• 主题
高级搜索  >
历史搜索 清空历史
首页> 外文期刊>Composite Structures >On the influence of laminate stacking on buckling of composite cylindrical shells subjected to axial compression
【24h】

On the influence of laminate stacking on buckling of composite cylindrical shells subjected to axial compression

机译：层压板叠合对复合材料圆柱壳轴向压缩屈曲的影响

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 buckling loads of laminated cylinders can strongly depend on the position of the differently oriented layers within the shell. This paper deals with two different laminated orthotropic cylinders with opposite stacking sequence of the laminate layers. Cylinders Of this construction had been thoroughly tested within a BRITE EURAM project. Analytical and semi-analytical methods have Been used to predict the buckling loads. And the results are reported in this paper as well as test results for comparison. An ex- Planation of the striking influence of stacking sequence is given. With some more examples the findings are verified. It is suggested That the presented results can be used for benchmarking purpose.
机译：叠层圆柱体的屈曲载荷可能在很大程度上取决于壳内不同方向的层的位置。本文研究了两种不同的正交各向异性圆柱体，它们的层叠顺序相反。这种结构的气缸已经在BRITE EURAM项目中进行了彻底的测试。分析和半分析方法已用于预测屈曲载荷。并将结果报告在本文中，并将测试结果进行比较。给出了堆叠顺序的显着影响的解释。通过更多示例，可以验证发现。建议提出的结果可用于基准测试。

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