首页> 外文期刊>International Journal of Computational Materials Science and Engineering >Nonlinear buckling of orthogonal carbon nanotube-reinforced composite cylindrical shells under axial compression surrounded by elastic foundation in thermal environment
【24h】

Nonlinear buckling of orthogonal carbon nanotube-reinforced composite cylindrical shells under axial compression surrounded by elastic foundation in thermal environment

机译:热环境中正交碳纳米管增强复合圆柱壳在轴向压缩下弹性基础的非线性屈曲

获取原文
获取原文并翻译 | 示例

摘要

Nonlinear buckling and postbuckling of orthogonal carbon nanotube-reinforced composite (Orthogonal CNTRC) cylindrical shells subjected to axial compression in thermal environments surrounded by elastic foundation are presented in this paper. Two layers of shell are reinforced by carbon nanotube (CNT) in two orthogonal directions (longitudinal and circumferential directions). Based on Donnell's shell theory with von Karman's nonlinearity and the Galerkin method, the governing equations are established to obtain the critical buckling loads and postbuckling load-deflection curves. The large effects of CNT volume fraction, temperature change, elastic foundation and geometrical parameters of cylindrical shells on the buckling load and postbuckling behavior of Orthogonal CNTRC cylindrical shells are obtained.
机译:提出了在弹性基础包围的热环境下,正交碳纳米管增强复合材料圆柱壳的非线性屈曲和后屈曲。碳纳米管(CNT)在两个正交方向(纵向和圆周方向)上增强了两层外壳。基于Donnell的壳理论和von Karman的非线性以及Galerkin方法,建立了控制方程,以获得临界屈曲载荷和后屈曲载荷-挠度曲线。获得了圆柱壳的CNT体积分数,温度变化,弹性基础和几何参数对正交CNTRC圆柱壳的屈曲载荷和后屈曲行为的巨大影响。

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