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Higher-order and adaptive Discontinuous Galerkin methods applied to turbulent delta wing flow

Hartmann, Ralf (2013) Higher-order and adaptive Discontinuous Galerkin methods applied to turbulent delta wing flow. In: New Results in Numerical and Experimental Fluid Mechanics VIII Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 121. Springer. pp. 497-505. ISBN 978-3-642-35679-7. ISSN 1612-2909

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Official URL: http://link.springer.com/chapter/10.1007%2F978-3-642-35680-3_59#

Abstract

Discontinuous Galerkin methods allow higher-order flow solutions on unstructured or locally refined meshes by increasing the polynomial degree and using curved instead of straight-sided elements. Residual-based adaptation targets at resolving all flow features. In this article, higher-order discontinuous Galerkin methods are combined with residual-based adaptation and applied to a fully turbulent subsonic flow around the second Vortex Flow Experiment (VFE-2) configuration.

Item URL in elib:https://elib.dlr.de/82628/
Document Type:Contribution to a Collection
Title:Higher-order and adaptive Discontinuous Galerkin methods applied to turbulent delta wing flow
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Hartmann, RalfRalf.Hartmann (at) dlr.deUNSPECIFIED
Date:2013
Journal or Publication Title:New Results in Numerical and Experimental Fluid Mechanics VIII
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Volume:121
Page Range:pp. 497-505
Editors:
EditorsEmail
Dillmann, AndreasUNSPECIFIED
Heller, GerdAirbus Deutschland, Bremen
Kreplin, Hans-PeterUNSPECIFIED
Nitsche, WolfgangTU Berlin, Germany
Peltzer, InkenBeechcraft Berlin aviation GmbH, Schönefeld, Germany
Publisher:Springer
Series Name:Notes on Numerical Fluid Mechanics and Multidisciplinary Design
ISSN:1612-2909
ISBN:978-3-642-35679-7
Status:Published
Keywords:Discontinuous Galerkin methods, residual-based adaptation, Vortex Flow Experiment
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 - Simulation & Validation (old)
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 Jun 2013 11:02
Last Modified:27 Feb 2015 11:43

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