Control of Leading-Edge Vortices with Suction
Author:
Affiliation:
1. University of Cincinnati, Cincinnati, Ohio 45221-0072
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.2279
Reference7 articles.
1. Transient response of leading-edge vortices to localized suction
2. Control of asymmetric vortical flows over delta wings at high anglesof attack
3. Control of vortices on a delta wing by leading-edge injection
4. Effect of shear-layer control on leading-edge vortices
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3. Aerodynamics and Vortex Flowfield of a Slender Delta Wing With Apex Flap and Tip Flap;Journal of Fluids Engineering;2017-03-20
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