Unsteady Aerodynamics of Free-to-Roll Nonslender Delta Wings
Author:
Affiliation:
1. University of Bath
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2007-1074
Reference21 articles.
1. Experimental investigations on limit cycle wing rock of slender wings
2. Body-axis rolling motion critical states of a 65-degree delta wing
3. Computation of vortex breakdown on a rolling delta wing
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