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Hybrid RANS/LES of a generic high-lift aircraft configuration near maximum lift

Probst, Axel and Melber-Wilkending, Stefan (2021) Hybrid RANS/LES of a generic high-lift aircraft configuration near maximum lift. International Journal of Numerical Methods for Heat and Fluid Flow, pp. 1-18. Emerald Group Publishing Ltd.. doi: 10.1108/HFF-08-2021-0525. ISSN 0961-5539.

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Official URL: https://www.emerald.com/insight/content/doi/10.1108/HFF-08-2021-0525/full/html


The paper aims to assess the feasibility of locally turbulence-resolving flow simulations for a high-lift aircraft configuration near maximum lift. It addresses the aspects of proper grid design and explores the ability of the hybrid turbulence model and the numerical scheme to automatically select adequate modes in different flow regions. By comparison with experimental and numerical reference data, the study aims to provide insights into the predictive potential of the method for high-lift flows. Apart from demonstrating the general feasibility of the numerical approach for complex high-lift flows, the results indicate somewhat improved maximum lift predictions compared to the Spalart-Allmaras model, which is consistent with a slightly closer agreement with measured pressure distributions and oil-flow pictures. However, the expected lift breakdown caused by an increasing inboard separation in the experiment is not well captured.

Item URL in elib:https://elib.dlr.de/145007/
Document Type:Article
Title:Hybrid RANS/LES of a generic high-lift aircraft configuration near maximum lift
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Probst, AxelAxel.Probst (at) dlr.deUNSPECIFIED
Melber-Wilkending, StefanStefan.Melber (at) dlr.deUNSPECIFIED
Date:11 October 2021
Journal or Publication Title:International Journal of Numerical Methods for Heat and Fluid Flow
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In ISI Web of Science:Yes
DOI :10.1108/HFF-08-2021-0525
Page Range:pp. 1-18
EditorsEmailEditor's ORCID iD
Publisher:Emerald Group Publishing Ltd.
Keywords:Hybrid RANS/LES, High-lift aerodynamics, JAXA standard model, Maximum lift, Wall-modelled LES
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Efficient Vehicle
DLR - Research area:Aeronautics
DLR - Program:L EV - Efficient Vehicle
DLR - Research theme (Project):L - Digital Technologies
Location: Braunschweig , Göttingen
Institutes and Institutions:Institute for Aerodynamics and Flow Technology > CASE, GO
Institute for Aerodynamics and Flow Technology > Transport Aircraft
Deposited By: Probst, Axel
Deposited On:03 Nov 2021 13:26
Last Modified:22 Feb 2022 18:24

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