The Effects of Scalloping Width and Position on Jet Mixing of Lobed Nozzles

Detalhes bibliográficos
Autor(a) principal: DaWei,Liu
Data de Publicação: 2015
Outros Autores: Jun,Huang, Zhiqiang,Sheng, Jinzu,Ji
Tipo de documento: Artigo
Idioma: eng
Título da fonte: Journal of Aerospace Technology and Management (Online)
Texto Completo: http://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462015000400425
Resumo: ABSTRACT: A series of geometric models of lobed nozzles with a central plug was created by different scalloping positions and widths. The shapes of lower and upper edges, cutting depth were kept unchanged. In this study, by the use of numerical simulation, the effects of scalloped width and position on the performance of jet mixing in the pumping condition were analyzed. The results indicated that, as the position of scalloped lower edge kept constant, the radial position of the accelerated mixing region of sidewalls did not change. The accelerated mixing region is enlarged as scalloped width increased, while the growth rate of enlarged region is less than the growth rate of scalloping width. When the scalloped region with the same width moved outward in the radial direction, the mixing rate of the region of the lobe outer edges increased. However, the distance for complete mixing of the primary stream in the core region was increased. It was also found that inward moving of scalloped lower edge enhanced the effect of strengthening streamwise vortices but induced more pressure loss.
id DCTA-1_b4a3a89854c161170224c051a5d3f82e
oai_identifier_str oai:scielo:S2175-91462015000400425
network_acronym_str DCTA-1
network_name_str Journal of Aerospace Technology and Management (Online)
repository_id_str
spelling The Effects of Scalloping Width and Position on Jet Mixing of Lobed NozzlesLobed nozzlesScallopingThermal mixing efficiencyStreamwise vorticityNumerical simulationABSTRACT: A series of geometric models of lobed nozzles with a central plug was created by different scalloping positions and widths. The shapes of lower and upper edges, cutting depth were kept unchanged. In this study, by the use of numerical simulation, the effects of scalloped width and position on the performance of jet mixing in the pumping condition were analyzed. The results indicated that, as the position of scalloped lower edge kept constant, the radial position of the accelerated mixing region of sidewalls did not change. The accelerated mixing region is enlarged as scalloped width increased, while the growth rate of enlarged region is less than the growth rate of scalloping width. When the scalloped region with the same width moved outward in the radial direction, the mixing rate of the region of the lobe outer edges increased. However, the distance for complete mixing of the primary stream in the core region was increased. It was also found that inward moving of scalloped lower edge enhanced the effect of strengthening streamwise vortices but induced more pressure loss.Departamento de Ciência e Tecnologia Aeroespacial2015-12-01info:eu-repo/semantics/articleinfo:eu-repo/semantics/publishedVersiontext/htmlhttp://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462015000400425Journal of Aerospace Technology and Management v.7 n.4 2015reponame:Journal of Aerospace Technology and Management (Online)instname:Departamento de Ciência e Tecnologia Aeroespacial (DCTA)instacron:DCTA10.5028/jatm.v7i4.519info:eu-repo/semantics/openAccessDaWei,LiuJun,HuangZhiqiang,ShengJinzu,Jieng2017-05-23T00:00:00Zoai:scielo:S2175-91462015000400425Revistahttp://www.jatm.com.br/ONGhttps://old.scielo.br/oai/scielo-oai.php||secretary@jatm.com.br2175-91461984-9648opendoar:2017-05-23T00:00Journal of Aerospace Technology and Management (Online) - Departamento de Ciência e Tecnologia Aeroespacial (DCTA)false
dc.title.none.fl_str_mv The Effects of Scalloping Width and Position on Jet Mixing of Lobed Nozzles
title The Effects of Scalloping Width and Position on Jet Mixing of Lobed Nozzles
spellingShingle The Effects of Scalloping Width and Position on Jet Mixing of Lobed Nozzles
DaWei,Liu
Lobed nozzles
Scalloping
Thermal mixing efficiency
Streamwise vorticity
Numerical simulation
title_short The Effects of Scalloping Width and Position on Jet Mixing of Lobed Nozzles
title_full The Effects of Scalloping Width and Position on Jet Mixing of Lobed Nozzles
title_fullStr The Effects of Scalloping Width and Position on Jet Mixing of Lobed Nozzles
title_full_unstemmed The Effects of Scalloping Width and Position on Jet Mixing of Lobed Nozzles
title_sort The Effects of Scalloping Width and Position on Jet Mixing of Lobed Nozzles
author DaWei,Liu
author_facet DaWei,Liu
Jun,Huang
Zhiqiang,Sheng
Jinzu,Ji
author_role author
author2 Jun,Huang
Zhiqiang,Sheng
Jinzu,Ji
author2_role author
author
author
dc.contributor.author.fl_str_mv DaWei,Liu
Jun,Huang
Zhiqiang,Sheng
Jinzu,Ji
dc.subject.por.fl_str_mv Lobed nozzles
Scalloping
Thermal mixing efficiency
Streamwise vorticity
Numerical simulation
topic Lobed nozzles
Scalloping
Thermal mixing efficiency
Streamwise vorticity
Numerical simulation
description ABSTRACT: A series of geometric models of lobed nozzles with a central plug was created by different scalloping positions and widths. The shapes of lower and upper edges, cutting depth were kept unchanged. In this study, by the use of numerical simulation, the effects of scalloped width and position on the performance of jet mixing in the pumping condition were analyzed. The results indicated that, as the position of scalloped lower edge kept constant, the radial position of the accelerated mixing region of sidewalls did not change. The accelerated mixing region is enlarged as scalloped width increased, while the growth rate of enlarged region is less than the growth rate of scalloping width. When the scalloped region with the same width moved outward in the radial direction, the mixing rate of the region of the lobe outer edges increased. However, the distance for complete mixing of the primary stream in the core region was increased. It was also found that inward moving of scalloped lower edge enhanced the effect of strengthening streamwise vortices but induced more pressure loss.
publishDate 2015
dc.date.none.fl_str_mv 2015-12-01
dc.type.driver.fl_str_mv info:eu-repo/semantics/article
dc.type.status.fl_str_mv info:eu-repo/semantics/publishedVersion
format article
status_str publishedVersion
dc.identifier.uri.fl_str_mv http://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462015000400425
url http://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462015000400425
dc.language.iso.fl_str_mv eng
language eng
dc.relation.none.fl_str_mv 10.5028/jatm.v7i4.519
dc.rights.driver.fl_str_mv info:eu-repo/semantics/openAccess
eu_rights_str_mv openAccess
dc.format.none.fl_str_mv text/html
dc.publisher.none.fl_str_mv Departamento de Ciência e Tecnologia Aeroespacial
publisher.none.fl_str_mv Departamento de Ciência e Tecnologia Aeroespacial
dc.source.none.fl_str_mv Journal of Aerospace Technology and Management v.7 n.4 2015
reponame:Journal of Aerospace Technology and Management (Online)
instname:Departamento de Ciência e Tecnologia Aeroespacial (DCTA)
instacron:DCTA
instname_str Departamento de Ciência e Tecnologia Aeroespacial (DCTA)
instacron_str DCTA
institution DCTA
reponame_str Journal of Aerospace Technology and Management (Online)
collection Journal of Aerospace Technology and Management (Online)
repository.name.fl_str_mv Journal of Aerospace Technology and Management (Online) - Departamento de Ciência e Tecnologia Aeroespacial (DCTA)
repository.mail.fl_str_mv ||secretary@jatm.com.br
_version_ 1754732531263995904