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• W3008701474 abstract "No AccessEngineering NotesOptimization of Dielectric Barrier Discharge Plasma Actuators for Icing ControlHaiyang Hu, Xuanshi Meng, Jinsheng Cai, Wenwu Zhou, Yang Liu and Hui HuHaiyang HuNorthwestern Polytechnical University, 710072 Xi’an, People’s Republic of China*Graduate Student; currenty Doctorate, Iowa State University, Iowa 50011.Search for more papers by this author, Xuanshi MengNorthwestern Polytechnical University, 710072 Xi’an, People’s Republic of China†Professor; (Corresponding Author).Search for more papers by this author, Jinsheng CaiNorthwestern Polytechnical University, 710072 Xi’an, People’s Republic of China‡Professor; .Search for more papers by this author, Wenwu ZhouShanghai Jiao Tong University, 200240 Shanghai, People’s Republic of China§Assistant Professor; .Search for more papers by this author, Yang LiuEast Carolina University, Greenville, North Carolina 27858¶Assistant Professor; .Search for more papers by this author and Hui HuIowa State University, Ames, Iowa 50011**Professor; .Search for more papers by this authorPublished Online:17 Feb 2020https://doi.org/10.2514/1.C035697SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Bragg M. 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M., “Single-Dielectric Barrier Discharge Plasma Enhanced Aerodynamics: Concepts Optimization, and Applications,” Journal of Propulsion and Power, Vol. 24, No. 5, 2008, pp. 935–945. https://doi.org/10.2514/1.24430 LinkGoogle Scholar Previous article FiguresReferencesRelatedDetailsCited byImproving aircraft aerodynamic performance with bionic wing obtained by ice shape modulationChinese Journal of Aeronautics, Vol. 36, No. 2Pulsed Velocity Created by a Plasma Actuator in the Vicinity of the WallXin Zhang and Yong Huang15 January 2023 | AIAA Journal, Vol. 0, No. 0Recent developments in thermal characteristics of surface dielectric barrier discharge plasma actuators driven by sinusoidal high-voltage powerChinese Journal of Aeronautics, Vol. 36, No. 1Recent Developments on Dielectric Barrier Discharge (DBD) Plasma Actuators for Icing Mitigation21 December 2022 | Actuators, Vol. 12, No. 1Plasma Gurney Flap Flight Control at Low Angle of AttackXin Gu, Huu Duc Vo, Njuki W. Mureithi and Eric Laurendeau23 August 2022 | Journal of Aircraft, Vol. 60, No. 1Determining Region of Installation of Flat-Ended Piezoelectric De-Icing Actuators on Curved SurfacesBo Miao , Wen Li, Lang Yuan and Chunling Zhu6 July 2022 | Journal of Aircraft, Vol. 60, No. 1Evolution of a single sessile droplet under the influence of the dielectric barrier discharge plasma actuatorPhysics of Fluids, Vol. 34, No. 12Lagrangian analysis of the flow induced by a dielectric barrier discharge plasma actuator array under burst mode actuationAIP Advances, Vol. 12, No. 11Design of the Thermoelectric Ice Protection System for a Tiltrotor ApplicationAlessandro Zanon and Michele De Gennaro21 April 2022 | Journal of Aircraft, Vol. 59, No. 5Formation Mechanism of Wall Jet Generated by Plasma Actuators in Quiescent AirXin Zhang and Feng Qu2 May 2022 | AIAA Journal, Vol. 60, No. 8Multipurpose distributed dielectric-barrier-discharge plasma actuation: Icing sensing, anti-icing, and flow control in onePhysics of Fluids, Vol. 34, No. 7Spatial–temporal evolution of the pressure field generated by a plasma actuator in quiescent airPhysics of Fluids, Vol. 34, No. 7A comparative study on post-stall flow separation control mechanism of steady and unsteady plasma actuatorsPhysics of Fluids, Vol. 34, No. 5Vortex Shedding Frequency Scaling of Coherent Structures Induced by a Plasma ActuatorXin Zhang and Haohua Zong21 September 2021 | AIAA Journal, Vol. 60, No. 2Characteristics of a nanosecond pulsed dielectric barrier plasma actuator with a surface water filmPhysics of Plasmas, Vol. 29, No. 1Acoustic streaming in water induced by an asymmetric dielectric-barrier-discharge plasma actuator at the initiation stagePhysics of Fluids, Vol. 34, No. 1Numerical simulation of the flow around a square cylinder under plasma actuator controlPhysics of Fluids, Vol. 33, No. 12The spatial-temporal evolution process of flow field generated by a pulsed-DC plasma actuator in quiescent airAerospace Science and Technology, Vol. 118 What's Popular Volume 57, Number 2March 2020 CrossmarkInformationCopyright © 2020 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 eISSN 1533-3868 to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp. TopicsActuatorsAerodynamic PerformanceAerodynamicsAeronautical EngineeringAeronauticsAircraft DesignAircraft Operations and TechnologyAircraft Wing DesignAirfoilAviationAviation SafetyAviation Weather HazardsAvionicsGuidance, Navigation, and Control SystemsWind Tunnels KeywordsPlasma ActuatorDielectric Barrier DischargeAirfoilAerodynamic CharacteristicsAnti IcingStagnation PointSupercoolingAerodynamic EfficiencyThermal EffectsElectrical EnergyAcknowledgmentsThis work is supported by the National Natural Science Foundation of China (grant no. 11672245), the Aeronautical Science Foundation of China (grant no. 2018ZA53), the National Key Laboratory Research Foundation of China (grant no. 9140C420301110C42), and the 111 Project (B17037).PDF Received8 August 2019Accepted7 October 2019Published online17 February 2020" @default.
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