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A damage zone model for the failure analysis of adhesively bonded joints
Authors:Andrew Sheppard  Don Kelly  Liyong Tong
Affiliation:

a Cooperative Research Centre for Advanced Composite Structures Ltd., 361 Milperra Road, P.O. Box 30 Bankstown, NSW 2200 Australia

b School of Mechanical and Manufacturing Engineering, University of New South Wales Sydney, N.S.W., 2051 Australia

c Department of Aeronautical Engineering, University of Sydney Sydney, N.S.W., 2006 Australia

Abstract:The design of structural adhesively bonded joints is complicated by the presence of singularities at the ends of the joint and the lack of suitable failure criteria. Literature reviews indicate that bonded joint failure typically occurs after a damage zone at the end of the joint reaches a critical size. In this paper, a damage zone model based on a critical damage zone size and strain-based failure criteria is proposed to predict the failure load of adhesively bonded joints. The proposed damage zone model correctly predicts the joint failure locus and appears to be relatively insensitive to finite element mesh refinement. Results from experimental testing of various composite and aluminium lap joints have been obtained and compared with numerical analysis. Initial numerical predictions indicate that by using the proposed damage zone model, good correlation with experimental results can be achieved. A modified version of the damage zone model is also proposed which allows the model to be implemented in a practical engineering analysis environment. It is concluded that the damage zone model can be successfully applied across a broad range of joint configurations and loading conditions.
Keywords:Bond strength (materials)   Adhesive joints   Mathematical models   Failure analysis   Composite structures   Finite element method   Stress analysis   Loads (forces)   Damage zone model   Adhesively bonded joints
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