Effects of Reynolds Numbers on Wing Rock Induced by Forebody Vortices
Author:
Affiliation:
1. Beihang University, 100191 Beijing, People’s Republic of China
Funder
National Natural Science Foundation of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J055461
Reference36 articles.
1. Wing/vortex interactions and wing rock
2. The unsteady aerodynamics of slender wings and aircraft undergoing large amplitude maneuvers
3. Review of forebody-induced wing rock
4. Self-induced wing rock of slender delta wings
5. Dynamic load measurements with delta wings undergoing self-induced roll oscillations
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