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Dynamics of flow around vibrating wing NACA 0012
- 1.0384635 - ÚT 2013 RIV CZ eng C - Conference Paper (international conference)
Uruba, Václav
Dynamics of flow around vibrating wing NACA 0012.
Interaction and Feedbacks 2012. Prague: Institute of Thermomechanics AS CR, v. v. i., 2012 - (Zolotarev, I.), s. 117-124. ISBN 978-80-87012-43-7.
[Interaction and Feedbacks 2012 /19./. Praha (CZ), 27.11.2012-28.11.2012]
R&D Projects: GA ČR GA101/09/1522
Institutional research plan: CEZ:AV0Z20760514
Keywords : vibrating wing * boundary layer separation * PIV
Subject RIV: BK - Fluid Dynamics
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.
Permanent Link: http://hdl.handle.net/11104/0216242
Number of the records: 1