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Curved grid generation and DG computation for the DLR-F11 high lift configuration

Hartmann, Ralf and Harlan, McMorris (2016) Curved grid generation and DG computation for the DLR-F11 high lift configuration. In: ECCOMAS Congress 2016 on Computational Methods in Applied Sciences and Engineering, 2, pp. 2843-2858. National Technical University of Athens (NTUA) Greece. ECCOMAS Congress 2016, 5–10 June 2016, Crete Island, Greece.

Full text not available from this repository.

Official URL: https://www.eccomas2016.org/

Abstract

The DLR-F11 high lift configuration previously considered at the 2nd AIAA High Lift Prediction workshop (HiLiftPW-2) consists of a wing-body configuration with a three-element high lift system including slat tracks and flap track fairings. This test case has been selected a ``computational/meshing challenge'' in the 4th International Workshop on High-Order CFD Methods due to its geometrical and computational complexity. In this article, we demonstrate the applicability of current grid generation technology (CENTAUR) to generate a quadratic curved mesh for this configuration. Furthermore, we employ a high-order Discontinuous Galerkin discretization for the Reynolds-averaged Navier-Stokes (RANS) equations with the Wilcox-kω turbulence model which is sufficiently stable to be applicable to this test case. Finally, a 3rd-order Discontinuous Galerkin (DG) flow solution is computed on the quadratic (3rd-order) computational mesh. The numerical results are compared to experimental data as well as to computational results published in the HiLiftPW-2.

Item URL in elib:https://elib.dlr.de/109320/
Document Type:Conference or Workshop Item (Speech)
Additional Information:ECCOMAS Congress 2016 Proceedings Band 2, Seiten 2843 - 2858
Title:Curved grid generation and DG computation for the DLR-F11 high lift configuration
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Hartmann, Ralfralf.hartmann (at) dlr.dehttps://orcid.org/0000-0002-0403-1221
Harlan, McMorrisharlan (at) centaursoft.comUNSPECIFIED
Date:June 2016
Journal or Publication Title:ECCOMAS Congress 2016 on Computational Methods in Applied Sciences and Engineering
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Volume:2
Page Range:pp. 2843-2858
Editors:
EditorsEmail
Papadrakakis, M.UNSPECIFIED
Papadopoulos, V.UNSPECIFIED
Stefanou, G.UNSPECIFIED
Plevris, V.UNSPECIFIED
Publisher:National Technical University of Athens (NTUA) Greece
Status:Published
Keywords:High-order grid generation, high-order Discontinuous Galerkin method, compressible flows, high lift configuration
Event Title:ECCOMAS Congress 2016
Event Location:Crete Island, Greece
Event Type:international Conference
Event Dates:5–10 June 2016
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:fixed-wing aircraft
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Simulation and Validation
Location: Braunschweig
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > C²A²S²E - Center for Computer Applications in AeroSpace Science and Engineering
Deposited By: Hartmann, Dr.rer.nat. Ralf
Deposited On:12 Dec 2016 09:54
Last Modified:19 Dec 2016 15:29

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