Fatigue Analysis and Load Spectrum Generation for Wing‐Fuselage Lug Joint With a Focus on Human Safety Transport Category Aircraft
ABSTRACT This research work focuses on fluctuating load spectrum generation and fatigue analysis of a wing‐fuselage attachment lug joint, in accordance with the requirements outlined in 14 CFR Part 25 for transport category aircraft. The study involves the generation of a fatigue load spectrum using...
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| Main Authors: | , , , , , |
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| Format: | Article |
| Language: | English |
| Published: |
Wiley
2025-03-01
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| Series: | Engineering Reports |
| Subjects: | |
| Online Access: | https://doi.org/10.1002/eng2.70053 |
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