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Krumbein, Andreas and Krimmelbein, Normann and Schrauf, Géza (2010) Automatic Transition Prediction for Three-Dimensional Aircraft Configurations using the DLR TAU Code. In: New Results in Numerical and Experimental Fluid Mechanics VII Notes on Numerical Fluid Mechanics and Multidisciplinary Design, Vol. 112. Springer Verlag, Berlin Heidelberg. pp. 101-108. ISBN 978-3-642-14242-0. ISSN 1612-2909
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Official URL: http://www.springer.com
Abstract
A Reynolds-averaged Navier-Stokes solver, a laminar boundary-layer code and a fully automated local, linear stability code for the prediction of Tollmien-Schlichting and cross flow instabilities were coupled for the automatic prediction of laminar-turbulent transition on general aircraft configurations during the ongoing flow computation. The procedure is applied to different three-dimensional wing-body configurations and the sensitivity of the coupled system to a variety of coupling parameters is investigated.
| Item URL in elib: | https://elib.dlr.de/65674/ | ||||||||||||||
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| Document Type: | Contribution to a Collection | ||||||||||||||
| Title: | Automatic Transition Prediction for Three-Dimensional Aircraft Configurations using the DLR TAU Code | ||||||||||||||
| Authors: |
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| Date: | 2010 | ||||||||||||||
| Journal or Publication Title: | New Results in Numerical and Experimental Fluid Mechanics VII | ||||||||||||||
| Refereed publication: | Yes | ||||||||||||||
| Open Access: | Yes | ||||||||||||||
| Gold Open Access: | Yes | ||||||||||||||
| In SCOPUS: | No | ||||||||||||||
| In ISI Web of Science: | No | ||||||||||||||
| Volume: | Vol. 112 | ||||||||||||||
| DOI : | 10.1007/978-3-642-14243-7_13 | ||||||||||||||
| Page Range: | pp. 101-108 | ||||||||||||||
| Editors: |
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| Publisher: | Springer Verlag, Berlin Heidelberg | ||||||||||||||
| Series Name: | Notes on Numerical Fluid Mechanics and Multidisciplinary Design | ||||||||||||||
| ISSN: | 1612-2909 | ||||||||||||||
| ISBN: | 978-3-642-14242-0 | ||||||||||||||
| Status: | Published | ||||||||||||||
| Keywords: | automatic transition prediction, 3d, aircraft, transonic, sensitivities, eN method, linear stability theory, laminar boundary layers, RANS, TAU code, COCO, LILO | ||||||||||||||
| 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 - Concepts & Integration (old) | ||||||||||||||
| Location: | Braunschweig , Göttingen | ||||||||||||||
| Institutes and Institutions: | Institute of Aerodynamics and Flow Technology > C²A²S²E - Center for Computer Applications in AeroSpace Science and Engineering | ||||||||||||||
| Deposited By: | Micknaus, Ilka | ||||||||||||||
| Deposited On: | 14 Oct 2010 14:03 | ||||||||||||||
| Last Modified: | 27 Feb 2015 15:54 |
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