On the Possibility of Cross-Flow Vortex Cancellation by Plasma Actuators
Cancellation of the cross-flow vortices in a swept-wing boundary layer is attempted by plasma actuator array in numerical simulation. The response of the boundary layer to the stationary excitation by a single actuator section is measured experimentally and compared to the response obtained from the...
Main Authors: | Amir Abdullaev, Alexander Kotvitskii, Ivan Moralev, Maxim Ustinov |
---|---|
Format: | Article |
Language: | English |
Published: |
MDPI AG
2023-05-01
|
Series: | Aerospace |
Subjects: | |
Online Access: | https://www.mdpi.com/2226-4310/10/5/469 |
Similar Items
-
Flow control of rectangular jet by DBD plasma actuators
by: Yoshihisa KATO, et al.
Published: (2015-03-01) -
Plasma Actuation for the Turbulent Mixing of Fuel Droplets and Oxidant Air in an Aerospace Combustor
by: Zhengqi Tai, et al.
Published: (2023-01-01) -
Ionizing Waves in Surface Dielectric Barrier Discharges Plasma Actuators
by: Ruggero Barni, et al.
Published: (2024-02-01) -
Turbulent Boundary Layer Separation Control Using Magnetohydrodynamic Plasma Actuator
by: Alexander Kotvitskii, et al.
Published: (2023-10-01) -
Stall Control by Plasma Actuators: Characterization along the Airfoil Span
by: Giulia Zoppini, et al.
Published: (2020-03-01)