Artigo Acesso aberto Revisado por pares

Single-Pixel Particle Image Velocimetry for Characterization of Dielectric Barrier Discharge Plasma Actuators

2020; American Institute of Aeronautics and Astronautics; Volume: 58; Issue: 11 Linguagem: Inglês

10.2514/1.j059239

ISSN

1533-385X

Autores

Taku Nonomura, Yuta Ozawa, Takuma Ibuki, Koki Nankai, Atsushi Komuro, Hiroyuki Nishida, Marios Kotsonis, Noritsugu Kubo, Hirokazu Kawabata,

Tópico(s)

Icing and De-icing Technologies

Resumo

No AccessTechnical NotesSingle-Pixel Particle Image Velocimetry for Characterization of Dielectric Barrier Discharge Plasma ActuatorsTaku Nonomura, Yuta Ozawa, Takuma Ibuki, Koki Nankai, Atsushi Komuro, Hiroyuki Nishida, Kotsonis Marios, Noritsugu Kubo and Hirokazu KawabataTaku NonomuraTohoku University, Sendai 980-8579, Japan, Yuta OzawaTohoku University, Sendai 980-8579, Japan, Takuma IbukiTohoku University, Sendai 980-8579, Japan, Koki NankaiTohoku University, Sendai 980-8579, Japan, Atsushi KomuroTohoku University, Sendai 980-8579, Japan, Hiroyuki NishidaTokyo University of Agriculture and Technology, Koganei 184-8588, Japan, Kotsonis MariosDelft University of Technology, 2629 HS Delft, The Netherlands, Noritsugu KuboNational Institute of Advanced Industrial Science and Technology, Koriyama 464-8603, Japan and Hirokazu KawabataNational Institute of Advanced Industrial Science and Technology, Koriyama 464-8603, JapanPublished Online:2 Sep 2020https://doi.org/10.2514/1.J059239SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Matsuda H., Tanaka M., Osako T., Yamazaki K., Shimura N., Asayama M. and Oryu Y., "Plasma Actuation Effect on a MW Class Wind Turbine," International Journal of Gas Turbine, Propulsion and Power Systems, Vol. 9, No. 1, 2015, pp. 47–52. 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Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. 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. TopicsActuatorsAerodynamicsAeronautical EngineeringAeronauticsAvionicsComputational Fluid DynamicsConservation of Momentum EquationsEquations of Fluid DynamicsExperimental Fluid DynamicsFlow MeasurementFlow RegimesFluid DynamicsFluid Flow PropertiesFluid MechanicsGuidance, Navigation, and Control SystemsSkin FrictionVelocimetry KeywordsParticle Image VelocimetryPlasma ActuatorDielectric Barrier DischargeKinematic ViscositySkin FrictionPressure CoefficientAlternating CurrentComputational Fluid DynamicsNavier Stokes EquationsArchimedes NumbersAcknowledgmentsM. Kotsonis was funded by the Japanese Society for Promotion of Science Postdoctoral Fellowship (grant number P17363) and supported by Tohoku University. T. Nonomura was funded by the Japan Science and Technology Agency Presto (grant number JPMJPR1678). The reference plasma actuator (PAK-Ref03) was provided by the National Institute of Advanced Industrial Science and Technology.PDF Received15 November 2019Accepted31 July 2020Published online2 September 2020

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