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dc.contributor.authorZeifang, Jonas-
dc.contributor.authorBeck, Andrea-
dc.date.accessioned2023-05-26T09:39:06Z-
dc.date.available2023-05-26T09:39:06Z-
dc.date.issued2021de
dc.identifier.issn2096-6385-
dc.identifier.issn2661-8893-
dc.identifier.other1847557120-
dc.identifier.urihttp://nbn-resolving.de/urn:nbn:de:bsz:93-opus-ds-130956de
dc.identifier.urihttp://elib.uni-stuttgart.de/handle/11682/13095-
dc.identifier.urihttp://dx.doi.org/10.18419/opus-13076-
dc.description.abstractConsidering droplet phenomena at low Mach numbers, large differences in the magnitude of the occurring characteristic waves are presented. As acoustic phenomena often play a minor role in such applications, classical explicit schemes which resolve these waves suffer from a very restrictive timestep restriction. In this work, a novel scheme based on a specific level set ghost fluid method and an implicit-explicit (IMEX) flux splitting is proposed to overcome this timestep restriction. A fully implicit narrow band around the sharp phase interface is combined with a splitting of the convective and acoustic phenomena away from the interface. In this part of the domain, the IMEX Runge-Kutta time discretization and the high order discontinuous Galerkin spectral element method are applied to achieve high accuracies in the bulk phases. It is shown that for low Mach numbers a significant gain in computational time can be achieved compared to a fully explicit method. Applications to typical droplet dynamic phenomena validate the proposed method and illustrate its capabilities.en
dc.description.sponsorshipDeutsche Forschungsgemeinschaftde
dc.description.sponsorshipProjekt DEALde
dc.language.isoende
dc.relation.uridoi:10.1007/s42967-021-00137-2de
dc.rightsinfo:eu-repo/semantics/openAccessde
dc.rights.urihttps://creativecommons.org/licenses/by/4.0/de
dc.subject.ddc620de
dc.titleA low Mach number IMEX flux splitting for the level set ghost fluid methoden
dc.typearticlede
dc.date.updated2023-03-28T01:29:58Z-
ubs.fakultaetLuft- und Raumfahrttechnik und Geodäsiede
ubs.fakultaetFakultätsübergreifend / Sonstige Einrichtungde
ubs.institutInstitut für Aerodynamik und Gasdynamikde
ubs.institutFakultätsübergreifend / Sonstige Einrichtungde
ubs.publikation.seiten722-750de
ubs.publikation.sourceCommunications on applied mathematics and computation 5 (2023), S. 722-750de
ubs.publikation.typZeitschriftenartikelde
Enthalten in den Sammlungen:06 Fakultät Luft- und Raumfahrttechnik und Geodäsie

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