厚壁胞体多孔结构接触强度研究

选用H59黄铜为材料,制备了含圆形单孔、双孔、三孔以及四孔的圆柱体试样,采用型号为YE-600的液压式压力试验机对试样进行压缩试验,探讨了布孔方式对厚壁胞体多孔结构接触强度的影响;并用有限元法探讨了多孔结构的破坏机理.结果表明:双孔材料水平布孔方式优于垂直布孔方式;三孔材料斜正三角形布孔方式优于正三角形布孔方式;四孔材料正方形布孔方式优于菱形布孔方式;微孔分布半径的增大和微孔个数的增加均有助于提高厚壁胞体多孔结构的接触强度;裂纹萌生于微孔边缘且离初始接触点最近的地方,它由最大拉伸主应力引起并沿着微孔拉应力集中区进行扩展.     

多孔材料塑性极限载荷及其破坏模式分析

运用塑性力学中的机动极限分析理论，研究韧性基体多孔材料的塑性极限承载能力和破坏模式。以多孔材料的细观结构为研究对象，将细观力学中的均匀化理论引入到塑性极限分析中，并结合有限元技术，建立细观结构极限载荷的一般计算格式，并提出相应的求解算法。数值算例表明：细观孔洞对材料的宏观强度影响明显；在单向拉伸作用下，孔洞呈现膨胀扩大规律；多孔材料破坏源于基体塑性区的贯通。     

岩土力学虚拟实验仿真系统开发及其应用

数值试验是认识岩土材料细观与宏观力学行为的一种重要手段,是常规岩土力学实验的补充和延伸.本文以pfc颗粒流为平台,利用matlab和fish语言混合编程编写了岩土力学虚拟实验仿真系统,系统根据获取的岩土材料天然结构构造图像信息,可以生成含不同天然结构构造信息的岩土体试件.可以对不同规格试件实现伺服加卸载,可以监测任意点的应力应变信息,可以捕捉试件加卸载过程中的边界输入能量和摩擦能、动能及应变能的转换信息,捕捉试件的最终破坏形态和破坏过程中裂纹扩展信息及不同类型裂纹的数量演化信息.利用其可以研究岩土材料天然结构构造特征对其宏观、细观力学行为的影响.     

多轴加载下混凝土细观破坏模拟的强度准则探讨

实际工程结构中混凝土材料大多处于双轴或三轴的复杂应力状态,已有的细观力学数值研究工作大多针对单轴加载问题,对于双轴或者三轴加载条件下混凝土破坏模拟的研究相对较少。复杂受力条件下的混凝土材料破坏模拟中,细观组分强度准则选取的合理与否将成为混凝土破坏模式及宏观力学性能数值研究准确和成功与否的关键。本文旨在探讨单轴强度准则,如最大拉应变准则在多轴加载条件下混凝土破坏过程研究中运用的合理性。鉴于此,首先在细观尺度上建立了混凝土试件的二维随机骨料模型,分别采用弹性损伤本构关系模型及塑性损伤本构关系模型来描述细观组分(即砂浆基质)的力学性能,对双轴加载条件下混凝土的细观破坏过程进行数值模拟,对比了单轴强度准则和多轴强度准则下混凝土试件破坏路径及宏观应力-应变关系的差异。数值结果表明,简单的单轴强度准则难以反映双轴加载下混凝土内部应力状态的复杂性,不宜采用单轴强度准则来描述多轴加载下混凝土的破坏行为。     

水泥土细观破裂过程的实时观测试验

利用中科院武汉岩土力学研究所的岩石破裂过程细观力学实验系统,对不同水泥掺量的水泥土试件进行了单轴压缩细观实验,该试验系统可通过显微镜和数码视频装置实时观测水泥土试件的细观结构及其破坏的全过程,试验得到了水泥土破裂过程中的细观图像及其相应应力应变关系曲线.分析了不同水泥掺量的水泥土试件的细观破坏特征及其与宏观力学行为的关系,研究为水泥土细观损伤本构模型的建立提供了实验依据.     

梯度多孔材料单轴压缩弹塑性变形的宏微观数值分析

针对闭孔的密度梯度多孔材料,建立含球形孔洞的三维数值分析模型,研究其单轴压缩力学行为。首先,研究密度梯度对多孔材料宏观力学行为(如弹性模量和屈服强度)的影响;其次,研究密度梯度与材料局部力学性能的关系,得到了沿梯度方向弹性模量和屈服强度的分布规律;最后,讨论梯度多孔材料单轴压缩变形局部化机制。结果表明:当梯度材料与均质材料的总体相对密度相同时,梯度材料的宏观弹性模量和屈服强度均低于均质材料水平,其宏观应力-应变关系曲线降低;梯度多孔材料沿梯度方向的力学性能发生急剧变化,等效弹性模量沿梯度方向呈线性分布,屈服强度呈非线性曲线分布,导致沿梯度方向应力、应变呈现高度的不均匀性;多孔材料的变形局部化产生于孔隙率较大的薄弱位置,再逐渐向孔隙率较小的位置发展。由此可知,孔隙率的梯度变化影响多孔材料的力学性能,通过改变孔隙率的分布可实现材料预期的力学性质。     

基于原位观测的泡沫金属细观与宏观压缩实验研究

采用原位观测的方法研究了脆性泡沫铝材料在压缩载荷下细观与宏观断裂破坏规律和吸能机理。针对多孔泡沫金属材料提出一种细观原位加载实验方法,采用特别设计与制备的试件,在S570扫描电镜下研究了特定胞孔在压缩过程中孔壁的失效顺序和破坏规律,并揭示了能量吸收的细观机理。对块体材料的宏观压缩实验表明,脆性泡沫铝是以多个断裂带的形式破坏。研究发现,孔壁缺陷和胞孔形态缺陷是诱发断裂带形成与发展的重要因素。依据尺寸效应对细观与宏观实验下泡沫铝的性能进行了比较。     

一个简化的空穴多级形核模型

1 引言为在细观机理基础上建立韧性材料在一定应力状态下宏观裂纹产生和发展的力学模型。一些学者已做了不少工作.人们力图通过细观研究找到一个较接近韧性材料损伤和断裂物理本质的材料破坏准则,以用来描述和预测韧性材料的损伤和断裂.直到现在,大多数研究都认为无裂纹体与裂纹体的破坏是两个截然不同的问题.人们一直是用不同的准则来判定无裂纹试件和含裂纹试件的破坏的.但若从细观角度来看,对     

混凝土中心裂缝单轴拉伸损伤断裂数值模拟研究

基于对混凝土细观力学的认识,假定混凝土是由砂浆基质,骨料及它们之间的界面组成的三相复合材料,各组分的材料性质按照某个给定的Weibull分布来赋值,细观单元满足弹性损伤的本构关系,应用细观力学损伤模型研究了混凝土的宏观力学性质,并且通过有限元程序对中心裂缝混凝土试件在单向拉伸情况下的破坏过程进行了数值模拟.模拟结果表明,该模型可以用来研究单向载荷作用下混凝土结构的破坏机理.     

混凝土拉伸断裂的细观数值分析

根据混凝土试件拉伸和三点弯曲的物理模型,用梁-颗粒模型BPM 2D(B eam-Particle M ode l)模拟了混凝土拉伸和三点弯曲试件微裂纹的萌生、扩展直至试件宏观破坏的全过程。在梁-颗粒模型中用三种类型梁单元形成混凝土细观数值模型,每种类型梁单元的力学性质均按韦伯(W e ibu ll)分布随机赋值以模拟混凝土细观结构的非均匀性。数值模拟结果给出了混凝土拉伸应力-应变曲线和三点弯曲载荷-位移曲线,以及混凝土试件破坏过程最大应力分布图和裂纹扩展图。数值模拟结果显示混凝土破坏过程实际上就是微裂纹萌生、扩展、贯通,直到宏观裂纹产生导致混凝土失稳断裂的过程。通过对数值模拟结果的分析,揭示出混凝土在拉伸条件下裂纹尖端的拉应力集中是裂纹扩展的动力,混凝土组成材料力学性质的非均匀性是造成裂纹扩展路径曲折的重要原因。     

Fracture analyses of different pre-holed concrete specimens under compression

Crack propagation processes in specially prepared concrete discs and rectangular specimens containing a single cylindrical hole or multiple holes of varying diameters have been studied both experimentally and numerically.In this research, the cracks coalescence paths in Brazilian disc and rectangular specimens made from rock-like material containing multi-holes are investigated. These concrete specimens are specially prepared from an appropriate mixture of Portland Pozzolana Cement(PPC), fine sands, and water.The pre-holed Brazilian discs and rectangular specimens are experimentally tested under compression. The breakage load in the ring type disc specimens containing an axial hole with varying diameters is measured and the distribution of the induced lateral stress is obtained. The mechanism of cracks propagation in the wall of the ring type specimens is also studied. In the case of multi-hole Brazilian disc and rectangular specimens, the cracks propagation and cracks coalescence are also investigated. These experiments are numerically modeled by a modified higher order displacement discontinuity method. It has been shown that the corresponding experimental and numerical results are in good agreement with each other. The results presented in this research validate the accuracy and applicability of these crack analyses procedures.     

高炉炉壳开孔位置对应力集中的影响

考虑到冶金行业中高炉炉壳开孔的实际情况，本文应用有限元分析的方法研究受远场均匀拉伸载荷，二维有限区域内菱形分布的圆孔中间不同开孔位置下的应力分布，得到最大应力集中系数随孔位置变化的三维变化曲面。此外，孔沿座标轴及沿原孔边缘位置变化对应力集中系数的影响被详细研究，从而为合理设计炉壳开孔提供了理论依据。     

岩石深孔爆破对邻近煤层的动应力作用

为解决松软煤体爆破孔成形困难导致深孔预裂爆破技术无法应用的问题,选择在运输巷底板距煤 层较近的岩石中进行爆破,利用数值模拟方法进行了相关理论探讨。分析了煤岩介质和单煤体介质中布孔的 差异,建立了单煤体和煤岩体深孔预裂爆破的5个数值计算模型。研究了单煤体和煤岩介质爆破孔与抽放孔 连心线上有效应力随距离的变化,从岩孔爆破传播到煤层其应力衰减的程度较单煤层中大得多,但在靠近抽 放孔附近煤层,二者的差距变小。抽放孔轴线方向所受有效应力的大小是决定爆破效果的重要因素,煤岩介 质中爆破孔与抽放孔间距为2.0m 时,抽放孔轴线方向上的平均有效应力与单煤层中爆破孔与抽放孔间距 为3.0m 时的相当,可作为实现岩孔爆破效果的布孔参数。     

The effects of surface injection through a perforated square cylinder on some aerodynamic parameters

The surface pressure distribution and the vortex shedding frequency were investigated for the flow around perforated horizontal and diagonal square cylinders with surface injection through various surfaces. For this purpose, surface pressure measurements on each square cylinder (horizontal and diagonal) and vortex shedding frequency measurements in the wake region were performed at three different Reynolds numbers in a wind tunnel. The parameters considered were injection coefficient, position of perforated surface (i.e., top, rear, top-rear and all), pressure coefficient, drag coefficient, and the Strouhal number. The results showed that pressure coefficient distribution, drag coefficient, and the Strouhal number were influenced by the position of the perforated surface and by the injection coefficient. The surface injections through the top-rear, rear and all surfaces of a diagonal square cylinder reduce the drag coefficient for the all Reynolds numbers, while the injection through all surfaces only reduces the drag coefficient of a horizontal square cylinder. The other aerodynamic parameter Strouhal number can also be controlled by injection through certain surfaces of a horizontal square cylinder.     

有限宽板孔边弹塑性变形测试

测量应变集中区域的弹塑性变形，对于研究材料损伤或微裂纹的产生，以预防宏观裂纹的产生及扩展具有重要的意义。为给航空发动机轮盘的损伤容限设计研究提供相关材料的力学实验参数，做了两个有限宽中心带孔试件的拉伸试验。试验中，采用单调逐级加、卸栽的循环加栽方式，并应用自动网格法和数字图像相关技术测量了孔用的全场位移分布。再应用最小二乘法将离散的位移分量拟合成二元多项式函数，求解出拉伸方向的应变分布，并给出孔边应力σ与孔边应变εy的关系曲线。     

On the optimum shape of apertures for a perforated plate subject to bending

The problem of finding the optimum shape of the holes in a perforated plate weakened by a triangular or square lattice of holes and subject to bending is considered by methods based on the theory of functions of a complex variable. The criterion determining the optimum shape of the hole is based on the condition that no stress concentration should occur on the hole contour or, alternatively, that a plastic region should be created around the whole contour of the hole at exactly the same instant.     

Stress-concentration factors at intersecting and closely approaching orthogonal coplanar holes

Using two models, each containing three groups of intersecting or closely approaching holes, 18 different cases were investigated by three-dinensional frozen-stress photoelasticity. In all cases, the coplanar holes were orthogonal to the applied uniaxial tension. Included were three cases of intersecting hoes with square corners and varying hole-diameter ratios. Five cases of intersecting holes with rounded corners were studied for two hole-diameter ratios and varying corner radius. Stresses were determined for two cases where the end of one drilled hole partially penetrated another hole leaving acute corners or feathered edges at the intersection. Three types of closely approaching holes were studied: two cases in which the end of one drilled hole nearly intersected the side of an-other hole, two cases in which the ends of two drilled holes approached each other along a common axis, and four cases (called corner-approach cases) in which the ends of two drilled holes approached each other along orthogonal axes. A stress-concentration factor of 13 was found for one of the partially penetrating drilled-hole cases. The upper limit on stress-concentration factor for a very small hole intersecting a large hole in an infinite body subjected to uniaxial stress is 8.4 for metals. This factor is reduced to 5.2 as the diameters of the intersecting holes become equal. Rounding the corners on intersecting holes reduced the stress concentration by only four to seven percent. Closely approaching drilled holes results in higher stresses than fully intersecting holes when the minimum ligament width is less than ten percent of the hole diameter. Corner approach cases do not result in high stress-concentration factors as long as the ligament width is greater than the percent of the hole diameter.     

Creep simulation of asymmetric effects by use of stress mode dependent weighting functions

The paper presents a framework for creep modeling of materials exhibiting different behaviors in different loading scenarios, such as tension, compression and shear, respectively. To this end an additive decomposition of the flow rule is assumed into a sum of weighted stress mode related quantities. The characterization of the stress modes is obtained in the octahedral plane of the deviatoric stress space in terms of a single scalar variable, such that stress mode dependent scalar weighting functions can be constructed. Furthermore the numerical implementation into a finite element program of the resulting set of constitutive equations and aspects of the sensitivity analysis for parameter identification are addressed. Verification of the constitutive equations is succeeded for an aluminum alloy AK4-1T and a superalloy René 95, respectively. In two finite element examples the proposed model is applied to investigate the relaxation behavior of a square plate with circular hole and the evolution of creep damage in a gasturbine blade subjected to centrifugal and thermal loads.     

Calculation of shells with large rectangular holes in the presence of finite bending deflections

The stability of shells perforated by large holes has been investigated previously [1–6]. The results published in the cited papers lead to the conclusion that the problem of the stability of shells with large holes is in a stage of vigorous development. The application of standard numerical methods in these problems is impeded by the fact that they are incapable of refining the stress concentration and local stability in the vicinity of corners of the holes and give an approximate smoothed distribution pattern of the forces and torques. Methods of approximation of the solutions in terms of regular functions [2] are complicated by the poor convergence of the corresponding series near the edges of a hole.Structural Engineering Institute, St. Petersburg. Translated from Prikladnaya Mekhanika, Vol. 30, No. 2, pp. 41–48, February, 1994.     

固体材料不稳定性的特征

基于分析势函数的二次变分,从理论上证明了固体材料不稳定性主要取决于材质不断退化的重要特征。另一特征是：材料往往会由基本变形路径漂移为一个轴向应变被限定的模态以至的失稳。文中以有限元方法计算模拟受周期性分布孔洞损伤的平面板材模型,结果显示,孔周边的应变局部化使变形路径转移到一个轴向应变被限定的失效模态。此类现象与金属板材拉胀实验中所观测到的结果相符合。