Gust alleviation using trailing-edge flaps
Author:
Affiliation:
1. Aiolos Engineering Corp., Toronto, Canada
2. Notre Dame, Univ., IN
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1999-649
Reference14 articles.
1. AIAA 99-0649
Cited by 9 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. Approach for Aerodynamic Gust Load Alleviation by Means of Spanwise-Segmented Flaps;Journal of Aircraft;2023-05
2. Active Gust Load Alleviation by Combined Actuation of Trailing Edge and Leading Edge Flap at Transonic Speeds;AIAA Scitech 2021 Forum;2021-01-04
3. Actuator concepts for active gust alleviation on transport aircraft at transonic speeds;AIAA Scitech 2020 Forum;2020-01-05
4. Dynamic lift measurements on an airfoil with periodic flap motion at high Reynolds number;AIAA Scitech 2019 Forum;2019-01-06
5. Revisiting Conventional Flaps at High Deflection Rate;AIAA Journal;2017-08
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