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碳管纳米弹簧快速建模与压缩特性有限元分析
引用本文:刘根林,沈海军.碳管纳米弹簧快速建模与压缩特性有限元分析[J].盐城工学院学报(自然科学版),2008,21(1):16-20.
作者姓名:刘根林  沈海军
作者单位:1. 盐城工学院基础科学部,江苏,盐城,224051
2. 南京航空航天大学,航空宇航学院,江苏,南京,210016
摘    要:给出了ANSYS有限元软件中碳管纳米弹簧的快速建模方法,对碳管纳米弹簧的轴向压缩进行了大变形有限元分析。为验证该方法与结果的有效性,还将一碳管纳米弹簧压缩刚度、临界失稳载荷的计算值与相应的试验结果、解析解进行了比较。研究表明,有限元结果与试验结果、解析解均较为接近,这说明碳管纳米弹簧的压缩特性分析是有效的;此外还发现,典型微米长度的碳管纳米弹簧的轴向压缩刚度为nN/nm量级,压缩失稳临界载荷为几十nN。

关 键 词:碳管纳米弹簧  有限元  建模  压缩特性
文章编号:1671-5322(2008)01-0016-05
修稿时间:2007年12月10

Rapid Modeling of Carbon-tube Nanospring and Analyzing its Compressive Properties by Finite Element Method
LIU Gen-lin,SHEN Hai-jun.Rapid Modeling of Carbon-tube Nanospring and Analyzing its Compressive Properties by Finite Element Method[J].Journal of Yancheng Institute of Technology(Natural Science Edition),2008,21(1):16-20.
Authors:LIU Gen-lin  SHEN Hai-jun
Institution:LIU Gen-lin,SHEN Hai-jun(1.Department of Basic Science of Yancheng Institute of Technology,Jiangsu Yancheng 224051,China;2.School of Aeronautics and Astronautics,Nanjing University of Aeronautics and Astronautics,Jiangsu Nanjing 210016,China)
Abstract:One rapid-modeling method of carbon-tube nanospring (CTNS) was given for the FE(finite-element) software environment of ANSYS,and the axial-compression of one CTNS was simulated by using large-deformation FE method.In order to verify the FE analyses,the present FE results of the compressive stiffness and critical load for the disability of the CTNS were compared with the corresponding experimental and analytic ones.It is found that the present FE results are very close to both the experimental and analytic ones,which implies the effectivity of the present FE analyses for the compressed CTNS.In addition,it is observed that the micron-length CTNS has the compressive stiffness of several nN/nm,and the critical load of decades of nN.
Keywords:carbon-tube nanospring  finite-element  modeling  compressive properties
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