弹性力学空间轴对称问题通解的研究

本文证明了横观各向同性弹性力学空间轴对称问题的通解是完备的.这里φ满足同时得到了轴对称问题一个新的完备通解这里φ满足     

厚圆板轴对称振动的弹性力学解

本文以轴对称三维弹性力学基本方程为基础,导出厚圆板强迫振动的状态方程式。利用Ｍａｃｌａｕｒｉｎ级数和Ｓｙｌｖｅｓｔｅｒ定理,厚圆板的位移和应力可以用中面位移和应力的微分算子表示。通过载荷分解和圆板表面条件,可以得到厚圆板在对称载荷与反对称载荷作用下的振动控制方程。求解了厚圆板在周边固支和简支条件下的对称与反对称的自由振动问题。通过数值计算得到了这两类自由振动的固有频率。本文的方法适用于求解厚圆板在     

基于Kriging插值无网格法求解轴对称弹性力学问题

基于Kriging插值无网格法,提出了实际应用中复杂轴对称弹性力学问题求解的一条新途径.Kriging插值无网格法是一种新型的无网格法,该方法构造的形函数满足Kronecker delta函数性质,可以直接施加本质边界条件.采用Kriging插值无网格法分析轴对称问题,得到了轴对称问题的无网格离散方程,并编制了相应的计算程序.通过厚壁圆筒的静力学和动力学分析,对所提方法进行了检验.数值算例结果表明,提出的方法对求解轴对称弹性力学问题是行之有效的.     

弹性力学中拉梅问题的讨论

拉梅公式为厚壁圆筒问题计算中的基本公式,具体表达式为式中,σ_(?)、σ_θ分别为筒任一点处的径向应力和环向应力;p_a、p_b 分别为筒内、外表面所承受的压强;a、b 分别为筒内、外半径.     

弹性力学平面问题的位移型解答

本文证明了一个线性常系数偏微分方程的通解定理,利用这个通解定理导出了弹性力学平面问题的位移通解。     

弹性力学边界积分方程的一个发展

本文讨论二维弹性力学平面问题，独立于Ｒｉｚｚｏ型边界分方程，一类新型的边界积分方程，其边界场变量包含应力分量σｉｊｔｉｔｊ（其中ｔｉ是边界切向余弦）。该应力分量可直接用数值方法解边界积分方程求出，它比常规的边界元解提高一阶精度。文末的算例表明确定论的实用性和有效性。     

圆柱型各向异性弹性力学平面问题

本文对圆柱型各向异性弹性力学平面问题的基本方程进行了改写。在此基础上，导出了应力函数Ｇ和位移函数φ，它们满足相同的控制方程，比文〔１〕的应力函数Ｆ的控制方程要简单，便于求得特解，并有Ｆ＝ｒＧ的关系。还对若干经典问题进行了求解。     

弹性力学平面问题位移函数的研究

本文推导出各向同性弹性力学平面问题位移的完备通解,该位移通解的导出,使求解任何边界条件的平面问题成为现实     

弹性力学空间问题的复变函数解

弹性力学空间问题的复变函数解贾普荣（西北工业大学,西安７１００７２）１基本方程对于弹性力学一般的空间问题,位移和应力分量可用伽辽金的３个双调和函数表出￣［１］。设ｆ＿１（ｘ,ｙ,ｚ）,ｆ＿２（ｘ,ｙ,ｚ）,ｆ＿３（ｘ,ｙ,ｚ）为双调和函数,即位移分量...     

线性变厚度圆锥壳扭转振动的弹性力学理论解

本文给出线性变厚度圆锥壳轴对称扭转振动的弹性力学理论解,探讨壳体的无剪扭振和剪切扭振,揭示了圆锥壳在厚度方向剪切、母线方向扭转的耦合振动特性。这些性质用经典壳理论是无法反映的。文末算例用许多数据表和曲线图描述变厚度圆锥壳的周有频率和振型。     

The representation problem of constrained linear elasticity

The title problem is given the following explicit solution: = _D S|D, where the elasticity tensor in the constrained case is the restriction to the constraint subspace D of a corresponding unconstrained elasticity tensor S, followed by composition with the orthogonal projection _D on D.     

Solution of a Riemann problem for elasticity

This paper describes a numerical algorithm for the Riemann solution for nonlinear elasticity. We assume that the material is hyperelastic, which means that the stress-strain relations are given by the specific internal energy. Our results become more explicit under further assumptions: that the material is isotropic and that the Riemann problem is uniaxial. We assume that any umbilical points lie outside the region of physical relevance. Our main conclusion is that the Riemann solution can be obtained by the iterative solution of functional equations (Godunov iterations) each defined in one- or two-dimensional spaces.Supported in part by AFOSR-88-0025.     

The Boussinesq problem in dipolar gradient elasticity

The three-dimensional axisymmetric Boussinesq problem of an isotropic half-space subjected to a concentrated normal quasi-static load is studied within the framework of dipolar gradient elasticity involving linear constitutive relations and small strains. Our main concern is to determine possible deviations from the predictions of classical linear elastostatics when a more refined theory is employed to attack the problem. Of special importance is the behavior of the new solution near to the point of application of the load where pathological singularities exist in the classical solution. The use of the theory of gradient elasticity is intended here to model the response of materials with microstructure in a manner that the classical theory cannot afford. A linear version of this theory (as regards both kinematics and constitutive response) results by considering a linear isotropic expression for the strain-energy density that depends on strain gradient terms, in addition to the standard strain terms appearing in classical elasticity and by considering small strains. Through this formulation, a microstructural material constant is introduced, in addition to the standard Lamé constants. The solution method is based on integral transforms and is exact. The present results show significant departure from the predictions of classical elasticity. Indeed, continuous and bounded displacements are predicted at the points of application of the concentrated load. Such a behavior of the displacement field is, of course, more natural than the singular behavior exhibited in the classical solution.     

An elasticity solution of a nonhomogeneous half-plane problem

ＡＮＥＬＡＳＴＩＣＩＴＹＳＯＬＵＴＩＯＮＯＦＡＮＯＮＨＯＭＯＧＥＮＥＯＵＳＨＡＬＦ－ＰＬＡＮＥＰＲＯＢＬＥＭＷｏＧｕｏ－ｗｅｉ（沃国纬）（ＳｈａｎｇｈａｉＪｉａｏｔｏｎｇＵｎｉｖｅｒｓｉｔｙ．Ｓｈａｎｇｈａｉ）（ＲｅｃｅｉｖｅｄＪａｎ．５．１９９４：...     

The problem of sharp notch in couple-stress elasticity

The problem of sharp notch in couple-stress elasticity is considered in this paper. The problem involves a sharp notch in a body of infinite extent. The body has microstructural properties, which are assumed to be characterized by couple-stress effects. Both symmetric and anti-symmetric loadings at remote regions are considered under plane-strain conditions. The faces of the notch are considered traction free. To determine the field around the tip of the notch, a boundary-layer approach is followed by considering an expansion of the displacements in a form of separated variables in a polar coordinate system. Our analysis is in the spirit of the Knein–Williams and Karp–Karal asymptotic techniques but it is much more involved than its corresponding analysis of standard elasticity due to the complicated boundary value problem (higher-order system of governing PDEs and additional boundary conditions as compared to the standard theory). Eventually, an eigenvalue problem is formulated and this, along with the restriction of a bounded potential energy, provides the asymptotic fields. The cases of a crack and a half-space are analyzed as limit cases of the general notch problem. Certain deviations from the standard classical elasticity results are noted.     

An old elasticity problem in a unilateral setting

A limiting case of the Michell problem involving an elastic wedge is the unbounded solid with a semi-infinite cut, the tip of which is subjected to a concentrated force. For the limiting case, the classical solution leads to overlapping of material whenever the component of the force along the axis of symmetry is directed away from the cut, and the problem must be solved anew using unilateral boundary conditions. The required mathematics is simple, and the subject is suitable for classroom discussion. Two examples are solved explicitly, and additional exercise problems are suggested.     

THE MIXED BOUNDARY-VALUE PROBLEM FOR NON-LOCAL ASYMMETRIC ELASTICITY

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New Statement of the elasticity problem for a layer

The problem on the equilibrium of an inhomogeneous anisotropic elastic layer is considered. The classical statement of the problem in displacements consists of three partial differential equations with variable coefficients for the three displacements and of three boundary conditions posed at each point of the boundary surface. Sometimes, instead of the statement in displacements, it is convenient to use the classical statement of the problem in stresses [1] or the new statement of the problem in stresses proposed by B. E. Pobedrya [2]. In the case of the problem in stresses, it is necessary to find six components of the stress tensor, which are functions of three coordinates. The choice of the statement of the problem depends on the researcher and, of course, on the specific problem. The fact that there are several statements of the problem makes for a wider choice of the method for solving the problem. In the present paper, for a layer with plane boundary surfaces, we propose a new statement of the problem, which, in contrast to the other two statements indicated above, can be called a mixed statement. The problem for a layer in the new statement consists of a system of three partial differential equations for the three components of the displacement vector of the midplane points. The system is coupled with three integro-differential equations for the three longitudinal components of the stress tensor. Thus, in the new statement, just as in the other statements in stresses, one should find six functions. In the new statement, three of these functions (the displacements of the midplane points) are functions of two coordinates, and the other three functions (the longitudinal components of the stress tensor) are functions of three coordinates. It is shown that all equations in the new statement are the Euler equations for the Reissner functional with additional constraints. After the problem is solved in the new statement, three components of the displacement vector and three transverse components of the stress tensor are determined at each point of the layer. The new statement of the problem can be used to construct various engineering theories of plates made of composite materials.