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Full Length Article | Open Access

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

Xin DINGaDawei HUANGb( )Zixu GUOcHan YANbXiaojun YANbYinzhuoran WANGdFeng YINaXu LUANa
Research and Development Center, Gas Turbine Corporation Ltd. of Aero Engine Corporation of China, Shenyang 110015, China
School of Energy and Power Engineering, Beihang University, Beijing 100191, China
Department of Mechanical Engineering, National University of Singapore, Singapore 117575, Singapore
School of Metallurgy, Northeastern University, Shenyang 110167, China

Peer review under responsibility of Editorial Committee of CJA

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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 (Rf). The growth law of MSE changes from linear to logarithmic as Rf decreases. Strain amplitudes in the dwell stage, observed unaffected by Rf, 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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Chinese Journal of Aeronautics
Article number: 103246

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Cite this article:
DING X, HUANG D, GUO Z, et al. Experimental investigations on combined high and low cycle fatigue: Material-level specimen design and strain response characteristics. Chinese Journal of Aeronautics, 2025, 38(1): 103246. https://doi.org/10.1016/j.cja.2024.09.022

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Received: 09 January 2024
Revised: 31 January 2024
Accepted: 10 June 2024
Published: 21 September 2024
© 2024 Chinese Society of Aeronautics and Astronautics.

This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).