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Unsteady compressible flow in ducts with varying cross-section : comparison between the nonconservative Euler system and the axisymmetric flow model

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Resumo:Most of nonconservative hyperbolic systems corresponds to a reduction of an initial three-dimensional problem deriving from a homogenization procedure. Unfortunately, the reduced model gives rise to two new difficulties : the resonance problem corresponding to a splitting or a merging of the genuinely nonlinear waves and the non uniqueness of the Riemann problem solution. The question arises to check whether the two problems correspond and provide similar solutions, at least numerically. In this paper, we propose a comparison between the one-dimensional nonconservative Euler equations modelling the duct with variable cross-sectional area with its original three-dimensional conservative Euler system. Based on the classification of the Riemann problems proposed in \cite{ClRo}, we compare the numerical results of the two models for a large series of representative configurations. We also propose a new example of non uniqueness for the Riemann problem involving the resonance phenomena.
Autores principais:Rochette, D.
Outros Autores:Clain, Stéphane; Bussière, W
Assunto:Riemann problem in ducts Nonconservative system Variable cross-section Axisymmetric flow Shock tube
Ano:2012
País:Portugal
Tipo de documento:artigo
Tipo de acesso:acesso restrito
Instituição associada:Universidade do Minho
Idioma:inglês
Origem:RepositóriUM - Universidade do Minho
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author Rochette, D.
author2 Clain, Stéphane
Bussière, W
author2_role author
author
author_facet Rochette, D.
Clain, Stéphane
Bussière, W
author_role author
contributor_name_str_mv Universidade do Minho
country_str PT
creators_json_txt [{\"Person.name\":\"Rochette, D.\"},{\"Person.name\":\"Clain, Stéphane\"},{\"Person.name\":\"Bussière, W\"}]
datacite.contributors.contributor.contributorName.fl_str_mv Universidade do Minho
datacite.creators.creator.creatorName.fl_str_mv Rochette, D.
Clain, Stéphane
Bussière, W
datacite.date.Accepted.fl_str_mv 2012-01-15T00:00:00Z
datacite.date.available.fl_str_mv 2011-11-15T16:17:08Z
datacite.date.embargoed.fl_str_mv 2011-11-15T16:17:08Z
datacite.rights.fl_str_mv http://purl.org/coar/access_right/c_16ec
datacite.subjects.subject.fl_str_mv Riemann problem in ducts
Nonconservative system
Variable cross-section
Axisymmetric flow
Shock tube
datacite.titles.title.fl_str_mv Unsteady compressible flow in ducts with varying cross-section : comparison between the nonconservative Euler system and the axisymmetric flow model
dc.contributor.none.fl_str_mv Universidade do Minho
dc.creator.none.fl_str_mv Rochette, D.
Clain, Stéphane
Bussière, W
dc.date.Accepted.fl_str_mv 2012-01-15T00:00:00Z
dc.date.available.fl_str_mv 2011-11-15T16:17:08Z
dc.date.embargoed.fl_str_mv 2011-11-15T16:17:08Z
dc.format.none.fl_str_mv application/pdf
dc.identifier.none.fl_str_mv https://hdl.handle.net/1822/14346
dc.language.none.fl_str_mv eng
dc.publisher.none.fl_str_mv Elsevier
dc.rights.none.fl_str_mv http://purl.org/coar/access_right/c_16ec
dc.subject.none.fl_str_mv Riemann problem in ducts
Nonconservative system
Variable cross-section
Axisymmetric flow
Shock tube
dc.title.fl_str_mv Unsteady compressible flow in ducts with varying cross-section : comparison between the nonconservative Euler system and the axisymmetric flow model
dc.type.none.fl_str_mv http://purl.org/coar/resource_type/c_6501
description Most of nonconservative hyperbolic systems corresponds to a reduction of an initial three-dimensional problem deriving from a homogenization procedure. Unfortunately, the reduced model gives rise to two new difficulties : the resonance problem corresponding to a splitting or a merging of the genuinely nonlinear waves and the non uniqueness of the Riemann problem solution. The question arises to check whether the two problems correspond and provide similar solutions, at least numerically. In this paper, we propose a comparison between the one-dimensional nonconservative Euler equations modelling the duct with variable cross-sectional area with its original three-dimensional conservative Euler system. Based on the classification of the Riemann problems proposed in \cite{ClRo}, we compare the numerical results of the two models for a large series of representative configurations. We also propose a new example of non uniqueness for the Riemann problem involving the resonance phenomena.
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language eng
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oai_identifier_str oai:repositorium.uminho.pt:1822/14346
organization_str_mv urn:organizationAcronym:repositorium
person_str_mv Rochette, D.
Clain, Stéphane
Bussière, W
publishDate 2012
publisher.none.fl_str_mv Elsevier
reponame_str RepositóriUM - Universidade do Minho
repository_id_str urn:repositoryAcronym:rum
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spelling engElsevierporMost of nonconservative hyperbolic systems corresponds to a reduction of an initial three-dimensional problem deriving from a homogenization procedure. Unfortunately, the reduced model gives rise to two new difficulties : the resonance problem corresponding to a splitting or a merging of the genuinely nonlinear waves and the non uniqueness of the Riemann problem solution. The question arises to check whether the two problems correspond and provide similar solutions, at least numerically. In this paper, we propose a comparison between the one-dimensional nonconservative Euler equations modelling the duct with variable cross-sectional area with its original three-dimensional conservative Euler system. Based on the classification of the Riemann problems proposed in \cite{ClRo}, we compare the numerical results of the two models for a large series of representative configurations. We also propose a new example of non uniqueness for the Riemann problem involving the resonance phenomena.application/pdfporUnsteady compressible flow in ducts with varying cross-section : comparison between the nonconservative Euler system and the axisymmetric flow modelRochette, D.Clain, StéphaneBussière, WHostingInstitutionOrganizationalUniversidade do Minhoe-mailmailto:repositorium@usdb.uminho.ptrepositorium@usdb.uminho.ptISSNIsPartOf0045-79302011-11-15T16:17:08Z2012-01-152012-01-15T00:00:00ZHandlehttps://hdl.handle.net/1822/14346http://purl.org/coar/access_right/c_16ecrestricted accessRiemann problem in ductsNonconservative systemVariable cross-sectionAxisymmetric flowShock tube3753116 bytesliteraturehttp://purl.org/coar/resource_type/c_6501journal articlehttp://purl.org/coar/access_right/c_16ecapplication/pdffulltexthttps://prod-dspace.uminho.pt/bitstreams/9dcbac2c-2816-4cc6-a736-6b6468518e76/download
spellingShingle Unsteady compressible flow in ducts with varying cross-section : comparison between the nonconservative Euler system and the axisymmetric flow model
Rochette, D.
Riemann problem in ducts
Nonconservative system
Variable cross-section
Axisymmetric flow
Shock tube
status SINGLETON
subject.fl_str_mv Riemann problem in ducts
Nonconservative system
Variable cross-section
Axisymmetric flow
Shock tube
title Unsteady compressible flow in ducts with varying cross-section : comparison between the nonconservative Euler system and the axisymmetric flow model
title_full Unsteady compressible flow in ducts with varying cross-section : comparison between the nonconservative Euler system and the axisymmetric flow model
title_fullStr Unsteady compressible flow in ducts with varying cross-section : comparison between the nonconservative Euler system and the axisymmetric flow model
title_full_unstemmed Unsteady compressible flow in ducts with varying cross-section : comparison between the nonconservative Euler system and the axisymmetric flow model
title_short Unsteady compressible flow in ducts with varying cross-section : comparison between the nonconservative Euler system and the axisymmetric flow model
title_sort Unsteady compressible flow in ducts with varying cross-section : comparison between the nonconservative Euler system and the axisymmetric flow model
topic Riemann problem in ducts
Nonconservative system
Variable cross-section
Axisymmetric flow
Shock tube
topic_facet Riemann problem in ducts
Nonconservative system
Variable cross-section
Axisymmetric flow
Shock tube
url https://hdl.handle.net/1822/14346
visible 1