Airflow Control by DBD Actuator Over an MDA Airfoil

Efforts have been performed on utilizing the dielectric barrier discharge actuator to control the flow separation over the top of the flap of a three-element airfoil. Images of the flow fields visualized by a particle image velocimetry system with actuators OFF and ON at the free-stream speeds of 20...

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Bibliographic Details
Published in:IEEE transactions on plasma science 2014-10, Vol.42 (10), p.2820-2821
Main Authors: Li, Jiang, Yang, Leilei, Wang, Bin, Cai, Jinsheng, Wang, Guangqiu
Format: Article
Language:English
Subjects:
Actuators
Aircraft
Automotive components
dielectric breakdown
Dielectrics
flow control
Lasers
Plasmas
Visualization
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Description
Summary:Efforts have been performed on utilizing the dielectric barrier discharge actuator to control the flow separation over the top of the flap of a three-element airfoil. Images of the flow fields visualized by a particle image velocimetry system with actuators OFF and ON at the free-stream speeds of 20 and 30 m/s are presented.
ISSN:0093-3813
1939-9375
DOI:10.1109/TPS.2014.2322931