Dynamics of flow around vibrating wing NACA 0012

Number of the records: 1

1.

SYSNO ASEP	0384635
Document Type	C - Proceedings Paper (int. conf.)
R&D Document Type	Conference Paper
Title	Dynamics of flow around vibrating wing NACA 0012
Author(s)	Uruba, Václav (UT-L)_{RID, ORCID}
Source Title	Interaction and Feedbacks 2012. - Prague : Institute of Thermomechanics AS CR, v. v. i., 2012 / Zolotarev I. - ISBN 978-80-87012-43-7
Pages	s. 117-124
Number of pages	6 s.
Publication form	Print - P
Action	Interaction and Feedbacks 2012 /19./
Event date	27.11.2012-28.11.2012
VEvent location	Praha
Country	CZ - Czech Republic
Event type	EUR
Language	eng - English
Country	CZ - Czech Republic
Keywords	vibrating wing ; boundary layer separation ; PIV
Subject RIV	BK - Fluid Dynamics
R&D Projects	GA101/09/1522 GA ČR - Czech Science Foundation (CSF)
CEZ	AV0Z20760514 - UT-L (2005-2011)
Annotation	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.
Workplace	Institute of Thermomechanics
Contact	Marie Kajprová, kajprova@it.cas.cz, Tel.: 266 053 154 ; Jana Lahovská, jaja@it.cas.cz, Tel.: 266 053 823
Year of Publishing	2013

Number of the records: 1