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Navier-Stokes High-Lift Airfoil Computations with Automatic Transition Prediction using the DLR TAU Code
Krumbein, Andreas (2007) Navier-Stokes High-Lift Airfoil Computations with Automatic Transition Prediction using the DLR TAU Code. Presentation at the Final Meeting of the DLR/ONERA Common Research Project MIRACLE. [Other]
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| Document Type: | Other | ||||
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| Title: | Navier-Stokes High-Lift Airfoil Computations with Automatic Transition Prediction using the DLR TAU Code | ||||
| Authors: |
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| Date: | 30 January 2007 | ||||
| Publisher: | Presentation at the Final Meeting of the DLR/ONERA Common Research Project MIRACLE | ||||
| Series Name: | ONERA-Châtillon, Paris, Frankreich; 30. Januar 2007 | ||||
| Status: | Published | ||||
| Keywords: | laminar-turbulent transition, eN method, RANS solver, TAU code, MIRACLE project high lift, 2d A310 take-off | ||||
| HGF - Research field: | Aeronautics, Space and Transport | ||||
| HGF - Program: | Aeronautics | ||||
| HGF - Program Themes: | L AR - Aircraft Research | ||||
| DLR - Research area: | Aeronautics | ||||
| DLR - Program: | L AR - Aircraft Research | ||||
| DLR - Research theme (Project): | L - Concepts & Integration | ||||
| Location: | Göttingen | ||||
| Institutes and Institutions: | Institute of Aerodynamics and Flow Technology > CASE | ||||
| Deposited By: | Dr.-Ing. Andreas Krumbein | ||||
| Deposited On: | 20 Feb 2008 | ||||
| Last Modified: | 15 Jan 2010 00:17 |
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