Reference : Influence of a static wing wake on the stall flutter behavior of a flexible wing
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Engineering, computing & technology : Aerospace & aeronautics engineering
Influence of a static wing wake on the stall flutter behavior of a flexible wing
Li, Jing [University of Loughborough > > > >]
Dimitriadis, Grigorios mailto [Université de Liège - ULg > Département d'aérospatiale et mécanique > Interactions Fluide-Structure - Aérodynamique expérimentale >]
Proceedings of the 13th International Conference on Wind Engineering, ICWE13
Multi-Science Publishing Co Ltd
Paper 053
13th International Conference on Wind Engineering
from 10-07-2011 to 15/07/2011
International Association for Wind Engineering (IAWE)
European Wind Energy Association (EWEA)
World Wind Energy Association (WWEA)
TU Delft
TU Eindhoven
The Netherlands
[en] Stall flutter ; Aeroelasticity ; Limit Cycle Oscillations
[en] The subject of this paper is the experimental study of the aeroelastic behavior of a wing undergoing stall flutter in the vicinity of second, static wing. While stall flutter has been the subject of several investigations, such work has almost always concentrated on isolated wings. Stall flutter is a phenomenon that is mostly encountered in rotating blades, such as wind turbine or helicopter blades. In such cases, the phenomenon is influenced by the wake of the preceding
blade. This paper presents a series of experiments carried out at the Goldstein Laboratory of the University of Manchester, concerning the phenomenon of stall flutter influenced by the proximity of a static wing. The work is an extension of the single wing stall flutter experiments
presented by Dimitriadis and Li (2009).
Researchers ; Professionals

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