Multiaxial fatigue behavior of a 2198-T8 Al-Li alloy under proportional and nonproportional loading

被引:3
|
作者
Su, Wei [1 ]
Zhu, Hong Mei [1 ]
机构
[1] Jilin Inst Chem Technol, Sch Aeronaut Engn, Jilin, Jilin, Peoples R China
关键词
aluminum-lithium alloy; fatigue constant; life prediction; multiaxial fatigue; non-proportional loading; MECHANICAL-PROPERTIES; CRACK GROWTH; CRITERION; EVOLUTION; LIFETIME; STRESS; PREDICTION; PRESSURE; STEEL;
D O I
10.1515/mt-2022-0172
中图分类号
TB3 [工程材料学];
学科分类号
0805 ; 080502 ;
摘要
2198-T8 Al-Li alloy was examined under different loading path. Uniaxial and multiaxial proportional and nonproportional loading tests were conducted to determine the material fatigue constant, and to study the multiaxial fatigue behavior, respectively. The multiaxial fatigue life was estimated by various criteria. The results show that, the torsional fatigue performance is better than the tension-compression fatigue performance. The fatigue life of nonproportional loading increases firstly and then decreases with the increase of phase difference from 0 degrees to 90 degrees. Shear Findley model and SWT model were modified by introducing shear damage parameters. The modified models provide fine results which are all within a factor of two.
引用
收藏
页码:1572 / 1585
页数:14
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