PERFORMANCE OF PROJECTION METHODS FOR LOW-REYNOLDS-NUMBER FLOWS
Autor(a) principal: | |
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Data de Publicação: | 2014 |
Outros Autores: | , , , , |
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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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 |
|
_version_ |
1808129400305090560 |