Numerical simulations of nonlinear post-critical vibrations of an airfoil after flutter instability
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216208%3A11320%2F11%3A10103893" target="_blank" >RIV/00216208:11320/11:10103893 - 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
Numerical simulations of nonlinear post-critical vibrations of an airfoil after flutter instability
Original language description
The contribution deals with the numerical simulation of the flutter of an airfoil with three degrees of freedom. The finite element solution of 2D incompressible Navier-Stokes equations written in the ALE form is coupled with a system of nonlinear ordinary differential equations describing the airfoil vibrations.
Czech name
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Czech description
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Classification
Type
O - Miscellaneous
CEP classification
BI - Acoustics and oscillation
OECD FORD branch
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Result continuities
Project
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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