期刊文献+

Three dimensional K-Tz stress fields around the embedded center elliptical crack front in elastic plates 被引量:2

Three dimensional K-Tz stress fields around the embedded center elliptical crack front in elastic plates
下载PDF
导出
摘要 Through detailed three-dimensional (3D) finite element (FE) calculations, the out-of-plane constraints Tz along embedded center-elliptical cracks in mode I elastic plates are studied. The distributions of Tz are obtained near the crack front with aspect ratios (a/c) of 0.2, 0.4, 0.5, 0.6, 0.8 and 1.0. Tz decreases from an approximate value of Poisson ratio v at the crack tip to zero with increasing normalized radial distances (r/a) in the normal plane of the crack front line, and increases gradually when the elliptical parameter angle φ changes from 0° to 90°at the same r/a. With a/c rising to 1.0, Tz is getting nearly independent of φ and is only related to r/a. Based on the present FE calculations for Tz, empirical formulas for Tz are obtained to describe the 3D distribution of Tz for embedded center-elliptical cracks using the least squares method in the range of 0.2 ≤ a/c ≤ 1.0. These Tz results together with the corresponding stress intensity factor K are well suitable for the analysis of the 3D embedded centerelliptical crack from field, and a two-parameter K-Tz principle is proposed. Through detailed three-dimensional (3D) finite element (FE) calculations, the out-of-plane constraints Tz along embedded center-elliptical cracks in mode I elastic plates are studied. The distributions of Tz are obtained near the crack front with aspect ratios (a/c) of 0.2, 0.4, 0.5, 0.6, 0.8 and 1.0. Tz decreases from an approximate value of Poisson ratio v at the crack tip to zero with increasing normalized radial distances (r/a) in the normal plane of the crack front line, and increases gradually when the elliptical parameter angle φ changes from 0° to 90°at the same r/a. With a/c rising to 1.0, Tz is getting nearly independent of φ and is only related to r/a. Based on the present FE calculations for Tz, empirical formulas for Tz are obtained to describe the 3D distribution of Tz for embedded center-elliptical cracks using the least squares method in the range of 0.2 ≤ a/c ≤ 1.0. These Tz results together with the corresponding stress intensity factor K are well suitable for the analysis of the 3D embedded centerelliptical crack from field, and a two-parameter K-Tz principle is proposed.
出处 《Acta Mechanica Sinica》 SCIE EI CAS CSCD 2006年第2期148-155,共8页 力学学报(英文版)
基金 The project supported by the National Natural Science Foundation of China (50275073)
关键词 Three-dimensional finite element Out-of-plane constraint Tz Embedded elliptical crack Stress intensity factor T-STRESS Stress field Three-dimensional finite element Out-of-plane constraint Tz Embedded elliptical crack Stress intensity factor T-Stress Stress field
  • 相关文献

参考文献1

二级参考文献4

共引文献4

同被引文献96

  • 1郭万林.航空结构损伤容限设计中的三维问题[J].航空学报,1995,16(2):129-136. 被引量:17
  • 2Broek D, Schijve J. The effect of sheet thickness on the fatigue crack propagation in 2024-T3 alclad sheet material, NLR Report No. TR-M2129, National Aero and Astronautical Research Institute, 1963.
  • 3Broek D, Schijve J. The influence of sheet thickness on crack propagation [ J ]. Aircraft Engineering, 1966, 38: 31-33.
  • 4Mills W J, Hertzberg R W, The effect of thickness on fatigue crack retardation in 2024-T3 aluminum alloy[J]. Engineering Fracture Mechanics, 1975, 7: 705-711.
  • 5Ting T C T, Anisotropic Elasticity:Theory and Applieations [ M ]. York New: Oxford University Press, 1996.
  • 6Rigby R H. Aliabadi M H. Decomposition of the mixed-mode J-integral revised[J]. International Journal of Solids and Structures, 1998.35: 2073-2099.
  • 7She C, Zhao J, Guo W. Three dimensional stress fields near notches and cracks[J]. International Journal of Fatigue. 2008. 151:151-160.
  • 8Pitt S D, Jones R. Compliance measurements for assessing structural integrity [J]. Engineering Failure Analysis, 2001, 8:371-397.
  • 9Paris P. Gomez M, Anderson W. A rational analytic theory of fatigue[J]. Trend Engineering,1961,13: 9- 14.
  • 10Elber W. Fatigue crack closure under cyclic tension [J]. Engineering Fracture Mechanics, 1970, 2: 37-45.

引证文献2

二级引证文献24

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部