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含中心裂纹有限加筋板应力强度因子理论及数值仿真分析 被引量:1

Theoretical Analysis and Numerical Simulation of Stress Intensity Factor for Stiffened Plates with Central Crack
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摘要 基于裂纹问题的复变应力函数、Paris位移公式和变分原理对板材和筋条均含裂纹的加筋板结构的应力强度因子进行了分析求解。对加筋板离散化,忽略受拉时筋、板弯曲的影响,将筋条对裂纹板的作用力转化为作用在板的节点剪力,从而求解了含裂纹加筋板的问题。采用数值仿真方法分析了应力强度因子随板材和加筋条上裂纹扩展的变化规律,研究了加筋条刚度和加筋条间距变化对裂尖处应力强度因子的影响。 The object of this paper is to develop a method to determine the stress intensity factor for ship stiffened plate subjected to correlated cracks in the stiffener and plate elements. The Paris displacement formula, the complex stress function and the variation principle are applied to analyze fracture linear elastic of ship stiffened panels. The bending effect is neglected in the investigation, and it is assumed that the tangential traction along two sides of the cracked plate is converted into sheer force of stiffener, and then the final solution is obtained. At the same time, the stress intensity factor calculated by finite element analysis is analyzed in the paper, accounting for the effect of stiffener's stiffness and spacing changes.
出处 《船舶工程》 北大核心 2015年第4期70-73,共4页 Ship Engineering
基金 中央高校基本科研业务费专项资金资助(2014-zy-019) 国家自然科学基金(51479153)
关键词 加筋板 应力强度因子 Paris位移公式 stiffened plates stress intensity factor Paris displacement factor
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参考文献7

  • 1Poe C. Fatigue Crack Propagation in Stiffened Panels[C]// Damage Tolerance in Aircraft Structures, Am Soc Testing MaterASTM STP 1971, 486: 79-97.
  • 2Isida M. Effect of Width and Length on Stress Intensity Factors under Various Boundary Conditions[J]. International Journal cf Fracture, 1971, 7(3): 301-306.
  • 3Paris P. C. The Growth of Fatigue Cracks Due to Variation in Load[D]. Ph.D.Thesis, Lehigh University, 1972.
  • 4Tada H, Paris E C, Irwin G. R. The Stress Analysis of Cracks Handbook[M]. Hellertown: Del Research Corp., 1973.
  • 5Poe C. The Effect of Riveted and Uniformly Spaced Stringer on the Stress-lntensity of a Cracked Sheet[M]. Virginia Polytechnic Institute, 1969.
  • 6Williams M L. On the Stress Distribution at the Base of a Stationary Crack[J]. Appl Mech, 1957, 24:109- I 13.
  • 7黄维扬.板和型材均含有裂纹的加筋板应力强度因子计算[J].航空学报,1992,13(2). 被引量:1

二级参考文献3

  • 1黄维扬,航空学报,1991年,12卷,2期,B22页
  • 2钱伟长,变分法及有限元.上,1980年
  • 3赵惠元,数学弹性力学的几个基本问题,1958年

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