Random Vibration Fatigue Life Analysis of Aeroengine Bolts Using the Frequency-Domain Method
By: Lilin Tian, Jun Wang, Chaofeng Zhang, Yuchao Guo and Liang Chang
Authors
National Key Laboratory of Strength and Structural Integrity, Aircraft Strength, Research Institute of China, Xi’an, China
Jun Wang
National Key Laboratory of Strength and Structural Integrity, Aircraft Strength, Research Institute of China, Xi’an, China
Chaofeng Zhang
National Key Laboratory of Strength and Structural Integrity, Aircraft Strength, Research Institute of China, Xi’an, China
Yuchao Guo
National Key Laboratory of Strength and Structural Integrity, Aircraft Strength, Research Institute of China, Xi’an, China
Liang Chang
National Key Laboratory of Strength and Structural Integrity, Aircraft Strength, Research Institute of China, Xi’an, China
DOI: https://doi.org/10.2478/fas-2024-0010 | Journal eISSN: 2300-7591
Language: English
Page range: 147 - 160
Published on: Oct 15, 2025
Published by: ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
In partnership with: Paradigm Publishing Services
Publication frequency: 1 issue per year
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© 2025 Lilin Tian, Jun Wang, Chaofeng Zhang, Yuchao Guo, Liang Chang, published by ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 3.0 License.