Numerical simulation of airfoil vibrations induced by turbulent flow
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216208%3A11320%2F15%3A10291259" target="_blank" >RIV/00216208:11320/15:10291259 - isvavai.cz</a>
Alternative codes found
RIV/61388998:_____/15:00437115 RIV/68407700:21220/15:00222869
Result on the web
<a href="http://dx.doi.org/10.4208/cicp.181213.230514a" target="_blank" >http://dx.doi.org/10.4208/cicp.181213.230514a</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.4208/cicp.181213.230514a" target="_blank" >10.4208/cicp.181213.230514a</a>
Alternative languages
Result language
angličtina
Original language name
Numerical simulation of airfoil vibrations induced by turbulent flow
Original language description
The subject of the paper is the numerical simulation of the interaction of two-dimensional incompressible viscous flow and a vibrating airfoil with large amplitudes. The airfoil with three degrees of freedom performs rotation around an elastic axis, oscillations in the vertical direction and rotation of a flap. The numerical simulation consists of the finite element solution of the Reynolds averaged Navier-Stokes equations combined with Spalart-Allmaras or $k-omega$ turbulence models, coupled with a system of nonlinear ordinary differential equations describing the airfoil motion with consideration of large amplitudes. The time-dependent computational domain and approximation on a moving grid are treated by the Arbitrary Lagrangian-Eulerian formulation of the flow equations. Due to large values of the involved Reynolds numbers an application of a suitable stabilization of the finite element discretization is employed. The developed method is used for the computation of flow-induced oscillations of the airfoil near the flutter instability, when the displacements of the airfoil are large, up to 40 degrees in rotation. The paper contains the comparison of the numerical results obtained by both turbulence models.
Czech name
—
Czech description
—
Classification
Type
J<sub>x</sub> - Unclassified - Peer-reviewed scientific article (Jimp, Jsc and Jost)
CEP classification
BA - General mathematics
OECD FORD branch
—
Result continuities
Project
Result was created during the realization of more than one project. More information in the Projects tab.
Continuities
I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace
Others
Publication year
2015
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Name of the periodical
Communications in Computational Physics
ISSN
1815-2406
e-ISSN
—
Volume of the periodical
17
Issue of the periodical within the volume
1
Country of publishing house
CN - CHINA
Number of pages
43
Pages from-to
146-188
UT code for WoS article
000353692300006
EID of the result in the Scopus database
2-s2.0-84925788899