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Fatigue damage development in new fibre metal laminates made by the VARTM process
ABSTRACT This paper investigates the tensile and fatigue properties of a newly developed fibre metal laminate (FML) manufactured using the vacuum assisted resin transfer moulding (VARTM) method. This manufacturing method allows the glass fibre reinforced epoxy and 2024‐T3 aluminium FML to be prepare...
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| Published in: | Fatigue & fracture of engineering materials & structures 2011-04, Vol.34 (4), p.240-249 |
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| Main Authors: | , , , , |
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| cited_by | cdi_FETCH-LOGICAL-c4249-b00588b8b24e6018a509b0adab6932e3c9203688e883dadf1cd69540b50d65b93 |
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| container_end_page | 249 |
| container_issue | 4 |
| container_start_page | 240 |
| container_title | Fatigue & fracture of engineering materials & structures |
| container_volume | 34 |
| creator | BAUMERT, E. K. JOHNSON, W. S. CANO, R. J. JENSEN, B. J. WEISER, E. S. |
| description | ABSTRACT
This paper investigates the tensile and fatigue properties of a newly developed fibre metal laminate (FML) manufactured using the vacuum assisted resin transfer moulding (VARTM) method. This manufacturing method allows the glass fibre reinforced epoxy and 2024‐T3 aluminium FML to be prepared at lower cost than conventionally manufactured FMLs. However, in order for the resin to infiltrate the FML, the metal sheets need to be perforated. These perforation holes act as crack initiators and reduce the FML's performance. Tension and fatigue test results of three different designs are reported and compared to mechanical property predictions. Additionally, single sheet Al alloy specimens were tested in order to analyse the influence of the drilling method. |
| doi_str_mv | 10.1111/j.1460-2695.2010.01509.x |
| format | article |
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This paper investigates the tensile and fatigue properties of a newly developed fibre metal laminate (FML) manufactured using the vacuum assisted resin transfer moulding (VARTM) method. This manufacturing method allows the glass fibre reinforced epoxy and 2024‐T3 aluminium FML to be prepared at lower cost than conventionally manufactured FMLs. However, in order for the resin to infiltrate the FML, the metal sheets need to be perforated. These perforation holes act as crack initiators and reduce the FML's performance. Tension and fatigue test results of three different designs are reported and compared to mechanical property predictions. Additionally, single sheet Al alloy specimens were tested in order to analyse the influence of the drilling method.</description><identifier>ISSN: 8756-758X</identifier><identifier>EISSN: 1460-2695</identifier><identifier>DOI: 10.1111/j.1460-2695.2010.01509.x</identifier><identifier>CODEN: FFESEY</identifier><language>eng</language><publisher>Oxford, UK: Blackwell Publishing Ltd</publisher><subject>Applied sciences ; Exact sciences and technology ; Fatigue ; Fatigue failure ; Fibre ; fibre metal laminate (FML) ; hybrid composite ; Laminates ; Materials fatigue ; Mechanical properties ; Mechanical properties and methods of testing. Rheology. Fracture mechanics. Tribology ; Metals. Metallurgy ; Resins ; tensile behaviour ; Tensile strength ; vacuum assisted resin transfer moulding (VARTM)</subject><ispartof>Fatigue & fracture of engineering materials & structures, 2011-04, Vol.34 (4), p.240-249</ispartof><rights>2010 Blackwell Publishing Ltd.</rights><rights>2015 INIST-CNRS</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c4249-b00588b8b24e6018a509b0adab6932e3c9203688e883dadf1cd69540b50d65b93</citedby></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,780,784,27924,27925</link.rule.ids><backlink>$$Uhttp://pascal-francis.inist.fr/vibad/index.php?action=getRecordDetail&idt=23932358$$DView record in Pascal Francis$$Hfree_for_read</backlink></links><search><creatorcontrib>BAUMERT, E. K.</creatorcontrib><creatorcontrib>JOHNSON, W. S.</creatorcontrib><creatorcontrib>CANO, R. J.</creatorcontrib><creatorcontrib>JENSEN, B. J.</creatorcontrib><creatorcontrib>WEISER, E. S.</creatorcontrib><title>Fatigue damage development in new fibre metal laminates made by the VARTM process</title><title>Fatigue & fracture of engineering materials & structures</title><description>ABSTRACT
This paper investigates the tensile and fatigue properties of a newly developed fibre metal laminate (FML) manufactured using the vacuum assisted resin transfer moulding (VARTM) method. This manufacturing method allows the glass fibre reinforced epoxy and 2024‐T3 aluminium FML to be prepared at lower cost than conventionally manufactured FMLs. However, in order for the resin to infiltrate the FML, the metal sheets need to be perforated. These perforation holes act as crack initiators and reduce the FML's performance. Tension and fatigue test results of three different designs are reported and compared to mechanical property predictions. Additionally, single sheet Al alloy specimens were tested in order to analyse the influence of the drilling method.</description><subject>Applied sciences</subject><subject>Exact sciences and technology</subject><subject>Fatigue</subject><subject>Fatigue failure</subject><subject>Fibre</subject><subject>fibre metal laminate (FML)</subject><subject>hybrid composite</subject><subject>Laminates</subject><subject>Materials fatigue</subject><subject>Mechanical properties</subject><subject>Mechanical properties and methods of testing. Rheology. Fracture mechanics. Tribology</subject><subject>Metals. Metallurgy</subject><subject>Resins</subject><subject>tensile behaviour</subject><subject>Tensile strength</subject><subject>vacuum assisted resin transfer moulding (VARTM)</subject><issn>8756-758X</issn><issn>1460-2695</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2011</creationdate><recordtype>article</recordtype><recordid>eNp9kU9vEzEQxS0EEqHwHSwkBJdN7fXaax84VKFpK0oraPkjLqPx7qQ47G7CekOTb4-XVDlwwJexPL83nqfHGJdiKtM5Xk5lYUSWG6enuUivQmrhpttHbHJoPGYTW2qTldp-e8qexbgUQppCqQn7OMch3G2I19jiXSr0m5rVuqVu4KHjHd3zRfA98ZYGbHiDbehwoMhbrIn7HR9-EP9y8un2A1_3q4pifM6eLLCJ9OKhHrHP89Pb2Xl2eX12MTu5zKoiL1zmhdDWeuvzgoyQFtPWXmCN3jiVk6pcLpSxlqxVNdYLWdXJSSG8FrXR3qkj9no_N_37a0NxgDbEipoGO1ptIljjbC6dLBP55r-kNKXUUjmpE_ryH3S52vRd8gFW61KVthjnvXqAMFbYLHrsqhBh3YcW-x3kKhlQ2ibu7Z67Dw3tDn0pYEwOljAGBGNAMCYHf5ODLcznp-Mt6bO9PsSBtgc99j_BpFU0fL06AytuZt9v3p_DO_UH0libFg</recordid><startdate>201104</startdate><enddate>201104</enddate><creator>BAUMERT, E. K.</creator><creator>JOHNSON, W. S.</creator><creator>CANO, R. J.</creator><creator>JENSEN, B. J.</creator><creator>WEISER, E. S.</creator><general>Blackwell Publishing Ltd</general><general>Blackwell</general><general>Wiley Subscription Services, Inc</general><scope>BSCLL</scope><scope>IQODW</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>201104</creationdate><title>Fatigue damage development in new fibre metal laminates made by the VARTM process</title><author>BAUMERT, E. K. ; JOHNSON, W. S. ; CANO, R. J. ; JENSEN, B. J. ; WEISER, E. 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K.</creatorcontrib><creatorcontrib>JOHNSON, W. S.</creatorcontrib><creatorcontrib>CANO, R. J.</creatorcontrib><creatorcontrib>JENSEN, B. J.</creatorcontrib><creatorcontrib>WEISER, E. S.</creatorcontrib><collection>Istex</collection><collection>Pascal-Francis</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>Fatigue & fracture of engineering materials & structures</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>BAUMERT, E. K.</au><au>JOHNSON, W. S.</au><au>CANO, R. J.</au><au>JENSEN, B. J.</au><au>WEISER, E. S.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Fatigue damage development in new fibre metal laminates made by the VARTM process</atitle><jtitle>Fatigue & fracture of engineering materials & structures</jtitle><date>2011-04</date><risdate>2011</risdate><volume>34</volume><issue>4</issue><spage>240</spage><epage>249</epage><pages>240-249</pages><issn>8756-758X</issn><eissn>1460-2695</eissn><coden>FFESEY</coden><abstract>ABSTRACT
This paper investigates the tensile and fatigue properties of a newly developed fibre metal laminate (FML) manufactured using the vacuum assisted resin transfer moulding (VARTM) method. This manufacturing method allows the glass fibre reinforced epoxy and 2024‐T3 aluminium FML to be prepared at lower cost than conventionally manufactured FMLs. However, in order for the resin to infiltrate the FML, the metal sheets need to be perforated. These perforation holes act as crack initiators and reduce the FML's performance. Tension and fatigue test results of three different designs are reported and compared to mechanical property predictions. Additionally, single sheet Al alloy specimens were tested in order to analyse the influence of the drilling method.</abstract><cop>Oxford, UK</cop><pub>Blackwell Publishing Ltd</pub><doi>10.1111/j.1460-2695.2010.01509.x</doi><tpages>10</tpages></addata></record> |
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| identifier | ISSN: 8756-758X |
| ispartof | Fatigue & fracture of engineering materials & structures, 2011-04, Vol.34 (4), p.240-249 |
| issn | 8756-758X 1460-2695 |
| language | eng |
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| source | Wiley-Blackwell Read & Publish Collection |
| subjects | Applied sciences Exact sciences and technology Fatigue Fatigue failure Fibre fibre metal laminate (FML) hybrid composite Laminates Materials fatigue Mechanical properties Mechanical properties and methods of testing. Rheology. Fracture mechanics. Tribology Metals. Metallurgy Resins tensile behaviour Tensile strength vacuum assisted resin transfer moulding (VARTM) |
| title | Fatigue damage development in new fibre metal laminates made by the VARTM process |
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