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Automatic Transition Prediction for Three-Dimensional Aircraft Configurations using the DLR TAU Code

Krumbein, Andreas and Krimmelbein, Normann and Schrauf, Géza (2010) Automatic Transition Prediction for Three-Dimensional Aircraft Configurations using the DLR TAU Code. In: New Results in Numerical and Experimental Fluid Mechanics VII Notes on Numerical Fluid Mechanics and Multidisciplinary Design, Vol. 112. Springer Verlag, Berlin Heidelberg. pp. 101-108. ISBN 978-3-642-14242-0. ISSN 1612-2909

Full text not available from this repository.

Official URL: http://www.springer.com

Abstract

A Reynolds-averaged Navier-Stokes solver, a laminar boundary-layer code and a fully automated local, linear stability code for the prediction of Tollmien-Schlichting and cross flow instabilities were coupled for the automatic prediction of laminar-turbulent transition on general aircraft configurations during the ongoing flow computation. The procedure is applied to different three-dimensional wing-body configurations and the sensitivity of the coupled system to a variety of coupling parameters is investigated.

Item URL in elib:https://elib.dlr.de/65674/
Document Type:Contribution to a Collection
Title:Automatic Transition Prediction for Three-Dimensional Aircraft Configurations using the DLR TAU Code
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Krumbein, Andreasandreas.krumbein (at) dlr.deUNSPECIFIED
Krimmelbein, Normannnormann.krimmelbein (at) dlr.deUNSPECIFIED
Schrauf, GézaAirbus, BremenUNSPECIFIED
Date:2010
Journal or Publication Title:New Results in Numerical and Experimental Fluid Mechanics VII
Refereed publication:Yes
Open Access:Yes
Gold Open Access:Yes
In SCOPUS:No
In ISI Web of Science:No
Volume:Vol. 112
DOI :10.1007/978-3-642-14243-7_13
Page Range:pp. 101-108
Editors:
EditorsEmail
Dillmann, AndreasDLR
Heller, GerdAirbus Deutschland
Klaas, Michael RWTH Aachen
Kreplin, Hans-PeterDLR
Nitsche, WolfgangTU Berlin
Schröder, WolfgangRWTH Aachen
Publisher:Springer Verlag, Berlin Heidelberg
Series Name:Notes on Numerical Fluid Mechanics and Multidisciplinary Design
ISSN:1612-2909
ISBN:978-3-642-14242-0
Status:Published
Keywords:automatic transition prediction, 3d, aircraft, transonic, sensitivities, eN method, linear stability theory, laminar boundary layers, RANS, TAU code, COCO, LILO
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: Braunschweig , Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > C²A²S²E - Center for Computer Applications in AeroSpace Science and Engineering
Deposited By: Micknaus, Ilka
Deposited On:14 Oct 2010 14:03
Last Modified:27 Feb 2015 15:54

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