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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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Item URL in elib:https://elib.dlr.de/47197/
Document Type:Other
Title:Navier-Stokes High-Lift Airfoil Computations with Automatic Transition Prediction using the DLR TAU Code
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Krumbein, AndreasUNSPECIFIEDUNSPECIFIED
Date:30 January 2007
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
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: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:20 Feb 2008
Last Modified:31 Jul 2019 19:18

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