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eN Transition Prediction for 3D Wing Configurations using Database Methods and a local, linear Stability Code

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/
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:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Krumbein, AndreasUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Date:6 October 2006
Refereed publication:No
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Editors:
EditorsEmailEditor's ORCID iDORCID Put Code
CD-ROM Proceedings, UNSPECIFIEDUNSPECIFIEDUNSPECIFIED
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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