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Krumbein, Andreas and Krimmelbein, Normann and Schrauf, Géza (2008) Automatic Transition Prediction for Three-Dimensional Aircraft Configurations using the DLR TAU Code. In: eingereicht zur Veröffentlichung (DOI: 1), pp. 101-108. Springer Verlag, Berlin-Heidelberg-New York. 16. DGLR-Fach-Symposium der STAB, 2008-11-03 - 2008-11-04, [Aachen, Germany]. ISBN ISBN: 978-3-642-14242-0.
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Official URL: http://www.springer.com/materials/mechanics/book/978-3-642-14242-0
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/56025/ | ||||||||||||||||
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| Document Type: | Conference or Workshop Item (Speech, Paper) | ||||||||||||||||
| Title: | Automatic Transition Prediction for Three-Dimensional Aircraft Configurations using the DLR TAU Code | ||||||||||||||||
| Authors: |
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| Date: | 4 November 2008 | ||||||||||||||||
| Journal or Publication Title: | eingereicht zur Veröffentlichung | ||||||||||||||||
| Refereed publication: | Yes | ||||||||||||||||
| Open Access: | Yes | ||||||||||||||||
| Gold Open Access: | No | ||||||||||||||||
| In SCOPUS: | No | ||||||||||||||||
| In ISI Web of Science: | No | ||||||||||||||||
| Page Range: | pp. 101-108 | ||||||||||||||||
| Publisher: | Springer Verlag, Berlin-Heidelberg-New York | ||||||||||||||||
| Series Name: | Notes on Numerical Fluid Mechanics and Multidisciplinary Design • Volume 112, New Results in Numerical and Experimental Fluid Mechanics ?? | ||||||||||||||||
| ISBN: | 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 | ||||||||||||||||
| Event Title: | 16. DGLR-Fach-Symposium der STAB | ||||||||||||||||
| Event Location: | [Aachen, Germany] | ||||||||||||||||
| Event Type: | national Conference | ||||||||||||||||
| Event Start Date: | 3 November 2008 | ||||||||||||||||
| Event End Date: | 4 November 2008 | ||||||||||||||||
| Organizer: | RWTH Aachen, Lehrstuhl für Strömungslehre und Aerodynamisches Institut | ||||||||||||||||
| 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: | Göttingen | ||||||||||||||||
| Institutes and Institutions: | Institute of Aerodynamics and Flow Technology > CASE | ||||||||||||||||
| Deposited By: | Krumbein, Dr.-Ing. Andreas | ||||||||||||||||
| Deposited On: | 27 Nov 2008 | ||||||||||||||||
| Last Modified: | 24 Apr 2024 19:20 |
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