非奇异应力对中央含V形切口试样断裂性能的影响

采用Williams渐近展开式表达V形切口尖端附近区域的位移场和应力场,将其代入弹性力学基本方程中,应力奇异性指数及其对应的位移和应力角函数由求解常微分方程组获得。由于在远离切口尖端的区域无应力奇异性,将切口尖端应力奇异性区域移出后,应用边界元法分析无应力奇异性的剩余结构;将Williams渐近展开式与弹性力学边界积分方程结合,解出切口尖端附近应力奇异性区域的各应力场渐近展开项系数,从而获得切口尖端附近区域的完整应力场;基于此,研究了非奇异应力项对中央含V形切口试样的表观断裂韧度和临界荷载预测值的影响。结果表明:考虑非奇异应力项时,脆性断裂的表观断裂韧度和临界荷载的预测值要比忽略非奇异应力项时的预测值更接近实验值。     

各向同性与各向异性三相材料接头应力奇异性研究

研究了各向同性与各向异性三相材料接头的应力奇性指数,通过引入奇异点附近区域位移场渐近展开的典型项,将各向同性与各向异性组合材料接头的控制方程和径向边界条件转化为变系数常微分方程的特征值问题;再利用插值矩阵法求解所建立的特征方程,得到接头端部的应力奇性指数和特征角函数。对由两个各向异性材料和一个各向同性材料以任意楔形角组成的三相接头结构的奇异性进行了研究,并比较了它们的应力奇性指数。计算结果表明:对于粘结接头,各向同性材料刚度越大应力奇异性越强;对于剥离接头,各向同性材料楔形角或材料刚度越大,第一阶应力奇异性越弱。计算结果与已有文献的结果对比吻合良好,证明了本文方法的有效性。     

垂直于界面V型缺口尖端的应力奇异性及其应用

基于双材料垂直于界面V型缺口理论,给出了单一材料和双材料裂纹问题、V型缺口问题应力强度因子的统一定义,得到了应力外推法计算双材料K_I的公式,数值算例验证了本文方法的有效性.以双材料单向拉伸和三点弯曲模型为对象,深入研究了双材料中弹性模量、泊松比、缺口深度、缺口张角对缺口尖端奇异应力场的影响,获得了一定范围内各种参数变化对缺口尖端奇异应力场的影响规律,为异体材料形成的V型缺口在应力断料中的应用提供了必要的参考依据.     

压电材料三维V形切口端部力电耦合奇异场分析

对于压电材料元器件,往往由于裂纹/切口而导致结构存在应力奇异性和电奇异性的现象。本文主要研究压电材料在力电耦合情形下的三维柱向V形切口问题。针对压电材料,结合Maxwell方程和Williams渐近展开式,推导并建立了三维柱向V形切口在力电耦合情形下的特征微分方程组,并采用插值矩阵法获得了其在不同边界条件下的奇性指数,算例表明,本文方法具有良好的计算精度。本文方法也适用于裂纹尖端的奇异性分析,且具有程序操作方便,前处理工作量小等优点。     

纤维与基体的轴对称界面端附近的奇异应力场

基于各向性弹性力学空间轴对称问题的基本方程,研究了纤维与基体的轴对称界面端的应力奇异性,并给出了界最佳 近的奇异应力场。研究结果表明,该轴对称界面端的应力奇异性与平面应变状态下相应模型的应力奇异性完全相同,材料对界面端附近奇异应力场的影响可用丰个双材料组合参数描述。     

纤维端部的界面裂纹分析

基于弹性力学空间轴对称问题的通解,研究了短纤维增强复合材料中纤维端部的轴对称币形和柱形界面裂纹尖端的应力奇异性,得到了裂纹尖端附近的奇异应力场．研究结果表明,这两种轴对称界面裂纹尖端的应力奇异性相同,并且与平面应变状态下相应模型的应力奇异性一致,材料性能对裂纹尖端附近奇异应力场的影响可用三个组合参数描述     

橡胶楔体与刚性缺口接触大变形分析

利用Ｋｕｏｗｌｅｓ与Ｓｔｅｒｎｂｅｒｇ提出的非线性弹性大变形应变能函数,对橡胶楔体与刚性缺口接触问题进行大变形渐近分析,推导了楔体尖端场的渐近方程,得到楔体尖端附近的应力应变场及应力的奇异性指数与橡胶楔体角度、刚性缺口角度及材料常数有关的表达式;楔尖附近同一半径上应力分量为常数,同时,利用非线性有限元理论编制了大变形有限元程序,考虑楔体尖端与缺口接触边界条件,计算得到了与分析解一致的结论,当缺口角     

含裂纹简支梁在均布荷载作用下的内聚区模型解析函数

对于含切口简支梁受均布荷载作用的问题,基于Williams应力函数,通过边界配置法并借用无裂纹体应力边界条件,求得了含高阶项的全场解析解及相应的应力强度因子K_Ⅰ。基于"Duan and Nakagawa’s"模型,通过对首项(奇异项)进行加权积分,消除了裂缝尖端应力呈无穷大的奇异性,得到了内聚区模型的全场解析解。通过对不同解法下典型截面正应力分布的比较,表明内聚区模型解消除了裂缝尖端应力的奇异性,比函数叠加法的结果精度更高,这样的数学力学模型可以从宏观上反映混凝土类材料的断裂特性。     

具有翼形、唇形缺陷的薄板的弯曲问题

薄板,是工程结构中的重要部件之一。研究薄板在弯曲载荷作用下,缺陷尖端附近的应力场和应力强度因子,不仅有理论意义,而且具有一定的实用价值。1952年Williams对拉伸载荷下,板中缺陷角点处的应力奇异性作了定性的讨论,并指出薄板弯曲时,角点附近具有类似的奇异性。1961年,Williams利用特征值展开方法详细导出了弯曲时直线裂纹尖端的应力表达式。与拉伸情况相同,尖端附近     

正交异性材料V型切口反对称变形下的尖端场

基于正交各向异性材料弹性平面问题的通解,导出了正交各向异性材料奇异点附近的位移场和奇异应力场的解析表达式,由此给出了反对称变形模态下V型切口尖端附近的位移场和奇异应力场的解析解,通过算例难证,解析解与有限元解吻合得非常好.研究结果表明,正交各向异性材料V型切口尖端附近的应力奇异性不仅与切口的张角有关,还与材料的弹性常数有关.     

The expression of stress and strain at the tip of three-dimensional notch

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复合材料切口应力奇性指数计算

提出一种计算广义平面应交状态下复合材料切口应力奇性指数的新方法.在切口尖端的位移幂级数渐近展开式被引入正交各向异性材料的物理方程后,将用位移表示的应力分量代入切口端部柱状邻域的线弹性理论控制方程,切口应力奇性指数的计算被转化为常微分方程组特征值的求解.采用插值矩阵法求解该常微分方程组,可一次性地获取切口尖端多阶应力奇性指数.本法适合平面和反平面应力场耦合或解耦的情形,并可退化计算裂纹或各向同性材料切口的应力奇性指数.算例表明,所提方法对分析复合材料切口应力奇性指数是一种准确有效的手段.     

Stress singularities for three-dimensional corners using the boundary integral equation method

The boundary integral equation method is developed to study three-dimensional asymptotic singular stress fields at vertices of a pyramidal notch or inclusion in an isotropic elastic space. Two-dimensional boundary integral equations are used for the infinite body with pyramidal notches and inclusions when either stresses or displacements are specified on its surface. Applying the Mellin integral transformation reduces the problem to one-dimensional singular integral equations over a closed, piece-wise smooth line. Using quadrature formulas for regular and singular integrals with Hilbert and logarithmic kernels, these integral equations are reduced to a homogeneous system of linear algebraic equations. Setting its determinant to zero provides a characteristic equation for the determination of the stress singularity power. Numerical results are obtained and compared against known eigenvalues from the literature for an infinite region with a conical notch or inclusion, for a Fichera vertex, and for a half-space with a wedge-shaped notch or inclusion.     

The singular field near a sharp notch with mixed boundary conditions for hardening materials under longitudinal shear

The field behavior near a sharp notch tip with mixed homogeneous stress and displacement boundary conditions is examined for a power law hardening material. Using the hodograph transformation, the singularity and the angular distribution of the fields are determined. Special cases as those for linear elastic and perfect plastic materials are discussed.     

A new boundary element approach of modeling singular stress fields of plane V-notch problems

In this paper, a new boundary element (BE) approach is proposed to determine the singular stress field in plane V-notch structures. The method is based on an asymptotic expansion of the stresses in a small region around a notch tip and application of the conventional BE in the remaining region of the structure. The evaluation of stress singularities at a notch tip is transformed into an eigenvalue problem of ordinary differential equations that is solved by the interpolating matrix method in order to obtain singularity orders (degrees) and associated eigen-functions of the V-notch. The combination of the eigen-analysis for the small region and the conventional BE analysis for the remaining part of the structure results in both the singular stress field near the notch tip and the notch stress intensity factors (SIFs).Examples are given for V-notch plates made of isotropic materials. Comparisons and parametric studies on stresses and notch SIFs are carried out for various V-notch plates. The studies show that the new approach is accurate and effective in simulating singular stress fields in V-notch/crack structures.     

Higher order fields for damaged nonlinear antiplane shear notch, crack and inclusion problems

Damaged nonlinear antiplane shear problems with a variety of singularities are studied analytically. A deformation plasticity theory coupled with damage is employed in analysis. The effect of microscopic damage is considered in terms of continuum damage mechanics approach. An exact solution for the general damaged nonlinear singular antiplane shear problem is derived in the stress plane by means of a hodograph transformation, then corresponding higher order asymptotic solutions are obtained by reversing the stress plane solution to the physical plane. As example, traction free sharp notch and crack, rigid sharp wedge and flat inclusion, and mixed boundary sharp notch problems are investigated, respectively. Consequently, higher order fields are obtained, in which analytical expressions of the dominant and second order singularity exponents and angular distribution functions of the near tip fields are derived. Effects of the damage and hardening exponents of materials and the geometric angle of notch/wedge on the near tip quantities are discussed in detail. It is found that damage leads to a weaker dominant singularity of stress, but to little stronger singularities of the dominant and second order terms of strain compared to that for undamaged material. It is also seen that damage has important effect on the angular distribution functions of the near tip stress and strain fields. As special cases, higher order analytical solutions of the crack and rigid flat inclusion tip fields are obtained, respectively, by reducing the notch/wedge tip solutions. Effects of damage and hardening exponents on the dominant and second order terms in the solutions of the crack and inclusion tip fields are discussed.     

Analytical representation of the non-square-root singular stress field at a finite angle sharp notch

The stress field near the tip of a finite angle sharp notch is singular. However, unlike a crack, the order of the singularity at the notch tip is less than one-half. Under tensile loading, such a singularity is characterized by a generalized stress intensity factor which is analogous to the mode I stress intensity factor used in fracture mechanics, but which has order less than one-half. By using a cohesive zone model for a notional crack emanating from the notch tip, we relate the critical value of the generalized stress intensity factor to the fracture toughness. The results show that this relation depends not only on the notch angle, but also on the maximum stress of the cohesive zone model. As expected the dependence on that maximum stress vanishes as the notch angle approaches zero. The results of this analysis compare very well with a numerical (finite element) analysis in the literature. For mixed-mode loading the limits of applicability of using a mode I failure criterion are explored.     

METHOD TO CALCULATE STRESS INTENSITY FACTOR OF V-NOTCH IN BI-MATERIALS

Based on Zak＇s stress function, the eigen-equation of stress singularity ofbi-materials with a V-notch was obtained. A new definition of stress intensity factor for a perpendicular interfacial V-notch of bi-material was put forward. The effects of shear modulus and Poisson＇s ratio of the matrix material and attaching material on eigen-values were analyzed. A generalized expression for calculating/（i of the perpendicular V-notch of bi-materials was obtained by means of stress extrapolation. Effects of notch depth, notch angle and Poisson＇s ratio of materials on the singular stress field near the tip of the V-notch were analyzed systematically with numerical simulations. As an example, a finite plate with double edge notches under uniaxial uniform tension was calculated by the method presented and the influence of the notch angle and Poisson＇s ratio on the stress singularity near the tip of notch was obtained.     

Modification of the fracture criterion for V-shaped notches (plane problem). Relationship between toughness and strength and structural parameters

A fracture criterion of the type of the Neuber-Novozhilov criterion is proposed to describe the fracture in the vicinity of the tip of a V-shaped notch under tensile and shear loading. In the proposed criterion, the limits of averaging of the stresses along the notch axis depend on the presence, location, and size of the initial defects in the material. The crystal lattice parameter of the initial material is chosen for the characteristic linear size. For a V-shaped notch subjected to tension and shear, simple equations are obtained that relate the stress intensity factors for the modified singularity coefficients, the singularity coefficients themselves, and the theoretical tensile and shear strengths of a single crystal of the material taking into account the damage to the material in the vicinity of the notch tip. The equations obtained allow a passage to the limit from a notch to a crack. It is shown that the classical critical stress intensity factor used in the strength analysis of cracked solids is not a material constant.Translated from Prikladnaya Mekhanika i Tekhnicheskaya Fizika, Vol. 46, No. 1, pp. 106–115, January–February, 2005.     

ANALYSIS OF 3-D NOTCHED/CRACKED STRUCTURES BY USING EXTENDED BOUNDARY ELEMENT METHOD 1)

在线弹性理论中,三维 V 形切口/裂纹结构尖端区域存在多重应力奇异性,常规数值方法不易求解. 本文提出和建立了三维扩展边界元法 (XBEM),用于分析三维线弹性 V 形切口/裂纹结构完整的位移和应力场. 先将三维线弹性 V 形切口/裂纹结构分为尖端小扇形柱和挖去小扇形柱后的外围结构. 尖端小扇形柱内的位移函数采用自尖端径向距离 $r$ 的渐近级数展开式表达,其中尖端区域的应力奇异指数、位移和应力特征角函数通过插值矩阵法获得. 而级数展开式各项的幅值系数作为基本未知量. 挖去扇形域后的外围结构采用常规边界元法分析. 两者方程联立求解可获得三维 V 形切口/裂纹结构完整的位移和应力场,包括切口/裂纹尖端区域精细的应力场. 扩展边界元法具有半解析法特征,适用于一般三维 V 形切口/裂纹结构完整位移场和应力场的分析,其解可精细描述从尖端区域到整体结构区域的完整应力场. 作者研制了三维扩展边界元法程序,文中给出了两个算例,通过计算结果分析,表明了扩展边界元法求解三维 V 形切口/裂纹结构完整应力场的准确性和有效性.