Investigation of an ionized shock layer in a rarefied gas flow around a reentry vehicle
In order to extend the existing approach of computing ionized flows about reentry spacecraft by the Direct Simulation Monte Carlo (DSMC) method, an ionized shock layer in a rarefied gas flow around a reentry vehicle is considered. The effect of various physical processes on the distribution of the e...
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creator | Shevyrin, Alexander A. Wu, Jong-Shinn Bondar, Yevgeniy A. |
description | In order to extend the existing approach of computing ionized flows about reentry spacecraft by the Direct Simulation Monte Carlo (DSMC) method, an ionized shock layer in a rarefied gas flow around a reentry vehicle is considered. The effect of various physical processes on the distribution of the electron temperature in the shock layer is analyzed by evaluation of the relevant relaxation and exchange terms in the equation of the electron energy balance. |
doi_str_mv | 10.1063/1.4964080 |
format | Conference Proceeding |
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The effect of various physical processes on the distribution of the electron temperature in the shock layer is analyzed by evaluation of the relevant relaxation and exchange terms in the equation of the electron energy balance.</description><identifier>ISSN: 0094-243X</identifier><identifier>EISSN: 1551-7616</identifier><identifier>DOI: 10.1063/1.4964080</identifier><identifier>CODEN: APCPCS</identifier><language>eng</language><publisher>Melville: American Institute of Physics</publisher><subject>Computer simulation ; Direct simulation Monte Carlo method ; Electron energy ; Gas flow ; Rarefied gases ; Reentry vehicles</subject><ispartof>AIP Conference Proceedings, 2016, Vol.1770 (1)</ispartof><rights>Author(s)</rights><rights>2016 Author(s). 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The effect of various physical processes on the distribution of the electron temperature in the shock layer is analyzed by evaluation of the relevant relaxation and exchange terms in the equation of the electron energy balance.</description><subject>Computer simulation</subject><subject>Direct simulation Monte Carlo method</subject><subject>Electron energy</subject><subject>Gas flow</subject><subject>Rarefied gases</subject><subject>Reentry vehicles</subject><issn>0094-243X</issn><issn>1551-7616</issn><fulltext>true</fulltext><rsrctype>conference_proceeding</rsrctype><creationdate>2016</creationdate><recordtype>conference_proceeding</recordtype><recordid>eNp9UE1LAzEUDKJgrR78BwFvwtZ8NckepfhRKHhR9BbSzds2dU1qdltZf72pLXjz9B7MzHszg9AlJSNKJL-hI1FKQTQ5QgM6HtNCSSqP0YCQUhRM8LdTdNa2K0JYqZQeoNdp2ELb-YXtfAw41tgGnDf_DQ63y1i948b2kLAP2OJkE9Q-Iwvb4rqJX9imuAluBwGELvV4C0tfNXCOTmrbtHBxmEP0cn_3PHksZk8P08ntrKi45F3BAEpBpRNCOdBVdqUt4aDnFdFWlXOi5gykdST7l8IpCVwoIVxpqctCzYfoan93neLnJicxq7hJIb80jDIqOVOaZdb1ntVWvvtNatbJf9jUm21MhppDaWbt6v_IlJhdy38C_gMov23A</recordid><startdate>20161013</startdate><enddate>20161013</enddate><creator>Shevyrin, Alexander A.</creator><creator>Wu, Jong-Shinn</creator><creator>Bondar, Yevgeniy A.</creator><general>American Institute of Physics</general><scope>8FD</scope><scope>H8D</scope><scope>L7M</scope></search><sort><creationdate>20161013</creationdate><title>Investigation of an ionized shock layer in a rarefied gas flow around a reentry vehicle</title><author>Shevyrin, Alexander A. ; Wu, Jong-Shinn ; Bondar, Yevgeniy A.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c363t-2ee9416d447de8c0298a03e8bc08a79b07b2e6ad000964d76e34744d9a1d94183</frbrgroupid><rsrctype>conference_proceedings</rsrctype><prefilter>conference_proceedings</prefilter><language>eng</language><creationdate>2016</creationdate><topic>Computer simulation</topic><topic>Direct simulation Monte Carlo method</topic><topic>Electron energy</topic><topic>Gas flow</topic><topic>Rarefied gases</topic><topic>Reentry vehicles</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Shevyrin, Alexander A.</creatorcontrib><creatorcontrib>Wu, Jong-Shinn</creatorcontrib><creatorcontrib>Bondar, Yevgeniy A.</creatorcontrib><collection>Technology Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Shevyrin, Alexander A.</au><au>Wu, Jong-Shinn</au><au>Bondar, Yevgeniy A.</au><au>Fomin, Vasily</au><format>book</format><genre>proceeding</genre><ristype>CONF</ristype><atitle>Investigation of an ionized shock layer in a rarefied gas flow around a reentry vehicle</atitle><btitle>AIP Conference Proceedings</btitle><date>2016-10-13</date><risdate>2016</risdate><volume>1770</volume><issue>1</issue><issn>0094-243X</issn><eissn>1551-7616</eissn><coden>APCPCS</coden><abstract>In order to extend the existing approach of computing ionized flows about reentry spacecraft by the Direct Simulation Monte Carlo (DSMC) method, an ionized shock layer in a rarefied gas flow around a reentry vehicle is considered. The effect of various physical processes on the distribution of the electron temperature in the shock layer is analyzed by evaluation of the relevant relaxation and exchange terms in the equation of the electron energy balance.</abstract><cop>Melville</cop><pub>American Institute of Physics</pub><doi>10.1063/1.4964080</doi><tpages>7</tpages></addata></record> |
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subjects | Computer simulation Direct simulation Monte Carlo method Electron energy Gas flow Rarefied gases Reentry vehicles |
title | Investigation of an ionized shock layer in a rarefied gas flow around a reentry vehicle |
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