中国科学院机构知识库网格
Chinese Academy of Sciences Institutional Repositories Grid
Multiaxial fatigue life estimation based on weight-averaged maximum damage plane under variable amplitude loading

文献类型:期刊论文

作者Tao ZQ(陶志强); Qian GA(钱桂安); Li, Xiang; Sun JY(孙经雨); Zhang, ZiLing; Li, DaoHang; Qian GA(钱桂安)
刊名JOURNAL OF MATERIALS RESEARCH AND TECHNOLOGY-JMR&T
出版日期2023-03
卷号23页码:2557-2575
ISSN号2238-7854
关键词Multiaxial fatigue Lifetime estimation Weight function Critical plane Variable amplitude loading
DOI10.1016/j.jmrt.2023.01.1962238-7854
英文摘要An innovative critical plane determination approach with weight-averaged largest fatigue damage is proposed, in which the material failure modes can be considered. If material exhibits shear cracking behavior, a strain-based critical plane model with shear failure mode is selected to evaluate the weight function. Otherwise, other one with tensile failure mode is adopted. According to the proposed critical plane, a multiaxial fatigue lifetime estimation methodology is established for evaluating fatigue life. And, six kinds of mate-rials are employed to validate the validity of presented methodology. The validation results reveal the presented methodology can estimate the orientation angles of failure plane accurately and supply satisfactory fatigue lifetime estimations for both shear and tensile failure mode materials. Furthermore, the proposed critical plane framework can be extended to be utilized with stress-based fatigue criteria, and prediction results show a good agreement with experimental data by another two materials.(c) 2023 The Author(s). Published by Elsevier B.V. This is an open access article under the CCBY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).
分类号一类
WOS研究方向WOS:000964352100001
语种英语
资助机构Academic Research Projects of Beijing Union University [ZK80202101] ; R & D Program of Beijing Municipal Education Commission [KM202211417012] ; National Natural Science Foundation of China [12002186, 12072345, 12002185, 51905334] ; Shanghai Sailing Program [19YF1418600] ; Science Center for Gas Turbine Project [P2022-B-III-008-001] ; Beijing Postdoctoral Research Foundation [2022-ZZ-044]
其他责任者Qian, GA
源URL[http://dspace.imech.ac.cn/handle/311007/92281]  
专题力学研究所_非线性力学国家重点实验室
作者单位1.(Li Xiang) China Special Equipment Inspection & Res Inst Beijing 100029 Peoples R China
2.(Tao Zhi-Qiang, Qian Guian, Sun Jingyu) Univ Chinese Acad Sci Sch Engn Sci Beijing 100049 Peoples R China
3.(Zhang Zi-Ling) Shanghai Maritime Univ Logist Engn Coll Shanghai 201306 Peoples R China
4.(Li Dao-Hang) Beijing Univ Technol Fac Mat & Mfg Beijing 100124 Peoples R China
5.(Tao Zhi-Qiang) Beijing Union Univ Coll Robot Beijing 100020 Peoples R China
6.(Tao Zhi-Qiang, Qian Guian, Sun Jingyu) Chinese Acad Sci Inst Mech State Key Lab Nonlinear Mech LNM Beijing Peoples R China
推荐引用方式
GB/T 7714
Tao ZQ,Qian GA,Li, Xiang,et al. Multiaxial fatigue life estimation based on weight-averaged maximum damage plane under variable amplitude loading[J]. JOURNAL OF MATERIALS RESEARCH AND TECHNOLOGY-JMR&T,2023,23:2557-2575.
APA 陶志强.,钱桂安.,Li, Xiang.,孙经雨.,Zhang, ZiLing.,...&Qian GA.(2023).Multiaxial fatigue life estimation based on weight-averaged maximum damage plane under variable amplitude loading.JOURNAL OF MATERIALS RESEARCH AND TECHNOLOGY-JMR&T,23,2557-2575.
MLA 陶志强,et al."Multiaxial fatigue life estimation based on weight-averaged maximum damage plane under variable amplitude loading".JOURNAL OF MATERIALS RESEARCH AND TECHNOLOGY-JMR&T 23(2023):2557-2575.

入库方式: OAI收割

来源:力学研究所

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