On approximation of an aeroelastic problem with consideration of nonlinear effects
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F11%3A00186575" target="_blank" >RIV/68407700:21220/11:00186575 - isvavai.cz</a>
Result on the web
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DOI - Digital Object Identifier
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Alternative languages
Result language
angličtina
Original language name
On approximation of an aeroelastic problem with consideration of nonlinear effects
Original language description
In this paper the numerical results of finite element approximations of two-dimensional 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 for three degrees of freedom coupled with the Navier-Stokes system of equations. The flow problem is approximated with the aid of stavilized finite element method and strongly coupled with time discretized solution of the system of ODEs. Numerical results are presented.
Czech name
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Czech description
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Classification
Type
D - Article in proceedings
CEP classification
BK - Liquid mechanics
OECD FORD branch
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Result continuities
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)
Others
Publication year
2011
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Article name in the collection
IC-EpsMsO 4th International Conference on Experiments/Process/System/Modelling/Simulation/Optimization
ISBN
978-960-98941-8-0
ISSN
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e-ISSN
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Number of pages
6
Pages from-to
453-458
Publisher name
Laboratory of Fluid Mechanics and Energy, University of Patras
Place of publication
Patras
Event location
Athens
Event date
Jul 6, 2011
Type of event by nationality
WRD - Celosvětová akce
UT code for WoS article
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