Tapered laminates under static and fatigue tension loading
Static and tension–tension fatigue tests have been undertaken on carbon-fiber/epoxy specimens with tapered sections. The effects of the value of the slope angle, a delamination in the tapered section, and ageing have been investigated. The results of this study show that the stress amplitude of the...
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| Veröffentlicht in: | Composites science and technology 2002-03, Vol.62 (4), p.597-603 |
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| container_title | Composites science and technology |
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| creator | Meirinhos, G Rocker, J Cabanac, J-P Barrau, J.-J |
| description | Static and tension–tension fatigue tests have been undertaken on carbon-fiber/epoxy specimens with tapered sections. The effects of the value of the slope angle, a delamination in the tapered section, and ageing have been investigated. The results of this study show that the stress amplitude of the civil-aircraft fatigue spectrum does not create any damage in the tapered section and has no contribution to the propagation of delamination when 132 g/m
2 material is used, with maximum 20° tapered specimens. A static strength reduction is induced by ageing. No effect on duration is observed. A statistical analysis is made to fix, on a A-value or B-value basis, the relationship between fatigue stress, fatigue life and residual strength. |
| doi_str_mv | 10.1016/S0266-3538(01)00156-7 |
| format | Article |
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2 material is used, with maximum 20° tapered specimens. A static strength reduction is induced by ageing. No effect on duration is observed. A statistical analysis is made to fix, on a A-value or B-value basis, the relationship between fatigue stress, fatigue life and residual strength.</description><subject>A. Carbon fibers</subject><subject>Applied sciences</subject><subject>B. Fatigue</subject><subject>C. Delamination</subject><subject>C. Statistics</subject><subject>Exact sciences and technology</subject><subject>Forms of application and semi-finished materials</subject><subject>Laminates</subject><subject>Ply drop-off</subject><subject>Polymer industry, paints, wood</subject><subject>Technology of polymers</subject><issn>0266-3538</issn><issn>1879-1050</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2002</creationdate><recordtype>article</recordtype><recordid>eNqFkE1LxDAQhoMouK7-BKEXRQ_VSdN81IvI4hcseHA9hzSdLJFuuiat4L-36y569DRzeN55mYeQUwpXFKi4foVCiJxxpi6AXgJQLnK5RyZUySqnwGGfTH6RQ3KU0jsASF4VE3KzMGuM2GStWflgekzZEBqMWepN721mQpO5cVsOmPUYku9C1nam8WF5TA6caROe7OaUvD3cL2ZP-fzl8Xl2N88tE6rPKSuY5LVzBp1TtlTWlUw5J6zlpZGqNkyCRV5VEhk2tatxfKDkoATQQpRsSs63d9ex-xgw9Xrlk8W2NQG7IelCSlGMVSPIt6CNXUoRnV5HvzLxS1PQG1P6x5TeaNBA9Y8pLcfc2a7AJGtaF02wPv2FWVkJXsHI3W45HL_99Bh1sh6DxcZHtL1uOv9P0zfZqHz6</recordid><startdate>200203</startdate><enddate>200203</enddate><creator>Meirinhos, G</creator><creator>Rocker, J</creator><creator>Cabanac, J-P</creator><creator>Barrau, J.-J</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>200203</creationdate><title>Tapered laminates under static and fatigue tension loading</title><author>Meirinhos, G ; Rocker, J ; Cabanac, J-P ; Barrau, J.-J</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c368t-132375bffaeff8c48cf438ff6cc54a78ba370ce5997e3edbfbe15645086012643</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2002</creationdate><topic>A. Carbon fibers</topic><topic>Applied sciences</topic><topic>B. Fatigue</topic><topic>C. Delamination</topic><topic>C. Statistics</topic><topic>Exact sciences and technology</topic><topic>Forms of application and semi-finished materials</topic><topic>Laminates</topic><topic>Ply drop-off</topic><topic>Polymer industry, paints, wood</topic><topic>Technology of polymers</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Meirinhos, G</creatorcontrib><creatorcontrib>Rocker, J</creatorcontrib><creatorcontrib>Cabanac, J-P</creatorcontrib><creatorcontrib>Barrau, J.-J</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>Meirinhos, G</au><au>Rocker, J</au><au>Cabanac, J-P</au><au>Barrau, J.-J</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Tapered laminates under static and fatigue tension loading</atitle><jtitle>Composites science and technology</jtitle><date>2002-03</date><risdate>2002</risdate><volume>62</volume><issue>4</issue><spage>597</spage><epage>603</epage><pages>597-603</pages><issn>0266-3538</issn><eissn>1879-1050</eissn><coden>CSTCEH</coden><abstract>Static and tension–tension fatigue tests have been undertaken on carbon-fiber/epoxy specimens with tapered sections. The effects of the value of the slope angle, a delamination in the tapered section, and ageing have been investigated. The results of this study show that the stress amplitude of the civil-aircraft fatigue spectrum does not create any damage in the tapered section and has no contribution to the propagation of delamination when 132 g/m
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| ispartof | Composites science and technology, 2002-03, Vol.62 (4), p.597-603 |
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| language | eng |
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| source | Elsevier ScienceDirect Journals Complete - AutoHoldings |
| subjects | A. Carbon fibers Applied sciences B. Fatigue C. Delamination C. Statistics Exact sciences and technology Forms of application and semi-finished materials Laminates Ply drop-off Polymer industry, paints, wood Technology of polymers |
| title | Tapered laminates under static and fatigue tension loading |
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