Towards laminar flow control on swept wings with AC-DBD plasma actuators as active roughness
Author:
Affiliation:
1. Delft University of Technology
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2017-1459
Reference29 articles.
1. Electrical and mechanical characteristics of surface AC dielectric barrier discharge plasma actuators applied to airflow control
2. Basic experiments on transition in three-dimensional boundary layers dominated by crossflow instability
3. Secondary instability of crossflow vortices: validation of the stability theory by direct numerical simulation
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1. Experimental Investigation of Spanwise-Periodic Surface Heating for Control of Crossflow-Dominated Laminar-Turbulent Transition;IUTAM Laminar-Turbulent Transition;2021-07-31
2. Damping of the longitudinal streak in the boundary layer by ‘plasma panel’ actuator;Journal of Physics D: Applied Physics;2019-05-24
3. Conditioning of cross-flow instability modes using dielectric barrier discharge plasma actuators;Journal of Fluid Mechanics;2017-11-02
4. Effect of Upstream Flow Deformation Using Plasma Actuators on Crossflow Transition Induced by Unsteady Vortical Free-Stream Disturbances;47th AIAA Fluid Dynamics Conference;2017-06-02
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