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An implicit splitting scheme with characteristic boundary conditions for compressible reactive flows on unstructured grid

Pries, Michael and Fiolitakis, Andreas and Gerlinger, Peter (2024) An implicit splitting scheme with characteristic boundary conditions for compressible reactive flows on unstructured grid. Journal of Computational and Applied Mathematics, 437, p. 115446. Elsevier. doi: 10.1016/j.cam.2023.115446. ISSN 0377-0427.

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Official URL: https://dx.doi.org/10.1016/j.cam.2023.115446


Item URL in elib:https://elib.dlr.de/199756/
Document Type:Article
Title:An implicit splitting scheme with characteristic boundary conditions for compressible reactive flows on unstructured grid
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Pries, MichaelUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Fiolitakis, AndreasUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Gerlinger, PeterUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Date:10 July 2024
Journal or Publication Title:Journal of Computational and Applied Mathematics
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:Yes
Volume:437
DOI:10.1016/j.cam.2023.115446
Page Range:p. 115446
Publisher:Elsevier
ISSN:0377-0427
Status:Published
Keywords:implicit characteristic splitting, Navier Stokes characteristic boundary condition (NSCBC), thermoacoustic instability, reacting flow, multi-species, unstructured mesh, low Mach number, finite volume, collocated variable arrangement
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Clean Propulsion
DLR - Research area:Aeronautics
DLR - Program:L CP - Clean Propulsion
DLR - Research theme (Project):L - Virtual Engine, E - Combustion and Power Plant Systems, R - Project TAUROS (TAU for Rocket Thrust Chamber Simulation)
Location: Stuttgart
Institutes and Institutions:Institute of Combustion Technology > Computer Simulation
Deposited By: Geigle, Dr. Klaus Peter
Deposited On:27 Nov 2023 09:40
Last Modified:29 Jan 2024 12:14

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