Flow Control to the surface on Airfoil with Plasma Synthetic Jet Actuator

• DOI: 10.1299/jsmemecjo.2003.7.0_255
• Publication Date: 2017-08-05T18:50:16Z
• Authors: Naoki NAKATANI; Kakuji OGAWARA; Souichi SAEKI
• Keywords: Plasma actuator; Flow Control; Synthetic jet; Rotary actuator

This paper presents a novel actuator for flow control, namely Plasma Synthetic Jet Actuator. is glow-discharge actuator, which composed of the electrodes with AC signal. In this present study, it was applied to separation control airfoil. To observe behavior in experiment, visualization used And NACA0012 blade, embedded, set wind tunnel. The wake velocity behind blade measured or without operating actuator. Consequently, desirable effect proposed could be observed. These results show that can execute surface on