Vortex Dynamics of Free-to-Roll Slender and Nonslender Delta Wings
Author:
Affiliation:
1. 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/10.2514/1.45425
Reference18 articles.
1. Dynamic load measurements with delta wings undergoing self-induced roll oscillations
2. Experimental investigations on limit cycle wing rock of slender wings
3. Wing/vortex interactions and wing rock
4. Body-axis rolling motion critical states of a 65-degree delta wing
5. Roll-induced cross-loads on a delta wing at high incidence
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