2017
DOI: 10.1016/j.euromechsol.2017.07.011
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Two-dimensional analytical stress distribution model for unbalanced FRP composite single-lap joints

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Cited by 6 publications
(3 citation statements)
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“…In their study, they combined the use of Euler-Bernoulli/Timoshenko beams and the 2D elasticity theory, involving thus the three stress components (shear, peel and longitudinal stresses) which were supposed to vary along the thickness of the adhesive layer. Some of these authors [9,10] further analyzed the case of unbalanced composite SLJs and derived new expressions for the stress fields and edge moment factors, in the context of large deformations.…”
Section: Introductionmentioning
confidence: 99%
“…In their study, they combined the use of Euler-Bernoulli/Timoshenko beams and the 2D elasticity theory, involving thus the three stress components (shear, peel and longitudinal stresses) which were supposed to vary along the thickness of the adhesive layer. Some of these authors [9,10] further analyzed the case of unbalanced composite SLJs and derived new expressions for the stress fields and edge moment factors, in the context of large deformations.…”
Section: Introductionmentioning
confidence: 99%
“…Spring-type models are also widely used (Benveniste and Miloh, 2001;Geymonat et al, 1999;Goland and Reissner, 1944;Hashin, 2002;Klarbring, 1991). There is a wide literature exploiting beam theories in the analysis of adhesive joints (Ascione and Mancusi, 2012;Bennati et al, 2009;Cheng et al, 1991;Goland and Reissner, 1944;Jiang et al, 2017;Kanninen, 1974;Kondo, 1995;Luo and Tong, 2004;Olsson, 1992;Qiao and Wang, 2004;Su and Gao, 2014;Whitney, 1989;Williams, 1989;Wu and Jenson, 2011;Wu and Zhao, 2013;Zou et al, 2013), just to cite a few. Other studies focus on obtaining composite beam theories via a rigorous asymptotic analysis, see e.g.…”
Section: Introductionmentioning
confidence: 99%
“…Though the model is general and includes bending, shearing, hygrothermal stresses, and nonlinear adhesive behavior, the solution is calculated numerically and a closed-form solution is hard to obtain. Recently, Jiang et al [23] derived a solution for unbalanced composite double-lap joints but accounting for shear and peeling stresses. Weißgraeber et al [24] derived an analytical model for single-lap, double-lap, T, and L adhesive joints, considering plane-strain framework.…”
Section: Introductionmentioning
confidence: 99%