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Effect of tip vortices on flow over NACA4412 aerofoil with different aspect ratios

Effect of tip vortices on flow and laminar separation bubble over NACA4412 aerofoil at low Reynolds numbers and different angles of attack was investigated in detail by performing force and flow visualization via smoke wire technique. Experiments have been done at Reynolds number of 50000 and the wi...

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Autors principals: Genç Mustafa Serdar, Özkan Gökhan, Açikel Halil Hakan, Kiriş Mehmet Sadık, Yildiz Rahime
Format: Artigo
Idioma:Inglês
Publicat: EDP Sciences 2016-01-01
Col·lecció:EPJ Web of Conferences
Accés en línia:http://dx.doi.org/10.1051/epjconf/201611402027
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