Attenuation of Self-Excited Roll Oscillations of Low-Aspect-Ratio Wings by Using Acoustic Forcing
Author:
Affiliation:
1. Department of Mechanical Engineering, University of Bath, Bath, England BA2 7AY, United Kingdom
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J052689
Reference26 articles.
1. Low Reynolds Number Aerodynamics of Low-Aspect-Ratio, Thin/Flat/Cambered-Plate Wings
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3. An Overview of Micro Air Vehicle Aerodynamics
4. Experimental investigations on limit cycle wing rock of slender wings
5. Wing/vortex interactions and wing rock
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