AERODYNAMISCHE KLAPPE EINES FLUGZEUGS MIT EINER DEN KLAPPENWIRBEL BEEINFLUSSENDEN VORRICHTUNG

A high-lift flap of an aircraft is provided having a device for influencing the flap vortex as well as a device for influencing the flap vortex at the lateral edge of the aerodynamic high-lift flap, which can be achieved effectively and at low cost.

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: REICHENBERGER, JOHANN, MAU, KNUT, BORCHERS, INGO, DROBIETZ, ROGER, GRUENEWALD, MICHAEL
Format: Patent
Sprache:ger
Online-Zugang:Volltext bestellen
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
Beschreibung
Zusammenfassung:A high-lift flap of an aircraft is provided having a device for influencing the flap vortex as well as a device for influencing the flap vortex at the lateral edge of the aerodynamic high-lift flap, which can be achieved effectively and at low cost.