Flow Control of Tip/Edge Vortices
Author:
Affiliation:
1. University of Bath, Bath, England BA2 7AY, United Kingdom
Funder
Air Force Office of Scientific Research
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/am-pdf/10.2514/1.J056586
Reference62 articles.
1. Vortex topology of wing tip blowing
2. Symmetry breaking and instabilities of conical vortex pairs over slender delta wings
3. Afterbody vortices of axisymmetric cylinders with a slanted base
4. The discrete vortices from a delta wing
5. Unsteady vortex structure over a delta wing
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