DocumentCode
17942
Title
Airflow Control by DBD Actuator Over an MDA Airfoil
Author
Jiang Li ; Leilei Yang ; Bin Wang ; Jinsheng Cai ; Guangqiu Wang
Author_Institution
Beijing Aeronaut. Sci. & Technol. Res. Inst., Commercial Aircraft Corp. of China, Beijing, China
Volume
42
Issue
10
fYear
2014
fDate
Oct. 2014
Firstpage
2820
Lastpage
2821
Abstract
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.
Keywords
actuators; aerospace components; dielectric-barrier discharges; flow control; flow visualisation; velocimeters; DBD actuator; MDA; MDA Airfoil; McDonnell Douglas aerospace; airflow control; dielectric barrier discharge; flow field visualisation; particle image velocimetry system; three-element airfoil; Actuators; Aircraft; Automotive components; Dielectrics; Lasers; Plasmas; Visualization; Actuators; dielectric breakdown; flow control; flow control.;
fLanguage
English
Journal_Title
Plasma Science, IEEE Transactions on
Publisher
ieee
ISSN
0093-3813
Type
jour
DOI
10.1109/TPS.2014.2322931
Filename
6819801
Link To Document