Overview
FrançaisABSTRACT
The single-lap joint under tensile load is widely spread in the industry to assess the adhesive bonding strength, due to its simple manufacturing process. However, its stress analysis is not so simple. For more than one century, simplified stress analyses have been developed to represent for the physical reality at global and local scales as close as possible and at low computational costs. This article presents the closed-form ready-to-use solutions mostly spread in the literature and aims at showing the difficulties encountered while refining the models.
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Read the articleAUTHORS
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Éric PAROISSIEN: Professor at the Institut Supérieur et de l'Aéronautique et de l'Espace (ISAE-SUPAERO) - Institut Clément Ader (ICA), University of Toulouse, ISAE-SUPAERO, INSA, IMT MINES ALBI, UTIII, CNRS
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Sébastien SCHWARTZ: Associate Professor at the Institut supérieur et de l'aéronautique et de l'espace (ISAE-SUPAERO) - Institut Clément Ader (ICA), University of Toulouse, ISAE-SUPAERO, INSA, IMT MINES ALBI, UTIII, CNRS
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Frédéric LACHAUD: Professor at the Institut Supérieur et de l'Aéronautique et de l'Espace (ISAE-SUPAERO) - Institut Clément Ader (ICA), University of Toulouse, ISAE-SUPAERO, INSA, IMT MINES ALBI, UTIII, CNRS
INTRODUCTION
The design of structural glued joints is a complex and open subject. There is currently no standard for the design of structural glued joints. A dimensioning approach is generally based on the comparison of a calculated criterion with a measured admissible criterion. Mechanical strength criteria can be defined theoretically and/or experimentally, and include safety factors derived from in-service experience. Their determination depends on the bonding system – defined by the combination of an adhesive, the prepared substrates and the manufacturing process –, the desired design strategy and requirements, and the properties of the adhesive used in the confined layer. The dimensioning approach therefore requires the definition of experimental characterization methodologies associated with calculation methodologies, dependent in particular on the modeling of characterized material behaviors.
This article deals with the adhesive bonding of two slender, flat structures, i.e. the bonded connection in simple shear, under quasi-static loading, possibly combined with uniform temperature variation. This type of structure can be found, for example, in the transportation (automotive, rail, naval, aerospace), energy or civil construction industries. Single-shear adhesive bonding is also widely used industrially to assess the mechanical performance of adhesive bonding. The aim here is to give the analytical solutions and associated hypotheses available in the literature, describing the stress distribution in the adhesive layer. Their limitations are also described and explained, while approaches based on semi-analytical resolution schemes are presented as alternative solutions. It is not the intention of this article to provide a design methodology for structural glued joints.
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KEYWORDS
load transfer | single lap shear | elastic foundation | simplified modeling | closed-form solutions
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Aerospace systems
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Analytical solutions for single-shear bonded joints
Bibliography
Standards and norms
- Adhesives – Determination of the tensile shear strength of single-lap adhesive joints. - NF EN 1465 - 2009
- Adhesives – Determination of shear behaviour of structural adhesives – Part 2 : Tensile test method using thick adherends. - ISO 11003-2 - 2019
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