Krumbein, Andreas (2006) eN Transition Prediction for 3D Wing Configurations using Database Methods and a local, linear Stability Code. ONERA, Centre de Toulouse. 7th ONERA-DLR Aerospace Symposium - ODAS 2006, 2006-10-04 - 2006-10-07, Toulouse, Frankreich.
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Abstract
A Reynolds-averaged Navier-Stokes solver, a laminar boundary-layer code and different transition prediction methods for the prediction of Tollmien-Schlichting and cross flow instabilities were coupled in order to perform Reynolds-averaged Navier-Stokes computations of three-dimensional, finite wings with automatic laminar-turbulent transition prediction. The results from computations based on two database methods and a local, linear stability code together with the eN-method are compared for a three-dimensional wing configuration.
Item URL in elib: | https://elib.dlr.de/44954/ | ||||||||
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Document Type: | Conference or Workshop Item (Speech, Paper) | ||||||||
Title: | eN Transition Prediction for 3D Wing Configurations using Database Methods and a local, linear Stability Code | ||||||||
Authors: |
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Date: | 6 October 2006 | ||||||||
Refereed publication: | No | ||||||||
Open Access: | Yes | ||||||||
Gold Open Access: | No | ||||||||
In SCOPUS: | No | ||||||||
In ISI Web of Science: | No | ||||||||
Editors: |
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Publisher: | ONERA, Centre de Toulouse | ||||||||
Status: | Published | ||||||||
Keywords: | Transition prediction, RANS solver, eN-method, 3D wings | ||||||||
Event Title: | 7th ONERA-DLR Aerospace Symposium - ODAS 2006 | ||||||||
Event Location: | Toulouse, Frankreich | ||||||||
Event Type: | international Conference | ||||||||
Event Start Date: | 4 October 2006 | ||||||||
Event End Date: | 7 October 2006 | ||||||||
Organizer: | ONERA, Centre de Toulouse | ||||||||
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: | 30 Oct 2006 | ||||||||
Last Modified: | 24 Apr 2024 19:06 |
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