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复合材料夹
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  composite sandwich
     Free Vibration of Composite Sandwich Plates Based on Zig-Zag Deformation Assumption
     基于Zig-Zag变形假定的复合材料夹层板的自由振动
短句来源
     Vibration Analysis of Composite Sandwich Shells
     复合材料夹芯壳的振动分析
短句来源
     The Theory of Composite Sandwich Box Beam
     复合材料夹芯箱梁理论
短句来源
     An eight-node isoparametric element of composite sandwich plates using Reissner Theory was developed,which provides a relative simple finite element method.
     本文用Reissner理论构造了一种八节点等参单元, 对于表层较薄、夹芯剪切模量较大的复合材料夹层板, 提供了一种相对简单的有限元计算方法。
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     Numerical analysis of residual compressive strength of damaged composite sandwich plates
     含损伤复合材料夹层板剩余压缩强度数值分析
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  “复合材料夹”译为未确定词的双语例句
     Namely the confectioning of the core skeleton structure and the face sheets is synchronal, and between the core’s skeleton structure and the face sheets do not have the interface.
     因此所设计和研制的夹芯结构与其他复合材料夹芯板的根本区别就是面板与芯材骨骼结构之间没有界面,这就从根本上改善了面板与芯材之间粘接性能薄弱问题。
短句来源
     AN EQUIVALENT ANALYSIS METHOD FOR SANDWICH SHELLS OF COMPOSITE MATERIALS
     复合材料夹层板壳一种等效分析方法
短句来源
     The typical 3-D integrated and sandwiched fabrics including X,V and honeycomb types in warp wise are designed and manufactured with glass fibers on the common 2-D loom,and reinforced composites are made of the fabrics by means of the technology of vacuum assisted resin infusion.
     用玻璃纤维在普通二维织机上分别试制经向为V形、X形和蜂窝形3种典型三维整体夹芯织物,利用真空辅助成型工艺研制复合材料夹芯板。
短句来源
     Vibration and Damping Analysis of Fibre Reinforced Composite Material Sandwich Plates
     复合材料夹层板的振动及阻尼分析
短句来源
     The element model DOM number for the laminated plate such as the vehicle body established by linear layer element is less 66% than by four nodes plane element, the calculation errors are below 2.74%.
     对于车厢这类复合材料夹层板结构,采用复合材料层状立体单元建模与传统上使用的四节点板单元相比单元自由度数目减少66%以上,大大提高了计算效率,计算误差不超过2.74%。
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  相似匹配句对
     A STUDY OF FORMABILITY OF COMPOSITE LAMINATES SHEET METALS
     复合材料层板成形性的研究
短句来源
     Plastic Buckling of Composite Sandwich Plates
     复合材料层板的塑性屈曲
短句来源
     Non-Destructive Testing on the Composite Material
     复合材料无损检测
短句来源
     Composite Material on Modern Aircraft
     客机上的复合材料
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  composite sandwich
Vibration characteristics of composite sandwich plates and layup optimization of their laminated FRP composite faces
      
This paper examines the vibration characteristics of rectangular, symmetric composite sandwich plates and the layup optimization of their top and bottom laminated FRP composite faces.
      
First, the fundamental frequency of the composite sandwich plate is discussed in the subspace of four in-plane lamination parameters of the laminated FRP composite face.
      
Optimization of nonhomogeneous facesheets in composite sandwich plates
      
The optimal design of composite sandwich plates in which the facesheets are composed of a carbon fiber/epoxy net is considered.
      
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This article to reviews the progress achieved in the study of damage behavior of composite sandwich plates after low velocity impact. Emphasis is placed on the residual tensile and/or compressive strength of the damaged sandwich plates in composite engineering structures. The contents of the article are as follows:(1) Analysis theory, model and corresponding finite element method of the composite sandwich.(2) Damage and failure configurations and classifications for the composite sandwich plates.(3) Residual...

This article to reviews the progress achieved in the study of damage behavior of composite sandwich plates after low velocity impact. Emphasis is placed on the residual tensile and/or compressive strength of the damaged sandwich plates in composite engineering structures. The contents of the article are as follows:(1) Analysis theory, model and corresponding finite element method of the composite sandwich.(2) Damage and failure configurations and classifications for the composite sandwich plates.(3) Residual tensile strength.(4) Residual compressive strength.(5) Related problems and perspective for developing new analysis methods. There are 90 recent references included in this article.

摘 要 综述了受低速冲击后复合材料夹层板的损伤性态研究进展,重点介绍了倍受复合材料工程结构设计师所关注的受损复合材料夹层板的剩余拉/压强度.主要内容为:m复合材料夹层板损伤特征;(2)剩余拉伸强度;(3)剩余压缩强度;闪相关问题的讨论与研究展望.

 
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