Original title: Aeroelastic experiments with the structural properties variation
Authors: Chládek, Štěpán ; Zolotarev, Igor ; Uruba, Václav
Document type: Papers
Conference/Event: Interaction and Feedbacks 2012 /19./, Praha (CZ), 2012-11-27 / 2012-11-28
Year: 2012
Language: eng
Abstract: The paper measurements on a model of the airfoil NACA0012. Usually there is a limit range of the flow velocity in the wind tunnel. The chosen wind tunnel is usually fixed, the only one possibility is to modify the structural properties of the experimental stand. There are presented two kinds of modifications, one is based on the geometry variation, the other one on the added mass approach. Both of them have been verified experimentally.
Keywords: aeroelasticity; flutter; wind tunnel tests
Project no.: CEZ:AV0Z20760514 (CEP), GA101/09/1522 (CEP)
Funding provider: GA ČR
Host item entry: Interaction and Feedbacks 2012, ISBN 978-80-87012-43-7

Institution: Institute of Thermomechanics AS ČR (web)
Document availability information: Fulltext is available at the institute of the Academy of Sciences.
Original record: http://hdl.handle.net/11104/0224210

Permalink: http://www.nusl.cz/ntk/nusl-156581


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Research > Institutes ASCR > Institute of Thermomechanics
Conference materials > Papers