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dc.contributor.author
 hal.structure.identifier
CINNELLA, Paola
134975 Laboratoire de Dynamique des Fluides [DynFluid]
dc.contributor.authorMICHEL, Bruno
dc.date.accessioned2015
dc.date.available2015
dc.date.issued2014
dc.date.submitted2015
dc.identifier.issn1061-8562
dc.identifier.urihttp://hdl.handle.net/10985/10078
dc.description.abstractResidual-based-compact schemes (RBC) of 2nd and 3rd-order accuracy are applied to a challenging 3D ow through a transonic compressor. The proposed schemes provide almost mesh-converged solutions in good agreement with experimental data on relatively coarse grids, which allows achieving a given accuracy level with computational cost reductions by a factor between 2 and 4 with respect to standard solvers.
dc.description.sponsorshipFP7- Projet IDIHOM
dc.language.isoen
dc.publisherTaylor & Francis
dc.rightsPost-print
dc.titleToward improved simulation tools for compressible turbomachinery: assessment of Residual-Based Compact schemes for the transonic compressor NASA Rotor 37
dc.identifier.doi10.1080/10618562.2014.886686
dc.typdocArticle dans une revue avec comité de lecture
dc.localisationCentre de Paris
dc.subject.halMathématique: Analyse numérique
dc.subject.halSciences de l'ingénieur: Mécanique: Mécanique des fluides
ensam.audienceInternationale
ensam.page31-40
ensam.journalInternational Journal of Computational Fluid Dynamics
ensam.volume28
hal.identifierhal-01202618
hal.version1
hal.submission.permittedupdateMetadata
hal.statusaccept
dc.identifier.eissn1029-0257


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