Experimental investigation of influence of sliding discharge DBD plasma on low-speed boundary layer
Author:
Affiliation:
1. Nanjing University of Science and Technology, Nanjing 210094, China
2. Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
3. Shenyang Aircraft Design and Research Institute, Shenyang 110035, China
Publisher
AIP Publishing
Subject
General Physics and Astronomy
Link
http://aip.scitation.org/doi/pdf/10.1063/1.5134848
Reference35 articles.
1. Aerodynamic flow acceleration using paraelectric and peristaltic electrohydrodynamic effects of a One Atmosphere Uniform Glow Discharge Plasma
2. Separation Control on HIgh Angle of Attack Airfoil Using Plasma Actuators
3. Stall control at high angle of attack with plasma sheet actuators
4. Optimization of a dielectric barrier discharge actuator by stationary and non-stationary measurements of the induced flow velocity: application to airflow control
5. Single dielectric barrier discharge plasma enhanced aerodynamics: physics, modeling and applications
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1. Characteristics of a nanosecond pulsed sliding discharge plasma actuator at low pressure;AIP Advances;2023-07-01
2. Experimental investigation of the dynamic characteristics of the flow generated by a sliding dielectric barrier discharge in the flat plate boundary layer flow;Physics of Fluids;2023-01
3. Numerical Study of Stream-wise and Span-wise Nanosecond DBD Plasma Actuators Effects on Supersonic Flow Separation;Journal of Applied Fluid Mechanics;2022-07-01
4. Experimental investigation of induced velocity by dielectric barrier discharge plasma actuator in different configurations;AIP Advances;2021-10-01
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