A Study on the Plasma Actuator Electrode Geometry Configurations for Improvement of the Aerodynamic Performance of an Airfoil

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dc.authoridYAVUZ, Hakan/0000-0002-6166-0921
dc.contributor.authorAkbiyik, Hurrem
dc.contributor.authorYavuz, Hakan
dc.contributor.authorAkansu, Yahya Erkan
dc.date.accessioned2024-11-07T13:32:17Z
dc.date.available2024-11-07T13:32:17Z
dc.date.issued2018
dc.departmentNiğde Ömer Halisdemir Üniversitesi
dc.description.abstractIn this study, the induced flow effects of plasma generated by various types of electrode geometry configurations are presented. The model chosen for the study is a NACA0015 airfoil. The experiments are conducted in a wind tunnel at Reynolds number of 4.8x10(4). The plasma actuators mounted on the leading edge of the airfoil at chord position of 0.1 (x/C). The plasma actuators consist of an embedded and exposed electrode between which a dielectric material is placed. The applied voltage is set to 7 kV(pp). The excitation frequency is also set to 3.5 kHz. Three different electrode geometry configurations, namely as rinear, saw-tooth and square, are considered for the study. As a part of the experimental study, the two dimensional and three dimensional flow structures generated by the plasma actuators and related analysis results are presented. In addition, necessary measurements are also made to determine the drag and lift forces.
dc.description.sponsorshipScientific Research Projects (BAP) of the Cukurova University [FBA-2017-7111]
dc.description.sponsorshipThe authors would like to acknowledge the financial support of this work by the Scientific Research Projects (BAP) of the Cukurova University under the Contact Number of FBA-2017-7111.
dc.identifier.doi10.5545/sv-jme.2017.5041
dc.identifier.endpage725
dc.identifier.issn0039-2480
dc.identifier.issue12
dc.identifier.scopus2-s2.0-85057873423
dc.identifier.scopusqualityQ3
dc.identifier.startpage719
dc.identifier.urihttps://doi.org/10.5545/sv-jme.2017.5041
dc.identifier.urihttps://hdl.handle.net/11480/15338
dc.identifier.volume64
dc.identifier.wosWOS:000450187100001
dc.identifier.wosqualityQ3
dc.indekslendigikaynakWeb of Science
dc.indekslendigikaynakScopus
dc.language.isoen
dc.publisherAssoc Mechanical Engineers Technicians Slovenia
dc.relation.ispartofStrojniski Vestnik-Journal of Mechanical Engineering
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanı
dc.rightsinfo:eu-repo/semantics/openAccess
dc.snmzKA_20241106
dc.subjectNACA0015 airfoil
dc.subjectlift and drag coefficients
dc.subjectsquare plasma actuator
dc.subjectsawtooth plasma actuator
dc.subjectlinear plasma actuator
dc.titleA Study on the Plasma Actuator Electrode Geometry Configurations for Improvement of the Aerodynamic Performance of an Airfoil
dc.typeArticle

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