Vol. 7, No. 4, 2012

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ISSN: 1559-3959
Thereotical solutions of adhesive stresses in bonded composite butt joints

Gang Li

Vol. 7 (2012), No. 4, 323–346
Abstract

In this paper, closed-form solutions for the adhesive stresses in bonded composite single-strap butt joints have been obtained. Two strategies were used for deriving the adhesive peel stress. The solutions are applicable to a butt joint made from different adherend and doubler laminates, as well as the unbalanced single-lap joints. In addition, three-dimensional finite element models of the unit-width composite joints were created for analyzing the adhesive stresses under a plane strain condition. A total of six joint conditions, three joint configurations and each with two layup sequences, were studied. Consistency in the peel stress predictions was obtained from the two theoretical strategies. Good agreement has been achieved between the theoretical and finite element results. The effects of the doubler thickness and laminate layup sequence on the adhesive stress variation can be displayed. The theoretical solution would provide a solid foundation for supporting the practical composite joint assessment.

Keywords
adhesive stresses, closed-form solutions, composite single-strap butt joint, finite element analysis
Mathematical Subject Classification 2010
Primary: 00A05
Milestones
Received: 1 September 2011
Revised: 24 November 2011
Accepted: 13 January 2012
Published: 26 July 2012
Authors
Gang Li
Structures Group, Aerospace Portfolio
National Reseach Council Canada
M-3, 1200 Montreal Road
Ottawa ON K1A 0R6
Canada