Abstract The application of active circulation control gives rise to a substantial increase in lift compared to conventional wings. Initial studies of the aeroelastic behaviour of a circulation-controlled wing have shown additional instabilities due to the active circulation control. Besides the heave flutter phenomenon, further investigation also reveals a destabilising effect of the aerodynamic derivatives related to pitch, which is peculiar to circulation-controlled wings. The goal of the present paper is to investigate these phenomena in detail.
Flutter of circulation-controlled wings
CEAS Aeronautical Journal ; 6 , 4 ; 589-598
2015-09-20
10 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Flutter of circulation-controlled wings
Online Contents | 2015
|Flutter of circulation control wings
AIAA | 1988
|Flutter of circulation control wings
AIAA | 1989
|The flutter of aeroplane wings
SLUB | 1929
|The flutter of aeroplane wings
Engineering Index Backfile | 1929
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