A fatigue damage accumulation model for reliability analysis of engine components under combined cycle loadings
Author:
Affiliation:
1. Key Laboratory of Electronic Equipment Structure Design, Ministry of EducationXidian University Xi'an China
2. Institute of Continuum MechanicsLeibniz Universität Hannover Hannover Germany
Funder
National Defense Pre-Research Foundation of China
National Natural Science Foundation of China
Publisher
Wiley
Subject
Mechanical Engineering,Mechanics of Materials,General Materials Science
Link
https://onlinelibrary.wiley.com/doi/pdf/10.1111/ffe.13246
Reference45 articles.
1. Combined fatigue experiments on full scale turbine components
2. Research on the fatigue performance of TC6 compressor blade under the CCF effect;Zhang YK;Int J Aerospace Eng,2018
3. Effect of combined cycle fatigue on Ti6242 fatigue strength
4. Combined high and low cycle fatigue life prediction model based on damage mechanics and its application in determining the aluminized location of turbine blade
5. Effect of Aluminized Coating on Combined Low and High Cycle Fatigue Life of Turbine Blade at Elevated Temperature
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