Modeling of fatigue damage under superimposed high-cycle and low-cycle fatigue loading for a cast aluminum alloy

被引:37
作者
Zheng, X. [1 ]
Engler-Pinto, C. C., Jr. [2 ]
Su, X. [2 ]
Cui, H. [1 ]
Wen, W. [1 ]
机构
[1] Nanjing Univ Aeronaut & Astronaut, Coll Energy & Power Engn, Nanjing 210016, Jiangsu, Peoples R China
[2] Ford Res & Innovat Ctr, Dearborn, MI 48124 USA
来源
MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING | 2013年 / 560卷
关键词
Cast aluminum alloys; High-cycle fatigue; Low-cycle fatigue; Load interaction; Fatigue damage; Crack closure; CRACK CLOSURE; 2024-T351; ALUMINUM; COMPRESSIVE UNDERLOADS; TENSILE OVERLOADS; STRESS; ACCUMULATION; GROWTH; STRAIN; PROPAGATION; THRESHOLD;
D O I
10.1016/j.msea.2012.10.037
中图分类号
TB3 [工程材料学];
学科分类号
0805 ; 080502 ;
摘要
This study investigates the interaction between high-cycle fatigue (HCF) and low-cycle fatigue (LCF) in cast aluminum alloys. Initially, the baseline HCF and LCF lives have been determined under constant amplitude loading; LCF HCF interaction fatigue tests were subsequently carried out through the application of periodic underloads. To account for the inherent scatter in fatigue life, probabilistic fatigue life curves were employed to establish the baseline HCF and LCF fatigue lives. The interaction fatigue damage was found to increase with the stress amplitude of the HCF cycles. Larger underloads (LCF cycles) also resulted in larger interaction damage. The impact of different numbers of HCF cycles per block (between underloads) was also studied. It was also found out that there is an additional damage caused by frequent applications of LCF cycles, which is related to the damaged Si particles in the large reversed plastic zone generated by the LCF cycles. The evolution of the crack opening stress following the application of an underload has been proposed as the major mechanism for the load interaction effect. An interaction damage model is proposed to account for these observed effects. (C) 2012 Elsevier B.V. All rights reserved.
引用
收藏
页码:792 / 801
页数:10
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