首页> 外文期刊>Frattura e Integrita Strutturale >Mode I Stress Intensity Factors for triangular corner crack nearby intersecting of cylindrical holes
【24h】

Mode I Stress Intensity Factors for triangular corner crack nearby intersecting of cylindrical holes

机译:圆柱孔相交附近的三角形拐角裂纹的模式I应力强度因子

获取原文
           

摘要

The paper deals with the Stress Intensity Factor assessment of cracks at the intersection of holesloaded by internal pressure.Triangular flaws are considered at the intersection of two holes inside a specific specimen. The researchexamines the influence of hole diameter ratio D1/D2 and the angle between their axes ?. Numerical analysis isperformed to determine the Stress Intensity Factors (SIF) of mode I in many different geometricconfigurations.The actual shape of a real crack nucleated at the intersection of two cylindrical holes is subject to variableinternal pressure and is usually geometrically complex. The Stress Intensity Factor changes along the crackcontour and the crack shape development is controlled by its local value, e.g. during a fatigue loading. Ingeneral, the estimation of the Stress Intensity Factors of cracks with a complex shape is made by means ofnumerical methods since closed form solutions in literature are limited. However, in order to solve the problemof crack propagation more quickly, in the case of a crack corner at the intersection between two cylindricalholes, we can assume, in agreement with scientific literature, a symmetrical triangular crack shape and the StressIntensity Factor are only calculated at the middle of the crack. Obviously, this is a strong approximation, butthis allows a reduction in the computation effort for crack growth rate assessments and safety evaluation.In this paper, the weight function technique is used by integrating the actual stress field evaluated in the uncrackedmodel. The method of the weight function is of general validity and the weight function is related to thedisplacement components close to the crack front, as proposed by Bueckner and Rice. From a computationalpoint of view, the use of the three-dimensional weight function is complex and in scientific literature a weightfunction of general validity is not available. Nevertheless, thanks to the work conducted by Petroski andAchenbach, Shen and Glinka, an efficient generalised weight function has been adopted and then developed bySha and Yang [9], which considers a series expansion of non-singular terms. In this way, the integration of theweight function, multiplied by a nominal stress, is made along a line and not in a two-dimensional domain.In this preliminary work, according to Herz et al., we consider a weight function with three terms by assuming apriori the coefficients of the second and third non-singular terms. This contribution is essentially an extensionof a previous paper by Herz et al. They only considered the case of D1/D2=1 and ?=90° (Di are the diametersof the two cylindrical holes and a is the angle between their axis). Here, we extend the analysis to D1/D2 equalto 2, 4 and 8 with an ? of 60 and 45 degrees.?With the aid of three-dimensional modelling, an accurate FE model of a triangular corner crack at differentcrack depths has been made. Subsequently, by using ANSYS finite element software, it is possible to employ thecommand KCAL that evaluates the Stress Intensity Factors in the middle of the crack. Subsequently, acomparison between numerical FE results and the analytical results, giving the values of the unknowncoefficients of the weight function (the unknown coefficient is indicated in the paper as M1).As reported in the tables, the accuracy of the weight functions in SIF predictions is about 5% despite the strongsimplification previously introduced in the model. This result is considerable because it is possible to determinethe Stress Intensity Factor of a triangular shaped crack by a line integral of a stress profile in a model withoutconsidering the crack.
机译:本文研究了在内部压力作用下的孔的交点处的裂纹的应力强度因子评估,在特定试样内部的两个孔的交点处考虑了三角形缺陷。研究考察了孔径比D1 / D2及其轴线之间的夹角θ的影响。进行数值分析以确定模式I在许多不同几何构型下的应力强度因子(SIF)。在两个圆柱孔相交处成核的实际裂纹的实际形状受可变内部压力的影响,通常在几何上是复杂的。应力强度因子沿裂纹轮廓变化,并且裂纹形状的发展受其局部值控制,例如在疲劳负荷期间。通常,由于文献中封闭形式的解决方案是有限的,因此通过数值方法可以对具有复杂形状的裂纹的应力强度因子进行估算。但是,为了更快地解决裂纹扩展问题,在两个圆柱孔之间的交点处出现裂纹角的情况下,我们可以假定,与科学文献一致,仅在以下位置计算对称的三角形裂纹形状和应力强度因子:裂缝的中间。显然,这是一个很强的近似值,但这可以减少用于裂纹扩展速率评估和安全性评估的计算工作量。本文将加权函数技术与未裂纹模型中评估的实际应力场相结合。如Bueckner和Rice所提出的那样,权重函数的方法具有普遍性,权重函数与靠近裂纹前沿的位移分量有关。从计算的角度来看,三维权重函数的使用很复杂,在科学文献中,一般有效性的权重函数不可用。然而,由于Petroski和Achenbach,Shen和Glinka所做的工作,Sha和Yang [9]采纳了有效的广义权重函数,然后对其进行了开发,该函数考虑了非奇异项的一系列展开。这样,权函数的积分乘以标称应力就沿着一条线而不是在二维域中进行。在这项初步工作中,根据Herz等人的研究,我们考虑了一个具有三个项的权函数通过先验地假定第二和第三非奇异项的系数。这种贡献本质上是Herz等人先前论文的扩展。他们只考虑了D1 / D2 = 1和θ= 90°的情况(Di是两个圆柱孔的直径,a是它们的轴线之间的夹角)。在这里,我们将分析扩展到D1,D2等于2、4和8的?分别具有60度和45度角。借助三维建模,已建立了在不同裂纹深度处的三角形拐角裂纹的精确有限元模型。随后,通过使用ANSYS有限元软件,可以使用命令KCAL评估裂纹中间的应力强度因子。随后,比较数值有限元结果和分析结果,得​​出权重函数的未知系数的值(本文中将未知系数表示为M1)。如表所示,SIF预测中权重函数的准确性尽管先前在模型中引入了极大的简化,但仍为5%。该结果是可观的,因为可以在不考虑裂纹的情况下通过应力分布的线积分确定模型中三角形裂纹的应力强度因子。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号