Vibration Fatigue Assessment of UAV Wing Pylons Based on the PSD Method
(1) Background: The structural integrity of key components in unmanned aerial vehicle (UAV) mission systems is crucial for achieving performance goals. The installation environment of military and civilian UAV wing pylons is very complex, as they are subject to various complex vibration excitations....
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| Autors principals: | , , |
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| Format: | Artigo |
| Idioma: | Inglês |
| Publicat: |
MDPI AG
2025-12-01
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| Col·lecció: | Drones |
| Matèries: | |
| Accés en línia: | https://www.mdpi.com/2504-446X/9/12/838 |
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