有限圆柱厚壳的一个分析

本文研究了一个弹性有限圆柱厚壳的轴对称弯曲问题.文中对这类壳体给出了一个表达成两个无穷级数之和的三维弹性理论解.这些级数的选择使它们能满足所有给定的边界条件.利用级数的正交性质,其中任一级数中的每项系数都可表达为另一级数的各项系数的线性函数.通过在级数中各取有限个项数进行计算,即可求得问题的近似数值解. 文中处理了一个两端刚性固定的有限圆柱壳体承受内、外均布压力作用的问题作为示范.还给出了计算实例,并将计算结果绘成曲线.这些曲线表明在两端刚性固支的情况下,经典板壳理论即使对薄壳的计算也是难以适用的.此外,这些结果还可作为各种厚壳理论进行比较的一个依据.     

复合材料回转壳的有限元级数解

本文用有限元法和Fourier级数展开技术求解复合材料回转壳体在各种荷载作用下的弯曲问题,文中利用回转壳在几何上的轴对称性质,将各物理量在环向展开为Fourei级数,而在母线和壳厚方向分割单元,所采用的单元为6节点18自由度等参元,它考虑了剪切变形和挤压变形的影响,能计算厚度方向的挤压应力,数值算例表明,本文提出的单元性能优良,算法稳定收敛。     

组合加肋旋转壳的强度和稳定性有限元分析

本文对轴对称加肋旋转壳及其组合壳体(锥-锥,锥-柱,球-柱壳等)在轴对称静载荷作用下的线弹性强度和稳定性计算,采用性能良好的轴对称拟协调单元推导了有限元的计算列式,并将计算结果与静水压力下的锥-柱-锥结合壳,加肋锥-柱结合壳的其它计算结果和实验结果进行比较。     

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。     

关于40个自由度八结点壳体单元的一些计算试验

1.引言由等参数单元发展而来的40个自由度八结点的壳体单元不仅可应用来计算厚壳,而且可用来计算薄壳.文[6]对单元通过任一点的中面法线的计算,给出一个与文[1—4]所采用的不同的合理的方案,文[6,7]进行过实例计算.我们对国内及国外这两种方案,都编制了程序,进行比较性计算.应力计算使用了一个线性外推公式,可     

集中载荷作用下弹性球壳大范围非线性问题

采用有限元法中的伪弧长法研究了集中载荷作用下弹性球壳轴对称大范围非线性问题，变形的范围从初始状态到壳体完全翻转．文中作了计算结果与实验结果的比较     

含轴对称初始缺陷的具有正交各向异性表层的夹层圆柱壳的非线性屈曲

夹层圆柱壳具有很高的结构效能。在许多工程结构中被广泛采用。本文研究分析了含有轴对称初始缺陷的夹层圆柱壳在轴压下的非线性屈曲问题。该夹层壳具有正交各向异性表层和各向同性可承剪的夹心．利用Stein的前屈曲一致理论得出了前屈曲挠度随轴向载荷及缺陷参数的变化情况，运用Galerkin法导出了屈曲控制方程，并进行了数值计算，得到了屈曲载荷、缺陷幅值、缺陷波数、夹心模量等参量之间的关系．结果表明与壳体实际屈曲模态相同的初始缺陷具有很大的危害性，可以通过增加壳体表层的轴向弹性模量或优化夹心的有关参数等途径来提高屈曲载荷，改善壳体屈曲性能。     

旋转壳对称载荷有限元应力分析的系数配置法

本文用有限元系数配置法分析轴对称旋转壳,计算时不需坐标转换,对各种类型的壳体元素统一采用同一组基本公式协调求解。算法简单,精度高,可用于圆柱壳,圆锥壳,平法兰等工程上常用的旋转壳结构。由于在协调求解中可插入解析公式,便于处理螺栓连接,结合裙等不连续结构。本法是在文献[1]基础上改进而成。     

弹性中厚扁球壳的边界积分方程解法

1.前言近年来,边界元法已成功地求解了薄壳弯曲等问题。经典薄壳理论采用Kirchhoff假设,忽略了剪切变形,转动惯性效应.此理论计算厚壳,带有小孔洞的壳体会带来较大的误差。本文所讨论的球壳平衡方程中,不仅包含薄膜内力项和弯矩项,而且还反映了横向剪切变形。利用假设位移函数法,推导出其基本解。然后由虚功原理导出一组五个边界积分方程。其中含有五个广义位移(两个转角分量和三个位     

板锥网壳结构的连续化分析

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。本文将板锥网壳结构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。     

Corotational nonlinear analyses of laminated shell structures using a 4-node quadrilateral flat shell element with drilling stiffness

A new 4-node quadrilateral flat shell element is developed for geometrically nonlinear analyses of thin and moderately thick laminated shell structures. The fiat shell element is constructed by combining a quadrilateral area co- ordinate method （QAC） based membrane element AGQ6- II, and a Timoshenko beam function （TBF） method based shear deformable plate bending element ARS-Q12. In order to model folded plates and connect with beam elements, the drilling stiffness is added to the element stiffness matrix based on the mixed variational principle. The transverse shear rigidity matrix, based on the first-order shear deformation theory （FSDT）, for the laminated composite plate is evaluated using the transverse equilibrium conditions, while the shear correction factors are not needed. The conventional TBF methods are also modified to efficiently calculate the element stiffness for laminate. The new shell element is extended to large deflection and post-buckling analyses of isotropic and laminated composite shells based on the element independent corotational formulation. Numerical re- sults show that the present shell element has an excellent numerical performance for the test examples, and is applicable to stiffened plates.     

一种厚板薄板通用的新型广义协调元

在适用于中厚板的八结点平板弯曲单元基础上，通过引入剪应变与位移的广义协调条件，建立起一种新型广义协调元，不仅保留了原单元适用于中厚板的特点，同时对薄板也给出了较精确的解，是一种厚板和薄板通用的新型广义协调元。     

THE CONSTRUCTION OF WAVELET-BASED TRUNCATED CONICAL SHELL ELEMENT USING B-SPLINE WAVELET ON THE INTERVAL

Based on B-spline wavelet on the interval (BSWI), two classes of truncated conicalshell elements were constructed to solve axisymmetric problems, i.e. BSWI thin truncated conicalshell element and BSWI moderately thick truncated conical shell element with independent slope-deformation interpolation. In the construction of wavelet-based element, instead of traditionalpolynomial interpolation, the scaling functions of BSWI were employed to form the shape functionsthrough the constructed elemental transformation matrix,and then construct BSWI element viathe variational principle. Unlike the process of direct wavelets adding in the wavelet Galerkinmethod, the elemental displacement field represented by the coefficients of wavelets expansionwas transformed into edges and internal modes via the constructed transformation matrix. BSWIelement combines the accuracy of B-spline function approximation and various wavelet-basedelements for structural analysis. Some static and dynamic numerical examples of conical shellswere studied to demonstrate the present element with higher efficiency and precision than thetraditional element.     

A new high-precision stress finite element for analysis of shell structures

A new high-precision finite element for analysis of shell structures is presented. It is derived from a slightly generalized equilibrium principle. Accordingly both stresses and displacements are obtained as primary result of analysis. At the assembly level the element has 45 degrees of freedom, all of them generalized displacements. For the price of some additional computational effort on the elemental level of analysis the proposed element is believed to gain certain advantages over the recently developed high-precision displacement elements. Thin as well as thick shell structures of arbitrary shape and loading can be equally analyzed. Engineering accuracy is attained with only very few elements. A variety of numerical examples demonstrates the applicability of the new element to all kinds of situations occuring in practice. A review of the existing high-precision shell elements is also included.     

一个基于膜板比拟理论的四节点二十四自由度的平板壳单元

应用膜板比拟关系 ,可以避开 c1 连续性的困难 ,为板单元的构造提供了一种新的途径 ,并已成功地构造出一系列相应的板单元。本文构造了一个四节点二十四自由度的平板壳单元 ,该单元由平面四节点理性元 RQ4(膜部分 )和由膜板比拟理论构造的一个四节点十二自由度的板单元 (弯曲部分 )构成。该单元构造简单 ,数值结果表明具有很好的收敛性和精度。     

A general solution of axisymmetric problem of arbitrary thick spherical shell and solid sphere

In this paper, the axisymmetric problems of arbitrary thick spherical shell and solid sphere are studied directly from equilibrium equations of three-dimensional problem, and the general solutions in forms of Legendre series for thick spherical shell and solid sphere are given by using the method of weighted residuals.     

一种提高四边形四节点平面壳单元计算精度的新方法

平面壳单元是由平面应力单元和平板弯曲单元叠加组合而成,具有简单的理论表达,但是它在计算曲面壳体结构时误差较大。为了进一步提高平面壳单元的计算精度,本文提出了一种计算平面壳单元刚度矩阵的新方法。通过该方法在高斯积分点建立多个单元局部坐标系,并保证每个局部坐标系都位于单元在高斯点处的切平面上,从而可以有效适应曲面壳体形状,达到进一步提高平面壳单元计算精度的目的。为了在这种新坐标系下计算单元刚度矩阵,给出了求解形函数对局部坐标的导数、局部到自然坐标系积分转换的雅可比、以及局部到整体坐标系的转换矩阵的新型计算方法。通过将这些新坐标系以及新计算方法运用到平面壳单元DKQ24中,可以有效提高平面壳单元尤其是在计算曲面壳体时的精度。计算结果表明,本文方法和平面壳单元相结合,不仅具有平面壳单元简单的理论表达式,还能得到满意的精度。另外,本文方法还可以应用到其他类型的平面壳单元,为提高其他类型平面壳单元的计算精度提供了一种新的途径和思路,具有广阔的应用前景。     

A new curved gradient deficient shell element of absolute nodal coordinate formulation for modeling thin shell structures

A curved gradient deficient shell element for the Absolute Nodal Coordinate Formulation (ANCF) is proposed for modeling initially thin curved structures. Unlike the fully parameterized elements of ANCF, a full mapping of the gradient vectors between different configurations is not available for gradient deficient elements, therefore it is cumbersome to work in a rectangular coordinate system for an initially curved element. In this study, a curvilinear coordinate system is adopted as the undeformed Lagrangian coordinates, and the Green–Lagrange strain tensor with respect to the curvilinear frame is utilized to characterize the deformation energy of the shell element. As a result, the strain due to the initially curved element shape is eliminated naturally, and the element formulation is obtained in a concise mathematical form with a clear physical interpretation. For thin structures, the simplified formulations for the evaluation of elastic forces are also given. Moreover, an approach to deal with the on-surface slope discontinuity is also proposed for modeling general curved shell structures. Finally, the developed element of ANCF is validated by several numerical examples.     

Shell-Core Method for the Analysis of a Long Circular Cylindrical Sandwich Shell Subjected to Axisymmetric Loading

The analysis of a sandwich shell having a thick core and thin outer and inner layers (facings) and subjected to axisymmetric loads is considered. The problem is solved by applying the three-dimensional theory of elasticity to the core and the classical thin shell theory for the outer and inner facings. The displacement and stress continuity conditions are satisfied along the junctions of the facings and core. The results obtained from this solution have been compared with the results obtained from the sandwich shell theory of Fulton.     

自由边界条件轴对称薄圆柱壳体的混合有限元数值解

基于文「８」发展的混合结构问题稳定方法的框架,针对自由边界条件轴对称薄圆柱壳体问题,给出了其新型混合有限元计算模型。应用线性元,已证明该模型是强制的,其对称正定代数方程组的条件数Ｏ（ｈ＾－２）。