Research on Whirl‑Flutter Characteristics of Distributed Propulsive Rotorcraft
Aiming at the problem of whirl-flutter dynamics of distributed propulsion rotorcraft in high-speed forward flight state， this paper proposes a highly versatile， fast and efficient distributed multi-rotor/tilt-wing coupled aeroelastic dynamics analysis method. Based on the theory of moderately deform...
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| Главные авторы: | , , , |
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| Формат: | Artigo |
| Язык: | Chinês |
| Опубликовано: |
Editorial Office of Journal of Nanjing University of Aeronautics and Astronautics
2025-04-01
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| Серии: | Nanjing Hangkong Hangtian Daxue Xuebao |
| Предметы: | |
| Online-ссылка: | https://jnuaa.nuaa.edu.cn/njhkht/article/html/202502004?st=article_issue |
| Метки: |
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