Modelling of the energy absorption by polymer composites upon ballistic impact
In this paper we report on the development of a simple model for calculating the energy absorption by polymer composites upon ballistic impact. Three major components were identified as contributing to the energy lost by the projectile during ballistic impact, namely the energy absorbed in tensile f...
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Veröffentlicht in: | Composites science and technology 2000-08, Vol.60 (14), p.2631-2642 |
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description | In this paper we report on the development of a simple model for calculating the energy absorption by polymer composites upon ballistic impact. Three major components were identified as contributing to the energy lost by the projectile during ballistic impact, namely the energy absorbed in tensile failure of the composite, the energy converted into elastic deformation of the composite and the energy converted into the kinetic energy of the moving portion of the composite. These three contributions are combined in the model to determine a value for the ballistic limit of the composite,
V
0. The required input parameters for the model were determined by a combination of physical characterisation (for the physical and mechanical properties of the composites and the characteristics of the projectile) and from high-speed photography (for the size of the deformed region and the cone velocity). As the failure event usually occurred between two of a relatively small number of frames from the high-speed camera, the model predicted a range for
V
0. This range of
V
0 was compared with experimentally determined values for three composite systems: woven Nylon-66 fibres in a 50:50 mixture of phenol formaldehyde resin and polyvinyl butyral resin, woven aramid fibres in a similar matrix and Dyneema UD66 (straight gel-spun polyethylene fibres laid in a 0/90 fibre arrangement in a thermoplastic matrix). In all cases, the experimentally measured values of
V
0 were found to lie within the range predicted by the model. The size of the deformed region, formed through shear deformation, on the back face of the composite was found to relate directly to the in-plane shear modulus of the material. Perhaps the most surprising result was that the dominant energy absorbing mechanism was found to be the kinetic energy of the moving portion of the composites. |
doi_str_mv | 10.1016/S0266-3538(00)00139-1 |
format | Article |
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V
0. The required input parameters for the model were determined by a combination of physical characterisation (for the physical and mechanical properties of the composites and the characteristics of the projectile) and from high-speed photography (for the size of the deformed region and the cone velocity). As the failure event usually occurred between two of a relatively small number of frames from the high-speed camera, the model predicted a range for
V
0. This range of
V
0 was compared with experimentally determined values for three composite systems: woven Nylon-66 fibres in a 50:50 mixture of phenol formaldehyde resin and polyvinyl butyral resin, woven aramid fibres in a similar matrix and Dyneema UD66 (straight gel-spun polyethylene fibres laid in a 0/90 fibre arrangement in a thermoplastic matrix). In all cases, the experimentally measured values of
V
0 were found to lie within the range predicted by the model. The size of the deformed region, formed through shear deformation, on the back face of the composite was found to relate directly to the in-plane shear modulus of the material. Perhaps the most surprising result was that the dominant energy absorbing mechanism was found to be the kinetic energy of the moving portion of the composites.</description><identifier>ISSN: 0266-3538</identifier><identifier>EISSN: 1879-1050</identifier><identifier>DOI: 10.1016/S0266-3538(00)00139-1</identifier><identifier>CODEN: CSTCEH</identifier><language>eng</language><publisher>Oxford: Elsevier Ltd</publisher><subject>Applied sciences ; Ballistic impact ; Exact sciences and technology ; Forms of application and semi-finished materials ; Impact behaviour ; Laminates ; Modelling ; Polymer industry, paints, wood ; Polymer matrix composites (PMC) ; Technology of polymers</subject><ispartof>Composites science and technology, 2000-08, Vol.60 (14), p.2631-2642</ispartof><rights>2000</rights><rights>2001 INIST-CNRS</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c418t-baea350f18f7f0ae6225156243dfee337a0b2b7e9696ce04a2a96470ba34fac83</citedby><cites>FETCH-LOGICAL-c418t-baea350f18f7f0ae6225156243dfee337a0b2b7e9696ce04a2a96470ba34fac83</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://dx.doi.org/10.1016/S0266-3538(00)00139-1$$EHTML$$P50$$Gelsevier$$H</linktohtml><link.rule.ids>314,778,782,3539,27907,27908,45978</link.rule.ids><backlink>$$Uhttp://pascal-francis.inist.fr/vibad/index.php?action=getRecordDetail&idt=816713$$DView record in Pascal Francis$$Hfree_for_read</backlink></links><search><creatorcontrib>Morye, S.S</creatorcontrib><creatorcontrib>Hine, P.J</creatorcontrib><creatorcontrib>Duckett, R.A</creatorcontrib><creatorcontrib>Carr, D.J</creatorcontrib><creatorcontrib>Ward, I.M</creatorcontrib><title>Modelling of the energy absorption by polymer composites upon ballistic impact</title><title>Composites science and technology</title><description>In this paper we report on the development of a simple model for calculating the energy absorption by polymer composites upon ballistic impact. Three major components were identified as contributing to the energy lost by the projectile during ballistic impact, namely the energy absorbed in tensile failure of the composite, the energy converted into elastic deformation of the composite and the energy converted into the kinetic energy of the moving portion of the composite. These three contributions are combined in the model to determine a value for the ballistic limit of the composite,
V
0. The required input parameters for the model were determined by a combination of physical characterisation (for the physical and mechanical properties of the composites and the characteristics of the projectile) and from high-speed photography (for the size of the deformed region and the cone velocity). As the failure event usually occurred between two of a relatively small number of frames from the high-speed camera, the model predicted a range for
V
0. This range of
V
0 was compared with experimentally determined values for three composite systems: woven Nylon-66 fibres in a 50:50 mixture of phenol formaldehyde resin and polyvinyl butyral resin, woven aramid fibres in a similar matrix and Dyneema UD66 (straight gel-spun polyethylene fibres laid in a 0/90 fibre arrangement in a thermoplastic matrix). In all cases, the experimentally measured values of
V
0 were found to lie within the range predicted by the model. The size of the deformed region, formed through shear deformation, on the back face of the composite was found to relate directly to the in-plane shear modulus of the material. Perhaps the most surprising result was that the dominant energy absorbing mechanism was found to be the kinetic energy of the moving portion of the composites.</description><subject>Applied sciences</subject><subject>Ballistic impact</subject><subject>Exact sciences and technology</subject><subject>Forms of application and semi-finished materials</subject><subject>Impact behaviour</subject><subject>Laminates</subject><subject>Modelling</subject><subject>Polymer industry, paints, wood</subject><subject>Polymer matrix composites (PMC)</subject><subject>Technology of polymers</subject><issn>0266-3538</issn><issn>1879-1050</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2000</creationdate><recordtype>article</recordtype><recordid>eNqFkF1L9DAQhYMouH78BCEgiF5UJ02btFcvL-IX-HGhXodpdqKRtqlJV9h_b3dXvPVqBuacM5yHsSMB5wKEuniGXKlMlrI6BTgDELLOxBabiUpPC5SwzWa_kl22l9IHAOiyzmfs8SHMqW19_8aD4-M7ceopvi05NinEYfSh582SD6FddhS5Dd0Qkh8p8cWwOuHkTaO33HcD2vGA7ThsEx3-zH32en31cnmb3T_d3F3-v89sIaoxa5BQluBE5bQDJJXnpShVXsi5I5JSIzR5o6lWtbIEBeZYq0JDg7JwaCu5z042uUMMnwtKo-l8slMR7Cksksl1qWsp5CQsN0IbQ0qRnBmi7zAujQCzomfW9MwKjQEwa3pGTL7jnweYLLYuYm99-jVXQul1-r-NiqauX56iSdZTb2nuI9nRzIP_4883JeWEQQ</recordid><startdate>200008</startdate><enddate>200008</enddate><creator>Morye, S.S</creator><creator>Hine, P.J</creator><creator>Duckett, R.A</creator><creator>Carr, D.J</creator><creator>Ward, I.M</creator><general>Elsevier Ltd</general><general>Elsevier</general><scope>IQODW</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>7SR</scope><scope>8FD</scope><scope>JG9</scope></search><sort><creationdate>200008</creationdate><title>Modelling of the energy absorption by polymer composites upon ballistic impact</title><author>Morye, S.S ; Hine, P.J ; Duckett, R.A ; Carr, D.J ; Ward, I.M</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c418t-baea350f18f7f0ae6225156243dfee337a0b2b7e9696ce04a2a96470ba34fac83</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2000</creationdate><topic>Applied sciences</topic><topic>Ballistic impact</topic><topic>Exact sciences and technology</topic><topic>Forms of application and semi-finished materials</topic><topic>Impact behaviour</topic><topic>Laminates</topic><topic>Modelling</topic><topic>Polymer industry, paints, wood</topic><topic>Polymer matrix composites (PMC)</topic><topic>Technology of polymers</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Morye, S.S</creatorcontrib><creatorcontrib>Hine, P.J</creatorcontrib><creatorcontrib>Duckett, R.A</creatorcontrib><creatorcontrib>Carr, D.J</creatorcontrib><creatorcontrib>Ward, I.M</creatorcontrib><collection>Pascal-Francis</collection><collection>CrossRef</collection><collection>Engineered Materials Abstracts</collection><collection>Technology Research Database</collection><collection>Materials Research Database</collection><jtitle>Composites science and technology</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Morye, S.S</au><au>Hine, P.J</au><au>Duckett, R.A</au><au>Carr, D.J</au><au>Ward, I.M</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Modelling of the energy absorption by polymer composites upon ballistic impact</atitle><jtitle>Composites science and technology</jtitle><date>2000-08</date><risdate>2000</risdate><volume>60</volume><issue>14</issue><spage>2631</spage><epage>2642</epage><pages>2631-2642</pages><issn>0266-3538</issn><eissn>1879-1050</eissn><coden>CSTCEH</coden><abstract>In this paper we report on the development of a simple model for calculating the energy absorption by polymer composites upon ballistic impact. Three major components were identified as contributing to the energy lost by the projectile during ballistic impact, namely the energy absorbed in tensile failure of the composite, the energy converted into elastic deformation of the composite and the energy converted into the kinetic energy of the moving portion of the composite. These three contributions are combined in the model to determine a value for the ballistic limit of the composite,
V
0. The required input parameters for the model were determined by a combination of physical characterisation (for the physical and mechanical properties of the composites and the characteristics of the projectile) and from high-speed photography (for the size of the deformed region and the cone velocity). As the failure event usually occurred between two of a relatively small number of frames from the high-speed camera, the model predicted a range for
V
0. This range of
V
0 was compared with experimentally determined values for three composite systems: woven Nylon-66 fibres in a 50:50 mixture of phenol formaldehyde resin and polyvinyl butyral resin, woven aramid fibres in a similar matrix and Dyneema UD66 (straight gel-spun polyethylene fibres laid in a 0/90 fibre arrangement in a thermoplastic matrix). In all cases, the experimentally measured values of
V
0 were found to lie within the range predicted by the model. The size of the deformed region, formed through shear deformation, on the back face of the composite was found to relate directly to the in-plane shear modulus of the material. Perhaps the most surprising result was that the dominant energy absorbing mechanism was found to be the kinetic energy of the moving portion of the composites.</abstract><cop>Oxford</cop><pub>Elsevier Ltd</pub><doi>10.1016/S0266-3538(00)00139-1</doi><tpages>12</tpages></addata></record> |
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subjects | Applied sciences Ballistic impact Exact sciences and technology Forms of application and semi-finished materials Impact behaviour Laminates Modelling Polymer industry, paints, wood Polymer matrix composites (PMC) Technology of polymers |
title | Modelling of the energy absorption by polymer composites upon ballistic impact |
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