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1.
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.  相似文献   

2.
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.  相似文献   

3.
压-剪混合型定常扩展裂纹尖端的弹黏塑性场   总被引:1,自引:2,他引:1  
梁文彦  王振清  周博 《力学学报》2006,38(5):618-625
假定黏性系数与塑性等效应变率的幂次成反比,考虑其黏性和裂纹面摩擦接触效应 建立了压-剪混合型定常扩展裂纹尖端弹黏塑性场的渐近方程,求得了裂纹尖端场不含应力、应变间 断的数值解. 并讨论了压-剪混合型裂纹数值解随各个参数的变化规律,计算结果 和分析表明,压-剪混合型裂纹尖端场是满塑性的,不含有弹性卸载区,黏性效应是研究扩展裂纹尖端场时的一个重要因素. 无论混合裂纹趋近I型还是趋近II型,静水压力随摩擦系数的增加都是增加的,裂纹面摩擦 效应是阻止裂纹扩展速度的因素,且摩擦作用越强,裂纹尖端场的韧性越高.  相似文献   

4.
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.  相似文献   

5.
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.  相似文献   

6.
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。  相似文献   

7.
稳恒扩展裂纹尖端的弹粘塑性场   总被引:16,自引:0,他引:16  
采用弹粘塑性力学模型代替通常的弹塑性模型,对于I型和Ⅱ型问题,分别求得了不可压缩材料中平面应变动态扩展裂纹尖端的指数奇异性场和对数奇异性场,消除了弹塑性解中存在的塑性激波。通过数值计算,分别求得了两种奇异属性的分界线,建立起统一的裂纹尖端奇异性场。  相似文献   

8.
蠕变材料Ⅰ型动态扩展裂纹尖端场   总被引:4,自引:1,他引:4  
唐立强  蔡艳红 《力学学报》2005,37(5):573-578
为了研究黏性效应作用下的动态扩展裂纹尖端渐近场,建立了蠕变材料Ⅰ型动态扩展裂纹的 力学模型.首先,依据在稳态蠕变阶段,弹性变形和黏性变形同时在裂纹尖端场中占主导地 位,由量级协调可知,应力和应变具有相同的奇异量级,即(σ,ε)∝/ r- 1/(n-1). 其次,通过渐近分析推导出动态扩展裂纹尖端场的控制方程并求得了裂纹尖端应 力、应变和位移分离变量形式的渐近解.最后,采用双参数打靶法求得了裂纹尖端应力、应 变的数值结果.数值计算表明,裂尖场主要受材料的蠕变指数n和马赫数M的控制;在Ⅰ 型动态扩展裂纹前方,环向应变达到最大值,可据此建立断裂准则. 由于裂纹稳定扩展与非稳定扩展的主奇异项相同,因此对于稳定扩展裂纹的渐近分析方 法,同样适用于非稳定的裂纹扩展问题.  相似文献   

9.
扩展裂纹准静态渐近解中的矛盾   总被引:4,自引:2,他引:4  
裂纹尖端附近的应力应变场是一个相当复杂的问题,对于不同的情况,这个场具有完全不同的渐近属性.具体说来,场的渐近属性取决于裂纹状态(静止还是扩展)、几何特征(平面应变还是平面应力)、加载速度(准静态还是动态)、裂纹型式(Ⅰ、Ⅱ、Ⅲ型)及材料性质(弹性、塑性、蠕变、……).其中,人们较为重视的一种情况是扩展裂纹尖端的塑性场.而且,为了使问题简化,通常采用准静态假定.对于理想塑性材料Ⅲ型扩展裂纹的渐近解由Chitaley和McClintock给出.对于Ⅰ型裂纹,Slepyan采用Tresca属服条件给出了渐近解,高玉臣和Rice采用Mises屈服条件得到了渐近解,但这些解只适用于  相似文献   

10.
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。  相似文献   

11.
The viscosity of material is considered at propagating crack-tip. Under the assumption that the artificial viscosity coefficient is in inverse proportion to power law of the plastic strain rate, an elastic-viscoplastic asymptotic analysis is carried out for moving crack-tip fields in power-hardening materials under plane-strain condition. A continuous solution is obtained containing no discontinuities. The variations of numerical solution are discussed for mode I crack according to each parameter. It is shown that stress and strain both possess exponential singularity. The elasticity, plasticity and viscosity of material at crack-tip only can be matched reasonably under linear-hardening condition. And the tip field contains no elastic unloading zone for mode I crack. It approaches the limiting case, crack-tip is under ultra-viscose situation and energy accumulates, crack-tip begins to propagate under different compression situations.  相似文献   

12.
The viscosity of material is considered at propagating crack-tip. Under the assumption that the artificial viscosity coefficient is in inverse proportion to power law of the plastic strain rate, an elastic-viscoplastic asymptotic analysis is carried out for moving crack-tip fields in power-hardening materials under plane-strain condition. A continuous solution is obtained containing no discontinuities. The variations of numerical solution are discussed for mode Ⅰ crack according to each parameter. It is shown that stress and strain both possess exponential singularity. The elasticity, plasticity and viscosity of material at crack-tip only can be matched reasonably under linear-hardening condition. And the tip field contains no elastic unloading zone for mode Ⅰ crack. It approaches the limiting case, crack-tip is under ultra-viscose situation and energy accumulates, crack-tip begins to propagate under different compression situations.  相似文献   

13.
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.  相似文献   

14.
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.  相似文献   

15.
An elastic-viscoplastic constitutive model was adopted to analyze asymptotically the tip-field of moving crack in linear-hardening materials under plane strain condition. Under the assumption that the artificial viscosity coefficient was in inverse proportion to power law of the rate of effective plastic strain, it is obtained that stress and strain both possess power law singularity and the singularity exponent is uniquely determined by the power law exponent of the rate of effective plastic strain. Variations of zoning structure according to each material parameter were discussed by means of numerical computation for the tip-field of mode Ⅱ dynamic propagating crack, which show that the structure of crack tip field is dominated by hardening coefficient rather than viscosity coefficient. The secondary plastic zone can be ignored for weak hardening materials while the secondary plastic zone and the secondary elastic zone both have important influence on crack tip field for strong hardening materials. The dynamic solution approaches to the corresponding quasi-static solution when the crack moving speed goes to zero, and further approaches to the HR (Hui-Riedel) solution when the hardening coefficient is equal to zero.  相似文献   

16.
Ⅲ型扩展裂纹尖端场渐近解的研究   总被引:3,自引:0,他引:3  
李范春 《力学学报》1993,25(6):732-737
本文采用弹性-粘塑性模型对反平面剪切扩展裂纹问题进行了研究。文中通过对动态扩展问题和准静态扩展问题的分析得到了各自的渐近解,并且证明了准静态扩展解是动态扩展解的特殊情况,从而使二者统一起来。  相似文献   

17.
For a compression-shear mixed mode interface crack, it is difficult to solve the stress and strain fields considering the material viscosity, the crack-tip singularity, the frictional effect, and the mixed loading level. In this paper, a mechanical model of the dynamic propagation interface crack for the compression-shear mixed mode is proposed using an elastic-viscoplastic constitutive model. The governing equations of propagation crack interface at the crack-tip are given. The numerical analysis is performed for the interface crack of the compression-shear mixed mode by introducing a displacement function and some boundary conditions. The distributed regularities of stress field of the interface crack-tip are discussed with several special parameters. The final results show that the viscosity effect and the frictional contact effect on the crack surface and the mixed-load parameter are important factors in studying the mixed mode interface crack- tip fields. These fields are controlled by the viscosity coefficient, the Mach number, and the singularity exponent.  相似文献   

18.
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