Folding Wingtips for Improved Roll Performance
Author:
Affiliation:
1. University of Bristol
2. Airbus Operations Ltd.
Publisher
American Institute of Aeronautics and Astronautics
Reference15 articles.
1. Nonlinear Folding Wing Tips for Gust Loads Alleviation
2. Testing of a Hinged Wingtip Device for Gust Loads Alleviation
Cited by 7 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献
1. Roll Maneuverability of Transonic High-Aspect-Ratio-Wing Aircraft with Flared Folding Wingtips;Journal of Aircraft;2024-05
2. Aeroelastic Scaling of a High-Aspect-Ratio Wing Incorporating a Semi-Aeroelastic Hinge;AIAA Journal;2024-04-17
3. Roll Maneuvers of Very Flexible Aircraft with Flared Folding Wingtips;AIAA SCITECH 2023 Forum;2023-01-19
4. Flight Dynamics of Aircraft Incorporating the Semi-Aeroelastic Hinge;2023
5. Conventional and Unconventional Control Effectors for Load Alleviation in High-Aspect-Ratio-Wing Aircraft;AIAA SCITECH 2022 Forum;2022-01-03
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