Behaviour of fibre metal laminates subjected to localised blast loading—Part II: Quantitative analysis
This two part paper examines the behaviour of fibre-metal laminates (FMLs) subjected to localised explosive blast loading. Part I presents the experimental observations of diamond and cross-shaped back face deformation, as well as pitting, global displacement and ring-buckling of the front face are...
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| Veröffentlicht in: | International journal of impact engineering 2007-07, Vol.34 (7), p.1223-1245 |
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| container_end_page | 1245 |
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| container_issue | 7 |
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| container_title | International journal of impact engineering |
| container_volume | 34 |
| creator | Lemanski, S.L. Nurick, G.N. Langdon, G.S. Simmons, M.C. Cantwell, W.J. Schleyer, G.K. |
| description | This two part paper examines the behaviour of fibre-metal laminates (FMLs) subjected to localised explosive blast loading. Part I presents the
experimental observations of diamond and cross-shaped back face deformation, as well as pitting, global displacement and ring-buckling of the front face are also discerned. Part II presents
quantitative analysis of the experimental data. When expressed in terms of non-dimensional parameters front and back face displacements fall within one plate thickness of a linear trend line. The threshold impulse for the onset of tearing is found to increase linearly with panel thickness. |
| doi_str_mv | 10.1016/j.ijimpeng.2006.05.009 |
| format | Article |
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experimental observations of diamond and cross-shaped back face deformation, as well as pitting, global displacement and ring-buckling of the front face are also discerned. Part II presents
quantitative analysis of the experimental data. When expressed in terms of non-dimensional parameters front and back face displacements fall within one plate thickness of a linear trend line. The threshold impulse for the onset of tearing is found to increase linearly with panel thickness.</description><identifier>ISSN: 0734-743X</identifier><identifier>EISSN: 1879-3509</identifier><identifier>DOI: 10.1016/j.ijimpeng.2006.05.009</identifier><identifier>CODEN: IJIED4</identifier><language>eng</language><publisher>Oxford: Elsevier Ltd</publisher><subject>Blast loading ; Buckling ; Composite ; Exact sciences and technology ; Failure ; Fibre-metal laminate ; Fracture mechanics (crack, fatigue, damage...) ; Fundamental areas of phenomenology (including applications) ; Panel ; Physics ; Solid mechanics ; Structural and continuum mechanics</subject><ispartof>International journal of impact engineering, 2007-07, Vol.34 (7), p.1223-1245</ispartof><rights>2006 Elsevier Ltd</rights><rights>2007 INIST-CNRS</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c373t-6f2f5d2426417e790a765f1aacadd4b4283ab3e692c85d391f44039c0bc013083</citedby><cites>FETCH-LOGICAL-c373t-6f2f5d2426417e790a765f1aacadd4b4283ab3e692c85d391f44039c0bc013083</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://dx.doi.org/10.1016/j.ijimpeng.2006.05.009$$EHTML$$P50$$Gelsevier$$H</linktohtml><link.rule.ids>315,781,785,3551,27929,27930,46000</link.rule.ids><backlink>$$Uhttp://pascal-francis.inist.fr/vibad/index.php?action=getRecordDetail&idt=18606907$$DView record in Pascal Francis$$Hfree_for_read</backlink></links><search><creatorcontrib>Lemanski, S.L.</creatorcontrib><creatorcontrib>Nurick, G.N.</creatorcontrib><creatorcontrib>Langdon, G.S.</creatorcontrib><creatorcontrib>Simmons, M.C.</creatorcontrib><creatorcontrib>Cantwell, W.J.</creatorcontrib><creatorcontrib>Schleyer, G.K.</creatorcontrib><title>Behaviour of fibre metal laminates subjected to localised blast loading—Part II: Quantitative analysis</title><title>International journal of impact engineering</title><description>This two part paper examines the behaviour of fibre-metal laminates (FMLs) subjected to localised explosive blast loading. Part I presents the
experimental observations of diamond and cross-shaped back face deformation, as well as pitting, global displacement and ring-buckling of the front face are also discerned. Part II presents
quantitative analysis of the experimental data. When expressed in terms of non-dimensional parameters front and back face displacements fall within one plate thickness of a linear trend line. The threshold impulse for the onset of tearing is found to increase linearly with panel thickness.</description><subject>Blast loading</subject><subject>Buckling</subject><subject>Composite</subject><subject>Exact sciences and technology</subject><subject>Failure</subject><subject>Fibre-metal laminate</subject><subject>Fracture mechanics (crack, fatigue, damage...)</subject><subject>Fundamental areas of phenomenology (including applications)</subject><subject>Panel</subject><subject>Physics</subject><subject>Solid mechanics</subject><subject>Structural and continuum mechanics</subject><issn>0734-743X</issn><issn>1879-3509</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2007</creationdate><recordtype>article</recordtype><recordid>eNqFkMuKFDEUhoMo2La-gmSjuypPKlVJxZU6eGkYUEHBXTiVOplJUZc2STXMzofwCX0Sa-wRl64OP_wXzsfYUwGlAKFeDGUYwnSk-aqsAFQJTQlg7rGdaLUpZAPmPtuBlnWha_ntIXuU0gAgNDSwY9dv6BpPYVkjXzz3oYvEJ8o48hGnMGOmxNPaDeQy9TwvfFwcjiFtohsx5U1jH-arXz9-fsKY-eHwkn9ecc4hYw4n4jjjeJNCesweeBwTPbm7e_b13dsvFx-Ky4_vDxevLwsntcyF8pVv-qquVC00aQOoVeMFosO-r7u6aiV2kpSpXNv00ghf1yCNg86BkNDKPXt-7j3G5ftKKdspJEfjiDMta7KV0bqFDceeqbPRxSWlSN4eY5gw3lgB9hasHexfsPYWrIXGbmC34LO7BUwbCx9xdiH9S7cKlPkz8Orso-3dU6Bokws0O-pD3HDafgn_m_oNeA6UNg</recordid><startdate>20070701</startdate><enddate>20070701</enddate><creator>Lemanski, S.L.</creator><creator>Nurick, G.N.</creator><creator>Langdon, G.S.</creator><creator>Simmons, M.C.</creator><creator>Cantwell, W.J.</creator><creator>Schleyer, G.K.</creator><general>Elsevier Ltd</general><general>Elsevier Science</general><scope>IQODW</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>7SR</scope><scope>7TB</scope><scope>8BQ</scope><scope>8FD</scope><scope>FR3</scope><scope>JG9</scope><scope>KR7</scope></search><sort><creationdate>20070701</creationdate><title>Behaviour of fibre metal laminates subjected to localised blast loading—Part II: Quantitative analysis</title><author>Lemanski, S.L. ; Nurick, G.N. ; Langdon, G.S. ; Simmons, M.C. ; Cantwell, W.J. ; Schleyer, G.K.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c373t-6f2f5d2426417e790a765f1aacadd4b4283ab3e692c85d391f44039c0bc013083</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2007</creationdate><topic>Blast loading</topic><topic>Buckling</topic><topic>Composite</topic><topic>Exact sciences and technology</topic><topic>Failure</topic><topic>Fibre-metal laminate</topic><topic>Fracture mechanics (crack, fatigue, damage...)</topic><topic>Fundamental areas of phenomenology (including applications)</topic><topic>Panel</topic><topic>Physics</topic><topic>Solid mechanics</topic><topic>Structural and continuum mechanics</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Lemanski, S.L.</creatorcontrib><creatorcontrib>Nurick, G.N.</creatorcontrib><creatorcontrib>Langdon, G.S.</creatorcontrib><creatorcontrib>Simmons, M.C.</creatorcontrib><creatorcontrib>Cantwell, W.J.</creatorcontrib><creatorcontrib>Schleyer, G.K.</creatorcontrib><collection>Pascal-Francis</collection><collection>CrossRef</collection><collection>Engineered Materials Abstracts</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>METADEX</collection><collection>Technology Research Database</collection><collection>Engineering Research Database</collection><collection>Materials Research Database</collection><collection>Civil Engineering Abstracts</collection><jtitle>International journal of impact engineering</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Lemanski, S.L.</au><au>Nurick, G.N.</au><au>Langdon, G.S.</au><au>Simmons, M.C.</au><au>Cantwell, W.J.</au><au>Schleyer, G.K.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Behaviour of fibre metal laminates subjected to localised blast loading—Part II: Quantitative analysis</atitle><jtitle>International journal of impact engineering</jtitle><date>2007-07-01</date><risdate>2007</risdate><volume>34</volume><issue>7</issue><spage>1223</spage><epage>1245</epage><pages>1223-1245</pages><issn>0734-743X</issn><eissn>1879-3509</eissn><coden>IJIED4</coden><abstract>This two part paper examines the behaviour of fibre-metal laminates (FMLs) subjected to localised explosive blast loading. Part I presents the
experimental observations of diamond and cross-shaped back face deformation, as well as pitting, global displacement and ring-buckling of the front face are also discerned. Part II presents
quantitative analysis of the experimental data. When expressed in terms of non-dimensional parameters front and back face displacements fall within one plate thickness of a linear trend line. The threshold impulse for the onset of tearing is found to increase linearly with panel thickness.</abstract><cop>Oxford</cop><pub>Elsevier Ltd</pub><doi>10.1016/j.ijimpeng.2006.05.009</doi><tpages>23</tpages></addata></record> |
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| ispartof | International journal of impact engineering, 2007-07, Vol.34 (7), p.1223-1245 |
| issn | 0734-743X 1879-3509 |
| language | eng |
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| source | ScienceDirect Journals (5 years ago - present) |
| subjects | Blast loading Buckling Composite Exact sciences and technology Failure Fibre-metal laminate Fracture mechanics (crack, fatigue, damage...) Fundamental areas of phenomenology (including applications) Panel Physics Solid mechanics Structural and continuum mechanics |
| title | Behaviour of fibre metal laminates subjected to localised blast loading—Part II: Quantitative analysis |
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