复合型裂纹应变能释放率逐点闭合的外推逼近研究

郭茂林; 孟庆元; 王彪

复合型裂纹应变能释放率逐点闭合的外推逼近研究

哈尔滨工业大学航天工程与力学系, 哈尔滨 150001

详细信息

作者简介:
郭茂林(1943- ),男,河北阳原人,教授,从事复合材料断裂力学研究(E-mail:hitgml@eyou.com).

中图分类号: O39;TB12
计量
- 文章访问数: 2563
- HTML全文浏览量: 147
- PDF下载量: 506
- 被引次数: 0
出版历程
- 收稿日期: 2001-12-21
- 修回日期: 2003-01-14
- 刊出日期: 2003-04-15

Research for the Strain Energy Release Rate of Complex Cracks by Using Point-by-Point Closed Extrapolation Approach

Department of Astronautics and Mechanics, P.O. Box 344, Harbin Institute of Technology, Harbin 150001, P. R. China

摘要

摘要: 提出用外推逼近法计算复合型裂纹的应变能量释放率的新方法,闭合能计算时,采用逐点闭合的方法。避免了某些文献中闭合能计算不能自治的缺点:"当沿经向闭合节点多于两个时,裂纹(脱层)前端节点力乘位移已计算了闭合能,中间点还要重复计算闭合能"。具体计算了DCB(双悬臂梁)试件并与理论解进行了比较,吻合度优于其他方法。同时,又计算了紧凑拉伸试件、三点弯曲试件、单边裂纹试件,均取得满意结果。与理论解比较,误差可控制在1%之内。此方法可以广泛用于类似复合材料脱层裂纹的断裂力学分析。
- 外推逼近 /
- 逐点闭合 /
- 复合型裂纹 /
- 应变能释放率
Abstract: A new extrapolation approach was proposed to calculate the strain energy release rates of complex cracks. The point-by-point closed method was used to calculate the closed energy, thus the disadvantage of self-inconsistency in some published papers can be avoided.The disadvantage is that the closed energy is repeatedly calculated: when closed nodal number along radial direction is more than two,the displacement of nodes behind the crack tip that is multiplied by nodal forces,the closed energy has been calculated and the crack surfaces have been closed, and that closed energy of middle point is calculated repeatedly.A DCB(double cantilever beam) specimen was calculated and compared with other theoretical results,it is shown that a better coincidence is obtained.In addition the same resalts are also obtained for compact tension specimen, three point bend specimen and single edge cracked specimen.ln comparison with theoretical results,the error can be limited within 1 per cent.This method can be extended to analyze the fiacture of composite laminates with various delamination cracks.
- extrapolation approach /
- point-by-point close /
- complex crack /
- strain energy release rate

HTML全文

参考文献(8)

[1]	Kardestuncer H.Finite Element Handbook[M].New York:McGraw-Hill Book Company,1987.
[2]	Rybicki E F,Kanninen M F.A finite element calculation of stress intensity factors by modified crack closure integral[J].Engineering Fracture Mechanics,1977,9(4):931-938.
[3]	de Moura M F S F,Goncalves J P M,Marques A T,et al.Modeling compression failure after low velocity impact on laminated composites using interface elements[J].J Composites Materials,1997,31(15):1462-1479.
[4]	Whitcomb J D.Three dimensional analysis of a posthuckled embedded delimitation[J].J Composite Materials,1989,23(9):862-887.
[5]	Mukher Jee Y X.A numerical and experimental study of delaminated layered composites[J].J Composite Materials,1994,28(9):837-870.
[6]	LU Xian-qiang,LIU Dah-sin.Finite element analysis of strain energy release rate at delamination front[J].Journal of Reinforced Plastics and Composites,1991,10(5):179-292.
[7]	张德兴.有限元素法新编教程[M].上海:同济大学出版社,1989.
[8]	杜善义,王彪.复合材料细观力学[M].北京:科学出版社,1998.