Ⅰ型裂缝经弱界面钝化扩展实验研究

天然裂缝或层理等弱界面的剪切破坏是体积压裂裂缝网络形成的关键因素。利用数字散斑相关技术,通过三点弯曲构建了Ⅰ型裂缝经过弱界面时的扩展特性实验,获得了试件表面位移场和应变场的变化规律。实验结果表明:Ⅰ型裂缝扩展至弱界面层后,裂缝发生短暂停滞扩展,裂缝尖端张开位移迅速增加,Ⅰ型裂缝尖端钝化,弱界面剪切应变迅速增加,裂缝由Ⅰ型裂缝转变为Ⅰ--Ⅱ复合型裂缝并转向扩展。     

EXPERIMENT STUDY OF I TYPE CRACK BLUNT EXTENSION INDUCED BY WEAK PLANE1)

天然裂缝或层理等弱界面的剪切破坏是体积压裂裂缝网络形成的关键因素。利用数字散斑相关技术,通过三点弯曲构建了I型裂缝经过弱界面时的扩展特性实验,获得了试件表面位移场和应变场的变化规律。实验结果表明：I型裂缝扩展至弱界面层后,裂缝发生短暂停滞扩展,裂缝尖端张开位移迅速增加,I型裂缝尖端钝化,弱界面剪切应变迅速增加,裂缝由I型裂缝转变为I-II复合型裂缝并转向扩展。     

金瓷双材料力学行为的现代光力学实验研究

金瓷修复体兼具金属强度及陶瓷美观的优点,在口腔医学上得到了广泛应用,但临床上时有发生脱瓷并且又多发生在界面处,针对这种情况,通过研究不同层厚比的金瓷修复体试件梁的界面力学行为,以分析其破坏机理。采用云纹干涉法和电子散斑法对界面具有缺陷形式的试件进行了实验研究。得到裂纹尖端及界面处的位移场,计算了界面断裂强度等参量,并给出了试件制备、实验方法。实验结果表明不同层厚比的试件以及不同界面缺陷形式的试件对抵抗破坏能力均有不同影响;现代光力学实验方法对研究具有小变形的双材料结构力学行为可行、有效。     

电子散斑干涉法在研究双材料界面力学行为中的应用

对于复合材料，界面往往是重要的组成部分，也是缺陷极易发生甚至断裂破坏的地方，从而影响材料整体的力学行为。为了考察不同界面缺陷形式以及材料层厚对界面力学行为的影响，应用电子散斑干涉法对金属基上烤瓷的双材料试件进行了实验研究，部分试件与云纹干涉法结果也进行了比较。实验结果表明具有垂直界面裂纹的试件梁抵抗破坏能力大大削弱，而界面处无缺陷的力学性能较好，其中又以金属层与烤瓷层厚比在3附近的较为理想，实验也表明电子散斑干涉法适用于测量绝对或相对微小的位移，灵敏度达到微米级。     

散斑图像相关数字技术原理及应用

研究图像处理技术在散斑测量中的应用，提出了一种散斑图像相关数字技术，该方法引进了亚像素技术，采用重心算法计算特征斑的重心，避免了数字散斑相关法计算相关系数的繁复过程；应用位移和应变的有关公式，可以获得物体变形实验曲线，实验结果表明，该方法在工程实际现场、振动过程以及变形测量的自动化等方面有着广泛的应用潜力，从而为光测力学拓展应用领域、实现自动化测量展现了新的前景。     

双金属层状板中软界面层对裂纹扩展的影响

采用带软界面层的双金属层状板，分析了裂纹垂直于界面扩展过程中的力学行为。带单边裂纹的钢／铝层板的弯曲疲劳实验表明，裂尖接近软铝界面层时裂纹扩展速率da／dN变化很大；裂纹扩展到达界面层时发生偏折。利用有限元软件分析了裂纹尖端前沿应力和应变的变化规律，计算结果表明：软铝界面层出现较大塑性应变，增加了裂纹扩展阻力，并使裂纹扩展力△K减小，导致了da／dN降低．而软界面层中的T应力增高，造成裂纹偏折现象。     

钢纤混凝土裂纹尖端应变场的实验研究

本文应用散斑干涉技术在四组含纤量分别为０，０．５％，１％，１．５％的钢纤混凝土三点弯曲裂纹试件的裂纹尖端位移场进行了测试，并换算为应变场。对钢纤混凝土开裂的基理进行了探讨；验证了最大位应变准则；并测定断裂韧度Ｊｉｃ．     

应用超声散斑相关法测量水下物内层界面位移

超声散斑相关法可应用于水下物体内层界面的位移测量,在工程建设中具有广泛的应用前景。根据所建立的测量实验系统,对位于水中的有机玻璃试件内层界面的面内位移和离面位移进行了实测,测量误差一般在7%以内。进一步研究结果表明:在刚体位移情况下,一般经粗磨、粗刨和粗铣加工或砂模铸造后的粗糙外层界面对超声散斑相关法内层界面位移测量结果的影响极小;当外层界面发生应变时,其变形前后内层界面上的散斑场的相关性将随应变量的增加而减弱,但外层界面应变小于0.05ε时,内层界面上超声散斑相关系数的减小不超过4%。     

复合材料层合板固化过程的数值模拟

在文［１］中作者采用了有限元和有限差分相结合的交替迭代法及Ｅｕｌｅｒ－Ｃａｕｃｈ解偶算法分析了复合材料层合板固化全过程中板内温度场和固化度场。在此基础上，本文进一步根据层合板在固化过程中不同阶段材料物性变化及损伤破坏特征，提出了两种不同破坏准则和后破坏模型，并采用非线性瞬态热弹性问题的Ｈａｍｉｌｔｏｎ半解析法，研究了层合板在固化全过程中的损伤破坏和热应力、变形的变化规律。通过数值模拟和分析，发现层合板在固化过程中，板内热应力出现多峰值和变号特征，这将是导致层合板早期破坏的原因，本文工作将对材料工艺工作者选择固化工艺参数具有参考价值。     

层合板六参量几何非线性高阶剪切理论

提出了层合板六参量的高阶剪切变形理论的位移场假定,以考虑在大变形条件下层合板法向变形和厚度的变化。同时对ｖｏｎ Ｋａｒｍａｎ应变位移简化假设进行补充修改,考虑某些有限变形条件下被忽略小量的影响,建立了对应于该文六参量模型和更加适凳大变形分析的层合板几何非线性关系,平衡方程和边界条件。利用该文模型分析了橡胶复合材料简支板的大变形弯曲行为,并对比Ｒｅｄｄｙ五参量几何非线性简单高阶剪切变形层合理论解和弹     

反倾层状岩体斜坡弯曲-拉裂两种失稳破坏之判据探讨

对反倾层状岩体斜坡弯曲-拉裂的失稳破坏判据,已有研究分别基于两种力学模型进行推导,即竖直压杆弹性屈曲稳定和平直梁弯折破坏模型,但对层间错动阻力及挠度产生附加弯矩等因素未加以考虑,不尽合理。在反倾斜坡岩层受力分析基础上,建立考虑了板侧层间错动阻力的下端嵌固、上端自由的斜置等厚弹性悬臂板梁模型,统一地通过瑞利-里兹能量方法,推导了弹性屈曲临界条件和嵌固端弯折破坏临界条件。实例计算及讨论表明,弹性屈曲判据适用于陡立岩层;而中-陡反倾岩层应主要为弯折破坏,但层间的力学性质对弯折临界判据值具有较大影响。     

缝合复合材料层间开裂的试验和数值研究

缝合复合材料层合板中贯穿厚度方向的缝线,能有效增强层合板的抗分层能力。本文对一种碳纤/环氧缝合复合材料层板进行了短梁三点弯试验,测得了压头的载荷-位移曲线,并观察了层间裂纹的扩展,证实了缝线对层间裂纹的阻滞作用。建立了三维有限元模型模拟了上述试验,模型中相邻的铺层之间布置了一层初始无厚度的界面单元,界面单元的失效自然模拟层间开裂,而缝线简化为面积等效的梁单元,数值结果与试验观测吻合。     

重组竹顺纹冲击力学性能研究

重组竹是一种新型竹基复合材料,其力学性能优于落叶松等木材。为评价重组竹在动态加载下的顺纹抗冲击力学性能,以密度1.06 g/cm3、含水率8.52%、龄期3～5年的毛竹基重组竹为研究对象,通过准静态单轴压缩和循环加卸载以及动态加载实验,研究了重组竹加载变形过程、各项力学性能指标以及对应变率的敏感性。结果表明:重组竹顺纹压缩过程可以分为弹性变形和弹塑性变形阶段,破坏类型为延性破坏,其各项强度指标随应变率的提高而提高,动态增长因子与应变率之间呈现线性关系,斜率为0.0024;重组竹压缩过程中的应变比能与应变之间呈线性关系,且随应变率的增长而增大,证明其吸能能力随着应变率的增大而提高。实验结果证明,重组竹顺纹具有良好的抗冲击力学性能和显著的应变率效应。     

Failure in the junction region of T-stiffeners: 3D-braided vs. 2D tape laminate stiffeners

Strain distributions and failure mechanisms are compared for a three-dimensionally (3D) braided T-stiffener (preform designed and supplied by 3TEX Inc.) and a conventional two-dimensional (2D) tape laminate T-stiffener, bonded onto a tape laminate skin. The strain distributions in a pull-off test are measured by laser speckle interferometry and calculated by computational simulations. With good agreement between experiment and theory, substantial differences are found between the two classes of stiffener. The tape laminate stiffeners exhibit large strain concentrations across the noodle region and in the adjacent radii, which correlate well with observed first cracking events. The 3D-braided stiffeners show relatively uniform strain distributions throughout the flanges, the web, and the flange/web junction region. Strain concentrations are modest at the corner of the junction and absent along the interface between the flanges and the skin. Failure in the 3D-braided stiffeners does not occur within the junction region, but by a sequence of cracking events, first next to the junction region and then at the end of one flange. The pull-off load at the first failure event is substantially higher for the 3D-braided stiffener than the tape laminate stiffener, which is attributed mainly to the relative absence of strain concentrations in the former.In predicting strain distributions, account is taken of the details of the 3D architecture of the 3D-braided stiffeners as specified by the supplier (3TEX Inc.) by using the Binary Model of textile composites, whose formulation has been described previously. Comparison of the predicted and measured spatial distributions of strain constitutes a critical test of the Binary Model. It is found to perform well in this case.     

Control of mechanical deformation of a laminate by piezoelectric actuator taking into account the transverse shear

Summary The control of dynamic deformation of a laminate plate is conducted by applying electrical load to a piezoelectric actuator integrated into the laminate. The dynamic behavior of the laminate is analyzed in the paper taking into account the effect of transverse shear. The analytical model of the laminate is composed of fiber-reinforced laminae and piezoelectric layers constituting a symmetric cross-ply laminate rectangular plate with simply-supported egdes. It is subjected to mechanical and electrical loads acting on the piezoelectric actuator in order to compensate the effect of the mechanical loads. The behavior of the laminate is analyzed based on the first-order shear deformation theory. Closed-form solutions are obtained for the following quantities: (1) natural frequencies of the laminate plate, (2) weight functions for the deflections and rotations and (3) transient deflections due to loads varying arbitrarily with time. Illustrative examples are shown for the control of deflections caused by the mechanical loads by means of electrical voltage applied to the piezoelectric actuators.     

Multi-scale Mechanical Characterization of Palmetto Wood using Digital Image Correlation to Develop a Template for Biologically-Inspired Polymer Composites

Palmetto wood is garnering growing interest as a template for creating biologically-inspired polymer composites due to its historical use as an energy absorbing material in protective structures. In this study, quasi-static three-point bend tests have been performed to characterize the mechanical behavior of Palmetto wood. Full-field deformation measurements are obtained using Digital Image Correlation (DIC) to elucidate on the strain fields associated with the mechanical response. By analyzing strain fields at multiple length scales, it is possible to study the more homogeneous mechanical behavior at the macro-scale associated with the global load-deformation response; while at the microscale the mechanical behavior is more inhomogeneous due to microstructural failure mechanisms. Thus, it was possible to determine that, despite the presence of discontinuous macro-fiber reinforcement, at the macro-scale the response is associated with classical bending and progressive failure processes that are adequately described by Weibull statistics proceeding from the tensile side of the specimen. At the microscale, however, the failure mechanisms giving rise to the macroscopic response consist of both shear-dominated debonding between the fiber and matrix, and inter-fiber matrix failure due to pore collapse. These microscale mechanisms are present in both the compressive and tensile regions of the specimen, most likely due to local macro-fiber bending, which is independent of the global bending state. The pore collapse mechanism observed during mechanical loading appears to improve the energy absorption of the matrix material, thereby, transferring less energy and shear strain to the macro-fiber-matrix interface for initiation of debonding. However, the pore collapse mechanism can also accumulate substantial shear strain, which results in matrix shear cracking. Through these complex failure mechanisms, Palmetto wood exhibits a high resistance to catastrophic failure after damage initiation, an observation that can be used as inspiration for creating new polymer composite materials.     

MESO-MECHANICAL ANALYSIS OF SHAPE MEMORY ALLOY REINFORCED SMART STRUCTURE WITH DAMAGE

The mechanical behaviors of shape memory alloy (SMA) wires reinforced smart structure with damage were analyzed through the variational principle, a governing equation for the structure was derived, mathematical expressions for the meso-displacement field, stress-strain field of typical element with damage were presented, and a failure criterion for interface failure between SMA wires and matrix was established under two kinds of actuation which are dead-load and temperature, where the temperature is included in effective free restoring strain. In addition, there are some other composing factors in the failure criterion such as the interface properties, dynamical properties of SMA, initial debonding length L-l etc. The results are significant to understand structural strength self-adapted control and failure mechanism of SMA wires reinforced smart structure with damage.     

固体发动机保险机构在高温高压下的实验研究

针对固体发动机部件保险机构所出现破现象,对其进行了激光散斑和电阻应变法联合测试。由于保险机构在高温和高压环境下工作,材料有蠕变现象,出现较大的热变形,传统的光我法实施,发展了一种叠合散斑技术,使之能够对大变形进行非接触式测量,在实验室测试的基础上,对保险机构进行了热容器试验,测量了点火后应变随时间的变化规律。实验结构发现,在保险机构机体上存在着一个接近破环应力的高危应力区,这是保险机破坏的主要因素     

Quasi-static tensile deformation and fracture behavior of a highly particle-filled composite using digital image correlation method

Polymer bonded explosives (PBXs) are highly particle-filled composite materials. This paper experimentally studies the tensile deformation and fracture behavior of a PBX simulation by using the semi-circular bending (SCB) test. The deformation and fracture process of a pre-notched SCB sample with a random speckle pattern is recorded by a charge coupled device camera. The displacement and strain fields on the observed surface during the loading process are obtained by using the digital image correlation method. The crack opening displacement is calculated from the displacement fields, the initiation and propagation of the crack are analyzed. In addition, the damage evolution and fracture mechanisms of the SCB sample are analyzed according to the strain fields and the correlation coefficient fields at different loading steps.