Experimental Study On Fracture Property Of Tapered Double Cantilever Beam Specimen With Aluminum Foam

It is indispensable to evaluate fracture energy as the bonding strength of adhesive at composite material with aluminum foam. This specimen is designed with tapered double cantilever beam by British standards (BS 7991 and ISO 11343). 4 kinds of specimens due to m values of 2, 2.5, 3 and 3.5 are manu...

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Main Authors: Kim Y.C., Kim S.S., Cho J.U.
Format: Article
Language:English
Published: Polish Academy of Sciences 2015-06-01
Series:Archives of Metallurgy and Materials
Subjects:
Online Access:http://www.degruyter.com/view/j/amm.2015.60.issue-2/amm-2015-0153/amm-2015-0153.xml?format=INT
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spelling doaj-f1fc5bd3f6d7448e9e61657a51f203722020-11-25T03:48:10ZengPolish Academy of SciencesArchives of Metallurgy and Materials2300-19092015-06-016021459146210.1515/amm-2015-0153amm-2015-0153Experimental Study On Fracture Property Of Tapered Double Cantilever Beam Specimen With Aluminum FoamKim Y.C.0Kim S.S.1Cho J.U.2 DIVISION OF MECHANICAL DIVISION OF MECHANICAL DIVISION OF MECHANICAL It is indispensable to evaluate fracture energy as the bonding strength of adhesive at composite material with aluminum foam. This specimen is designed with tapered double cantilever beam by British standards (BS 7991 and ISO 11343). 4 kinds of specimens due to m values of 2, 2.5, 3 and 3.5 are manufactured and compared each other with the experimental results. Adhesive fracture energy is calculated from the formulae of British standards. The value of m is the gradient which is denoted as the length and the height of specimen. As m becomes greater at static experimental result, the maximum load becomes higher and the displacement becomes lower. And the critical fracture energy becomes higher. As m becomes less at fatigue experimental result, the displacement becomes higher and the critical fracture energy becomes higher. Fracture behavior of adhesive can be analyzed by this study and these experimental results can be applied into real field effectively. The stability on TDCB structure bonded with aluminum foam composite can be predicted by use of this experimental result. Adhesive fracture energy is calculated from the formulae of British standards. Based on correlations obtained in this study, the fracture behavior of bonded material would possibly be analyzed and aluminum foam material bonded with adhesive would be applied to a composite structure in various fields, thereby analyzing the mechanical and fracture characteristic of the material.http://www.degruyter.com/view/j/amm.2015.60.issue-2/amm-2015-0153/amm-2015-0153.xml?format=INTAluminum foamTapered double cantilever beam (TDCB)Fracture behaviorAdhesively bonded structuresAdhesive fracture energy
collection DOAJ
language English
format Article
sources DOAJ
author Kim Y.C.
Kim S.S.
Cho J.U.
spellingShingle Kim Y.C.
Kim S.S.
Cho J.U.
Experimental Study On Fracture Property Of Tapered Double Cantilever Beam Specimen With Aluminum Foam
Archives of Metallurgy and Materials
Aluminum foam
Tapered double cantilever beam (TDCB)
Fracture behavior
Adhesively bonded structures
Adhesive fracture energy
author_facet Kim Y.C.
Kim S.S.
Cho J.U.
author_sort Kim Y.C.
title Experimental Study On Fracture Property Of Tapered Double Cantilever Beam Specimen With Aluminum Foam
title_short Experimental Study On Fracture Property Of Tapered Double Cantilever Beam Specimen With Aluminum Foam
title_full Experimental Study On Fracture Property Of Tapered Double Cantilever Beam Specimen With Aluminum Foam
title_fullStr Experimental Study On Fracture Property Of Tapered Double Cantilever Beam Specimen With Aluminum Foam
title_full_unstemmed Experimental Study On Fracture Property Of Tapered Double Cantilever Beam Specimen With Aluminum Foam
title_sort experimental study on fracture property of tapered double cantilever beam specimen with aluminum foam
publisher Polish Academy of Sciences
series Archives of Metallurgy and Materials
issn 2300-1909
publishDate 2015-06-01
description It is indispensable to evaluate fracture energy as the bonding strength of adhesive at composite material with aluminum foam. This specimen is designed with tapered double cantilever beam by British standards (BS 7991 and ISO 11343). 4 kinds of specimens due to m values of 2, 2.5, 3 and 3.5 are manufactured and compared each other with the experimental results. Adhesive fracture energy is calculated from the formulae of British standards. The value of m is the gradient which is denoted as the length and the height of specimen. As m becomes greater at static experimental result, the maximum load becomes higher and the displacement becomes lower. And the critical fracture energy becomes higher. As m becomes less at fatigue experimental result, the displacement becomes higher and the critical fracture energy becomes higher. Fracture behavior of adhesive can be analyzed by this study and these experimental results can be applied into real field effectively. The stability on TDCB structure bonded with aluminum foam composite can be predicted by use of this experimental result. Adhesive fracture energy is calculated from the formulae of British standards. Based on correlations obtained in this study, the fracture behavior of bonded material would possibly be analyzed and aluminum foam material bonded with adhesive would be applied to a composite structure in various fields, thereby analyzing the mechanical and fracture characteristic of the material.
topic Aluminum foam
Tapered double cantilever beam (TDCB)
Fracture behavior
Adhesively bonded structures
Adhesive fracture energy
url http://www.degruyter.com/view/j/amm.2015.60.issue-2/amm-2015-0153/amm-2015-0153.xml?format=INT
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AT kimss experimentalstudyonfracturepropertyoftapereddoublecantileverbeamspecimenwithaluminumfoam
AT choju experimentalstudyonfracturepropertyoftapereddoublecantileverbeamspecimenwithaluminumfoam
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