双材料应力分析中的镜像点方法

提出一种分析各类双材料中任一点受集中力作用问题的方法.通过将结合界面或其自由表面看作镜面,将应力函数或位移函数设定成固定于受载点及其镜像点上的局部坐标系下的形式,利用界面连续条件和Dirichlet的单值性原理,所有应力函数或位移函数就可由无限体中集中力的解或半无限体表面集中力的解的应力函数求得.这种方法不仅可适用于单一界面的情况,也可使用于多个界面并存的情况,并且也可适用于具有自由表面的结合材料.这一方法可应用于各类结合材料、涂层薄膜材料、板材等.     

板材自由表面受法向集中力时的理论解

基于三维轴对称弹性理论,利用镜像点方法,给出了无限板表面受法向集中力作用的显式理论解．该解可用作格林函数,来求解分布力的问题．由于板的两个表面的反复映射,载荷点的镜像点有无穷多个,严密解是以固定在各镜像点的局部坐标系下的位移函数的和的形式给出的,但只需考虑前几个镜像点,就可获得足够精确的解．关于各镜像点的位移函数,是以递推形式给出的,易于计算机编程。     

等厚双层涂层材料受集中力作用的平面问题理论解

界面应力的正确评价是分析薄膜涂层材料力学特性的难题之一。利用镜像点法和Dirichlet等值性原理，本文推导了等厚双层薄膜涂层材料受表面集中力作用的平面问题理论解。该显式理论解是以固定在各镜像点上的局部坐标系下的Goursat应力函数的形式给出的。对应于高阶镜像点的应力函数，可通过递推的方法，从对应于低阶镜像点的应力函数求得，而且也易于计算机编程。随着镜像点阶数的增大，它与界面的距离也越来越大，因而相对应的应力函数对界面应力的影响越来越小。最后的算例表明，只需考虑前面有限个镜像点，便可获得足够精度的解。该理论解可作为格林函数，以求解复杂问题的理论解，也可用作边界元法的基本解，提高数值计算的精度和效率。     

弹性半空间表面在水平谐和集中力作用下的位移

自[1]以后,已有许多学者对理想弹性半空间表面在集中动荷载作用下的位移问题进行了大量的理论及试验研究.在一些专著中[2,3,4],对此问题曾作过系统的阐述.在这些研究中,竖向力作用的问题讨论得比较充分,水平力作用的问题则很少涉及.静水平集中力作用下的位移和应力问题已由Cerruti 在1882年解决了.1960年赵继昌得到了以Heaviside 阶跃函数H(t)表示的突加水平集中力作用下的位移闭合解.半空间表面在水平集中谐和力作用下位移的精确闭合解尚未见报道.本文放弃了从积分形式解出发的Lamb 传统求解途径,而从突加水平集中力作用下的解答出发,最终求得了闭合精确解,由此解得的结果以几种无量纲图表示之,并与鸟海的理论结果作了对比.     

黏弹性半空间体内部作用水平力时的理论分析

研究假定半无限体为线性黏弹性介质,土体在内部水平集中力作用下的应力球张量和应变球张量之间符合弹性关系,而应力偏张量和应变偏张量之间符合三参数固体黏弹性应力应变关系.利用半空间体内部受水平向集中力的Mindlin弹性理论解,根据弹性--弹黏性相应原理,系统推导了水平集中力作用在半无限体内部时的应力与位移分量的黏弹性解.通过对应力与位移分量在拉氏域内的解答进行Laplace逆变换,给出了应力与位移分量的时域解.作为黏弹性解答的应用,基于上述解答给出了水平向均布荷栽下作用在半空间体内部时的黏弹性位移计算公式,并编制了便于工程应用的计算程序.结果验证与深埋锚板的算例分析表明,本文的理论解答对实际工程具有一定的理论及应用价值.     

薄膜涂层材料中币形界面裂纹的弹性波散射

研究了薄膜涂层材料中币形界面裂纹的弹性波散射问题,建立了含有币形界面裂纹的覆层半空间模型,采用Hankel积分变换,将裂纹对弹性波散射的问题转化为求解矩阵形式的奇异积分方程。结合渐近分析和围道积分技术得到积分方程的解,进一步推导了散射波的应力场和位移场,以及动应力强度因子的理论计算公式。在数值算例中,分析了不同材料组合和裂纹尺寸情况下动应力强度因子与入射波频率的关系,并给出了裂纹张开位移的结果。为薄膜涂层材料的动态破坏分析提供了一定的理论基础。     

轴对称环形片状界面裂纹问题分析

讨论受拉伸载荷作用的轴对称环形片状界而裂纹问题．该问题归结为求解一组超奇异积分-微分方程．方程中的未知位移间断近似表示为基本密度函数与多项式之积,其中基本密度函数考虑到问题的对称性用二维界面裂纹精确解表示．在圆形片状裂纹的情况下,数值结果与现有理论解作比较的结果表明,数值结果与相应界面圆形片状裂纹和均质体圆形片状裂纹的精确解均吻合得很好．文中以图表形式给出应力强度因子与材料组合和几何条件之间的关系．     

自由端受集中力作用下压电悬臂梁弯曲问题解析解

本文对由横观各向同性压电介质构成的悬臂梁，在自由端受集中力作用下的弯曲问题进行了研究。首先根据问题的特点，得到简化的线弹性压电悬臂梁的基本方程。然后根据正交各向异性材料悬臂梁应力分布特点，采用逆解法，建立了该问题的应力函数与电势分布函数，进而得到精确多项式解析解。该解析解形式简单，便于应用。文中对自由端受集中力的常规材料和压电材料悬臂梁的挠度也进行了比较。     

用点源函数解受集中力圆板的非对称弯曲

本文将作用于板上任意位置的一个垂直于板中面的集中力看作一个点源,用δ函数表示,导出了受集中力作用的圆板非对称弯曲微分方程的封闭式特解和级数式齐次解,从而得出了适用于全板的统一的位移表达式。     

平行于异材界面的三维椭圆平片裂纹分析

讨论了拉伸载荷作用下平行于两相材料界面的椭圆平片裂纹问题．首先,使用有限部积分概念和两相材料界面完全接合时的点力基本解导出了一组以裂纹表面位移差为未知函数的超奇异积分方程组．该组方程表明,此时三种裂纹模型同时存在;其次,在数值求解该组方程的过程中,未知函数裂纹表面位移差被近似为位移差的基本密度函数与多项式之积．基本密度函数反映了裂纹前沿应力奇性性态;最后,以拉伸载荷为例,讨论了椭圆平片裂纹与界面的距离、裂纹形状比和不同材料组合对应力强度因子的影响,并以图表形式给出。     

Fundamental solution for bonded materials with a free surface parallel to the interface. Part II: Solutions of concentrated force acting at the interior of the substrate and the case when the force acting at the interface

In this work, the exact analyses are presented for the plane problem of a coating material subjected to a concentrated force acting at the interior of the substrate and the case when the force at the interface. The stress functions are constructed as an infinite series form by utilizing the method of image. According to the orders of the image points from lower to higher, the terms in the stress functions series have the recursive relationships. For the case when the force acting at the substrate, the first two terms are the original stress functions for a homogenous infinite plane subjected to a concentrated force, which are known and simple. For the case when the force acting at the interface, the fundamental solution is obtained for two bonded dissimilar semi-infinite plane. The stress functions in this solution can be used as the first two terms for the problem considered in this paper. Therefore, all other terms can be derived by the recurrence equations explicitly. Also, through comparisons between the theoretical results and the numerical results by FEM, it is verified that the convergence rate of the solutions is very rapid. In most practical cases only the first several image points can ensure the solutions with satisfactory accuracy.     

Fundamental solution for bonded materials with a free surface parallel to the interface. Part I: Solution of concentrated forces acting at the inside of the material with a free surface

The problem studied in this paper is that of a coated semi-infinite plane subjected to a concentrated force in the upper thin layer (or film). The elastic properties of the coating material are different from those of the substrate, and a perfect bond is assumed between the two materials. The exact solutions of stress functions in a series form are obtained by the method of image. The terms in series form of the stress functions correspond to the image points from the lower order to the higher. The recurrence relations of the stress functions are given, i.e., the stress functions corresponding to the higher order image points are determined by the lower ones. Hence, from the original stress functions for an infinite plane subjected to a concentrated force, the explicit formulas of all terms of the stress function series can be derived. Also, through comparisons between the theoretical results and the numerical results by FEM, it is verified that the convergence rate of the solutions is very rapid. In most practical cases only the first several image points are sufficient to ensure the accuracy of the solutions.     

磁电弹性圆锥顶端作用集中荷载的解析解

当磁电弹性材料特征根互异时，用5个势函数表示的通解出发，对圆锥顶端作用集中扭矩Mx的扭转、集中力Px和点电荷Q的压缩、集中力Px和集中力矩My的弯曲变形问题，用一些调和函数的线性组合分别构造了势函数，并根据边界条件求出了势函数中的待定系数从而确定势函数，再将势函数代入通解得到磁电弹性圆锥顶端作用集中载荷时的位移、电势、磁势、应力、电位移和磁感应强度的三维解析解。此解形式简单便于应用。当圆锥角2α=π时，可退化得到半空间问题的解。     

A Normal Force on the Free Surface of a Coated Material

The three-dimensional theoretical solution of a concentrated normal force acting on the free surface of a coated material has been deduced by applying the reflection method. It is found that all stress functions defined in the local coordinate systems with their origins placed at each mirror point can be deduced from the fundamental solution of a concentrated normal force acting on the free surface of a semi-infinite homogeneous medium. The structure of the elastic solution has been illustrated by numerical analysis. It is found that only the stress functions corresponding to the first few mirror points are influential. It is also found that the effect of material combination on the stress field shall be described by three parameters, the two Dundurs' parameters and one additional parameter.     

含界面效应纳米尺度圆环形涂层中螺型位错分析

研究了纳米尺度圆环形涂层(界面层)中螺型位错与圆形夹杂以及无限大基体材料的干涉效应.涂层与夹杂的界面和涂层与基体的界面均考虑界面应力效应.运用复势方法,获得了三个区域复势函数的解析解答.利用求得的应力场和Peach-Koehler公式,得到了作用在螺型位错上位错力的精确表达式.主要讨论了界面应力对涂层(界面层)中螺型位错运动和平衡稳定的影响规律.结果表明,界面应力对界面附近位错的运动有大的影响,由于界面应力的存在,可以改变涂层内位错与夹杂/基体干涉的引斥规律,并使位错在涂层内部产生三个稳定或非稳定的平衡点.考虑界面效应后,有一个额外的排斥力或吸引力作用在位错上,使原有的位错力增加或减小.     

Dynamic Green’s Functions for an Anisotropic Multilayered Poroelastic Half-Space

The dynamic responses of an anisotropic multilayered poroelastic half-space to a point load or a fluid source are studied based on Stroh formalism and Fourier transforms. Taking the boundary conditions and the continuity of the materials into consideration, the three-dimensional Green’s functions of generalized concentrated forces (force and fluid source) applied at the free surface, interface and in the interior of a layer are derived in the Fourier transformed domain, respectively. The actual solutions in the frequency domain can further be acquired by inverting the Fourier transform. Finally, numerical examples are carried out to verify the presented theory and discuss the Green’s fields due to three cases of a concentrated force or a fluid source applied at three different locations for an anisotropic multilayered poroelastic half-space.

     

含非完整界面涂层夹杂中螺型位错的弹性分析

研究了含非完整界面圆形涂层夹杂内部一个螺型位错在夹杂、涂层与无限大基体材料中产生的弹性场.运用复变函数函数方法,获得了三个区域复势函数的解析解答.利用求得的应力场和Peach-Koehler公式,得到了作用在螺型位错上位错力的精确表达式.主要讨论了两个非完整界面对位错力的影响规律.结果表明,涂层界面对夹杂内部螺型位错的吸引力随着界面粘结强度的弱化而变大.界面非完整程度增加削弱材料弹性失配对位错力的影响.在一定条件下,非完整界面可以改变夹杂内位错与涂层/基体系统之间的引斥干涉规律,并使位错在夹杂内部产生一个稳定或非稳定的平衡点.     

Dynamic Green’s functions of a two-phase saturated medium subjected to a concentrated force

The Green’s functions of a two-phase saturated medium subjected to a concentrated force are known to play an important role in seismology, earthquake engineering, soil dynamics, geophysics, and dynamic foundation theory. This paper presents a physical method for obtaining the dynamic Green’s functions of a two-phase saturated medium for materials considered to be isotropic and for low frequencies. First, the pore-fluid pressure in a two-phase saturated medium is divided into two parts: flow pressure and deformation pressure. Next, based on the compatibility condition of Biot’s equation and the property of the δ-function, the problem of coupled_fast and slow dilational waves is solved using the decomposition condition of the potential dilation field. The Green’s function for a concentrated force is then obtained by solving Biot’s complex modular equations, and their physical characteristics are discussed. The behavior of Green’s functions for the solid and fluid phases of a δ-impulsive force is investigated, from which the Green’s functions for a unit Heaviside force are also obtained by time integration. Finally, the present Green’s functions for a unit Heaviside force are compared with those obtained by a purely mathematical method; the two differ in form, but the numerical results are identical. The physical meaning of the expressions of Green’s functions obtained in this paper is evident. Therefore, the results may benefit future research on the dynamic responses of a two-phase saturated medium.     

GREEN＇S FUNCTIONS OF TWO－DIMENSIONAL ANISOTROPIC BODY WITH A PARABOLIC BOUNDARY

ＧＲＥＥＮ＇ＳＦＵＮＣＴＩＯＮＳＯＦＴＷＯ－ＤＩＭＥＮＳＩＯＮＡＬＡＮＩＳＯＴＲＯＰＩＣ ＢＯＤＹ ＷＩＴＨ Ａ ＰＡＲＡＢＯＬＩＣ ＢＯＵＮＤＡＲＹ（胡元太）（赵兴华）ＧＲＥＥＮ＇ＳＦＵＮＣＴＩＯＮＳＯＦＴＷＯ－ＤＩＭＥＮＳＩＯＮＡＬＡＮＩＳＯＴＲＯＰ?..     

Green’s functions for bending problem of a thin anisotropic plate with an elliptic hole

The Green’s functions have not been studied in open literatures for the bending problem of an anisotropic plate with an elliptic hole subjected to a normal concentrated force and a concentrated moment. In this paper, the problem is investigated and the Green’s functions are first obtained by using the complex potential approach. The techniques of conformal mapping transformation and analytic continuation are used to derive the closed-form complex stress functions. The Green’s functions obtained have some potential applications in the analysis of composite structures such as the modification of the displacement compatibility model for notched stiffened composite panels and the formulation of a new method for interlaminar stress analysis around holes of laminates.