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Low Mach Number Preconditioning for the DLR-TAU Code and Application to High-Lift Flows

Melber, S. and Heinrich, R. (2004) Low Mach Number Preconditioning for the DLR-TAU Code and Application to High-Lift Flows. In: New Results in Numerical and Experimental Fluid Mechanics IV, Vol. 87, pp. 390-397. Springer Verlag, Berlin Heidelberg, New York. 13th STAB/DGLR Symposium, München (de), 12.-14.11.2002. ISBN 3-540-20258-7.

Full text not available from this repository.

Abstract

This report presents first results for the application of the DLR TAU-code with respect to low Mach-number preconditioning for complex high-lift configurations. It comprises the numerical simulation of the viscous compressible flow around simple test cases and a transport aircraft high-lift configuration with engine.

Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=2004,
Title:Low Mach Number Preconditioning for the DLR-TAU Code and Application to High-Lift Flows
Authors:
AuthorsInstitution or Email of Authors
Melber, S.UNSPECIFIED
Heinrich, R.UNSPECIFIED
Date:2004
Journal or Publication Title:New Results in Numerical and Experimental Fluid Mechanics IV
Volume:Vol. 87
Page Range:pp. 390-397
Editors:
EditorsEmail
Breitsamter, C.UNSPECIFIED
Laschka, B.UNSPECIFIED
Heinemann, J.-H. Hilbig, R., UNSPECIFIED
Publisher:Springer Verlag, Berlin Heidelberg, New York
Series Name:Notes on Numerical Fluid Mechanics and Multidisciplinary Design
ISBN:3-540-20258-7
Status:Published
Keywords:CFD, viscous compressible flow, RANS, unstructured data concept, TAU, low Mach-number preconditioning, complex configurations, high lift, engine
Event Title:13th STAB/DGLR Symposium, München (de), 12.-14.11.2002
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:Aircraft Research
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Concepts & Integration
Location: Köln-Porz , Braunschweig , Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology
Deposited By: Claudia Grant
Deposited On:31 Jan 2006
Last Modified:14 Jan 2010 19:26

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