任意厚度层合开口柱壳的温度应力

基于层合柱壳混合状态方程和边界条件的弱形式,建立了具有固支边的层合开口柱壳的温度应力混合方程,给出了任意厚度层合开口柱壳在温度荷载和机械荷载共同作用下的解析解。     

层合闭口厚柱壳的温度应力

基于层合柱壳混合状态方程和边界条件的弱形式，建立了两端固支层合闭口柱壳的温度应力混合方程，给出了任意厚度合闭口柱壳在温度荷载和机械荷载共同作用下的解析解。     

任意厚度层合闭口柱壳的轴对称温度应力

基于层合柱壳混合状态方程和边界条件的弱形式，在轴对称情况下，建立了两端固支层合闭口柱壳的温度应力混合方程，给出了任意厚层合柱壳在温度荷载和机械荷载共同作用下的解析解。     

两端固支强厚度叠层闭口柱壳轴对称问题的精确解

抛弃任何有关应力或位移模式的人为假设,在文献【1】、【2】的基础上,引入δ—函数,在轴对称情况下,对两端固支叠层闭口柱壳建立其状态方程。给出薄的、中厚的以及强厚的叠层闭口柱壳的静力和动力问题的统一的精确解。此解满足所有的弹性力学基本方程,并计及了全部弹性常数。任意需要的精确度都能得到。     

一般叠层圆柱厚壳的非线性动力稳定性分析

基于Ｔｉｍｏｓｈｅｎｋｏ－Ｍｉｎｄｌｉｎ假设及Ｈａｍｉｌｔｏｎ原理，建立了一般纤维叠层圆柱厚壳在参数激励下的非线性振动方程；应用多模态近似和增量谐波平衡法求解了叠层圆柱厚壳的非线性动力稳定性问题。横向剪切变形、端部支承条件等因素的影响被讨论。     

一般叠层圆柱厚壳的非线性动力稳定性分析

基于Ｔｉｍｏｓｈｅｎｋｏ－Ｍｉｎｄｌｉｎ假设及Ｈａｍｉｌｔｏｎ原理，建立了一般纤维叠层圆柱厚壳在参数激励下的非线性振动方程；应用多模态近似和增量谐波平衡法求解了叠层圆柱厚壳的非线性动力稳定性问题。横向剪切变形、端部支承条件等因素的影响被讨论。     

考虑横向剪切变形矩形底中厚扁壳的屈曲研究

基于考虑横向剪切变形直角坐标下矩形中厚扁壳的几何方程、本构关系、平衡方程,建立了关于三个中面位移和两个中面转角为独立变量的矩形中厚扁壳小挠度屈曲的基本微分方程。该方程可退化为矩形中厚板屈曲的基本微分方程,从而说明本文推导过程的正确性及一般性。文中矩形中厚扁壳小挠度屈曲的基本微分方程是一组耦合的变系数二阶偏微分方程,对常曲率扁壳使用双重三角级数并将其作为广义坐标对该方程组进行解耦,进一步建立中厚扁壳小挠度屈曲的特征方程,并得到了简支矩形中厚壳屈曲的临界荷载表达式,最后获得了其屈曲的临界荷载曲线及其相应的临界荷载值。该临界荷载曲线及其相应的临界荷载值可以退化为矩形中厚板的临界荷载曲线及临界荷载值。结果表明：本文提出的算法求解过程简便,矩形中厚扁壳临界荷载收敛较快。     

轴对称层合圆柱壳混合状态方程的弱形式及其边值问题

从Ｈｅｌｉｎｇｅｒ－Ｒｅｉｓｓｎｅｒ变分原理出发，在柱坐标系中，导出圆柱壳轴对称问题的弱形式混合状态方程和边界条件，联用状态空间法给出强厚度叠层柱壳的解析解，此法使得求解该类问题的形式得以扩大和统一。     

变截面短柱壳的热应力

在变截面薄柱壳平衡方程的一般推导中,常忽略剪力对挠度的影响。但是对于短柱壳,这种影响就不可忽略。从等截面圆柱壳受静荷载的情况来看,在壳体长度与壁厚比值的一定范围内,与不考虑剪力对挠度影响的结果相比,考虑剪力影响后弯矩的修正值可以达到(20-40)%。本文从考虑剪力对挠度的影响出发,导出了截面厚度随壳体轴向坐标线性变化的变截面短圆柱壳在...     

基于热-磁-弹性耦合的二维导电薄柱壳数值分析

基于几何方程、物理方程、运动方程和电动力学方程，建立了二维导电薄柱壳热磁弹性基本方程．考虑到Joule热效应，引入热平衡方程及广义Ohm定律，得出导电薄柱壳的温度场．利用变量代换方法，整理成具有10个基本未知量的标准型方程组．采用差分法和准线性化方法，给出准线性微分方程组．对于二维导电薄柱壳，导出了Lorentz力表达式、温度场积分特征值．通过实例计算，得到了二维导电薄柱壳应力、位移、温度随外加电磁参量的变化规律．研究结果可为二维导电薄壳热磁弹性问题研究提供理论参考．     

The solution of weak formulation for axisymmetric problem of orthotropic cantilever cylindrical shell

Weak formulation of equilibrium equations including boundary conditions of laminated cylindrical shell is presented, and thermal stresses mixed state equation for axisymmetric problem of closed cantilever cylindrical shell is established. A unified approach and weak solutions are obtained for closed laminated cantilever cylindrical shell of arbitrary thickness under thermal and mechanical loadings. The equation and boundary conditions proposed in this paper are weakened, the method of this paper would be easy to popularize in dynamics analysis of elasticity. Foundation item: the National Natural Science Foundation of China (19392305)     

ACTIVE CONTROL OF THE PIEZOELASTIC LAMINATED CYLINDRICAL SHELL''''S VIBRATION UNDER HYDROSTATIC PRESSURE

IntroductionDuetotheintrinsicdirectandconversepiezoelectriceffects,piezoelectricmaterialscanbeeffectivelyusedtoproducesensorsoractuatorsfortheactiveshapeorvibrationcontrolostructures.Therefore,theuseofpiezoelectricmaterialsinintelligentstructuresattractedmanyattentionsinrecentyears.Thedesignofsuchactivesystemsrequiresgoodunderstandingofthemechanical_electricinteractionbetweenthestructuresandpiezoelectricmaterials.Manyinvestigationshavebeendoneinthisfield[1].However,mostofthesestudiesarebasedo…     

Buckling and post-buckling analyses for an axially compressed laminated cylindrical shell of FGM with PFRC in thermal environments

In this paper, investigation on buckling and post-buckling behaviors of a laminated cylindrical shell of functionally graded material (FGM) with the piezoelectric fiber reinforced composite (PFRC) actuators subjected to thermal and axial compressed loads is presented. Based on the Donnell assumptions, the material properties of the FGM layer vary smoothly through the laminated cylindrical shell thickness according to a power law distribution of the volume fraction of constituent materials. In the present study, a numerical procedure for the laminated cylindrical shell is used based on the Ritz energy method and the nonlinear strain–displacement relations. Some useful discussion and numerical examples are presented to show various effects of temperature field, volume fraction and geometric parameters on the buckling and post-buckling behaviors of the laminated cylindrical shell with PFRC.     

层合圆柱壳体表层局部分层屈曲及其扩展

应用能量法研究了对称铺层的闭合圆柱形层合壳体的表层局部分层屈曲问题；表层分层形式有三角形，椭圆和双纽线；分析了母层壳，子层壳的几何参数，物理参数同分层屈曲临界应变值之间的关系；给出了子层分层为椭圆的分层扩展的可能发生方向。     

Refined Analysis of the Influence of the Inhomogeneous Layers on the Stress State of Circular and Noncircular Cylindrical Shells

We study the stress state of laminated inhomogeneous closed cylindrical shells generally with an arbitrary cross section, taking transverse shear into account on the basis of the straight-line element hypothesis. As an example, results are presented for a two-layer cylindrical shell whose cross section is a combination of an oval and a circle.     

一种求解层合圆柱壳的杂交应力单元

根据修正的余能原理，推导出一种求解复合材料层合圆柱壳的杂交应力单元。取用六面体等参单元，此单元反映了各层材料性质不同及应力分布沿整个厚度不连续现象，同时计入横向剪切变形和法向挤压变形，适用于厚层壳体。文章通过实例说明此单元能准确求出各层内的应力值，实用价值高。     

Postbuckling analysis of axially-loaded laminated cylindrical shells with piezoelectric actuators

A compressive postbuckling analysis is presented for a laminated cylindrical shell with piezoelectric actuators subjected to the combined action of mechanical, electric and thermal loads. The temperature field considered is assumed to be a uniform distribution over the shell surface and through the shell thickness, and the electric field is assumed to be the transverse component E_Z only. The material properties are assumed to be independent of the temperature and the electric field. The governing equations are based on the classical shell theory with von Kármán–Donnell-type kinematic nonlinearity. The nonlinear prebuckling deformations and initial geometric imperfections of the shell are both taken into account. A boundary layer theory of shell buckling, which includes the effects of nonlinear prebuckling deformations, large deflections in the postbuckling range, and initial geometric imperfections of the shell, is extended to the case of hybrid laminated cylindrical shells. A singular perturbation technique is employed to determine the buckling loads and postbuckling equilibrium paths. The numerical illustrations concern the compressive postbuckling behavior of perfect and imperfect, cross-ply laminated cylindrical thin shells with fully covered or embedded piezoelectric actuators under different sets of thermal and electric loading conditions. The effects played by temperature rise, applied voltage, shell geometric parameter, stacking sequence, as well as initial geometric imperfections are studied.