用改进型广义协调元分析薄板的振动与稳定

本文在文献[1]和[2]的基础上,将改进型三角形广义协调元TGC-9-1应用于薄板振动和稳定分析中。推导出带有一个内部自由度(外部结点有九个自由度)的三角形板单元的协调质量矩阵和几何刚度矩阵。并通过算例表明,改进型广义协调三角形单元(TGC-9-1)具有良好的性态和更好的精度,程序简便。     

基于面积坐标与B网方法的四边形样条单元

传统等参元方法中, S型等参元完备阶较低,对网格畸变敏感, L型等参元具有高阶完备性但需要使用内部节点. 另外,由于引入等参变换, 采用数值积分可能导致总刚度矩阵出现奇异性.利用三角形面积坐标与B网方法建立了一类平面四边形的样条单元函数,它们的特点是满足协调条件, 克服网格畸变敏感性.其中8节点和12节点单元分别为2次和3次样条函数,对直角坐标分别具有二阶和三阶完备性, 高于相同节点的S型等参元.通过算例测试了这些样条单元, 并与等参元和其它四边形单元比较,数值结果显示了它们的高精度和有效性.      

薄板几何非线性中的精化元方法及膜闭锁问题

基于放松单元间协调条件的大变形变分原理和全局拉格朗日方法，推导了几何非线性精化三角形薄板单元。对几何刚度矩阵，通过引入特殊的单元位移函数，有效地消除了薄板弯曲问题中伴生的膜闭锁现象。数值结果表明该单元在几何非线性分析中既能消除膜闭锁又具有较高精度。     

薄板几何非线性中的精化元方法及膜闭锁问题

基于放松单元间协调条件的大变形分原理和全局拉拉格朗日方法，推导出几何非线性精化三角形薄板单元，对几何刚度矩阵，通过引入特殊的单元位移函数，有效地消除了薄板弯曲问题中伴生的膜闭锁现象，数值结果表明该单元在几何非线性分析中既能消除膜闭锁又具有较高精度。     

用通用单元计算板的固有振动和弹性稳定

本文用依据二类变量广义变分原理构造的一种新型的考虑横向剪切影响的任意四边形四节点通用单元[8],研究板的固有振动和弹性稳定问题,计算了各种类型板的固有频率、振型和临界载荷,得到了满意的结果,此单元具有通用性好、公式推导和程序编制简单等特点,并有显式的刚度矩阵和质量矩阵,可节省计算时间。     

基于解析试函数三角形带旋转自由度膜元的显式格式研究

三角形单元是有限元分析中常用的单元.在平面单元内引入结点转动自由度,可以提高单元位移场的阶次,在不增加单元结点的前提下提高单元性能.论文利用问题基本解析解作为试函数来构造带旋转自由度的三角形单元ATF-R3H,采用了杂交应力函数单元模式,确保了单元优良的抗畸变性能和较高应力计算精度.论文利用直角坐标与三角形面积坐标的线性关系,以及面积坐标幂函数在三角形域内和边界上的积分公式,直接给出单元刚度矩阵的显式表达式,从而避免了大量数值积分,提高了计算效率.数值算例表明,显式格式的ATF-R3H单元具有良好的性能.     

埃尔米特梁单元的分块对角与高阶质量矩阵

埃尔米特梁单元常用的集中质量矩阵,是由挠度自由度对应的一致质量矩阵元素通过行求和或节点积分构造。然而,数值结果表明该集中质量矩阵在求解包含自由端的梁振动问题时,会出现频率精度掉阶现象。本文首先从保障质量矩阵最优收敛性的数值积分精度出发,分别针对三次和五次梁单元,发展了质量矩阵的梯度增强节点积分方案。利用梯度增强节点积分方案,可以得到具有分块对角形式的单元质量矩阵,而其组装的整体质量矩阵除边界节点外仍然呈现对角形式。对于两种单元,其分块对角质量矩阵分别具有4阶最优精度和6阶次优精度。再者,将标准一致质量矩阵和具有同阶精度的梯度增强节点积分质量矩阵进行优化组合,建立了具有超收敛特性的高阶质量矩阵。最后,通过数值算例系统验证了三次和五次单元的分块对角与高阶质量矩阵的频率计算精度。     

一种提高薄板稳定分析精度的方法

在薄板稳定分析中，九参数三角形薄板单元因其形状简单，使用方便，在实际工程中得到了广泛应用。本文基于参数调正的几何刚度矩阵，对九参数三角形薄板单元的一致刚度矩阵进行了修正，为提高计算精度提供了一种有效方法。     

组合结构总体节点参数自动标定的基本定理

在有限元位移法中,单元矩阵(刚度矩阵、几何矩阵、一致质量矩阵、载荷列阵等)往往是在单元局部坐标下计算的(以下简称局部方位);结构整体矩阵的形成,单元应力和变形的计算,都要求确定总体节点参数(自由度)和单 ...     

非节点连接有限元及其在加筋结构中的应用

针对现有加筋结构有限元模型的不足,提出了自由度层次的非节点连接方法.加筋单元的各节点可位于一个或多个其它单元内部,内节点的自由度无需全部与母单元的位移场一致;通过在节点坐标系下对内节点设置独立自由度,可模拟加筋构件与基体材料之间的粘结滑移、无粘结和体外布置等位移不连续性.节点为内节点的单元的刚度矩阵和荷载向量利用虚功原理变换到对应于其广义自由度向量的形式,按照广义自由度的位置向结构整体刚度矩阵和荷载向量组装,以此实现单元问非节点位置的连接.利用开发的有限元软件计算了多个算例,验证了非节点连接方法用于加筋结构有限元建模的正确性和便利性.     

A hybrid-stress element based on Hamilton principle

A novel hybrid-stress finite element method is proposed for constructing simple 4-node quadrilateral plane elements, and the new element is denoted as HH4-3fl here. Firstly, the theoretical basis of the traditional hybrid-stress elements, i.e., the Hellinger-Reissner variational principle, is replaced by the Hamilton variational principle, in which the number of the stress variables is reduced from 3 to 2. Secondly, three stress parameters and corresponding trial functions are introduced into the system equations. Thirdly, the displacement fields of the conventional bilinear isoparametric element are employed in the new models. Finally, from the stationary condition, the stress parameters can be expressed in terms of the displacement parameters, and thus the new element stiffness matrices can be obtained. Since the required number of stress variables in the Hamilton variational principle is less than that in the Hellinger-Reissner variational principle, and no additional incompatible displacement modes are considered, the new hybrid-stress element is simpler than the traditional ones. Furthermore, in order to improve the accuracy of the stress solutions, two enhanced post-processing schemes are also proposed for element HH4-3β. Numerical examples show that the proposed model exhibits great improvements in both displacement and stress solutions, implying that the proposed technique is an effective way for developing simple finite element models with high performance.     

对流_扩散问题的6节点三角形单元流线迎风有限元法和自适应网格重分技术

A streamline upwind finite element method using 6-node triangular element is presented. The method is applied to the convection term of the governing transport equation directly along local streamlines. Several convective-diffusion examples are used to evaluate efficiency of the method. Results show that the method is monotonic and does not produce any oscillation. In addition, an adaptive meshing technique is combined with the method to further increase accuracy of the solution, and at the same time, to minimize computational time and computer memory requirement.     

基于重叠划分的自由网格四边形单元计算方法

提出了一种基于重叠划分的自由网格四边形单元计算方法。这一方法将四边形单元引入到自由网格计算方法中，不仅提高了计算的精度，同时还保留了自由网格计算方法的特点。方法首先对分析域内自动生成的每一个节点建立一套临时三角形单元，利用这些临时三角形单元组合生成四边形单元，以节点为单位进行计算。由于各矩阵的计算与组集均以节点为中心进行处理，因而特别适合于并行计算环境。在详细介绍自由网格四边形单元计算方法的基础上，利用数值算例证实了这一方法改善计算精度方面的有效性。     

Triangular elements for Reissner-Mindlin plate

I-IntroductionInrecentyearsmuchresearchefforthasbeenspentonthedevel0pmentofreliableandefficientplateelementsbasedonReissner-Mindlintheory.Adifficultyisthelockingbehaviorexhibitedasl- 0(tisthethicknessoftheplate)forlowerorderc'elements.BasedonTaylorexpendi…     

Effect of the order of the finite element and selection of the constrained modes in deformable body dynamics

Finite elements with different orders can be used in the analysis of constrained deformable bodies that undergo large rigid body displacements. The constrained mode shapes resulting from the use of finite elements with different orders differ in the way the stiffness of the body bending and extension are defined. The constrained modes also depend on the selection of the boundary conditions. Using the same type of finite element, different sets of boundary conditions lead to different sets of constrained modes. In this investigation, the effect of the order of the element as well as the selection of the constrained mode shapes is examined numerically. To this end, the constant strain three node triangular element and the quadratic six node triangular element are used. The results obtained using the three node triangular element are compared with the higher order six node triangular element. The equations of motion for the three and six node triangular elements are formulated from assumed linear and quadratic displacement fields, respectively. Both assumed displacement fields can describe large rigid body translational and rotational displacements. Consequently, the dynamic formulation presented in this investigation can also be used in the large deformation analysis. Using the finite element displacement field, the mass, stiffness, and inertia invariants of the three and six-node triangular elements are formulated. Standard finite element assembly techniques are used to formulate the differential equations of motion for mechanical systems consisting of interconnected deformable bodies. Using a multibody four bar mechanism, numerical results of the different elements and their respective performance are presented. These results indicate that the three node triangular element does not perform well in bending modes of deformation.     

A 17-node quadrilateral spline finite element using the triangular area coordinates

Isopaxametric quadrilateral elements are widely used in the finite element method. However, they have a disadvantage of accuracy loss when elements are distorted. Spline functions have properties of simpleness and conformality. A 17onode quadrilateral element has been developed using the bivaxiate quaxtic spline interpolation basis and the triangular area coordinates, which can exactly model the quartic displacement fields. Some appropriate examples are employed to illustrate that the element possesses high precision and is insensitive to mesh distortions.     

基于宏观三角形分区平板壳单元的非线性有限元分析

针对剪切闭锁效应,本文研究了一种基于假设自然应变方法的宏观三角形分区平板壳单元。利用通用有限元软件ABAQUS所提供的用户自定义单元(UEL)和用户自定义材料(UMAT)子程序,本文将宏观三角形分区平板壳单元和基于损伤能释放率的混凝土弹塑性损伤本构模型成功嵌入了ABAQUS的主分析模块。经典试验McNeice双向混凝土板的数值模拟结果表明:宏观三角形分区平板壳单元对于描述板壳结构的非线性损伤行为是行之有效的。     

An improved discrete Kirchhoff triangular element for bending,vibration and buckling analyses

In this paper, an improved triangular discrete Kirchhoff thin plate element IMDKT is introduced for bending, vibration and buckling analysis. In the case of bending analysis, new boundary displacements coupled with a correction factor are introduced in the proposed element for improving the accuracy. As for vibration and buckling analyses, the combined mass and combined geometric stiffness matrices are employed to improve the calculations of natural frequency and buckling load, respectively. Several numerical examples have been used to illustrate the versatility and potential accuracy of the present methods. A comparison between the proposed and some existing elements shows that the former is superior to the latter for thin plate bending, vibration and buckling analyses.     

A reconstructed edge-based smoothed DSG element based on global coordinates for analysis of Reissner–Mindlin plates

A reconstructed edge-based smoothed triangular element, which is incorporated with the discrete shear gap(DSG) method, is formulated based on the global coordinate for analysis of Reissner–Mindlin plates. A symbolic integration combined with the smoothing technique is implemented to calculate the smoothed finite element matrices,which is integrated along the boundaries of each smoothing cell. Numerical results show that the proposed element is free from shear locking, and its results are in good agreement with the exact solutions, even for very thin plates with extremely distorted elements. The proposed element gives more accurate results than the original DSG element without smoothing, and it can be taken as an alternative element for analysis of Reissner–Mindlin plates. The prominent feature of the present element is that the integration scheme is unified in the smoothed form for all of the finite element matrices.     

Geometrically non-linear analysis of laminated composite structures using a 4-node co-rotational shell element with enhanced strains

To demonstrate the solutions of linear and geometrically non-linear analysis of laminated composite plates and shells, the co-rotational non-linear formulation of the shell element is presented. The combinations of an enhanced assumed strain (EAS) in the membrane strains and assumed natural strains (ANS) in the shear strains improve the behavior of 4-node shell element. To secure computational efficiency in the incremental non-linear analysis, the present element uses the form of the resultant forces pre-integrated through the thickness. The transverse shear stiffness of the laminates is defined by an equilibrium approach instead of the shear correction factor. Numerical examples of this study show very good agreement with the references.