Langer, Stefan (2013) Point and Line Implicit Methods to Improve the Efficiency and Robustness of the DLR Tau Code. In: New Results in Numerical and Experimental Fluid Mechanics VIII Notes on Numerical Fluid Mechanics and Multidisciplinary Design, Vol. 121. Springer Verlag. pp. 419-428. doi: 10.1007/978-3-642-35680-3_50. ISBN 978-3-642-35679-7. ISSN 1612-2909.
Full text not available from this repository.
Abstract
We present a line implicit preconditioned multistage Runge-Katta method to significantly improve the convergence rate for approximating steady state solutions of high Reynolds number viscous flows. The Runge-Katta method is used as a smoother in the context of an agglomarated multigrid method for unstructured grids. A simplification of a first order approximation to the Jacobian of the residual function is used as a preconditioner. Predetermined lines identifying mesh regions of high cell stretching are exploited to extract the relevant parts of the Jacobian matrix. The lines are identified using an efficient algorithm based on a weighted graph. This has the advantage that high aspect ratio cells are determined everywhere in the mesh, for example also in the wake of a wing.
| Item URL in elib: | https://elib.dlr.de/82860/ | ||||||||||||||||||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| Document Type: | Contribution to a Collection | ||||||||||||||||||||||||
| Title: | Point and Line Implicit Methods to Improve the Efficiency and Robustness of the DLR Tau Code | ||||||||||||||||||||||||
| Authors: |
| ||||||||||||||||||||||||
| Date: | 2013 | ||||||||||||||||||||||||
| Journal or Publication Title: | New Results in Numerical and Experimental Fluid Mechanics VIII | ||||||||||||||||||||||||
| Refereed publication: | Yes | ||||||||||||||||||||||||
| Open Access: | No | ||||||||||||||||||||||||
| Gold Open Access: | No | ||||||||||||||||||||||||
| In SCOPUS: | No | ||||||||||||||||||||||||
| In ISI Web of Science: | No | ||||||||||||||||||||||||
| Volume: | Vol. 121 | ||||||||||||||||||||||||
| DOI: | 10.1007/978-3-642-35680-3_50 | ||||||||||||||||||||||||
| Page Range: | pp. 419-428 | ||||||||||||||||||||||||
| Editors: |
| ||||||||||||||||||||||||
| Publisher: | Springer Verlag | ||||||||||||||||||||||||
| Series Name: | Notes on Numerical Fluid Mechanics and Multidisciplinary Design | ||||||||||||||||||||||||
| ISSN: | 1612-2909 | ||||||||||||||||||||||||
| ISBN: | 978-3-642-35679-7 | ||||||||||||||||||||||||
| Status: | Published | ||||||||||||||||||||||||
| Keywords: | Flow solver, point implicit, line implicit, agglomerated multigrid | ||||||||||||||||||||||||
| HGF - Research field: | Aeronautics, Space and Transport | ||||||||||||||||||||||||
| HGF - Program: | Aeronautics | ||||||||||||||||||||||||
| HGF - Program Themes: | Aircraft Research (old) | ||||||||||||||||||||||||
| DLR - Research area: | Aeronautics | ||||||||||||||||||||||||
| DLR - Program: | L AR - Aircraft Research | ||||||||||||||||||||||||
| DLR - Research theme (Project): | L - Simulation & Validation (old) | ||||||||||||||||||||||||
| Location: | Braunschweig | ||||||||||||||||||||||||
| Institutes and Institutions: | Institute of Aerodynamics and Flow Technology > C²A²S²E - Center for Computer Applications in AeroSpace Science and Engineering | ||||||||||||||||||||||||
| Deposited By: | Seyfried, Beate | ||||||||||||||||||||||||
| Deposited On: | 08 Jul 2013 09:52 | ||||||||||||||||||||||||
| Last Modified: | 05 Nov 2024 08:51 |
Repository Staff Only: item control page