Structural comparison of vertical and horizontal layout of carrying arms of rotary-wing UAV with finite element analysis
In this study, numerical analysis of the fuselage of a rotary wing unmanned aerial vehicle was conducted. A fuselage that is resistant to the loads on the fuselage and has maximum lightness has been designed. In this context, the fuselage design was conducted based on the loads that the aircraft's f...
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| Autors principals: | , , , |
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| Format: | Artigo |
| Idioma: | Inglês |
| Publicat: |
Ahmet Çalık
2023-06-01
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| Col·lecció: | European Mechanical Science |
| Matèries: | |
| Accés en línia: | https://dergipark.org.tr/en/download/article-file/2918590 |
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