用圆孔平台巴西圆盘确定岩石拉伸强度的非局部应力方法

对用圆孔平台巴西圆盘确定岩石拉伸强度的方法进行了研究.用有限元法分析了试件加载直径上的双向应力分布.由于加载直径靠近孔边处存在较大的拉伸应力梯度,如果以加载直径与中心圆孔相交点的最大拉伸应力来确定岩石的拉伸强度σt,拉伸强度的试验值会随着中心圆孔与圆盘半径之比r/R的增加而减小.采用非局部应力方法,考虑双向应力状态作用下发生破坏的Griffith强度准则的等效应力σG,在加载直径上选取材料特征尺寸,让σG"在特征尺寸上积分后取均值后得到岩石的拉伸强度σt.利用该方法得到的圆孔平台巴西圆盘测得的σt值不随r/R的变化而变化,其平均值大约为平台巴西圆盘测试值的1.23倍左右.     

预制裂缝宽度对HCFBD试件确定岩石断裂韧度的影响

为了考察人工预制裂缝宽度对确定岩石断裂韧度的影响,采用大理岩制作了含有不同预制裂缝宽度的中心圆孔裂缝平台巴西圆盘试件(hole-cracked flattened Brazilian disc, HCFBD),在RMT150B试验机上进行试验,对不同预制裂缝宽度圆盘的应力强度因子进行有限元计算,并对测试方法进行了研究。结果表明,采用将预制裂缝宽度视作零宽度裂缝方法确定的断裂韧度值偏低,给出了一种采用最小载荷和最大无量纲应力强度因子确定岩石断裂韧度的新方法,该方法能够消除预制裂缝宽度对圆盘试件测定岩石断裂韧度的影响。     

岩石动态断裂韧度的尺寸效应

采用两种圆孔裂缝平台巴西圆盘试件(一种为直径分别为42、80、122、155 mm的几何相似试件，另一种为直径80 mm、仅裂缝长度不同的单一尺寸试件)对岩石动态断裂韧度的尺寸效应进行了研究。给出了在霍普金森压杆系统上对试件进行径向撞击产生的应变波形和断裂模式。实验结果表明，对于几何相似试件，动态断裂韧度的测试值随着尺寸的增大而增大，而对于单一尺寸试件，其测试值随着中心裂缝长度的增加呈现先增大后减小的趋势。裂缝前端的断裂过程区长度和孕育时间是岩石动态断裂韧度测试值表现为尺寸效应的主要原因，为了减小尺寸效应，建立了考虑这两个参数在空间-时间域对动态应力强度因子的分布进行积分后再平均来确定岩石动态断裂韧度的方法。     

岩石断裂韧度试样CCNBD临界应力强度因子的全新数值标定

国际岩石力学学会（ISRM）提出的用人字型切槽巴西圆盘（Cracked Chevron Notched Brazilian Disc—CCNBD）测试岩石I型断裂韧度所必需的量纲为一的临界应力强度因子Y＊min的精度需要进一步改进。本文对CCNBD试样的Y＊min进行了系统的重新标定,CCNBD的几何参数有效范围为0.44≤αB≤1.04、0≤α0≤0.69、0.4≤α1≤0.8。采用有限单元法对CCNBD做三维数值分析,得到了435种CCNBD试样的Y＊min值标定结果;在此基础上全面修正了CCNBD试样Y＊min计算公式中u和v的取值表;给出了不用查表直接确定CCNBD试样Y＊min值的近似表达式,该表达式计算结果与标定结果的相对误差绝对值在1.87%以内。对于ISRM建议的CCNBD标准试样的Y＊min值：ISRM标定值0.84比本文结果0.957小12.2%;分片合成法标定值0.947比本文结果小1.0%;子模型法标定值0.943比本文结果小1.5%。本文特别强调了任何CCNBD试样Y＊min的取值必须在它对应的上限和下限所限定的范围内,这一要求对判断Y＊min标定值是否合理是很重要的。     

围压对巴西圆盘应力强度因子影响的数值分析

为了验证巴西圆盘在围压作用下应力强度因子公式的正确性,论文使用有限元分析方法计算了不同相对裂纹长度下围压单独作用以及围压与集中力共同作用时巴西圆盘的应力强度因子,并与解析解进行了对比分析.计算结果表明:纯围压作用下巴西圆盘的应力强度因子的解析解与数值解结果非常接近,两者的相对误差最大仅为0.535%;围压与集中力共同作用时的I型应力强度因子解析解与数值解也非常吻合,两者计算误差很小,仅在纯II型裂纹临界加载角附近有较大误差,但最大相对误差仅为2%,从而证明了巴西圆盘在围压作用下应力强度因子公式的有效性和可靠性.计算结果亦表明:直接将试件放在液体中加压去研究围压对断裂韧度的影响,在实验方法上缺乏理论依据.     

岩石SHPB实验加载过程中应力平衡问题分析

运用一维应力波理论,分析了弹性应力波在分离式Hopkinson压杆(SHPB)实验中的传播过程,推 导出试件和压杆中应力分布相关计算公式。探讨了有关因素对试件应力平衡时间的影响规律,发现试件应力 平衡时间受试件/压杆广义波阻抗比和入射加载升时的影响显著,而不受试件/压杆截面积比和入射加载应力 幅值的影响。结合岩石SHPB实验,计算分析了不同入射加载应力幅值在不同入射加载升时情况下,试件达 到应力平衡时的应变变化特征,并提出了降低试件在应力平衡时的应变控制方法,使试件在未达到断裂应变 之前达到应力平衡,以保证实验的有效性。得出的结论对岩石类脆性材料SHPB实验方案设计具有一定的 参考意义。     

云纹干涉法研究复合材料构件的应力强度因子

本文采用贴片云纹干涉法，测试并研究了正交异性板纯弯试件及拉伸试件的应力强度因子。文中给出了复合材料纤维加强方向不同时位移与应力强度因子的关系式，通过测试得出受力模型的全场位移，给出云纹图，进而由裂纹尖端位移场推算出应力强度因子Ｋ１及Ｋ值。试验结果与有限元计算结果吻合良好。     

温度影响下基于应力波的钛合金试件疲劳裂纹监测实验研究

本文对温度影响下应用应力波监测钛合金CT试件中的疲劳裂纹进行了研究。建立了由MTS材料试验机和温控箱组成的实验装置,模拟温度变化对应力波在钛合金试件中传播的影响。采用PZT压电元件分别在试件中激励和接收应力波信号。通过连续小波分析,提取应力波信号的多种特征用于表征疲劳裂纹的发生与发展,并对信号特征进行了统计分析。为在温度变化下监测钛合金试件中的疲劳裂纹,对信号特征进行多元偏值分析,采用马氏平方距离融合多个信号特征,在概率统计意义下确定钛合金试件中是否存在疲劳裂纹。实验结果表明了所提出方法的可行性和有效性。     

封闭应力方向对巴西圆盘试验影响的数值模拟

为揭示封闭应力对巴西圆盘应力分布和破裂演化过程的影响,开展不同方向封闭应力对巴西圆盘破裂二维数值模拟研究。将封闭应力的区域等效成一个封闭的包裹体分布在岩体中,探究不同方向封闭应力对圆盘应力分布和裂纹扩展的影响。结果表明,施加封闭应力的部位出现局部应力变化明显高于未施加的区域,随着加载的进行,施加封闭应力区域的局部应力小于周围未施加封闭应力的区域;对比有无封闭应力存在时加载过程中最大米塞斯应力,得出当封闭应力与加载方向夹角为0°时最大,为20.78 MPa;当无封闭应力和封闭应力方向为0°时,圆盘中心起裂,封闭应力方向为30°,60°,90°时,圆盘的裂纹带发生倾斜并出现多条倾斜短裂纹,圆盘未中心起裂。     

侧切试件可行性论证

文章首先阐述了侧切 SE(B)试件的基本原理,其次介绍了 K_I 因子标定结果,以及试验结果有效性分析等。从而此文全面地论证了侧切试件用于直接测定延性材料 K_(IC)值的合理性和可行性。     

A finite-element technique to analyze the data measured by the hole-drilling method

A finite-element technique to analyze the data obtained by the hole-drilling strain-gage method is presented. In this study, residual stresses are assumed as initial stresses existing in the structural material or component. It is also assumed that the elimination of the initial stresses in the region of the drilled hole changes the measured strains. After putting initial stresses into displacement finite-element equations and comparing the stiffness matrix and the initial stresses matrix with those of the previous increment, equations relating unknown initial stresses and measured strains were obtained. By solving these equations, residual stresses were obtained. In this paper three examples are studied. In the first two examples, calibration constants C1 to be used in determining residual stress were calculated which varied with depth. In the third example, the data obtained by using the hole-drilling method are analyzed. All examples show good agreement with previous studies. Using the present method allows greater flexibility of choice of specimen shape, materials, and experimental procedure than would be possible if only analytic solutions were used.     

三维电子散斑干涉法在检测残余应力中的应用

本文提出一种新的大错位三维电子散斑干涉法,并将其和钻 法检测残余应力技术结合起来,其特点一是利用三个激光器,从不同的方向照射被测物体,二是在被测物附近放置一参考物,利用大错位棱镜,使物体表面的信息和参考物上的信息都进及ＣＣＤ中,可以得到与三个位移场有关的电子散斑干涉条纹图,并可以运算和分离获得独立的ｕ,ｖ和ｗ场信息,本文介绍了大错位三维电子散斑干涉法的原理、方法和系统,并将其应用于钻孔法释放残余应     

Residual-stress measurement using surface displacements around an indentation

An experimental method is described which can measure the direction and magnitude of residual and applied stress in metals. The method uses optical interference to measure the permanent surface deformation around a shallow spherical indentation in a polished area on the metal specimen. The deviation from circularly symmetrical surface deformations is measured at known values of applied stress in calibration specimens. This deviation from symmetry can then be used to determine the direction and magnitude of tensile residual stress in specimens of the same material. Determination of compressive residual stress is more limited. A model of the indentation process is offered which qualitatively describes experimental results in 4340 steel for both tensile and compressive stress. The model assumes that the deformation around an indentation os controlled by stresses analogous to those around a hole in an elastic plate. Various conditions are discussed which affect the indentation process and its use to measure stress, including (a) the rigidity of support of the indentor and specimen, (b) the size and depth of the indentation, (c) the uniaxial stress-strain behavior of the specimen material.     

Method of calculating residual stresses in semicircular notches in a surface hardened hollow cylindrical specimen

A method is proposed to study the distribution of residual stresses in a semicircular notch in a hollow cylindrical specimen after advanced surface plastic deformation. The initial information used in the method is one or two experimentally determined components of the residual stress tensor in the hardened layer of the smooth specimen. The problem is solved using a finite element technique taking into account initial plastic strains, which are set in correspondence to the residual stresses according to the laws of elasticity. The effect of the hardening technology and notch depth on the distribution of residual stresses is studied. Experimental verification of the method showed that the calculated and experimental data on the stress distribution over the depth of the layer are in good agreement.     

Examination of the ring method for determination of residual stresses

A semidestructive method for determining residual stresses on the surface of an isotropic material is examined. The method requires that a ring be cut around the point where residual stresses are to be found. Calibration is done by using a specimen with a known residual-stress distribution. Sensitivity of the technique is found to be much better than that of the conventional semidestructive method of hole drilling.     

Direct method of solving the boundary-value problem of relaxation of residual stresses in a hardened cylindrical specimen under creep conditions

A direct method of solving a boundary-value problem for a surface-hardened cylindrical specimen affected by a tensile load under creep conditions is proposed. Relations for estimating the kinetics of the stress-strain state in the hardened layer are obtained. The adequacy of the solution is verified by experimental data on relaxation of residual stresses in the hardened layer of a cylindrical specimen made of éI 691 steel at T = 400°C. The calculated and experimental residual stresses are demonstrated to be in good agreement.     

Measuring Inaccessible Residual Stresses Using Multiple Methods and Superposition

The traditional contour method maps a single component of residual stress by cutting a body carefully in two and measuring the contour of the cut surface. The cut also exposes previously inaccessible regions of the body to residual stress measurement using a variety of other techniques, but the stresses have been changed by the relaxation after cutting. In this paper, it is shown that superposition of stresses measured post-cutting with results from the contour method analysis can determine the original (pre-cut) residual stresses. The general superposition theory using Bueckner’s principle is developed and limitations are discussed. The procedure is experimentally demonstrated by determining the triaxial residual stress state on a cross section plane. The 2024-T351 aluminum alloy test specimen was a disk plastically indented to produce multiaxial residual stresses. After cutting the disk in half, the stresses on the cut surface of one half were determined with X-ray diffraction and with hole drilling on the other half. To determine the original residual stresses, the measured surface stresses were superimposed with the change stress calculated by the contour method. Within uncertainty, the results agreed with neutron diffraction measurements taken on an uncut disk.     

Residual Stress Measurements in Finite-Thickness Materials by Hole-Drilling

Hole-drilling measurements of residual stresses are traditionally made on materials that are either very thick or very thin compared with the hole diameter. The calibration constants needed to evaluate the local residual stresses from the measured strain data are well established for these two extreme cases. However, the calibration constants for a material with finite thickness between the extremes cannot be determined by simple interpolations because of the occurrence of local bending effects not present at either extreme. An analytical model is presented of the bending around a drilled hole in a finite thickness material and a practical procedure is proposed to evaluate the corresponding hole-drilling calibration constants.     

A bending-to-stretching analysis of the blister test in the presence of tensile residual stress

The adhesion of films and coatings to rigid substrates is often measured using blister geometries, which are loaded either by an applied pressure or a central shaft. The measurement will be affected if there are residual stresses that make a contribution to the energy release rate. This effect is investigated using analytical solutions based on the principle of virtual displacements. A geometrically nonlinear finite element analysis is conducted for comparison. Furthermore, the relationships among strain energy release rate, load, deflection, and fracture radius are discussed in detail. Both analytical solutions and numerical results reveal that uniform tensile residual stresses reduce a specimen’s deflection if it experiences plate behavior under small loads. However, this effect becomes negligible when membrane stresses induced by the loading become dominant.