INVESTIGATING THE EFFECTS OF PLASMA ACTUATOR ON THE FLOW CONTROL AROUND NACA2415 AIRFOIL

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dc.contributor.authorSanlisoy, Aytac
dc.contributor.authorAkansu, Yahya Erkan
dc.date.accessioned2024-11-07T13:32:09Z
dc.date.available2024-11-07T13:32:09Z
dc.date.issued2020
dc.departmentNiğde Ömer Halisdemir Üniversitesi
dc.description.abstractIn this study, the effects of the plasma actuator on flow control at varied Reynolds numbers and attack angles are examined. Plasma actuator is placed on the NACA2415 airfoil at x/C = 0.1. The effect of the actuator to active flow control is examined at Reynolds number between 8x10(3) and 9x10(4) in the wind tunnel. The lift force which acted on the airfoil was measured by using a force balance system. The velocity measurements were done by the hot-wire probe, located at the wake region, and the flow around model was visualized by the smoke wire method. When the plasma was active, an increased lift force and a narrowed wake region are observed. The stall angle shifted to the higher attack angle by the effective active flow control at low Reynolds numbers. Prevent of the flow separation was enhanced up to 18 degrees angle of attack and the maximum lift force occurred at the 14 degrees angle of attack which is doubled when the plasma actuator is on.
dc.description.sponsorshipScientific and Technological Research Council of Turkey (TUBITAK) [110M056]
dc.description.sponsorshipThe authors would like to acknowledge the financial support of this work by the Scientific and Technological Research Council of Turkey (TUBITAK) under the Contract Number of 110M056. The authors also thank the rest of project team for their assistance in the performing of the study.
dc.identifier.endpage139
dc.identifier.issn1300-3615
dc.identifier.issue1
dc.identifier.scopus2-s2.0-85096779961
dc.identifier.scopusqualityQ4
dc.identifier.startpage131
dc.identifier.trdizinid365257
dc.identifier.urihttps://search.trdizin.gov.tr/tr/yayin/detay/365257
dc.identifier.urihttps://hdl.handle.net/11480/15253
dc.identifier.volume40
dc.identifier.wosWOS:000537942400011
dc.identifier.wosqualityQ4
dc.indekslendigikaynakWeb of Science
dc.indekslendigikaynakScopus
dc.indekslendigikaynakTR-Dizin
dc.language.isoen
dc.publisherTurkish Soc Thermal Sciences Technology
dc.relation.ispartofIsi Bilimi Ve Teknigi Dergisi-Journal of Thermal Science and Technology
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanı
dc.rightsinfo:eu-repo/semantics/closedAccess
dc.snmzKA_20241106
dc.subjectairfoil
dc.subjectflow control
dc.subjectlift force
dc.subjectplasma actuator
dc.titleINVESTIGATING THE EFFECTS OF PLASMA ACTUATOR ON THE FLOW CONTROL AROUND NACA2415 AIRFOIL
dc.title.alternativePLAZMA AKTÜATÖRÜN NACA2415 AIRFOIL ETRAFINDA AKIŞ KONTROLÜNE ETKİLERİNİN ARAŞTIRILMASI
dc.typeArticle

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