Evolution and Breakdown of a Leading Edge Vortex on a Rotating Wing
Author:
Affiliation:
1. University of Maryland, College Park
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2013-843
Reference27 articles.
1. Challenges Facing Future Micro-Air-Vehicle Development
2. Aerodynamics of Low Reynolds Number Flyers
3. Comparison of the Hovering Efficiency of Rotating Wing and Flapping Wing Micro Air Vehicles
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4. Flow structure on a rotating wing: effect of radius of gyration;Journal of Fluid Mechanics;2014-08-14
5. Flow Structure of Low-Aspect-Ratio Rotating Wings from Dye Visualization;AIAA Journal;2014-05
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