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Application of a Hybrid Navier-Stokes Solver with Automatic Transition Prediction

Krumbein, Andreas and Krimmelbein, Normann and Schrauf, Géza (2007) Application of a Hybrid Navier-Stokes Solver with Automatic Transition Prediction. American Institute of Aeronautics and Astronautics,. AIAA 25th Applied Aerodynamics Conference, [2007-06-25 - 2007-06-28], AIAA-2007-4284, Miami, Florida, U.S.A..

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Abstract

A hybrid Reynolds-averaged Navier-Stokes solver, a laminar boundary layer code and a fully automated local, linear stability code were coupled in order to predict the laminar-turbulent transition due to Tollmien-Schlichting and cross flow instabilities using the eN-method based on the two N factor approach. The coupled system was designed to be applied to three-dimensional aircraft configurations which are of industrial relevance. The application of the system to a two-dimensional two-element airfoil configuration and a three-dimensional generic full aircraft configuration is described and documented in this paper. The prediction of the laminar-turbulent transition lines was done in a fully automatic manner. It will be shown that complex aircraft configurations can be handled without a priori knowledge of the transition characteristics of the specific flow problem. The computational results are partially compared to experimental data.

Item URL in elib:https://elib.dlr.de/49276/
Document Type:Conference or Workshop Item (Speech, Paper)
Title:Application of a Hybrid Navier-Stokes Solver with Automatic Transition Prediction
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Krumbein, AndreasUNSPECIFIEDUNSPECIFIED
Krimmelbein, NormannTechnische Universität Braunschweig, Institut für StrömungsmechanikUNSPECIFIED
Schrauf, GézaAirbus, BremenUNSPECIFIED
Date:27 June 2007
Refereed publication:No
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Publisher:American Institute of Aeronautics and Astronautics,
Status:Published
Keywords:TAU code, RANS, transition prediction, en method, linear stability code LILO, 3d, full aircraft, multi-element
Event Title:AIAA 25th Applied Aerodynamics Conference
Event Location:Miami, Florida, U.S.A.
Event Type:international Conference
Event Dates:[2007-06-25 - 2007-06-28], AIAA-2007-4284
Organizer:American Institute of Aeronautics and Astronautics
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Rotorcraft (old)
DLR - Research area:Aeronautics
DLR - Program:L RR - Rotorcraft Research
DLR - Research theme (Project):L - The Virtual Aerodynamic Rotorcraft (old)
Location: Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > CASE
Deposited By: Krumbein, Dr.-Ing. Andreas
Deposited On:06 Jul 2007
Last Modified:31 Jul 2019 19:19

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