Two-Dimensional and Three-Dimensional Finite Element Analysis of Finite Contact Width on Fretting Fatigue

被引:5
|
作者
Kim, Heung Soo [1 ]
Mall, Shankar [2 ]
Ghoshal, Anindya [3 ]
机构
[1] Dongguk Univ Seoul, Dept Mech Robot & Energy Eng, Seoul 100715, South Korea
[2] USAF, Dept Aeronaut & Astronaut, Inst Technol, Wright Patterson AFB, OH 45433 USA
[3] USA, Res Lab, Aberdeen Proving Ground, MD 21005 USA
关键词
fretting fatigue; contact; stick-slip; finite element analysis; three-dimensional effects; traction distribution; hybrid layer method; CRACK INITIATION; TI-6AL-4V; BEHAVIOR; MECHANICS; WEAR;
D O I
10.2320/matertrans.M2010268
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Three-dimensional effects of finite contact width fretting fatigue were investigated using the combination of full three-dimensional finite element model and two-dimensional plane strain finite element model, named as a hybrid layer method. Free edge boundary effect in finite contact width fretting fatigue problem required full three-dimensional finite element analysis to obtain accurate stress state and relative displacement in contact zone. To save the computational cost with sufficient accuracy, traction distributions obtained from coarse three-dimensional finite element analysis was applied to the two-dimensional plane strain finite element model. The key idea of this hybrid layer method was that traction distributions converged faster than the stresses. The proposed hybrid layer method predicted the free edge boundary effects of finite contact width fretting fatigue less than eight percent error bound and reduce the execution time to 5 percent of three-dimensional submodeling technique. [doi: 10.2320/matertrans.M2010268]
引用
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页码:147 / 154
页数:8
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