On mathematical modelling of gust response using the finite element method

Sváček, Petr, and Horáček, Jaromír. "On mathematical modelling of gust response using the finite element method." Applications of Mathematics 2013. Prague: Institute of Mathematics AS CR, 2013. 197-206. <http://eudml.org/doc/287787>.

@inProceedings{Sváček2013,
abstract = {In this paper the numerical approximation of aeroelastic response to sudden gust is presented. The fully coupled formulation of two dimensional incompressible viscous fluid flow over a flexibly supported structure is used. The flow is modelled with the system of Navier-Stokes equations written in Arbitrary Lagrangian-Eulerian form and coupled with system of ordinary differential equations describing the airfoil vibrations with two degrees of freedom. The Navier-Stokes equations are spatially discretized by the fully stabilized finite element method. The numerical results are shown.},
author = {Sváček, Petr, Horáček, Jaromír},
booktitle = {Applications of Mathematics 2013},
keywords = {aeroelastic; incompressible; viscous; fluid flow; fluid structure interaction; Navier-Stokes equations; arbitrary Lagrangian-Eulerian form},
location = {Prague},
pages = {197-206},
publisher = {Institute of Mathematics AS CR},
title = {On mathematical modelling of gust response using the finite element method},
url = {http://eudml.org/doc/287787},
year = {2013},
}

TY - CLSWK
AU - Sváček, Petr
AU - Horáček, Jaromír
TI - On mathematical modelling of gust response using the finite element method
T2 - Applications of Mathematics 2013
PY - 2013
CY - Prague
PB - Institute of Mathematics AS CR
SP - 197
EP - 206
AB - In this paper the numerical approximation of aeroelastic response to sudden gust is presented. The fully coupled formulation of two dimensional incompressible viscous fluid flow over a flexibly supported structure is used. The flow is modelled with the system of Navier-Stokes equations written in Arbitrary Lagrangian-Eulerian form and coupled with system of ordinary differential equations describing the airfoil vibrations with two degrees of freedom. The Navier-Stokes equations are spatially discretized by the fully stabilized finite element method. The numerical results are shown.
KW - aeroelastic; incompressible; viscous; fluid flow; fluid structure interaction; Navier-Stokes equations; arbitrary Lagrangian-Eulerian form
UR - http://eudml.org/doc/287787
ER -