各向异性复合材料的混合模应力奇异性

W. Yin
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引用次数: 1

摘要

由全各向异性弹性扇区组成的多材料楔块通常表现出反平面和内平面变形模式的内在耦合。每个各向异性扇区都有三个材料特征解的复共轭对,其表达形式取决于五种不同类型的各向异性材料。扇形界面上位移和牵引力的连续性以及两个外边界上无牵引力的条件决定了多材料楔块的特征值和特征解的无穷序列。这些特征解被线性组合以匹配环绕奇点的圆形路径上的牵引边界数据(由结构的全局有限元分析生成)。该分析方法适用于四层角层复合材料自由边缘附近的双材料楔块,以及三层复合材料中嵌入斜裂纹尖端周围的三材料楔块。在均匀温度载荷下,基于本征级数的弹性解产生的界面应力与渐近解(由本征级数的第一项给出)显著不同,即使距离奇点减小到亚原子尺度。以前在各向同性和正交异性多材料楔中也发现了类似的观察结果。这就提出了一个严重的问题,即仅仅根据渐近解和相关的应力强度因子或广义应力强度因子来表征应力奇点的临界性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Mixed Mode Stress Singularities in Anisotropic Composites
Multi-material wedges composed of fully anisotropic elastic sectors generally show intrinsic coupling of the anti-plane and in-plane modes of deformation. Each anisotropic sector has three complex conjugate pairs of material eigensolutions whose form of expression depends on five distinct types of anisotropic materials. Continuity of the displacements and the tractions across the sector interfaces and the traction-free conditions on two exterior boundary edges determine an infinite sequence of eigenvalues and eigensolutions of the multi-material wedge. These eigensolutions are linearly combined to match the traction-boundary data (generated by global finite element analysis of the structure) on a circular path encircling the singularity. The analysis method is applied to a bimaterial wedge near the free edge of a four-layer angle-ply laminate, and to a trimaterial wedge surrounding the tip of an embedded oblique crack in a three-layer composite. Under a uniform temperature load, the elasticity solution based on the eigenseries yields interfacial stresses that are significantly different from the asymptotic solution (given by the first term of the eigenseries), even as the distance from the singularity decreases to subatomic scales. Similar observations have been found previously for isotropic and orthotropic multi-material wedges. This raises serious questions with regard to characterizing the criticality of stress singularity exclusively in terms of the asymptotic solution and the associated stress intensity factors or generalized stress intensity factors.
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