Role of surface discharge dynamics in the generation of electrohydrodynamic force: toward performance improvement of dielectric barrier discharge plasma actuators

被引:1
作者
Sato, Shintaro [1 ]
Ohnishi, Naofumi [1 ]
机构
[1] Tohoku Univ, Dept Aerosp Engn, Sendai 9808579, Japan
关键词
dielectric barrier discharge; electrohydrodynamics; plasma actuator; numerical simulation; plasma fluid model; surface charge; FLOW SEPARATION CONTROL; PARTICLE-IN-CELL; AIR-FLOW; ATMOSPHERIC-PRESSURE; BOUNDARY-LAYER; ENHANCED AERODYNAMICS; CORONA DISCHARGE; STALL CONTROL; HIGH-SPEED; HIGH-ANGLE;
D O I
10.1088/1361-6463/adb3af
中图分类号
O59 [应用物理学];
学科分类号
摘要
Dielectric barrier discharge (DBD) plasma actuators are devices that actively control the airflow using nonequilibrium atmospheric-pressure plasmas, showing promise for practical applications in the field of aerospace engineering. Numerous studies have revealed the dynamics of surface discharge and the process of generating electrohydrodynamic (EHD) force in detail. The performance of DBD plasma actuators has improved continuously over the past 20 years. However, there is a need for further improvement in EHD force generation to enable the practical applications of DBD plasma actuators. In this review, we provide insights that contribute to the development of a high-performance DBD plasma actuator by reviewing previous studies focused on revealing the surface discharge and EHD force generation processes. The foundations of the discharge process in DBD plasma actuators are briefly described from the perspectives of experiments and numerical simulations. We also reviewed various strategies for improving EHD force generation by optimizing the geometric structure and the applied voltage waveform as well as by controlling the surface charge accumulation. Improving EHD force generation and its efficiency is a fundamental research area to realize the practical applications of a novel active airflow control device that uses nonequilibrium plasmas.
引用
收藏
页数:42
相关论文
共 160 条
[71]   Numerical simulation on mode transition of atmospheric dielectric barrier discharge in helium-oxygen mixture [J].
Lee, D ;
Park, JM ;
Hong, SH ;
Kim, Y .
IEEE TRANSACTIONS ON PLASMA SCIENCE, 2005, 33 (02) :949-957
[72]   Influence of a DC corona discharge on the airflow along an inclined flat plate [J].
Léger, L ;
Moreau, E ;
Artana, G ;
Touchard, G .
JOURNAL OF ELECTROSTATICS, 2001, 51 (1-4) :300-306
[73]   Dynamics of near-surface electric discharges and mechanisms of their interaction with the airflow [J].
Leonov, Sergey B. ;
Adamovich, Igor V. ;
Soloviev, Victor R. .
PLASMA SOURCES SCIENCE & TECHNOLOGY, 2016, 25 (06)
[74]   Dynamics of energy coupling and thermalization in barrier discharges over dielectric and weakly conducting surfaces on μs to ms time scales [J].
Leonov, Sergey B. ;
Petrishchev, Vitaly ;
Adamovich, Igor V. .
JOURNAL OF PHYSICS D-APPLIED PHYSICS, 2014, 47 (46)
[75]   Modeling of dielectric barrier discharge plasma actuators driven by repetitive nanosecond pulses [J].
Likhanskii, Alexandre V. ;
Shneider, Mikhail N. ;
Macheret, Sergey O. ;
Miles, Richard B. .
PHYSICS OF PLASMAS, 2007, 14 (07)
[76]  
Lindner M., 2019, AIAA Aviation 2019 Forum, DOI [10.2514/6.2019-2998, DOI 10.2514/6.2019-2998]
[77]   Localized Thermal Perturbations for Control of Turbulent Shear Flows [J].
Little, Jesse .
AIAA JOURNAL, 2019, 57 (02) :655-669
[78]   Separation Control with Nanosecond-Pulse-Driven Dielectric Barrier Discharge Plasma Actuators [J].
Little, Jesse ;
Takashima, Keisuke ;
Nishihara, Munetake ;
Adamovich, Igor ;
Samimy, Mo .
AIAA JOURNAL, 2012, 50 (02) :350-365
[79]   High-lift airfoil trailing edge separation control using a single dielectric barrier discharge plasma actuator [J].
Little, Jesse ;
Nishihara, Munetake ;
Adamovich, Igor ;
Samimy, Mo .
EXPERIMENTS IN FLUIDS, 2010, 48 (03) :521-537
[80]   Closed-Loop Dynamic Stall Control Using a Plasma Actuator [J].
Lombardi, Andrew J. ;
Bowles, Patrick O. ;
Corke, Thomas C. .
AIAA JOURNAL, 2013, 51 (05) :1130-1141