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The parallel mesh deformation of the DLR TAU-Code

Gerhold, Thomas and Neumann, Jens (2006) The parallel mesh deformation of the DLR TAU-Code. 15. DGLR-Fach-Symposium der STAB, 2006-11-29-2006-12-01, Darmstadt (Germany). (Submitted)

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Mesh deformation for unstructured grids is usually solved employing algorithms based on a spring analogy or on a linear elasticity analogy. These methods require solving discrete equations for the given grid using iterative methods. The computational effort for these methods is not negligible compared to the effort required by the flow solver. In order to optimise the efficiency of the computational chain for coupled simulations of fluid structure interaction an alternative algebraic method was developed for the DLR TAU-Code. The TAU-Code is parallelized by domain decomposition using the message passing concept based on MPI such that each process works on one partition of the grid only. In order to employ the grid deformation on the grid partitions distributed over the processes, a parallel method is required. This paper describes the parallel grid deformation method and shows its efficiency and robustness for the DLR F6 geometry. Further applications are shown in order to demonstrate the grid deformation for dynamic aeroelastic simulations.

Item URL in elib:https://elib.dlr.de/45362/
Document Type:Conference or Workshop Item (Speech, Paper)
Title:The parallel mesh deformation of the DLR TAU-Code
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Date:8 November 2006
Open Access:No
Gold Open Access:No
In ISI Web of Science:No
Keywords:CFD, aeroelastic simulations, hybrid meshes, mesh deformation
Event Title:15. DGLR-Fach-Symposium der STAB
Event Location:Darmstadt (Germany)
Event Type:national Conference
Event Dates:2006-11-29-2006-12-01
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:other
HGF - Program Themes:other
DLR - Research area:Aeronautics
DLR - Program:L - no assignment
DLR - Research theme (Project):L - no assignment (old)
Location: Köln-Porz , Braunschweig , Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology
Institute of Aeroelasticity
Institute of Aerodynamics and Flow Technology > CASE
Deposited By: Gerhold, Dr.-Ing. Thomas
Deposited On:05 Jan 2007
Last Modified:12 Dec 2013 20:21

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