On a finite element method application in aeroelasticity
- Programs and Algorithms of Numerical Mathematics, Publisher: Institute of Mathematics AS CR(Prague), page 235-239
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topSváček, Petr. "On a finite element method application in aeroelasticity." Programs and Algorithms of Numerical Mathematics. Prague: Institute of Mathematics AS CR, 2006. 235-239. <http://eudml.org/doc/271353>.
@inProceedings{Sváček2006,
abstract = {The subject of this paper is the numerical simulation of aeroelastic problems. The interaction of two-dimensional incompressible viscous flow and a vibrating airfoil is modelled. The solid airfoil, which can rotate around the elastic axis and oscillate in the vertical direction, is considered. The
numerical simulation consists of the finite element solution of the Navier-Stokes equations coupled with the system of ordinary differential equations describing the airfoil motion. The stabilization procedure is of GLS type. The developed numerical approximation is applied on an aeroelastic problem.},
author = {Sváček, Petr},
booktitle = {Programs and Algorithms of Numerical Mathematics},
location = {Prague},
pages = {235-239},
publisher = {Institute of Mathematics AS CR},
title = {On a finite element method application in aeroelasticity},
url = {http://eudml.org/doc/271353},
year = {2006},
}
TY - CLSWK
AU - Sváček, Petr
TI - On a finite element method application in aeroelasticity
T2 - Programs and Algorithms of Numerical Mathematics
PY - 2006
CY - Prague
PB - Institute of Mathematics AS CR
SP - 235
EP - 239
AB - The subject of this paper is the numerical simulation of aeroelastic problems. The interaction of two-dimensional incompressible viscous flow and a vibrating airfoil is modelled. The solid airfoil, which can rotate around the elastic axis and oscillate in the vertical direction, is considered. The
numerical simulation consists of the finite element solution of the Navier-Stokes equations coupled with the system of ordinary differential equations describing the airfoil motion. The stabilization procedure is of GLS type. The developed numerical approximation is applied on an aeroelastic problem.
UR - http://eudml.org/doc/271353
ER -
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