空心车轴不同深度表面裂纹应力强度因子研究

分析了空心车轴的旋转弯曲载荷的特点,建立了空心轴表面周向半椭圆裂纹的模型,给出了半椭圆裂纹的构形参数定义,即形状比、深度比和裂纹前缘相对位置。采用四分之一20节点等参退化奇异单元,通过有限元计算,模拟裂纹前沿的应力奇异性。在此基础上,计算了裂纹前缘表面点和中心点的应力强度因子随着裂纹扩展深度和旋转角度的变化。计算结果表明,对于给定的裂纹构形,在车轴的一个载荷循环中,裂纹前缘同一相对位置的应力强度因子是不断变化的,不同位置的应力强度因子在达到最大值的角度也是不同的,这就导致了裂纹前缘表面点在一些角度下的扩展是不对称的。这些结果为进一步研究空心轴表面裂纹的扩展路径和寿命提供了参考。     

CT试样三维疲劳裂纹扩展数值模拟

在循环载荷下疲劳裂纹的裂纹形貌在稳定扩展区近似为半椭圆形状,因此通过Paris方法根据疲劳裂纹表面尖端点应力强度因子的变化幅值(△K)得到扩展速率与真实的裂纹速率会有误差.为了更好的研究疲劳裂纹的性质,本文通过分析紧凑拉伸(CT)试样的疲劳裂纹扩展后的三维形貌,采用Jiang-Sehitoglu循环塑性模型和疲劳准则以...     

拉伸螺杆半椭圆表面裂纹应力强度因子

将拉伸螺杆简化为理论应力集中系数Kt不同的带“V”形缺口圆杆,采用裂纹尖端为20节点奇异单元的三维有限元模型,对螺杆半椭圆表面裂纹的应力强度因子进行了计算.给出了具有普遍性意义的螺杆表面裂纹应力强度因子公式.为验证本文计算结果的有效性,还将本文M22×1.5螺杆的应力强度因子计算结果与试验结果进行了对比.     

基于子模型法的带有表面裂纹钢丝应力强度因子研究

钢丝裂纹应力强度因子是进行钢丝疲劳断裂寿命评估、疲劳裂纹扩展分析和钢丝断裂强度评估等工作的重要参数。本文首先介绍了裂纹扩展分析软件FRANC3D,然后基于子模型法模拟研究了拉伸荷载作用下带有表面裂纹钢丝的应力强度因子,裂纹种类包括直线形裂纹和半圆形裂纹,最后拟合得到拉伸荷载作用下带表面裂纹钢丝的应力强度因子形状修正系数表达式,分析了利用该公式进行承载力评估时产生误差的原因。研究结果表明,利用子模型模拟分析拉伸荷载作用下带有表面裂纹的钢丝应力强度因子时计算精度高,计算速度快,对计算机硬件要求低;利用该方法得到的钢丝裂纹应力强度因子,在进行索承式桥梁吊索安全性能评估时,评估结果更精确。     

焊趾表面裂纹的形态发展曲线与疲劳寿命预测

以作者建立的焊地椭圆表面裂纹应力强度因子数据库以及复杂应力场中焊践半随圆表面裂纹前缘应力强度因子分布计算的基本模式法为基础上,给出了复杂应力场中焊践表面表纹在疲劳扩展过程中形态变化规律及寿命的工程分析方法。     

扭力轴三维裂纹扩展寿命仿真研究

对疲劳载荷谱作用下三维表面裂纹,采用双重边界元理论求解裂纹前沿的应力应变场,运用Forman理论、最小应变能密度法和Elber模型,计算裂纹前沿各点的扩展长度、扩展方向和应力强度因子等特征量.根据增量步下裂纹几何形状的改变,对裂纹面进行网格重划分和迭代计算,模拟三维裂纹的扩展,预测裂纹扩展寿命.扭力轴表面裂纹扩展的仿真结果表明该方法合理可行.     

拉伸载荷作用下共面表面裂纹间应力强度因子影响系数的有限元分析

采用参数化有限元方法,结合节点力法和循环迭代算法,对一有限厚矩形板表面有两个相邻共面半椭圆表面裂纹在拉伸载荷作用下进行了求解,得到了两裂纹在不同形状和相隔距离时的应力强度因子的影响系数,计算结果对含三维广布裂纹结构的剩余强度和疲劳寿命有参考意义.     

用三维光弹法确定轴表面横向半椭圆裂纹应力强度因子及其修正系数

用三维光弹法测定了轴表面横向半椭圆裂纹的应力强度因子，并分析计算了应力强度因子修正系数，结果表明，应力强度因子的分布型式对加载条件和裂纹几何不敏感；修正系数对裂纹深度呈现对称分布趋势，仅取决于裂纹几何参数。     

基于表面弹性理论的开裂椭圆孔断裂力学研究

研究纳米尺度时开裂椭圆孔的III型断裂性能。基于表面弹性理论和保角映射技术，利用复势函数理论获得了缺陷(裂纹和椭圆孔)周围应力场和裂纹尖端应力强度因子的闭合解答。所得结果具有一般性，许多已有和新的解答可由本文退化的特殊情形得到。利用解析结果讨论了缺陷的绝对尺寸、椭圆孔的形状比以及裂纹的相对尺寸对应力强度因子的影响。结果表明：考虑表面效应且缺陷尺寸在纳米尺度时，应力强度因子具有显著的尺寸依赖效应；应力强度因子随椭圆孔形状比的变化规律受缺陷表面常数的影响；缺陷表面效应的影响取决于椭圆孔的形状比，非常大的形状比屏蔽了表面效应的影响；裂纹相对尺寸非常小时表面效应影响较弱，裂纹相对尺寸较大时表面效应较为明显。     

钢轨表面三维疲劳裂纹扩展数值分析

在车轮循环滚动接触载荷作用下,钢轨接触表面裂纹问题频发,严重威胁高速列车运行安全,开展钢轨表面三维滚动接触疲劳裂纹扩展分析意义重大.首先,考虑不同初始裂纹角度,建立钢轨轨头含初始裂纹的三维有限元模型,对钢轨表面施加循环滚动接触载荷,进行轮轨滚动接触计算;然后,基于相互作用积分法计算裂纹前缘的应力强度因子;最后,采用最大周向应力准则和Paris公式计算当前状态下裂纹扩展方向和扩展速率,进而更新下一时刻的裂纹形状和尺寸.通过对上述过程重复实现,从而预测钢轨表面三维裂纹的扩展路径.加载过程中裂纹前缘应力强度因子计算结果表明,随着初始裂纹角度增加,K_Ⅰ的峰值逐渐减小,K_Ⅱ的峰值逐渐增大,裂纹前缘各位置的等效应力强度因子逐渐减小;裂纹前缘节点的位置越靠近钢轨表面,等效应力强度因子越大.疲劳裂纹扩展计算结果表明,随着循环次数的增加,不同初始角度下的裂纹都发生了偏折,逐渐朝着钢轨深度方向扩展,且裂纹的初始角度越大,发生扩展时需要的循环次数越多.对比三种初始裂纹角度下裂纹长度随循环次数的演化曲线可以发现,初始裂纹角度越小,裂纹扩展速率越大.所开发的方法也适用...     

Crack kinking from an interface crack with initial contact between the crack lips

The authors recently theoretically studied crack kinking and opening from an initially closed crack (without friction) in some homogeneous medium. The same problem, but for an interface crack, is considered here. Comninou has shown that the asymptotic stress field prior to kinking is governed by a single, mode II stress intensity factor (SIF). Using this result, plus a homogeneity property of the problems of elastic fracture mechanics with unilateral contact envisaged, a change of scale, and two reasonable hypotheses, we establish the expression of the SIF at the tip of the small, open crack extension. It is shown that whatever the geometry of the external boundary and the crack and whatever the loading, these SIF depend solely upon the initial (mode II) SIF (in a linear way), the kink angle and Dundurs' parameters α and β. Using this result and Goldstein and Salganik's “principle of local symmetry” to predict the kink angle, one finds that it is independent of the loading but does depend upon Dundurs' parameters α and β. This contrasts with the case of an ordinary (initially closed) crack in some homogeneous medium, for which the kink angle was not only independent of the loading but an absolute constant. However, it is numerically found that the influence of the mismatch of elastic properties upon the kink angle is rather weak.     

Elastic-plastic analysis of antiplane crack near crack surface region

The elastic-plastic stress distribution and the elastic-plastic boundary con- figuration near a crack surface region are significant but hard to obtain by means of the conventional analysis. A crack line analysis method is developed in this paper by consid- ering the crack surface as an extension of the crack line. The stresses in the plastic zone, the length, and the unit normal vector of the elastic-plastic boundary near a crack surface region are obtained for an antiplane crack in an elastic-perfectly plastic solid. The usual small scale yielding assumptions are not needed in the analysis.     

THE EXACT SOLUTIONS OF ELASTIC－PLASTIC CRACK LINE FIELD FOR MODE ⅡPLANE STRESS CRACK

ＴＨＥＥＸＡＣＴＳＯＬＵＴＩＯＮＳＯＦＥＬＡＳＴＩＣ－ＰＬＡＳＴＩＣＣＲＡＣＫＬＩＮＥＦＩＥＬＤＦＯＲＭＯＤＥＩＩＰＬＡＮＥＳＴＲＥＳＳＣＲＡＣＫＹｉＺｈｉｊｉａｎ（易志坚）ＷａｎｇＳｈｉｊｉｅ（王士杰）ＷａｎｇＸｉａｎｇｊｉａｎ（王向坚）（Ｒｅｃｅ...     

一种新型三角形裂尖单元及其在结构裂纹分析中的应用

构造了一种适合边界元分析裂纹问题的三角形单元,该单元中的形函数包含两部分,主要部分用于捕捉裂纹尖端上位移分布的陡峭特性(性质),另一部分为常规的拟合函数,体现裂纹尖端位置附近的物理量在其他方向上的连续分布。形函数主要部分的构造充分利用了已有理论研究获得的结论,在裂纹表面,随着距离远离尖端,位移分布与■函数保持同阶变化。在传统形函数的基础上,通过先乘以一项同阶于■的变量项,再在系数中将其在形函数所在点上的值除去,便得到新型的用于拟合裂纹尖端附近位移和面力分布的形函数。新的形函数能够满足形函数的delta性质,但归一性不再满足,因此,新的形函数只用于物理量的拟合,而几何量的拟合依然采用传统方案。通过对偶边界元方法计算裂纹尖端的张开位移后,利用一种位移外插方法计算获得应力强度因子。数值算例关注了一种无限域内的圆盘裂纹,应用新构造的三角形单元于对偶边界元中计算结构在受到斜拉力时裂纹尖端的三种应力强度因子。通过与参考解进行对比,验证了该插值方案用于对偶边界元分析裂纹问题时的正确性和高精度。     

A Zener-Stroh crack interacting with an edge dislocation

A Zener-Stroh crack interacting with an edge dislocation is studied. The crack faces are assumed to be traction free. The applied ‘generalized loading’ for crack is the initial displacement jump and the intervention of the edge dislocation. Through decomposing the problem into two sub-simple problems, using the superposition principle, its solution is obtained. To demonstrate both the validity of the solution and its potential application, two simple examples related to the crack stress intensity factors are presented on the basis of the solution. The application of the solution to model crack initiations arising from dislocation-pileup is discussed.     

NEAR CRACK LINE ELASTIC－PLASTIC ANALYSIS FOR A CRACK LOADED BY ANTIPLANE POINT FORCES

ＮＥＡＲ　ＣＲＡＣＫ　ＬＩＮＥ　ＥＬＡＳＴＩＣ－ＰＬＡＳＴＩＣ　ＡＮＡＬＹＳＩＳ　ＦＯＲ　Ａ　ＣＲＡＣＫ　ＬＯＡＤＥＤ　ＢＹ　ＡＮＴＩＰＬＡＮＥ　ＰＯＩＮＴ　ＦＯＲＣＥＳＷｕＣｈｅｎｇｐｉｎｇ（吴承平）；ＷａｎｇＣｈｅｎｇ（王成）（ＲｅｃｅｉｖｅｄＳ...     

Interaction between crack and elastic inclusion

ＩＮＴＥＲＡＣＴＩＯＮＢＥＴＷＥＥＮＣＲＡＣＫＡＮＤＥＬＡＳＴＩＣＩＮＣＬＵＳＩＯＮＺｈａｎｇＭｉｎｇ－ｈｕａｎ（张明焕）,ＴａｎｇＲｅｎ－ｊｉ（汤任基）（ＳｈａｎｇｈａｉＪｉａｏｔｏｎｇＵｎｉｖｅｒｓｉｔｙ,Ｓｈａｎｇｈａｉ,２０００３０,Ｐ．Ｒ．...     

Stress-strain field near crack tip and calculation of critical stress of crack propagation in a pure bending beam of rectangular section with one-sided mode i crack

This paper studies the stress-strain field near crack tip in a pure bending beam of rectangular section with one-sided mode I crack by the analytic method of Ref. [1], then it gives the stress and strain components at the crack tip when the crack propagates and further it obtains the formulas of calculating the elastic deformed area width, the deformed intensity area width and the equation groups of calculating the critical stress of crack propagation, last the equation group of calculating critical stress of crack propagation is verified by calculating instance. The maximum error is 0.18%. First Received May 7, 1994.     

Micromechanics analyses of interface crack

A new mechanics model based on Peierls concept is presented in this paper, which can clearly characterize the intrinsic features near a tip of an interfacial crack. The stress and displacement fields are calculated under general combined tensile and shear loadings. The near tip stress fields show some oscillatory behaviors but without any singularity and the crack faces open completely without any overlapping when remote tensile loading is comparable with remote shear loading. A fracture criterion for predicting interface toughness has been also proposed, which takes into account for the shielding effects of emitted dislocations. The theoretical toughness curve gives excellent prediction, as compared with the existing experiment data. The project supported by the National Natural Science Foundation of China     

Perturbation solutions for non-linear crack problems

Approximate solutions ofJ integrals under plane loadings (modes I and II combined) and antiplane shear loadings (mode III) are obtained for bodies with central through cracks of power hardening materials, by using a perturbation method. The obtained calculating formula is very simple and a comparison with available results shows that the formula enjoys quite good accuracy and is suitable for engineering uses.