 9 MPa√m),预裂纹不会发生向尖端的反向滑移,也不会发生裂纹扩展;而在高应力强度范围内(ΔK I I I nom = 19 MPa√m),预裂纹的有效应力强度范围不到名义上应用的一半。确定了裂纹侧面摩擦衰减的三个来源:预裂引起的压残余应力,在凸起上的I型楔入,以及互锁凸起的总塑性变形。假设裂纹侧面的摩擦应力服从恒定的界面剪应力摩擦规律,成功地模拟了实测的解锁响应。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Toward an understanding of Mode II fatigue crack growth
The Mode II crack flank displacement and crack growth responses of three precracked specimens made from structural steel were measured, using plastic replicas and a crack-tip compliance gage. Crack surface interaction wasfound to dominate behavior: at low stress intensity range (ΔK I I n o m = 9 MPa √m) the precracks did not suffer reversed slip to their tips and no crack growth occurred, while at high stress intensity range (ΔK I I n o m = 19 MPa √m) the effective stress intensity range was less than half that nominally applied. Three sources of crack flank frictional attenuation were identified: compressive residual stresses due to precracking, Mode I wedging over asperities, and gross plastic deformation of interlocking asperities. The measured unlocking response was modeled successfully by assuming that crack flank frictional stresses obeyed a constant interfacial shear stress friction law.
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
Atw-International Journal for Nuclear Power
Atw-International Journal for Nuclear Power NUCLEAR SCIENCE & TECHNOLOGY-
自引率
0.00%
发文量
1
审稿时长
6-12 weeks
×
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