Nonlinear aeroelastic simulations for aeroelastic system with three degrees of freedom

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F11%3A00186498" target="_blank" >RIV/68407700:21220/11:00186498 - 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
Nonlinear aeroelastic simulations for aeroelastic system with three degrees of freedom
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
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

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

Article name in the collection
Interaction of Dynamic Systems with Surroundings and Systems with Feedbacks
ISBN
978-80-87012-37-6
ISSN
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e-ISSN
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Number of pages
6
Pages from-to
45-50
Publisher name
Ústav termomechaniky AV ČR
Place of publication
Praha
Event location
Prague
Event date
Nov 29, 2011
Type of event by nationality
EUR - Evropská akce
UT code for WoS article
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