Coupled High Pressure-Temperature Effects on Performance of Dielectric Barrier Discharge Actuators (2022)

No AccessTechnical NotesCoupled High Pressure-Temperature Effects on Performance of Dielectric Barrier Discharge ActuatorsHassen Dammak, Philippe Versailles and Huu Duc VoHassen DammakPolytechnique Montreal, Montreal, Quebec H3T 1 J4, Canada, Philippe VersaillesPolytechnique Montreal, Montreal, Quebec H3T 1 J4, Canada and Huu Duc VoPolytechnique Montreal, Montreal, Quebec H3T 1 J4, CanadaPublished Online:27 Apr 2022https://doi.org/10.2514/1.J061405SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations About References [1] Enloe C. L., McLaughlin T. E., Van Dyken R. D., Kachner K. D., Jumper E. 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C., Iqbal M., Kozlov A. and Schatzman D., "Optimization of Dielectric Barrier Discharge Plasma Actuators for Active Aerodynamic Flow Control," AIAA Journal, Vol. 47, No. 9, 2009, pp. 2169–2178. https://doi.org/10.2514/1.41588 LinkGoogle Scholar Previous article Next article FiguresReferencesRelatedDetails What's Popular Volume 60, Number 6June 2022 CrossmarkInformationCopyright © 2022 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 1533-385X to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp. TopicsActuatorsAerodynamicsAeronauticsAviationAviation RiskAviation SafetyAvionicsCompressor StallElectric HeatingFluid DynamicsHeating SystemHeating, Ventilating, and Air ConditioningIntegrated CircuitsSemiconductor DevicesThermal Control and ProtectionThermal EffectsThermal InsulationThermal MeasurementThermocouplesThermodynamicsThermophysics and Heat Transfer KeywordsPlasma ActuatorDielectric Barrier DischargeTemperature EffectsParticle Image VelocimetryAtmospheric ConditionsThermocouplesAero EngineBoundary Layer SeparationCharge Coupled DeviceComputational Fluid Dynamics SimulationAcknowledgmentsThe authors would like to thank the Natural Sciences and Engineering Research Council of Canada, whose funding under the Discovery Grants program was used for this research. The authors also gratefully acknowledge the support of Njuki W. Mureithi and Xin Gu for the particle image velocimetry system, and Philippe Massé for his help in setting up the experimental apparatus.PDF Received29 October 2021Accepted14 March 2022Published online27 April 2022