含面内转动自由度的广义协调曲面矩形扁壳元

扁壳单元中引入结点转角自由度可以在不增加结点的情况下,增加位移场的阶次,提高计算精度,从而显著地提高单元性能。同时在单元中引入泡状位移场,能有效地扩大了单元位移场的解空间,所构造的单元具有计算精度高、对计算网格畸变不敏感的优良特性。本文利用广义协调薄板单元RGC-12的位移函数作为扁壳元的法向位移,利广义协调矩形膜元的位移函数作为扁壳面的切向位移,通过附加面内转动自由度构造了一个具有24个自由度的4结点广义协调曲面矩形扁壳元GRC-S24。在此基础上再增加一个广义泡状位移,又构造了一个具有更高计算精度的曲面矩形扁壳元GRC-S24M。并通过实例分析对这两个单元的收敛性和精度进行了验证。     

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。     

用于热应力分析的体—壳过渡元

以往体－壳过渡元中采用的一般三维应变状态下的初即热应变表达式，与过渡元规定的变形方式不一致。本文利用“相应体元”算出１５节点过渡元热膨胀时因壳面上法线不伸长引起的应变，以此修正一般三维初始热应变，给出过渡元初始热应变的正确表达式。本文方法扩大了体－壳过渡元的应用范围。     

用于热应力分析的体－壳过渡元

以往体－壳过渡元中采用的一般三维应变状态下的初始热应变表达式，与过渡元规定的变形方式不一致。本文利用“相应体元”算出１５节，点过渡元热膨胀时因壳面上法线不伸长引起的应变，以此修正一般三维初始热应变，给出过渡元初始热应变的正确表达式。本文方法扩大了体－壳过渡元的应用范围。     

加肋开孔柱壳混合有限条——有限元屈曲分析

本文提出了一种分析环加肋开孔柱壳屈曲问题的混合有限条──有限元法。环加肋柱壳作为一个构造上的正交各向异性壳处理，柱壳非开孔区采用有限条元离散，开孔区采用有限单元离散。在有限条元与有限单元交界面上，根据位移协调条件建立条元和单元的耦合关系，并据此构造一种特殊的过渡单元、联接条元和单元，进行整体分析。算例表明，这一方法对开孔柱壳屈曲问题的分折十分有效。     

拟协调大变形矩形扁壳元及其应用

本文采用拟协调元方法,引用简化的扁壳应变分量,构造了一个大变形矩彤扁壳单元,该单元适用于薄板壳的线性和几何非线性分析,数值例题的结果表明本文单元的性态很好。     

关于非协调位移元与广义杂交元的等价性的进一步研究

本文通过定义非协调位移元的单元特性函数,提出了一种建立非协调元与广义杂交元之间的等价关系的一般方法,进一步证明了两种有限元模型之间存在强等价性,为两种单元模型的构造提供了相互借鉴的理论依据和有效的准则。     

拟协调SemiLoof和Loof扁壳元

1 前言目前工程上对任意壳结构分析常用的平板壳元和扁壳元存在着一个问题:如果一个结点周围的单元共面或近似共面,则对应垂直这个面的法向转角θ_N 的刚度是零或近似为零,这时若θ_N 没有被约束住,则结构刚度阵是奇异的,造成了求解困难.现有的一些解     

板锥网壳结构几何非线性受力性能的广义协调元分析

板锥网壳网络是一种新型的空间结构，它是在板锥单元和常规的双层刚壳结构的基础上组合形成的一种新型结构形式，具有良好的技术经济效益和建筑视觉效果。本文在对这类结构有限法分析的基础上，根据板锥网壳结构的构成特点，应用广义协调元的基本思想，对这类结构进行了分析，给出了这类结构广义协调元分析的基本公式。分析表明：广义协调元法适宜于板锥网壳结构的受力性能分析，广义协调元固有的简便，高效和可靠的特性，将会使结构分析得到更为可信和可靠的论证。     

线性蠕变问题的摄动边界元-有限元方法

本文将摄动、边界元、有限元方法结合起来,提出一种求解线性蠕变问题的新方法。该方法不采用一般增量法中在一个时段内各物理量保持不变或作线性变化的假设,加大了计算步长提高了精度。文中构造了边界元摄动格式,构造了包含钢筋在内的边界元有限元耦合摄动格式,并给出了满意的数值结果。     

Electrode layers in flows of an inviscid plasma with good conductivity

The structure of the electromagnetic electrode layers that are produced in flows across a magnetic field by a completely ionized and inviscid plasma with good conductivity and a high magnetic Reynolds number is examined in a linear approximation. Flow past a corrugated wall and flow in a plane channel of slowly varying cross section with segmented electrodes are taken as specific examples. The possibility is demonstrated of the formation of nondissipative electrode layers with thicknesses on the order of the Debye distance or electron Larmor radius and of dissipative layers with thicknesses on the order of the skin thickness, as calculated from the diffusion rate in a magnetic field [2].In plasma flow in a transverse magnetic field, near the walls, along with the gasdynamie boundary layers, which owe their formation to viscosity, thermal conductivity, etc. (because of the presence of electromagnetic fields, their structures may vary considerably from that of ordinary gasdynamic layers), proper electromagnetic boundary layers may also be produced. An example of such layers is the Debye layer in which the quasi-neutrality of the plasma is upset. No less important, in a number of cases, is the quasi-neutral electromagnetic boundary layer, in which there is an abrupt change in the frozen-in parameter k=B/p (B is the magnetic field and p is the density of the medium). This layer plays a special role when we must explicitly allow for the Hall effect and the related formation of a longitudinal electric field (in the direction of the veloeiryv of the medium). We will call this the magnetic layer. The magnetic boundary layer can be dissipative as well as noudissipative (see below). The dissipative magnetic layer has been examined in a number of papers: for an incompressible medium with a given motion law in [1], for a compressible medium with good conductivity in [2], and with poor conductivity in [3]. In the present paper, particular attention will be devoted to nondissipative magnetic boundary layers.     

A twofold strength and toughness criterion for the onset of free-edge shear delamination in angle-ply laminates

Free edge delamination in composite structures results from very localised stress fields which induce a stress concentration promoting the nucleation of an interfacial crack. To predict such a delamination onset at the free edge of a $(\pm \theta {)}_s$ laminate in traction, use is made of a strength and toughness criterion which combines a stress condition with an energy analysis. A generalised plane strain model allows to determine the stress distribution near the free edge and the energy released by the nucleation of an interfacial crack. The results show that this approach can predict the delamination onset for $((\pm 10{)}_s\text{,}(\pm 20{)}_s)$ laminates provided the interfacial fracture energy and interlaminar shear strength are known. These characteristic values can be identified with the help of traction tests performed on samples with different thicknesses.     

An Algebraic Method of Stabilization for a Class of Boundary Control Systems of Parabolic Type

Stabilization of linear parabolic boundary control systems is studied. The boundary control system is composed of a system of linear differential operators (, ) in a bounded domain with the smooth boundary. A significant feature of the paper is that, while being a standard elliptic operator, characterizes the boundary condition partly of the Dirichlet type and partly of the generalized Neumann type. We present a new algebraic approach and show that the stabilization is achieved under the standard controllability and observability conditions associated with the system.     

An absence of a certain class of periodic solutions in the Navier-Stokes equations

In the case of the 3D Navier-Stokes equations, it is proved that there exists a constant>0 with the following property: Every time-periodic solution with a period smaller than is necessarily a stationary solution. An explicit formula for is also provided.