2012
DOI: 10.1007/s10704-012-9782-3
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An efficient BEM formulation for analysis of bond-line cracks in thin walled aircraft structures

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Cited by 8 publications
(6 citation statements)
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“…A number of studies on debonding strength have been made so far [14][15][16]. Naito investigated the geometrical effect of adhesive thickness on the tensile and shear strength for butt and single lap joints [5].…”
Section: Introductionmentioning
confidence: 99%
“…A number of studies on debonding strength have been made so far [14][15][16]. Naito investigated the geometrical effect of adhesive thickness on the tensile and shear strength for butt and single lap joints [5].…”
Section: Introductionmentioning
confidence: 99%
“…When dealing with weakly singular integrals with singularities of the order ln(1/r) or 1/r such as those seen in equations ( 2)-( 4), ( 8), ( 9), ( 12)-( 13), (16), the transformation of variable technique proposed by Telles [28] is used. For equations (2) and (12), rigid body motion is also applied. The strongly singular integrals with singularities of the order of 1/r 2 seen in equations ( 7) and ( 15) only become singular when both the collocation node and the field point are on a crack surface.…”
Section: Dbem For Plate Bending Problemsmentioning
confidence: 99%
“…Reissner theory is used instead of Kirchoff theory since it is able to obtain crack tip stress fields that show better agreement to those provided by 3D elasticity [8]. The approach outlined in [7] has since been adapted to a wide range of problems, the most relevant of which include: the analysis of cracks in structures undergoing large deflection [9], dynamic fracture mechanics [10], fatigue crack growth in assembled plate structures [11], and the analysis of bond-line cracks in laminated plates [12]. Among the different Boundary Element methods used to solve problems involving fracture mechanics with Reissner plates, the DBEM is the most commonly used.…”
Section: Introductionmentioning
confidence: 99%
“…However, different materials properties cause singular stress at the end of the interface, which may lead to failure of bonding portions in structures. Several problems on debonding strength have been studied recently [1][2][3]. By using butt and single lap joints, the study showed that the tensile strength of the butt joints decreased as adhesive thickness increases while the shear strength did not affected by the adhesive thickness of single lap joints [4].…”
Section: Introductionmentioning
confidence: 99%