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Viscosity of aluminum under shock-loading conditions
A reliable data treatment method is critical for viscosity measurements using the disturbance amplitude damping method of shock waves. In this paper the finite difference method is used to obtain the numerical solutions for the disturbance amplitude damping behaviour of the sinusoidal shock front in...
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Published in: | Chinese physics B 2011-06, Vol.20 (6), p.505-508 |
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creator | 马小娟 刘福生 张明建 孙燕云 |
description | A reliable data treatment method is critical for viscosity measurements using the disturbance amplitude damping method of shock waves. In this paper the finite difference method is used to obtain the numerical solutions for the disturbance amplitude damping behaviour of the sinusoidal shock front in a flyer-impact experiment. The disturbance amplitude damping curves are used to depict the numerical solutions of viscous flow. By fitting the experimental data to the numerical solutions of different viscosities, we find that the effective shear viscosity coefficients of shocked aluminum at pressures of 42, 78 and 101 GPa are (1500±100) Pa
s, (2800±100) Pa.s and (3500±100) Pa.s respectively. It is clear that the shear viscosity of aluminum increases with an increase in shock pressure, so aluminum does not melt below a shock pressure of 101 GPa. This conclusion is consistent with the sound velocity measurement. |
doi_str_mv | 10.1088/1674-1056/20/6/068301 |
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s, (2800±100) Pa.s and (3500±100) Pa.s respectively. It is clear that the shear viscosity of aluminum increases with an increase in shock pressure, so aluminum does not melt below a shock pressure of 101 GPa. This conclusion is consistent with the sound velocity measurement.</description><identifier>ISSN: 1674-1056</identifier><identifier>EISSN: 2058-3834</identifier><identifier>DOI: 10.1088/1674-1056/20/6/068301</identifier><language>eng</language><publisher>IOP Publishing</publisher><subject>Aluminum ; Amplitudes ; Damping ; Disturbances ; Finite difference method ; Mathematical models ; Shear viscosity ; Viscosity ; 冲击压力 ; 加载条件 ; 宾夕法尼亚州 ; 数据处理方法 ; 有限差分方法 ; 粘度测量 ; 铝 ; 阻尼行为</subject><ispartof>Chinese physics B, 2011-06, Vol.20 (6), p.505-508</ispartof><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c390t-e15117519fcb6af8eb7b472a4d3c2ebd4d7b0f773d055c294b3d28d8187b19223</citedby><cites>FETCH-LOGICAL-c390t-e15117519fcb6af8eb7b472a4d3c2ebd4d7b0f773d055c294b3d28d8187b19223</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Uhttp://image.cqvip.com/vip1000/qk/85823A/85823A.jpg</thumbnail><link.rule.ids>315,786,790,27957,27958</link.rule.ids></links><search><creatorcontrib>马小娟 刘福生 张明建 孙燕云</creatorcontrib><title>Viscosity of aluminum under shock-loading conditions</title><title>Chinese physics B</title><addtitle>Chinese Physics</addtitle><description>A reliable data treatment method is critical for viscosity measurements using the disturbance amplitude damping method of shock waves. In this paper the finite difference method is used to obtain the numerical solutions for the disturbance amplitude damping behaviour of the sinusoidal shock front in a flyer-impact experiment. The disturbance amplitude damping curves are used to depict the numerical solutions of viscous flow. By fitting the experimental data to the numerical solutions of different viscosities, we find that the effective shear viscosity coefficients of shocked aluminum at pressures of 42, 78 and 101 GPa are (1500±100) Pa
s, (2800±100) Pa.s and (3500±100) Pa.s respectively. It is clear that the shear viscosity of aluminum increases with an increase in shock pressure, so aluminum does not melt below a shock pressure of 101 GPa. This conclusion is consistent with the sound velocity measurement.</description><subject>Aluminum</subject><subject>Amplitudes</subject><subject>Damping</subject><subject>Disturbances</subject><subject>Finite difference method</subject><subject>Mathematical models</subject><subject>Shear viscosity</subject><subject>Viscosity</subject><subject>冲击压力</subject><subject>加载条件</subject><subject>宾夕法尼亚州</subject><subject>数据处理方法</subject><subject>有限差分方法</subject><subject>粘度测量</subject><subject>铝</subject><subject>阻尼行为</subject><issn>1674-1056</issn><issn>2058-3834</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2011</creationdate><recordtype>article</recordtype><recordid>eNqFkbtOwzAUhi0EEqXwCEhhYyDk-BY7I6ooIFViAVYrsZ3WkMRpnAx9e1KlKkslprN8_7l8B6FbDI8YpExwKliMgacJgSRNIJUU8BmaEeAyppKyczQ7MpfoKoRvgBQDoTPEvlzQPrh-F_kyyquhds1QR0NjbBeFjdc_ceVz45p1pH1jXO98E67RRZlXwd4c6hx9Lp8_Fq_x6v3lbfG0ijXNoI8t5hgLjrNSF2leSluIggmSM0M1sYVhRhRQCkENcK5JxgpqiDQSS1HgjBA6R_dT37bz28GGXtXjtraq8sb6IajxKEw5ySiMKJ9Q3fkQOluqtnN13u0UBrW3tIeZ2htQBFSqJktj7mHKOd_-RU6hqjXliMMJ_J8Jd4fNNr5Zb0eTxyCVmI2fYPQX46CAhw</recordid><startdate>20110601</startdate><enddate>20110601</enddate><creator>马小娟 刘福生 张明建 孙燕云</creator><general>IOP Publishing</general><scope>2RA</scope><scope>92L</scope><scope>CQIGP</scope><scope>~WA</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>7QF</scope><scope>7U5</scope><scope>8FD</scope><scope>JG9</scope><scope>L7M</scope></search><sort><creationdate>20110601</creationdate><title>Viscosity of aluminum under shock-loading conditions</title><author>马小娟 刘福生 张明建 孙燕云</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c390t-e15117519fcb6af8eb7b472a4d3c2ebd4d7b0f773d055c294b3d28d8187b19223</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2011</creationdate><topic>Aluminum</topic><topic>Amplitudes</topic><topic>Damping</topic><topic>Disturbances</topic><topic>Finite difference method</topic><topic>Mathematical models</topic><topic>Shear viscosity</topic><topic>Viscosity</topic><topic>冲击压力</topic><topic>加载条件</topic><topic>宾夕法尼亚州</topic><topic>数据处理方法</topic><topic>有限差分方法</topic><topic>粘度测量</topic><topic>铝</topic><topic>阻尼行为</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>马小娟 刘福生 张明建 孙燕云</creatorcontrib><collection>维普_期刊</collection><collection>中文科技期刊数据库-CALIS站点</collection><collection>维普中文期刊数据库</collection><collection>中文科技期刊数据库- 镜像站点</collection><collection>CrossRef</collection><collection>Aluminium Industry Abstracts</collection><collection>Solid State and Superconductivity Abstracts</collection><collection>Technology Research Database</collection><collection>Materials Research Database</collection><collection>Advanced Technologies Database with Aerospace</collection><jtitle>Chinese physics B</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>马小娟 刘福生 张明建 孙燕云</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Viscosity of aluminum under shock-loading conditions</atitle><jtitle>Chinese physics B</jtitle><addtitle>Chinese Physics</addtitle><date>2011-06-01</date><risdate>2011</risdate><volume>20</volume><issue>6</issue><spage>505</spage><epage>508</epage><pages>505-508</pages><issn>1674-1056</issn><eissn>2058-3834</eissn><notes>A reliable data treatment method is critical for viscosity measurements using the disturbance amplitude damping method of shock waves. In this paper the finite difference method is used to obtain the numerical solutions for the disturbance amplitude damping behaviour of the sinusoidal shock front in a flyer-impact experiment. The disturbance amplitude damping curves are used to depict the numerical solutions of viscous flow. By fitting the experimental data to the numerical solutions of different viscosities, we find that the effective shear viscosity coefficients of shocked aluminum at pressures of 42, 78 and 101 GPa are (1500±100) Pa s, (2800±100) Pa.s and (3500±100) Pa.s respectively. It is clear that the shear viscosity of aluminum increases with an increase in shock pressure, so aluminum does not melt below a shock pressure of 101 GPa. This conclusion is consistent with the sound velocity measurement.</notes><notes>Ma Xiao-Juan, Liu Fu-Sheng, Zhang Ming-Jian, and Sun Yan-Yun(School of Physical Science and Technology, Southwest giaotong University, Chengdu 610031, China)</notes><notes>shear viscosity, aluminum, shock-load</notes><notes>11-5639/O4</notes><notes>ObjectType-Article-1</notes><notes>SourceType-Scholarly Journals-1</notes><notes>ObjectType-Feature-2</notes><notes>content type line 23</notes><abstract>A reliable data treatment method is critical for viscosity measurements using the disturbance amplitude damping method of shock waves. In this paper the finite difference method is used to obtain the numerical solutions for the disturbance amplitude damping behaviour of the sinusoidal shock front in a flyer-impact experiment. The disturbance amplitude damping curves are used to depict the numerical solutions of viscous flow. By fitting the experimental data to the numerical solutions of different viscosities, we find that the effective shear viscosity coefficients of shocked aluminum at pressures of 42, 78 and 101 GPa are (1500±100) Pa
s, (2800±100) Pa.s and (3500±100) Pa.s respectively. It is clear that the shear viscosity of aluminum increases with an increase in shock pressure, so aluminum does not melt below a shock pressure of 101 GPa. This conclusion is consistent with the sound velocity measurement.</abstract><pub>IOP Publishing</pub><doi>10.1088/1674-1056/20/6/068301</doi><tpages>4</tpages></addata></record> |
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subjects | Aluminum Amplitudes Damping Disturbances Finite difference method Mathematical models Shear viscosity Viscosity 冲击压力 加载条件 宾夕法尼亚州 数据处理方法 有限差分方法 粘度测量 铝 阻尼行为 |
title | Viscosity of aluminum under shock-loading conditions |
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