首页> 外文期刊>Aerospace science and technology >A new trigonometric zigzag theory for static analysis of laminated composite and sandwich plates
【24h】

A new trigonometric zigzag theory for static analysis of laminated composite and sandwich plates

机译:三角曲折理论用于层合板和夹层板静力分析

获取原文
获取原文并翻译 | 示例
       

摘要

In this work, a new trigonometric zigzag theory is proposed for the static analysis of laminated composite and sandwich plates. This theory considers shear strain shape function assuming the non-linear distribution of in-plane displacement across the thickness. It satisfies the shear-stress-free boundary conditions at top and bottom surfaces of the plate as well as the continuity of transverse shear stress at the layer interfaces obviating the need of an artificial shear correction factor. An efficient displacement based C~0 finite element model is employed for the accurate assessment of the static behavior of laminated composite and sandwich plates. Some numerical examples covering various features such as different material properties, loading and boundary conditions of cross-ply composite and sandwich composite plates are solved. Efficiency and applicability of the present model is ascertained by validating the evaluated results not only with three-dimensional elasticity solutions but also with the available published results based on other shear deformation theories.
机译:在这项工作中,提出了一种新的三角曲折理论,用于层合复合材料和夹心板的静力分析。该理论假设剪切应变形状函数假设整个厚度内的平面内位移呈非线性分布。它满足了板顶面和底面的无剪切应力边界条件,以及层界面处的横向剪切应力的连续性,从而无需人工剪切校正因子。基于有效位移的C〜0有限元模型被用于精确评估层压复合材料和夹心板的静态性能。解决了一些数值示例,这些示例涵盖了各种特征,例如,不同的材料特性,交叉复合板和夹心复合板的载荷和边界条件。通过不仅使用三维弹性解验证评估结果,而且使用基于其他剪切变形理论的可用公开结果验证评估结果,可以确定本模型的效率和适用性。

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