dc.contributorUniversidade de São Paulo (USP)
dc.contributorUniversidade do Oeste Paulista (UNOESTE)
dc.contributorUniversidade Estadual Paulista (Unesp)
dc.date.accessioned2014-05-20T13:26:18Z
dc.date.available2014-05-20T13:26:18Z
dc.date.created2014-05-20T13:26:18Z
dc.date.issued2012-05-01
dc.identifierApplied Mathematics and Computation. New York: Elsevier B.V., v. 218, n. 17, p. 8614-8633, 2012.
dc.identifier0096-3003
dc.identifierhttp://hdl.handle.net/11449/8454
dc.identifier10.1016/j.amc.2012.02.024
dc.identifierWOS:000302769100036
dc.identifier7730719476451232
dc.identifier0000-0001-5762-6424
dc.description.abstractThis paper deals with the numerical solution of complex fluid dynamics problems using a new bounded high resolution upwind scheme (called SDPUS-C1 henceforth), for convection term discretization. The scheme is based on TVD and CBC stability criteria and is implemented in the context of the finite volume/difference methodologies, either into the CLAWPACK software package for compressible flows or in the Freeflow simulation system for incompressible viscous flows. The performance of the proposed upwind non-oscillatory scheme is demonstrated by solving two-dimensional compressible flow problems, such as shock wave propagation and two-dimensional/axisymmetric incompressible moving free surface flows. The numerical results demonstrate that this new cell-interface reconstruction technique works very well in several practical applications. (C) 2012 Elsevier B.V. All rights reserved.
dc.languageeng
dc.publisherElsevier B.V.
dc.relationApplied Mathematics and Computation
dc.relation2.300
dc.relation1,065
dc.rightsAcesso restrito
dc.sourceWeb of Science
dc.subjectTVD/CBC stability
dc.subjectHigh resolution schemes
dc.subjectUpwinding
dc.subjectConvection term discretization
dc.subjectBoundedness criteria
dc.subjectShock-capturing
dc.subjectConservation laws
dc.subjectFree surface flows
dc.titleA continuously differentiable upwinding scheme for the simulation of fluid flow problems
dc.typeArtículos de revistas


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