Drag and Flutter Characteristics of Loop Membranes

We present the results of experimental investigations on the aerodynamic characteristics of high-drag devices with flexible membranes joined at their short ends (loops). The loops were placed in a low-speed wind tunnel and tested at speeds up to 19 m/s. The range of Reynolds numbers was Re = 2 x 10....

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Veröffentlicht in:Journal of aircraft 2007-01, Vol.44 (1), p.317-322
Hauptverfasser: Carruthers, Anna C, Filippone, Antonio
Format: Artikel
Sprache:eng
Schlagworte:
Online-Zugang:Volltext
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
Beschreibung
Zusammenfassung:We present the results of experimental investigations on the aerodynamic characteristics of high-drag devices with flexible membranes joined at their short ends (loops). The loops were placed in a low-speed wind tunnel and tested at speeds up to 19 m/s. The range of Reynolds numbers was Re = 2 x 10... x 10... The loops were tested for a variety of aspect ratios, from 3.3 to 30, three planform areas, and two mounting methods. Results are presented for the drag coefficient and for the flutter characteristics. We prove that with a low aspect ratio the loops form a teardrop shape and their flutter mode is a sinusoidal-like oscillation. Furthermore, the drag coefficient decreases with the increasing wind speed, but it depends strongly on the aspect ratio and the planform area. Empirical correlations for the drag coefficient are polynomial equations. (ProQuest Information and Learning: ... denotes formulae/symbols omitted.)
ISSN:0021-8669
1533-3868
DOI:10.2514/1.23679