Dynamics of flow around vibrating wing NACA 0012

Result code in IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F61388998%3A_____%2F12%3A00384635" target="_blank" >RIV/61388998:_____/12:00384635 - isvavai.cz</a>

Result on the web

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DOI - Digital Object Identifier

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Result language

angličtina

Original language name

Dynamics of flow around vibrating wing NACA 0012

Original language description

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 ofthe 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.

Czech name

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Czech description

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Type

D - Article in proceedings

CEP classification

BK - Liquid mechanics

OECD FORD branch

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Project

<a href="/en/project/GA101%2F09%2F1522" target="_blank" >GA101/09/1522: Experimental investigation of unsteady flow patterns around vibrating airfoil with application in aeroelasticity</a><br>

Continuities

Z - Vyzkumny zamer (s odkazem do CEZ)

Publication year

2012

Confidentiality

S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Article name in the collection

Interaction and Feedbacks 2012

ISBN

978-80-87012-43-7

ISSN

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e-ISSN

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Number of pages

6

Pages from-to

117-124

Publisher name

Institute of Thermomechanics AS CR, v. v. i.

Place of publication

Prague

Event location

Praha

Event date

Nov 27, 2012

Type of event by nationality

EUR - Evropská akce

UT code for WoS article

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