圆柱壳在两种非轴对称同步移动载荷作用下的动力响应

本文根据工程实例计算的需要,研究了有限长弹性圆柱薄壳在两种非轴对称同步移动载荷作用下的动力响应问题。两种非轴对称同步移动载荷作用是指非轴对称移动的集中载荷,以及同步移动且作用范围随移动位置增加的均布载荷的共同作用。建立了在上述两种不同类型载荷作用下的具有对称形式的动力学微分方程组;分别采用Dirac函数与Heaviside函数表示移动的均布载荷与集中载荷,设定位移函数的基础上,应用Galerkin法及Laplace变换,求得了圆柱薄壳应力与位移动态响应的解析解;通过具体算例,将所得到解析解的计算结果与ANSYS数值解进行了对比分析,验证了解析解的可靠性。     

薄壳的低频振动

用奇异摄动理论给出了一般形状旋转薄壳的低频自由振动解。此时,本征模态在壳内是无矩的,在边界附近存在边界层。文中列出了全部可能的齐次边界条件下的求解步骤和结果。最后,给出了圆柱壳的数值算例。     

变厚度锥壳方程及其渐近解

本文用薄壳理论导出了壁厚线性变化的锥壳在承受轴对称截荷时的复变量方程，在薄壳理论误差范围内求得了齐次方程的渐近解和工程实用载荷的非齐次解，并给出了算例。     

充满液体的封闭圆柱壳受轴压时屈曲过程的实验研究

报导了对充满水的金属圆柱薄壳在轴向压缩时屈曲性能的实验结果。实验观察表明，充满液体的金属圆柱壳在轴压作用下的屈曲模态呈轴对称型，液体的内压与外部轴压随轴向缩短的变化趋势大致相同。由于壳内液体的存在，同内空的圆柱壳相比只是临界载荷略有提高，屈曲后承载能力并无显著降低，且对初始几何缺陷表现得远不象内空柱壳那样敏感。     

轴对称正交异性圆环壳的齐次完全渐近解

承受轴对称载荷的正交异性圆环壳的静力分析,归结为求解一非齐次二阶复变量方程.当所含参数μ较大时,常采用渐近解法.因方程含一阶转点,所以求全域一致有效且达到薄壳理论精度的完全渐近解较为困难.过去,齐次解只求到一级近似.本文采用广义Airy函数方法,求出了高级近似.这样,轴对称正交异性圆环壳的齐次解第一次有了达到薄壳理论精度的完全的渐近展开.     

用Green函数求解扁球壳受环状线载和线偶作用的问题

本文从复变量形式的扁壳基本方程出发,通过建立复Green函数导出了在环状线载和线偶作用下扁球壳的位移和内力分布,通过积分可以求得轴对称的表面受变化分布载荷情况的解答,本文方法还可求得圆饭、圆柱壳等问题的解答,而且适用于各种轴对称边界条件。     

钢筋混凝土圆球壳基于双剪屈服准则无矩理论的极限分析

利用已建立的基于双剪屈服准则的钢筋混凝土壳体的屈服条件,研究了圆球壳屈服时无矩理论下内力状态,导出了壳体各区域的本构关系和塑性屈服条件,并用机动法和静力平衡法计算了圆球壳在竖向均布载下的极限载荷.计算结果与用已有的塑性屈服线理论计算结果相符.     

线载荷作用下圆柱壳环向弯曲变形的研究

通过引入单三角级数形式的位移函数, 求解了法向任意分布载荷作用下对 边简支时圆柱壳的环向弯曲问题, 把线载荷近似为微元矩形区的分布载荷, 推导出了线 载荷作用下圆柱壳的环向弯曲变形计算式, 并给出了线载荷为均布和线性变化时的具体解. 计算表明, 该种边界约束条件下圆柱壳的环向弯曲变形位移分布场的理论计算结果与有限元 分析结果基本吻合.     

正交各向异性功能梯度圆柱壳的应力分析及材料剪裁

假设正交各向异性功能梯度材料的弹性系数沿圆柱壳的径向按照任意连续函数变化,采用应力函数法和加权残值法导出了圆柱壳在非轴对称载荷作用下应力分析的一种新的数值解.建立了圆柱壳内部应力状态给定时材料剪裁问题的基本方程,提出了实现圆柱壳内部一种特殊的应力分布时所需要的材料弹性系数沿径向变化的解析解.通过数值算例验证了本文所导出的应力分析的数值解的正确性和收敛性,分析了弹性系数沿径向的变化对圆柱壳内部应力分布的影响.数值算例还给出了实现圆柱壳内部环向应力和切应力沿径向均匀分布时功能梯度材料的弹性系数沿径向的三种不同变化形式.所得研究结果可为正交各向异性功能梯度材料圆柱壳的设计提供一定的参考,同时材料剪裁的解析结果也可作为其他数值方法计算结果验证的考题.     

圆柱壳的非线性动力屈曲分析

本文研究在轴向冲击作用下，具有初始几何缺陷的圆柱壳的非线性弹性动力屈曲问题。由于冲击过程中作用时间极短，应力波的影响变得相当重要，同时认为圆柱壳经历大挠度变形。分析中不仅考虑圆柱壳的径向惯性力，而且也考虑轴向惯性力和几何非线性的影响。假设圆柱壳中位移和薄膜力可分成轴对称分量和非轴对称分量之和，并引入应力函数表示非轴对称内力，对平衡方程应用伽辽金方法，将导出的和冲击物体的质量对动屈曲性能的影响很大。     

Boundary-layer hygrothermal stresses in laminated, composite, circular, cylindrical shell panels

Free-edge effects in laminated, circular, cylindrical shell panels subjected to hygrothermal loading are studied by utilizing displacement-based technical theories. Starting from the most general displacement field of elasticity for long, circular, cylindrical shells, appropriate reduced displacement fields are determined for laminated composite shell panels with cross-ply and antisymmetric angle-ply layups. An equivalent single-layer shell theory is used to analytically determine the constant parameters appearing in the reduced displacement fields. A layerwise shell theory is then employed to analytically determine the local displacement functions and the boundary-layer interlaminar stresses in cross-ply and antisymmetric angle-ply shell panels under hygroscopic and/or thermal changes. Several numerical examples for the distributions of transverse shear and normal stresses in various shell panels under a uniform temperature change are presented and discussed.     

On the application of boundary layer method in the large deflection plastic buckling of a cylindrical shell

Using a cylindrical shell under axial loading as an example, we discuss the possibility of applying the membrane theory together with the boundary layer correction to analyze the large deflection plastic buckling problem. In the cases of fixed ends and simply-supported ends, the conditions to be satisfied for using the boundary layer method (also called the composite-expansion method) are given and discussed.     

Viscoelastoplastic Deformation of Reinforced Shells of Revolution Under Nonstationary Loading

The elastoviscoplastic behavior of a discretely reinforced shell under axisymmetric nonstationary loading is considered within the framework of the geometrically and physically nonlinear Timoshenko-type theory of shells. The stress–strain state of the structure is studied in terms of the incremental plasticity with kinematic hardening and dynamic yielding condition, which allows for the dynamic viscosity of the structure. The nonstationary behavior of a rigidly fastened reinforced shell under axisymmetric pulse loading normal to the shell surface is considered as an example. The deflection–time and deflection–space relationships are found     

Refined Stress Analysis of Flexible Multilayered Shells of Revolution with Orthotropic Layers of Variable Thickness

A refined theory of flexible layered shells with orthotropic layers of variable thickness is considered. The theory assumes that each layer has a local rotation angle due to lateral shear. This makes it possible to derive equations whose order does not depend on the number of layers. The basic equations and calculation results are presented for a three-layer orthotropic toroidal shell under axisymmetric loading     

Flow-induced deformation of an elastic membrane adhering to a wall

The flow-induced deformation of a two-dimensional membrane with a circular unstressed shape clamped at the two ends on a plane wall at an arbitrary contact angle is considered. Working under the auspices of generalized shell theory, the membrane is allowed to develop in-plane tensions, transverse tensions, and bending moments determined by the curvature of the resting and deformed shapes. A system of ordinary differential equations governing the membrane shape is formulated, and the associated boundary-value problem is solved by numerical methods. Numerical results are presented to illustrate the deformation of a clamped membrane due to gravity or a negative transmural pressure. The shell formulation is coupled with a boundary-integral formulation for Stokes flow, and an efficient iterative scheme is developed to describe deformed equilibrium shapes of a membrane attached to a plane wall in the presence of an overpassing shear flow. Computations for different contact angles and shear rates reveal a wide variety of profiles and illustrate the distribution of the membrane tension developing due to the flow-induced deformation.     

板壳有限变形精确理论及有限元列式

以位移型退化壳理论为基础,提出了板壳模型的有限变形精确理论,该理论引入转动伪矢量概念,充分发挥刚性线段的运动学模型和有限转动矩和作用,精确表达非线性位移－应变关系,抛弃以往的小位移、小应变、小转动增量乃至小加载小长等各种简化假设,并严格遵循能量共轭关系建立有限元平衡方程,能够可靠和有效地用于板壳结构的大位移、大转动分析。算例表明,该文列式在弹性范围内具明显的平方收敛效率,并且计算结果与加载步长无关。由于不受小加载步长、小转动增量等的限制,实现了板壳几何非线性问题的大步长加载。     

Buckling of unstiffened conical shells under combined loading

An experimental program was conducted in order to determine the family of interaction curves for the buckling of unstiffened conical shells under combined axial compression, torsion, and external or internal pressure. Careful experimental technique permitted many repeated buckling tests on the same aluminumalloy shell without noticeable damage and yielded reliable interaction curves. Results of combined-loading tests are presented and compared with linear theory. Test results show that the interaction curve for compression-torsion-pressure loading is defined by superposition of compression-pressure, torsion-pressure and compression-torsion behavior.     

Dynamic non-linear behavior and stability of a ventricular assist device

This paper investigates the non-linear dynamic behavior and stability of the internal membrane of a ventricular assist device (VAD). This membrane separates the blood chamber from the pneumatic chamber, transmitting the driving cyclic pneumatic loading to blood flowing from the left ventricle into the aorta. The membrane is a thin, nearly spherical axi-symmetric shallow cap made of polyurethane and reinforced with a cotton mesh. Experimental evidence shows that the reinforced membrane behaves as an isotropic elastic material and exhibits both membrane and flexural stiffness. So, the membrane is modeled as an isotropic pressure loaded shallow spherical shell and its dynamic behavior and snap-through buckling considering different types of dynamic excitation relevant to the understanding of the VAD behavior is investigated. Based on Marguerre kinematical assumptions, the governing partial differential equations of motion are presented in the form of a compatibility equation and a transverse motion equation. The results show that the shell, when subjected to compressive pressure loading, may loose its stability at a limit point, jumping to an inverted position. If the compressive load is removed, the shell jumps back to its original configuration. This non-linear behavior is the key feature in the VAD behavior.     

Axisymmetric deformation of poroelastic shells of revolution

A linear theory is developed for axisymmetric deformation of thin poroelastic shells of revolution. With fluid solid coupling included through Biot's consolidation theory, results are presented for cylindrical shells with an oscillating internal pressure and various surface boundary conditions on the fluid. First, the effects of fluid flow and shell inertia on the stretching behavior are studied through a separation of variables solution. Then, the bending behavior near a clamped edge is examined through an asymptotic solution of a matrix form of the governing equations. The results show that the asymptotic solution is accurate in the low frequency range, when the loading time is large compared to the consolidation time. In addition, for the examples studied, the fluid flow influences the membrane more than the bending behavior, but damping due to flow resistance is limited near resonance.     

张拉膜结构的有限元分析

应用有限元程序ANSYS进行了薄膜结构的找形分析和荷载分析．张拉结构受力后将产生较大的位移,因此需要采用非线性理论．通过一系列计算,可以发现影响找形结果的因素有：单元的划分,初始弹性模量的选取,膜的预张力,边索和脊索的预张拉力值及其比值．在实际工程中,由于膜结构建筑要求和边界条件的限制,找到具有极小曲面性质的初始平衡形状较难,因此,一般把应力的差值控制在一定的范围内．工程实例计算结果表明：在风荷载作用下膜结构的竖向位移反应比较大,风吸力通常是索膜结构设计的控制因素．