含层间短裂纹层合板的解析－分区变分解法

将层板横截面分为含裂纹区与不含裂纹区，在每一区内，根据夏变函数理论与特征函数展开法，得到了各自区内满足所有支配方程、裂纹表面边界条件与层间连续条件的位移与应力的特征展开式，然后利用分区广义变分原理满足裂纹表面边界以外的边界条件以及两区之间的交界条件，并由此求得奇异场控制量（广义应力强度因子）。     

含层间短裂纹层合板的解析－分区变分解法

将层板横截面分为含裂纹区与不含裂纹区,在每一区内,根据夏变函数理论与特征函数展开法,得到了各自区内满足所有支配方程、裂纹表面边界条件与层间连续条件的位移与应力的特征展开式,然后利用分区广义变分原理满足裂纹表面边界以外的边界条件以及两区之间的交界条件,并由此求得奇异场控制量（广义应力强度因子）。     

含层间长裂纹的对称正交层合板的角析—分区广义变分解法

本文首先将层板横截面分为含裂尖区、韧带区以及裂纹区等三个区域，用复变函数理论与特征函数层开法，得到了各区内满足所有基本方程、裂纹表面边界条件与层间连续条件的位移与应力的特征展开式，然后利用分区广义变分原理满足裂纹表面边界以外的边界条件以及各区之间的交界条件，并由此求得奇异场控制量。     

各向异性板应力强度因子的分区广义变分解法

本文以单边边缘裂纹二维应力场与位移场的级数展开式为基础,以分区广义变分原理求解含双边非对称边缘裂纹板的应力强度因子。首先建立精确满足各向异性板基本微分方程和裂纹表面边界条件的应力场和位移场的本征展开式,然后用分区广义变分原理满足其余边界条件与交界连续条件并由此确定应力强度因子。在变分方程中只有沿板边界的线积分。计算程序简单,输入数据很少,结果收敛迅速并与已有结果完全吻合,同时计算节省机时与人力。本文还给出了有关的全新计算曲线。     

紧凑拉伸试件应力强度因子的解析-变分解法以及有关系统计算结果

本文推导了在材料断裂性能测试中常见的受钉传载荷含边缘裂纹试件应力与位移的函数项级数表达式。该级数逐项满足弹性力学所有基本方程、裂纹表面边界条件与绕钉孔的合力平衡条件以及位移单值条件。通过以最小势能原理为基础的变分方程满足其余的静力边界条件,从而求解级数中的待定系数并确定应力强度因子。计算结果表明,级数收敛迅速、正确,计算节省机时,简化数据准备工作。本文还通过计算指出了目前通用的有关矩形紧凑拉伸试件应力强度因子计算公式与曲线的不准确性并且给出了正确、系统的计算曲线,同时还提供了圆形紧凑拉伸试件系统的计算结果。     

正交各向异性板平面剪切型裂纹应力强度因子的复变—变分解法

1 引言为了改善计算的精度和效率并消除离散化所带来的力学模型不确定性,本文提供了求解具有内部裂纹的有限宽板平面剪切型应力强度因子的复变-变分解法.2 各向异性边缘裂纹板的应力与位移场由二维各向异性弹性理论,满足所有基本方程的应力与位移分量可以表达为如下形式     

含裂纹体的单位分解扩展无网格方法

不连续体的数值模拟尤其是动态裂纹的追踪问题一直是工程界研究的热点和难点问题。无网格方法仅仅需要结点信息,非常适合于求解这类问题。基于单位分解思想,在移动最小二乘近似函数(MLS)中根据裂纹面的不连续位移增加一个Heaviside函数,在裂尖则增加四个扩展函数描述渐进裂纹位移场;应用Galerkin方法推导了平衡方程的离散线性方程,并给出了求解裂纹问题应力强度因子的计算公式。与其他类型的扩展无网格相比,在裂尖处近似函数不需要使用可视准则,很容易生成r1/2奇异;另一个优势是影响域并没有因为裂纹的存在而改变,不会降低方程的稀疏性,求解效率较高。数值算例表明,该方法能方便有效地模拟不连续问题,具有十分广阔的应用空间。     

含共线双半无限裂纹的正交异性复合材料板平面弹性问题的解析解

运用广义复变函数方法,通过构造适当的广义保角映射研究了含有共线双半无限裂纹的正交异性复合材料板的平面弹性问题,得出了部分裂纹面上受均匀面内载荷时应力场与两裂纹尖端处应力强度因子的解析解.结果表明:应力场的大小不仅与材料的几何构型及外载荷有关,还与材料的弹性常数有关,这是正交异性复合材料不同于各向同性材料的显著特征;两裂纹尖端处应力强度因子的大小只与材料的几何构型及外载荷有关;当两裂纹尖端的距离趋于无穷大时,所得到的解析解可退化为已有的正交异性复合材料板中半无限裂纹问题的解,通过将其与已有文献中的结果进行对比,验证了本文解析解的正确性.并通过数值算例分析了裂纹面上的受载长度、两裂纹尖端的距离对应力强度因子的影响规律以及两裂纹之间的相互作用.     

含夹杂和裂纹的平面内应力干涉半解析模型

材料不可避免引入的夹杂、裂纹等缺陷影响其力学特性.为了研究各向同性全空间内裂纹与夹杂的相互干涉作用,本文基于等效夹杂法与分布位错技术相结合的方法,将非均质夹杂近似为与基体具有相同弹性模量且含有未知本征应变的均质夹杂,将Ⅰ/Ⅱ混合型裂纹近似为密度未知的攀移位错和滑移位错,建立了可仿真各向同性全空间内夹杂和裂纹干涉作用的半解析模型,并基于位错分布求解了裂纹尖端的应力强度因子.模型采用共轭梯度法迭代求解了未知量,并借助快速傅里叶变换算法提高计算效率,最后通过有限元方法验证了模型的有效性.本模型可为缺陷材料内各结构的干涉作用以及由此诱导的断裂行为的解析提供理论方法.     

界面端附近裂纹的应力强度因子

结合材料的断裂形式可分为从界面端产生裂纹（沿界面或向母材内部层折）然后断裂与稍稍离开界面端处产生裂纹然后断裂这两种情况，在金属／陶瓷类结合材料中，后者出现的概率更大，本文利用结合材料界面端的奇异应力场和叠加原理，给出了界面端附近裂纹的应力强度因子近似计算公式，并用边界元数值计算验证了其有效性。     

求解界面裂纹应力强度因子的高次权函数法

从界面裂纹完备的特征展开式出发,利用伪正交特性,提出了计算界面裂纹特征展开式系数和应力强度因子的高次权函数法.文中计算的均匀材料应力强度因子,与已有结果吻合得非常好.并给出了界面裂纹的应力强度因子K1/K0和K2/K0随材料弹性模量比及裂纹长度的变化.     

The approximate solution of penny-shaped cracks periodically distributed in infinite elastic body

The penny-shaped cracks periodically distributed in infinite elastic body are studied. The problem is approximately simplified to that of a single crack embedded in finite length cylinder and the stress intensity factor is obtained by solving a Fredholm integral equation. Numerical results are given and the effects of crack interaction on the stress intensity factor are discussed. The project suppoted by National Natural Science Foundation of China     

Special approach for the determination of fracture mechanical parameters at an interface crack tip

An interface crack of finite length is considered between two semi-infinite planes with an artificial contact zone at one of the two crack tips. A transcendental equation and certain simple asymptotic formulas are established for the real contact zone (in the Comninou-Dundurs sense) in terms of the stress intensity factors (SIFs) of the considered model. In these terms analytical expressions are also provided for the energy release rate and for the SIF of the classical interface crack model with an oscillating singularity at the crack tip. The appropriate length of the artifical contact zone is shown to be attainable on the basis of the analysis of the stresses at the crack tip. The use of the proposed model is suggested for integrity assessment of inhomogeneous structural elements of composites containing interface cracks. Received 26 March 1997; accepted for publication 12 September 1997     

Analysis of stress intensity factor in orthotropic bi-material mixed interface crack

Adopting the complex function approach, the paper studies the stress intensity factor in orthotropic bi-material interface cracks under mixed loads. With consideration of the boundary conditions, a new stress function is introduced to transform the problem of bi-material interface crack into a boundary value problem of partial differential equations. Two sets of non-homogeneous linear equations with 16 unknowns are constructed. By solving the equations, the expressions for the real bi-material elastic constant εt and the real stress singularity exponents λt are obtained with the bi-material engineering parameters satisfying certain conditions. By the uniqueness theorem of limit,undetermined coefficients are determined, and thus the bi-material stress intensity factor in mixed cracks is obtained. The bi-material stress intensity factor characterizes features of mixed cracks. When orthotropic bi-materials are of the same material, the degenerate solution to the stress intensity factor in mixed bi-material interface cracks is in complete agreement with the present classic conclusion. The relationship between the bi-material stress intensity factor and the ratio of bi-material shear modulus and the relationship between the bi-material stress intensity factor and the ratio of bi-material Young's modulus are given in the numerical analysis.     

Semi-weight function method on computation of stress intensity factors in dissimilar materials

Semi-weight function method is developed to solve the plane problem of two bonded dissimilar materials containing a crack along the bond. From equilibrium equation, stress and strain relationship, conditions of continuity across interface and free crack surface, the stress and displacement fields were obtained. The eigenvalue of these fields is lambda. Semi-weight functions were obtained as virtual displacement and stress fields with eigenvalue-lambda. Integral expression of fracture parameters, KⅠ and KⅡ, were obtained from reciprocal work theorem with semi-weight functions and approximate displacement and stress values on any integral path around crack tip. The calculation results of applications show that the semi-weight function method is a simple, convenient and high precision calculation method.     

夹杂对两相材料界面裂纹的影响

根据界面上应力和位移的连续条件,得到了单向拉伸状态下,含有椭圆夹杂的无限大双材料组合板的复势解。进一步通过求解Hilbert问题,得到了含有夹杂和半无限界面裂纹的无限大板的应力场,并由此给出了裂尖的应力强度因子K。计算了夹杂的形状、夹杂的位置、夹杂的材料选取以及上、下半平面材料与夹杂材料的不同组合对裂尖应力强度的影响。计算结果表明夹杂到裂尖的距离和夹杂材料的性质对K影响较大,对于不同材料组合,该影响有较大差异。夹杂距裂尖较近时,会对K产生明显屏蔽作用,随着夹杂远离裂尖,对K的影响也逐渐减小。另外,软夹杂对K有屏蔽作用,硬夹杂对K有反屏蔽作用,而夹杂形状对K几乎没有影响。