Experimental Characterization of a Novel Cyclotronic Plasma Actuator
Author:
Funder
Langley Research Center
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/am-pdf/10.2514/1.J058708
Reference29 articles.
1. Dielectric Barrier Discharge Plasma Actuators for Flow Control
2. Optimization of Dielectric Barrier Discharge Plasma Actuators for Active Aerodynamic Flow Control
3. Optimization of a dielectric barrier discharge actuator by stationary and non-stationary measurements of the induced flow velocity: application to airflow control
4. Electrohydrodynamic Flow Control with a Glow-Discharge Surface Plasma
5. Dielectric Barrier Discharge Flow Control at Very Low Flight Reynolds Numbers
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