通电瞬时板内半无限长裂纹尖端域的应力场

以导电弹性体的麦克斯威尔方程为出发点,借助于边界条件和初始条件,推得了在向含半无限长直线裂纹的无限大导电薄板内通入电流的瞬时,裂纹尖端附近电流密度的表达式。在此基础上,得到了裂纹尖端区域处温度和应力的具体表达式。算例表明,在电流所产生的焦耳热源的作用下,裂尖区域处的温度将瞬时升高,并伴有压应力的产生,从而可达到阻止裂纹扩展的目的。     

载流金属材料裂纹尖端电磁应力的数值模拟

用数值模拟方法研究了金属裂纹尖端电磁应力的分布情况,给出了电流分布、磁场分布和电磁应力的分布.模拟结果表明,金属材料裂纹尖端受的电磁应力是最大的,并且这个力的大小随着电流密度的增加而增大,裂纹尖端的电磁力指向金属的内部.通过具体算例表明,在金属能承受的电流密度下,金属材料裂纹尖端的电磁应力约能达到1MPa的数量级.因此,在研究电磁场处理金属裂纹时,不能忽略电磁应力.     

载流薄板中裂纹形成瞬间尖端附近的热电磁场

给出了载流无限大薄板在形成裂纹的瞬间,尖端区域附近的电流密度以及由于集中效应而产生的焦耳热源功率表达式。在此基础上,通过对热传导方程求解温度场,得到了裂纹尖端区域的温度表达式．通过算例分析证实了：在电磁场作用瞬间,由于裂尖处的热集中效应,能够使其在附近一定范围内熔化形成微小焊口．从而可达到阻止裂纹扩展的目的。     

混凝土脆性断裂电磁发射理论研究

通过研究混凝土断裂时的电磁发射现象,提出了由于混凝土裂纹尖端电荷随着裂纹的加速扩展运动而产生电磁辐射的解释。应用断裂力学理论建立了混凝土断裂时裂纹扩展加速度与初始裂纹长度之间的关系;根据实验结果,利用电磁学理论,分析了裂纹尖端电荷的加速运动所激发的电磁场强度及其频谱特性。     

压电-压磁板条中反平面裂纹的电-磁-弹性分析

基于线性电磁弹性理论,获得了压电-压磁板条中反平面裂纹尖端附近的奇异应力、电场和磁场。假设裂纹位于和板条边界平行的中心位置,并且裂纹是电磁渗透型的。利用Fourier变换,将裂纹面的混合边值问题化为对偶积分方程,即而归结为第二类Fredholm积分方程。通过渐近分析,得到了裂纹尖端附近应力、应变、电位移、电场、磁场和磁感的封闭表达式。结果表明,对于电磁渗透裂纹,电场强度因子和磁场强度因子总为0;板条的宽度对应力强度因子有显著的影响;能量释放率总为正值。     

阶跃递增电流作用下导电薄板中的裂纹止裂效应

研究了在带有有限长裂纹的无限大导电薄板中，垂直裂纹通入阶跃递增电流的情况下，裂纹尖端处的电磁场和温度场．给出了裂纹尖端温度的计算方法和算例．指出适当调整阶跃电流的变化值和阶跃次数，可使裂纹尖端处熔化形成焊点，从而遏制了裂纹的扩展．     

裂纹面荷载作用下多裂纹应力强度因子计算

该文基于比例边界有限元法计算了裂纹面荷载作用下平面多裂纹应力强度因子.比例边界有限元法可以给出裂纹尖端位移场和应力场的解析表达式,该特点可以使应力强度因子根据定义直接计算,同时不需要对裂纹尖端进行特殊处理.联合子结构技术可以计算多裂纹问题的应力强度因子.数值算例表明该文方法是有效且高精确的,进而推广了比例边界有限元法的...     

轴对称金属模具电磁热裂纹止裂温度场的分析

选择带有半埋藏环形裂纹的金属凹模为研究对象,通过金属凹模内外环面均匀通入强脉冲电流,应用电磁热效应实现了金属凹模中环形裂纹的止裂。采用复变函数的方法求解了脉冲电流放电瞬间裂纹尖端附近的温度场。由于脉冲电流放电瞬间,裂尖处电流绕流的热集中效应,在金属凹模内部,环形裂纹尖端金属的温升超过熔点,金属熔化,在金属凹模内部沿着环形裂纹尖端形成堆焊,致使环形裂纹尖端的曲率半径瞬间增大,阻止了干线裂纹源的开裂趋势。     

裂纹稳态扩展下正交异性材料的动应力强度因子KⅢ解答

研究了无限大正交异性材料中半无限长Ⅲ型裂纹的动态扩展问题.裂纹尖端附近的应力和位移被表达为解析复函数的形式,而复函数可以表达为幂级数的形式,幂级数的系数由研究问题的边界条件来确定.这样就给出了裂纹尖端附近的应力分量和位移分量的简单近似表达式,由推导出的动应力分量和动位移分量可以退化为其在各向同性材料静态断裂问题中的情况.最后,裂纹扩展特性由裂纹几何参数和裂纹扩展速度来反映出来,相同的几何参数情况下,裂纹扩展愈快,裂纹尖端附近的最大应力分量和最大位移分量愈大.     

沿直线有多条裂纹的薄板弯曲问题

本文首先用复变函数的虚部构成了一平面上沿y轴有矩形开口的位移函数,并用加权积分法将裂纹尖端交换为光滑接触的形状：然后由此函数构成的重调和函数,导出了沿不同弹性介质界面(y轴)有多条裂纹的薄板弯曲问题的应力函数。用加权积分法将裂纹尖端无穷大的应力集中有限化,并不意味着消除了复变函数中的奇异点。文中图示了将应力奇点移至其他分支,而在XY全平面应力呈有限连续的情形。本分析方法的成功之处在于在裂纹尖端附近构成了一开口位移和截面内力相并存的过渡区,同时消除了过去研究中呈现的界面裂纹尖端附近无穷大应力的剧烈振荡现象。     

含圆形埋藏裂纹金属构件电磁热止裂时应变能密度分析

对带有圆形埋藏裂纹金属构件在脉冲放电瞬间的应变能密度进行了理论分析。在求解过程中,以张开型裂纹为例,应用了热传导、非定常热应力及汉克尔变换等理论知识,得出了含埋藏圆片裂纹在脉冲放电瞬间的温度场理论公式、热应力场公式和应变能密度公式。由热应力场公式和应变能密度公式可知,放电瞬间电磁热在裂纹尖端形成热压应力场,热压应力对金属构件做负功,减小了拉应力对构件的破坏程度,放电后构件的应变能密度降低了。以Cr12MoV模具钢中埋藏圆裂纹止裂为例,具体计算了脉冲放电前后不同拉应力作用下的应变能密度变化情况,为空间裂纹电磁热止裂技术的实际应用提供了理论基础。     

Crack closure in fibre metal laminates

GLARE is a fibre metal laminate (FML) built up of alternating layers of S2-glass/FM94 prepreg and aluminium 2024-T3. The excellent fatigue behaviour of GLARE can be described with a recently published analytical prediction model. This model is based on linear elastic fracture mechanics and the assumption that a similar stress state in the aluminium layers of GLARE and monolithic aluminium result in the same crack growth behaviour. It therefore describes the crack growth with an effective stress intensity factor (SIF) range at the crack tip in the aluminium layers, including the effect of internal residual stress as result of curing and the stiffness differences between the individual layers. In that model, an empirical relation is used to calculate the effective SIF range, which had been determined without sufficiently investigating the effect of crack closure. This paper presents the research performed on crack closure in GLARE. It is assumed that crack closure in FMLs is determined by the actual stress cycles in the metal layers and that it can be described with the available relations for monolithic aluminium published in the literature. Fatigue crack growth experiments have been performed on GLARE specimens in which crack growth rates and crack opening stresses have been recorded. The prediction model incorporating the crack closure relation for aluminium 2024-T3 obtained from the literature has been validated with the test results. It is concluded that crack growth in GLARE can be correlated with the effective SIF range at the crack tip in the aluminium layers, if it is determined with the crack closure relation for aluminium 2024-T3 based on actual stresses in the aluminium layers.     

Effect of biaxial loads on elastic-plastic <Emphasis Type="Italic">J</Emphasis> and crack tip constraint for cracked plates: finite element study

Based on detailed two-dimensional (2-D) and three-dimensional (3-D) finite element (FE) analyses, this paper attempts to quantify in-plane and out-of-plane constraint effects on elastic-plastic J and crack tip stresses for a plate with a through-thickness crack and semi-elliptical surface crack under positive biaxial loading. For the plate with a through-thickness crack, plate thickness and relative crack length are systematically varied, whereas for the plate with a semi-elliptical surface crack, the relative crack depth and aspect ratio of the semi-elliptical crack are systematically varied. It is found that the reference stress based approach for uniaxial loading can be applied to estimate J under biaxial loading, provided that the limit load specific to biaxial loading is used, implying that quantification of the biaxiality effect on the limit load is important. Investigation on the effect of biaxiality on the limit load suggests that for relatively thin plates with small cracks, in particular with semi-elliptical surface cracks, the effect of biaxiality on the limit load can be neglected for positive biaxial loading, and thus elastic-plastic J for a biaxially loaded plate could be estimated, assuming that such plate is subject to uniaxial load. Regarding the effect of biaxiality on crack tip stress triaxiality, it is found that such effect is more pronounced for a thicker plate. For plates with semi-elliptical surface cracks, the crack aspect ratio is found to be more important than the relative crack depth, and the effect of biaxiality on crack tip stress triaxiality is found to be more pronounced near the surface points along the crack front.     

On higher order parameters in cracked composite plates under far‐field pure shear

This paper presents the analytical solution of the crack tip fields as well as the crack parameters in an infinitely large composite plate with a central crack subjected to pure shear loading. To this end, the complex variable method is employed to formulate an asymptotic solution for the crack tip fields in an anisotropic plane. Using a stress‐based definition of the crack tip modes of loading, only the mode II crack parameters are found to be non‐zero under pure shear load. Special focus is given to the determination of the higher order parameters of the crack tip asymptotic field, particularly the first non‐singular term, ie, the T‐stress. Unlike the isotropic materials, in which the T‐stress is zero under pure shear, it is found that the T‐stress is non‐zero for the case of anisotropic materials, being the only material‐dependent crack tip stress parameter. The veracity of our exact crack tip fields is assessed and verified through a comparison made with respect to the finite element (FE) solution. Finally, we demonstrate the significance of the T‐stress on stresses near the crack tip in composite plates under pure shear loads.     

A crack in a linear-elastic material under mode II loading, revisited

A sharp crack in a two-dimensional infinite linear-elastic material, under pure shear (mode II) loading is re-examined. Several criteria have been proposed for the prediction of the onset and direction of crack extension along a path emanating from the tip of the initial crack. These criteria date back some three decades and are well documented in the literature. All the predictions from the different criteria are close and indicate that the crack extension takes a direction at an angle of ≈ −70° measured counterclockwise from the positive x -axis, in the case of a remotely applied positive shear stress. However, the possibility seems to have been overlooked that the crack extension may initiate not from the crack tip itself, but instead may initiate on the free surface at an infinitesimal distance behind the crack tip. The effect of crack tip plasticity on the relevant stresses in the region of the crack tip is investigated by the application of an elastic–plastic finite element program.     

Prediction of fatigue crack growth under constant amplitude loading and a single overload based on elasto-plastic crack tip stresses and strains

It is generally accepted that the fatigue crack growth (FCG) depends mainly on the stress intensity factor range (ΔK) and the maximum stress intensity factor (K_max). The two parameters are usually combined into one expression called often as the driving force and many various driving forces have been proposed up to date. The driving force can be successful as long as the stress intensity factors are appropriately correlated with the actual elasto-plastic crack tip stress-strain field. However, the correlation between the stress intensity factors and the crack tip stress-strain field is often influenced by residual stresses induced in due course.A two-parameter (ΔK_tot, K_max,tot) driving force based on the elasto-plastic crack tip stress-strain history has been proposed. The applied stress intensity factors (ΔK_appl, K_max,appl) were modified to the total stress intensity factors (ΔK_tot, K_max,tot) in order to account for the effect of the local crack tip stresses and strains on fatigue crack growth. The FCG was predicted by simulating the stress-strain response in the material volume adjacent to the crack tip and estimating the accumulated fatigue damage. The fatigue crack growth was regarded as a process of successive crack re-initiations in the crack tip region. The model was developed to predict the effect of the mean and residual stresses induced by the cyclic loading. The effect of variable amplitude loadings on FCG can be also quantified on the basis of the proposed model. A two-parameter driving force in the form of: was derived based on the local stresses and strains at the crack tip and the Smith-Watson-Topper (SWT) fatigue damage parameter: D = σ_maxΔε/2. The effect of the internal (residual) stress induced by the reversed cyclic plasticity manifested itself in the change of the resultant (total) stress intensity factors controlling the fatigue crack growth.The model was verified using experimental fatigue crack growth data for aluminum alloy 7075-T6 obtained under constant amplitude loading and a single overload.     

Stress analysis in a cracked infinite electrostrictive plate with local saturation electric fields

Based on the electric circular saturation zone near an ideal crack tip, the approximate complete solution for electric and stress field in a cracked electrostrictive plate under general loading at infinity is carried out. The SIFs are then obtained. We find that the stress distributions in front of the crack tip can be divided into four different regions. The fracture behavior is closely related to these distributions.