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Effective numerical approach with complete damage transfer under multi-step loading
  • ISSN号:0253-4827
  • 期刊名称:Applied Mathematics and Mechanics (English Edition
  • 时间:2014.3.3
  • 页码:391-402
  • 分类:TB33[一般工业技术—材料科学与工程] TU452[建筑科学—岩土工程;建筑科学—土工工程]
  • 作者机构:[1]School of Aeronautics, Northwest Polytechnical University, Xi'an 710072, P. R. China, [2]Chengdu Aircraft Design and Research Institute, Chengdu 610041, P. R. China
  • 相关基金:Project supported by the National Natural Science Foundation of China (No. 11072202)
  • 相关项目:复合材料热隔膜成型的力学基础研究
中文摘要:

In order to effectively describe the progressively intralaminar and interlaminar damage for composite laminates,a three dimensional progressive damage model for composite laminates to be used for low-velocity impact is presented.Being applied to three-dimensional(3D) solid elements and cohesive elements,the nonhnear damage model can be used to analyze the dynamic performance of composite structure and its failure behavior.For the intralaminar damage,as a function of the energy release rate,the damage model in an exponential function can describe progressive development of the damage.For the interlaminar damage,the damage evolution is described by the framework of the continuum mechanics through cohesive elements.Coding the user subroutine VUMAT of the finite element software ABAQUS/Explicit,the model is applied to an example,i.e.,carbon fiber reinforced epoxy composite laminates under low-velocity impact.It is shown that the prediction of damage and deformation agrees well with the experimental results.

英文摘要:

In order to effectively describe the progressively intralaminar and interlam- inar damage for composite laminates, a three dimensional progressive damage model for composite laminates to be used for low-velocity impact is presented. Being applied to three-dimensional (3D) solid elements and cohesive elements, the nonlinear damage model can be used to analyze the dynamic performance of composite structure and its failure be- havior. For the intralaminar damage, as a function of the energy release rate, the damage model in an exponential function can describe progressive development of the damage. For the interlaminar damage, the damage evolution is described by the framework of the continuum mechanics through cohesive elements. Coding the user subroutine VUMAT of the finite element software ABAQUS/Explicit, the model is applied to an example, i.e., carbon fiber reinforced epoxy composite laminates under low-velocity impact. It is shown that the prediction of damage and deformation agrees well with the experimental results.

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期刊信息
  • 《应用数学和力学:英文版》
  • 主管单位:交通部
  • 主办单位:上海大学
  • 主编:周哲玮
  • 地址:上海市宝山区上大路99号上海大学122信箱
  • 邮编:200444
  • 邮箱:amm@department.shu.edu.cn
  • 电话:021-66135219 66165601
  • 国际标准刊号:ISSN:0253-4827
  • 国内统一刊号:ISSN:31-1650/O1
  • 邮发代号:
  • 获奖情况:
  • 上海市优秀科技期刊一等奖,中国期刊方阵“双效”期刊
  • 国内外数据库收录:
  • 美国数学评论(网络版),波兰哥白尼索引,德国数学文摘,荷兰文摘与引文数据库,美国工程索引,美国科学引文索引(扩展库),英国科学文摘数据库,日本日本科学技术振兴机构数据库,美国应用力学评论
  • 被引量:541