Original title: Dynamics of flow around vibrating wing NACA 0012
Authors: 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: Flow around vibrating wing consisting of airfoil profile NACA 0012 has been studied experimentally using time resolved PIV technique. The unsteady velocity field close to the profile trailing edge is highly affected by the wing vibrations. The dynamic of the flow is analyzed using BOD technique of the flow-field for cases with and without vibrations. Comparison shows strong influence of the airfoil vibrations on the flow dynamics.
Keywords: boundary layer separation; PIV; vibrating wing
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/11104/0216242

Permalink: http://www.nusl.cz/ntk/nusl-135954


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