粘弹性介质中扩展裂纹与J积分

本文提出了在线弹性及粘弹性介质中扩展裂纹与路径无关的J~*积分,并给出了严密的证明。文中证明了J~*积分与扩展裂纹尖端的张开位移(动态COD)之间有简单的关系,同时利用J~*积分求得了粘弹性介质中变速扩展裂纹尖端的奇异性。当裂纹以常速扩展时,J~*积分与能量释放率、动应力强度因子之间也有简单的关系。利用这些关系,我们给出了动态COD与动应力强度因子之间的关系式。     

压电效应下一维六方准晶双材料孔边裂纹的反平面问题研究

利用复变函数方法和保角变换技术研究了压电效应下一维六方准晶双材料中圆孔边单裂纹的反平面问题．考虑电不可渗透型边界条件,运用保角变换和Stroh公式得到了弹性体受远场剪切力和面内电载荷作用下裂纹尖端应力强度因子和能量释放率的解析解. 数值算例分析了几何参数、远场受力、电位移载荷对能量释放率的影响．结果表明：裂纹长度、耦合系数和远场剪切力的减小可以抑制裂纹的扩展．不考虑电场时,声子场应力对能量释放率的影响较小．本文的研究结果可作为研究一维六方压电准晶双材料孔边裂纹问题的理论基础,同时为压电准晶及其复合材料的设计、制备、优化和性能评估提供理论依据．     

一维六方压电准晶三角形孔边裂纹反平面问题

通过引入合适的数值保角映射,利用Stroh型公式研究一维六方压电准晶中正三角形孔边裂纹的反平面问题,给出在电非渗透边界条件下三角形孔边裂纹尖端的场强度因子和能量释放率。通过数值算例,讨论场强度因子和能量释放率随缺陷几何尺寸和力电荷载的变化规律。结果表明:随孔边裂纹长度的增加,场强度因子先急剧增加后减小,并趋于定值1,正三角形孔洞的尺寸对其影响可忽略不计;声子场和相位子场机械载荷总是促进裂纹扩展,而电位移对裂纹的扩展极大地依赖于声子场和相位子场载荷的大小。     

橡胶—钢粘接界面断裂韧性实验研究

采用双悬臂夹层梁试样,对橡胶—钢粘接界面的I型边缘裂纹的扩展情况及断裂韧性进行实验研究.通过声发射技术的监测将裂纹扩展划分为无损伤、开裂、失稳扩展三个阶段,把线弹性断裂力学中的柔度和能量释放率引入到橡胶—钢粘接界面断裂韧性的计算中,由实验测出裂纹的张开位移计算出夹层梁的柔度曲线,进而得到了能量释放率曲线,并对断裂韧性的变化规律进行了分析.     

能量释放率G的两种解法的统一

在线弹性断裂力学中,从能量的观点考察裂纹的扩展过程是研究破坏机理的一条有效途径.如果裂纹扩展过程中系统所释放出的能量,足以提供裂纹扩展所需要的能量,则裂纹便发生扩展.能量释放率G 就是描述裂纹扩展物体能量变化的一个参数,它是线弹性断裂力学中一个很重要的概念.在一些文献和断裂...     

反平面扩展裂纹的J积分与COD

给出一个以任意速率扩展的反平面裂纹与路径无关的Ｊ积分，证明Ｊ积分扩展裂纹尖端的张开位移（动态ＣＯＤ）之间有的简单的关系，Ｊ积分与能量释放率，动应力强度因子之间也有简单关系，利用这些关系，给出了动态ＣＯＤ与动应力强度因子之间的关系式。     

弹性T项对裂尖参数和裂纹扩展路径稳定性的作用

研究了弹性T项在主裂纹与近裂尖微空洞干涉问题中对裂尖参数和裂纹扩展路径稳定性的影响作用.利用“伪力”法,并通过解决主裂纹与近裂尖微空洞干涉问题,对远场纯1型载荷和远场弹性T项载荷下,该干涉问题中弹性T项的影响作用进行了分析从数值结果可以看出：由于空洞的存在;释放了弹性T项所引起的应力,弹性T项对裂尖参数;应力强度因子和J积分都有直接显著的影响,因而,它对该载荷下的裂纹扩展路径的稳定性有控制作用。     

层状非均匀材料边裂纹引起的J积分变化量分析

均匀材料无裂纹时沿封闭路径的J积分为零,层状非均匀材料无裂纹时沿封闭路径的J积分通常不为零且与路径相关。在位移载荷保持不变条件下引入裂纹会使J积分改变,本文分析引入裂纹所导致的远场J积分变化量,即有裂纹时与无裂纹时沿同一远场路径的J积分之差,其值等于裂尖J积分与界面J积分变化量之和。对于层状非均匀材料,虽然无裂纹时和有裂纹时的远场J积分、界面J积分都与路径相关,但当积分路径远离裂尖后,有裂纹与无裂纹时的远场J积分之差、界面J积分之差与路径无关,引入裂纹所引起的远场J积分变化量等于边界应变能密度释放量沿边界的积分。对于均匀材料半无限大平面的边裂纹,裂纹能量释放率等于无裂纹时应变能密度与8倍裂纹长度的乘积;对于层状材料的边裂纹,裂纹能量释放率等于应变能密度释放量沿边界的积分减去界面J积分变化量。     

涂层式裂纹监测系统中基体裂纹穿越行为研究

建立了智能涂层的两相模型与三相模型,基于能量准则分别用这两种模型研究了基体裂纹达到涂层界面后的穿越/偏转行为. 用有限元法分析了相对裂纹扩展长度、弹性错配参数及界面层厚度对偏转裂纹与穿越裂纹能量释放率之比的影响,结果表明当基体裂纹到达驱动层与基体界面时,能量释放率之比不仅与基体和驱动层之间的弹性错配相关,而且当驱动层较薄时对驱动层与传感层之间的弹性错配亦有较强的依赖性. 此外,随着驱动层厚度的增加,能量释放率之比对驱动层与传感层之间的弹性错配的依赖性逐渐降低. 通过与实验结果相比,建立的模型能够较好的解释基体裂纹在界面的扩展行为,可用于智能涂层裂纹传感器的优化设计.      

Z—pins增强陶瓷基复合材料单搭接接头的裂纹尖端能量释放率

对典型Z-pins增强陶瓷基复合材料单搭接接头的裂纹尖端能量释放率进行了数值模拟,重点研究Z-pins在不同直径和间距下裂纹尖端能量释放率随裂纹扩展的变化规律.研究发现能够形成桥联的Z-pins具有一定抑制开裂的能力,形成桥联后,Z-pins的直径对于裂纹尖端能量释放率的影响较大,而Z-pins的间距对于裂纹尖端能量释放率也有影响,但当间距小到某一限度时,再减小间距裂纹尖端能量释放率基本保持不变.     

裂纹垂直于双相介质界面时的应力强度因子

本文利用Ｊ积分与应力强度因子的关系,采用有限元数值方法研究了当裂纹与双相介质的界面垂直时,其裂纹的近界面端和远界面端的应力强度因子随双相介质参数和裂纹端部到界面的距离的变化规律,同时还分析了当边裂纹逐渐扩展时,应力强度因子的变化特征。     

含圆形嵌体弹性平面中径向裂纹问题的超奇异积分方程方法

根据含圆形嵌体平面问题在极坐标下的弹性力学基本解,使用Betti互换定理,在有限部积分意义下将问题归结为两个以裂纹岸位移间断为基本未知量、对于Ⅰ型和Ⅱ型问题相互独立的超奇异积分方程,对含圆形嵌体弹性平面中的径向裂纹问题进行了研究.根据有限部积分原理,建立了问题的数值算法.计算结果表明,嵌体半径、裂纹位置及材料剪切弹性模量等都对裂纹应力强度因子具有较为明显的影响.     

三维断裂力学的超奇异积分方程方法

本文利用有限部积分的概念和方法,严格地证明了三维弹性体中受任意载荷作用的平片裂纹问题的超奇异积分方程组,并对未知解的性态作了理论分析,得到了性态指数,在此基础上通过主部分析,精确地求得了裂纹前沿光滑点附近的奇性应力场,从而找到了以裂纹面位移间断(位错)表示的应力强度因子表达式,最后对所得的超奇异积分方程组建立了数值法,并用此计算了若干典型的平片裂纹问题,数值结果令人满意。     

The scattering of general SH plane wave by interface crack between two dissimilar viscoelastic bodies

The scattering of general SH plane wave by an interface crack between two dissimilar viscoelastic bodies is studied and the dynamic stress intensity factor at the crack-tip is computed. The scattering problem can be decomposed into two problems: one is the reflection and refraction problem of general SH plane waves at perfect interface (with no crack); another is the scattering problem due to the existence of crack. For the first problem, the viscoelastic wave equation, displacement and stress continuity conditions across the interface are used to obtain the shear stress distribution at the interface. For the second problem, the integral transformation method is used to reduce the scattering problem into dual integral equations. Then, the dual integral equations are transformed into the Cauchy singular integral equation of first kind by introduction of the crack dislocation density function. Finally, the singular integral equation is solved by Kurtz's piecewise continuous function method. As a consequence, the crack opening displacement and dynamic stress intensity factor are obtained. At the end of the paper, a numerical example is given. The effects of incident angle, incident frequency and viscoelastic material parameters are analyzed. It is found that there is a frequency region for viscoelastic material within which the viscoelastic effects cannot be ignored. This work was supported by the National Natural Science Foundation of China (No.19772064) and by the project of CAS KJ 951-1-20     

A Mode- II Griffith Crack in Decagonal Quasicrystals

By using the method of stress functions, the problem of mode-II Griffith crack in decagonal quasicrystals was solved. First, the crack problem of two-dimensional quasicrystals was decomposed into a plane strain state problem superposed on anti-plane state problem and secondly, by introducing stress functions, the18 basic elasticity equations on coupling phonon-phason field of decagonal quasicrystals were reduced to a single higher-order partial differential equations. The solution of this equation under mixed boundary conditions of mode-II Griffith crack was obtained in terms of Fourier transform and dual integral equations methods. All components of stresses and displacements can be expressed by elemental functions and the stress intensity factor and the strain energy release rate were determined. Biography: GUO Yu-cui (1962-), Associate professor, Doctor     

Numerical methods for solving singular integral equations obtained by fracture mechanical analysis of cracked wedge简

The numerical solutions to the singular integral equations obtained by the fracture mechanical analyses of a cracked wedge under three different conditions are considered. The three considered conditions are: (i) a radial crack on a wedge with a non-finite radius under the traction-traction boundary condition, (ii) a radial crack on a wedge with a finite radius under the traction-traction boundary condition, and (iii) a radial crack on a finite radius wedge under the traction-displacement boundary condition. According to the boundary conditions, the extracted singular integral equations have different forms. Numerical methods are used to solve the obtained coupled singular integral equations, where the Gauss-Legendre and the Gauss-Chebyshev polynomials are used to approximate the responses of the singular integral equations. The results are presented in figures and compared with those obtained by the analytical response. The results show that the obtained Gauss-Chebyshev polynomial response is closer to the analytical response.     

基于扩展有限元的应力强度因子的位移外推法

针对平面裂纹问题,阐述了扩展有限元法的单元位移模式、推导了扩展有限元法的控制方程、介绍了特殊单元的数值积分技术.基于最小二乘法,建立了应力强度因子位移外推法的计算公式.利用MATLAB编写计算程序,对平面裂纹问题用扩展有限元法进行了计算.基于扩展有限元法的计算结果,分别利用位移外推法和相互作用积分法,对平面裂纹的应力强度因子进行了计算.计算结果表明,位移外推法比相互作用积分法能更方便和准确地计算平面裂纹的应力强度因子.     

三维体内含垂直于双材料界面混合型裂纹的超奇异积分解法

利用双材料位移基本解和Somigliana公式,将三维体内含垂直于双材料界面混合型裂纹问题归结为求解一组超奇异积分方程。使用主部分析法,通过对裂纹前沿应力奇性的分析,得到用裂纹面位移间断表示的应力强度因子的计算公式,进而利用超奇异积分方程未知解的理论分析结果和有限部积分理论,给出了超奇异积分方程的数值求解方法。最后,对典型算例的应力强度因子做了计算,并讨论了应力强度因子数值结果的收敛性及其随各参数变化的规律。     

Analysis of three-dimensional edge cracks under tensile loading

Three-dimensional edge cracks are analyzed using the Self-Similar Crack Expansion (SSCE) method with a boundary integral equation technique. The boundary integral equations for surface cracks in a half space are presented based on a half space Green's function (Mindlin, 1936). By using the SSCE method, the stress intensity factors are determined by the crack-opening displacement over the crack surface. In discrete boundary integral equations, the regular and singular integrals on the crack surface elements are evaluated by an analytical method, and the closed form expressions of the integrals are given for subsurface cracks and edge crakcs. This globally numerical and locally analytical method improves the solution accuracy and computational effort. Numerical results for edge cracks under tensile loading with various geometries, such as rectangular cracks, elliptical cracks, and semi-circular cracks, are presented using the SSCE method. Results for stress intensity factors of those surface breaking cracks are in good agreement with other numerical and analytical solutions.     

AN ANALYSIS OF 3D FINITE CRACKED BODIES

The new-type traction boundary integral equations developed by Hu and with no hypersingular integral are applied to analysis of 3D finite cracked bodies. A numerical algorithm for general 3D problems and a semi-analytical one for axisymmetric problems are presented. Some examples of thick plates and cylindrical columns including penny-shaped crack(s), and rectangular plates including an elliptical crack normal to the surface are analyzed. The comparison between present results and those in literature shows the high accuracy and effectiveness of the present method. Project supported by the National Natural Science Foundation of China (No. 19972060) and the Foundation of Key Laboratory of the Ministry of Education, Tongji University.