Wing Rock Induced by a Hemisphere–Cylinder Forebody
Author:
Affiliation:
1. Key Laboratory of Fluid Mechanics, Beihang University, 100191 Beijing, People’s Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C032311
Reference24 articles.
1. Wing/vortex interactions and wing rock
2. The unsteady aerodynamics of slender wings and aircraft undergoing large amplitude maneuvers
3. Self-induced wing rock of slender delta wings
4. Dynamic load measurements with delta wings undergoing self-induced roll oscillations
5. Experimental study of vortex flows over delta wings in wing-rock motion
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1. Wing rock mode and its mechanism of a flying-wing aircraft;Flow;2023
2. Effects of Reynolds Numbers on Wing Rock Induced by Forebody Vortices;AIAA Journal;2017-09
3. Effects of wing locations on wing rock induced by forebody vortices;Chinese Journal of Aeronautics;2016-10
4. The self-excited rolling oscillations induced by fore-body vortices;Aerospace Science and Technology;2015-12
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