Numerical Approximation of Flow Induced Airfoil Vibrations

Result code in IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F06%3A00120360" target="_blank" >RIV/68407700:21220/06:00120360 - 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

Numerical Approximation of Flow Induced Airfoil Vibrations

Original language description

In this paper we are interested in the interaction of two dimensional incompressible viscous laminar flow and a solid airfoil. The airfoil can rotate and oscillate in vertical direction. In order to take the grid motion into account the Arbitrary Lagrangian-Eulerian formulation of the Navier-Stokes system of equation is used. We discuss the GLS stabilization of the FEM, evaluation of forces acting on the profile, time discretization and the solution of the discrete problem. The obtained results are compared with available data.

Czech name

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Czech description

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Type

D - Article in proceedings

CEP classification

BA - General mathematics

OECD FORD branch

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Project

<a href="/en/project/GP201%2F05%2FP142" target="_blank" >GP201/05/P142: Numerical solution of aeroelastic problems with higher order finite element methods</a><br>

Continuities

Z - Vyzkumny zamer (s odkazem do CEZ)

Publication year

2006

Confidentiality

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

Article name in the collection

BAIL 2006, Proceedings

ISBN

3-00-019600-5

ISSN

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e-ISSN

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Number of pages

9

Pages from-to

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Publisher name

Georg August Universität Gőttingen

Place of publication

Göttingen

Event location

Göttingen

Event date

Jul 24, 2006

Type of event by nationality

WRD - Celosvětová akce

UT code for WoS article

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