纤维—基体界面脱粘能量释放率

研究一个纤维拔出界面脱粘断裂能量释放率分析的简单模型,给出纤维－基体界面断裂能ＧⅡ工程计算公式的推导过程,用有限元法检查了该公式的可靠性与适用范围,并提出一个修正表达式。     

SiC纤维增强复合材料基体裂纹偏移机理的有限元分析

运用基于能量的裂纹偏移准则, 分别建立了两相和三相复合材料基体裂纹偏移/ 穿透的轴对称有限元模型, 考察了纤维体积分数、描述材料特性弹性失配的Dundurs 参数α和相对裂纹扩展长度a_d / a_p 对相对能量释放率Gd / Gp 的影响。将两相复合材料的有限元结果与He 等人的结果进行对比, 进一步考察了三相复合材料界面层厚度和Dundurs 参数α₁ 和α₂ 对G_d / G_p 的影响。分别将碳涂层SiC 纤维增强复合材料SiC/ C/ Ti-6A1-4V 和碳涂层陶瓷基增强复合材料SiC/ C/ SiC 运用于有限元分析中, 结果表明, 所建立的模型能够准确地预测和比较基体裂纹偏移的机理。      

纤维─基体界面脱粘能量释放率

研究一个纤维拔出界面脱粘断裂能量释放率分析的简单模型，给出纤维－基体界面断裂能ＧⅡ工程计算公式的推导过程．用有限元法检查了该公式的可靠性与适用范围．并提出一个修正表达式     

纤维—基体脱粘的界面应力分析

本文建立了单纤维拔出时考虑纤维与基体间径向压应力及界面剪应力的简单模型，分析了纤维的轴向脱粘应力与界面剪应力纤维包埋长度的分布规律。     

单纤维拔出方法表征CFRP界面强度的研究

提出了单根碳纤维从环氧树脂基体中拔出的一种简易方法，在国内首次实现了用该方法表征碳纤维增强树脂基复合材料（ＣＦＲＰ）界面粘合性能的技术。     

复合材料层合板三维分层问题的断裂力学分析

对复合材料层板中椭圆分层的断裂力学问题进行了研究。根据层板平面剪切型分层和反平面剪切型分层尖端附近位移场、应力场与应力强度因子的关系,利用法向切片法,得到椭圆分层前缘应力强度因子与能量释放率的关系。结合由附加位移所确定的总位能,确定了能量释放率和应力强度因子沿分层前缘分布的表达形式。数值计算给出了二者随分层区形状、载荷以及各层厚度比等参数变化的分布情况。     

含面芯开裂损伤复合材料夹层板考虑几何非线性的能量释放率数值分析

基于一阶剪切变形理论,zig-zag变形假定和von Karman大挠度理论,提出了含不同形状面芯开裂损伤复合材料夹层板在受压缩载荷作用下的开裂前缘能量释放率研究的有限元分析方法,研究了在轴向应变作用下,具有面芯开裂损伤复合材料夹层板的分层断裂力学行为,并讨论了在大变形下几何非线性对能量释放率分布规律的影响。通过典型算例分析表明:具有面芯开裂损伤复合材料夹层板的分层前缘能量释放率的大小和分布规律与开裂面积、开裂形状和受载方向有关。     

纤维增强复合材料界面疲劳裂纹扩展的模拟研究

脱粘是纤维增强复合材料界面裂纹扩展的主要表现形式.基于剪切筒模型和常用的实验加载方式,研究了纤维增强复合材料中纤维与基体界面在拉-拉循环荷载作用下的裂纹扩展.借助描述疲劳裂纹扩展的Paris公式,得到了疲劳裂纹扩展速率、扩展长度以及界面上摩擦系数与加载次数的关系.在分析中,考虑了疲劳加载引起的脱粘界面的损伤及损伤分布的不均匀性,同时还考虑了材料的泊松效应.     

黄麻纤维束力学性能的尺寸和应变率效应

为了探究黄麻纤维束的尺寸效应和应变率敏感性,利用C43电子式万能试验机和CEAST 9340落锤试验冲击系统分别在静动载条件下对黄麻纤维束进行测试,获得了杨氏模量、强度、峰值应变和韧性随标距和应变率的变化关系静载试验在1/600s-1应变率条件下进行,测试了6组不同标距(25、50、100、150、200和300mm)的试件;动载试验以应变率为变量,在4组不同的应变率(40、80、120和160s-1)条件下进行了测试,试件标距均为25mm。测试结果表明:随着试件标距增大,杨氏模量初始增大,当标距大于100mm时趋于稳定;强度、峰值应变和韧性均减小。随着应变率增大,杨氏模量和强度均增大;峰值应变初始减小后趋于稳定;韧性先减小后增大。鉴于植物纤维束材料较大的性能离散性,采用Weibull分布对试验数据进行拟合,获得了黄麻纤维束强度在不同试验条件(标距和应变率)下的分布规律。     

Arbitrarily oriented microcracks near the tip of an interface macrocrack in bonded dissimilar anisotropic materials

It is well known that microcracking in brittle materials results in a reduction of the stress intensity factor (SIF) and energy release rate (ERR). The reduced SIF or ERR represents crack tip shielding which is of significant interest to micromechanics and material science researchers. However, the effect of microcracking on the SIF and ERR is a complicated subject even for isotropic homogeneous materials, and becomes much more formidable in case of interface cracks in bonded dissimilar solids. To unravel the micromechanics of interface crack tip shielding in bonded dissimilar anisotropic solids, an interface crack interacting with arbitrarily oriented subinterface microcracks in bonded dissimilar anisotropic materials is studied. After deducing the fundamental solutions for a subinterface crack under concentrated normal and tangential tractions, the present interaction problem is reduced to a system of integral equations which is then solved numerically. A J‐integral analysis is then performed with special attention focused on the J₂‐integral in a local coordinate system attached to the microcracks. Theoretical and numerical results reassert the conservation law of the J‐integral derived for isotropic materials 1 , 2 also to be valid for bonded dissimilar anisotropic materials. It is further concluded that there is a wastage when the remote J‐integral transmits across the microcracking zone from infinity to the interface macrocrack tip. In order to highlight the influence of microstructure on the interfacial crack tip stress field, the crack tip SIF and ERR in several typical cases are presented. It is interesting to note that the Mode I SIF at the interface crack tip is quite different from the ERR in bonded dissimilar anisotropic materials.     

金属陶瓷功能梯度材料的颗粒界面断裂能量释放率的研究

研究了功能梯度材料富陶瓷区金属颗粒界面断裂能量释放率。采用双层嵌套模型给出了金属颗粒界面的热应力与金属体积浓度的关系,对于得到的第五梯度层中的颗粒界面热应力,分析了颗粒界面断裂的释放率,并研究了每一梯镀层中金属颗粒的临界尺寸变化规律。     

A sandwich three-point bend specimen for testing mode-I interlaminar fracture toughness for fiber-reinforced composite materials

A sandwich three-point bend specimen has recently been proposed to test mode-I interlaminar fracture toughness for fiber-reinforced composite materials. The test composite consist of a thin layer bonded by two lateral reusable steel bars (Sohn et al. 1995). Some time earlier this specimen configuration was used to test fracture toughness of adhesives (Zdaniewsk et al. 1987). However, formulae for analysing its fracture mechanics parameters such as stress intensity factor and energy release rate can not be found in the literature. The lack of adequate formulae may explain why suitable quantitative analysis using this specimen configuration has not been achieved. In this paper, a simple and effective homogenisation method is used to change the bi-material system, which represents the specimen, into single uniform test material. This physical homogenisation is carried out by geometric change of the cross section of lateral steel parts based on equal deflection rigidity. For the transformed specimen configuration of single uniform material, the corresponding stress intensity factor solution from handbooks is available. Two formulae of stress intensity factor for the sandwich three-point bend specimen are given as upper limit and lower limit respectively, they are plotted with varying elastic tensile modulus mismatch. Then the relation between stress intensity factor and energy release rate, with special consideration of orthotropy of the tested composite material, is used to derive its energy release rate. The specimen and its formulae can also be applied to test other materials such as wood, welded joints (Burstow and Ainsworth, 1995), as well as to test dynamic fracture toughness. This revised version was published online in July 2006 with corrections to the Cover Date.     

Asymmetrical Cracks Parallel to an Interface between Dissimilar Materials

This paper solves a plane strain problem for two bonded dissimilar planes containing a crack parallel to the interface in each layer. The bimaterial system is loaded by tractions distributed along the crack surfaces. Based on the Fourier transform, the problem is reduced to a system of Cauchy type singular integral equations which contain exact and explicit kernel functions. The solution of these equations is obtained easily by utilizing Gauss–Chebyshev integral formulae for various material combinations and geometrical parameters. Several numerical results of stress intensity factors, energy release rate and stress distribution along the interface are presented to exhibit the interaction among cracks and interface. This revised version was published online in July 2006 with corrections to the Cover Date.     

纯弯曲Sandwich梁试样界面裂纹扩展的应变能释放率

纯弯曲的Sandwich 梁试样在评价界面断裂抗力方面有重要作用。利用能量的叠加原理和截面转换方法, 本文导出了纯弯曲Sandw ich 梁试样界面裂纹扩展应变能释放率的显式解, 并根据实验测得的界面裂纹扩展的临界载荷, 用其计算出了四点弯曲Si₃N₄/Al/Si₃N 4试样Si₃N₄/Al 扩散连接界面的断裂韧度。      

Non-Axisymmetric Matrix Cracking and Interface Debonding with Friction in Ceramic Composites

A three-dimensional analytical model based on the principle of minimum potential energy is developed and applied to determine the stress state in a discrete fiber/matrix composite cylinder subjected to axial tensile loading in the fiber direction and containing a non-axisymmetric transverse matrix crack and an interface debond. The friction over the debonded interface is incorporated into the analysis. The strain energy release rates associated with the matrix crack and the interface debonding under the combination of the applied load and the interface frictional force are computed. The strain energy release rate criterion has been employed to evaluate the critical applied loads for the two fracture modes and to assess the competition between propagation of a matrix crack and growth of interface debonding. A parametric study has been carried out. The computed results show that the interface friction plays an important role in the failure of brittle matrix composites.     

Kinking of an interface crack in an orthotropic bimaterial

We investigated the asymptotic problem of a kinked interface crack in an orthotropic bimaterial under in‐plane loading conditions. The stress intensity factors at the tip of the kinked interface crack are described in terms of the stress intensity factors of the interface crack prior to the kink combined with a dimensionless matrix function. Using a modified Stroh formalism and an orthotropy rescaling technique, the matrix function was obtained from the solutions of the corresponding problem in transformed bimaterial. The effects of orthotropic and bimaterial parameters on the matrix function were examined. A reduction in the number of dependent material parameters on the matrix function was made using the modified Stroh formalism. Moreover, the explicit dependence of one orthotropic parameter on the matrix function was determined using an orthotropic rescaling technique. The effects of the other material parameters on the matrix function were numerically examined. The energy release rate was obtained for a kinked interface crack in an orthotropic bimaterial.