The flow control mechanism of trailing-edge Gurney flap on a 50°-swept delta wing in forced pitching

The flow control effect of the trailing-edge Gurney flap (TG) on the dynamic lift characteristics for a 50°-swept delta wing during large-amplitude pitching oscillations at various reduced frequencies (k = 0.072, 0.144, 0.287, and 0.575) was investigated via force, particle image velocity, and dye v...

Ausführliche Beschreibung

Bibliographische Detailangaben

Veröffentlicht in:	Physics of fluids (1994) 2024-08, Vol.36 (8)
1. Verfasser:	Akkermans, Rinie A. D.
Format:	Artikel
Sprache:	eng
Schlagworte:	Angle of attack Delta wings Flow control Lift Pressure Pressure effects Trailing edge flaps Trailing edges
Online-Zugang:	Volltext
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!