Krumbein, Andreas and Krimmelbein, Normann (2007) Navier-Stokes High-Lift Airfoil Computations with Automatic Transition Prediction using the DLR TAU Code. Notes on Numerical Fluid Mechanics and Multidisciplinary Design • Volume 96, New Results in Numerical and Experimental Fluid Mechanics VI, Seiten 210-218. Springer Verlag, Berlin-Heidelberg-New York. ISBN 3-540-74458-4.
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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 for the automatic prediction of laminar-turbulent transition on general 3-dimensional aircraft configurations during the ongoing computation of the flow. The prediction procedure is applied to a two-dimensional three-element high-lift airfoil configuration which is characterized by the existence of laminar separation bubbles using different operation modes of the procedure.
Item URL in elib: | https://elib.dlr.de/46002/ | ||||||||||||||||||||||||
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Document Type: | Editorship of Proceedings | ||||||||||||||||||||||||
Title: | Navier-Stokes High-Lift Airfoil Computations with Automatic Transition Prediction using the DLR TAU Code | ||||||||||||||||||||||||
Authors: |
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Date: | December 2007 | ||||||||||||||||||||||||
Refereed publication: | Yes | ||||||||||||||||||||||||
Open Access: | Yes | ||||||||||||||||||||||||
Gold Open Access: | No | ||||||||||||||||||||||||
In SCOPUS: | No | ||||||||||||||||||||||||
In ISI Web of Science: | No | ||||||||||||||||||||||||
Number of Pages: | 472 | ||||||||||||||||||||||||
Editors: |
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Publisher: | Springer Verlag, Berlin-Heidelberg-New York | ||||||||||||||||||||||||
Series Name: | Notes on Numerical Fluid Mechanics and Multidisciplinary Design • Volume 96, New Results in Numerical and Experimental Fluid Mechanics VI, Seiten 210-218 | ||||||||||||||||||||||||
ISBN: | 3-540-74458-4 | ||||||||||||||||||||||||
Status: | Published | ||||||||||||||||||||||||
Keywords: | RANS, Transition Prediction, automatic, TAU Code, eN Method, laminar separation bubble | ||||||||||||||||||||||||
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: | 20 Feb 2008 | ||||||||||||||||||||||||
Last Modified: | 24 Apr 2024 19:08 |
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