• 文献检索
  • 文档翻译
  • 深度研究
  • 学术资讯
  • Suppr Zotero 插件Zotero 插件
  • 邀请有礼
  • 套餐&价格
  • 历史记录
应用&插件
Suppr Zotero 插件Zotero 插件浏览器插件Mac 客户端Windows 客户端微信小程序
定价
高级版会员购买积分包购买API积分包
服务
文献检索文档翻译深度研究API 文档MCP 服务
关于我们
关于 Suppr公司介绍联系我们用户协议隐私条款
关注我们

Suppr 超能文献

核心技术专利:CN118964589B侵权必究
粤ICP备2023148730 号-1Suppr @ 2026

文献检索

告别复杂PubMed语法,用中文像聊天一样搜索,搜遍4000万医学文献。AI智能推荐,让科研检索更轻松。

立即免费搜索

文件翻译

保留排版,准确专业,支持PDF/Word/PPT等文件格式,支持 12+语言互译。

免费翻译文档

深度研究

AI帮你快速写综述,25分钟生成高质量综述,智能提取关键信息,辅助科研写作。

立即免费体验

I型和混合模式(I+II)加载下紧凑拉伸试样的数值疲劳裂纹扩展

Numerical Fatigue Crack Growth on Compact Tension Specimens under Mode I and Mixed-Mode (I+II) Loading.

作者信息

Martins Rui F, Xavier José, Caldeira João

机构信息

UNIDEMI, Department of Mechanical and Industrial Engineering, NOVA School of Science and Technology, Universidade NOVA de Lisboa, Campus de Caparica, 2829-516 Caparica, Portugal.

Intelligent Systems Associate Laboratory (LASI), 4800-058 Guimarães, Portugal.

出版信息

Materials (Basel). 2024 Sep 18;17(18):4570. doi: 10.3390/ma17184570.

DOI:10.3390/ma17184570
PMID:39336311
原文链接:https://pmc.ncbi.nlm.nih.gov/articles/PMC11433036/
Abstract

This study focused on standard Compact Tension (CT) specimens and two loading modes during the numerical analyses carried out, namely: pure mode I and mixed-mode loading (Modes I+II). Numerical stress intensity factors, K, were calculated using Abaqus 2022 and compared with those given analytically under pure mode I loading, showing very good agreement. Additionally, K, K, and K results obtained from Abaqus were presented for mixed-mode loading, analyzing crack growth and variation through the thickness of the CT specimen. Moreover, fatigue crack growth simulations under mode I loading were conducted on standard CT specimens using the Extended Finite Element Method (XFEM) and the Paris Law parameters of an AISI 316L stainless steel. It was shown that XFEM effectively determines crack propagation direction and growth, provided that an appropriate mesh is implemented.

摘要

本研究聚焦于标准紧凑拉伸(CT)试样以及在进行数值分析时的两种加载模式,即:纯I型模式和混合模式加载(I + II型模式)。使用Abaqus 2022计算数值应力强度因子K,并将其与纯I型模式加载下的解析值进行比较,结果显示出非常好的一致性。此外,还给出了Abaqus在混合模式加载下获得的K₁、K₂和K₃结果,分析了CT试样厚度方向上的裂纹扩展和变化情况。此外,使用扩展有限元法(XFEM)和AISI 316L不锈钢的巴黎定律参数,对标准CT试样进行了I型模式加载下的疲劳裂纹扩展模拟。结果表明,只要实施合适的网格划分,XFEM就能有效地确定裂纹扩展方向和扩展情况。

https://cdn.ncbi.nlm.nih.gov/pmc/blobs/5f99/11433036/ec17b2f1a81a/materials-17-04570-g007.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/5f99/11433036/8c8174c65211/materials-17-04570-g001.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/5f99/11433036/42b65d3a731a/materials-17-04570-g002.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/5f99/11433036/4ab4c05c03e6/materials-17-04570-g003.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/5f99/11433036/c22130a39f33/materials-17-04570-g004.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/5f99/11433036/76dcf7b431ec/materials-17-04570-g005.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/5f99/11433036/cbf84df4e6d6/materials-17-04570-g006.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/5f99/11433036/ec17b2f1a81a/materials-17-04570-g007.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/5f99/11433036/8c8174c65211/materials-17-04570-g001.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/5f99/11433036/42b65d3a731a/materials-17-04570-g002.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/5f99/11433036/4ab4c05c03e6/materials-17-04570-g003.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/5f99/11433036/c22130a39f33/materials-17-04570-g004.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/5f99/11433036/76dcf7b431ec/materials-17-04570-g005.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/5f99/11433036/cbf84df4e6d6/materials-17-04570-g006.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/5f99/11433036/ec17b2f1a81a/materials-17-04570-g007.jpg

相似文献

1
Numerical Fatigue Crack Growth on Compact Tension Specimens under Mode I and Mixed-Mode (I+II) Loading.I型和混合模式(I+II)加载下紧凑拉伸试样的数值疲劳裂纹扩展
Materials (Basel). 2024 Sep 18;17(18):4570. doi: 10.3390/ma17184570.
2
Study of the Fatigue Crack Growth in Long-Term Operated Mild Steel under Mixed-Mode (I + II, I + III) Loading Conditions.长期运行低碳钢在混合模式(I + II、I + III)加载条件下疲劳裂纹扩展的研究
Materials (Basel). 2020 Jan 1;13(1):160. doi: 10.3390/ma13010160.
3
Fatigue Crack Growth Behavior of CP-Ti Cruciform Specimens with Mixed Mode I-II Crack under Biaxial Loading.双轴载荷下含Ⅰ-Ⅱ复合型裂纹的工业纯钛十字形试样疲劳裂纹扩展行为
Materials (Basel). 2022 Mar 4;15(5):1926. doi: 10.3390/ma15051926.
4
Numerical Analysis of Fatigue Crack Growth Path and Life Predictions for Linear Elastic Material.线性弹性材料疲劳裂纹扩展路径的数值分析及寿命预测
Materials (Basel). 2020 Jul 30;13(15):3380. doi: 10.3390/ma13153380.
5
Corrosion-Fatigue Crack Growth in Plates: A Model Based on the Paris Law.板材中的腐蚀疲劳裂纹扩展:基于巴黎定律的模型
Materials (Basel). 2017 Apr 22;10(4):439. doi: 10.3390/ma10040439.
6
Fracture Toughness and Fatigue Crack Growth Analyses on a Biomedical Ti-27Nb Alloy under Constant Amplitude Loading Using Extended Finite Element Modelling.基于扩展有限元模型的生物医学Ti-27Nb合金在常幅载荷下的断裂韧性与疲劳裂纹扩展分析
Materials (Basel). 2023 Jun 19;16(12):4467. doi: 10.3390/ma16124467.
7
Predicting Stress Intensity Factor for Aluminum 6062 T6 Material in L-Shaped Lower Control Arm (LCA) Design Using Extended Finite Element Analysis.使用扩展有限元分析预测L形下控制臂(LCA)设计中6062 T6铝合金材料的应力强度因子
Materials (Basel). 2023 Dec 30;17(1):206. doi: 10.3390/ma17010206.
8
Fatigue crack propagation behavior of ultra high molecular weight polyethylene under mixed mode conditions.超高分子量聚乙烯在混合模式条件下的疲劳裂纹扩展行为。
J Biomed Mater Res. 1994 Feb;28(2):181-7. doi: 10.1002/jbm.820280207.
9
Fatigue Crack Growth Analysis under Constant Amplitude Loading Using Finite Element Method.基于有限元法的等幅载荷作用下疲劳裂纹扩展分析
Materials (Basel). 2022 Apr 18;15(8):2937. doi: 10.3390/ma15082937.
10
Adaptive Finite Element Modeling of Linear Elastic Fatigue Crack Growth.线性弹性疲劳裂纹扩展的自适应有限元建模
Materials (Basel). 2022 Oct 30;15(21):7632. doi: 10.3390/ma15217632.

引用本文的文献

1
Mixed-Mode Crack Growth Behavior of Compact Tension Shear (CTS) Specimens: A Study on the Impact of the Fatigue Stress Ratio, Loading Angle, and Geometry Thickness.紧凑拉伸剪切(CTS)试样的混合模式裂纹扩展行为:疲劳应力比、加载角度和几何厚度影响的研究
Materials (Basel). 2025 Mar 26;18(7):1484. doi: 10.3390/ma18071484.

本文引用的文献

1
Effect of Pre-Corrosion Pits on Residual Fatigue Life for 42CrMo Steel.预腐蚀坑对42CrMo钢残余疲劳寿命的影响
Materials (Basel). 2019 Jul 2;12(13):2130. doi: 10.3390/ma12132130.