Aerodynamic Research on the Wing Design of a 3000 kg Hexa Tiltrotor eVTOL
This paper describes a design method for 3000 kg hexa tiltrotor eVTOL wings. According to this design method, this paper designs and optimizes the wing area and incidence angle using CFD technology, provides the optimal wing design scheme, and estimates the range of eVTOL based on CFD results. The r...
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| Главные авторы: | , , |
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| Формат: | Artigo |
| Язык: | Inglês |
| Опубликовано: |
MDPI AG
2025-03-01
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| Серии: | Engineering Proceedings |
| Предметы: | |
| Online-ссылка: | https://www.mdpi.com/2673-4591/80/1/41 |
| Метки: |
Нет меток, Требуется 1-ая метка записи!
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