Controlling the near vortex wake of a swept half-wing by means of mini-flaps

The effect of mini-flaps on the flow pattern in the near vortex wake behind a model swept half-wing is investigated. The distributions of the time-average flow velocity were measured in a subsonic wind tunnel, in a section normal to the freestream velocity vector located at a distance of 3.8 wing ha...

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Veröffentlicht in:	Fluid dynamics 2008-10, Vol.43 (5), p.718-724
Hauptverfasser:	Zhigulev, S. V., Kogan, M. N., Kuryachii, A. P., Litvinov, V. M., Uspenskii, A. A.
Format:	Artikel
Sprache:	eng
Schlagworte:	Classical and Continuum Physics Classical Mechanics Computational fluid dynamics Engineering Fluid Dynamics Fluid flow Fluid- and Aerodynamics Mathematical analysis Physics Physics and Astronomy Subsonic wind tunnels Trailing edges Vectors (mathematics) Vortices Wakes
Online-Zugang:	Volltext
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