| 某型导弹弹翼静力分析的一种数学模型 |
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| 引用本文： | 姚志敏,王竹林,谷宏强. 某型导弹弹翼静力分析的一种数学模型[J]. 军械工程学院学报, 1998, 0(3) |
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| 作者姓名： | 姚志敏 王竹林 谷宏强 |
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| 作者单位： | 军械工程学院导弹工程教研室，军械工程学院导弹工程教研室，军械工程学院导弹工程教研室 石家庄 050003，石家庄 050003，石家庄 050003 |
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| 摘 要： | 应用有限元方法,建立了变厚度薄板三角形单元刚度矩阵,给出了变厚度薄板三角形单元形心上的应力和位移计算的数学模型。通过对某型反坦克导弹弹翼进行静力分析和实验比较,表明采用这种模型进行分析合乎结构设计精度要求。
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| 关 键 词： | 变厚度薄板 弹翼 三角形单元 刚度矩阵 |
A MATHEMATIC MODEL FOR THE STATIC FORCE ANALYSIS OF A MISSILE WING |
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| Yao Zhimin Wang Zhulin Gu Hongqiang. A MATHEMATIC MODEL FOR THE STATIC FORCE ANALYSIS OF A MISSILE WING[J]. Journal of Ordnance Engineering College, 1998, 0(3) |
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| Authors: | Yao Zhimin Wang Zhulin Gu Hongqiang |
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| Affiliation: | Teaching and Research Section of Missile Engineering |
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| Abstract: | By using the method of limited unit , we build up the stiffness matrix of triangular unit of the light gauge sheet of variable thickness and produce the mathematic model for the computation of the stress and displacement at the center of the triangular unit.. Through the analysis of the static force of a missile wing and experimental comparison, we find out that the demand of the structural design accuracy can be met by using this model. |
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| Keywords: | light gauge sheet of variable thickness wings of a missile triangular unit stiffness matrix |
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