A coupled computational framework for the transient heat transfer in the typical pyrotechnic device
Propellant combustion in pyrotechnic devices produces high-temperature, high-pressure gas. The component is moved by high-pressure gas, which subsequently impacts the energy absorber and causes it to compress and deform. The temperature difference between the high-temperature gas and the wall causes...
Gespeichert in:
Veröffentlicht in: | AIP advances 2023-07, Vol.13 (7), p.075312-075312-13 |
---|---|
Hauptverfasser: | , , , |
Format: | Artikel |
Sprache: | eng |
Schlagworte: | |
Online-Zugang: | Volltext |
Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
container_end_page | 075312-13 |
---|---|
container_issue | 7 |
container_start_page | 075312 |
container_title | AIP advances |
container_volume | 13 |
creator | Jiang, Kun Lu, Xinggan Cheng, ShenShen Jian, Wang |
description | Propellant combustion in pyrotechnic devices produces high-temperature, high-pressure gas. The component is moved by high-pressure gas, which subsequently impacts the energy absorber and causes it to compress and deform. The temperature difference between the high-temperature gas and the wall causes transient heat transfer. Propellant combustion, transient heat transfer, and structural response are coupled, but previous studies had to independently analyze them. Therefore, a multi-physical field numerical model is developed based on the commercial software ABAQUS in this paper, which couples energetic material combustion, transient heat transfer, and structural response. In the user subroutine VUAMP, a lumped-parameter model is used to predict the parameter distribution of combustion products. This determines the load applied on the thin-walled tube and the boundary conditions of transient heat transfer. In ABAQUS, the transient heat transfer and structural response are investigated by the direct thermo-dynamic coupling method. The coupling effect between multiple physical fields is realized by real-time parameter exchange. The rationality and accuracy of the coupling model are verified by comparison with the experiment. The results show that the coupling model can effectively simulate the complex coupling process after considering the transient heat transfer and the interaction between multiple physical fields. Taking a pyrotechnic device as the research object, the pressure load accuracy obtained by the coupled model is improved by 5.1%, and the structure response obtained is also closer to the experiment result. At the same time, more characteristic parameters of the structure field and temperature field are obtained. |
doi_str_mv | 10.1063/5.0141723 |
format | Article |
fullrecord | <record><control><sourceid>proquest_scita</sourceid><recordid>TN_cdi_scitation_primary_10_1063_5_0141723</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><doaj_id>oai_doaj_org_article_958f65cd44dd4c3a90e9ca0ed072d902</doaj_id><sourcerecordid>2835641777</sourcerecordid><originalsourceid>FETCH-LOGICAL-c393t-f6b15a66d4804d210e79de364db96c0fd6952a81bdc3a99cb18a98ca66aef05d3</originalsourceid><addsrcrecordid>eNp9kU1LAzEQhhdRsNQe_AcLnhSq-d7NsRQ_CoIXPYc0mdjUdrMmqdJ_b-qKeHIuM5l55g28U1XnGF1jJOgNv0aY4YbQo2pEMG-nlBBx_Kc-rSYprVEJJjFq2agys9qEXb8BW_K232Wdfej0pnZRb-EzxLfahVjnFdQ56i556HK9Ap2Hp4NY-24Y73tvymK_jyGDWXXe1BY-vIGz6sTpTYLJTx5XL3e3z_OH6ePT_WI-e5waKmmeOrHEXAthWYuYJRhBIy1QwexSCoOcFZIT3eKlNVRLaZa41bI1ZUODQ9zScbUYdG3Qa9VHv9Vxr4L26rsR4qvSMXuzASV56wQ3ljFr2UEOgTQagUUNsRKRonUxaPUxvO8gZbUOu1iMSYq0lItic9MU6nKgTAwpRXC_v2KkDidRXP2cpLBXA5uMH1z-B_4C-GiL6A</addsrcrecordid><sourcetype>Open Website</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>2835641777</pqid></control><display><type>article</type><title>A coupled computational framework for the transient heat transfer in the typical pyrotechnic device</title><source>DOAJ Directory of Open Access Journals</source><source>EZB-FREE-00999 freely available EZB journals</source><source>Alma/SFX Local Collection</source><source>Free Full-Text Journals in Chemistry</source><creator>Jiang, Kun ; Lu, Xinggan ; Cheng, ShenShen ; Jian, Wang</creator><creatorcontrib>Jiang, Kun ; Lu, Xinggan ; Cheng, ShenShen ; Jian, Wang</creatorcontrib><description>Propellant combustion in pyrotechnic devices produces high-temperature, high-pressure gas. The component is moved by high-pressure gas, which subsequently impacts the energy absorber and causes it to compress and deform. The temperature difference between the high-temperature gas and the wall causes transient heat transfer. Propellant combustion, transient heat transfer, and structural response are coupled, but previous studies had to independently analyze them. Therefore, a multi-physical field numerical model is developed based on the commercial software ABAQUS in this paper, which couples energetic material combustion, transient heat transfer, and structural response. In the user subroutine VUAMP, a lumped-parameter model is used to predict the parameter distribution of combustion products. This determines the load applied on the thin-walled tube and the boundary conditions of transient heat transfer. In ABAQUS, the transient heat transfer and structural response are investigated by the direct thermo-dynamic coupling method. The coupling effect between multiple physical fields is realized by real-time parameter exchange. The rationality and accuracy of the coupling model are verified by comparison with the experiment. The results show that the coupling model can effectively simulate the complex coupling process after considering the transient heat transfer and the interaction between multiple physical fields. Taking a pyrotechnic device as the research object, the pressure load accuracy obtained by the coupled model is improved by 5.1%, and the structure response obtained is also closer to the experiment result. At the same time, more characteristic parameters of the structure field and temperature field are obtained.</description><identifier>ISSN: 2158-3226</identifier><identifier>EISSN: 2158-3226</identifier><identifier>DOI: 10.1063/5.0141723</identifier><identifier>CODEN: AAIDBI</identifier><language>eng</language><publisher>Melville: American Institute of Physics</publisher><subject>Accuracy ; Boundary conditions ; Combustion products ; Coupling ; Energetic materials ; Finite element method ; Fireworks ; Heat transfer ; High pressure ; High temperature gases ; Mathematical models ; Numerical models ; Parameters ; Propellant combustion ; Propellant transfer ; Structural response ; Temperature distribution ; Temperature gradients ; Transient heat transfer</subject><ispartof>AIP advances, 2023-07, Vol.13 (7), p.075312-075312-13</ispartof><rights>Author(s)</rights><rights>2023 Author(s). All article content, except where otherwise noted, is licensed under a Creative Commons Attribution (CC BY) license (http://creativecommons.org/licenses/by/4.0/).</rights><lds50>peer_reviewed</lds50><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c393t-f6b15a66d4804d210e79de364db96c0fd6952a81bdc3a99cb18a98ca66aef05d3</citedby><cites>FETCH-LOGICAL-c393t-f6b15a66d4804d210e79de364db96c0fd6952a81bdc3a99cb18a98ca66aef05d3</cites><orcidid>0000-0002-6597-3933 ; 0000-0002-9156-2812 ; 0000-0002-6735-6998</orcidid></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,780,784,864,2102,27924,27925</link.rule.ids></links><search><creatorcontrib>Jiang, Kun</creatorcontrib><creatorcontrib>Lu, Xinggan</creatorcontrib><creatorcontrib>Cheng, ShenShen</creatorcontrib><creatorcontrib>Jian, Wang</creatorcontrib><title>A coupled computational framework for the transient heat transfer in the typical pyrotechnic device</title><title>AIP advances</title><description>Propellant combustion in pyrotechnic devices produces high-temperature, high-pressure gas. The component is moved by high-pressure gas, which subsequently impacts the energy absorber and causes it to compress and deform. The temperature difference between the high-temperature gas and the wall causes transient heat transfer. Propellant combustion, transient heat transfer, and structural response are coupled, but previous studies had to independently analyze them. Therefore, a multi-physical field numerical model is developed based on the commercial software ABAQUS in this paper, which couples energetic material combustion, transient heat transfer, and structural response. In the user subroutine VUAMP, a lumped-parameter model is used to predict the parameter distribution of combustion products. This determines the load applied on the thin-walled tube and the boundary conditions of transient heat transfer. In ABAQUS, the transient heat transfer and structural response are investigated by the direct thermo-dynamic coupling method. The coupling effect between multiple physical fields is realized by real-time parameter exchange. The rationality and accuracy of the coupling model are verified by comparison with the experiment. The results show that the coupling model can effectively simulate the complex coupling process after considering the transient heat transfer and the interaction between multiple physical fields. Taking a pyrotechnic device as the research object, the pressure load accuracy obtained by the coupled model is improved by 5.1%, and the structure response obtained is also closer to the experiment result. At the same time, more characteristic parameters of the structure field and temperature field are obtained.</description><subject>Accuracy</subject><subject>Boundary conditions</subject><subject>Combustion products</subject><subject>Coupling</subject><subject>Energetic materials</subject><subject>Finite element method</subject><subject>Fireworks</subject><subject>Heat transfer</subject><subject>High pressure</subject><subject>High temperature gases</subject><subject>Mathematical models</subject><subject>Numerical models</subject><subject>Parameters</subject><subject>Propellant combustion</subject><subject>Propellant transfer</subject><subject>Structural response</subject><subject>Temperature distribution</subject><subject>Temperature gradients</subject><subject>Transient heat transfer</subject><issn>2158-3226</issn><issn>2158-3226</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2023</creationdate><recordtype>article</recordtype><sourceid>DOA</sourceid><recordid>eNp9kU1LAzEQhhdRsNQe_AcLnhSq-d7NsRQ_CoIXPYc0mdjUdrMmqdJ_b-qKeHIuM5l55g28U1XnGF1jJOgNv0aY4YbQo2pEMG-nlBBx_Kc-rSYprVEJJjFq2agys9qEXb8BW_K232Wdfej0pnZRb-EzxLfahVjnFdQ56i556HK9Ap2Hp4NY-24Y73tvymK_jyGDWXXe1BY-vIGz6sTpTYLJTx5XL3e3z_OH6ePT_WI-e5waKmmeOrHEXAthWYuYJRhBIy1QwexSCoOcFZIT3eKlNVRLaZa41bI1ZUODQ9zScbUYdG3Qa9VHv9Vxr4L26rsR4qvSMXuzASV56wQ3ljFr2UEOgTQagUUNsRKRonUxaPUxvO8gZbUOu1iMSYq0lItic9MU6nKgTAwpRXC_v2KkDidRXP2cpLBXA5uMH1z-B_4C-GiL6A</recordid><startdate>20230701</startdate><enddate>20230701</enddate><creator>Jiang, Kun</creator><creator>Lu, Xinggan</creator><creator>Cheng, ShenShen</creator><creator>Jian, Wang</creator><general>American Institute of Physics</general><general>AIP Publishing LLC</general><scope>AJDQP</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>8FD</scope><scope>H8D</scope><scope>L7M</scope><scope>DOA</scope><orcidid>https://orcid.org/0000-0002-6597-3933</orcidid><orcidid>https://orcid.org/0000-0002-9156-2812</orcidid><orcidid>https://orcid.org/0000-0002-6735-6998</orcidid></search><sort><creationdate>20230701</creationdate><title>A coupled computational framework for the transient heat transfer in the typical pyrotechnic device</title><author>Jiang, Kun ; Lu, Xinggan ; Cheng, ShenShen ; Jian, Wang</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c393t-f6b15a66d4804d210e79de364db96c0fd6952a81bdc3a99cb18a98ca66aef05d3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2023</creationdate><topic>Accuracy</topic><topic>Boundary conditions</topic><topic>Combustion products</topic><topic>Coupling</topic><topic>Energetic materials</topic><topic>Finite element method</topic><topic>Fireworks</topic><topic>Heat transfer</topic><topic>High pressure</topic><topic>High temperature gases</topic><topic>Mathematical models</topic><topic>Numerical models</topic><topic>Parameters</topic><topic>Propellant combustion</topic><topic>Propellant transfer</topic><topic>Structural response</topic><topic>Temperature distribution</topic><topic>Temperature gradients</topic><topic>Transient heat transfer</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Jiang, Kun</creatorcontrib><creatorcontrib>Lu, Xinggan</creatorcontrib><creatorcontrib>Cheng, ShenShen</creatorcontrib><creatorcontrib>Jian, Wang</creatorcontrib><collection>AIP Open Access Journals</collection><collection>CrossRef</collection><collection>Technology Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection><collection>DOAJ Directory of Open Access Journals</collection><jtitle>AIP advances</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Jiang, Kun</au><au>Lu, Xinggan</au><au>Cheng, ShenShen</au><au>Jian, Wang</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>A coupled computational framework for the transient heat transfer in the typical pyrotechnic device</atitle><jtitle>AIP advances</jtitle><date>2023-07-01</date><risdate>2023</risdate><volume>13</volume><issue>7</issue><spage>075312</spage><epage>075312-13</epage><pages>075312-075312-13</pages><issn>2158-3226</issn><eissn>2158-3226</eissn><coden>AAIDBI</coden><abstract>Propellant combustion in pyrotechnic devices produces high-temperature, high-pressure gas. The component is moved by high-pressure gas, which subsequently impacts the energy absorber and causes it to compress and deform. The temperature difference between the high-temperature gas and the wall causes transient heat transfer. Propellant combustion, transient heat transfer, and structural response are coupled, but previous studies had to independently analyze them. Therefore, a multi-physical field numerical model is developed based on the commercial software ABAQUS in this paper, which couples energetic material combustion, transient heat transfer, and structural response. In the user subroutine VUAMP, a lumped-parameter model is used to predict the parameter distribution of combustion products. This determines the load applied on the thin-walled tube and the boundary conditions of transient heat transfer. In ABAQUS, the transient heat transfer and structural response are investigated by the direct thermo-dynamic coupling method. The coupling effect between multiple physical fields is realized by real-time parameter exchange. The rationality and accuracy of the coupling model are verified by comparison with the experiment. The results show that the coupling model can effectively simulate the complex coupling process after considering the transient heat transfer and the interaction between multiple physical fields. Taking a pyrotechnic device as the research object, the pressure load accuracy obtained by the coupled model is improved by 5.1%, and the structure response obtained is also closer to the experiment result. At the same time, more characteristic parameters of the structure field and temperature field are obtained.</abstract><cop>Melville</cop><pub>American Institute of Physics</pub><doi>10.1063/5.0141723</doi><tpages>13</tpages><orcidid>https://orcid.org/0000-0002-6597-3933</orcidid><orcidid>https://orcid.org/0000-0002-9156-2812</orcidid><orcidid>https://orcid.org/0000-0002-6735-6998</orcidid><oa>free_for_read</oa></addata></record> |
fulltext | fulltext |
identifier | ISSN: 2158-3226 |
ispartof | AIP advances, 2023-07, Vol.13 (7), p.075312-075312-13 |
issn | 2158-3226 2158-3226 |
language | eng |
recordid | cdi_scitation_primary_10_1063_5_0141723 |
source | DOAJ Directory of Open Access Journals; EZB-FREE-00999 freely available EZB journals; Alma/SFX Local Collection; Free Full-Text Journals in Chemistry |
subjects | Accuracy Boundary conditions Combustion products Coupling Energetic materials Finite element method Fireworks Heat transfer High pressure High temperature gases Mathematical models Numerical models Parameters Propellant combustion Propellant transfer Structural response Temperature distribution Temperature gradients Transient heat transfer |
title | A coupled computational framework for the transient heat transfer in the typical pyrotechnic device |
url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2024-12-29T03%3A40%3A22IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-proquest_scita&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=A%20coupled%20computational%20framework%20for%20the%20transient%20heat%20transfer%20in%20the%20typical%20pyrotechnic%20device&rft.jtitle=AIP%20advances&rft.au=Jiang,%20Kun&rft.date=2023-07-01&rft.volume=13&rft.issue=7&rft.spage=075312&rft.epage=075312-13&rft.pages=075312-075312-13&rft.issn=2158-3226&rft.eissn=2158-3226&rft.coden=AAIDBI&rft_id=info:doi/10.1063/5.0141723&rft_dat=%3Cproquest_scita%3E2835641777%3C/proquest_scita%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_pqid=2835641777&rft_id=info:pmid/&rft_doaj_id=oai_doaj_org_article_958f65cd44dd4c3a90e9ca0ed072d902&rfr_iscdi=true |