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正交各向异性复合材料圆柱壳轴对称大变形解析

Axisymmetrical Large Deformation Analysis of Orthotropic Laminated Composite Cylindrical Shells

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【作者】 郭明

【Author】 Guo Ming(The 41st Institute of the Fourth Academy of CASC, Xi’an, 710025)

【机构】 中国航天工业总公司四院四十一所!西安710025

【摘要】 按照考虑横向剪切变形的大挠度理论,研究了在轴对称法向载荷和均匀轴向载荷作用下,正交各向异性复合材料圆柱壳的轴对称大变形问题。得到了边界条件为固支和简支时,有限长圆柱壳的解析解。文中还给出了碳纤维/环氧复合材料圆柱壳的算例,说明了边界条件的影响。

【Abstract】 The axisymmetrical large deformation problems of orthotropic laminated composite cylindricalshells subjected to axisymmetrical radial pressure and uniform axial loading are investigated on the basis of thegeometrically nonlinear theory. Closed-form solutions of finite length laminated cylindrical shells are obtained for a given set of boundary conditions at the edges. Numerical examples for the shells made of carbon fiber/epoxy resin composite materials are presented and the effects of boundary conditions are illustrated.

  • 【文献出处】 固体火箭技术 ,JOURNAL OF SOLID ROCKET TECHNOLOGY , 编辑部邮箱 ,1997年02期
  • 【分类号】TB33
  • 【被引频次】7
  • 【下载频次】136
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