Numerical simulation of turbulent combustion of subsonic gas jet flows
A physical and mathematical model of turbulent combustion of subsonic gas fuel jet flows flowing into an air space is proposed. The processes are described by averaged equations of the boundary layer with a turbulent viscosity model and a combustion diffusion model. As turbulent viscosity models, th...
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Veröffentlicht in: | Mathematical models and computer simulations 2012-09, Vol.4 (5), p.484-492 |
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creator | Lipnitskii, Yu. M. Safronov, A. V. |
description | A physical and mathematical model of turbulent combustion of subsonic gas fuel jet flows flowing into an air space is proposed. The processes are described by averaged equations of the boundary layer with a turbulent viscosity model and a combustion diffusion model. As turbulent viscosity models, the well-known two-parameter
k
-ɛ standard and
k
-ω models are taken. The results of the averaged and pulsating flow characteristics’ comparison of numerical calculations with the experimental data are presented. |
doi_str_mv | 10.1134/S2070048212050067 |
format | Article |
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k
-ɛ standard and
k
-ω models are taken. The results of the averaged and pulsating flow characteristics’ comparison of numerical calculations with the experimental data are presented.</description><identifier>ISSN: 2070-0482</identifier><identifier>EISSN: 2070-0490</identifier><identifier>DOI: 10.1134/S2070048212050067</identifier><language>eng</language><publisher>Dordrecht: SP MAIK Nauka/Interperiodica</publisher><subject>Mathematical Modeling and Industrial Mathematics ; Mathematics ; Mathematics and Statistics ; Simulation and Modeling</subject><ispartof>Mathematical models and computer simulations, 2012-09, Vol.4 (5), p.484-492</ispartof><rights>Pleiades Publishing, Ltd. 2012</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c2037-9dce5bd9612e8b7aef04fb6a263e87e19e7c1427aa843d57d6fd2e3b6bfaa4183</citedby><cites>FETCH-LOGICAL-c2037-9dce5bd9612e8b7aef04fb6a263e87e19e7c1427aa843d57d6fd2e3b6bfaa4183</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://link.springer.com/content/pdf/10.1134/S2070048212050067$$EPDF$$P50$$Gspringer$$H</linktopdf><linktohtml>$$Uhttps://link.springer.com/10.1134/S2070048212050067$$EHTML$$P50$$Gspringer$$H</linktohtml><link.rule.ids>314,776,780,27901,27902,41464,42533,51294</link.rule.ids></links><search><creatorcontrib>Lipnitskii, Yu. M.</creatorcontrib><creatorcontrib>Safronov, A. V.</creatorcontrib><title>Numerical simulation of turbulent combustion of subsonic gas jet flows</title><title>Mathematical models and computer simulations</title><addtitle>Math Models Comput Simul</addtitle><description>A physical and mathematical model of turbulent combustion of subsonic gas fuel jet flows flowing into an air space is proposed. The processes are described by averaged equations of the boundary layer with a turbulent viscosity model and a combustion diffusion model. As turbulent viscosity models, the well-known two-parameter
k
-ɛ standard and
k
-ω models are taken. The results of the averaged and pulsating flow characteristics’ comparison of numerical calculations with the experimental data are presented.</description><subject>Mathematical Modeling and Industrial Mathematics</subject><subject>Mathematics</subject><subject>Mathematics and Statistics</subject><subject>Simulation and Modeling</subject><issn>2070-0482</issn><issn>2070-0490</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2012</creationdate><recordtype>article</recordtype><recordid>eNp9kE9LxDAQxYMouKz7AbzlC1Qnf9qkR1lcFRY9qOeSpJOlS9tI0iB-e7us7kVwLm94zO8xPEKuGdwwJuTtKwcFIDVnHEqASp2RxcEqQNZwfto1vySrlPYwj-BKC70gm-c8YOyc6WnqhtybqQsjDZ5OOdrc4zhRFwab06-fsk1h7BzdmUT3OFHfh890RS686ROufnRJ3jf3b-vHYvvy8LS-2xaOg1BF3TosbVtXjKO2yqAH6W1leCVQK2Q1KsckV8ZoKdpStZVvOQpbWW-MZFosCTvmuhhSiuibj9gNJn41DJpDF82fLmaGH5k03447jM0-5DjOb_4DfQOmQGFZ</recordid><startdate>20120901</startdate><enddate>20120901</enddate><creator>Lipnitskii, Yu. M.</creator><creator>Safronov, A. V.</creator><general>SP MAIK Nauka/Interperiodica</general><scope>AAYXX</scope><scope>CITATION</scope></search><sort><creationdate>20120901</creationdate><title>Numerical simulation of turbulent combustion of subsonic gas jet flows</title><author>Lipnitskii, Yu. M. ; Safronov, A. V.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c2037-9dce5bd9612e8b7aef04fb6a263e87e19e7c1427aa843d57d6fd2e3b6bfaa4183</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2012</creationdate><topic>Mathematical Modeling and Industrial Mathematics</topic><topic>Mathematics</topic><topic>Mathematics and Statistics</topic><topic>Simulation and Modeling</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Lipnitskii, Yu. M.</creatorcontrib><creatorcontrib>Safronov, A. V.</creatorcontrib><collection>CrossRef</collection><jtitle>Mathematical models and computer simulations</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Lipnitskii, Yu. M.</au><au>Safronov, A. V.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Numerical simulation of turbulent combustion of subsonic gas jet flows</atitle><jtitle>Mathematical models and computer simulations</jtitle><stitle>Math Models Comput Simul</stitle><date>2012-09-01</date><risdate>2012</risdate><volume>4</volume><issue>5</issue><spage>484</spage><epage>492</epage><pages>484-492</pages><issn>2070-0482</issn><eissn>2070-0490</eissn><abstract>A physical and mathematical model of turbulent combustion of subsonic gas fuel jet flows flowing into an air space is proposed. The processes are described by averaged equations of the boundary layer with a turbulent viscosity model and a combustion diffusion model. As turbulent viscosity models, the well-known two-parameter
k
-ɛ standard and
k
-ω models are taken. The results of the averaged and pulsating flow characteristics’ comparison of numerical calculations with the experimental data are presented.</abstract><cop>Dordrecht</cop><pub>SP MAIK Nauka/Interperiodica</pub><doi>10.1134/S2070048212050067</doi><tpages>9</tpages></addata></record> |
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subjects | Mathematical Modeling and Industrial Mathematics Mathematics Mathematics and Statistics Simulation and Modeling |
title | Numerical simulation of turbulent combustion of subsonic gas jet flows |
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