扩展裂纹尖端奇异场的实验研究

用云纹方法测量了 LY12-M 铝材,双边裂纹试件、扩展裂纹沿 x和y方向位移场u_x,u_y。实验的裂纹尖端奇异场与 GH 理论奇异场进行了比较。两者偏差在±10％范围内,得到实验的 GH 奇异场范围与形状。实验证明:扩展裂纹尖端场有(lnA/r)~(α+1)奇异主导区。该主导区形状由腰子形向扁圆、圆形过渡,接近裂纹扩展时形状不规则。在 GH 主导区内,裂纹尖端附近有一个三维贲形,材料损伤区。在该区内 GH 奇异性不存在。     

幂率型非线性粘弹性裂纹尖端场

研究幂率型非线性粘弹性裂纹尖端场为了推导的需要,首先列出了幂率型硬化材料的HRR奇异场和高阶渐近场论证了它们实质上是各向同性、不可压缩、幂率型、非线性弹性裂纹尖端场,回顾了求解非线性粘弹性问题的弹性回复对应原理之后,给出了在第一类边界条件下求解幂率型非线性粘弹性材料裂纹问题的对应原理得到了幂率型非线性粘弹性材料,特别是改性聚丙稀的裂纹尖端应力、应变和位移的解答.     

裂纹尖端扩展位移场的云纹干涉实验分析

1.前言在裂纹的稳定扩展问题中,能否用J 作为控制扩展的参数是一个有争议的问题.文献[1]从理论上证明:在某些条件下,J 可用于分析和描述扩展.本文用实验的方法研究了扩展问题,对含中心裂纹的铝板试件,在扩展过程中的裂纹尖端位移场进行了分析,证明并讨论了裂纹尖端HRR 场及其变化,并在此基础上用HRR 理论拟合实测位移场求出了J以及J-△a 曲线.     

不同材料界面Ⅲ型裂纹尖端场实验研究

本文应用激光全息干涉法获得了两种材料Ⅲ型界面裂纹试件的离面位移场,通过试验数据处理求得了裂纹尖端附近位移、应力场强度的控制参量K_(Ⅲ),J值,给出了局部解的适用区域。还研究了两种材料粘结界面处的连续条件,分析了结果的合理性。为了对比和分析界面裂纹问题,还对同种材料试件进行了试验和数据处理。     

复合材料断裂力学参量的实验测定

本文采用三维云纹干涉仪同步测量含裂纹复合材料弯曲板的面内位移场及离面位移场，并对离面位移场云纹图进行计算机自动采集和处理，编制了云纹数字图像处理软件。文中推导了正交异性复合材料弯曲问题的离面位移场表达式，得到了弯曲板裂纹尖端位移w与应力场强度因子K1的关系式。通过实测位移，结合裂尖位移场推导出应力强度因子K1值。     

HRR理论的近似解析解

本文根据文献[3]给出的HRR 解的角函数数值表,利用数值拟合方法,给出了HRR理论的近似解析解.本文结果不仅形式简单,而且和精确解符合得很好.对幂硬化指数n在0和1之间的任何弹塑性材料均适用.给进一步研究裂纹尖端附近的弹塑性应力应变场以及工程安全评定提供了一个方便的解析工具.为了计算方便,我们把应力、应变、位移无量纲化,它们与实际应力、应变、位移的关系为     

双材料界面Ⅰ型扩展裂纹尖端的弹黏塑性场

双材料界面中存在材料黏性效应, 对界面裂纹尖端场的分布和界面本身性能 的变化起着重要的影响. 考虑裂纹尖端的奇异性, 建立了双材料界面扩展裂纹尖端的弹黏塑 性控制方程. 引入界面裂纹尖端的位移势函数和边界条件, 对刚性-弹黏塑性界面I型界面 裂纹进行了数值分析, 求得了界面裂纹尖端应力应变场, 并讨论了界面裂纹尖端场随各影响 参数的变化规律. 计算结果表明, 黏性效应是研究界面扩展裂纹尖端场时的一个主要因素, 界面裂纹尖端为弹黏塑性场, 其场受材料的黏性系数、马赫数和奇异性指数控制.     

应用云纹干涉法测量力电耦合作用下铁电陶瓷的破坏行为

本文采用云纹干涉系统对的电陶瓷在力电耦合载荷作用下裂纹尖端的力学行为进行全场实时非接触动态细观测量,采用三点弯实验获取裂纹尖端区域在力电耦合作用下与电场集中有关的电致伸缩位移场,应变场,通过分析实验取得的云纹图得到了裂尖区域的位移场,应变场,发现裂尖区域就变随着与裂尖距离的增加衰减的速率比没有电场作用下的理论计算结果要快。     

瓷修复体界面断裂行为的模拟实验研究

本文利用云纹干涉法和云纹干涉－－有限元混合法，对瓷修复体的模拟双材料模型界面断裂问题进行了实验研究。用云纹干涉和数字错位云纹干涉法测量带边裂纹的双材料四点简支梁在剪切作用下界面表面的剪应变分布及界面两侧局部表面的位移场，实验表明，由于界面两两侧材料力学性质不同，表现出界面剪切断裂问题的非称性和裂尖附近复合型断裂的特点；用云纹干涉法和有限元法相结合的混合法对粘接界面角点应力奇异性进行研究，并对角点附近应力应变场作了分析，得到了应力奇异指数与边界楔角，载荷的关系，证明了用界面应力强度因子Kf来描述界面端部区域应力分布的公式，并得到了双材料界面端部区域的应力应变分布情况。本文的实验结果为进一步研究口腔金瓷修复体界面的优化设计提供了基础，同时也说明云纹干涉法对于双材料界面断裂行为的研究是有效的。     

幂硬化弹塑性-刚性界面Ⅲ型定常扩展裂纹尖端的渐近场

对幂硬化弹塑性材料－刚性材料界面上裂纹以定常方式扩展的Ⅲ型问题进行弹塑性渐近分析，给出裂纹尖端的应力，应变和位移场解。通过数值计算，考察了不同Mach数以及裂纹尖端混合参数对场解的构造以及应力，应变分布的影响，为给出合理的断裂准则提供理论依据。     

Higher order fields for damaged nonlinear antiplane shear notch, crack and inclusion problems

Damaged nonlinear antiplane shear problems with a variety of singularities are studied analytically. A deformation plasticity theory coupled with damage is employed in analysis. The effect of microscopic damage is considered in terms of continuum damage mechanics approach. An exact solution for the general damaged nonlinear singular antiplane shear problem is derived in the stress plane by means of a hodograph transformation, then corresponding higher order asymptotic solutions are obtained by reversing the stress plane solution to the physical plane. As example, traction free sharp notch and crack, rigid sharp wedge and flat inclusion, and mixed boundary sharp notch problems are investigated, respectively. Consequently, higher order fields are obtained, in which analytical expressions of the dominant and second order singularity exponents and angular distribution functions of the near tip fields are derived. Effects of the damage and hardening exponents of materials and the geometric angle of notch/wedge on the near tip quantities are discussed in detail. It is found that damage leads to a weaker dominant singularity of stress, but to little stronger singularities of the dominant and second order terms of strain compared to that for undamaged material. It is also seen that damage has important effect on the angular distribution functions of the near tip stress and strain fields. As special cases, higher order analytical solutions of the crack and rigid flat inclusion tip fields are obtained, respectively, by reducing the notch/wedge tip solutions. Effects of damage and hardening exponents on the dominant and second order terms in the solutions of the crack and inclusion tip fields are discussed.     

组件裂尖变形场的云纹显微倍增研究

将云纹干涉法与显微、倍增技术相结合，发展了一种位移场云纹条纹显微倍增方法．对该方法进行了严格的理论推导和精确的实验验证，并用该方法对热载下微电子模拟组件的层间裂纹尖端位移场和奇异性进行了实验研究     

Experimental investigation of GH singularity field of the growing crack-tip for different ductile metals

The displacementsu _x ,u _y inx, y directions at growing crack tip of the specimens with double edge cracks for four different alumium alloys and two coppers are measured by using moire method and optical spatial filtering technique. From experimental displacement fields, the displacement singularity fields are obtained and compared with GH theoretical field. Unknown constantsA and _yo in theoretical solution are determined from experimental data. The theoretical singularity field thus compared is given for plane-stress, mode-I, strain-hardening materials. The error in both the experimental and theoretical evaluations is within ± 10%. The experiments show that there exists dominant singularity region around a growing crack-tip. In the experiments, the strain hardening indexn amounts from 3.158 to 14. The shape of this dominant region ranges from butterfly wing to oblate or circular shape. The size and shape of GH dominant region depend on the material property, the specimen geometry and loading type. Inside GH-field, there is a 3-D deformed damage zone, where no GH singularity exists. Very near to the crack-tip, there is a fracture process zone.The project is supported by the National Science Foundation of China.     

垂直界面裂纹断裂力学问题的实验研究

用实验方法研究了具有垂直界面方向裂纹的界面断裂力学问题．根据实验结果对裂尖区域的奇异性性质、角位移分布、应力强度因子等进行了分析，并将实验结果与理论结果进行了比较和讨论     

倍增云纹的显微测量及密集云纹场的应变测算

为了提高云纹法的准确度,文中提出了使倍增后的云纹宽度变细并进行显微测量的技术,以及由密集云纹场测算应变的条纹间距插值和小间距均匀法。给出了估计由此法算得的应变的误差及其修正方法。所做的曲杆实验其数据与理论值符合得很好。文中还将云纹法中闪耀光栅与振幅栅相匹配的光学空间滤波系统改进为实时系统,导出其条纹倍增率及云纹图的最佳对比度条件。     

韧性金属裂纹尖端损伤区内应变场测量——数字散斑相关法应用

本文用数字散斑相关方法测量了五种不同幂硬化指数韧性金属材料(铝和铜),双边裂纹尖端细观区域内应变场.对所得结果用韧性损伤模型进行了分析.在此法中以金属自然表面结构为散斑场,不同加载状态的散斑场进行比较,得到相对变形与应变.图象之间相关性 C 是变形参数或是位移及其导数的泛函.使其相关性 C 取最大值的试凑变形即为其真实变形场.这一方法在细观测量中应用得到满意的结果.     

Experimental GH singularity field around growing crack-tip

The displacement fieldsu _x ,u _y at growing crack tip of LY12-M specimens with double edge cracks are measured using moire method. The experimental singularity fields are compared with GH theoretical field [12–14]. The size and shape of the experimental GH singularity fields are obtained. The error in both the experimental and theoretical evaluations is controlled within ±10%. The experiments show that there is singularity dominant around a growing crack tip. The shape of this dominant region ranges from butterfly wing to oblate and circular. Inside GH-field, there is a 3-D deformed damage zone where no GH singularity exists. The project suppoted by National Natural Science Foundation of China     

Crack tip singular fields in ductile crystals with taylor power-law hardening. I: Anti-plane shear

Asymptotic singular solutions of the HRR type are presented for anti-plane shear cracks in ductile crystals. These are assumed to undergo Taylor hardening with a power-law relation between stress and strain at sufficiently large strain. Results are given for several crack orientations in fcc and bcc crystals. The neartip region divides into angular sectors which are the maps of successive flat segments and vertices on the yield locus. Analysis is simplified by use of new general integrals of crack tip singular fields of the HRR type. It is conjectured that the single crystal HRR fields are dominant only over part of the plastic region immediately adjacent to the crack tip, even at small scale yielding, and that their domain of validity vanishes as the perfectly plastic limit is approached. This follows from the fact that while in the perfectly plastic limit the HRR stress states approach the correct discontinuous distributions of the complete elasticideally plastic solutions for crystals (Rice and Nikolic, J. Mech. Phys. Solids33, 595 (1985)), the HRR displacement fields in that limit remain continuous. Instead, the complete elastic-ideally plastic solutions have discontinuous displacements along planar plastic regions emanating from the tip in otherwise elastically stressed material. The approach of the HRR stress fields to their discontinuous limiting distributions is illustrated in graphical plots of results. A case examined here of a fcc crystal with a crack along a slip plane is shown to lead to a discontinuous near-tip stress state even in the hardening regime.Through another limiting process, the asymptotic solution for the near-tip field for an isotropic material is also derived from the present single crystal framework.     

Conservation integrals and determination of HRR singularity fields

The angular distribution functions of HRR singularity fields are analyzed via conservation integrals. Two functional equations are proved for the angular distribution functions and can be used for their solutions. The detailed forms of the functional equations and the final governing equations for solutions are given for the cases of plane strain and plane stress. Accurate numerical results are also given for some typical parameters and the equivalence of different governing equations is proved.