Numerical prediction of vortical flow over slender delta wings
Author:
Affiliation:
1. NASA Ames Research Center, Moffett Field, California 94035
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.46437
Reference22 articles.
1. On the Breakdown at High Incidences of the Leading Edge Vortices on Delta Wings
2. On stationary and travelling vortex breakdowns
3. Vortex Breakdown in Swirling Conical Flows
4. An experimental map of the internal structure of a vortex breakdown
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2. Open-Type Separation on Delta Wings for Leading-Edge Bluntness;TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2007
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