Boundary layer effects on the flow of a leading edge vortex
Author:
Affiliation:
1. Delft Univ. of Technology, Netherlands
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1993-3463
Reference15 articles.
1. The inner viscous solution for the core of a leading-edge vortex
2. Similarity solutions for viscous vortex cores
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1. Detached-eddy simulations and analyses on new vortical flows over a 76/40° double delta wing;Science China Physics, Mechanics and Astronomy;2013-05-03
2. Leading-Edge Radius Effects on 50-deg Delta Wing Flow;47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition;2009-01-05
3. Effects of Leading-Edge Shape on the Flow Over 50-deg Delta Wings;26th AIAA Applied Aerodynamics Conference;2008-06-14
4. Analysis of Delta-Wing Vortical Substructures Using Detached-Eddy Simulation;AIAA Journal;2006-05
5. Physical Considerations of Leading Edge Flows;22nd Applied Aerodynamics Conference and Exhibit;2004-06-20
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