Numerical Study on the Gas-Particle Two-Phase Jet Flow during Canister Launching Process
The Euler-Lagrange model of Jet-gas and AL 2 O 3 is established to study the impact of gas-particle jet flow during canister launching process. The gas phase is the Navier-Stokes equation of the two-component transport of gas and air, and the turbulence model is the realizable two-equation model. Th...
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Veröffentlicht in: | Journal of physics. Conference series 2021-06, Vol.1948 (1), p.12074 |
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creator | Liang, Xiao-yang Zhou, Zhi-tan Yu, Qi-rui Le, Gui-gao |
description | The Euler-Lagrange model of Jet-gas and
AL
2
O
3
is established to study the impact of gas-particle jet flow during canister launching process. The gas phase is the Navier-Stokes equation of the two-component transport of gas and air, and the turbulence model is the realizable two-equation model. The airflow flux is numerically discretized via AUSM format, and the viscous dissipation flux is a second-order central difference. The movement trajectories of particles with different diameters ranging from 1 to 100 μm and the distribution characteristics of jet flow dynamic parameters in the launching box are studied. The jet impingement flow field results of gas-particle two-phase flow are compared with those without particle phase. The results show that the particle phase has a retardation and heat transfer effect on the expansion of jet flow, which affects the distribution of jet flow parameters in the launch canister. Furthermore, compared with the pure jet flow impingement effect, the velocity of the two-phase jet flow along the central axis decreases and the temperature increases. Meanwhile, the trajectory of the particle phase is related to the particle diameter. As the diameter of the particles becomes smaller, the flow ability is better and affected by turbulence, and a random movement area in the downstream area of the jet is formed. As the diameter of the particles becomes larger, a particle aggregation area is formed on the jet axis due to inertial force. |
doi_str_mv | 10.1088/1742-6596/1948/1/012074 |
format | Article |
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AL
2
O
3
is established to study the impact of gas-particle jet flow during canister launching process. The gas phase is the Navier-Stokes equation of the two-component transport of gas and air, and the turbulence model is the realizable two-equation model. The airflow flux is numerically discretized via AUSM format, and the viscous dissipation flux is a second-order central difference. The movement trajectories of particles with different diameters ranging from 1 to 100 μm and the distribution characteristics of jet flow dynamic parameters in the launching box are studied. The jet impingement flow field results of gas-particle two-phase flow are compared with those without particle phase. The results show that the particle phase has a retardation and heat transfer effect on the expansion of jet flow, which affects the distribution of jet flow parameters in the launch canister. Furthermore, compared with the pure jet flow impingement effect, the velocity of the two-phase jet flow along the central axis decreases and the temperature increases. Meanwhile, the trajectory of the particle phase is related to the particle diameter. As the diameter of the particles becomes smaller, the flow ability is better and affected by turbulence, and a random movement area in the downstream area of the jet is formed. As the diameter of the particles becomes larger, a particle aggregation area is formed on the jet axis due to inertial force.</description><identifier>ISSN: 1742-6588</identifier><identifier>EISSN: 1742-6596</identifier><identifier>DOI: 10.1088/1742-6596/1948/1/012074</identifier><language>eng</language><publisher>Bristol: IOP Publishing</publisher><subject>Aerodynamics ; Air flow ; Computational fluid dynamics ; Jet flow ; Jet impingement ; Parameters ; Particle size ; Trajectories ; Turbulence models ; Two phase flow ; Vapor phases</subject><ispartof>Journal of physics. Conference series, 2021-06, Vol.1948 (1), p.12074</ispartof><rights>Published under licence by IOP Publishing Ltd</rights><rights>2021. This work is published under http://creativecommons.org/licenses/by/3.0/ (the “License”). Notwithstanding the ProQuest Terms and Conditions, you may use this content in accordance with the terms of the License.</rights><lds50>peer_reviewed</lds50><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed><cites>FETCH-LOGICAL-c2744-cbc43a6047e0e46a657f02f0f8093c79c81822b77a312bf5a77f94616fc2db6e3</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://iopscience.iop.org/article/10.1088/1742-6596/1948/1/012074/pdf$$EPDF$$P50$$Giop$$Hfree_for_read</linktopdf><link.rule.ids>314,776,780,27901,27902,38845,38867,53815,53842</link.rule.ids></links><search><creatorcontrib>Liang, Xiao-yang</creatorcontrib><creatorcontrib>Zhou, Zhi-tan</creatorcontrib><creatorcontrib>Yu, Qi-rui</creatorcontrib><creatorcontrib>Le, Gui-gao</creatorcontrib><title>Numerical Study on the Gas-Particle Two-Phase Jet Flow during Canister Launching Process</title><title>Journal of physics. Conference series</title><addtitle>J. Phys.: Conf. Ser</addtitle><description>The Euler-Lagrange model of Jet-gas and
AL
2
O
3
is established to study the impact of gas-particle jet flow during canister launching process. The gas phase is the Navier-Stokes equation of the two-component transport of gas and air, and the turbulence model is the realizable two-equation model. The airflow flux is numerically discretized via AUSM format, and the viscous dissipation flux is a second-order central difference. The movement trajectories of particles with different diameters ranging from 1 to 100 μm and the distribution characteristics of jet flow dynamic parameters in the launching box are studied. The jet impingement flow field results of gas-particle two-phase flow are compared with those without particle phase. The results show that the particle phase has a retardation and heat transfer effect on the expansion of jet flow, which affects the distribution of jet flow parameters in the launch canister. Furthermore, compared with the pure jet flow impingement effect, the velocity of the two-phase jet flow along the central axis decreases and the temperature increases. Meanwhile, the trajectory of the particle phase is related to the particle diameter. As the diameter of the particles becomes smaller, the flow ability is better and affected by turbulence, and a random movement area in the downstream area of the jet is formed. As the diameter of the particles becomes larger, a particle aggregation area is formed on the jet axis due to inertial force.</description><subject>Aerodynamics</subject><subject>Air flow</subject><subject>Computational fluid dynamics</subject><subject>Jet flow</subject><subject>Jet impingement</subject><subject>Parameters</subject><subject>Particle size</subject><subject>Trajectories</subject><subject>Turbulence models</subject><subject>Two phase flow</subject><subject>Vapor phases</subject><issn>1742-6588</issn><issn>1742-6596</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2021</creationdate><recordtype>article</recordtype><sourceid>O3W</sourceid><sourceid>BENPR</sourceid><recordid>eNqFkF1LwzAUhoMoOKe_wYB3Ql2Spkl7KUWnY2hhE7wLaZq4jq6pScvYv7elMhEEz835et9z4AHgGqM7jOJ4hjklAYsSNsMJ7dsZwgRxegImx83psY7jc3Dh_RahsA8-Ae8v3U67UskKrtquOEBbw3aj4Vz6IJOuLVWl4Xpvg2wjvYYL3cLHyu5h0bmy_oCprEvfageXsqvVZhhlzirt_SU4M7Ly-uo7T8Hb48M6fQqWr_Pn9H4ZKMIpDVSuaCgZolwjTZlkETeIGGRilISKJyrGMSE55zLEJDeR5NwklGFmFClypsMpuBnvNs5-dtq3Yms7V_cvBYkoQz2TkPUqPqqUs947bUTjyp10B4GRGDCKAZAYYIkBo8BixNg7w9FZ2ubn9P-u2z9ciyxd_RaKpjDhF-2UgPw</recordid><startdate>20210601</startdate><enddate>20210601</enddate><creator>Liang, Xiao-yang</creator><creator>Zhou, Zhi-tan</creator><creator>Yu, Qi-rui</creator><creator>Le, Gui-gao</creator><general>IOP Publishing</general><scope>O3W</scope><scope>TSCCA</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>8FD</scope><scope>8FE</scope><scope>8FG</scope><scope>ABUWG</scope><scope>AFKRA</scope><scope>ARAPS</scope><scope>AZQEC</scope><scope>BENPR</scope><scope>BGLVJ</scope><scope>CCPQU</scope><scope>DWQXO</scope><scope>H8D</scope><scope>HCIFZ</scope><scope>L7M</scope><scope>P5Z</scope><scope>P62</scope><scope>PHGZM</scope><scope>PHGZT</scope><scope>PIMPY</scope><scope>PKEHL</scope><scope>PQEST</scope><scope>PQGLB</scope><scope>PQQKQ</scope><scope>PQUKI</scope><scope>PRINS</scope></search><sort><creationdate>20210601</creationdate><title>Numerical Study on the Gas-Particle Two-Phase Jet Flow during Canister Launching Process</title><author>Liang, Xiao-yang ; Zhou, Zhi-tan ; Yu, Qi-rui ; Le, Gui-gao</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c2744-cbc43a6047e0e46a657f02f0f8093c79c81822b77a312bf5a77f94616fc2db6e3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2021</creationdate><topic>Aerodynamics</topic><topic>Air flow</topic><topic>Computational fluid dynamics</topic><topic>Jet flow</topic><topic>Jet impingement</topic><topic>Parameters</topic><topic>Particle size</topic><topic>Trajectories</topic><topic>Turbulence models</topic><topic>Two phase flow</topic><topic>Vapor phases</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Liang, Xiao-yang</creatorcontrib><creatorcontrib>Zhou, Zhi-tan</creatorcontrib><creatorcontrib>Yu, Qi-rui</creatorcontrib><creatorcontrib>Le, Gui-gao</creatorcontrib><collection>IOP Publishing Free Content</collection><collection>IOPscience (Open Access)</collection><collection>CrossRef</collection><collection>Technology Research Database</collection><collection>ProQuest SciTech Collection</collection><collection>ProQuest Technology Collection</collection><collection>ProQuest Central (Alumni Edition)</collection><collection>ProQuest Central UK/Ireland</collection><collection>Advanced Technologies & Aerospace Collection</collection><collection>ProQuest Central Essentials</collection><collection>ProQuest Central</collection><collection>Technology Collection</collection><collection>ProQuest One Community College</collection><collection>ProQuest Central Korea</collection><collection>Aerospace Database</collection><collection>SciTech Premium Collection</collection><collection>Advanced Technologies Database with Aerospace</collection><collection>Advanced Technologies & Aerospace Database</collection><collection>ProQuest Advanced Technologies & Aerospace Collection</collection><collection>ProQuest Central (New)</collection><collection>ProQuest One Academic (New)</collection><collection>Publicly Available Content Database</collection><collection>ProQuest One Academic Middle East (New)</collection><collection>ProQuest One Academic Eastern Edition (DO NOT USE)</collection><collection>ProQuest One Applied & Life Sciences</collection><collection>ProQuest One Academic</collection><collection>ProQuest One Academic UKI Edition</collection><collection>ProQuest Central China</collection><jtitle>Journal of physics. Conference series</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Liang, Xiao-yang</au><au>Zhou, Zhi-tan</au><au>Yu, Qi-rui</au><au>Le, Gui-gao</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Numerical Study on the Gas-Particle Two-Phase Jet Flow during Canister Launching Process</atitle><jtitle>Journal of physics. Conference series</jtitle><addtitle>J. Phys.: Conf. Ser</addtitle><date>2021-06-01</date><risdate>2021</risdate><volume>1948</volume><issue>1</issue><spage>12074</spage><pages>12074-</pages><issn>1742-6588</issn><eissn>1742-6596</eissn><abstract>The Euler-Lagrange model of Jet-gas and
AL
2
O
3
is established to study the impact of gas-particle jet flow during canister launching process. The gas phase is the Navier-Stokes equation of the two-component transport of gas and air, and the turbulence model is the realizable two-equation model. The airflow flux is numerically discretized via AUSM format, and the viscous dissipation flux is a second-order central difference. The movement trajectories of particles with different diameters ranging from 1 to 100 μm and the distribution characteristics of jet flow dynamic parameters in the launching box are studied. The jet impingement flow field results of gas-particle two-phase flow are compared with those without particle phase. The results show that the particle phase has a retardation and heat transfer effect on the expansion of jet flow, which affects the distribution of jet flow parameters in the launch canister. Furthermore, compared with the pure jet flow impingement effect, the velocity of the two-phase jet flow along the central axis decreases and the temperature increases. Meanwhile, the trajectory of the particle phase is related to the particle diameter. As the diameter of the particles becomes smaller, the flow ability is better and affected by turbulence, and a random movement area in the downstream area of the jet is formed. As the diameter of the particles becomes larger, a particle aggregation area is formed on the jet axis due to inertial force.</abstract><cop>Bristol</cop><pub>IOP Publishing</pub><doi>10.1088/1742-6596/1948/1/012074</doi><tpages>6</tpages><oa>free_for_read</oa></addata></record> |
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subjects | Aerodynamics Air flow Computational fluid dynamics Jet flow Jet impingement Parameters Particle size Trajectories Turbulence models Two phase flow Vapor phases |
title | Numerical Study on the Gas-Particle Two-Phase Jet Flow during Canister Launching Process |
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