Visualized Vortices on Unmanned Combat Air Vehicle Planform: Effect of Reynolds Number
Author:
Affiliation:
1. Lehigh University, Bethlehem, Pennsylvania 18015
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.6290
Reference6 articles.
1. Reynolds number effects on the vortical-flow structure generated by a double-delta wing
2. Effects of Reynolds Number on Flow over 76/40-Degree Double-Delta Wings
3. A study of the vortex flow over a 76/40-deg double-delta wing
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