Defect induced cracking and modeling of fatigue strength for an additively manufactured Ti-6Al-4V alloy in very high cycle fatigue regime

doi:10.1016/j.tafmec.2022.103380

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	Defect induced cracking and modeling of fatigue strength for an additively manufactured Ti-6Al-4V alloy in very high cycle fatigue regime
	Chi, Weiqian 1; Wang, Wenjing 1; Li, Ying2 ; Xu, Wei2 ; Sun CQ(孙成奇)3,4
通讯作者	Wang, Wenjing(wjwang@bjtu.edu.cn) ; Sun, Chengqi(scq@lnm.imech.ac.cn)
发表期刊	THEORETICAL AND APPLIED FRACTURE MECHANICS
	2022-06-01
卷号	119 页码:10
ISSN	0167-8442
摘要	Additively manufactured (AM) alloy usually inevitably contains defects during the manufacturing process or in service. Defect, as a harmful factor, could significantly reduce the fatigue performance of materials. This paper shows that the location and introduced form of defects play an important role in high cycle fatigue and very high cycle fatigue (VHCF) behavior of selective laser melting Ti-6Al-4V alloys. The S-N curve descends approximately linearly for internal defect induced failure. While for artificial surface defect induced failure, the S-N curve descends at first and then exhibits a plateau region feature. The competition of interior crack initiation with fine granular area feature is also observed in VHCF regime. The paper indicates that only the size or the stress in-tensity factor range of the defect is not an appropriate parameter for describing the effect of defect on fatigue crack initiation. Finally, the effect of artificial surface defect on high cycle fatigue and VHCF strength is modeled,& nbsp;i.e., the fatigue strength sigma, fatigue life N and defect size & nbsp;(sic)area(square(root of the projection area of defect & nbsp;& nbsp;perpendicular to principal stress direction) is expressed as sigma = {CNa((sic)area)(n,& nbsp;)& nbsp;N < N0 & nbsp;CN0a((sic)area)(n,& nbsp;)& nbsp;N >= N-0 & nbsp;& nbsp;where C, a and n are constants, and N-0 is the number of cycles at the knee point of the curve.
关键词	Very high cycle fatigue Additively manufactured titanium alloy Defect Fatigue strength modeling
DOI	10.1016/j.tafmec.2022.103380
收录类别	SCI ; EI
语种	英语
WOS记录号	WOS:000798924600002
关键词[WOS]	DIRECT LASER DEPOSITION ; MECHANICAL-BEHAVIOR ; SURFACE-ROUGHNESS ; PERFORMANCE ; LIFE ; INITIATION ; PREDICTION ; INCLUSION ; ELECTRON ; GROWTH
WOS研究方向	Engineering ; Mechanics
WOS类目	Engineering, Mechanical ; Mechanics
资助项目	National Natural Sci-ence Foundation of China[91860112] ; National Natural Sci-ence Foundation of China[52075032] ; Science and Technology Research and Development Program of China State Railway Group Co., Ltd.[P2020J024]
项目资助者	National Natural Sci-ence Foundation of China ; Science and Technology Research and Development Program of China State Railway Group Co., Ltd.
论文分区	二类/Q1
力学所作者排名	1
RpAuthor	Wang, Wenjing ; Sun, Chengqi
引用统计	被引频次：10[WOS] [WOS记录] [WOS相关记录]
文献类型	期刊论文
条目标识符	http://dspace.imech.ac.cn/handle/311007/89475
专题	非线性力学国家重点实验室
作者单位	1.Beijing Jiaotong Univ, Key Lab Vehicle Adv Mfg, Measuring & Control Technol, Minist Educ, Beijing 100044, Peoples R China; 2.Beijing Inst Aeronaut Mat, Aviat Key Lab Sci & Technol Aeronaut Mat Testing &, Beijing Key Lab Aeronaut Mat Testing & Evaluat, Beijing 100095, Peoples R China; 3.Inst Mech, Chinese Acad Sci, State Key Lab Nonlinear Mech, Beijing 100190, Peoples R China; 4.Univ Chinese Acad Sci, Sch Engn Sci, Beijing 100049, Peoples R China
推荐引用方式 GB/T 7714	Chi, Weiqian,Wang, Wenjing,Li, Ying,et al. Defect induced cracking and modeling of fatigue strength for an additively manufactured Ti-6Al-4V alloy in very high cycle fatigue regime[J]. THEORETICAL AND APPLIED FRACTURE MECHANICS,2022,119:10.
APA	Chi, Weiqian,Wang, Wenjing,Li, Ying,Xu, Wei,&孙成奇.(2022).Defect induced cracking and modeling of fatigue strength for an additively manufactured Ti-6Al-4V alloy in very high cycle fatigue regime.THEORETICAL AND APPLIED FRACTURE MECHANICS,119,10.
MLA	Chi, Weiqian,et al."Defect induced cracking and modeling of fatigue strength for an additively manufactured Ti-6Al-4V alloy in very high cycle fatigue regime".THEORETICAL AND APPLIED FRACTURE MECHANICS 119(2022):10.

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