Experimental investigations on combined high and low cycle fatigue: Material-level specimen design and strain response characteristics

The paper designs a novel material-level specimen and its dedicated fixture suitable for applying Combined high- and low- Cycle Fatigue (CCF) loads. Unlike full-scale or simulation specimens, the CCF specimen eliminates geometrically induced stress gradients in the test region. Experimental data on CCF life and strain responses of ZSGH4169 alloy are acquired under different CCF loads. The Maximum Strain within Each (MSE) CCF cycle is demonstrated to be independent of the Low-Cycle Fatigue (LCF) loads and High-Cycle Fatigue (HCF) stress amplitudes, but exhibits a correlation with the Cycle Ratio of HCF/LCF ( R f ). The growth law of MSE changes from linear to logarithmic as R f decreases. Strain amplitudes in the dwell stage, observed unaffected by R f , are quantified as a function of LCF nominal stresses and HCF stress amplitudes. However, under a defined CCF load, strain amplitudes in the dwell stage remain constant. Strain peaks in the dwell stage in a single CCF cycle decrease in a power function with increasing HCF cycles.

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Publication Details

Journal
Chinese Journal of Aeronautics
Published
2024-09-21
DOI
https://doi.org/10.1016/j.cja.2024.09.022
Citations
6
Primary Topic
Fatigue and fracture mechanics
Type
article
Field-Weighted Citation Impact
1.62

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article

Experimental investigations on combined high and low cycle fatigue: Material-level specimen design and strain response characteristics

Luan Xu, Yin Feng, Zixu Guo, Han Yan et al.
6 citations
Chinese Journal of Aeronautics
Fatigue and fracture mechanics
1.62
article

Experimental investigations on combined high and low cycle fatigue: Material-level specimen design and strain response characteristics

Luan Xu, Yin Feng, Zixu Guo, Han Yan, Xiaojun Yan, Dawei Huang, Xin Ding, Yinzhuoran WANG
article en
6 citations

Abstract

The paper designs a novel material-level specimen and its dedicated fixture suitable for applying Combined high- and low- Cycle Fatigue (CCF) loads. Unlike full-scale or simulation specimens, the CCF specimen eliminates geometrically induced stress gradients in the test region. Experimental data on CCF life and strain responses of ZSGH4169 alloy are acquired under different CCF loads. The Maximum Strain within Each (MSE) CCF cycle is demonstrated to be independent of the Low-Cycle Fatigue (LCF) loads and High-Cycle Fatigue (HCF) stress amplitudes, but exhibits a correlation with the Cycle Ratio of HCF/LCF ( R f ). The growth law of MSE changes from linear to logarithmic as R f decreases. Strain amplitudes in the dwell stage, observed unaffected by R f , are quantified as a function of LCF nominal stresses and HCF stress amplitudes. However, under a defined CCF load, strain amplitudes in the dwell stage remain constant. Strain peaks in the dwell stage in a single CCF cycle decrease in a power function with increasing HCF cycles.

Chinese Journal of AeronauticsVol. 38(1)
National University of Singapore (SG), Aero Engine Corporation of China (China) (CN), Beihang University (CN), Northeastern University (CN)
National Natural Science Foundation of China, National Major Science and Technology Projects of China
Openalex Percentile: Top 19%
Fatigue and fracture mechanics
1.62
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Experimental investigations on combined high and low cycle fatigue: Material-level specimen design and strain response characteristics — Luan Xu, Yin Feng, et al. · Chinese Journal of Aeronautics (2024) | TGRS Research Map | TGRS