Significance of Three-dimensional Unsteady Flows inside the Cavity on Separated-flow Control around an NACA0015 using a Synthetic Jet
Author:
Affiliation:
1. University of Tokyo
2. Ryoyu Systems Company, Ltd.
3. Japan Aerospace Exploration Agency (JAXA)
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2013-2748
Reference25 articles.
1. The control of flow separation by periodic excitation
2. Dielectric Barrier Discharge Plasma Actuators for Flow Control
3. Role of Actuation Frequency in Controlled Flow Reattachment over a Stalled Airfoil
4. SYNTHETIC JETS
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2. Computational Study of Wing Tip Effect for the Flow Control Authority of DBD Plasma Actuator;AIAA Aviation 2019 Forum;2019-06-15
3. Effects of Wall-Normal and Angular Momentum Injections in Airfoil Separation Control;AIAA Journal;2018-05
4. Spatial Growth of the Spanwise Disturbance Induced by a Synthetic Jet on Separation Control over an Airfoil;53rd AIAA Aerospace Sciences Meeting;2015-01-03
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