Phase Synchronization of Vortex Shedding from Two Side-by-Side Circular Cylinders Using Plasma Actuators
Author:
Affiliation:
1. University of Notre Dame
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2004-925
Reference31 articles.
1. Vortex Dynamics in the Cylinder Wake
2. Local and Global Instabilities in Spatially Developing Flows
3. The Generation of Vortices in Fluids of Small Viscosity
4. The mechanics of the formation region of vortices behind bluff bodies
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1. Optimization of Induced Velocity for Plasma Actuator with Multiple Encapsulated Electrodes using Response Surface Methodology;49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2011-01-04
2. The Influence of Electrode Configuration and Dielectric Temperature on Plasma Actuator Performance;49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2011-01-04
3. Phase Synchronization of Vortex Shedding from Two Circular Cylinders Using Plasma Actuators;AIAA Journal;2009-07
4. Attenuation of Low-Speed Flow-Induced Cavity Tones Using Plasma Actuators;AIAA Journal;2007-07
5. On the Use of Reynolds Number as the Scaling Parameter for the Performance of Plasma Actuator in a Weakly Compressible Flow;44th AIAA Aerospace Sciences Meeting and Exhibit;2006-01-09
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