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Computational Modelling of Transonic Aerodynamic Flows Using Near-Wall, Reynolds Stress Transport Models

Jakirlic, Suad and Eisfeld, Bernhard and Jester-Zürker, Roland and Tropea, Cameron and Kroll, Norbert (2009) Computational Modelling of Transonic Aerodynamic Flows Using Near-Wall, Reynolds Stress Transport Models. In: MEGADESIGN and MegaOpt - German Initiatives for Aerodynamic Simulation and Optimization in Aircraft Design Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 107. Springer. pp. 73-92. ISBN 978-3-642-04092-4. ISSN 1612-2909

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Abstract

The present work reports on the further development of the Hanjalic-Jakirlic (1998) near-wall, second-moment closure (SMC) model in the RANS (Reynolds-Averaged Navier-Stokes) framework, updated to account for a wall-normal free, non-linear version of the pressure-strain term model, its implementation into the DLR-FLOWer code and its validation in computing some (compressible) transonic flow configurations. Furthermore, the wall boundary condition is based on the asymptotic behaviour of the Taylor microscale lambda and its exact relationship to the dissipation rate epsilon in the immediate wall vicinity. In addition, the calculations were performed using the DLR-FLOWer's default Reynolds stress transport model (Eisfeld, 2006), representing a numerically robust combination of the Launder-Reece-Rodi (1975) model resolving the near-wall layer with the Speziale-Sarkar-Gatski (1991) model being employed in the outer region. The flow geometries considered in this work include the transonic RAE 2822 profiles (cases 9 and 10), the ONERA M6 wing and the DLR-ALVAST wing-body configuration. The model results are analysed and discussed in conjunction with available experimental databases and the results of two widely used eddy-viscosity-based models, the one-equation Spalart-Allmaras model (1994) and the two-equation k-omega model of Wilcox (1988). The SMC predictions show encouraging results with respect to the shock position, shock-affected flow structure and the strength of the wing-tip vortex.

Item URL in elib:https://elib.dlr.de/60674/
Document Type:Book Section
Title:Computational Modelling of Transonic Aerodynamic Flows Using Near-Wall, Reynolds Stress Transport Models
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Jakirlic, Suads.jakirlic (at) sla.tu-darmstadt.deUNSPECIFIED
Eisfeld, Bernhardbernhard.eisfeld (at) dlr.deUNSPECIFIED
Jester-Zürker, RolandTU DarmstadtUNSPECIFIED
Tropea, CameronTU DarmstadtUNSPECIFIED
Kroll, Norbertnorbert.kroll (at) dlr.deUNSPECIFIED
Date:2009
Journal or Publication Title:MEGADESIGN and MegaOpt - German Initiatives for Aerodynamic Simulation and Optimization in Aircraft Design
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Volume:107
Page Range:pp. 73-92
Editors:
EditorsEmail
Kroll, Norbertnorbert.kroll@dlr.de
Schwamborn, Dieterdieter.schwamborn@dlr.de
Becker, Klausklaus.becker@airbus.com
Rieger, Herbertherbert.rieger@eads.com
Thiele, Frankthiele@pi.tu-berlin.de
Publisher:Springer
Series Name:Notes on Numerical Fluid Mechanics and Multidisciplinary Design
ISSN:1612-2909
ISBN:978-3-642-04092-4
Status:Published
Keywords:Reynolds stress models, transonic flow
HGF - Research field:Aeronautics, Space and Transport (old)
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
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > CASE
Deposited By: Eisfeld, Dr.-Ing. Bernhard
Deposited On:12 Nov 2009 10:51
Last Modified:12 Nov 2009 10:51

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