Scalability of the parallel CFD simulations of flow past a fluttering airfoil in OpenFOAM

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F46747885%3A24220%2F15%3A%230003392" target="_blank" >RIV/46747885:24220/15:#0003392 - isvavai.cz</a>
Result on the web
<a href="http://www.epj-conferences.org/articles/epjconf/abs/2015/11/epjconf_efm2014_02080/epjconf_efm2014_02080.html" target="_blank" >http://www.epj-conferences.org/articles/epjconf/abs/2015/11/epjconf_efm2014_02080/epjconf_efm2014_02080.html</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.1051/epjconf/20159202080" target="_blank" >10.1051/epjconf/20159202080</a>

Result language
angličtina
Original language name
Scalability of the parallel CFD simulations of flow past a fluttering airfoil in OpenFOAM
Original language description
The paper is devoted to investigation of unsteady subsonic airflow past an elastically supported airfoil during onset of the flutter instability. Based on the geometry, boundary conditions and airfoil motion data identified from wind-tunnel measurements,a 3D CFD model has been set up in OpenFOAM. The model is based on incompressible Navier-Stokes equations. The turbulence is modelled by the Menter?s k-omega shear stress transport turbulence model. The computational mesh was generated in GridPro, a meshgenerator capable of producing highly orthogonal structured C-type meshes. The mesh totals 3.1 million elements. Parallel scalability was measured on a small shared-memory SGI Altix UV 100 supercomputer.
Czech name
—
Czech description
—

Project
<a href="/en/project/GA13-10527S" target="_blank" >GA13-10527S: Subsonic flutter analysis of elastically supported airfoils using interferometry and CFD</a><br>
Continuities
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Publication year
2015
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Similar results(10)