节点文献

碳纳米锥与刚体平面作用的分子动力学模拟

MD simulations on the interaction between carbon nano-cones and rigid plane

  • 推荐 CAJ下载
  • PDF下载
  • 不支持迅雷等下载工具,请取消加速工具后下载。

【作者】 沈海军史友进

【Author】 SHEN Hai-jun SHI You-jin(School of Aeronautics and Astronautics,Nanjing University of Aeronautics and Astronautics, Nanjing 210016,China)

【机构】 南京航空航天大学航空宇航学院南京航空航天大学航空宇航学院 南京210016南京210016

【摘要】 采用Brenner势的分子动力学方法,模拟了47°、69°及93°锥度碳纳米锥与刚体平面压缩、分离的全过程;获得了三种碳纳米锥与刚体平面作用过程中的构形演变、能量-变形曲线以及力-变形曲线;根据模拟结果,分析了它们承载能力以及变形能力的差异.研究表明,47°纳米锥压缩后,锥尖倒向一边,而69°及93°纳米锥锥尖内陷;47°及69°碳纳米锥产生永久变形时的最小压缩量分别为15%和19%左右,而93°碳纳米锥大于38.9%;三种碳纳米锥的最大承受载荷均为29nN左右.

【Abstract】 The Brenner potential based MD (molecular dynamics) simulations are performed to study the compression and detaching between the 47°, 69° and 93° carbon nano-cones and one rigid plane, and the configuration, energy and external-loading evolvement during the compression and detaching are obtained. According to the calculated results, the three nanocones’ compressive properties are compared. The results show that the tip of the compressed 47° cone will fall aside, whereas the ones of the 47° and 69° cones cave in, that the 93° nancone has much higher deformation supporting-capability than the 47° and 69° ones, and that all the three nanocones have the maximal load supporting-capability of 29 nN.

【关键词】 碳纳米锥分子动力学压缩刚体平面
【Key words】 carbon nanoconeMDcompressionrigid plane
【基金】 南航大科研创新基金(05B-013)
  • 【文献出处】 原子与分子物理学报 ,Journal of Atomic and Molecular Physics , 编辑部邮箱 ,2007年05期
  • 【分类号】TB301
  • 【被引频次】6
  • 【下载频次】131
节点文献中: 

本文链接的文献网络图示:

本文的引文网络