- Article
Flow Control around NACA0015 Airfoil Using a Dielectric Barrier Discharge Plasma Actuator over a Wide Range of the Reynolds Number
- Satoshi Sekimoto,
- Kozo Fujii,
- Masayuki Anyoji,
- Yuma Miyakawa,
- Shinichiro Ito,
- Satoshi Shimomura,
- Hiroyuki Nishida,
- Taku Nonomura and
- Takashi Matsuno
In this study, an experimental investigation of separation control using a dielectric barrier discharge plasma actuator was performed on an NACA0015 airfoil over a wide range of Reynolds numbers, angles of attack, and nondimensional burst frequencies...

