Measurement of Velocity Induced by a Propagating Arc Magneto-hydrodynamic Plasma Actuator
Author:
Affiliation:
1. University of Texas, Austin
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2017-0156
Reference20 articles.
1. Actuators for Active Flow Control
2. Delta Wing Stall and Roll Control Using Segmented Piezoelectric Fluidic Actuators
3. New Generation of Synthetic Jet Actuators
4. Recent developments in DBD plasma flow control
5. Active Flow Control and Part-Span Slat Interactions
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