一种考虑横向剪切变形的三角形板弯曲单元

本文从部分协调的三角形薄板弯曲单元出发,并假设横向剪切应变在单元内线性变化,提出了一种考虑横向剪切变形的具有15个自由度的三角平板弯曲单元。该单元应用于薄板和中等厚度板分析均有较高的精度,计算效率高,可用于工程中具有复杂形状的薄板和中等厚度板结构的分析。     

一个厚薄板通用的三角形板弯元

本文提出了一个新的厚薄板通用的三角形板弯元,根据Hellinger-Reissner变分原理推导出来的新单元具有独立的转角、位移、剪应变和弯曲应变的插入函数,它没有其它混合元所存在的一些缺点。一些典型例子表明这个新单元具有很好的特性,刚度矩阵简单,计算精度高,收敛速度快以及厚薄板通用性强。     

厚薄板通用三角形位移元

本文构造出了一种具有九个自由度的厚薄板通用三角形位移单元，并给出了单元刚度矩阵显式。这种单元以其简洁的常规位移元列式可在相当宽的板厚变化范围内（包括板厚为零）获得很高的计算精度，其结果可与相应的矩形单元相比。而且不会出现剪切自锁。     

采用SemiLoof型约束条件的薄板三角形广义协调元

本文综合广义协调元和SemiLoof元的优点,消除其缺点,建立一个九自由度三角形薄板单元。单元自由度只含常规的角点自由度,不采用SemiLoof元还包含边点自由度的复杂作法。着眼于广义协调,克服了某些非协调元不能通过分片检验的致命弱点。采用SemiLoof型约束条件,即全部采用离散型(点型)协调条件,不采用广义协调元通常采用的积分型协调条件的复杂作法。从简便实用、高精度和收敛可靠进行全面衡量,本单元是同类低阶薄板单元中的最优单元。     

广义协调扇形板弯曲单元

本文基于修正的势能泛函,引入适当的广义协调条件,导出了一种具有12个自由度的广义协调板弯曲扇形位移单元GC—S12,这种单元自由度少,列式简单,精度高。     

离散Kirchhoff三角形薄板单元的改进

本文构造了一类改进的离散Ｋｉｒｃｈｈｏｆｆ三角形薄板单元。通过对离散Ｋｉｒｃｈｈｏｆｆ单元能量表达式的分解，发现存在一项不影响单元的收敛，但能控制单元精度的积分－－有关绕Ｚ轴的转动偶的积分。该项在经典薄板理论下是不存在的，但在粗网络下它会对单元的精度产生重要影响。通过合理调整该项在能量泛函中的比例，会使单元的精度得到明显改善。     

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。     

Bending and Shear Mode Decomposition in C° Structural Elements

ABSTRACT Various formulations for ° structural finite elements are discussed. By means of two examples, a linear beam and a triangular plate element, it is shown that the proper decomposition of the deformed configuration into its bending and shear modes is essential for the effective performance of C° elements. It is also shown that reduced integration can only be successful if it is equivalent to this decomposition.     

新型整体-局部高阶剪切变形理论及层合板精化三角形单元

基于整体-局部位移方法,建立了一种高阶剪切变形理论。整体位移部分采用的是Reddy理论的位移模式（1984）,局部位移为LIXY等（1997）建立的1,2-3理论的局部函数。这一理论使满足自由表面条件的Red@理论进一步满足层间位移、应力连续,同时有效减少了1,2—3理论的未知数个数。基于此理论深入开展了有限元法研究,建立了满足C^1连续条件的精化三节点三角形单元（每个节点参数为9个）。计算结果表明：建立的精化单元能准确计算整体位移和层间应力。     

薄板弯曲分析的高阶高效无网格法

与传统有限元法相比,无网格法具有节点形函数高度光滑、易于形成高阶近似等优势,更适合于以薄板弯曲问题为代表的高阶偏微分方程的数值求解。然而,高阶无网格法的形函数是非多项式的有理函数,导致弱形式的区域积分难以得到精确计算,通常采用的高阶高斯积分方法需使用大量积分点,计算效率低且精度不高。本文针对薄板弯曲问题的高阶（三阶）无网格法分析,首次发展了与该高阶近似相一致的曲率光顺方案,并基于背景三角形积分单元建立了相应的数值积分格式,大幅度减少了所需的积分点数目。所发展方法的关键在于计算刚度阵所需的形函数的二阶导数由形函数及其一阶导数通过散度定理确定,而非对形函数直接求导获得。数值结果表明,基于标准的高斯积分方案的高阶无网格法精度不高,不能精确再现纯弯曲和线性弯曲模式,且得到的弯矩场分布存在严重的虚假数值振荡。而本文所建议的基于曲率光顺方案的高阶无网格法能够方便高效地求解薄板弯曲问题,尤其是它能精确反映纯弯曲和线性弯曲模式。与标准的高斯积分方法和目前主流的常曲率光顺方法相比,本文方法在计算效率、精度、弯矩分布等方面均展现出显著优势,因而具有较好的应用价值。     

A NEW QUADRILATERAL THIN PLATE ELEMENT BASED ON THE MEMBRANE-PLATE SIMILARITY THEORY

ＩｎｔｒｏｄｕｃｔｉｏｎＢｅｃａｕｓｅｏｆｔｈｅｒｅｑｕｉｒｅｍｅｎｔｏｆｃ1ｃｏｎｔｉｎｕｉｔｙ ,ｉｔｉｓｖｅｒｙｄｉｆｆｉｃｕｌｔｔｏｃｏｎｓｔｒｕｃｔｃｏｎｆｏｒｍｉｎｇＫｉｒｃｈｈｏｆｆｐｌａｔｅｂｅｎｄｉｎｇｅｌｅｍｅｎｔｓ.Ｉｎｏｒｄｅｒｔｏｏｖｅｒｃｏｍｅｔｈｅｄｉｆｆｉｃｕｌｔｙ ,ｍａｎｙａｐｐｒｏａｃｈｅｓｈａｖｅｂｅｅｎｐｒｅｓｅｎｔｅｄ .Ｉｎｔｈｅｓｅａｐｐｒｏａｃｈｅｓ,ｔｈｅｒｅｑｕｉｒｅｍｅｎｔｏｆｃ1ｉｓｒｅｌｅａｓｅｄｏｎｃｏｎｄｉｔｉｏｎｏｆｔｈｅｃｏｎｖｅｒｇｅｎ…     

AN EXACT ELEMENT METHOD FOR THE BENDING OF NONHOMOGENEOUS REISSNER’S PLATE

In this paper,based on the step reduction method and exact analytic method,a new method,the exact element method for constructing finite element,is presented.Since the new method doesn’t need variational principle,it can be applied to solve non-positive and positive definite partial differential equations with arbitrary variable coefficients.By this method,a triangle noncompatible element with15 degrees of freedom is derived to solve the bending of nonhomogenous Reissner’s plate.Because the displacement parameters at the nodal point only contain deflection and rotation angle.it is convenient to deal with arbitrary boundary conditions.In this paper,the convergence of displacement and stress resultants is proved.The element obtained by the present method can be used for thin and thick plates as well,Four numerical examples are given at the end of this paper,which indicates that we can obtain satisfactory results and have higher numerical precision.     

Bending and vibration of composite laminated plates

Hybrid-stress finite element method is applied for analysis of bending and vibration of composite laminated plates in this paper. Firstly, based on the modified complementary principle, a rectangular hybrid-stress plate bending element is presented which applies to analysis of laminates. Inside the element, different stress parameters are assumed according to different layers. The boundary displacements are determined by means of the assumption of YNS theory on the boundary of elements. The element formed in this way not only can take effects of transverse shear deformation and local warping into account, but also has less degrees of freedom. Then, problems of bending and vibration of laminates are solved by using this element, and the numerical results are compared with the exact solutions. This shows that the results obtained in the paper are very close to the exact results.     

带旋转自由度C^0类任意四边形板（壳）单元

基于Ｒｅｉｓｓｎｅｒ－Ｍｉｎｄｉｌｉｎ板弯曲理论和Ｖｏｎ－Ｋａｒｍａｎ大挠度理论,采用单元域内和边界位移插值一致性的概念,将四节点等参弯曲单元与Ａｌｌｍａｎ膜变形二次插值模式相结合,对层合板壳的大挠度分析提供了一种实用的带旋转自由度的四节点Ｃ＾０类板单元。大量算例表明：该单元对板壳结构的线性强度、稳定性和后屈曲分析都表现出良好的收敛性和足够的工程精度。     

基于平面弹性—板弯曲模拟关系的薄板有限元列式——从膜单元到薄板单元

本文全面讨论了基于平面弹性－－板弯曲模拟关系的薄板有限单元的理论和方法,由于直接对弯矩函数进行插值,c1连续性的要求得以自然避免,薄板单元可以直接在c0连续的层面上加以构造,无需借用Reissner-Mindlin的中厚板理论,由之引发的闭锁问题也得以避免,本文系统地阐明了平面弹性膜单元与薄板弯曲单元的对应关系,及由平面弹性膜单元的向薄板弯曲单元转换的一整套方法。为薄板单元的构造提供了一条新的有余的途径,文中给出了对应于平面弹性膜单元CST,LST,Q4,Q8的薄板单元,我们称之为MPS板单元,MPS板元以挠度和转角为自由度,便于实际应用,和其它板单元相比具有非常高的精度。     

An eight noded composite plate element for the dynamic analysis of spatial mechanism systems

The development of a shear-deformable laminated plate element, based on the Mindlin plate theory, for use in large reference displacement analysis is presented. The element is sufficiently general to accept an arbitrary number of layers and an arbitrary number of orthotrophic material property sets. Coordinate mapping is utilized so that non-rectangular elements may be modeled. The Gauss quadrature method of numerical integration is utilized to evaluate volume integrals. A comparative study is done on the use of full Gauss quadrature, reduced Gauss quadrature, mixed Gauss quadrature, and closed form integration techniques for the element. Dynamic analysis is performed on the RSSR (Revolute-Spherical-Spherical-Revolute) mechanism, with the coupler modeled as a flexible plate. The results indicate the differences in the dynamic response of the transverse shear deformable eight-noded element as compared to a four-noded plate element. Dynamically induced stresses are examined, with the results indicating that the primary deformation mode of the eight-noded Mindlin plate model being bending.     

An exact element method for bending of nonhomogeneous thin plates

In this paper, based on the step reduction method, a new method, the exact element method for constructing finite element, is presented. Since the new method doesn't need the variational principle, it can be applied to solve non-positive and positive definite partial differential equations with arbitrary variable coefficient. By this method, a triangle noncompatible element with 6 degrees of freedom is derived to solve the bending of nonhomogeneous plate. The convergence of displacements and stress resultants which have satisfactory numerical precision is proved. Numerical examples are given at the end of this paper, which indicate satisfactory results of stress resultants and displacements can be obtained by the present method.     

Mixed hybrid penalty finite element method and its application

The penalty and hybrid methods are being much used in dealing with the general incompatible element, With the penalty method convergence can always be assured, but comparatively speaking its accuracy is lower, and the condition number and sparsity are not so good. With the hybrid method, convergence can be assured only when the rank condition is satisfied. So the construction of the element is extremely limited. This paper presents the mixed hybrid penalty element method, which combines the two methods together. And it is proved theoretically that this new method is convergent, and it has the same accuracy, condition number and sparsity as the compatible element. That is to say, they are optimal to each other.Finally, a new triangle element for plate bending with nine freedom degrees is constructed with this method (three degreesof freedom are given on each corner——one displacement and tworotations), the calculating formula of the element stiffness matrix is almost the same as that of the old triangle element for plate bending with nine degrees of freedom But it is converged to true solution with arbitrary irregrlar triangle subdivision. If the true solution u∈H³ with this method the linear and quadratic rates of convergence are obtianed for three bending moments and for the displacement and two rotations respectively.     

一种精确积分的四结点板弯曲单元

本文从Ｍｉｎｄｌｉｎ／Ｒｅｉｓｓｎｅｒ理论出发,采用一种新的平行四边形母单元和相应的形函数推导四结点板弯曲单元刚度矩阵的精确积分解。弯曲应变和横向剪切应变分别采用不同的插值公式构成单元刚度矩阵。理论和算例分析表明本文方法克服了“闭锁”现象并能应用于很薄的板,单元刚度矩阵计算速度比采用数值积分计算的同类单元的快四倍。     

数值流形方法在连续体数值分析中的应用

在平面连续作的数值计算中使用数值流形方法的各阶覆盖位移函数和统一的三节点三角形流形单元,能够得到高精度的数值结果,且具有编程和前后处理简单等优点,克服了有限元法复杂理论的不足．文中还引入了三角形单元Ｈａｍｍｅｒ数值积分,使流形方法的程序编制通用化．