层状地基轴对称问题的Mindlin解

本文在文献〔１〕的基础上，对层状地基应力和位移的计算方法做了一些创新的工作，首先作者提出求解传矩阵的逆矩阵的简便公式。并在应力、位移的计算上，对荷载作用面上下分别采用二种不同的传递矩阵。加快了计算速度，避免了层状体系计算中常见的溢出问题及大数减大数造成的计算困难。     

求解双参数层状地基模型的积分变换法

计算弹性地基梁板时，大都采用文克尔地基模型。由于该模型过于简化，不能正确反映土的工程性质，为此本文提出了一种双参数层状地基模型。该模型由一系列的弹性层组成，并对每一层中应力应变分布做了假设。通过积分变换的方法可以求出每一层表面处位移与力之间的关系，进而形成层刚度矩阵。按照有限元法的原理，可把每一层的刚度矩阵凝聚成总体刚度矩阵进行求解。本文模型是V1azov模型的延伸和发展。通过与V1azov模型计算结果的比较，证明本文方法是正确的。并且本文得到了荷载作用于层状模型内部时的解答，为将双参数地基模型用于桩基分析打下了理论基础。     

用边界元方法分析复合材料中的裂纹问题

利用层状材料的广义Klevin基本解，建立了计算三维层状材料中的裂纹边界元方法。采用边界元方法中的多区域方法和能反映均匀介质中裂纹尖端应力场和位移场特征的面力奇异单元。裂纹的应力强度因子由裂纹面上的位移经插值计算得到。算例分析表明，本文建议的方法可以获得较高的计算精度。     

梯度材料中矩形裂纹的对偶边界元方法分析

采用对偶边界元方法分析了梯度材料中的矩形裂纹. 该方法基于层状材料基本解,以非裂纹边界的位移和面力以及裂纹面的间断位移作为未知量. 位移边界积分方程的源点配置在非裂纹边界上,面力边界积分方程的源点配置在裂纹面上. 发展了边界积分方程中不同类型奇异积分的数值方法. 借助层状材料基本解,采用分层方法逼近梯度材料夹层沿厚度方向力学参数的变化. 与均匀介质中矩形裂纹的数值解对比,建议方法可以获得高精度的计算结果. 最后,分析了梯度材料中均匀张应力作用下矩形裂纹的应力强度因子,讨论了梯度材料非均匀参数、夹层厚度和裂纹与夹层之间相对位置对应力强度因子的影响.      

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 ...     

成层非饱和地基上矩形基础稳态响应解析研究

采用积分变换法求解非饱和土的控制方程,得到变换域内土体的位移和应力表达式;建立了单层非饱和土体的刚度矩阵,并组装每一层的刚度矩阵,构成了层状地基的总体刚度矩阵;结合地基上下表面的边界条件,推导了层状非饱和地基表面位移的积分形式解答。另外,选取带有补充项的双重余弦级数解作为矩形基础的振型函数,并令其与地表位移按余弦级数展开的表达式相等,建立了矩形基础与地基的协调条件。最后,联立矩形基础的控制方程、边界条件和基础与地基之间的协调条件,求解得到矩形基础的挠度幅值、弯矩幅值以及基底压力幅值。选取已有文献中的非饱和土参数计算,其结果与文献吻合良好,验证了本文方法的正确性。本文进一步研究了单层地基和双层地基上矩形板的动力响应,分析了土体参数对矩形基础动力响应幅值的影响规律。结果表明:地基层厚与基础尺寸之比为5时,地基就可以看作半空间地基;矩形基础的稳态响应随非饱和土的饱和度的增大而减小;渗透率对矩形基础动力响应的影响不明显。     

多层地基上轴对称受荷刚性圆板问题

利用刚性圆板表面各点位移相等,并结合刚性圆板与地基表面的位移相容条件与光滑接触条件,经由Hankel变换,推导出了刚性圆板与分层地基表面接触应力的对偶积分方程;求解该对偶积分方程,再由多层地基应力与位移的传递矩阵解,并经Hankel逆变换,得到了多层地基上轴对称受荷刚性圆板问题的解.编制了计算程序,并进行了数值分析与计算.计算结果表明:对均匀地基而言,实际工程的计算分析可只考虑4倍刚性圆板直径以内深度范围内的应力与位移;而地基的分层性对地基的位移和应力有着较大的影响,简单地将均匀地基的结论推广到分层和非均匀地基是不恰当的.     

非线性复合材料的一种杂交应力有限单元方法

建立了非线性复合材料模型的杂交应力有限元方法,并在材料主坐标系下提出直接方法计算单元非线性应力场,然后由此计算单元切线刚度矩阵和剩余载荷并转换到整体坐标系下,利用Newton-Raphson方法进行结构的位移迭代。在Hahn-Tsai非线性复合材料杂交元分析中,由位移和应力方程所导出求解单元非线性应力场的简单迭代法是条件收敛的,对较大载荷当迭代位移增加到一定程度以后无法得到应力收敛解。但是,利用本文提出的直接法由于完全避免了非线性应力场迭代,不仅很好地解决了这一问题,而且极大地提高了计算效率。数值算例说明该方法是确实有效的。     

线弹性多材料接头端部应力奇异性特征分析

文章研究多材料接头并计算其应力奇性特征.通过引入接头端部位移场的渐近级数展开式,将应力平衡方程转化为关于奇性指数的特征常微分方程组,由插值矩阵法求解获得多材料接头应力奇性指数以及相应的位移特征函数,与已有的结果对照证实了本文方法的有效性.本文计算结果还表明了多材料接头结构在不同材料粘结界面处位移场特征函数的一阶导数发生了突变,导致应力场在接头粘结界面处不连续.     

构造满足特征值要求的杂交元应力子空间

通过引进适当参数给出了杂交元应力空间特征值与参数之间的关系,从而可以通过调节参数来构造满足特征值即模态刚度要求的杂交元应力子空间。本在位移元本征应力模式基础上引进调节参数,同时,利用矩阵H对角化方法计算杂交元应力子空间的本征应力模式,然后由此方便有效地计算特征值,从而大大提高了计算效率。本通过建立Q4杂交应力元特征值与参数之间关系说明了这一方法是确定可行的。     

非牛顿流体传递过程研究进展及应用

本文简述了非牛顿流体的传递过程的学科发展史.本学科从50年代开始,到80年代形成完整的体系.并综述了非牛顿流体的动量、热量和质量传递的最新研究成果及动向.     

Flow and heat transfer analysis in porous wick of CPL evaporator based on field synergy principle

In order to optimize the structure of a CPL evaporator and enhance heat transfer, a mathematical and physical model is developed to analyze the flow and heat transfer in the porous wick of the evaporator, whose calculation domain is divided into two parts: vapor-saturated region and liquid-saturated region. The characteristics of flow and heat transfer in the porous wick of a CPL evaporator have been numerically studied according to the field synergy principle. The influences of geometrical structures and heat flux on heat transfer enhancement are analyzed and illustrated by the figures in the present paper.     

Preliminary results of MCPHE by experimental studies

The influence of grooves in the U-turn areas for the multi-channel-plate heat exchangers (MCPHEs) is significant due to the friction and flow phenomena in this region. In this study, two types of MCPHE made of acrylic plates were tested: one with grooves in the U-turn area, one without. During this series of experiments, heat transfer rate, overall volumetric heat transfer coefficient, Nusselt number and overall pressure drop (i.e., including the entrance and exit losses) were measured and calculated in order to understand the overall performance of these two different constructions of MCPHE. The experimental results show that the heat exchanger without grooves in the U-turn area possessed higher heat transfer performance and lower overall pressure drop.     

Heat transfer and flow temperature measurements in a rotating triangular channel with various rib arrangements

In the present study, the regionally-averaged heat transfer coefficients and flow temperature distributions were measured in an equilateral triangular channel with three different rib arrangements (α = 45, 90 and 135°). To measure regionally-averaged heat transfer coefficients in the channel, two rows of copper blocks and a single heater were installed on two ribbed walls. The fluid temperature distributions were obtained using a thermocouple-array. The rotation number ranged from 0.0 to 0.1 with a fixed Reynolds number of 10,000. For the 90° ribs, the heat transfer coefficients on the pressure side surface were increased significantly with rotation, while the suction side surface had lower heat transfer coefficients than the stationary channel. For the angled ribs, rib-induced secondary flow dominated the heat transfer characteristics and high heat transfer rates were observed on the regions near the inner wall for the 45° angled ribs and near the leading edge for the 135° angled ribs.     

Étude numérique de l'écoulement d'un fluide non newtonien thermodépendant entre deux plaques parallèles

In this study, the heat transfer of a non Newtonian thermodependent fluid flowing between two parallel plates is considered. The effects of different parameters on the evolutions of thermal boundary layer and of Nusselt number are numerically investigated in two heating cases and correlations are proposed to compute the heat transfer. To cite this article: N. Van Tuan, M. Lebouche, C. R. Mecanique 333 (2005).     

基于惯性参考系基准的快速传递对准方法

研究了以惯性参考系为基准的新型传递对准方法。推导了计算惯性坐标系和计算体坐标系传递对准动态误差模型,并给出了相应的"速度+姿态"观测方程。基于惯性参考系的对准方法通过链式法则将子惯导输出的姿态矩阵描述为三个变换矩阵之积,其中两个变换矩阵通过对准时间和主惯导提供的位置信息可得到精确求解,剩余的变换矩阵(子惯导体坐标系至惯性坐标系间的变换矩阵)通过子惯导陀螺仪的输出进行解算,其误差通过传递对准估计得到的失准角进行补偿。对提出的两种对准方法进行摇摆实验验证,方位对准误差优于4’(1)。与传统基于导航坐标系的方法相比,基于惯性坐标系的方法直接将误差定位到惯性坐标系上,具有算法简便的特点。     

The influence of multiple tubes on the tube-to-bed heat transfer in a fluidised bed

There have been few studies modelling both flow and heat transfer in fluidised beds. The kinetic theory of granular flow (KTGF) has been used for flow prediction in the past without heat transfer modelling. In the present study, a two-fluid Eulerian–Eulerian formulation incorporating the KTGF was applied first to a tube-to-bed reactor with one immersed tube and compared with the results in the literature. The bed was then modified to introduce two and three heated tubes. The effects on the flow and temperature distribution, local heat transfer coefficients and averaged heat transfer coefficients over a 3.0 s time period were carried out. Results showed that increasing the number of tubes promotes heat transfer from tubes to the particles and flow. The heat transfer coefficients extracted from the single-tube to three-tube cases were analysed in detail, confirming the importance of linking flow/particle and heat transfer calculations.     

Large Eddy Simulations of Turbulent Mixing Layers Excited with Two Frequencies

In this study, we investigate the energy transfer during the pairing and merging process of two vortices into one in an excited turbulent mixing layer using Large Eddy Simulations. We present simulations of natural and periodically excited mixing layers for validation purposes and study the vortex pairing dynamics by exciting the mixing layer by two frequencies. The results help in understanding the effects of the energy transfer in the long-wave turbulent spectrum and assessing the role of backscatter.     

大陀螺零偏条件下的快速传递对准算法

针对某些某些微机械陀螺零偏重复性差的特点,提出了滤波反馈修正和陀螺零偏粗对准预处理两种方法,使“速度＋姿态”快速传递对准算法在大陀螺零偏条件下能够不损失估计精度。在简要介绍“速度＋姿态”．决速传递对准算法数学模型的基础上,探讨了大陀螺零偏导致的惯导系统非线性误差。为减小上述非线性误差的影响,提出用每一步滤波估计值修正子掼导状态的反馈修正方法,和在进行卡尔曼滤波前直接测量比较主、子惯导陀螺输出的陀螺零偏粗对准预处理方法。仿真结果表明,采用上述两种方法,快速传递对准算法可在陀螺零偏过大的情况下保持算法的有效性和估计精度。     

二维系统传递矩阵法

以薄板横向振动的振动特性问题为例提出了二维系统传递矩阵法. 从质点和无质量梁的传递 矩阵出发,建立了按列排列的薄板子结构的传递矩阵. 用二维系统传递矩阵法获得了整个板 的总体传递方程,从而可得到板在任意一种边界条件下的特征方程. 数值求解了两种情况下 薄板横向振动的固有振动特性. 计算结果表明,用该方法可用于研究类似薄板的二维系统的 动力学问题,且无需建立系统的总体动力学方程.