首页> 外文会议>Virtual European Conference on Fracture >Stress intensity factors Ki, Kn, Km, K_(eq), induced at the crack tip of CT specimens subjected to torsional loading
【24h】

Stress intensity factors Ki, Kn, Km, K_(eq), induced at the crack tip of CT specimens subjected to torsional loading

机译:应力强度因子ki,kn,km,k_(eq),在CT标本的裂纹尖端诱导扭转载荷

获取原文

摘要

The paper herein presented shows the Stress Intensity Factors (SIF), K_I, KII, K_(III), and K_(eq), calculated for Compact Tension (CT) specimens with different thicknesses (B), namely 2.5 mm; 3 mm; 5 mm; 7.5 mm, and 10 mm, that were subjected to three torsional loads (T): 6 N. m; 7.5 N. m; 9 N. m. Fatigue pre-crack subjected to torsional loading was found to be predominantly under Mode-II loading, and a crack branch was observed. The CT specimens, which were analysed using the Finite Element Method (FEM), were then modelled with two cracks that had grown experimentally from a fatigue pre-crack along two directions (+70° and -70°), and for several crack lengths (a/L=0; a/L=0.25; a/L=0.50; a/L=0.75; a/L=1.0). Therefore, equivalent SIF, K_(eq), were calculated from the numerical results of K_I, K_(II), and Km, and a polynomial regression function was determined in function of the thickness of the specimen (B), the crack length (a/L) and the applied torque (T). It was observed that even in the case of a Mode-III loading is applied, Mode I was locally dominant at the branched crack tip, followed by Mode III and Mode II, in that order of relevance. It was also observed that the maximum equivalent SIF occurred at the two outer lateral surfaces of the CT specimens under test, resulting in high crack growth rates in those locations, and minimum at the midplane of the specimen.
机译:本文提出的本文显示了针对具有不同厚度(B)的紧凑张力(CT)样本计算的应力强度因子(SIF),K_I,KII,K_(III)和K_(等式),即2.5mm; 3毫米; 5毫米; 7.5毫米和10毫米,经受三个扭转载荷(T):6 N.M; 7.5 N.M; 9 n. m。发现扭转载荷的疲劳预裂纹主要在模式-II-II负载下主要是在载荷下,并且观察到裂缝分支。然后使用有限元法(FEM)分析的CT样本,然后用两个裂缝模拟,该裂缝从沿两个方向(+ 70°和-70°)和几个裂缝长度从疲劳前裂缝进行实验生长(a / l = 0; a / l = 0.25; a / l = 0.50; a / l = 0.75; a / l = 1.0)。因此,从K_I,K_(II)和KM的数值结果计算等效SIF,K_(EQ),并且在样本(B)的厚度的功能中确定多项式回归函数,裂缝长度( a / l)和施加的扭矩(t)。观察到,即使在应用模式-III载荷的情况下,即使在施加模式-III载荷时,也可以在分支裂纹尖端处局部地显着,然后是模式III和模式II,以这种相关性。还观察到,在被测CT样本的两个外侧表面发生的最大当量SIF,在这些位置处产生高裂纹的生长速率,并在样本的中间板处的最小值。

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