Multiple-actuator control of vortex breakdown on a pitching delta wing
Author:
Affiliation:
1. Lehigh University, Bethlehem, Pennsylvania 18015-3085
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.13369
Reference6 articles.
1. Control of leading-edge vortices on a delta wing
2. Flow structure on stalled delta wing subjected to small amplitude pitching oscillations
3. Structure of vortex breakdown on a pitching delta wing
4. Three-dimensional flow structure on delta wings at high angle-of-attack - Experimental concepts and issues
5. Control of vortices on a delta wing by leading-edge injection
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1. References;Fundamentals and Applications of Modern Flow Control;2009-08-22
2. Response of unconfined vortex breakdown to axial pulsing;Physics of Fluids;2006-03
3. Closed-loop control of vortex breakdown: a model study;Journal of Fluid Mechanics;2004-07-25
4. Unsteady aerodynamics and flow control for flapping wing flyers;Progress in Aerospace Sciences;2003-11
5. Control of vortex breakdown by a coaxial wire;Physics of Fluids;2003-01
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