Wind Tunnel Testing of Plasma Actuator with Two Mesh Electrodes to Boundary Layer Control at High Angle of Attack

Wind Tunnel Testing of Plasma Actuator with Two Mesh Electrodes to Boundary Layer Control at High Angle of Attack

The manuscript presents experimental research carried out on the wing model with the SD 7003 profile. A plasma actuator with DBD (Dielectric Barrier Discharge) discharges was placed on the wing surface to control boundary layer. The experimental tests were carried out in the AeroLab wind tunnel wher...

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Bibliographic Details
Main Authors: Ernest Gnapowski, Jarosław Pytka, Jerzy Józwik, Jan Laskowski, Joanna Michałowska
Format: Article
Language:English
Published: MDPI AG 2021-01-01
Series:Sensors
Subjects:
plasma actuator
flow control
wing airfoil
wind tunnel
mesh electrodes
DBD
Online Access:https://www.mdpi.com/1424-8220/21/2/363

Internet

https://www.mdpi.com/1424-8220/21/2/363

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