受谐激励的带压电层充液圆柱容器稳态解

基于线性压电理论和可压缩无粘流场运动方程,推导出无限长带压电圆柱体流固耦合稳态解,由于流固耦合与力电耦合的复杂性,文中只考虑轴对称问题,研究了流固耦合智能结构在不同电压作用下位移、应力、流体压力的分布情况,为振动噪声控制奠定基础。     

无限均质弹性体中圆片裂纹受均布载荷时的超奇异积分方程封闭解

本文运用一种特殊技巧将一个受均布压力作用的圆片裂纹超奇异积分方程化为Ａｂｅｌ积分形式，从而可获得超奇异积分方程中未知位移间断的封闭解。再利用这个封闭解和应力强度因子的定义，得到了一个无限弹性体中受均布载荷分布时圆片裂纹前沿Ｉ型应力强度因子的精确表达式。所得到的结果与现有解完全相同。     

径向辛体系一种新的差分格式

通过对Hellinger-Reissner变分原理进行坐标变换,将径向模拟为时间,导向辛体系,得到Hamilton对偶方程组.将微分形式的有限差分法引入弹性力学极坐标系下径向辛体系,把对偶方程组中的微分方程直接改用差分方程代替,推导出极坐标系下问题的辛差分方程,从而得到一种全新的径向辛体系差分格式.求解方程组,可直接得到位移和应力.编程计算曲梁等算例,结果表明该辛差分格式是有效的,丰富了弹性力学辛体系差分法的内容.     

直角坐标下厚圆柱扁壳弯曲的一般解

基于直角坐标下考虑横向剪切变形情况下厚圆柱扁壳的几何方程、物理方程、平衡微分方程,建立了以3个中面位移和2个中面转角为独立变量的中厚圆柱扁壳弯曲的位移型基本微分方程.因该方程可退化为薄圆柱扁壳弯曲的基本微分方程,说明了其推导过程的正确性及一般性.此外,厚圆柱扁壳的位移型基本微分方程是一个10阶微分方程,对其使用双重三角...     

无限粘弹介质中圆孔时变问题的解析分析

本文推导粘弹介质中圆孔孔径时变时的应力和位移.由粘弹解与弹性解的对应关系得到粘弹时变应力解.用直接解方程法求径向位移,最终归结为求解关于待定函数的l阶非齐次微分方程.将半径时变函数泰勒展开,用幂级数解法得到一般情况下的解.在寻找定解条件时,采用了对待定函数的光滑化处理,认为在t=0的微小邻域内函数仍满足微分方程,通过积分得到与待定系数数目相同的定解条件,从而获得本问题径向位移解析解.对Maxwell粘弹模型的求解证明了该法的可靠性.文中解适用于任意粘弹模型和孔径任意时变的情况.     

纤维增强复合材料层合球壳的应力分析

1. 引言本文对受内压的复合材料球壳应用经典层合理论进行应力应变的分析。由一般球形壳体理论的五个平衡方程、六个几何方程及由层合理论导出的六个物理方程,共有十七个独立的方程可求解十七个未知函数,它们是三个中面位移、三个中面应变、三个曲面的曲率变化、五个应力合力、三个合力矩。应用球形壳体的应力函数U以后,得到二个基本微分方程。如为对称铺设此二基本微分方程可以简化。本文用有限差分法解此二基本微分方程。2. 基本方程的推导球壳的平衡方程如下:     

四边简支各向同性矩形厚板的插值矩阵法解

针对强厚度矩形板四边简支情况,论文根据状态变量法思想,基于三维弹性理论基本方程,以3个位移分量及3个应力分量按双三角级数展开,将三维弹性力学控制方程转化为常微分方程边值问题.尽管一些各向异性弹性矩形厚板早已由状态空间法获得分析解,可是各向同性厚板的分析解至今难以获得,因为状态空间解法中特征方程有重根问题而不易于收敛.论文提出采用插值矩阵法直接对常微分方程进行求解,获得各向同性矩形厚板在四边简支边界条件下三维理论的位移和应力解,并与有限元精细结果进行比较,证明了本文解的准确性.     

阶梯式变厚度旋转轮盘的应力解析解

本文应用广义函数导出阶梯式变厚度旋转轮盘的位移微分方程，用Ｗ运算符来表述和求解轮盘的位移和应力，并将此法应用于计算汽轮机轮盘的应力     

任意荷载作用下成层粘弹性体的求解

基于粘弹性体经关于时间：作Ｌａｐｌａｃｅ变换的基本方程的转换及Ｈａｎｋｅｌ变换,得到了任意荷载作用情形下,无限粘弹性层不同深度经这两种的位移应力向量间的传递矩阵。运用该传递矩阵可求解成层的层全拼情形的多种弹性模型的空间总理２。本文最后用这种方法计算了一个算例。     

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.     

Three-dimensional elastostatics of a layer and a layered medium

This paper is concerned with the determination of the distribution of stresses and displacements in an infinite three-dimensional, linear, elastic, isotropic, homogeneous layer subjected to concentrated body forces acting upon an arbitrary internal point.In §2 and §3 the governing partial differential field equations are reduced to a system or ordinary differential equations by the use of the two-dimensional Fourier transform, taken with respect to the two in-plane geometric variables (§4). Analytical expressions for the stresses and displacements are then obtained for the particular case of concentrated body forces, represented as Dirac delta functions (§5).The results are subsequently utilized to formulate the multilayered medium problem by means of transfer matrices. In §8 the typical problem of a non-adhesive layered medium is undertaken.     

层合厚板混合状态Hamiltonian动力元及其半解析解

文中在时间方向采用Ｌａｐｌａｃｅ变换，给出了层合厚板动力学问题混合状态Ｈａｍｉｌｔｏｎ正则方程及其半解析法．该方法在层板平面内采用通常的有限元离散，而沿板厚方向采用状态控制方程给出解析解答．在层与层之间采用迁移矩阵法，给出层合板上下表面力学量之间的关系式．利用打靶法得到响应在象空间的一般解，然后再利用拉氏逆变换的数值解求出层合板的瞬时位移场和应力场．     

Interaction of plane elastic harmonic waves with a perfectly bonded elastic inclusion

The interaction of plane harmonic waves with a thin elastic inclusion in the form of a strip in an infinite body (matrix) under plane strain conditions is studied. It is assumed that the bending and shear displacements of the inclusion coincide with the displacements of its midplane. The displacements in the midplane are found from the theory of plates. The priblem-solving method represents the displacements as discontinuous solutions of the Lamé equations and finds the unknown discontinuities solving singular integral equations by the numerical collocation method. Approximate formulas for the stress intensity factors at the ends of the inclusion are derived     

Numerical solution of three-dimensional static problems of elasticity for a body with a noncanonical inclusion

A boundary-element scheme is proposed for the numerical determination of the stress-strain state of a three-dimensional composite body, which is an elastic inclusion of arbitrary shape perfectly bonded to an infinite elastic matrix. The scheme involves the reduction of the original problem to six boundary integral equations for the components of interfacial displacements and forces and the boundary-element parametrization and discretization of these equations using generalized Gaussian integrals and topological maps with regularizing Jacobians. Numerical results are obtained for a cylindrical inclusion with rounded ends in a matrix subject at infinity to constant forces acting along this fiber. The influence of the length-to-radius ratio of the fiber and the ratio of the elastic moduli of the matrix and fiber on the stresses is examined __________ Translated from Prikladnaya Mekhanika, Vol. 43, No. 4, pp. 27–35, April 2007.     

多层压电材料层合板的精确解

抛弃有关位移和应力的所有假设，直接从三维弹性力学理论的静电学理论，先导出正交各向异性压电材料板的状态方程，由此得到四边简支压电材料板的状态主程，再根据矩阵分析理论，建立了单层压电材料板的上下表面状态量之间的关系，进一步建立了多层压电板上，下表面状态量之间关系式，利用上下表面已知状态量，得到上表面未知状态的求解方程解。通过求解方程组，便得上表面未知状态量，最终可以得到任意位置处状态量，最后，同时给出了四边简支，两层不同压电材料组成，不同纵横比的层合板受正弦分布载荷作用下的精确解，其结果与现有解比较，吻合较好。     

层状饱和土Biot固结问题状态空间法

针对饱和多孔介质空间非轴对Biot固结问题，引入状态变量，构造了两组相比独立的状态变量方程，利用Fourier级数和Laplace-Hankel变换，将状态变量方程转换为两组一阶常微分方程组，提出了均质饱和多孔介质空间非轴对称Biot固结问题的传递矩阵，得到以状态变量和传递矩阵乘积的形式表示的均质饱和多孔介质空间非轴对称Biot固结问题的解，利用层间完全接触的条件，可得到N层饱和多孔介质空间非轴对称Biot固结问题的一般解析表达式，文中考虑几种不同的边界条件，分析了两个算例，数值结果表明该方法具有较高的计算精度和良好的计算稳定性。     

饱和土体中圆柱形孔洞的动力分析

本文采用工程通用的土力学模型，利用积分变换法推导了置于饱和土体中的圆柱形孔洞瞬态动力响应解答的一般解析表达式，并将其与经典弹性动力学中圆柱形空腔问题的解答作了有价值的比较，文末利用一种十分有效的数值反变换方法给出了有意义的算例。本文为进一步分析岩土工程、地震工程中隧道、管道等地下结构的动力响应提供了有效途径，具有理论与应用价值。     

A general solution for static piezothermoelastic problems of crystal class 6mm solids

In this paper, a general solution for three-dimensional static piezothermoelastic problems of crystal class 6mm solids is presented. The general solution involves four piezoelastic potential functions and a piezothermoelastic potential function, of which four piezoelastic potential functions are governed by weighted harmonic differential equations. Compared with the general solution given by Ashida et al., in which seven potential functions are introduced, the general solution proposed in the present paper is more rigorously derived. Moreover, it has a simple form and is convenient for application. As an illustrative example, the problem of a pyroelectric half-space subjected to axisymmetric heating is studied. Numerical results of displacements stresses, electric potential and electric displacements are obtained for a cadmium selenide half-space. Thermally induced displacements and stress distribution are compared with those obtained for the same material without piezoelectric and pyroelectric effects. Project supported by the National Natural Science Foundation of China (19872060).     

State space solution to 3D multilayered elastic soils based on order reduction method

Starting with the governing equations in terms of displacements of 3D elastic media, the solutions to displacement components and their first derivatives are obtained by the application of a double Fourier transform and an order reduction method based on the Cayley-Hamilton theorem. Combining the solutions and the constitutive equations which connect the displacements and stresses, the transfer matrix of a single soil layer is acquired. Then, the state space solution to multilayered elastic soils is further obtained by introducing the boundary conditions and continuity conditions between adjacent soil layers. The numerical analysis based on the present theory is carried out, and the vertical displacements of multilayered foundation with a weak and a hard underlying stratums are compared and discussed.     

Reducing three-dimensional elasticity problems to two-dimensional problems by approximating stresses and displacements by legendre polynomials

Shell equations are constructed in orthogonal curvilinear coordinates using approximations of stresses and displacements by Legendre polynomials. The order of the constructed system of differential equations is independent of whether stresses and displacements or their combination are specified on the shell surfaces, which provides the correct formulation of the surface conditions in terms of both displacements and stresses. This allows the system of differential equations of laminated shells to be constructed using matching conditions for displacements and stresses on the contact surfaces. __________ Translated from Prikladnaya Mekhanika i Tekhnicheskaya Fizika, Vol. 48, No. 3, pp. 179–190, May–June, 2007.