Low-Reynolds-Number Effects on Delta-Wing Aerodynamics
Author:
Affiliation:
1. Texas A&M University, College Station, Texas 77840-3141
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.2352
Reference15 articles.
1. Leading-edge vortices due to low Reynolds number flow past a pitching delta wing
2. Instabilities in Leading-Edge Vortex Development
3. Visualization measurements of vortex flows
4. Vortex breakdown on slender sharp-edged wings
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