ANALYSIS OF SYMMETRIC LAMINATED RECTANGULAR PLATES IN PLANE STRESS

Symmetric laminated plates used usually are anisotropic plates. Based on the fundamental equation for anisotropic rectangular plates in plane stress problem, a general analytical solution is established accurately by method of stress function. Therefore the general formula of stress and displacement in plane is given. The integral constants in general formula can be determined by boundary conditions. This general solution is composed of solutions made by trigonometric function and hyperbolic function, which can satisfy the problem of arbitrary boundary conditions along four edges, and the algebraic polynomial solutions which can satisfy the problem of boundary conditions at four corners. Consequently this general solution can be used to solve the plane stress problem with arbitrary boundary conditions. For example, a symmetric laminated square plate acted with uniform normal load, tangential load and nonuniform normal load on four edges is calculated and analyzed.     

ON THE STRONG SINGULAR METHOD FOR THE PROBLEMS OF SUBSONIC FLOW PAST OBSTACLES

The purpose of this paper is to give a new investigation onthe doublet elementary solution method of solving the problem ofsubsonic flow.A strong singular integral equation is produced.The definition and the calculating formula of the effective prin-ciple value of strong singular integral are given.From this in-tegral equation,some numerical methods corresponding to the wholecontinuous distribution of elementary solution can be deduced.This method is applicable to calculating subsonic aerodynamicforce.     

FREE VIBRATION OF ANISOTROPIC RECTANGULAR PLATES BY GENERAL ANALYTICAL METHOD

According to the differential equation for transverse displacement function of anisotropic rectangular thin plates in free vibration, a general analytical solution is established. This general solution, composed of the composite solutions of trigonometric function and hyperbolic function, can satisfy the problem of arbitrary boundary conditions along four edges. The algebraic polynomial with double sine series solutions can also satisfy the problem of boundary conditions at four corners. Consequently, this general solution can be used to solve the vibration problem of anisotropic rectangular plates with arbitrary boundaries accurately. The integral constants can be determined by boundary conditions of four edges and four corners. Each natural frequency and vibration mode can be solved by the determinate of coefficient matrix from the homogeneous linear algebraic equations equal to zero. For example, a composite symmetric angle ply laminated plate with four edges clamped has been calculated and discussed.     

SOLUTION OF NONLINEAR HEAT CONDUCTION EQUATION AND IMAGE METHOD

In this paper,the author proves that, for a nonlinear heat conduction equation, there is no discontinuous solution. Some methods of solution for a nonlinear conduction equation are depicted. For a plane interface, the reflection and transmission of a heat wave are given by the method of images. The 1st order of approximation of this method is proved. Lastly, the prevention of superheated electrons is laser implosion of deuterium tritium gas sphere with a shell made of high Z material is interpreted.     

NUMERICAL SIMULATION OF COMPLICATED PIPE FLOW WITH k-εMODEL

In this paper, turbulence in a complicated pipe is simulated by using the k-ε model. The ladder-like mesh approximation is used to solve the problem of complicated boundary with the result of numerical simulation favorable. Two computational examples are given to validate the strong adaptability and stability of k-ε model.     

Iterative approximation of the solution of a locally Lipschitzian equation

Suppose X=L_p,(or l_p),p>2.T:D(T)→X is a locally Lipschitzian and strictlyaccretive operator.In this paper.the iterative approximation of the solution of nonlinearequation Tx=y is given and the iterative approximation of a fixed point of a locallyLipschitzian and strictly pseudo-contractive mapping is discussed.     

INVESTIGATION OF BEHAVIOR OF MODE-Ⅰ INTERFACE CRACK IN PIEZOELECTRIC MATERIALS BY USING SCHMIDT METHOD

The behavior of a Mode-Ⅰ interface crack in piezoelectric materials was investigated under the assumptions that the effect of the crack surface overlapping very near the crack tips was negligible. By use of the Fourier transform, the problem can be solved with the help of two pairs of dual integral equations. To solve the dual integral equations, the jumps of the displacements across the crack surfaces were expanded in a series of Jacobi polynomials. It is found that the stress and the electric displacement singularities of the present interface crack solution are the same as ones of the ordinary crack in homogenous materials. The solution of the present paper can be returned to the exact solution when the upper half plane material is the same as the lower half plane material.     

Multiresolution method for bending of plates with complex shapes

A high-accuracy multiresolution method is proposed to solve mechanics problems subject to complex shapes or irregular domains. To realize this method, we design a new wavelet basis function, by which we construct a fifth-order numerical scheme for the approximation of multi-dimensional functions and their multiple integrals defined in complex domains. In the solution of differential equations, various derivatives of the unknown function are denoted as new functions. Then, the integral relations ...     

ON PROBLEM OF NEAREST COMMON FIXED POINT OF NONEXPANSIVE MAPPINGS

The purpose is by using the viscosity approximation method to study the convergence problem of the iterative scheme for an infinite family of nonexpansive mappings and a given contractive mapping in a reflexive Banach space. Under suitable conditions, it was proved that the iterative sequence converges strongly to a common fixed point which was also the unique solution of some variational inequality in a reflexive Banach space. The results presented extend and improve some recent results.     

ANALYTICAL SOLUTION FOR MODE Ⅲ DYNAMIC RUPTURE OF STANDARD LINEAR VISCOELASTIC SOLID WITH NONLINEAR DAMPING

Introducing the nonlinear Rayleigh damping into the governing equation of the Mode Ⅲ dynamic rupture for standard viscoelastic solid, this equation is a partial differential and integral equation. First, eliminating the integral term, a PDE of third-order is obtained. Then, applying the small parameter expansion method, linearized asymptotic governing equation for each order of the small parameter is obtained. Dividing the third-order PDE into an elastic part with known solution, the rest part pertains to viscous effect which is neither a Mathieu equation nor a Hill one. The WKBJ method is still adopted to solve it analytically.     

Orthogonal polynomials and determinant formulas of function-valued Padé-type approximation using for solution of integral equations

To solve Fredholm integral equations of the second kind, a generalized linear functional is introduced and a new function-valued Padé-type approximation is defined. By means of the power series expansion of the solution, this method can construct an approximate solution to solve the given integral equation. On the basis of the orthogonal polynomials, two useful determinant expressions of the numerator polynomial and the denominator polynomial for Padé-type approximation are explicitly given. Project supported by the National Natural Science Foundation of China (No.10271074)     

KdV-Burgers方程的级数解

给出ＫｄＶ－Ｂｕｒｇｅｒｓ方程的有界行波解的精确级数解,采用Ａｄｏｍｉａｎ算子分解法分别求行二个区域ζ〈０和ζ〉０的级数解,然后利用对接连续条件构成整体级数解。所得级数解能精确满足对接连续条件,并由此得到确定级数的系数递推公式,无需解非红性高阶代数方程组。与某些精确解及其它方法比较,计算简捷具在对接点处是收剑的。对某些非线性波动现象的研究,可作为计算和分析的数学依据。     

局部彼得洛夫-伽辽金法分析各向异性板屈曲

基于Kirchhoff板理论和对挠度函数采用移动最小二乘近似函数进行插值，进一步研究无网格局部Petrov-Galerkin(MLPG)方法在各向异性板稳定问题中的应用．分析中，本质边界条件采用罚因子法施加，离散的特征值方程由板稳定控制方程的局部积分对称弱形式中得到．通过数值算例并与其他方法的结果进行比较，表明MLPG法求解各向异性薄板稳定问题具有收敛性好、精度高等一系列优点．     

非均匀介质散射问题的体积分方程数值解法

将非均匀介质视为某一均匀背景介质中的扰动，可建立用均匀背景介质格林函数作基本解的体积分方程．给出了配置法求解体积分方程的数值方法，首先解得扰动域内各点以速度扰动为权的波场函数，然后回代计算得到观测面上各接收点的散射波场．与边界元法和Ｂｏｒｎ近似法计算结果比较表明该方法具有很高的精度，可得到穿过非     

Large deflections of a beam subject to three-point bending

In this paper, a solution for the equilibrium configuration of an elastic beam subject to three-point bending is given in terms of Jacobi elliptical functions. General equations are derived, and the domain of the solution is established. Several examples that illustrate a use of the solution are discussed. The obtained numerical results are compared with the results of other authors. An approximation formula by which the beam load is given as a polynomial function of beam deflection is also derived. The range of applicability of the approximation is illustrated by numerical examples.     

One solution of an axisymmetric problem of the elasticity theory for a transversely isotropic material

A numerical-analytical method based on approximation of the sought solution by a system of basis functions is proposed to solve the boundary-value problem of axisymmetric deformation of articles made of a transversely isotropic material. An algorithm for constructing polynomial functions on the basis of invariant-group solutions is described.     

有限长界面裂纹对冲击载荷的响应

本文研究了受冲击载荷作用下界面裂纹的瞬态特性。通过引入裂纹尖端附近裂纹面无摩擦接触区,消除了界面裂纹问题中存在的振荡奇异性。由于产生了随时间变化的运动边界,应用积分变换及路径积分方法进行反演,在时间-空间域上给出了问题的控制积分方程。应用chebyshev多项式展开,将问题转化为非线性微分-积分方程组的求解。给出了剪切应力强度因子和裂纹面接触区尺寸的数值结果。所得结果表明,拉伸场中界面裂纹的扩展和剪切失效有密切关系。     

超空化航行体气体流量率的确定方法研究

通气超空化技术是大幅提高水下航行体速度的重要途径,通气流量率的确定是实现该技术的核心问题之一. 通常 的流量率预估没有考虑雷诺数的影响,因而造成统计数据过于分散. 基于边界层理论及其相关假设,提出了一种确定人工通气超空化气体流量率的预估方法,并引用相关试验数据进行验证. 结果表明,所得近似关系式在雷诺数为0.35×10⁵～ 5.4×10⁵, 空化器锥角为30°～ 180°的变化范围内都是适用的.     

基于DDA的弹性力学全高阶多项式位移逼近方法及其实例验证

基于维尔斯特拉斯多项式函数的逼近定理,通过DDA高阶全多项式位移函数条件下的弹性力学推导,提出了一个逼近弹性力学连续位移函数真解的全多项式位移函数逼近方法。该方法采用完整的高阶多项式位移函数,以不同阶次条件下的多项式系数为未知数,以单纯形积分为解析积分方法,通过建立和求解平衡方程,逐步逼近弹性体真解。在对单纯形积分计算过程研究的基础上,给出了三维空间单纯形计算图解法,该图解法诠释了三维空间单纯形积分公式中各变量间的逻辑关系及计算过程的图形表达。基于上述方法,编写了相应计算程序,并以一个三维简支梁受均布荷载及一个四周固定的弹性薄板受集中力作用两算例为实例,验证了所提方法的可行性。实例计算结果表明,随着逼近函数阶次的提高,数值方法获得的多项式函数计算值均单调地逐步逼近解析解。在文中所用的6阶多项式函数逼近中,简支梁实例位移计算误差小于0.2%,弹性薄板实例位移误差小于0.91%,并且,两算例与解析解位移差值都在微m级。