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Two-Dimensional Orthotropic Plate Analysis for an Integral Thermal Protection System

机译:整体热保护系统的二维正交各向异性板分析

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This paper is concerned with homogenization of a corrugated-core sandwich panel, which is a candidate structure for integrated thermal protection systems for space vehicles. The focus is on determining the local stresses in an integrated thermal protection system panel subjected to mechanical and thermal loads. A micromechanical method is developed to homogenize the sandwich panel as an equivalent orthotropic plate. Mechanical and thermal loads are applied to the equivalent thick plate, and the resulting plate deformations were obtained through a shear deformable plate theory. The two-dimensional plate deformations are used to obtain local integrated thermal protection system stresses through reverse homogenization. In addition, simple beam models are used to obtain local facesheet deformations and stress. The local stresses and deflections computed using the analytical method were compared with those from a detailed finite element analysis of the integrated thermal protection system. For the integrated thermal protection system examples considered in this paper, the maximum error in stresses and deflections is less than 5%. This was true for both mechanical and thermal loads acting on the integrated thermal protection system.
机译:本文涉及瓦楞芯夹心板的均质化,这是航天器集成热保护系统的候选结构。重点是确定承受机械和热负荷的集成热保护系统面板中的局部应力。开发了一种微机械方法来将夹心板均质化为等效的正交各向异性板。将机械载荷和热载荷施加到等效的厚板上,然后通过可剪切变形的板理论获得最终的板变形。二维板变形用于通过反向均化获得局部综合热保护系统应力。另外,简单的梁模型用于获得局部面板变形和应力。使用分析方法计算的局部应力和挠度与集成热保护系统的详细有限元分析中的局部应力和挠度进行了比较。对于本文中考虑的集成热保护系统示例,应力和挠度的最大误差小于5%。对于作用在集成式热保护系统上的机械负载和热负载均是如此。

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