Flow Control around NACA0015 Airfoil Using a Dielectric Barrier Discharge Plasma Actuator over a Wide Range of the Reynolds Number

Flow Control around NACA0015 Airfoil Using a Dielectric Barrier Discharge Plasma Actuator over a Wide Range of the Reynolds Number

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. The range of the Reynolds number was based on a...

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Bibliographic Details
Main Authors: Satoshi Sekimoto, Kozo Fujii, Masayuki Anyoji, Yuma Miyakawa, Shinichiro Ito, Satoshi Shimomura, Hiroyuki Nishida, Taku Nonomura, Takashi Matsuno
Format: Article
Language:English
Published: MDPI AG 2023-01-01
Series:Actuators
Subjects:
plasma actuator
NACA0015 airfoil
wind tunnel experiment
wide range of Reynolds number
Online Access:https://www.mdpi.com/2076-0825/12/1/43

Internet

https://www.mdpi.com/2076-0825/12/1/43

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