A survey on fatigue life analysis approaches for metallic notched components under multi-axial loading

被引:18
作者
Luo, Peng [1 ]
Yao, Weixing [1 ,2 ]
Wang, Yingyu [1 ,2 ]
Li, Piao [1 ]
机构
[1] Nanjing Univ Aeronaut & Astronaut, State Key Lab Mech & Control Mech Struct, Nanjing, Jiangsu, Peoples R China
[2] Nanjing Univ Aeronaut & Astronaut, Key Lab Fundamental Sci Natl Def Adv Design Techn, Nanjing, Jiangsu, Peoples R China
关键词
Multi-axial fatigue; notched components; fatigue life analysis approach; STRESS-STRAIN CALCULATION; CRITICAL DISTANCES; ELASTOPLASTIC STRAINS; PLASTIC STRESS; WOHLER CURVE; CRITERION; PHASE; STRENGTH; BEHAVIOR; FAILURE;
D O I
10.1177/0954410018809838
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
In this paper, several fatigue failure approaches of metallic notched components under multi-axial loading in recent decades are reviewed in detail. They are classified into three categories according to their different fatigue physical mechanisms and hypotheses: nominal stress approach, local stress-strain approach and the theory of critical distance. The accuracy, applicable range and computing complexity of these three different fatigue failure theories of metallic notched specimen under multi-axial fatigue loading are given. It is concluded that theory of critical distance accords with experimental results under multi-axial fatigue loading and it gives unambiguous explanation for physical mechanism of fatigue damage. However, the computing process is complex, especially under non-proportional fatigue loading, and the key parameter of theory of critical distance is difficult to calculate especially in engineering. These difficulties limit the application of theory of critical distance.
引用
收藏
页码:3870 / 3890
页数:21
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