期刊文献+

无限大板圆孔边双裂纹的裂纹面位移权函数解 被引量:5

Weight Function Solutions of Crack Surface Displacements for Double Cracks Emanating from a Circular Hole in an Infinite Plate
原文传递
导出
摘要 针对飞机结构中常见的孔边裂纹问题,结合塑性诱发的疲劳裂纹闭合分析需求,利用权函数封闭解法计算了无限大板圆孔边双裂纹在远方拉伸和部分裂纹面均布应力两种载荷条件下的裂纹面位移。研究表明,权函数法是一种强有力的计算任意载荷条件下裂纹面位移的高效、高精度方法。通过对权函数法计算结果的合理拟合,得到了两种载荷条件下裂纹面位移的高精度解析表达式,从而为无限大板圆孔边双裂纹的裂纹闭合分析和张开应力求解提供了高效、高精度的手段。 This paper is aimed at crack surface displacement solutions for cracks at a circular hote, which is a common crack configuration in aircraft structures. The weight function method is used for calculating crack surface displacements for double cracks under both remote uniform tension and partial crack surface uniform segment loading. It is found that the weight function method is a very efficient and highly accurate method for calculating crack surface displacements under arbitrary load conditions. By rational curve fitting to the results obtained from the weight function method, accurate analytical expressions for crack surface displacements for the two load cases are developed. The present study provides an efficient and accurate means for crack closure and crack opening stress analysis for double cracks emanating from a circular hole in an infinite plate.
出处 《航空学报》 EI CAS CSCD 北大核心 2013年第10期2341-2348,共8页 Acta Aeronautica et Astronautica Sinica
关键词 孔边裂纹 裂纹面位移 条带屈服模型 权函数法 裂纹面位移方程 crack at a circular hole crack surface displacement strip-yield model weight function method crack surface displacement equation
  • 相关文献

参考文献15

  • 1Newman J C, Jr. A crack-closure model for predicting fa- tigue crack growth under aircraft spectrum loading. ASTM STP 748, 1981: 53-84.
  • 2Budiansky B, Hutchinson J W. Analysis of closure in fa- tigue crack growth. Journal of Applied Mechanics, 1978, 45(2) : 267 -276.
  • 3Kim J H, Lee S B. Fatigue crack opening stress based on the strip-yield model. Theoretical and Applied Fracture Mechanics, 2000, 34(1): 73-84.
  • 4Liu J Z, Wu X R. Study on fatigue crack closure behavior for various cracked geometries. Engineering Fracture Me- chanics, 1997, 57(5): 475-491.
  • 5Ziegler B, Yamada Y, Newman J C, Jr. Application of a strip-yield model to predict crack growth under variable- amplitude and spectrum loading, Part 2.- middle-crack-ten- sion specimens. Engineering Fracture Mechanics, 2011, 78(14) : 2609-2619.
  • 6Wu X R, Zhao W. Dugdale model solution for compact specimen. Mechanical Behaviour of Materials: V, 1988: 243-248.
  • 7Wang G S, Blom A F. A strip model for fatigue crack growth predictions under general load conditions. Engi- neering Fracture Mechanics, 1991, 40(3).. 507-533.
  • 8Yamada Y, Ziegler B, Newman J C, Jr. Application of a strip-yield model to predict crack growth under variable- amplitude and spectrum loading, Part 1: compact speci- mens. Engineering Fracture Mechanics, 2011, 78 (14) : 2597-2608.
  • 9Mall S, Newman J C, Jr. The Dugdale model for compact specimen. ASTM STP. 868, 1985: 113-1:78.
  • 10Newman J C, Jr. A nonlinear fracture mechanics approach to the growth of small cracks. In: Zocher H. Behaviour of Short Cracks in Airframe Materials. AGARD CP, 1983, 328:61 -626.

同被引文献37

引证文献5

二级引证文献22

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