Unsteady Vortex Structure Induced by a Trielectrode Sliding Discharge Plasma Actuator

Abstract

No AccessTechnical NotesUnsteady Vortex Structure Induced by a Trielectrode Sliding Discharge Plasma ActuatorBorui Zheng, Ming Xue, Xizheng Ke, Chang Ge, YuShuai Wang, Feng Liu and Shijun LuoBorui ZhengXi’an University of Technology, 710048 Xi’an, People’s Republic of China*Lecturer, School of Automation and Information Engineering, Shaanxi; also Postdoctoral Researcher, Science and Technology on Plasma Dynamics Laboratory, Air Force Engineering University, Xi’an, PRC; .Search for more papers by this author, Ming XueNorthwestern Polytechnical University, 710072 Xi’an, People’s Republic of China†Ph.D. Candidate, Department of Aeronautics and Astronautics, Shaanxi.Search for more papers by this author, Xizheng KeXi’an University of Technology, 710048 Xi’an, People’s Republic of China‡Professor, School of Automation and Information Engineering, Shaanxi.Search for more papers by this author, Chang GeXi’an University of Technology, 710048 Xi’an, People’s Republic of China§Postdoctoral Researcher, School of Mechanical and Precision Instrument Engineering, Shaanxi.Search for more papers by this author, YuShuai WangNorthwestern Polytechnical University, 710072 Xi’an, People’s Republic of China†Ph.D. Candidate, Department of Aeronautics and Astronautics, Shaanxi.Search for more papers by this author, Feng LiuUniversity of California, Irvine, Irvine, California 92697-3975¶Professor, Department of Mechanical and Aerospace Engineering. Fellow AIAA.Search for more papers by this author and Shijun LuoUniversity of California, Irvine, Irvine, California 92697-3975**Researcher, Department of Mechanical and Aerospace Engineering.Search for more papers by this authorPublished Online:3 Dec 2018https://doi.org/10.2514/1.J057596SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Adamovich I., Baalrud S. D., Bogaerts A., Bruggeman P. J., Cappelli M., Colombo V., Czarnetzki U., Ebert U., Eden J. G. and Favia P., “The 2017 Plasma Roadmap: Low Temperature Plasma Science and Technology,” Journal of Physics D: Applied Physics, Vol. 50, No. 32, 2017, Paper 323001. doi:https://doi.org/10.1088/1361-6463/aa76f5 JPAPBE 0022-3727 CrossrefGoogle Scholar[2] Wang J. J., Choi K. S., Feng L. H., Jukes T. N. and Whalley R. D., “Recent Developments in DBD Plasma Flow Control,” Progress in Aerospace Sciences, Vol. 62, Oct. 2013, pp. 52–78. doi:https://doi.org/10.1016/j.paerosci.2013.05.003 PAESD6 0376-0421 CrossrefGoogle Scholar[3] Corke T. C., Enloe C. L. and Wilkinson S. P., “Dielectric Barrier Discharge Plasma Actuators for Flow Control,” Annual Review of Fluid Mechanics, Vol. 42, Jan. 2010, pp. 505–529. doi:https://doi.org/10.1146/annurev-fluid-121108-145550 ARVFA3 0066-4189 CrossrefGoogle Scholar[4] Benard N. and Moreau E., “Electrical and Mechanical Characteristics of Surface AC Dielectric Barrier Discharge Plasma Actuators Applied to Airflow Control,” Experiments in Fluids, Vol. 55, Nov. 2014, Paper 1846. doi:https://doi.org/10.1007/s00348-014-1846-x EXFLDU 0723-4864 CrossrefGoogle Scholar[5] Steven D. S., Richard E. H. and William B., “Improving Performance of a Sliding Dielectric Barrier Discharge Actuator Using Multiple Potentials,” AIAA Journal, Vol. 54, No. 10, 2016, pp. 3313–3316. doi:https://doi.org/10.2514/1.J055108 AIAJAH 0001-1452 Google Scholar[6] Louste C., Artana G., Moreau E. and Touchard G., “Sliding Discharge in Air at Atmospheric Pressure: Electrical Properties,” Journal of Electrostatics, Vol. 63, Nos. 6-10, 2005, pp. 615–620. doi:https://doi.org/10.1016/j.elstat.2005.03.026 JOELDH 0304-3886 CrossrefGoogle Scholar[7] Moreau E., Sosa R. and Artana G., “Electric Wind Produced by Surface Plasma Actuators: A New Dielectric Barrier Discharge Based on a Three-Electrode Geometry,” Journal of Physics D: Applied Physics, Vol. 41, No. 11, 2008, Paper 115204. doi:https://doi.org/10.1088/0022-3727/41/11/115204 JPAPBE 0022-3727 CrossrefGoogle Scholar[8] Bénard N., Jolibois J., Moreau E., Sosa R., Artana G. and Touchard G., “Aerodynamic Plasma Actuators: A Directional Micro-Jet Device,” Thin Solid Films, Vol. 516, No. 19, 2008, pp. 6660–6667. doi:https://doi.org/10.1016/j.tsf.2007.11.039 THSFAP 0040-6090 CrossrefGoogle Scholar[9] Nishida H., Nakia K. and Matsuno T., “Physical Mechanism of Tri-Electrode Plasma Actuator with Direct-Current High Voltage,” AIAA Journal, Vol. 55, No. 6, 2017, pp. 1852–1861. doi:https://doi.org/10.2514/1.J055560 AIAJAH 0001-1452 LinkGoogle Scholar[10] Berendt A., Podlinski J. and Mizeraczyk J., “Multi-DBD Actuator with Floating Inter-Electrode for Aerodynamic Control,” Nukleonika, Vol. 57, No. 2, 2012, pp. 249–252. NUKLAS 0029-5922 Google Scholar[11] Zheng B. R., Gao C., Li Y. B., Liu F. and Luo S. J., “Flow Control Over a Conical Forebody by Duty-Cycle Actuations,” Plasma Science and Technology, Vol. 14, No. 1, 2012, pp. 58–63. doi:https://doi.org/10.1088/1009-0630/14/1/13 1009-0630 CrossrefGoogle Scholar[12] Zheng B. R., Gao C., Li Y. B., Liu F. and Luo S. J., “Flow Control Over a Conical Forebody by Periodic Pulsed Plasma Actuation,” Plasma Science and Technology, Vol. 15, No. 4, 2013, pp. 350–356. doi:https://doi.org/10.1088/1009-0630/15/4/08 1009-0630 CrossrefGoogle Scholar[13] Neretti G., Cristofolini A. and Borghi C., “Experimental Investigation on a Vectorized Aerodynamic Dielectric Barrier Discharge Plasma Actuator Array,” Journal of Applied Physics, Vol. 115, No. 16, 2014, Paper 163304. doi:https://doi.org/10.1063/1.4873896 JAPIAU 0021-8979 CrossrefGoogle Scholar Previous article Next article FiguresReferencesRelatedDetailsCited byCombustion Characteristics of Hydrogen/Air Mixtures in a Plasma-Assisted Micro Combustor27 February 2023 | Energies, Vol. 16, No. 5Pulsed Velocity Created by a Plasma Actuator in the Vicinity of the WallXin Zhang and Yong Huang15 January 2023 | AIAA Journal, Vol. 0, No. 0Experimental investigation of the dynamic characteristics of the flow generated by a sliding dielectric barrier discharge in the flat plate boundary layer flowPhysics of Fluids, Vol. 35, No. 1Recent developments in thermal characteristics of surface dielectric barrier discharge plasma actuators driven by sinusoidal high-voltage powerChinese Journal of Aeronautics, Vol. 36, No. 1Evolution of a single sessile droplet under the influence of the dielectric barrier discharge plasma actuatorPhysics of Fluids, Vol. 34, No. 12Electrical and aerodynamic characteristics of sliding discharge based on a microsecond pulsed plasma supply22 August 2022 | Plasma Science and Technology, Vol. 24, No. 11Sliding discharge plasma jet actuators for circular-cylinder wake modification8 November 2022 | Modern Physics Letters B, Vol. 36, No. 25Formation Mechanism of Wall Jet Generated by Plasma Actuators in Quiescent AirXin Zhang and Feng Qu2 May 2022 | AIAA Journal, Vol. 60, No. 8Spatial–temporal evolution of the pressure field generated by a plasma actuator in quiescent airPhysics of Fluids, Vol. 34, No. 7Analysis of discharge characteristics of pulsed plasma power source in the microsecond scaleJournal of Physics: Conference Series, Vol. 2313, No. 1Deflected Synthetic Jet due to Vortices Induced by a Tri-Electrode Plasma ActuatorMing Xue, Zhangsong Ni, Chao Gao, Bin Wu and Borui Zheng31 March 2022 | AIAA Journal, Vol. 60, No. 6A comparative study on post-stall flow separation control mechanism of steady and unsteady plasma actuators20 April 2022 | Physics of FluidsVortex Shedding Frequency Scaling of Coherent Structures Induced by a Plasma ActuatorXin Zhang and Haohua Zong21 September 2021 | AIAA Journal, Vol. 60, No. 2Acoustic streaming in water induced by an asymmetric dielectric-barrier-discharge plasma actuator at the initiation stagePhysics of Fluids, Vol. 34, No. 1The spatial-temporal evolution process of flow field generated by a pulsed-DC plasma actuator in quiescent airAerospace Science and Technology, Vol. 72Periodic Oscillating Flow Created by a Single Dielectric Barrier Discharge Plasma ActuatorXin Zhang and Chang Wang1 March 2021 | AIAA Journal, Vol. 59, No. 5Acoustic streaming flow generated by surface dielectric barrier discharge in quiescent airPhysics of Fluids, Vol. 33, No. 5Unsteady Flow Structures Induced by Single Microsecond-Pulsed Plasma ActuatorXin Zhang, Y. D. Cui, Jonathan Chien Ming Tay and B. C. Khoo10 March 2020 | AIAA Journal, Vol. 58, No. 7Forebody asymmetric vortex control with extended dielectric barrier discharge plasma actuators*Chinese Physics B, Vol. 29, No. 6Discharge and flow characterizations of the double-side sliding discharge plasma actuator*Chinese Physics B, Vol. 29, No. 6Sliding discharge plasma actuation for forebody vortex control on a slender body at high angles of attackAIP Advances, Vol. 10, No. 5The pressure wave induced by an asymmetrical Dielectric Barrier Discharge plasma actuator under the influence of residual chargeAerospace Science and Technology, Vol. 99Electrical and Flow Characteristics of a Double-Side Sliding Pulsed Discharge Plasma ActuatorBorui Zheng, Xizheng Ke, Chang Ge, Yifei Zhu, Yun Wu, Feng Liu and Shijun Luo25 October 2019 | AIAA Journal, Vol. 58, No. 2Unsteady Flow Structures Induced by a Single Microsecond Pulsed DBD Plasma Actuator in Quiescent AirXin Zhang, Yongdong Cui, Jonathan Chien Ming Tay and Boo Cheong Khoo5 January 2020The effect of the voltage waveform on performance of dielectric barrier discharge plasma actuatorJournal of Applied Physics, Vol. 126, No. 17Experimental Study on Plasma Flow Control of Symmetric Flying Wing Based on Two Kinds of Scaling Models9 October 2019 | Symmetry, Vol. 11, No. 10 What's Popular Volume 57, Number 1January 2019 CrossmarkInformationCopyright © 2018 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved. All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the ISSN 0001-1452 (print) or 1533-385X (online) to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp. TopicsActuatorsAerodynamic PerformanceAerodynamicsAeronautical EngineeringAeronauticsAvionicsComputational Fluid DynamicsExperimental Fluid DynamicsFlow MeasurementFlow RegimesFluid DynamicsFluid Flow PropertiesGuidance, Navigation, and Control SystemsVelocimetryVortex DynamicsWind Tunnels KeywordsVortex StructurePlasma ActuatorFlow CharacteristicsDielectric Barrier DischargeFlow VisualizationParticle Image VelocimetryAerodynamic FlowsElectric PotentialJet VectoringComputational Fluid Dynamics SimulationAcknowledgmentsThe present study was supported by the National Natural Science Foundation of China (no. 51607188), the Ph.D. research startup foundation of Xi’an University of Technology (no. 256081802), and the Xi’an Science and Technology Project [201805037YD15CG21(28)]. We would like to express our gratitude to Zhengke Zhang of Northwestern Polytechnical University for his valuable technical guidance.PDF Received6 June 2018Accepted22 September 2018Published online3 December 2018