Experimental Study of the Aerodynamic Performance and Flow Characteristics of an Integrated UAV Inlet with Double 90° Bends
Many UAVs today have an S-bend inlet for the sake of stealth; however, the majority of them have a relatively gentle transition of the flow channel. This study presents an experimental investigation of the aerodynamic performance and swirl flow characteristics of a UAV inlet with double 90° bends, w...
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| Главные авторы: | , , , , , , |
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| Формат: | Artigo |
| Язык: | Inglês |
| Опубликовано: |
MDPI AG
2024-07-01
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| Серии: | Aerospace |
| Предметы: | |
| Online-ссылка: | https://www.mdpi.com/2226-4310/11/7/593 |
| Метки: |
Нет меток, Требуется 1-ая метка записи!
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