Effect of Vortex Generators on Transonic Swept Wings

This paper examines the effects of corotating blade-type vortex generators on transonic sweptback wings using computational fluid dynamics studies. Infinite-span (two-dimensional) swept wings are first considered to understand the basic physics of vortex generators. Sweep angles are given virtually...

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Veröffentlicht in:	Journal of aircraft 2016-11, Vol.53 (6), p.1890-1904
Hauptverfasser:	Ito, Yasushi, Yamamoto, Kazuomi, Kusunose, Kazuhiro, Koike, Shunsuke, Nakakita, Kazuyuki, Murayama, Mitsuhiro, Tanaka, Kentaro
Format:	Artikel
Sprache:	eng
Schlagworte:	Boundary layers Computational fluid dynamics Fluid flow Incidence angle Local flow Sweep angle Swept wings Sweptback wings Three dimensional models Vortex generators Vortices Wing tip vortices
Online-Zugang:	Volltext
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