• 主题
高级搜索  >
历史搜索 清空历史
首页> 外文期刊>Journal of the Aeronautical Society of India >FREE VIBRATION BEHAVIOURS OF THICK LAMINATED NON-CIRCULAR CYLINDRICAL SHELLS
【24h】

FREE VIBRATION BEHAVIOURS OF THICK LAMINATED NON-CIRCULAR CYLINDRICAL SHELLS

机译：厚层非圆圆柱壳的自由振动行为

获取原文
获取原文并翻译 | 示例
           
页面导航
  • 摘要
  • 著录项
  • 相似文献
  • 相关主题

摘要

In this paper the free vibration behaviours of thick laminated composite non-circular cylindrical shells are investigated using higher-order theory. The formulation accounts for the variation of the in-plane and transverse displacements through the thickness, abrupt discontinuity in slope of the in-plane displacements at the interfaces, and includes in-plane, rotary inertia terms, and also the inertia contributions due to the coupling between the different order displacement terms. The strain-displacement relations are accurately accounted for in the formulation without neglecting/approximating the (1 +z/R) terms. The solutions are obtained employing finite element procedure. Detailed study is made to highlight the influences of length and thickness ratios, eccentricity parameter, ply-angles and number of layers on the free vibration characteristics of non-circular shells.
机译：本文利用高阶理论研究了厚层状复合非圆形圆柱壳的自由振动行为。该公式考虑了沿厚度方向的平面位移和横向位移的变化，界面处平面位移的斜率的突然不连续性，并且包括平面惯性，旋转惯性项以及由于惯性引起的惯性贡献。不同阶位移项之间的耦合。在不忽略/逼近（1 + z / R）项的情况下，可以精确地计算出应变-位移关系。使用有限元程序获得解。进行了详细的研究，以突出长度和厚度比，偏心率参数，层角和层数对非圆形壳体自由振动特性的影响。

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