Abstract:Anti-plane interaction of an elliptically cylindrical layered media with an arbitrarily oriented crack embedded in an infinite matrix, intermediate layer, or inner inclusion under a remote uniform shear load is considered in this paper. Based on the technique of conformal mapping and the method of analytical continuation in conjunction with the alternating technique, the solution for a screw dislocation in the inclusions and the matrix is first derived in a series form. The integral equations with logarithmic … Show more
“…where, Meanwhile, the complex potential functions of the other case in which the screw dislocation is located in core inclusion can be expressed in Equation 5 where recurrence formula for Θn(z) is expressed in Equation 6 and Equation 7. A crack can be modeled by place a dislocation distribution along the prospective site of the crack.…”
Section: Solution Proceduresmentioning
confidence: 99%
“…The merit of this technique is that allows us to easily deal with the interface continuity conditions of multi-layered composites. The studies that has been done using those techiques including an anti-plane crack interacting with reinforced elliptic hole [6], elliptically layered media [7], eccentric circular inclusion [8], and tri-material media [9]. To our knowledge, an anti-plane crack interacting with multi layered circular media has not been recorded in the literature.…”
Interaction between an anti-plane crack with a three-phase circular composite by using complex potential methods is considered in this paper. The solution procedures for solving this problem consist of two parts. In the first part, based on complex potential methods in conjunction with analytical continuation theorem and alternating technique, the complex potential functions of a screw dislocation interacting with three-phase circular composites are obtained. The second part consists of the derivation of logarithmic singular integral equations by introducing the complex potential functions of screw dislocation along the crack border together with superposition technique. The logarithmic singular integral equations is then solved numerically by modeling a crack in place of several segments. Linear interpolation formulae with undetermined coefficients are applied to approximate the dislocation distribution along the elements, except at vicinity of crack tip where the dislocation distribution preserves a square-root singularity. The mode-III stress intensity factors are then obtained numerically in terms of the values of the dislocation density functions of the logarithmic singular integral equations.
“…where, Meanwhile, the complex potential functions of the other case in which the screw dislocation is located in core inclusion can be expressed in Equation 5 where recurrence formula for Θn(z) is expressed in Equation 6 and Equation 7. A crack can be modeled by place a dislocation distribution along the prospective site of the crack.…”
Section: Solution Proceduresmentioning
confidence: 99%
“…The merit of this technique is that allows us to easily deal with the interface continuity conditions of multi-layered composites. The studies that has been done using those techiques including an anti-plane crack interacting with reinforced elliptic hole [6], elliptically layered media [7], eccentric circular inclusion [8], and tri-material media [9]. To our knowledge, an anti-plane crack interacting with multi layered circular media has not been recorded in the literature.…”
Interaction between an anti-plane crack with a three-phase circular composite by using complex potential methods is considered in this paper. The solution procedures for solving this problem consist of two parts. In the first part, based on complex potential methods in conjunction with analytical continuation theorem and alternating technique, the complex potential functions of a screw dislocation interacting with three-phase circular composites are obtained. The second part consists of the derivation of logarithmic singular integral equations by introducing the complex potential functions of screw dislocation along the crack border together with superposition technique. The logarithmic singular integral equations is then solved numerically by modeling a crack in place of several segments. Linear interpolation formulae with undetermined coefficients are applied to approximate the dislocation distribution along the elements, except at vicinity of crack tip where the dislocation distribution preserves a square-root singularity. The mode-III stress intensity factors are then obtained numerically in terms of the values of the dislocation density functions of the logarithmic singular integral equations.
“…Chen et al developed a multilayer hybrid-stress finite element model together with two types of composite multilayer elements to analyze the influence of various crack parameters (position, length, thickness and fiber orientation) on the estimation of SIFs of composite laminates [4]. Different boundary element methods were applied by a number of researchers (e.g., Miyazaki et al [5], Lu et al [6], Lu and Cheng [7], Chao and Wikarta [8] and Chao and Lu [9]) to analyze two-dimensional crack problems including biomaterial interface crack problems, dynamic propagation problem concerning Mode I crack, Asymmetrical dynamic propagation problem concerning Mode III crack, layered structures, respectively. Giner et al proposed an Extended Finite Element Method (X-FEM) for the numerical analysis of crack problems and implemented it in the finite element code Abaqus [10].…”
A new approach for the analysis of stress intensity factors (SIFs) for cracked plane plate is proposed based on the wavelet finite element method using the scaling functions of B-spline wavelet on the interval (BSWI). The performance of the method is investigated through the comparison of the results with the available numerical examples in the literate. It is shown that the solution quality is much better than that of the traditional adaptive finite element method. Though the method is applied to plane structures in this paper, it can be extended to solving problems for other classes of structures.
“…Indeed, a number of investigations concerning the crack problem in multi-layered composite have appeared in the literature, these include the work of [4][5]. However, the aforementioned works focused on problems with elliptic and straight boundaries.…”
In this study, the interaction between a coated circular inclusion with an anti-plane crack located in matrix is considered. The solution procedures for solving this problem consist of two parts. In the first part, based on the method of analytical continuation in conjunction with the alternating technique, the complex potential functions of screw dislocation interacting with multi-layered composites are obtained. The second part consists of the derivation of logarithmic singular integral equations by introducing the complex potential functions of screw dislocation along the crack border together with superposition technique. The logarithmic singular integral equations is the solved numerically by modeling a crack in place of several segments. Linear interpolation formulae with undetermined coefficients are applied to approximate the dislocation distribution along the elements, except at vicinity of crack tip where the dislocation distribution preserves a square-root singularity. The stress intensity factors are then obtained numerically in terms of the values of the dislocation density functions of the logarithmic singular integral equations.
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