Control of Boundary Layer Separation and the Wake of an Airfoil using ns-DBD Plasma Actuators
The efficacy of nanosecond pulse driven dielectric barrier discharge (ns-DBD) plasma actuators for boundary layer separation and wake control is investigated experimentally. A single ns-DBD plasma actuator is placed at the leading edge of a NACA 0012 airfoil model. Both baseline and controlled flow...
| Main Author: | |
|---|---|
| Other Authors: | |
| Language: | en_US |
| Published: |
The University of Arizona.
2016
|
| Subjects: | |
| Online Access: | http://hdl.handle.net/10150/605119 http://arizona.openrepository.com/arizona/handle/10150/605119 |