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。
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.
出处
《导弹与航天运载技术》
北大核心
2005年第5期37-42,共6页
Missiles and Space Vehicles
基金
国防重点攻关项目
关键词
C/E复合材料网格缠绕结构
结构设计
分析
Carbon-epoxy composite trellis wound structure
Structural design
Analysis
