加肋圆柱壳在轴压作用下的屈曲和后屈曲

本文讨论完善和非完善的,纵向加肋和正交加肋圆柱壳在轴压作用下的屈曲和后屈曲性态.依据文[1]提供的圆柱薄壳屈曲的边界层理论及其分析方法,给出了加肋圆柱壳在轴压作用下的屈曲和后屈曲理论分析.本文同时讨论肋骨与壳板材料不同时对加肋圆柱壳屈曲和后屈曲性态的影响.     

任意边界条件下圆柱厚壳自由振动分析的空间变量变换法

本文提出一种一般解析方法——空间变量变换法,用以求解任意边界条件下圆柱厚壳自由振动问题.运用本文方法对悬臂圆柱厚壳的自振特性作了计算,计算结果与薄壳理论相应结果及试验值作了比较.理论分析和计算结果表明,本文方法具有很好的收敛性和精确性,可以推广用于分析梁、板、壳的自由振动.     

严格求解夹层圆柱壳在轴压下的轴对称失稳问题

本文在文献[1]的基础上,用严格的方法求解两端简支的夹层圆柱壳在均匀轴压下的轴对称失稳问题.内、外表层很薄弹性模量又大,按薄壳理论处理;夹心较厚弹性模量又相当小,横向剪切变形的影响必须考虑,在研究夹层壳的整体失稳尤其是局部失稳时,横向的拉伸和压缩变形也不可忽略,用数学弹性力学的方法处理.本文导得了可求解轴对称整体失稳和局部失稳临界载荷的超越方程,用数值计算的方法可算得临界载荷的最小值.对于整体失稳的情况,给出算例,与夹层壳理论的解作了比较.     

正交各向异性圆柱体在轴压作用下的应力场

基于材料体积不可压假设,对轴向压缩作用下圆柱试件在加载面内的环向和径向应力分布进行理论分析,计算结果表明:当试件材料本构为正交各向异性时,环向和径向应力分布为半径的幂函数形式;试件材料为横观各向同性时,环向和径向应力为半径的二次函数.在圆柱试件轴线上环向和径向应力相等,且均具有最大值;试件圆周边界上径向应力为0,环向应力具有极小值.通过最大拉伸应变破坏理论对试件环向应变进行分析,获得了产生环向拉伸破坏时的临界轴向载荷;并采用Hill-蔡强度理论对试件圆周边界上计算得到的应力参量进行描述,得到了轴压作用下圆柱试件的Hill-蔡强度理论表达式,其不仅取决于轴向应力和试件材料的基本力学性能,还与试件轴向变形的应变率及应变率随时间的变化率相关.     

一种新的叠层板壳高阶理论

本文提出了一种新的叠层板壳高阶理论,然后又研究了正交对称叠层板,反对称叠层板,圆柱弯曲和球壳弯曲问题.为了检验理论的准确性,文中计算了几个特殊例子,数值结果和精确解吻合得相当好,说明本理论具有较高的准确度,且表现出未知数较少,解题方便的优点.     

加载和卸载过程中复合材料叠层圆柱曲板后屈曲路径的研究

本文用动态松弛法研究了在加载和卸载过程中复合材料叠层圆柱曲板的后屈曲路径,发现了加载路径与卸载路径不重合的现象,给出了在均匀单轴压力作用下的十字叠层圆柱曲板在两种边界条件下的数值结果,并讨论了层数、曲率半径、初始几何缺陷等因素对后屈曲路径的影响.     

复合材料叠层圆柱壳的非线性动力稳定性理论

用Hamilton原理建立了复合材料叠层圆柱壳非线性动力稳定性理论的一般性基本方程,其中包含了非线性大挠度,横向剪切,纵向惯性力等因素。用变分法获得基本方程的解。分析表明:叠层圆柱壳在动载荷下会发生参数共振而进入动力不稳定区域而导致动力失稳。计算了几种典型复合材料圆柱壳:即T300/5208石墨环氧,E-玻璃环氧和ARALL圆柱壳。结果表明:这些因素对于各种复合材料圆柱壳的动力稳定性具有程度不同的重要影响,所以研究叠层圆柱壳动力稳定性时,考虑这些因素是重要的。     

弹性圆柱壳扭转屈曲研究

本文给出两端固支的弹性圆柱壳扭转屈曲实验与理论计算结果.实验发现,对于较长的壳,其屈曲后的变形并不占据整个壳体的长度.另外在计算中仅考虑壳体的法向边界条件,而不考虑其周向和轴向边界条件,结果和Yamaki精确解以及本文实验结果相符较好,说明周向和轴向边界条件对圆柱壳的扭转屈曲影响较小.     

多层复合材料圆柱壳的非线性失稳计算

本文用能量法和有限差分法分析了多层复合材料圆柱壳在轴压、静水压力及扭转等载荷作用下的非线性屈曲和后屈曲性能。本文考虑了柱壳的初始缺陷、几何非线性、材料的物理非线性(剪切模量非线性)等因素对于临界载荷的影响。同时还讨论了横向剪切效应。计算分析结果与一些实验结果比较一致。     

轴压加筋圆柱壳Koiter-边界层奇异摄动法

将Koiter理论和奇异摄动理论中的边界层法相结合,处理加筋圆柱壳无因次化非线性边界层型Karman－Donnell方程由分支点和边界层导致的双重奇异性,提出轴压加筋圆柱壳Koiter-边界层奇异摄动法.对AS－2壳分析表明,本方法具有很好的计算效率和计算精度,与数值解相比更能揭示其内在的影响规律.     

非完善加筋圆柱壳在外压和热荷载共同作用下的后屈曲

基于壳体屈曲的边界层理论,本文给出有限长加筋圆柱壳在侧向外压和均布热荷载共同作用下的后屈曲分析。分析中同时考虑壳体非线性前屈曲变形,大挠度和初始几何缺陷的影响。肋条的处理采用“平均刚度”法。采用奇异摄动方法导得壳体屈曲载荷关系曲线和后屈曲平衡路径,并给出完善和非完善,纵向加筋或环向加筋圆柱壳数值算例。     

环肋加劲圆柱壳在静水压力作用下的初始后屈曲分析

本文用Koiter理论分析环肋加劲圆柱壳在静水压力作用下的后屈曲性能.前屈曲状态采用与边界条件一致的非线性有矩方程,本征值问题的解用伽辽金方法求出,得到的临界载荷与经典线性解作了比较.具体计算了三种不同环肋参数的外肋加劲圆柱壳.结果表明,肋的强弱不仅显著影响临界载荷值,同时也改变了柱壳的缺陷敏感度.     

The dynamic stability and nonlinear vibration analysis of stiffened functionally graded cylindrical shells

A theoretical model is developed to study the dynamic stability and nonlinear vibrations of the stiffened functionally graded (FG) cylindrical shell in thermal environment. Von Kármán nonlinear theory, first-order shear deformation theory, smearing stiffener approach and Bolotin method are used to model stiffened FG cylindrical shells. Galerkin method and modal analysis technique is utilized to obtain the discrete nonlinear ordinary differential equations. Based on the static condensation method, a reduction model is presented. The effects of thermal environment, stiffeners number, material characteristics on the dynamic stability, transient responses and primary resonance responses are examined.     

Formulation and evaluation of a finite element model for the linear analysis of stiffened composite cylindrical panels

A finite element model for linear static and free vibration analysis of composite cylindrical panels with composite stiffeners is presented. The proposed model is based on a cylindrical shell finite element, which uses a first-roder shear deformation theory. The stiffeners are curved beam elements based on Timoshenko and Saint-Venant assumptions for bending and torsion respectively. The two elements are developed in a cylindrical coordinate system and their stiffness matrices result from a hybrid-mixed formulation where the element assumed stress field is such that exact equilibrium equations are satisfied. The elements are free of membrane and shear locking with correct satisfaction of rigid body motions. Several examples dealing with stiffened isotropic and laminated plates and shells with eccentric as well as concentric stiffeners are analyzed showing the validity of the models.     

Numerical analysis of free vibrations of laminated composite conical and cylindrical shells: Discrete singular convolution (DSC) approach

A numerical study on the free vibration analysis for laminated conical and cylindrical shell is presented. The analysis is carried out using Love's first approximation thin shell theory and solved using discrete singular convolution (DSC) method. Numerical results in free vibrations of laminated conical and cylindrical shells are presented graphically for different geometric and material parameters. Free vibrations of isotropic cylindrical shells and annular plates are treated as special cases. The effects of circumferential wave number, number of layers on frequencies characteristics are also discussed. The numerical results show that the present method is quite easy to implement, accurate and efficient for the problems considered.     

A new finite element model for the analysis of arbitrary stiffened shells

A new stiffened shallow shell finite element has been introduced for the static analysis of stiffened plates and shells. This approach has been presented to cater for stiffeners in which the positions and properties remain undisturbed in the formulation and the element can accomodate the stiffener anywhere within the shell element and in any direction, which introduces a considerable flexibility in the analysis. This is a distinct improvement over the existing models. Stiffened shells having various disposition of stiffeners as available in the literature, have been analysed by the proposed approach. Comparison obtained with the existing theoretical and/or experimental values have indicated good accuracy with relatively coarser mesh sizes and less CPU time.     

Numerical computation of weak solutions of nonlinear motion equations of stiffened cylindrical shells

An algorithm is presented for the numerical solution of nonlinear equations of motion of stiffened cylindrical shells described by a Timoshenko-type theory. This algorithm is constructed using a weak solution of nonlinear motion equations of stiffened cylindrical shells. A difference scheme is constructed using the approximation of integral identities. A dependence was found between the steps of the time and space variables for the linearized difference scheme.Presented at the Ninth International Conference on the Mechanics of Composite Materials, Riga, Latvia, October, 1995.Translated from Mekhanika Kompozitnykh Materialov, Vol. 31, No. 6. pp. 808–815, November–December, 1995.     

Static and dynamic analyses of isogeometric curvilinearly stiffened plates

The isogeometric analysis (IGA) is a new approach which builds a seamless connection between Computer Aided Design (CAD) and Computer Aided Engineering (CAE). This approach which uses the B-Splines or the Non-Uniform Rational B-Splines (NURBS) as a geometric representation of the object is a discretization technology for numerical analysis. The IGA has advantages of capturing exact geometry and making the flexibility of refinement, which results in higher calculation accuracy. To study the static and dynamic characteristics of curvilinearly stiffened plates, the NURBS based isogeometric analysis approach is developed in this paper. We use this approach to analyze the static deformation, the free vibration and the vibration behavior in the presence of in-plane loads of curvilinearly stiffened plates. Furthermore, the large deformation and the large amplitude vibration of the curvilinearly stiffened plates are also studied based on the von Karman's large deformation theory. One of the superiorities of the present method in the analysis of the stiffened plates is that the element number is much less than commercial finite element software, whereas another advantage is that the mesh refinement process is much more convenient compared with traditional finite element method (FEM). Some numerical examples are shown to validate the correctness and superiority of the present method by comparing with the results from commercial software and finite element analysis.     

环向和纵向加肋非均匀大变形圆柱壳的自由振动*

环向和纵向加肋非均匀圆柱壳在航空,宇航等工业广泛运用,本文使用阶梯折算法得到了环向和纵向加肋非均匀大变形圆柱壳在任意边界条件下自由振动的一般解.问题最后归结为求解一个超越代数方程,这个方程可以用一个具体的解析表达式表示出来.文中还给出了收敛性证明和算例.算例表明,利用本文的方法,可得到满意的结果.