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Moens, Frédéric and Perraud, Jean and Krumbein, Andreas and Toulorge, Thomas and Iannelli, Pierluigi and Eliasson, Peter and Hanifi, Ardeshir (2008) Transition Prediction and Impact on a Three-Dimensional High-Lift-Wing Configuration. Journal of Aircraft, Vol. 4 (No. 5), [1751]-[1766]. American Institute of Aeronautics and Astronautics. doi: 10.2514/1.36238.
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Abstract
The evolution of maximum lift coefficient of a transport aircraft as a function of Reynolds number can be linked to modifications of the laminar-turbulent transition process. In the framework of European project EUROLIFT (I), a task was dedicated to the physical understanding and the numerical modeling of the transition process in high-lift configurations. Then, in the follow-on project EUROLIFT II, a major step is the integration of transition prediction tools within Reynolds-averaged Navier-Stokes (RANS) solvers in order to estimate the impact of transition on performance. This paper presents an overview of the different activities dealing with transition in the EUROLIFT II project.
| Item URL in elib: | https://elib.dlr.de/55391/ | ||||||||||||||||||||||||||||||||
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| Document Type: | Article | ||||||||||||||||||||||||||||||||
| Title: | Transition Prediction and Impact on a Three-Dimensional High-Lift-Wing Configuration | ||||||||||||||||||||||||||||||||
| Authors: |
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| Date: | September 2008 | ||||||||||||||||||||||||||||||||
| Journal or Publication Title: | Journal of Aircraft | ||||||||||||||||||||||||||||||||
| Open Access: | No | ||||||||||||||||||||||||||||||||
| Gold Open Access: | No | ||||||||||||||||||||||||||||||||
| In SCOPUS: | No | ||||||||||||||||||||||||||||||||
| In ISI Web of Science: | No | ||||||||||||||||||||||||||||||||
| Volume: | Vol. 4 | ||||||||||||||||||||||||||||||||
| DOI: | 10.2514/1.36238 | ||||||||||||||||||||||||||||||||
| Page Range: | [1751]-[1766] | ||||||||||||||||||||||||||||||||
| Publisher: | American Institute of Aeronautics and Astronautics | ||||||||||||||||||||||||||||||||
| Status: | Published | ||||||||||||||||||||||||||||||||
| Keywords: | transition prediction, RANS solvers, high-lift, 3d, realistic aircraft | ||||||||||||||||||||||||||||||||
| 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: | 02 Oct 2008 | ||||||||||||||||||||||||||||||||
| Last Modified: | 24 Apr 2024 19:19 |
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