PERFORMANCE OF PROJECTION METHODS FOR LOW-REYNOLDS-NUMBER FLOWS

Detalhes bibliográficos
Autor(a) principal: Sousa, Fabricio S.
Data de Publicação: 2014
Outros Autores: Oishi, Cassio M. [UNESP], Buscaglia, Gustavo C., Onate, E., Oliver, X, Huerta, A.
Tipo de documento: Artigo de conferência
Idioma: eng
Título da fonte: Repositório Institucional da UNESP
Texto Completo: http://hdl.handle.net/11449/196170
Resumo: There exists growing interest in modelling flows at millimetric and micrometric scales, characterised by low Reynolds numbers (Re << 1). In this work, we investigate the performance of projection methods (of the algebraic-splitting kind) for the computation of steady-state simple benchmark problems. The most popular approximate factorization methods are assessed, together with two so-called exact factorization methods. The results show that: (a) The error introduced by non-incremental schemes on the steady state solution is unacceptably large even in the simplest of flows. This is well-known for the basic first order scheme and motivated variants aiming at increased accuracy. Unfortunately, the variants studied either become unstable for the time steps of interest, or yield steady states with larger error than the basic first order scheme. (b) Incremental schemes have an optimal time step delta t* so as to reach the steady state with minimum computational effort. Taking delta t = delta t* the code reaches the steady state in not less than a few hundred time steps. Such a cost is significantly higher than that of solving the velocity-pressure coupled system, which can compute the steady state in one shot. (c) The main difficulty, however, is that if delta t is chosen too large (in general delta t* is not known), then thousands or tens of thousands of time steps are required to reach the numerical steady state with incremental projection methods. The numerical solutions of these methods follow a time-step-dependent spurious transient which makes the computation of steady states prohibitively expensive.
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spelling PERFORMANCE OF PROJECTION METHODS FOR LOW-REYNOLDS-NUMBER FLOWSProjection methodNavier-Stokes equationsIncompressible flowAlgebraic splittingLow Reynolds numberMicrofluidicsThere exists growing interest in modelling flows at millimetric and micrometric scales, characterised by low Reynolds numbers (Re << 1). In this work, we investigate the performance of projection methods (of the algebraic-splitting kind) for the computation of steady-state simple benchmark problems. The most popular approximate factorization methods are assessed, together with two so-called exact factorization methods. The results show that: (a) The error introduced by non-incremental schemes on the steady state solution is unacceptably large even in the simplest of flows. This is well-known for the basic first order scheme and motivated variants aiming at increased accuracy. Unfortunately, the variants studied either become unstable for the time steps of interest, or yield steady states with larger error than the basic first order scheme. (b) Incremental schemes have an optimal time step delta t* so as to reach the steady state with minimum computational effort. Taking delta t = delta t* the code reaches the steady state in not less than a few hundred time steps. Such a cost is significantly higher than that of solving the velocity-pressure coupled system, which can compute the steady state in one shot. (c) The main difficulty, however, is that if delta t is chosen too large (in general delta t* is not known), then thousands or tens of thousands of time steps are required to reach the numerical steady state with incremental projection methods. The numerical solutions of these methods follow a time-step-dependent spurious transient which makes the computation of steady states prohibitively expensive.Conselho Nacional de Desenvolvimento Científico e Tecnológico (CNPq)Fundação de Amparo à Pesquisa do Estado de São Paulo (FAPESP)Univ Sao Paulo ICMC USP, Dept Appl Math & Stat, Sao Carlos, SP, BrazilUniv Estadual Paulista UNESP, Dept Math & Comp Sci, Presidente Prudente, SP, BrazilUniv Estadual Paulista UNESP, Dept Math & Comp Sci, Presidente Prudente, SP, BrazilFAPESP: 2013/07375-0Int Center Numerical Methods EngineeringUniversidade de São Paulo (USP)Universidade Estadual Paulista (Unesp)Sousa, Fabricio S.Oishi, Cassio M. [UNESP]Buscaglia, Gustavo C.Onate, E.Oliver, XHuerta, A.2020-12-10T19:35:43Z2020-12-10T19:35:43Z2014-01-01info:eu-repo/semantics/publishedVersioninfo:eu-repo/semantics/conferenceObject4950-496111th World Congress On Computational Mechanics; 5th European Conference On Computational Mechanics; 6th European Conference On Computational Fluid Dynamics, Vols V - Vi. 08034 Barcelona: Int Center Numerical Methods Engineering, p. 4950-4961, 2014.http://hdl.handle.net/11449/196170WOS:000485094600031Web of Sciencereponame:Repositório Institucional da UNESPinstname:Universidade Estadual Paulista (UNESP)instacron:UNESPeng11th World Congress On Computational Mechanics; 5th European Conference On Computational Mechanics; 6th European Conference On Computational Fluid Dynamics, Vols V - Viinfo:eu-repo/semantics/openAccess2024-06-19T14:32:27Zoai:repositorio.unesp.br:11449/196170Repositório InstitucionalPUBhttp://repositorio.unesp.br/oai/requestopendoar:29462024-08-05T22:10:33.041662Repositório Institucional da UNESP - Universidade Estadual Paulista (UNESP)false
dc.title.none.fl_str_mv PERFORMANCE OF PROJECTION METHODS FOR LOW-REYNOLDS-NUMBER FLOWS
title PERFORMANCE OF PROJECTION METHODS FOR LOW-REYNOLDS-NUMBER FLOWS
spellingShingle PERFORMANCE OF PROJECTION METHODS FOR LOW-REYNOLDS-NUMBER FLOWS
Sousa, Fabricio S.
Projection method
Navier-Stokes equations
Incompressible flow
Algebraic splitting
Low Reynolds number
Microfluidics
title_short PERFORMANCE OF PROJECTION METHODS FOR LOW-REYNOLDS-NUMBER FLOWS
title_full PERFORMANCE OF PROJECTION METHODS FOR LOW-REYNOLDS-NUMBER FLOWS
title_fullStr PERFORMANCE OF PROJECTION METHODS FOR LOW-REYNOLDS-NUMBER FLOWS
title_full_unstemmed PERFORMANCE OF PROJECTION METHODS FOR LOW-REYNOLDS-NUMBER FLOWS
title_sort PERFORMANCE OF PROJECTION METHODS FOR LOW-REYNOLDS-NUMBER FLOWS
author Sousa, Fabricio S.
author_facet Sousa, Fabricio S.
Oishi, Cassio M. [UNESP]
Buscaglia, Gustavo C.
Onate, E.
Oliver, X
Huerta, A.
author_role author
author2 Oishi, Cassio M. [UNESP]
Buscaglia, Gustavo C.
Onate, E.
Oliver, X
Huerta, A.
author2_role author
author
author
author
author
dc.contributor.none.fl_str_mv Universidade de São Paulo (USP)
Universidade Estadual Paulista (Unesp)
dc.contributor.author.fl_str_mv Sousa, Fabricio S.
Oishi, Cassio M. [UNESP]
Buscaglia, Gustavo C.
Onate, E.
Oliver, X
Huerta, A.
dc.subject.por.fl_str_mv Projection method
Navier-Stokes equations
Incompressible flow
Algebraic splitting
Low Reynolds number
Microfluidics
topic Projection method
Navier-Stokes equations
Incompressible flow
Algebraic splitting
Low Reynolds number
Microfluidics
description There exists growing interest in modelling flows at millimetric and micrometric scales, characterised by low Reynolds numbers (Re << 1). In this work, we investigate the performance of projection methods (of the algebraic-splitting kind) for the computation of steady-state simple benchmark problems. The most popular approximate factorization methods are assessed, together with two so-called exact factorization methods. The results show that: (a) The error introduced by non-incremental schemes on the steady state solution is unacceptably large even in the simplest of flows. This is well-known for the basic first order scheme and motivated variants aiming at increased accuracy. Unfortunately, the variants studied either become unstable for the time steps of interest, or yield steady states with larger error than the basic first order scheme. (b) Incremental schemes have an optimal time step delta t* so as to reach the steady state with minimum computational effort. Taking delta t = delta t* the code reaches the steady state in not less than a few hundred time steps. Such a cost is significantly higher than that of solving the velocity-pressure coupled system, which can compute the steady state in one shot. (c) The main difficulty, however, is that if delta t is chosen too large (in general delta t* is not known), then thousands or tens of thousands of time steps are required to reach the numerical steady state with incremental projection methods. The numerical solutions of these methods follow a time-step-dependent spurious transient which makes the computation of steady states prohibitively expensive.
publishDate 2014
dc.date.none.fl_str_mv 2014-01-01
2020-12-10T19:35:43Z
2020-12-10T19:35:43Z
dc.type.status.fl_str_mv info:eu-repo/semantics/publishedVersion
dc.type.driver.fl_str_mv info:eu-repo/semantics/conferenceObject
format conferenceObject
status_str publishedVersion
dc.identifier.uri.fl_str_mv 11th World Congress On Computational Mechanics; 5th European Conference On Computational Mechanics; 6th European Conference On Computational Fluid Dynamics, Vols V - Vi. 08034 Barcelona: Int Center Numerical Methods Engineering, p. 4950-4961, 2014.
http://hdl.handle.net/11449/196170
WOS:000485094600031
identifier_str_mv 11th World Congress On Computational Mechanics; 5th European Conference On Computational Mechanics; 6th European Conference On Computational Fluid Dynamics, Vols V - Vi. 08034 Barcelona: Int Center Numerical Methods Engineering, p. 4950-4961, 2014.
WOS:000485094600031
url http://hdl.handle.net/11449/196170
dc.language.iso.fl_str_mv eng
language eng
dc.relation.none.fl_str_mv 11th World Congress On Computational Mechanics; 5th European Conference On Computational Mechanics; 6th European Conference On Computational Fluid Dynamics, Vols V - Vi
dc.rights.driver.fl_str_mv info:eu-repo/semantics/openAccess
eu_rights_str_mv openAccess
dc.format.none.fl_str_mv 4950-4961
dc.publisher.none.fl_str_mv Int Center Numerical Methods Engineering
publisher.none.fl_str_mv Int Center Numerical Methods Engineering
dc.source.none.fl_str_mv Web of Science
reponame:Repositório Institucional da UNESP
instname:Universidade Estadual Paulista (UNESP)
instacron:UNESP
instname_str Universidade Estadual Paulista (UNESP)
instacron_str UNESP
institution UNESP
reponame_str Repositório Institucional da UNESP
collection Repositório Institucional da UNESP
repository.name.fl_str_mv Repositório Institucional da UNESP - Universidade Estadual Paulista (UNESP)
repository.mail.fl_str_mv
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