Numerical Investigations on Dynamics and Heat Transfer in a Turbulent Underexpanded Jet

A fully elliptic Navier-Stokes equation solver in conjunction with a Reynolds stress model is validated for mildly and strongly underexpanded jets. For mildly underexpanded jets, good agreement has been found compared to available measurements for the shock reflections. The model even demonstrated s...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Veröffentlicht in:AIAA journal 2002-11, Vol.40 (11), p.2257-2265
Hauptverfasser: Bartosiewicz, Yann, Mercadier, Yves, Proulx, Pierre
Format: Artikel
Sprache:eng
Schlagworte:
Online-Zugang:Volltext
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
container_end_page 2265
container_issue 11
container_start_page 2257
container_title AIAA journal
container_volume 40
creator Bartosiewicz, Yann
Mercadier, Yves
Proulx, Pierre
description A fully elliptic Navier-Stokes equation solver in conjunction with a Reynolds stress model is validated for mildly and strongly underexpanded jets. For mildly underexpanded jets, good agreement has been found compared to available measurements for the shock reflections. The model even demonstrated some improvements over a three-dimensional modified kappa-epsilon model for turbulent predictions, which confirms the inadequacy of isotropic eddyviscosity-based models to represent properly the turbulence in those flows. For the strongly underexpanded case, the predicted Mach disk location and size are found to be in excellent agreement compared to available measurements. In addition, the predicted flow structure beyond the disk agrees with experimental observations. An attempt is also made to explain the strong coupling between some dynamic features and heat transfer aspects. The sonic line location is revealed to be an important parameter in understanding the global dynamics/heat transfer coupling. In addition, it is demonstrated that a fraction of heat dissipation may be given back to the flow and boost its temperature, which may be useful for spraying applications.
doi_str_mv 10.2514/2.1562
format Article
fullrecord <record><control><sourceid>proquest_pasca</sourceid><recordid>TN_cdi_proquest_miscellaneous_27588281</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>234067401</sourcerecordid><originalsourceid>FETCH-LOGICAL-a370t-a59ed57faa71b1c781c72cdde757ff58ea5c022b5def90b8883ba5032c06a6193</originalsourceid><addsrcrecordid>eNptkE1LAzEURYMoWKv-hqAobkaTTNPJLMWvVkQ3LboLbzIvEplmajIj-u9NtaCIq_DC4d7LIWSfs1Mh-ehMnHI5FhtkwGWeZ7mST5tkwBjjGR9JsU12YnxJlygUH5DH-36BwRlo6NS_YezcM3Su9ZG2nl5-eFg4Eyn4mk4QOjoL4KPFQJ2nQGd9qPoGfUfnvsaA78sEYk1vsdslWxaaiHvrd0jm11ezi0l293AzvTi_yyAvWJeBLLGWhQUoeMVNmmQKYeoai_RppUKQhglRyRptySqlVF6BZLkwbAxjXuZDcvyduwzta5_264WLBpsGPLZ91KKQSgnFE3jwB3xp--DTNi1WolRRqp80E9oYA1q9DG4B4UNzpldytdAruQk8WqdBTO5s0mJc_KHzsuTsq_XkmwMH8KvxK0Uva6tt3zQdvncJPfwP_VP8CTl5kbk</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>215338798</pqid></control><display><type>article</type><title>Numerical Investigations on Dynamics and Heat Transfer in a Turbulent Underexpanded Jet</title><source>Alma/SFX Local Collection</source><creator>Bartosiewicz, Yann ; Mercadier, Yves ; Proulx, Pierre</creator><creatorcontrib>Bartosiewicz, Yann ; Mercadier, Yves ; Proulx, Pierre</creatorcontrib><description>A fully elliptic Navier-Stokes equation solver in conjunction with a Reynolds stress model is validated for mildly and strongly underexpanded jets. For mildly underexpanded jets, good agreement has been found compared to available measurements for the shock reflections. The model even demonstrated some improvements over a three-dimensional modified kappa-epsilon model for turbulent predictions, which confirms the inadequacy of isotropic eddyviscosity-based models to represent properly the turbulence in those flows. For the strongly underexpanded case, the predicted Mach disk location and size are found to be in excellent agreement compared to available measurements. In addition, the predicted flow structure beyond the disk agrees with experimental observations. An attempt is also made to explain the strong coupling between some dynamic features and heat transfer aspects. The sonic line location is revealed to be an important parameter in understanding the global dynamics/heat transfer coupling. In addition, it is demonstrated that a fraction of heat dissipation may be given back to the flow and boost its temperature, which may be useful for spraying applications.</description><identifier>ISSN: 0001-1452</identifier><identifier>EISSN: 1533-385X</identifier><identifier>DOI: 10.2514/2.1562</identifier><identifier>CODEN: AIAJAH</identifier><language>eng</language><publisher>Reston, VA: American Institute of Aeronautics and Astronautics</publisher><subject>Aerodynamics ; Aircraft ; Compressible flows; shock and detonation phenomena ; Exact sciences and technology ; Fluid dynamics ; Fundamental areas of phenomenology (including applications) ; Heat ; Jets ; Physics ; Shock-wave interactions and shock effects ; Shock-wave interactions and shockeffects ; Turbulence ; Turbulence simulation and modeling ; Turbulent flows, convection, and heat transfer</subject><ispartof>AIAA journal, 2002-11, Vol.40 (11), p.2257-2265</ispartof><rights>2002 INIST-CNRS</rights><rights>Copyright American Institute of Aeronautics and Astronautics Nov 2002</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-a370t-a59ed57faa71b1c781c72cdde757ff58ea5c022b5def90b8883ba5032c06a6193</citedby><cites>FETCH-LOGICAL-a370t-a59ed57faa71b1c781c72cdde757ff58ea5c022b5def90b8883ba5032c06a6193</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,777,781,27905,27906</link.rule.ids><backlink>$$Uhttp://pascal-francis.inist.fr/vibad/index.php?action=getRecordDetail&amp;idt=13991081$$DView record in Pascal Francis$$Hfree_for_read</backlink></links><search><creatorcontrib>Bartosiewicz, Yann</creatorcontrib><creatorcontrib>Mercadier, Yves</creatorcontrib><creatorcontrib>Proulx, Pierre</creatorcontrib><title>Numerical Investigations on Dynamics and Heat Transfer in a Turbulent Underexpanded Jet</title><title>AIAA journal</title><description>A fully elliptic Navier-Stokes equation solver in conjunction with a Reynolds stress model is validated for mildly and strongly underexpanded jets. For mildly underexpanded jets, good agreement has been found compared to available measurements for the shock reflections. The model even demonstrated some improvements over a three-dimensional modified kappa-epsilon model for turbulent predictions, which confirms the inadequacy of isotropic eddyviscosity-based models to represent properly the turbulence in those flows. For the strongly underexpanded case, the predicted Mach disk location and size are found to be in excellent agreement compared to available measurements. In addition, the predicted flow structure beyond the disk agrees with experimental observations. An attempt is also made to explain the strong coupling between some dynamic features and heat transfer aspects. The sonic line location is revealed to be an important parameter in understanding the global dynamics/heat transfer coupling. In addition, it is demonstrated that a fraction of heat dissipation may be given back to the flow and boost its temperature, which may be useful for spraying applications.</description><subject>Aerodynamics</subject><subject>Aircraft</subject><subject>Compressible flows; shock and detonation phenomena</subject><subject>Exact sciences and technology</subject><subject>Fluid dynamics</subject><subject>Fundamental areas of phenomenology (including applications)</subject><subject>Heat</subject><subject>Jets</subject><subject>Physics</subject><subject>Shock-wave interactions and shock effects</subject><subject>Shock-wave interactions and shockeffects</subject><subject>Turbulence</subject><subject>Turbulence simulation and modeling</subject><subject>Turbulent flows, convection, and heat transfer</subject><issn>0001-1452</issn><issn>1533-385X</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2002</creationdate><recordtype>article</recordtype><recordid>eNptkE1LAzEURYMoWKv-hqAobkaTTNPJLMWvVkQ3LboLbzIvEplmajIj-u9NtaCIq_DC4d7LIWSfs1Mh-ehMnHI5FhtkwGWeZ7mST5tkwBjjGR9JsU12YnxJlygUH5DH-36BwRlo6NS_YezcM3Su9ZG2nl5-eFg4Eyn4mk4QOjoL4KPFQJ2nQGd9qPoGfUfnvsaA78sEYk1vsdslWxaaiHvrd0jm11ezi0l293AzvTi_yyAvWJeBLLGWhQUoeMVNmmQKYeoai_RppUKQhglRyRptySqlVF6BZLkwbAxjXuZDcvyduwzta5_264WLBpsGPLZ91KKQSgnFE3jwB3xp--DTNi1WolRRqp80E9oYA1q9DG4B4UNzpldytdAruQk8WqdBTO5s0mJc_KHzsuTsq_XkmwMH8KvxK0Uva6tt3zQdvncJPfwP_VP8CTl5kbk</recordid><startdate>20021101</startdate><enddate>20021101</enddate><creator>Bartosiewicz, Yann</creator><creator>Mercadier, Yves</creator><creator>Proulx, Pierre</creator><general>American Institute of Aeronautics and Astronautics</general><scope>IQODW</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>7TB</scope><scope>8FD</scope><scope>FR3</scope><scope>H8D</scope><scope>L7M</scope></search><sort><creationdate>20021101</creationdate><title>Numerical Investigations on Dynamics and Heat Transfer in a Turbulent Underexpanded Jet</title><author>Bartosiewicz, Yann ; Mercadier, Yves ; Proulx, Pierre</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-a370t-a59ed57faa71b1c781c72cdde757ff58ea5c022b5def90b8883ba5032c06a6193</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2002</creationdate><topic>Aerodynamics</topic><topic>Aircraft</topic><topic>Compressible flows; shock and detonation phenomena</topic><topic>Exact sciences and technology</topic><topic>Fluid dynamics</topic><topic>Fundamental areas of phenomenology (including applications)</topic><topic>Heat</topic><topic>Jets</topic><topic>Physics</topic><topic>Shock-wave interactions and shock effects</topic><topic>Shock-wave interactions and shockeffects</topic><topic>Turbulence</topic><topic>Turbulence simulation and modeling</topic><topic>Turbulent flows, convection, and heat transfer</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Bartosiewicz, Yann</creatorcontrib><creatorcontrib>Mercadier, Yves</creatorcontrib><creatorcontrib>Proulx, Pierre</creatorcontrib><collection>Pascal-Francis</collection><collection>CrossRef</collection><collection>Mechanical &amp; Transportation Engineering Abstracts</collection><collection>Technology Research Database</collection><collection>Engineering Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection><jtitle>AIAA journal</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Bartosiewicz, Yann</au><au>Mercadier, Yves</au><au>Proulx, Pierre</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Numerical Investigations on Dynamics and Heat Transfer in a Turbulent Underexpanded Jet</atitle><jtitle>AIAA journal</jtitle><date>2002-11-01</date><risdate>2002</risdate><volume>40</volume><issue>11</issue><spage>2257</spage><epage>2265</epage><pages>2257-2265</pages><issn>0001-1452</issn><eissn>1533-385X</eissn><coden>AIAJAH</coden><abstract>A fully elliptic Navier-Stokes equation solver in conjunction with a Reynolds stress model is validated for mildly and strongly underexpanded jets. For mildly underexpanded jets, good agreement has been found compared to available measurements for the shock reflections. The model even demonstrated some improvements over a three-dimensional modified kappa-epsilon model for turbulent predictions, which confirms the inadequacy of isotropic eddyviscosity-based models to represent properly the turbulence in those flows. For the strongly underexpanded case, the predicted Mach disk location and size are found to be in excellent agreement compared to available measurements. In addition, the predicted flow structure beyond the disk agrees with experimental observations. An attempt is also made to explain the strong coupling between some dynamic features and heat transfer aspects. The sonic line location is revealed to be an important parameter in understanding the global dynamics/heat transfer coupling. In addition, it is demonstrated that a fraction of heat dissipation may be given back to the flow and boost its temperature, which may be useful for spraying applications.</abstract><cop>Reston, VA</cop><pub>American Institute of Aeronautics and Astronautics</pub><doi>10.2514/2.1562</doi><tpages>9</tpages></addata></record>
fulltext fulltext
identifier ISSN: 0001-1452
ispartof AIAA journal, 2002-11, Vol.40 (11), p.2257-2265
issn 0001-1452
1533-385X
language eng
recordid cdi_proquest_miscellaneous_27588281
source Alma/SFX Local Collection
subjects Aerodynamics
Aircraft
Compressible flows
shock and detonation phenomena
Exact sciences and technology
Fluid dynamics
Fundamental areas of phenomenology (including applications)
Heat
Jets
Physics
Shock-wave interactions and shock effects
Shock-wave interactions and shockeffects
Turbulence
Turbulence simulation and modeling
Turbulent flows, convection, and heat transfer
title Numerical Investigations on Dynamics and Heat Transfer in a Turbulent Underexpanded Jet
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-18T15%3A55%3A55IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-proquest_pasca&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=Numerical%20Investigations%20on%20Dynamics%20and%20Heat%20Transfer%20in%20a%20Turbulent%20Underexpanded%20Jet&rft.jtitle=AIAA%20journal&rft.au=Bartosiewicz,%20Yann&rft.date=2002-11-01&rft.volume=40&rft.issue=11&rft.spage=2257&rft.epage=2265&rft.pages=2257-2265&rft.issn=0001-1452&rft.eissn=1533-385X&rft.coden=AIAJAH&rft_id=info:doi/10.2514/2.1562&rft_dat=%3Cproquest_pasca%3E234067401%3C/proquest_pasca%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_pqid=215338798&rft_id=info:pmid/&rfr_iscdi=true