A Study on Fatigue Crack Closure Associated with the Growth of Long Crack in a New Titanium Alloy

被引:3
|
作者
Liu, Jiarui [1 ,2 ]
Chen, Jiawei [3 ]
Sun, Zhengyi [4 ]
Zhang, Haicheng [1 ]
Yuan, Qingsong [4 ]
机构
[1] Hunan Univ, Coll Mech & Vehicle Engn, Changsha 410082, Peoples R China
[2] China Ship Sci Res Ctr, 702 Res Inst, Wuxi 214082, Peoples R China
[3] Wuhan Univ Technol, Sch Transportat, Wuhan 430070, Peoples R China
[4] Jiangsu Univ Sci & Technol, Sch Naval Architecture & Ocean Engn, Zhenjiang 212100, Peoples R China
基金
中国国家自然科学基金;
关键词
new titanium alloy; crack closure; load ratio; fatigue crack growth rate; STRESS;
D O I
10.3390/met13081377
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
In this article, the fatigue crack closure in a new titanium alloy is carried out under constant amplitude cyclic loading with the combination of the simulation method and experiments. A numerical simulation of the crack closure effect on a new titanium alloy under different load ratios was carried out to analyze the effect of grid size on the crack closure level and to obtain the fatigue crack opening load level under different load ratios. The experimental study of the fatigue crack growth rate of the new titanium alloy under different load ratios has demonstrated that the fatigue crack growth rate is affected by the stress ratio. With the increase in load ratio, the crack expansion rate of new titanium also increases. Combined with the simulation, the experiments show that the crack closure effect induced by the plastic region at the crack tip is the main reason for the load ratio effect on the fatigue crack expansion rate of the new titanium alloy.
引用
收藏
页数:11
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