CFD analysis in spray combustion using a pressure swirl injector
| Main Author: | |
|---|---|
| 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. |
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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 |
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reponame:Biblioteca Digital de Teses e Dissertações do ITA instname:Instituto Tecnológico de Aeronáutica instacron:ITA |
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Biblioteca Digital de Teses e Dissertações do ITA |
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Biblioteca Digital de Teses e Dissertações do ITA |
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Instituto Tecnológico de Aeronáutica |
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ITA |
| institution |
ITA |
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Biblioteca Digital de Teses e Dissertações do ITA - Instituto Tecnológico de Aeronáutica |
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|
| subject_por_txtF_mv |
Pulverizadores Injetores Dinâmica dos fluidos computacional Cinética das reações Engenharia química Engenharia mecânica |
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1706809298269503488 |