幂硬化粘塑性材料动态扩展裂纹尖端场的渐近解

采用弹性－粘塑性本构模型，对幂硬化粘塑性介质中反平面剪切动态扩展裂纹尖端的应力，应变场进行了渐近分析，给出了反平面剪切动态扩展纹尖端场的渐进方程。分析结果表明，在裂纹法端应力具有（ｌｎＲ／ｒ）１／ｎ－１的奇异性，应变具有（ｌｎＲ／Ｒｎ／ｎ－１的奇异性。从而提示了幂硬化粘塑材料反平面剪动态扩展裂纹尖端场的渐近行为。     

蠕变硬化材料中Ⅱ型扩展裂纹尖端场特性研究

采用弹牯塑性力学模型,对蠕变硬化材料中平面应变扩展裂纹尖端场进行了渐近分析.假设人工粘性系数与等效塑性应变率的幂次成反比,通过量级匹配表明应力和应变均具有幂奇异性,奇异性指数由粘性系数中等效塑性应变率的幂指数唯一确定.通过数值计算讨论了Ⅱ型准静态扩展裂纹尖端场的分区构造以及裂纹尖端应力和应变场的特性随各材料参数的变化规律,结果表明裂尖场由材料的粘性和塑性共同主导.当硬化系数为零时裂尖场可退化为相应的HR场.     

具有鲍氏效应的幂硬化材料Ⅲ型定常扩展裂纹奇异场

本文利用和提出的考虑鲍氏效应的塑性硬化(即各向异性硬化)模型,通过引入一表征各向异性硬化效应的参数β,得到了幂硬化材料的本构方程。分析了Ⅲ型定常扩展裂纹尖端的弹塑性场,得到了对数奇异性的解。给出了尖端附近应力应变场的可能变化范围,及裂纹的开口位移。并对真实解作出了预期。     

动态裂纹尖端弹粘塑性场的研究

本文利用弹一粘一塑性材料力学模型,对动态扩展裂纹尖端的指数奇异性和对数奇异性进行了渐近分析。文中假定,弹性阶段的粘性效应可以略去,仅在塑性应变中粘性才起作用,对于这种模型,推导出了其率敏感型的本构关系。以Ⅱ型裂纹为例,进一步推导了两种奇异性下裂纹尖端场的渐近微分控制方程,并进行了数值仿真分析。同时讨论了粘性系数α、马赫数M^2对裂纹尖端应力应变场的影响,即,弹粘塑性材料扩展裂纹的奇异性取决于其粘性系数和马赫数,粘性系数较大时,裂纹尖端场具有对数奇异性;粘性系数较小时,裂纹尖端场具有指数奇异性。修正了文献中对数奇异性区域的大小;解释了文献中过渡区的成因;给出了过渡区尖端应力场解的形式,从而建立了裂纹尖端场的统一解。     

某抽水蓄能电站地下洞室围岩岩体质量特征分析

考虑材料的黏性效应建立了II型动态扩展裂纹尖端的力学模型,假设黏性 系数与塑性等效应变率的幂次成反比,通过分析使尖端场的弹、黏、塑性得到合理匹配,并 给出边界条件作为扩展裂纹定解的补充条件,对理想塑性材料中平面应变扩展裂纹尖端场进 行了弹黏塑性渐近分析,得到了不含间断的连续解,并讨论了II型裂纹数值解的性质随各参 数的变化规律. 分析表明应力和应变均具有幂奇异性,对于II型裂纹,裂尖场不含弹性卸载 区. 引入Airy应力函数,求得了II型准静态裂纹尖端场的控制方程,并进行了数值分析, 给出了裂纹尖端的应力应变场. 当裂纹扩展速度($M\to 0$)趋于零时,动态解趋 于准静态解,表明准静态解是动态解的特殊形式.     

Ⅱ型动态扩展裂纹尖端的弹黏塑性渐近场

考虑材料的黏性效应建立了Ⅱ型动态扩展裂纹尖端的力学模型,假设黏性系数与塑性等效应变率的幂次成反比,通过分析使尖端场的弹、黏、塑性得到合理匹配,并给出边界条件作为扩展裂纹定解的补充条件,对理想塑性材料中平面应变扩展裂纹尖端场进行了弹黏塑性渐近分析,得到了不含间断的连续解,并讨论了Ⅱ型裂纹数值解的性质随各参数的变化规律.分析表明应力和应变均具有幂奇异性,对于Ⅱ型裂纹,裂尖场不含弹性卸载区.引入Airy应力函数,求得了Ⅱ型准静态裂纹尖端场的控制方程,并进行了数值分析,给出了裂纹尖端的应力应变场.当裂纹扩展速度(M→0)趋于零时,动态解趋于准静态解,表明准静态解是动态解的特殊形式.     

I型定常扩展裂纹尖端的弹黏塑性场

考虑材料在扩展裂纹尖端的黏性效应，假设黏性系数与塑性应变率的幂次成反比，对幂硬化材料中平面应变扩展裂纹尖端场进行了弹黏塑性渐近分析，得到了不含间断的连续解，并讨论了I型裂纹数值解的性质随各参数的变化规律. 分析表明应力和应变均具有幂奇异性，并且只有在线性硬化时，尖端场的弹、黏、塑性才可以合理匹配. 对于I型裂纹，裂尖场不含弹性卸载区. 当裂纹扩展速度趋于零时，动态解趋于准静态解，表明准静态解是动态解的特殊形式；如果进一步考虑硬化系数为零的极限情况，便可退化为Hui和Riedel的非线性黏弹性解.     

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.     

幂硬化材料Ⅲ型稳恒扩展裂纹奇异场

幂硬化材料稳恒扩展裂纹奇异场的分析是久未解决的困难问题。本文对Ⅲ型问题得到了含有对数奇异性的解,给出了尖端附近应力与应变的奇异场的可能变化范围。     

应变损伤材料I型动态扩展裂纹尖端场的渐近分析

研究了应变损伤材料Ｉ型动态扩展的裂纹尖端场。假定材料服从Ｊ２流动理论，且损伤规律以幂律应变软化的规律给出。对于塑性区引进了应力函数φ，ψ０借助于动力学方程的分析，给出了渐近方程及数值解。结果表明，对于可压缩材料Ｉ型平面应变尖端场是完全由塑性区组成，没有弹性卸载区。在裂纹尖端附近，应力和应变分别具有如下的奇异性：σ￣（ｌｎＲ／ｒ）＾－ｎ／ｎ＋１，ε￣（ｌｎＲ／ｒ）＾１／ｎ＋１。     

Plane stress dynamic fields near a propagating crack-tip in a power-law material

Based on the plastic-dynamic equations, the asymptotic behaviour of the near-tip fields for a plane stress tensile crack propagating in a power-law material has been studied in this paper. It is shown that the stress and strain singularities are, respectively, of the order and , whereA is a constant which is related to the size of plastic region,r is the distance to the crack tip,n is the power-law exponent. Projects sponsored by the National Science Foundation.     

A weighted residual method for elastic-plastic analysis near a crack tip and the calculation of the plastic stress intensity factors

In this paper,a weighted residual method for the elastic-plastic analysis near a crack tip is systematically given by taking the model of power-law hardening under plane strain condition as a sample.The elastic-plastic solutions of the crack tip field and an approach based on the superposition of the nonlinear finite element method on the complete solution in the whole crack body field,to calculate the plastic stress intensity factors,are also developed.Therefore,a complete analysis based on the calculation both for the crack tip field and for the whole crack body field is provided.     

A phenomenological model of fatigue crack growth in perfectly plastic infinite plates under completely reversed uniaxial loading

The fatigue failure of a thin infinite center-cracked plate under completely reversed uniaxial loading is considered. A two-stage fatigue crack model including the incubation and crack propagation stages is constructed. The stress distribution in the vicinity of the crack tip is described using the concept of a conventional elastic crack. The crack-tip plastic zone is simulated by a Dugdale thin plastic zone, and the condition for the movement of the failure front is given by criteria of damage mechanics. It is shown that the fatigue crack growth rate in perfectly plastic materials with a plastic zone of constant length is a power-law function of the stress intensity factor range. This relationship is quadratic when the length of the plastic zone is not constant Published in Prikladnaya Mekhanika, Vol. 41, No. 12, pp. 116–127, December 2005.     

Crack propagation in the power-law nonlinear viscoelastic material

I.IntroductionCrazingdamageisacommonphenon1enonoffractureofpolymericmaterials.Theformationofcrazezoneisamid-stateinthefractureprocessofthematerialsfromperfectstatetofaiIurc.Microscopically,inthisregionthereexistssomefibrilslinkingthetwocracksurfacesandres…     

On the interaction between a dislocation and a crack in a material with a nonlinear stress-strain law

The problem of the interaction of a crack and a dislocation in a medium with a nonlinear stress-strain law is considered for the case of a semi-infinite crack in a displacement loaded strip under longitudinal shear deformation. A power law stress-strain relation is considered and the dislocation is assumed positioned so that the net effect of its interaction with the crack is to produce a zero stress intensity factor when combined with the effect of the applied displacements. Thus the Atkinson-Kay superdislocation model of a relaxed crack tip is extended to the situation where the material satisfies a power-law stress-strain relationship.     

Field structure at mode III dynamically propagating crack tip in elastic-viscoplastic materials

An elastic-viscoplastic mechanics model is used to investigate asymptotically the mode Ⅲ dynamically propagating crack tip field in elastic-viscoplastic materials. The stress and strain fields at the crack tip possess the same power-law singularity under a linear-hardening condition. The singularity exponent is uniquely determined by the viscosity coefficient of the material. Numerical results indicate that the motion parameter of the crack propagating speed has little effect on the zone structure at the crack tip. The hardening coefficient dominates the structure of the crack-tip field. However, the secondary plastic zone has little influence on the field. The viscosity of the material dominates the strength of stress and strain fields at the crack tip while it does have certain influence on the crack-tip field structure. The dynamic crack-tip field degenerates into the relevant quasi-static solution when the crack moving speed is zero. The corresponding perfectly-plastic solution is recovered from the linear-hardening solution when the hardening coefficient becomes zero.     

圆形域多圆孔多裂纹反平面问题研究

本文运用复变函数及积分方程方法，求解了圆形域多圆孔多裂纹反平面问题，建立了两种类型的基本解。复叠加原理和所得的基本解并沿国圆孔和裂纹表面取待定的基本解密度函数，可得到一组以基本解密度函数为未知函数的Ｆｒｅｄｈｏｌｍ积分方程。通过该积分方程组的数值可以得到密度函数的离散值，进而得到了裂纹尖端的应力强度因子。     

Field structure at mode Ⅲ dynamically propagating crack tip in elastic-viscoplastic materials

An elastic-viscoplastic mechanics model is used to investigate asymptotically the mode Ⅲ dynamically propagating crack tip field in elastic-viscoplastic materials. The stress and strain fields at the crack tip possess the same power-law singularity under a linear-hardening condition. The singularity exponent is uniquely determined by the viscosity coefficient of the material. Numerical results indicate that the motion parameter of the crack propagating speed has little effect on the zone structure at the crack tip. The hardening coefficient dominates the structure of the crack-tip field. However, the secondary plastic zone has little influence on the field. The viscosity of the material dominates the strength of stress and strain fields at the crack tip while it does have certain influence on the crack-tip field structure. The dynamic crack-tip field degenerates into the relevant quasi-static solution when the crack moving speed is zero. The corresponding perfectly-plastic solution is recovered from the linear-hardening solution when the hardening coefficient becomes zero.     

理想塑性介质中平面应力 静止裂纹的尖端弹塑性场

本文详细分析了理想塑性介质中平面应力I型静止裂纹的尖端弹塑性场,结果表明:裂纹尖端应力场内可以不包含应力间断线,但含有弹性区,作为这个一般解的特殊情况,当弹性区被两侧的塑性区挤压消失而尖端场成为满塑性区时,便得到Hutchinson(1968)给出的解,此外,文中还给出了另一种均匀应力区位于裂纹前方的解,这是[1]未曾得到的。     

平面幂律塑性Ⅰ型裂纹尖端应力场全解

在航空航天、船舶、石油管道和核电等领域,服役结构或部件在长期极端条件下运行,不可避免地会产生裂纹,因此,为研究含裂纹结构的准静态断裂行为,必须了解裂纹尖端附近区域的应力应变场特点.对于幂律材料裂纹构元,研究平面应变和平面应力条件下Ⅰ型裂纹尖端应力场的解析分布.基于能量密度等效和量纲分析,推导了能量密度中值点代表性体积单元(representative volume element, RVE)的等效应力解析方程,并定义其为应力因子,进而针对有限平面应变和平面应力紧凑拉伸(compact tension, CT)试样和单边裂纹弯曲(single edge bend, SEB)试样,以应力因子作为应力特征量,并构造用于表征裂尖等效应力等值线的蝶翅轮廓式和扇贝轮廓式三角特殊函数,提出描述幂律塑性条件下平面I型裂纹尖端应力场的半解析模型.该半解析模型形式简单,对CT和SEB试样的裂尖应力场的预测结果与有限元分析的结果比较表明,两者之间均密切吻合,模型公式可直接用于预测Ⅰ型裂纹尖端应力分布,方便于断裂安全评价和理论发展.