Preliminary Design and Optimization of Primary Structures for a Tilt-Duct UAV
Tilt-duct Unmanned Aerial Vehicles (UAV) combine the high-speed efficiency of fixed-wing aircrafts with vertical takeoff and landing (VTOL) and the hover capabilities of rotary-wing aircrafts while maximizing the advantages of ducted fans in terms of noise reduction, efficiency, and safety, making i...
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| Asıl Yazarlar: | , , , |
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| Materyal Türü: | Artigo |
| Dil: | Inglês |
| Baskı/Yayın Bilgisi: |
MDPI AG
2024-04-01
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| Seri Bilgileri: | Aerospace |
| Konular: | |
| Online Erişim: | https://www.mdpi.com/2226-4310/11/4/286 |
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