| 在轴、外压联合作用下的 C/E复合材料网格缠绕结构的设计与分析 |
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| 引用本文： | 提亚峰,唐国金. 在轴、外压联合作用下的 C/E复合材料网格缠绕结构的设计与分析[J]. 导弹与航天运载技术, 2005, 0(5): 37-42 |
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| 作者姓名： | 提亚峰 唐国金 |
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| 作者单位： | 国防科技大学航天与材料工程学院,长沙,410073;北京宇航系统工程研究所,北京,100076;国防科技大学航天与材料工程学院,长沙,410073 |
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| 摘 要： | 在复合材料网格结构临界轴、外压计算公式的基础上讨论了C/E复合材料网格缠绕结构的设计问题,并在工程中加以应用,取得了较好效果.
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| 关 键 词： | C/E复合材料网格缠绕结构 结构设计 分析 |
| 文章编号： | 1004-7182（2005）05-0037-06 |
| 收稿时间： | 2004-02-18 |
| 修稿时间： | 2004-04-10 |
Design and Analysis of Carbon-Epoxy Composite Trellis Wound Structure under Axial Force Combined with External Pressure |
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| Ti Yafeng,Tang Guojin. Design and Analysis of Carbon-Epoxy Composite Trellis Wound Structure under Axial Force Combined with External Pressure[J]. Missiles and Space Vehicles, 2005, 0(5): 37-42 |
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| Authors: | Ti Yafeng Tang Guojin |
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| Affiliation: | 1. College of Aerospace and Marterial Engineering, National Univ. of Defence Technology, Changsha,410073; 2. Beijing Institute of Astronautical Systems Engineering, Beijing, 100076 |
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| Abstract: | This paper discusses the design of the carbon-epoxy composite trellis wound structure. On the basis of the formulae of buckling load of carbon-epoxy composite trellis wound structure under axial force combined with external pressure, The result of the calculation method has been applied to project design, and it is proved feasible. |
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| Keywords: | Carbon-epoxy composite trellis wound structure Structural design Analysis |
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