Interaction of compressible flow with an airfoil

Česenek, Jan, and Feistauer, Miloslav. "Interaction of compressible flow with an airfoil." Programs and Algorithms of Numerical Mathematics. Prague: Institute of Mathematics AS CR, 2010. 35-41. <http://eudml.org/doc/271279>.

@inProceedings{Česenek2010,
abstract = {The paper is concerned with the numerical solution of interaction of compressible flow and a vibrating airfoil with two degrees of freedom, which can rotate around an elastic axis and oscillate in the vertical direction. Compressible flow is described by the Navier-Stokes equations written in the ALE form. This system is discretized by the semi-implicit discontinuous Galerkin finite element method (DGFEM) and coupled with the solution of ordinary differential equations describing the airfoil motion. Computational results showing the flow induced airfoil vibrations are presented.},
author = {Česenek, Jan, Feistauer, Miloslav},
booktitle = {Programs and Algorithms of Numerical Mathematics},
keywords = {compressible flow; discontinuous Galerkin method; aeroelasticity},
location = {Prague},
pages = {35-41},
publisher = {Institute of Mathematics AS CR},
title = {Interaction of compressible flow with an airfoil},
url = {http://eudml.org/doc/271279},
year = {2010},
}

TY - CLSWK
AU - Česenek, Jan
AU - Feistauer, Miloslav
TI - Interaction of compressible flow with an airfoil
T2 - Programs and Algorithms of Numerical Mathematics
PY - 2010
CY - Prague
PB - Institute of Mathematics AS CR
SP - 35
EP - 41
AB - The paper is concerned with the numerical solution of interaction of compressible flow and a vibrating airfoil with two degrees of freedom, which can rotate around an elastic axis and oscillate in the vertical direction. Compressible flow is described by the Navier-Stokes equations written in the ALE form. This system is discretized by the semi-implicit discontinuous Galerkin finite element method (DGFEM) and coupled with the solution of ordinary differential equations describing the airfoil motion. Computational results showing the flow induced airfoil vibrations are presented.
KW - compressible flow; discontinuous Galerkin method; aeroelasticity
UR - http://eudml.org/doc/271279
ER -