• 主题
高级搜索  >
历史搜索 清空历史
首页> 外文期刊>Composite Structures >Free vibrations of laminated composite shells using the rotation-free plate elements based on Reddy's layerwise discontinuous displacement model
【24h】

Free vibrations of laminated composite shells using the rotation-free plate elements based on Reddy's layerwise discontinuous displacement model

机译：基于雷迪分层不连续位移模型的无旋转板单元的层合复合材料壳体的自由振动

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

The goal of this paper is to develop a computational model for the free vibration analysis of laminated composite shells with embedded delaminations. Laminated composite shells of different shape are modeled using the assembly of layered plate finite elements based on the Generalized Laminated Plate Theory of Reddy. Discontinuities in the displacement field are implemented using the Heaviside step functions. The material is assumed as orthotropic and linearly elastic. The solver is coded in MATLAB. For the generation of models and the visualization of results, GiD Pre/Post Processor is used. After the verification of the proposed model for the intact composite shells using the existing data from the literature, the effect of delamination size on the fundamental frequencies is investigated numerically. A variety of new results for delaminated shells is presented as a benchmark for future investigations. (C) 2015 Elsevier Ltd. All rights reserved.
机译：本文的目的是开发一种计算模型，用于带有分层结构的层合复合材料壳的自由振动分析。基于Reddy的广义层合板理论，使用层合板有限元的装配对不同形状的层合复合壳进行建模。位移字段中的不连续性是通过Heaviside阶跃函数实现的。假定该材料为正交各向异性且线性弹性。求解器是用MATLAB编写的。为了生成模型并可视化结果，使用了GiD前置/后置处理器。在使用文献中的现有数据验证完好复合壳的提议模型后，对分层大小对基频的影响进行了数值研究。脱壳的各种新结果被提出作为未来研究的基准。 （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