Experimental investigation of impact on composite laminates with protective layers
This paper presents an experimental study of low energy impacts on composite plates covered with a protective layer. In service, composite materials are subjected to low energy impacts. Such impacts can generate damage in the material that results in significant reduction in material strength. In or...
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| Veröffentlicht in: | Composites science and technology 2012-01, Vol.72 (2), p.182-189 |
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| container_title | Composites science and technology |
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| creator | Rahmé, P. Bouvet, C. Rivallant, S. Fascio, V. Valembois, G. |
| description | This paper presents an experimental study of low energy impacts on composite plates covered with a protective layer. In service, composite materials are subjected to low energy impacts. Such impacts can generate damage in the material that results in significant reduction in material strength. In order to reduce the damage severity, one solution is to add a mechanical protection on composite structures. The protection layer is made up of a low density energy absorbent material (hollow spheres) of a certain thickness and a thin layer of composite laminate (Kevlar). Energy absorption ability of these protective layers can be deduced from the load/displacement impact curves. First, two configurations of protection are tested on an aluminium plate in order to identify their performance against impact, then the same are tested on composite plates. Test results from force–displacement curves and C-scan control are compared and discussed and finally a comparison of impact on composite plates with and without protection is made for different configurations. |
| doi_str_mv | 10.1016/j.compscitech.2011.10.015 |
| format | Article |
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In service, composite materials are subjected to low energy impacts. Such impacts can generate damage in the material that results in significant reduction in material strength. In order to reduce the damage severity, one solution is to add a mechanical protection on composite structures. The protection layer is made up of a low density energy absorbent material (hollow spheres) of a certain thickness and a thin layer of composite laminate (Kevlar). Energy absorption ability of these protective layers can be deduced from the load/displacement impact curves. First, two configurations of protection are tested on an aluminium plate in order to identify their performance against impact, then the same are tested on composite plates. 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In service, composite materials are subjected to low energy impacts. Such impacts can generate damage in the material that results in significant reduction in material strength. In order to reduce the damage severity, one solution is to add a mechanical protection on composite structures. The protection layer is made up of a low density energy absorbent material (hollow spheres) of a certain thickness and a thin layer of composite laminate (Kevlar). Energy absorption ability of these protective layers can be deduced from the load/displacement impact curves. First, two configurations of protection are tested on an aluminium plate in order to identify their performance against impact, then the same are tested on composite plates. Test results from force–displacement curves and C-scan control are compared and discussed and finally a comparison of impact on composite plates with and without protection is made for different configurations.</description><subject>Aluminum</subject><subject>Applied sciences</subject><subject>B. Delamination</subject><subject>B. Impact behaviour</subject><subject>C. Damage tolerance</subject><subject>Composites</subject><subject>Damage</subject><subject>Density</subject><subject>Engineering Sciences</subject><subject>Exact sciences and technology</subject><subject>Forms of application and semi-finished materials</subject><subject>Laminates</subject><subject>Low energy</subject><subject>Mechanical engineering</subject><subject>Mechanics</subject><subject>Plates</subject><subject>Polymer industry, paints, wood</subject><subject>Protective</subject><subject>Reduction</subject><subject>Technology of polymers</subject><issn>0266-3538</issn><issn>1879-1050</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2012</creationdate><recordtype>article</recordtype><recordid>eNqNkE9r3DAQxUVpods038E5FJqDNzOSZcvHsOQfLBRCchayLGW12JYrKdvk20dmQ8ixp0Ezb97T_Ag5Q1gjYH2xX2s_zlG7ZPRuTQEx99eA_AtZoWjaEoHDV7ICWtcl40x8Jz9i3ANAw1u6IvdXL7MJbjRTUkPhpoOJyT2p5PxUeFu4cVY6FfmxxPiYY4pBjW5SycTin0u7Yg4-Zyd3WCavJsSf5JtVQzSn7_WEPF5fPWxuy-2fm7vN5bbUVd2mUlluG1ubvmqRarSdrmnTokXKKsq4aJmomoopwUXX9x2n0IFB3VSirxtBO3ZCzo--OzXIOd-gwqv0ysnby61ceoCCM2jYAbP291Gbf_v3Od8oRxe1GQY1Gf8cJQKlgtfARJa2R6kOPsZg7Ic3glyYy738xFwuzJdRZp53f73HqKjVYIOatIsfBpRXggrGsm5z1JnM5-BMkNnNTNr0LmSWsvfuP9LeAFwxnZo</recordid><startdate>20120118</startdate><enddate>20120118</enddate><creator>Rahmé, P.</creator><creator>Bouvet, C.</creator><creator>Rivallant, S.</creator><creator>Fascio, V.</creator><creator>Valembois, G.</creator><general>Elsevier Ltd</general><general>Elsevier</general><scope>IQODW</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>7QF</scope><scope>7SR</scope><scope>8FD</scope><scope>JG9</scope><scope>1XC</scope><scope>VOOES</scope><orcidid>https://orcid.org/0000-0002-8882-3161</orcidid><orcidid>https://orcid.org/0000-0003-2637-9170</orcidid></search><sort><creationdate>20120118</creationdate><title>Experimental investigation of impact on composite laminates with protective layers</title><author>Rahmé, P. ; Bouvet, C. ; Rivallant, S. ; Fascio, V. ; Valembois, G.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c469t-af5f7f6ed4912c1fbc62791f123423589384743a858bddb520b0e1c748d6782b3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2012</creationdate><topic>Aluminum</topic><topic>Applied sciences</topic><topic>B. Delamination</topic><topic>B. Impact behaviour</topic><topic>C. Damage tolerance</topic><topic>Composites</topic><topic>Damage</topic><topic>Density</topic><topic>Engineering Sciences</topic><topic>Exact sciences and technology</topic><topic>Forms of application and semi-finished materials</topic><topic>Laminates</topic><topic>Low energy</topic><topic>Mechanical engineering</topic><topic>Mechanics</topic><topic>Plates</topic><topic>Polymer industry, paints, wood</topic><topic>Protective</topic><topic>Reduction</topic><topic>Technology of polymers</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Rahmé, P.</creatorcontrib><creatorcontrib>Bouvet, C.</creatorcontrib><creatorcontrib>Rivallant, S.</creatorcontrib><creatorcontrib>Fascio, V.</creatorcontrib><creatorcontrib>Valembois, G.</creatorcontrib><collection>Pascal-Francis</collection><collection>CrossRef</collection><collection>Aluminium Industry Abstracts</collection><collection>Engineered Materials Abstracts</collection><collection>Technology Research Database</collection><collection>Materials Research Database</collection><collection>Hyper Article en Ligne (HAL)</collection><collection>Hyper Article en Ligne (HAL) (Open Access)</collection><jtitle>Composites science and technology</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Rahmé, P.</au><au>Bouvet, C.</au><au>Rivallant, S.</au><au>Fascio, V.</au><au>Valembois, G.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Experimental investigation of impact on composite laminates with protective layers</atitle><jtitle>Composites science and technology</jtitle><date>2012-01-18</date><risdate>2012</risdate><volume>72</volume><issue>2</issue><spage>182</spage><epage>189</epage><pages>182-189</pages><issn>0266-3538</issn><eissn>1879-1050</eissn><coden>CSTCEH</coden><abstract>This paper presents an experimental study of low energy impacts on composite plates covered with a protective layer. In service, composite materials are subjected to low energy impacts. Such impacts can generate damage in the material that results in significant reduction in material strength. In order to reduce the damage severity, one solution is to add a mechanical protection on composite structures. The protection layer is made up of a low density energy absorbent material (hollow spheres) of a certain thickness and a thin layer of composite laminate (Kevlar). Energy absorption ability of these protective layers can be deduced from the load/displacement impact curves. First, two configurations of protection are tested on an aluminium plate in order to identify their performance against impact, then the same are tested on composite plates. Test results from force–displacement curves and C-scan control are compared and discussed and finally a comparison of impact on composite plates with and without protection is made for different configurations.</abstract><cop>Kidlington</cop><pub>Elsevier Ltd</pub><doi>10.1016/j.compscitech.2011.10.015</doi><tpages>8</tpages><orcidid>https://orcid.org/0000-0002-8882-3161</orcidid><orcidid>https://orcid.org/0000-0003-2637-9170</orcidid><oa>free_for_read</oa></addata></record> |
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| ispartof | Composites science and technology, 2012-01, Vol.72 (2), p.182-189 |
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| language | eng |
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| source | ScienceDirect Freedom Collection (Elsevier) |
| subjects | Aluminum Applied sciences B. Delamination B. Impact behaviour C. Damage tolerance Composites Damage Density Engineering Sciences Exact sciences and technology Forms of application and semi-finished materials Laminates Low energy Mechanical engineering Mechanics Plates Polymer industry, paints, wood Protective Reduction Technology of polymers |
| title | Experimental investigation of impact on composite laminates with protective layers |
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