An experimental study of tip shape effects on the flutter of aft-swept, flat-plate wings

The effects of tip chord orientation on wing flutter are investigated experimentally using six cantilever-mounted, flat-plate wing models. Experimentally determined flutter characteristics of the six models are presented covering both the subsonic and transonic Mach number ranges. While all models h...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	Dansberry, Bryan E., Rivera, Jose A., Jr, Farmer, Moses G.
Format:	Report
Sprache:	eng
Schlagworte:	Aircraft Design, Testing And Performance
Online-Zugang:	Volltext bestellen
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