Numerical Investigation of Flow Structure around NACA 0018 with slot

Basit Öğe Kaydı
dc.contributor.authorAsan, Omer Fethi
dc.contributor.authorGuler, Emre
dc.contributor.authorAksoy, Muhammed Murat
dc.contributor.authorPınar, Engin
dc.contributor.authorDurhasan, Tahir
dc.date.accessioned2025-01-06T17:24:28Z
dc.date.available2025-01-06T17:24:28Z
dc.date.issued2023
dc.departmentAdana Alparslan Türkeş Bilim ve Teknoloji Üniversitesi
dc.description.abstractWe numerically investigated NACA 0018 airfoil with slot at various angles of attack. The computational fluid dynamics (CFD) results were compared with the base airfoil to show the effectiveness of the airfoil. Reynolds number was kept constant as Re=3x105 to thoroughly understand how different locations of slot would provide passive flow control from aerodynamic perspective. We have used three different slot locations to reveal the effectiveness of the slot compared to the base airfoil for higher angles of attack. Our results show that the slotted design would yield to increase the lift and to delay the stall angle of base airfoil.
dc.identifier.endpage167
dc.identifier.issn2687-3729
dc.identifier.issueEk Sayı
dc.identifier.startpage152
dc.identifier.trdizinid1227160
dc.identifier.urihttps://search.trdizin.gov.tr/tr/yayin/detay/1227160
dc.identifier.urihttps://hdl.handle.net/20.500.14669/1259
dc.identifier.volume6
dc.indekslendigikaynakTR-Dizin
dc.language.isoen
dc.relation.ispartofOsmaniye Korkut Ata Üniversitesi Fen Bilimleri Enstitüsü Dergisi (Online)
dc.relation.publicationcategoryMakale - Ulusal Hakemli Dergi - Kurum Öğretim Elemanı
dc.rightsinfo:eu-repo/semantics/openAccess
dc.snmzKA_20241211
dc.subjectCFD
dc.subjectAirfoil
dc.subjectReynolds number
dc.subjectPassive flow control
dc.subjectSlot
dc.titleNumerical Investigation of Flow Structure around NACA 0018 with slot
dc.typeArticle

Dosyalar

Koleksiyon

TR-Dizin İndeksli Yayınlar Koleksiyonu