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Dissipation of upwind schemes at high wave numbers

Hannemann, Volker and Siegmund, Alexander and Oßwald, Kai and Birken, Philipp and Weinman, Keith and Meister, Andreas (2012) Dissipation of upwind schemes at high wave numbers. International Conference on Computational Fluid Dynamics, ICCFD7, 09.-13. Jul. 2012, Hawaii, USA.

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Official URL: http://www.iccfd.org/iccfd7/proceedings.html

Abstract

A modification of the Roe scheme aimed at low Mach number flows is discussed. It improves the dissipation of kinetic energy at the highest resolved wave numbers in a low Mach number test case of decaying isotropic turbulence. No conflict is observed between the reduced dissipation and the accuracy or stability of the scheme in any of the investigated test cases ranging from low Mach number potential flow to hypersonic viscous flow around a cylinder.

Item URL in elib:https://elib.dlr.de/76675/
Document Type:Conference or Workshop Item (Speech, Paper)
Title:Dissipation of upwind schemes at high wave numbers
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Hannemann, VolkerUNSPECIFIEDUNSPECIFIED
Siegmund, AlexanderUniversität KassselUNSPECIFIED
Oßwald, KaiUNSPECIFIEDUNSPECIFIED
Birken, PhilippUniversität KassselUNSPECIFIED
Weinman, KeithUNSPECIFIEDUNSPECIFIED
Meister, AndreasUniversität KassselUNSPECIFIED
Date:2012
Refereed publication:No
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Page Range:pp. 1-12
Series Name:Conference Proceedings
Status:Published
Keywords:Numerische Dissipation, Godunov Typ Verfahren
Event Title:International Conference on Computational Fluid Dynamics, ICCFD7
Event Location:Hawaii, USA
Event Type:international Conference
Event Dates:09.-13. Jul. 2012
Organizer:ICCFD
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space Transport
DLR - Research area:Raumfahrt
DLR - Program:R RP - Raumtransport
DLR - Research theme (Project):R - Raumfahrzeugsysteme - Numerische Verfahren und Simulation
Location: Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Spacecraft
Institute of Aerodynamics and Flow Technology > Fluid Systems
Deposited By: Hannemann, Dr.rer.nat. Volker
Deposited On:30 Jul 2012 15:52
Last Modified:31 Jul 2019 19:36

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