Reference : Unsteady Navier-Stokes simulation of low-Reynolds stall flutter
Scientific congresses and symposiums : Paper published in a book
Engineering, computing & technology : Aerospace & aeronautics engineering
http://hdl.handle.net/2268/107555
Unsteady Navier-Stokes simulation of low-Reynolds stall flutter
English
Yabili, Sacha [Université de Liège - ULg > > > 1re an. master sc. écon., or. gén., à finalité]
Smith, Marilyn [Georgia Institute of Technology > Daniel Guggenheim School of Aerospace Engineering > > >]
Dimitriadis, Grigorios mailto [Université de Liège - ULg > Département d'aérospatiale et mécanique > Interactions Fluide-Structure - Aérodynamique expérimentale >]
Jan-2012
Proceedings of the 50th AIAA Aerospace Sciences Meeting
AIAA
AIAA-2012-0037
No
No
International
50th AIAA Aerospace Sciences Meeting
from 9-1-2012 to 12-1-2012
American Institute of Aeronautics and Astronautics
Nashville, Tennesses
United States of America
[en] CFD ; Stall Flutter ; Wind Tunnel
[en] A solver has been developed within the OpenFoam framework to compute large amplitude motion of two-dimensional rigid configurations. The results obtained with this code were successfully validated on rigid airfoils at static and dynamic conditions, as well as correlated with experimental data and numerical solutions from similar unsteady solvers. The results demonstrate that current computational methods are, within the constraints imposed by spatial grids, temporal integration and turbulence modeling, capable of capturing the self-sustained oscillations characterizing stall flutter event with reasonable accuracy, including the mechanisms of energy transfer.
Researchers ; Professionals
http://hdl.handle.net/2268/107555

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