Study on creep-fatigue interaction mechanism and life prediction of aero-engine turbine blade
Author:
Publisher
Elsevier BV
Subject
General Engineering,General Materials Science
Reference31 articles.
1. Creep/fatigue accelerated failure of Ni-based superalloy turbine blade: Microscopic characteristics and void migration mechanism;Han;Int. J. Fatigue,2022
2. Uncovering the high-temperature microstructural evolution and creep-fatigue damage mechanism of CMSX-4 brazed joints;Lu;Int. J. Fatigue,2023
3. Experimental Study on Fatigue-Creep of P/M FGH96 Superalloy with Different Holding Time;Xiao;Journal of Northwestern Polytechnical University,2020
4. Creep–fatigue interaction behavior of nickel-based single crystal superalloy at high temperature by in-situ SEM observation;Wang;Int. J. Fatigue,2020
5. The effect of cyclic loading on the creep fatigue life and creep strength of a DS superalloy: Damage mechanism and life modeling;Hu;Int. J. Fatigue,2020
Cited by 2 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Fusing image and physical data for fatigue life prediction of nickel-based single crystal superalloys;Engineering Failure Analysis;2024-08
2. A Short Introduction of Blade Cooling Mechanisms in Old Gas Turbines with the Aim of Proper Distribution of Temperature Profile;Journal of Advanced Thermal Science Research;2023-12-29
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