Sheared wing-tip aerodynamics - Wind-tunnel and computational investigation

Computational and experimental performance benefits are presented for a high-aspect-ratio unswept wing configuration with sheared tips. The sheared tip is a highly swept and highly tapered surface located in the same plane as the inboard wing panel to which it is attached. The compuational results w...

Ausführliche Beschreibung

Bibliographische Detailangaben

Veröffentlicht in:	Journal of aircraft 1989-03, Vol.26 (3), p.207-213
Hauptverfasser:	Vijgen, P. M. H. W, van Dam, C. P, Holmes, B. J
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerodynamics Applied fluid mechanics Exact sciences and technology Fluid dynamics Fundamental areas of phenomenology (including applications) Physics
Online-Zugang:	Volltext
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!