Analysis of the mechanical behaviour of adhesively bonded assemblies of composites under tensile-shear out-of-plane loads

被引：7

作者：

Sohier, L. ^{[1
]}

Cognard, J. Y. ^{[2
]}

Davies, P. ^{[3
]}

机构：

[1] Univ Brest, ENSTA Bretagne, Lab Brestois Mecan & Syst, ENIB,UEB, F-29285 Brest, France

[2] Univ Brest, ENSTA Bretagne, Lab Brestois Mecan & Syst, ENIB,UEB, F-29285 Brest, France

[3] IFREMER, Ctr Brest, Mat & Struct Grp, F-29280 Plouzane, France

来源：

COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING | 2013年 / 53卷

关键词：

Laminates; Adhesion; Stress concentrations; Mechanical testing; JOINTS; STRENGTH; STRESSES; FAILURE; REPAIR;

D O I：

10.1016/j.compositesa.2013.05.008

中图分类号：

T [工业技术];

学科分类号：

08 ;

摘要：

The use of composite materials is a key element in energy reduction strategies, particularly in all areas of transportation. The study of the behaviour of assemblies of composites, including bonded assemblies, is of great importance. Complex 3D loadings are needed to analyse the response of both the assemblies and the composites. However, few experimental devices allow out-of-plane loading to be studied, except by using thick composite specimens which are not always representative of industrial applications. This paper presents some possibilities of an experimental device, using a modified Arcan test, and optimized hybrid bonded assemblies, which limit the influence of edge effects. The influence of some design parameters are presented in the case of naval composites, they underline the possibilities of the proposed strategy. The failure envelope curves in the normal stress tangential stress plane for proportional monotonic out-of-plane loadings are presented in the case of a bonded assembly for different composites. (C) 2013 Published by Elsevier Ltd.

引用

页码：65 / 74

页数：10

共 30 条

[1] On non-linear thermal stresses in an adhesively bonded single lap joint [J].

Apalak, MK ;

Gunes, R .

COMPUTERS & STRUCTURES, 2002, 80 (01) :85-98

[2] METHOD TO PRODUCE UNIFORM PLANE-STRESS STATES WITH APPLICATIONS TO FIBER-REINFORCED MATERIALS [J].

ARCAN, M ;

HASHIN, Z ;

VOLOSHIN, A .

EXPERIMENTAL MECHANICS, 1978, 18 (04) :141-146

[3]

ASTM International, 2004, COMP MAT HDB MIL17, V1

[4] Out-of-plane singular stress fields in V-notched plates and welded lap joints induced by in-plane shear load conditions [J].

Berto, F. ;

Lazzarin, P. ;

Kotousov, A. ;

Harding, S. .

FATIGUE & FRACTURE OF ENGINEERING MATERIALS & STRUCTURES, 2011, 34 (04) :291-304

[5] Buckling strength of adhesively-bonded single and double-strap repairs on carbon-epoxy structures [J].

Campilho, R. D. S. G. ;

de Moura, M. F. S. F. ;

Ramantani, D. A. ;

Morais, J. J. L. ;

Domingues, J. J. M. S. .

COMPOSITES SCIENCE AND TECHNOLOGY, 2010, 70 (02) :371-379

[6] Determining the elastic interlaminar shear modulus of composite laminates [J].

Chan, A. ;

Chiu, W. K. ;

Liu, X. L. .

COMPOSITE STRUCTURES, 2007, 80 (03) :396-408

[7] A study of the non-linear behaviour of adhesively-bonded composite assemblies [J].

Cognard, J. Y. ;

Davies, P. ;

Sohier, L. ;

Creac'hcadec, R. .

COMPOSITE STRUCTURES, 2006, 76 (1-2) :34-46

[8] Numerical analysis of the stress distribution in single-lap shear tests under elastic assumption-Application to the optimisation of the mechanical behaviour [J].

Cognard, J. Y. ;

Creac'hcadec, R. ;

Maurice, J. .

INTERNATIONAL JOURNAL OF ADHESION AND ADHESIVES, 2011, 31 (07) :715-724

[9] A modified Arcan test to analyze the behavior of composites and their assemblies under out-of-plane loadings [J].

Cognard, J. Y. ;

Sohier, L. ;

Davies, P. .

COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2011, 42 (01) :111-121

[10]

da Silva LFM, 2011, HYBRID AHESIVE JOINT

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