Influence of Reynolds Number on Vortex Flow over a Non-slender Delta Wing
Author:
Affiliation:
1. Beijing University of Aeronautics and Astronautics, 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.J050246
Reference22 articles.
1. Visualized Vortices on Unmanned Combat Air Vehicle Planform: Effect of Reynolds Number
2. Unsteady aerodynamics of nonslender delta wings
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