Random Vibration Fatigue Life Analysis of Aeroengine Bolts Using the Frequency-Domain Method

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Open Access

|Oct 2025

Authors

National Key Laboratory of Strength and Structural Integrity, Aircraft Strength, Research Institute of China, Xi’an, China

National Key Laboratory of Strength and Structural Integrity, Aircraft Strength, Research Institute of China, Xi’an, China

National Key Laboratory of Strength and Structural Integrity, Aircraft Strength, Research Institute of China, Xi’an, China

National Key Laboratory of Strength and Structural Integrity, Aircraft Strength, Research Institute of China, Xi’an, China

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 | Journal ISSN: 2081-7738

Language: English

Page range: 147 - 160

Published on: Oct 15, 2025

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.