Three-Electrode Plasma Synthetic Jet Actuator for High-Speed Flow Control
Author:
Affiliation:
1. Science and Technology on Scramjet Laboratory, National University of Defense Technology, 410073 Changsha, People’s Republic of China
2. Beijing Space Physics Major Laboratory, 100076 Beijing, People’s Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J052686
Reference12 articles.
1. Actuators for Active Flow Control
2. Airflow control by non-thermal plasma actuators
3. Mechanisms and Responses of a Single Dielectric Barrier Plasma Actuator: Plasma Morphology
4. Characterization of a Direct-Current Glow Discharge Plasma Actuator in Low-Pressure Supersonic Flow
5. Properties of surface arc discharge in a supersonic airflow
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