Multifactorial Effects of Operating Conditions of Dielectric-Barrier-Discharge Plasma Actuator on Laminar-Separated-Flow Control

Authors :: Kozo Fujii
Taku Nonomura
Makoto Sato
Koichi Okada
Kengo Asada
Aiko Yakeno
Hikaru Aono
Source :: AIAA Journal. 53(9):2544-2559
Publication Year :: 2015
Publisher :: American Institute of Aeronautics and Astronautics, 2015.
Abstract: Accepted: 2015-01-06<br />資料番号: SA1150075000

Subjects :: Physics::Fluid Dynamics
Airfoil
Lift-to-drag ratio
Lift coefficient
Flow control (fluid)
Drag coefficient
Materials science
Control theory
Angle of attack
Aerospace Engineering
Mechanics
Plasma actuator
NACA airfoil

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