Nose landing gear strength test strain gauge vs FEA correlation
This article conducts finite element modeling analysis on the nose landing gear, and calculates and analyzes several severe load conditions. Strength tests were conducted on the nose landing gear to verify that the static strength of the landing gear meets the requirements. By comparing the strength test and finite element analysis results of the landing gear, it is shown that the analysis and test results are within the tolerance range, indicating that the finite element analysis and results are reliable and can be used for subsequent analysis.
Authors
- Wenjie Chen (ORCID: https://orcid.org/0000-0003-0556-7391)
- Shanshan Cao (ORCID: https://orcid.org/0000-0002-9594-7269)
- Wenxu Xu
- S.J. Yang (ORCID: https://orcid.org/0000-0001-8684-7488)
Institutions
- Commercial Aircraft Corporation of China (China) (CN)
Publication Details
- Journal
- IET conference proceedings.
- Published
- 2025-01-01
- DOI
- https://doi.org/10.1049/icp.2024.3156
- Primary Topic
- Mechanical Engineering and Vibrations Research
- Type
- article
- Field-Weighted Citation Impact
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