Strength of CFRP open hole laminates made from NCF, TFP and braided preforms under cyclic tensile loading
Tensile tests and tension-tension cyclic tests were performed on carbon fibre reinforced plastics open-hole laminates. Specimens made from non-crimp fabric preforms, tailored fibre placement preforms and braided preforms in three different lay-up configurations ([+45] 8 s , [+45/0/−45] 6 s , [0/90]...
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| Veröffentlicht in: | Plastics, rubber & composites rubber & composites, 2010-07, Vol.39 (6), p.247-255 |
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| container_title | Plastics, rubber & composites |
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| creator | Uhlig, K. Spickenheuer, A. Gliesche, K. Karb, I. |
| description | Tensile tests and tension-tension cyclic tests were performed on carbon fibre reinforced plastics open-hole laminates. Specimens made from non-crimp fabric preforms, tailored fibre placement preforms and braided preforms in three different lay-up configurations ([+45]
8 s
, [+45/0/−45]
6 s
, [0/90]
8 s
) were investigated and compared. The laminates were manufactured using a vacuum assisted processing technology and Hexcel RTM6 epoxy resin. Tensile strength and residual tensile strength values were measured and compared with unnotched specimens in order to evaluate the notch sensitivity. To evaluate deterioration during cyclic testing a two-dimensional digital image correlation system was used to capture deformation images of the specimen surface in the open-hole area. Observed similarities and differences in deformation and in load-elongation graphs of the tested specimens are discussed. |
| doi_str_mv | 10.1179/174328910X12647080902772 |
| format | Article |
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8 s
, [+45/0/−45]
6 s
, [0/90]
8 s
) were investigated and compared. The laminates were manufactured using a vacuum assisted processing technology and Hexcel RTM6 epoxy resin. Tensile strength and residual tensile strength values were measured and compared with unnotched specimens in order to evaluate the notch sensitivity. To evaluate deterioration during cyclic testing a two-dimensional digital image correlation system was used to capture deformation images of the specimen surface in the open-hole area. Observed similarities and differences in deformation and in load-elongation graphs of the tested specimens are discussed.</description><identifier>ISSN: 1465-8011</identifier><identifier>EISSN: 1743-2898</identifier><identifier>DOI: 10.1179/174328910X12647080902772</identifier><language>eng</language><publisher>London, England: Taylor & Francis</publisher><subject>Applied sciences ; Braiding ; Carbon fiber reinforced plastics ; Deformation ; Exact sciences and technology ; Fiber placement ; Forms of application and semi-finished materials ; Laminates ; MATERIAL TESTING ; MECHANICAL PROPERTIES ; POLYMER COMPOSITE ; Polymer industry, paints, wood ; Preforms ; Technology of polymers ; Tensile strength</subject><ispartof>Plastics, rubber & composites, 2010-07, Vol.39 (6), p.247-255</ispartof><rights>2010 Maney Publishing 2010</rights><rights>2010 Maney Publishing</rights><rights>2015 INIST-CNRS</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c427t-8f9903e2bd5c584df03c641ab4d21030f4223e0f9143ccfb19f252c035e9b9ed3</citedby><cites>FETCH-LOGICAL-c427t-8f9903e2bd5c584df03c641ab4d21030f4223e0f9143ccfb19f252c035e9b9ed3</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://journals.sagepub.com/doi/pdf/10.1179/174328910X12647080902772$$EPDF$$P50$$Gsage$$H</linktopdf><linktohtml>$$Uhttps://journals.sagepub.com/doi/10.1179/174328910X12647080902772$$EHTML$$P50$$Gsage$$H</linktohtml><link.rule.ids>314,780,784,21817,27922,27923,43619,43620</link.rule.ids><backlink>$$Uhttp://pascal-francis.inist.fr/vibad/index.php?action=getRecordDetail&idt=22984182$$DView record in Pascal Francis$$Hfree_for_read</backlink></links><search><creatorcontrib>Uhlig, K.</creatorcontrib><creatorcontrib>Spickenheuer, A.</creatorcontrib><creatorcontrib>Gliesche, K.</creatorcontrib><creatorcontrib>Karb, I.</creatorcontrib><title>Strength of CFRP open hole laminates made from NCF, TFP and braided preforms under cyclic tensile loading</title><title>Plastics, rubber & composites</title><description>Tensile tests and tension-tension cyclic tests were performed on carbon fibre reinforced plastics open-hole laminates. Specimens made from non-crimp fabric preforms, tailored fibre placement preforms and braided preforms in three different lay-up configurations ([+45]
8 s
, [+45/0/−45]
6 s
, [0/90]
8 s
) were investigated and compared. The laminates were manufactured using a vacuum assisted processing technology and Hexcel RTM6 epoxy resin. Tensile strength and residual tensile strength values were measured and compared with unnotched specimens in order to evaluate the notch sensitivity. To evaluate deterioration during cyclic testing a two-dimensional digital image correlation system was used to capture deformation images of the specimen surface in the open-hole area. Observed similarities and differences in deformation and in load-elongation graphs of the tested specimens are discussed.</description><subject>Applied sciences</subject><subject>Braiding</subject><subject>Carbon fiber reinforced plastics</subject><subject>Deformation</subject><subject>Exact sciences and technology</subject><subject>Fiber placement</subject><subject>Forms of application and semi-finished materials</subject><subject>Laminates</subject><subject>MATERIAL TESTING</subject><subject>MECHANICAL PROPERTIES</subject><subject>POLYMER COMPOSITE</subject><subject>Polymer industry, paints, wood</subject><subject>Preforms</subject><subject>Technology of polymers</subject><subject>Tensile strength</subject><issn>1465-8011</issn><issn>1743-2898</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2010</creationdate><recordtype>article</recordtype><recordid>eNqNUMtq3DAUNaWBhjT_oE3ppm70siUtg-k0gdCEZALZGVm6mijI0lTyEObvYzOT7kq7uhfOi3OqChH8nRChLojgjEpF8BOhLRdYYoWpEPRDdbpA9YzJj_PP26aWmJBP1XkpfsBYNrhlSpxW_mHKEDfTM0oOdav7O5S2ENFzCoCCHn3UExQ0agvI5TSiX93qG1qv7pCOFg1ZewsWbTO4lMeCdtFCRmZvgjdoglj8YpO09XHzuTpxOhQ4P96z6nH1Y91d1Te3P6-7y5vacCqmWjqlMAM62MY0kluHmWk50QO3lGCGHaeUAXaKcGaMG4hytKEGswbUoMCys-rrwXeb0-8dlKkffTEQgo6QdqUXDWtbIqicmfLANDmVMnfot9mPOu97gvtl3_5v-87SL8cQXYwOLutofPmjp1RJTuTCaw68ojfQv6RdjnP3__HvDjofl2X1a8rB9pPeh5Tfw9g_Xd4AITKdVg</recordid><startdate>20100701</startdate><enddate>20100701</enddate><creator>Uhlig, K.</creator><creator>Spickenheuer, A.</creator><creator>Gliesche, K.</creator><creator>Karb, I.</creator><general>Taylor & Francis</general><general>SAGE Publications</general><general>Maney</general><scope>IQODW</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>7SR</scope><scope>8FD</scope><scope>JG9</scope></search><sort><creationdate>20100701</creationdate><title>Strength of CFRP open hole laminates made from NCF, TFP and braided preforms under cyclic tensile loading</title><author>Uhlig, K. ; Spickenheuer, A. ; Gliesche, K. ; Karb, I.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c427t-8f9903e2bd5c584df03c641ab4d21030f4223e0f9143ccfb19f252c035e9b9ed3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2010</creationdate><topic>Applied sciences</topic><topic>Braiding</topic><topic>Carbon fiber reinforced plastics</topic><topic>Deformation</topic><topic>Exact sciences and technology</topic><topic>Fiber placement</topic><topic>Forms of application and semi-finished materials</topic><topic>Laminates</topic><topic>MATERIAL TESTING</topic><topic>MECHANICAL PROPERTIES</topic><topic>POLYMER COMPOSITE</topic><topic>Polymer industry, paints, wood</topic><topic>Preforms</topic><topic>Technology of polymers</topic><topic>Tensile strength</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Uhlig, K.</creatorcontrib><creatorcontrib>Spickenheuer, A.</creatorcontrib><creatorcontrib>Gliesche, K.</creatorcontrib><creatorcontrib>Karb, I.</creatorcontrib><collection>Pascal-Francis</collection><collection>CrossRef</collection><collection>Engineered Materials Abstracts</collection><collection>Technology Research Database</collection><collection>Materials Research Database</collection><jtitle>Plastics, rubber & composites</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Uhlig, K.</au><au>Spickenheuer, A.</au><au>Gliesche, K.</au><au>Karb, I.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Strength of CFRP open hole laminates made from NCF, TFP and braided preforms under cyclic tensile loading</atitle><jtitle>Plastics, rubber & composites</jtitle><date>2010-07-01</date><risdate>2010</risdate><volume>39</volume><issue>6</issue><spage>247</spage><epage>255</epage><pages>247-255</pages><issn>1465-8011</issn><eissn>1743-2898</eissn><abstract>Tensile tests and tension-tension cyclic tests were performed on carbon fibre reinforced plastics open-hole laminates. Specimens made from non-crimp fabric preforms, tailored fibre placement preforms and braided preforms in three different lay-up configurations ([+45]
8 s
, [+45/0/−45]
6 s
, [0/90]
8 s
) were investigated and compared. The laminates were manufactured using a vacuum assisted processing technology and Hexcel RTM6 epoxy resin. Tensile strength and residual tensile strength values were measured and compared with unnotched specimens in order to evaluate the notch sensitivity. To evaluate deterioration during cyclic testing a two-dimensional digital image correlation system was used to capture deformation images of the specimen surface in the open-hole area. Observed similarities and differences in deformation and in load-elongation graphs of the tested specimens are discussed.</abstract><cop>London, England</cop><pub>Taylor & Francis</pub><doi>10.1179/174328910X12647080902772</doi><tpages>9</tpages></addata></record> |
| fulltext | fulltext |
| identifier | ISSN: 1465-8011 |
| ispartof | Plastics, rubber & composites, 2010-07, Vol.39 (6), p.247-255 |
| issn | 1465-8011 1743-2898 |
| language | eng |
| recordid | cdi_proquest_miscellaneous_753661728 |
| source | SAGE Complete |
| subjects | Applied sciences Braiding Carbon fiber reinforced plastics Deformation Exact sciences and technology Fiber placement Forms of application and semi-finished materials Laminates MATERIAL TESTING MECHANICAL PROPERTIES POLYMER COMPOSITE Polymer industry, paints, wood Preforms Technology of polymers Tensile strength |
| title | Strength of CFRP open hole laminates made from NCF, TFP and braided preforms under cyclic tensile loading |
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