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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 (2008) Automatic Transition Prediction for Three-Dimensional Aircraft Configurations using the DLR TAU Code. In: eingereicht zur Veröffentlichung (DOI: 1), pp. 101-108. Springer Verlag, Berlin-Heidelberg-New York. 16. DGLR-Fach-Symposium der STAB, [2008-11-03 - 2008-11-04], [Aachen, Germany]. ISBN ISBN: 978-3-642-14242-0

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Official URL: http://www.springer.com/materials/mechanics/book/978-3-642-14242-0

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/56025/
Document Type:Conference or Workshop Item (Speech, Paper)
Title:Automatic Transition Prediction for Three-Dimensional Aircraft Configurations using the DLR TAU Code
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Krumbein, AndreasUNSPECIFIEDUNSPECIFIED
Krimmelbein, NormannUNSPECIFIEDUNSPECIFIED
Schrauf, GézaAirbus, BremenUNSPECIFIED
Date:4 November 2008
Journal or Publication Title:eingereicht zur Veröffentlichung
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Page Range:pp. 101-108
Publisher:Springer Verlag, Berlin-Heidelberg-New York
Series Name:Notes on Numerical Fluid Mechanics and Multidisciplinary Design • Volume 112, New Results in Numerical and Experimental Fluid Mechanics ??
ISBN: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
Event Title:16. DGLR-Fach-Symposium der STAB
Event Location:[Aachen, Germany]
Event Type:national Conference
Event Dates:[2008-11-03 - 2008-11-04]
Organizer:RWTH Aachen, Lehrstuhl für Strömungslehre und Aerodynamisches Institut
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:27 Nov 2008
Last Modified:31 Jul 2019 19:23

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