On Numerical Approximation of Airfoil Vibrations after Loosing of Aeroelastic Stability

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F11%3A00183352" target="_blank" >RIV/68407700:21220/11:00183352 - isvavai.cz</a>
Result on the web
<a href="http://dx.doi.org/10.1063/1.3636679" target="_blank" >http://dx.doi.org/10.1063/1.3636679</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.1063/1.3636679" target="_blank" >10.1063/1.3636679</a>

Result language
angličtina
Original language name
On Numerical Approximation of Airfoil Vibrations after Loosing of Aeroelastic Stability
Original language description
This paper describes the numerical approximation of flow around flexibly supported NACA 0012 airfoil with rotating aileron. The motion of the airfoil is described with the aid of system of ordinary differential equations (ODE) for three degrees of freedom coupled with the Navier-Stokes system of equations. The flow problem is approximated with the aid of stabilized finite element method and strongly coupled with solution of the system of ODEs. Numerical results are presented.
Czech name
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Czech description
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Project
<a href="/en/project/GAP101%2F11%2F0207" target="_blank" >GAP101/11/0207: Coupled problems of fluid and solid mechanics - nonlinear aeroelasticity</a><br>
Continuities
Z - Vyzkumny zamer (s odkazem do CEZ)

Publication year
2011
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Article name in the collection
ICNAAM-2011 Proceedings of the International Conference on Numerical Analysis and Applied Mathematics 2011
ISBN
978-0-7354-0954-5
ISSN
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e-ISSN
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Number of pages
4
Pages from-to
98-101
Publisher name
American Institute of Physics
Place of publication
Melville, New York
Event location
Halkidiki
Event date
Sep 19, 2011
Type of event by nationality
WRD - Celosvětová akce
UT code for WoS article
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