CFD analysis in spray combustion using a pressure swirl injector

Bibliographic Details
Main Author: Saulo Alfredo Gómez Salcedo
Publication Date: 2015
Format: Master thesis
Language: eng
Source: Biblioteca Digital de Teses e Dissertações do ITA
Download full: http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=3292
Summary: The object of this work is to apply CFD simulation in the description of the spray burning. As a case study, a pressure swirl injector, characterized and tested by NIST, has been chosen, which atomize liquid kerosene in an atmosphere of gaseous oxygen. The chamber dimensions allow a complete evaporation, avoiding the impact of drops on the circular wall. Swirl-axisymmetric domain and steady state permit to include combustion, a complex process, without requiring of high computational resources. Continuous phase is treated with an Eulerian reference, while fuel drops are tracked following the Lagrangian formulation. Chemical kinetics is reduced to the concept of mixture fraction. This assumption avoids the solution of too many transport equations for all involved species. In the first simulation, the inlet boundary of the continuous phase is obtained from the numerical solution of a fully developed flow transporting the oxidant gas. Then, four cases are proposed and solved, changing the turbulence intensity and swirl velocity on the inlet boundary, each parameter with two different values. Finally, results for the axial velocity, streamlines, drops trajectories, temperature, distribution and total production of selected species are analyzed and compared with other related studies.
id ITA_d6ec92df71f11ba80237dec71d3f10d6
oai_identifier_str oai:agregador.ibict.br.BDTD_ITA:oai:ita.br:3292
network_acronym_str ITA
network_name_str Biblioteca Digital de Teses e Dissertações do ITA
spelling CFD analysis in spray combustion using a pressure swirl injectorPulverizadoresInjetoresDinâmica dos fluidos computacionalCinética das reaçõesEngenharia químicaEngenharia mecânicaThe object of this work is to apply CFD simulation in the description of the spray burning. As a case study, a pressure swirl injector, characterized and tested by NIST, has been chosen, which atomize liquid kerosene in an atmosphere of gaseous oxygen. The chamber dimensions allow a complete evaporation, avoiding the impact of drops on the circular wall. Swirl-axisymmetric domain and steady state permit to include combustion, a complex process, without requiring of high computational resources. Continuous phase is treated with an Eulerian reference, while fuel drops are tracked following the Lagrangian formulation. Chemical kinetics is reduced to the concept of mixture fraction. This assumption avoids the solution of too many transport equations for all involved species. In the first simulation, the inlet boundary of the continuous phase is obtained from the numerical solution of a fully developed flow transporting the oxidant gas. Then, four cases are proposed and solved, changing the turbulence intensity and swirl velocity on the inlet boundary, each parameter with two different values. Finally, results for the axial velocity, streamlines, drops trajectories, temperature, distribution and total production of selected species are analyzed and compared with other related studies.Instituto Tecnológico de AeronáuticaAmilcar Porto PimentaSaulo Alfredo Gómez Salcedo2015-08-17info:eu-repo/semantics/publishedVersioninfo:eu-repo/semantics/masterThesishttp://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=3292reponame:Biblioteca Digital de Teses e Dissertações do ITAinstname:Instituto Tecnológico de Aeronáuticainstacron:ITAenginfo:eu-repo/semantics/openAccessapplication/pdf2019-02-02T14:05:08Zoai:agregador.ibict.br.BDTD_ITA:oai:ita.br:3292http://oai.bdtd.ibict.br/requestopendoar:null2020-05-28 19:41:34.869Biblioteca Digital de Teses e Dissertações do ITA - Instituto Tecnológico de Aeronáuticatrue
dc.title.none.fl_str_mv CFD analysis in spray combustion using a pressure swirl injector
title CFD analysis in spray combustion using a pressure swirl injector
spellingShingle CFD analysis in spray combustion using a pressure swirl injector
Saulo Alfredo Gómez Salcedo
Pulverizadores
Injetores
Dinâmica dos fluidos computacional
Cinética das reações
Engenharia química
Engenharia mecânica
title_short CFD analysis in spray combustion using a pressure swirl injector
title_full CFD analysis in spray combustion using a pressure swirl injector
title_fullStr CFD analysis in spray combustion using a pressure swirl injector
title_full_unstemmed CFD analysis in spray combustion using a pressure swirl injector
title_sort CFD analysis in spray combustion using a pressure swirl injector
author Saulo Alfredo Gómez Salcedo
author_facet Saulo Alfredo Gómez Salcedo
author_role author
dc.contributor.none.fl_str_mv Amilcar Porto Pimenta
dc.contributor.author.fl_str_mv Saulo Alfredo Gómez Salcedo
dc.subject.por.fl_str_mv Pulverizadores
Injetores
Dinâmica dos fluidos computacional
Cinética das reações
Engenharia química
Engenharia mecânica
topic Pulverizadores
Injetores
Dinâmica dos fluidos computacional
Cinética das reações
Engenharia química
Engenharia mecânica
dc.description.none.fl_txt_mv The object of this work is to apply CFD simulation in the description of the spray burning. As a case study, a pressure swirl injector, characterized and tested by NIST, has been chosen, which atomize liquid kerosene in an atmosphere of gaseous oxygen. The chamber dimensions allow a complete evaporation, avoiding the impact of drops on the circular wall. Swirl-axisymmetric domain and steady state permit to include combustion, a complex process, without requiring of high computational resources. Continuous phase is treated with an Eulerian reference, while fuel drops are tracked following the Lagrangian formulation. Chemical kinetics is reduced to the concept of mixture fraction. This assumption avoids the solution of too many transport equations for all involved species. In the first simulation, the inlet boundary of the continuous phase is obtained from the numerical solution of a fully developed flow transporting the oxidant gas. Then, four cases are proposed and solved, changing the turbulence intensity and swirl velocity on the inlet boundary, each parameter with two different values. Finally, results for the axial velocity, streamlines, drops trajectories, temperature, distribution and total production of selected species are analyzed and compared with other related studies.
description The object of this work is to apply CFD simulation in the description of the spray burning. As a case study, a pressure swirl injector, characterized and tested by NIST, has been chosen, which atomize liquid kerosene in an atmosphere of gaseous oxygen. The chamber dimensions allow a complete evaporation, avoiding the impact of drops on the circular wall. Swirl-axisymmetric domain and steady state permit to include combustion, a complex process, without requiring of high computational resources. Continuous phase is treated with an Eulerian reference, while fuel drops are tracked following the Lagrangian formulation. Chemical kinetics is reduced to the concept of mixture fraction. This assumption avoids the solution of too many transport equations for all involved species. In the first simulation, the inlet boundary of the continuous phase is obtained from the numerical solution of a fully developed flow transporting the oxidant gas. Then, four cases are proposed and solved, changing the turbulence intensity and swirl velocity on the inlet boundary, each parameter with two different values. Finally, results for the axial velocity, streamlines, drops trajectories, temperature, distribution and total production of selected species are analyzed and compared with other related studies.
publishDate 2015
dc.date.none.fl_str_mv 2015-08-17
dc.type.driver.fl_str_mv info:eu-repo/semantics/publishedVersion
info:eu-repo/semantics/masterThesis
status_str publishedVersion
format masterThesis
dc.identifier.uri.fl_str_mv http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=3292
url http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=3292
dc.language.iso.fl_str_mv eng
language eng
dc.rights.driver.fl_str_mv info:eu-repo/semantics/openAccess
eu_rights_str_mv openAccess
dc.format.none.fl_str_mv application/pdf
dc.publisher.none.fl_str_mv Instituto Tecnológico de Aeronáutica
publisher.none.fl_str_mv Instituto Tecnológico de Aeronáutica
dc.source.none.fl_str_mv reponame:Biblioteca Digital de Teses e Dissertações do ITA
instname:Instituto Tecnológico de Aeronáutica
instacron:ITA
reponame_str Biblioteca Digital de Teses e Dissertações do ITA
collection Biblioteca Digital de Teses e Dissertações do ITA
instname_str Instituto Tecnológico de Aeronáutica
instacron_str ITA
institution ITA
repository.name.fl_str_mv Biblioteca Digital de Teses e Dissertações do ITA - Instituto Tecnológico de Aeronáutica
repository.mail.fl_str_mv
subject_por_txtF_mv Pulverizadores
Injetores
Dinâmica dos fluidos computacional
Cinética das reações
Engenharia química
Engenharia mecânica
_version_ 1706809298269503488