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Automatic Transition Prediction for High-Lift Configurations using a Hybrid CFD Code

Krumbein, Andreas and Krimmelbein, Normann (2008) Automatic Transition Prediction for High-Lift Configurations using a Hybrid CFD Code. 46th AIAA Aerospace Sciences Meeting and Exhibit, 2008-01-07 - 2008-01-10, Reno, NV (USA).

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Item URL in elib:https://elib.dlr.de/52812/
Document Type:Conference or Workshop Item (Speech, Paper)
Title:Automatic Transition Prediction for High-Lift Configurations using a Hybrid CFD Code
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Krumbein, AndreasUNSPECIFIEDUNSPECIFIED
Krimmelbein, NormannTechnische Universität Braunschweig, Institut für StrömungsmechanikUNSPECIFIED
Date:9 January 2008
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Editors:
EditorsEmail
American Institute of Aeronautics and Astronautics, AIAAUNSPECIFIED
Status:Published
Keywords:transition, automatic transition prediction, Reynolds averaged Navier-Stokes, DLR TAU code, 3d aircraft, wing body, high lift, local linear stability code, laminar boundary layer code
Event Title:46th AIAA Aerospace Sciences Meeting and Exhibit
Event Location:Reno, NV (USA)
Event Type:international Conference
Event Dates:2008-01-07 - 2008-01-10
Organizer:AIAA
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:16 Jan 2008
Last Modified:12 Dec 2013 20:29

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