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Lax-Wendroff and Cell-Vertex Upwind Discretizations

Rossow, Cord-Christian (2013) Lax-Wendroff and Cell-Vertex Upwind Discretizations. In: New Results in Numerical and Experimental Fluid Mechanics VIII Notes on Numerical Fluid Mechanics and Multidisciplinary Design, Vol. 121. Springer Verlag. pp. 377-386. ISBN 978-3-642-35679-7. ISSN 1612-2909.

Full text not available from this repository.

Abstract

For Cell-Vertex Finite Volume methods, upwinding may be establisehd by Cell Vertex Upwind or Residual Distribution schemes. Interpreted as a Residual Distribution Scheme, the classical Lax-Wendroff method is augmented by accounting for all eigenvalues, and to improve shock capturing it is blended with a Cell Vertex Upwind method. For inviscid, subsonic flow superconvergence is shown, and for viscious flows accuray close to second order or higher is achieved

Item URL in elib:https://elib.dlr.de/82802/
Document Type:Contribution to a Collection
Title:Lax-Wendroff and Cell-Vertex Upwind Discretizations
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Rossow, Cord-ChristianUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
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:Vol. 121
Page Range:pp. 377-386
Editors:
EditorsEmailEditor's ORCID iDORCID Put Code
Dillmann, AndreasUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Heller, GerdAirbus Deutschland, BremenUNSPECIFIEDUNSPECIFIED
Kreplin, Hans-PeterUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Nitsche, WolfgangTU Berlin, GermanyUNSPECIFIEDUNSPECIFIED
Peltzer, InkenBeechcraft Berlin aviation GmbH, Schönefeld, GermanyUNSPECIFIEDUNSPECIFIED
Publisher:Springer Verlag
Series Name:Notes on Numerical Fluid Mechanics and Multidisciplinary Design
ISSN:1612-2909
ISBN:978-3-642-35679-7
Status:Published
Keywords:Cell-Vertex, upwind, Lax-Wendroff
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 > Leitungsbereich AS BS
Deposited By: Seyfried, Beate
Deposited On:08 Jul 2013 09:56
Last Modified:27 Feb 2015 11:59

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