Show simple item record

hal.structure.identifierDipartimento di Ingegneria Meccanica e Aerospaziale [Roma La Sapienza] [DIMA]
dc.contributor.authorASSONITIS, Alessia
hal.structure.identifierDipartimento di Ingegneria Meccanica e Aerospaziale [Roma La Sapienza] [DIMA]
dc.contributor.authorPACIORRI, Renato
hal.structure.identifierCertified Adaptive discRete moDels for robust simulAtions of CoMplex flOws with Moving fronts [CARDAMOM]
dc.contributor.authorCIALLELLA, Mirco
hal.structure.identifierCertified Adaptive discRete moDels for robust simulAtions of CoMplex flOws with Moving fronts [CARDAMOM]
dc.contributor.authorRICCHIUTO, Mario
hal.structure.identifierUniversità degli studi della Basilicata = University of Basilicata [UNIBAS]
dc.contributor.authorBONFIGLIOLI, Aldo
dc.date.accessioned2024-04-04T02:37:22Z
dc.date.available2024-04-04T02:37:22Z
dc.date.issued2022-11
dc.identifier.issn0001-1452
dc.identifier.urihttps://oskar-bordeaux.fr/handle/20.500.12278/190795
dc.description.abstractEnOver the years the development of structured-grid shock-fitting techniques faced two main problems: the handling of a moving discontinuity on a fixed background grid and the capability of simulating complex flow configurations. In the proposed work, the authors present a new shock-fitting technique for structured-grid solvers that is capable of overcoming the limitations that affected the different approaches originally developed. The technique presented here removes the tight link between grid topology and shock topology, which characterizes previous shock fitting as well as front tracking methods. This significantly simplifies their implementation and more importantly reduces the computational overhead related to these geometrical manipulations. Interacting discontinuities and shocks interacting with a solid boundary are discussed and analyzed. Finally, a quantitative investigation of the error reduction obtained with the approach proposed via a global grid convergence analysis is presented.
dc.language.isoen
dc.publisherAmerican Institute of Aeronautics and Astronautics
dc.title.enExtrapolated Shock Fitting for Two-Dimensional Flows on Structured Grids
dc.typeArticle de revue
dc.identifier.doi10.2514/1.J061893
dc.subject.halInformatique [cs]/Modélisation et simulation
bordeaux.journalAIAA Journal
bordeaux.page6301-6312
bordeaux.volume60
bordeaux.hal.laboratoriesInstitut de Mathématiques de Bordeaux (IMB) - UMR 5251*
bordeaux.issue11
bordeaux.institutionUniversité de Bordeaux
bordeaux.institutionBordeaux INP
bordeaux.institutionCNRS
bordeaux.peerReviewedoui
hal.identifierhal-03887410
hal.version1
hal.popularnon
hal.audienceInternationale
hal.origin.linkhttps://hal.archives-ouvertes.fr//hal-03887410v1
bordeaux.COinSctx_ver=Z39.88-2004&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.jtitle=AIAA%20Journal&rft.date=2022-11&rft.volume=60&rft.issue=11&rft.spage=6301-6312&rft.epage=6301-6312&rft.eissn=0001-1452&rft.issn=0001-1452&rft.au=ASSONITIS,%20Alessia&PACIORRI,%20Renato&CIALLELLA,%20Mirco&RICCHIUTO,%20Mario&BONFIGLIOLI,%20Aldo&rft.genre=article


Files in this item

FilesSizeFormatView

There are no files associated with this item.

This item appears in the following Collection(s)

Show simple item record