Reference : Implicit high-order geometrically conservative scheme for the solution of flow proble...
Scientific congresses and symposiums : Unpublished conference
Engineering, computing & technology : Aerospace & aeronautics engineering
Physical, chemical, mathematical & earth Sciences : Physics
Physical, chemical, mathematical & earth Sciences : Mathematics
http://hdl.handle.net/2268/20940
Implicit high-order geometrically conservative scheme for the solution of flow problems on moving unstructured grids
English
Lepot, Ingrid [ > > ]
Vigneron, Didier mailto [Université de Liège - ULg > Département d'aérospatiale et mécanique > LTAS - Aérodynamique >]
Essers, Jean-André mailto [Université de Liège - ULg > Département d'aérospatiale et mécanique > LTAS - Aérodynamique >]
Léonard, Olivier mailto [Université de Liège - ULg > Département d'aérospatiale et mécanique > Turbomachines et propulsion aérospatiale >]
Mar-2003
Pages 992-996
No
International
Second MIT Conference on Compurational Fluid and Solid Mechanics
June 17–20, 2003
Massachussets Instiute of Technology
Massachussets
USA
[en] finite volume solver ; inviscid compressible perfect gases ; rbitrary polyhedral cells
[en] This paper presents a finite volume solver for the computation of three-dimensional unsteady flows of inviscid compressible perfect gases on moving unstructured meshes. This solver, based on a cell-centered approach for arbitrary polyhedral cells, provides unconditional second-order space and time truncation error. A new way of satisfying the Discrete Geometric Conservation Law (DGCL) adapted to this scheme is proposed. Preliminary results are presented.
Researchers ; Professionals ; Students
http://hdl.handle.net/2268/20940
10.1016/B978-008044046-0.50242-6

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