厚扁球壳位移型基本方程及矩形底厚扁球壳控制方程的一般解

基于考虑横向剪切变形的厚壳位移型基本方程及扁壳基本假定,建立关于5个中面位移为5个独立变量的厚扁壳及厚扁球壳的位移型基本方程．对矩形底厚扁球壳的位移型基本方程（变系数十阶微分方程）,通过引入5个辅助位移函数,同时运用柯西——黎曼条件,建立其解耦的控制微分方程,最后使用5个辅助位移函数求出5个位移分量．厚扁壳的位移型基本方程退化为厚扁球壳及薄扁球壳的位移型方程的正确性说明所推导方程具有一般性．     

圆底球面厚扁壳的位移型控制方程及一般解

基于考虑横向剪切变形的厚壳位移型基本方程及扁壳基本假定,建立了以5个中面位移为5个独立变量的厚扁壳位移型基本方程,并由此得到厚扁球壳在正交曲线坐标及极坐标下的位移型基本方程。为了求解圆底球面厚扁壳在极坐标下的位移型基本方程,通过引入4个辅助位移函数,建立其解耦的控制微分方程,最后通过这4个辅助位移函数求出5个位移分量。结果表明,厚扁壳的位移型基本方程退化为厚扁球壳及薄扁球壳的位移型方程是正确的,且所推导方程具有一般性。     

考虑横向剪切变形厚旋转壳振动的位移型基本方程

本文基于考虑横向剪切变形的中厚旋转壳的几何方程、物理方程、中面平衡方程，建立关于五个中面位移u,v,w,Φ，Ψ为五个独立变量的中厚旋转壳振动的位移型基本方程。该方程退化为薄旋转壳、厚圆柱壳、厚圆锥壳及厚球壳振动的位移基本方程的正确性说明所推导方程具有一般性。     

网格圆柱扁壳的稳定性

本文用将网格壳转化为连续壳的方法建立了网格圆柱扁亮屋盖的稳定平衡微分方程,所得的方程是属于异性圆柱扁壳的方程,并用方法求得简支边界条件的网格圆柱扁壳的临界荷载计算公式。     

弹性地基上中厚扁球壳的弯曲

以中厚度扁球壳的一般理论为基础,得到了极坐标系下的弹性地基上中厚度扁球壳的基本方程.该控制方程组是十阶方程组(对轴对称问题,则为八阶方程组).以应力函数、位移函数和壳体中面的法向位移为基本未知量,利用混合法对该控制方程组进行了求解,所得的解析解答则是以三角级数、Bessel函数和调和函数表示的.求解结果表明,当n=0时,中厚度扁球壳每边的边界条件为3个;当n=1时,每边的边界条件为4个;当n>1时,每边的边界条件为5个.解答还可以退化到无地基影响的中厚度扁球壳的计算以及薄扁球壳的计算.文末对位于Win-kler弹性地基上的圆底封顶中厚度扁球壳进行了数值计算,并与薄壳理论的计算结果进行了比较.     

抛物旋转扁壳的大挠度问题

本文使用积分方程理论,将旋转扁壳轴对称大挠度问题的基本微分方程化成等效的积分方程,给出了积分方程的迭代解。     

层合板壳振动控制LQR方法的理论推导

从层合板壳弹性力学基本方程出发,考虑各种因素影响,导出统一形式的振动方程,利用LQR最优控制理论,根据能量原理确定了Q,R,求出符合条件的最优控制集中力,等效分布荷载的表达式及位移衰减函数。     

具有初始缺陷的扁球面网壳的混沌运动

在圆形三向网架非线性动力学基本方程的基础上,用拟壳法给出了具有初始缺陷圆底扁球面网壳的大挠度方程和非线性动力学基本方程.在固定边界条件下,引入了异于等厚度壳的无量纲量,对基本方程和边界条件进行无量纲化.首先求出扁球面网壳的大挠度解,继之将大挠度解当作扁球面网壳的初始缺陷,通过Galerkin作用得到了一个含二次、三次的非线性动力学方程.通过求Melnikov函数,给出了具有初始缺陷的扁球面网壳系统可能发生混沌运动的临界条件.通过数字仿真绘出了平面相图,证实了混沌运动的存在.同时也发现考虑初始缺陷的扁球面系统固有频率增大了,从而发生混沌运动的临界载荷值减小了.     

具有错边、角变形圆柱壳广义样条子域内时弹塑性分析

针对具有初始几何缺陷的非完善圆柱壳。以非等距B_3样条为基函数,采取分别沿子午向和环向插值的方式得到结点任意分布的广义样条子域位移模式,利用内时理论建立了壳体本构方程,并计入了温度的变化。对具有错边、角变形圆柱壳进行了弹塑性分析。结果表明该类缺陷对应力分布有着一定的影响,随着塑性变形的发展,其影响程度更大。     

弹性地基上扁球壳的自由振动

本文研究双参数弹性地基上扁球壳的自由振动频率和振型，推导了计及地基惯性力影响的扁壳自由振动控制方程。方程的精确解以贝塞尔函数表达。同时，分别导出了壳的经向、环向和横向位移分量的表示式。根据所得的解，文中给出了固定边扁球壳的频率方程和数值结果。同时。还给出了对应于前三个频率的振型变化曲线。     

板锥网壳结构的拟三层壳分析法

板锥网壳结构是一种受力性能合理 ,技术经济效益良好的新型空间结构形式。本文对板锥网壳结构提出了一种连续化的分析方法 ,根据其受力特点按照刚度等效的原理 ,采用弹性力学的基本方法推导出板锥网壳结构的等代壳体刚度 ,将其连续化为能共同作用的特殊形式的三层薄壳 ,按薄壳理论建立其位移法和混合法的基本微分方程。通过对微分方程的求解 ,计算其整体位移及结构内力。该法具有一定的精度 ,可宏观地了解结构的力学性能 ,并可用于板锥网壳结构的初步设计。     

埋置力源下横观各向同性饱和地基的三维Lamb问题解答

基于横观各向同性饱和介质的三维Biot波动方程,首先引入位移函数,将圆柱坐标系下的波动方程解耦,并利用算子理论,给出了Biot波动方程的通解。利用Fourier展开和Hankel变换,求解波动方程,得到土骨架位移、孔隙水压力和饱和介质总应力分量的积分形式一般解。其次,系统研究了横观各向同性饱和半空间体在埋置动力荷载作用下的三维Lamb问题,结合边界条件,给出了问题的基本解。算例表明,水平力作用下,荷载埋置较浅时,地表竖向位移幅值沿径向衰减迅速,埋深和频率增大时,地表位移波动性增强,衰减不明显。     

弹性地基上厚板的计算分析

以弹性地基上Reissner板为研究对象,地基采用双参数模型,把地基效应归并到厚板的弯曲微分方程中。利用导出的双参数地基上厚板弯曲问题的基本解,从虚功原理出发,依据胡海昌的中厚板弯曲理论,推导出三个广义位移表示的边界积分方程。适用于任意边界条件、任意形状及任意荷载的薄板及中厚板的弯曲问题。文中给出了算例,并对各种参数变化进行了分析,获得了满意的结果。     

Buckling and postbuckling behaviors of imperfect cylindrical shells subjected to torsion

Buckling and postbuckling behaviors of imperfect cylindrical shell subjected to torsion are investigated. The governing equations are based on the Karman–Donnell-type nonlinear differential equations. A boundary layer theory of shell buckling is applied to obtain the analytic solutions that meet the boundary conditions strictly. A singular perturbation technique is employed to determine the buckling loads and postbuckling equilibrium paths. Numerical results reveal that the current theory gives quite good estimates of the postbuckling paths of cylindrical shells. The effects of the geometric parameters on the buckling and postbuckling behaviors of the cylindrical shells are analyzed. It is confirmed that the postbuckling equilibrium paths of cylindrical shells subjected to torsion are unstable and the relatively shorter shells have higher postbuckling equilibrium paths. Finally, the effects of the initial imperfections on the buckling and postbuckling behaviors of the cylindrical shells are clarified. The illustrated results of the imperfect shells with different initial transverse deflections show that extremely small imperfections do indeed reduce the buckling loads and make the postbuckling equilibrium paths be lower. The buckling and postbuckling of cylindrical shells under torsion exhibit obvious imperfect sensitivity. Furthermore, the effects become greater following with the larger imperfections.     

均布荷载下多波连续球面扁壳的计算

本文根据扁壳的弯矩理论讨论了矩形底球面扁壳的解析解。给出的内力及位移分量的表达式可用来考虑连续壳体的边界影响。解析解采取单级数形式。通过数值计算的结果分析,证明解的收敛性较好,可满足工程设计的要求。已编制了输入数据简单且勿需较大内存的微机通用程序。     

On a special class of boundary-value problems in the theory of shells and plates

This paper is concerned with problems in shell theory in which displacements are specified on a major surface of a three-dimensional shell-like body. It is unclear whether the theory of shells is in fact applicable to such problems; in virtually any treatment of shells, the equations of motion are derived by assuming that the tractions on both major surfaces are known. These known tractions manifest themselves as body forces in the resulting two-dimensional set of equations. We demonstrate in this paper that provided certain modifications are made, the latter set can indeed be used to solve problems in which displacements are specified on a major surface. These modifications are essential; they in fact reduce the number of differential equations and change the nature of the boundary conditions. We outline a clear procedure to treat such problems. The procedure is general in that it is valid for finite deformations of shells made of any material. We illustrate the efficacy of the final set of equations by presenting some examples from the linear theory of elastic plates.     

Shallow shell finite element for the large deflection geometrically nonlinear analysis of shells and plates

An investigation into the large deflection, geometrically nonlinear behaviour of shells is carried out in the present paper. The finite element method is used in conjunction with linearised incrementation and the Newton-Raphson iterative technique.The finite element used is based on independent strain assumptions insofar as it is allowed by the compatibility equations. Strain-displacement relationships based on shallow shell formulation are used and applied to an element having three principal curvatures. The resulting element has the only essential external degrees of freedom, satisfies the exact requirement of strain free rigid body modes of displacements and can be used for the representation of cylindrical, spherical and hyperbolic paraboloid shells.Complex load-deflection curves are obtained for cylindrical and spherical shells by incrementing loads as well as deflections. The relative behaviour of cylindrical and spherical panels having the same overall dimensions are also discussed in terms of stiffness, instability and snap-through phenomena.