Jester-Zürker, Roland and Jakirlic, Suad and Eisfeld, Bernhard (2006) Near-Wall, Reynolds-Stress Model Calculations of Transonic Flow Configurations Relevant to Aircraft Aerodynamics. In: Proceedings of the Conference on Modelling Fluid Flow (CMFF'06), pp. 264-271. Conference on Modelling Fluid Flow (CMFF'06), 2006-09-06 - 2006-09-09, Budapest. ISBN 963 420 872 X.
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Abstract
The present work focuses on the application of a near-wall, wall-normal free, second-moment closure (SMC) model in the RANS (Reynolds-Averaged Navier-Stokes) framework in computing the (compressible) transonic flow past aircraft configurations and their elements (airfoils and wings). The flow geometries primarily considered in this work include the transonic RAE 2822 profiles (cases 9 and 10), the ONERA M6 wing and the ALVAST wing-body configuration. The SMC predictions show encouraging results with respect to the shock position and its structure and the strength of the wing-tip vortex.
Item URL in elib: | https://elib.dlr.de/45043/ | ||||||||||||||||
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Document Type: | Conference or Workshop Item (Paper) | ||||||||||||||||
Title: | Near-Wall, Reynolds-Stress Model Calculations of Transonic Flow Configurations Relevant to Aircraft Aerodynamics | ||||||||||||||||
Authors: |
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Date: | 2006 | ||||||||||||||||
Journal or Publication Title: | Proceedings of the Conference on Modelling Fluid Flow (CMFF'06) | ||||||||||||||||
Refereed publication: | Yes | ||||||||||||||||
Open Access: | No | ||||||||||||||||
Gold Open Access: | No | ||||||||||||||||
In SCOPUS: | No | ||||||||||||||||
In ISI Web of Science: | No | ||||||||||||||||
Page Range: | pp. 264-271 | ||||||||||||||||
Editors: |
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ISBN: | 963 420 872 X | ||||||||||||||||
Status: | Published | ||||||||||||||||
Keywords: | RANS, Reynolds-stress models, near-wall treatment, transonic flow configurations, aircraft aerodynamics | ||||||||||||||||
Event Title: | Conference on Modelling Fluid Flow (CMFF'06) | ||||||||||||||||
Event Location: | Budapest | ||||||||||||||||
Event Type: | international Conference | ||||||||||||||||
Event Start Date: | 6 September 2006 | ||||||||||||||||
Event End Date: | 9 September 2006 | ||||||||||||||||
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 | ||||||||||||||||
Institutes and Institutions: | Institute of Aerodynamics and Flow Technology > CASE | ||||||||||||||||
Deposited By: | Eisfeld, Dr.-Ing. Bernhard | ||||||||||||||||
Deposited On: | 08 Nov 2006 | ||||||||||||||||
Last Modified: | 24 Apr 2024 19:06 |
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