...
首页> 外文期刊>Composite Structures >On the postbuckling behavior of geometrically imperfect cylindrical nanoshells subjected to radial compression including surface stress effects
【24h】

On the postbuckling behavior of geometrically imperfect cylindrical nanoshells subjected to radial compression including surface stress effects

机译:关于几何不完美的圆柱纳米壳在包括表面应力效应的径向压缩下的后屈曲行为

获取原文
获取原文并翻译 | 示例

摘要

The main objective of the present study is to investigate the effect of surface stress on the nonlinear buckling and postbuckling behavior of cylindrical nanoshells with initial geometric imperfection subjected to radial compressive load. Gurtin-Murdoch elasticity theory is implemented into the classical shell theory to develop a size-dependent shell model which is capable to capture surface stress effects efficiently. In order to satisfy balance conditions on the surfaces of nanoshell, a linear variation through the thickness is considered for the normal stress component of the bulk. The principle of virtual work is put to use in order to formulate the non-classical governing differential equations. Afterwards, a boundary layer theory is employed including the nonlinear prebuckling deformations, initial geometric imperfection and large postbuckling deflections. Finally, a two-stepped singular perturbation methodology is utilized to obtain the size-dependent critical buckling loads and the postbuckling equilibrium paths of imperfect nanoshells corresponding to both lateral and hydrostatic pressure loading cases. It is found that for the positive and negative values of surface elastic constants, the both critical buckling load and critical end-shortening of nanoshell increase and decrease, respectively. (C) 2015 Elsevier Ltd. All rights reserved.
机译:本研究的主要目的是研究表面应力对具有径向压缩载荷的初始几何缺陷的圆柱纳米壳的非线性屈曲和后屈曲行为的影响。 Gurtin-Murdoch弹性理论被应用到经典的壳理论中,以开发尺寸相关的壳模型,该模型能够有效地捕获表面应力效应。为了满足纳米壳表面上的平衡条件,对于块体的法向应力分量,考虑通过厚度的线性变化。运用虚功原理来制定非经典的控制微分方程。之后,采用边界层理论,包括非线性预屈曲变形,初始几何缺陷和较大的后屈曲挠度。最后,采用两步奇异摄动方法获得了尺寸依赖性的临界屈曲载荷和不完善的纳米壳的屈曲后平衡路径,分别对应于横向和静水压力载荷情况。发现,对于表面弹性常数的正值和负值,纳米壳的临界屈曲载荷和临界端部缩短分别增加和减少。 (C)2015 Elsevier Ltd.保留所有权利。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号