An experimental study on laminar separation bubble and transition over an aerofoil at low reynolds number

Basit Öğe Kaydı
dc.authorscopusid54977980200
dc.authorscopusid24400712600
dc.authorscopusid55805951800
dc.authorscopusid57203990469
dc.contributor.authorKarasu, Ilyas
dc.contributor.authorGenç, MMustafa Serdar
dc.contributor.authorAçikel, H. Hakan
dc.contributor.authorAkpolat, M. Tu?rul
dc.date.accessioned2024-09-19T15:41:14Z
dc.date.available2024-09-19T15:41:14Z
dc.date.issued2012
dc.departmentHatay Mustafa Kemal Üniversitesien_US
dc.descriptionAmerican Institute for Aeronautics and Astronautics (AIAA)en_US
dc.description30th AIAA Applied Aerodynamics Conference 2012 -- 25 June 2012 through 28 June 2012 -- New Orleans, LA -- 98230en_US
dc.description.abstractLaminar separation bubble over NACA2415 aerofoil at Re=50,000 and different angles of attack was investigated in detail by performing force, pressure, hot-wire and flow visualization via smoke wire technique. From the experiments, the flow separation, the reattachment and forming the laminar separation bubble were clearly seen. From the experimental results, it was indicated that the point of separation moved towards the leading edge as the angle of attack increased. Moreover, the flow visualization results showed that as the angle of attack increased further, at the angle of attack of 13o the bubble burst and the separated flow was not able to reattach to the aerofoil surface, which indicated the stall. © 2012 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.en_US
dc.identifier.doi10.2514/6.2012-3030
dc.identifier.endpage1592en_US
dc.identifier.isbn978-162410185-4
dc.identifier.scopus2-s2.0-84880767537en_US
dc.identifier.scopusqualityN/Aen_US
dc.identifier.startpage1584en_US
dc.identifier.urihttps://doi.org/10.2514/6.2012-3030
dc.identifier.urihttps://hdl.handle.net/20.500.12483/14117
dc.indekslendigikaynakScopusen_US
dc.language.isoenen_US
dc.publisherAmerican Institute of Aeronautics and Astronautics Inc.en_US
dc.relation.ispartof30th AIAA Applied Aerodynamics Conference 2012en_US
dc.relation.publicationcategoryKonferans Öğesi - Uluslararası - Kurum Öğretim Elemanıen_US
dc.rightsinfo:eu-repo/semantics/closedAccessen_US
dc.subjectFlow separationen_US
dc.subjectFlow visualizationen_US
dc.subjectLaminar flowen_US
dc.subjectReynolds numberen_US
dc.subjectAngles of attacken_US
dc.subjectHot wiresen_US
dc.subjectLaminar separation bubbleen_US
dc.subjectLow Reynolds numberen_US
dc.subjectSeparated flowsen_US
dc.subjectSmoke wire techniqueen_US
dc.subjectVisualization resultsen_US
dc.subjectAngle of attacken_US
dc.titleAn experimental study on laminar separation bubble and transition over an aerofoil at low reynolds numberen_US
dc.typeConference Objecten_US

Dosyalar

Orijinal paket
Listeleniyor 1 - 1 / 1
[ N/A ]
İsim:
Tam Metin / Full Text
Boyut:
745.64 KB
Biçim:
Adobe Portable Document Format
İndir

Koleksiyon

Scopus İndeksli Yayınlar Koleksiyonu