压电体中考虑表面效应时开裂孔洞的断裂特征

研究了反平面机械载荷和面内电载荷作用下压电体中考虑表面效应时孔边双裂纹问题的断裂特征。基于Gurtin-Murdoch表面理论模型，通过构造映射函数，利用复势电弹理论获得了应力场和电位移场的闭合解答。给出了裂纹尖端应力强度因子、电位移场强因子和能量释放率的解析解。讨论了开裂孔洞几何参数和施加力电载荷对电弹场强因子和能量释放率的影响。     

磁电弹性体中唇形运动裂纹问题分析

本文通过共形映射公式,利用复变函数方法研究了磁电弹性体中的唇形运动裂纹问题.对裂纹面上受反平面剪应力和面内磁电载荷共同作用情况,导出了磁电全非渗透型边界条件下运动裂纹尖端场应力强度因子和机械应变能释放率的解析解.当运动速度为零时这两解都退化成了静止状态下的解.通过算例,与具有相同尺寸的带双裂纹的椭圆孔口问题进行了比较,给出了两种裂纹尖端点处应力强度因子和机械应变能释放率随孔口高度h与裂纹半长a之比h/a的变化规律曲线图,得出了两种孔口裂纹问题在应力强度因子和能量释放率两方面的异同点,结果表明采用唇形孔口裂纹比采用带双裂纹的椭圆孔口能降低裂纹的扩展,这在工程建设及构件的制造上有一些指导作用.     

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．     

一维六方准晶中纳米尺度开裂孔洞的III型断裂力学

研究了一维六方准晶中纳米尺度开裂孔洞的Ⅲ型断裂力学问题。基于复变弹性理论和表面弹性理论获得了考虑表面效应时椭圆孔边裂纹的应力场、应力强度因子和能量释放率的解析表达;讨论了缺陷尺寸、裂纹/孔洞比、耦合系数和施加载荷对应力强度因子和能量释放率的影响。研究表明：考虑表面效应且缺陷的尺寸在纳米尺度时,声子场和相位子场的无量纲应力强度因子以及无量纲能量释放率具有明显的尺寸依赖;裂纹相对尺寸较小时,表面效应对声子场和相位子场的无量纲应力强度因子影响较小;纳米尺度时无量纲能量释放率随耦合系数的增加而增大;耦合系数一定时,无量纲能量释放率受到椭圆孔尺寸影响;随着声子场载荷的增大,无量纲能量释放率先减小后增加,最后趋于稳定;无量纲能量释放率随相位子场载荷的增大单调减小,非常小和非常大的声子场载荷(或相位子场载荷)屏蔽了相位子场载荷(或声子场载荷)的影响。     

一维六方准晶中纳米尺度开裂孔洞的III型断裂力学

研究了一维六方准晶中纳米尺度开裂孔洞的Ⅲ型断裂力学问题。基于复变弹性理论和表面弹性理论获得了考虑表面效应时椭圆孔边裂纹的应力场、应力强度因子和能量释放率的解析表达；讨论了缺陷尺寸、裂纹/孔洞比、耦合系数和施加载荷对应力强度因子和能量释放率的影响。研究表明：考虑表面效应且缺陷的尺寸在纳米尺度时，声子场和相位子场的无量纲应力强度因子以及无量纲能量释放率具有明显的尺寸依赖；裂纹相对尺寸较小时，表面效应对声子场和相位子场的无量纲应力强度因子影响较小；纳米尺度时无量纲能量释放率随耦合系数的增加而增大；耦合系数一定时，无量纲能量释放率受到椭圆孔尺寸影响；随着声子场载荷的增大，无量纲能量释放率先减小后增加，最后趋于稳定；无量纲能量释放率随相位子场载荷的增大单调减小，非常小和非常大的声子场载荷(或相位子场载荷)屏蔽了相位子场载荷(或声子场载荷)的影响。     

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。     

矩形压电体中反平面裂纹的电弹性场

基于线性压电理论,本文获得了含有中心反平面裂纹的矩形压电体中的奇异应力和电场。利用Fourier积分变换和Fourier正弦级数将电绝缘型裂纹问题化为对偶积分方程,并进一步归结为易于求解的第二类Fred-holm积分方程。获得了裂纹尖端应力、应变、电位移和电场的解析解,求得了裂纹尖端场的强度因子及能量释放率。分析了压电矩形体的几何尺寸对它们的影响。结果表明,对于电绝缘型裂纹,裂纹尖端附近的各个场变量都具有-1/2阶的奇异性,能量释放率与电荷载的方向及大小有关,并且有可能为负值。     

冲击载荷下扩展裂纹尖端动态能量释放率分布的焦散线分析

借助高速摄影捕捉裂纹瞬态扩展过程，利用动态焦散线研究了含有裂纹的三点弯曲梁在冲击载荷作用下扩展裂纹尖端的动态能量释放率分布规律；综合分析了裂纹扩展时间、长度、速度，以及扩展裂纹尖端动态应力强度因子与它的变化关系，表明了动态能量释放率在裂纹扩展过程中的驱动作用。     

含弧形裂纹复合陶瓷强度的尺度效应

认为含弧形裂纹复合陶瓷由随机方向的三相胞元与有效介质构成,用细观力学的方法研究了复合陶瓷的损伤失效和强度。首先确定三相胞元的外载应变,再依据复合陶瓷在损伤过程中的细观应力场和广义热力学力,计算出三相胞元内基体和颗粒的损伤等效应力,当基体和颗粒的损伤等效应力分别等于两者的极限应力时,得到基体和颗粒的破坏应力。然后,根据混合型应力强度因子计算弧形裂纹扩展时的能量释放率,进而得到界面的破坏应力。最后综合考虑基体、颗粒和和界面损伤影响,获得含弧形裂纹复合陶瓷的宏观强度及其尺度效应。     

两种材料组成弹性体的界面裂纹问题

本文研究了两种材料的半空间组成的弹性体在交界面上含半无限平面裂纹时的裂纹尖端应力场与应力强度因子,应用弹性力学位移场的通解以及Kontorovitch-Lebedev积分变换求解出了在裂纹面上作用有对称法向载荷时的裂纹尖端应力场以及应力强度因子的具体形式。     

电可通纳米尺度孔边均布多裂纹的电弹断裂分析

解析研究了面内电载荷和反平面机械载荷作用下压电体中纳米尺度圆孔边均布电可通多裂纹问题的断裂性能。基于Gurtin-Murdoch表面弹性理论，利用保角映射方法和复变弹性理论给出了裂纹尖端电弹场分布、电弹场强度因子及能量释放率的解析结果。阐述了无量纲电弹场强度因子、无量纲能量释放率的尺寸依赖效应，讨论了裂纹数量和缺陷几何参数对无量纲场强度因子和无量纲能量释放率的影响。结果表明：无量纲电弹场强度因子和无量纲能量释放率具有显著的尺寸依赖效应；考虑表面效应，孔径和裂纹长度相当时，电弹场强度因子达到最大；裂纹/孔径比对电弹场强度因子随裂纹数量变化的制约会随着裂纹数量的增加而逐渐消失；过大或过小的裂纹孔径比会削弱裂纹长度对能量释放率的影响。     

电可通纳米尺度孔边均布多裂纹的电弹断裂分析

解析研究了面内电载荷和反平面机械载荷作用下压电体中纳米尺度圆孔边均布电可通多裂纹问题的断裂性能。基于Gurtin-Murdoch表面弹性理论,利用保角映射方法和复变弹性理论给出了裂纹尖端电弹场分布、电弹场强度因子及能量释放率的解析结果。阐述了无量纲电弹场强度因子、无量纲能量释放率的尺寸依赖效应,讨论了裂纹数量和缺陷几何参数对无量纲场强度因子和无量纲能量释放率的影响。结果表明：无量纲电弹场强度因子和无量纲能量释放率具有显著的尺寸依赖效应;考虑表面效应,孔径和裂纹长度相当时,电弹场强度因子达到最大;裂纹/孔径比对电弹场强度因子随裂纹数量变化的制约会随着裂纹数量的增加而逐渐消失;过大或过小的裂纹孔径比会削弱裂纹长度对能量释放率的影响。     

基于有限断裂法和比例边界有限元法的裂纹扩展模拟

基于有限断裂法和比例边界有限元法提出了一种裂缝开裂过程模拟的数值模型。采用基于有限断裂法的混合断裂准则作为起裂及扩展的判断标准,当最大环向应力和能量释放率同时达到其临界值时,裂缝扩展。结合多边形比例边界有限元法,可以半解析地求解裂尖区域附近的应力场和位移场,在裂尖附近无需富集即可获得高精度的解。计算能量释放率时,只需将裂尖多边形内的裂尖位置局部调整,无需改变整体网格的分布,网格重剖分的工作量降至最少。裂缝扩展步长通过混合断裂准则确定,避免了人为假设的随意性,并可以实现裂缝变步长扩展的模拟,更符合实际情况。通过对四点剪切梁的复合型裂缝扩展过程的模拟,对本文模型进行了验证,并应用于重力坝模型的裂缝扩展模拟,计算结果表明,本文提出的模型简单易行且精度较高。     

Analysis of elastic crack bridging in ceramic matrix composites

A micromechanics analytical model based on the consistent shear lag theory is developed for predicting the failure modes in fiber reinforced unidirectional stiff matrix composites. The model accounts for a relatively large matrix stiffness and hence its load carrying capacity. The fiber and matrix stresses are established as functions of the applied stress, crack geometry, and the microstructural properties of the constituents. From the predicted stresses, the mode of failure is established based on a point stress failure criterion. The role of the microstructural parameters of the constituents on the failure modes such as self-similar continuous cracking, crack bridging and debonding parallel to the fibers is assessed.     

Damage growth by debonding in a single fibre metal matrix composite: Elastoplasticity and strain energy density criterion

A displacement-based finite element-based numerical approach has been employed to study the damage growth in a unidirectional SiC/Al composite containing a pre-existing crack along the fibre/matrix interface. The composite is modeled as a two-material cylinder subjected to uniform displacement. A detailed analysis is made for the stress field in the vicinity of the debond crack tip. This approach incorporates an elastic-plastic analysis combined with a strain energy density criterion to predict debonded crack growth direction, extended stable growth and final termination. The influence of contact taking place between the debonded surfaces is also considered. It is shown that such surface contact leads to reduced stress and strain fields around the crack tip, while the extent of reduction is increased with debonding length. By combining the reduced stress field with the strain energy density criterion, a limiting value for the debonding extension can be calculated for the critical applied displacement that led to fibre fracture.     

The weight function for cracks in piezoelectrics

The weight function in fracture mechanics is the stress intensity factor at the tip of a crack in an elastic material due to a point load at an arbitrary location in the body containing the crack. For a piezoelectric material, this definition is extended to include the effect of point charges and the presence of an electric displacement intensity factor at the tip of the crack. Thus, the weight function permits the calculation of the crack tip intensity factors for an arbitrary distribution of applied loads and imposed electric charges. In this paper, the weight function for calculating the stress and electric displacement intensity factors for cracks in piezoelectric materials is formulated from Maxwell relationships among the energy release rate, the physical displacements and the electric potential as dependent variables and the applied loads and electric charges as independent variables. These Maxwell relationships arise as a result of an electric enthalpy for the body that can be formulated in terms of the applied loads and imposed electric charges. An electric enthalpy for a body containing an electrically impermeable crack can then be stated that accounts for the presence of loads and charges for a problem that has been solved previously plus the loads and charges associated with an unsolved problem for which the stress and electric displacement intensity factors are to be found. Differentiation of the electric enthalpy twice with respect to the applied loads (or imposed charges) and with respect to the crack length gives rise to Maxwell relationships for the derivative of the crack tip energy release rate with respect to the applied loads (or imposed charges) of the unsolved problem equal to the derivative of the physical displacements (or the electric potential) of the solved problem with respect to the crack length. The Irwin relationship for the crack tip energy release rate in terms of the crack tip intensity factors then allows the intensity factors for the unsolved problem to be formulated, thereby giving the desired weight function. The results are used to derive the weight function for an electrically impermeable Griffith crack in an infinite piezoelectric body, thereby giving the stress intensity factors and the electric displacement intensity factor due to a point load and a point charge anywhere in an infinite piezoelectric body. The use of the weight function to compute the electric displacement factor for an electrically permeable crack is then presented. Explicit results based on a previous analysis are given for a Griffith crack in an infinite body of PZT-5H poled orthogonally to the crack surfaces.     

Comparison of energy release rate and minimum strain energy density for potential failure of composite with bi-material interface

An analytical method is developed to describe the fields of stress and displacement in a bi-material strip specimen with an edge interfacial crack. All of the basic governing equations, boundary conditions on crack surfaces and conditions of continuity along the interface are satisfied by the eigenfunction expansion method. The other boundary conditions are satisfied by the generalized variational principle. The stress intensity factors are calculated for determining the energy release rate and minimum strain energy density factor S_min that is used the strain energy density criterion. Problems with oscillatory singularity and contact zone are discussed. Not only the effects of bi-material modulus ratio, thickness ratio, Poisson's ratio and crack length to S_min, but also the influences of bi-material modulus ratio, thickness ratio to phase angle are presented. Among these parameters, particular situations where S_min become jeopardously high and lead to failure are discussed.     

深埋椭圆形片状裂纹的偏折扩展

基于无限大弹性基体深埋椭圆形片状裂纹的变形场,推导了椭圆形片状裂纹的能量释放率,采用能量平衡方法建立了椭圆形片状裂纹承受拉应力和剪应力时的复合断裂准则. 考虑裂纹在拉-剪应力作用下的偏折扩展,分析了裂纹的偏折方向,提出了椭圆形片状裂纹发生偏折扩展时的初始偏折位置的确定方法.      

拉伸荷载下分支裂隙破坏机理研究

为研究拉伸荷载下分支裂隙对破坏模式的影响,保持主裂隙参数不变,改变分支裂隙倾角和长度,利用扩展有限元方法模拟了弯折裂隙的动态扩展,总结了分支裂隙参数变化对破坏模式的影响。利用ABAQUS中的轮廓积分计算了分支裂隙尖端应力强度因子,并根据最大周向应力准则计算起裂角。结果表明:拉伸荷载下分支裂隙出现三种破坏模式;分支裂隙倾角和长度均对破坏模式有一定的影响。I型应力强度因子与分支裂隙倾角关系曲线呈斜"S"型,相应II型应力强度因子曲线呈上凸型;由于分支裂隙存在非尖端破坏,利用裂隙尖端应力强度因子判断开裂应结合相应的破坏模式。