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Analysis and optimum design of composite grid structures.

机译:复合网格结构的分析与优化设计。

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摘要

As composite grid structures with unidirectional fibers appear to be a promising concept, an integrated equivalent stiffness model is developed to describe a composite grid structure with or without laminated skins. No extra degree of freedom is introduced to include the in-plane bending and shear of ribs so that Mindlin's plate theory can still be adopted. As a result, the model can be directly incorporated with the existing FEM technique. The model proves to be very accurate for displacements and reasonably accurate for strains or stresses. If high precision is required, the equivalent stiffness model can be incorporated with exact FEM modeling to obtain a refined stress analysis. The proposed model is demonstrated to be rather simple and efficient, especially for dynamic analysis. Hygrothermal behavior and local buckling are also taken into account.; With the equivalent stiffness model as a tool, the performance of composite grid structures compared to traditional laminates, sandwich plates and metal grid structures is clearly demonstrated. Composite grid structures possess several unique properties coming from the combination of the grid configuration and unidirectional fibers. They have excellent strength, flexural stiffness, damage tolerance and low hygrothermal expansion coefficients.; As the equivalent stiffness model provides the basis of analysis, a method of optimum design is established to design a composite grid structure with or without laminated skins. Multiple loads and multiple failure modes are considered. Discrete design is also included. Furthermore, it can be easily incorporated with the FEM to perform structural optimization. The optimization code is demonstrated to be a very powerful design tool.; Finally, a user-friendly computer code is developed to perform the above tasks.
机译:由于具有单向纤维的复合网格结构似乎是一个有前途的概念,因此开发了一个集成的等效刚度模型来描述带有或不带有层压蒙皮的复合网格结构。没有引入额外的自由度来包括肋的平面内弯曲和剪切,因此Mindlin的板理论仍然可以采用。结果,该模型可以直接与现有的FEM技术结合。该模型被证明对位移非常准确,对应变或应力也相当准确。如果需要高精度,则可以将等效刚度模型与精确的FEM建模合并,以获得精确的应力分析。所提出的模型被证明是相当简单和有效的,特别是对于动态分析。还考虑了湿热行为和局部屈曲。使用等效刚度模型作为工具,与传统的层压板,夹心板和金属网格结构相比,复合网格结构的性能得到了明显证明。复合网格结构具有几种独特的属性,这些属性来自网格配置和单向纤维的组合。它们具有优异的强度,抗弯刚度,破坏耐受性和低湿热膨胀系数。由于等效刚度模型提供了分析的基础,因此建立了一种最佳设计方法来设计带有或不带有层压蒙皮的复合网格结构。考虑了多种载荷和多种失效模式。离散设计也包括在内。此外,它可以很容易地与FEM合并以执行结构优化。优化代码被证明是一个非常强大的设计工具。最后,开发了一种用户友好的计算机代码来执行上述任务。

著录项

  • 作者

    Chen, Hong-Ji.;

  • 作者单位

    Stanford University.;

  • 授予单位 Stanford University.;
  • 学科 Engineering Aerospace.
  • 学位 Ph.D.
  • 年度 1995
  • 页码 147 p.
  • 总页数 147
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 航空、航天技术的研究与探索;
  • 关键词

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