| 飞航式导弹翼面优化设计 |
| |
| 引用本文： | 周福生. 飞航式导弹翼面优化设计[J]. 战术导弹技术, 1990, 0(3): 18-26 |
| |
| 作者姓名： | 周福生 |
| |
| 作者单位： | 航空航天部三院三部 |
| |
| 摘 要： | 本文针对飞航式导弹翼面的特点,对翼面结构进行优化设计计算,其中包括结构布局优化和受力构件截面尺寸优化。探讨了各种设计参数及材料特性对优化设计结果的影响,经过对几十种设计结果的分析、对比,找到一种最优的设计结果。
|
| 关 键 词： | 导弹 翼面 优化设计 有限元法 |
OPTIMUM DESIGN FOR CRUISE MISSILE WINGS |
| |
| Zhou Fusheng Third Academy of MAS. OPTIMUM DESIGN FOR CRUISE MISSILE WINGS[J]. Tactical Missile Technology, 1990, 0(3): 18-26 |
| |
| Authors: | Zhou Fusheng Third Academy of MAS |
| |
| Affiliation: | Zhou Fusheng Third Academy of MAS |
| |
| Abstract: | The Optimum design and calculation for the wings of cruise missile have been carried out, in which the optimization of structure layout and section dimensions of stressed frame is included. The innuence of various design parameters and material characteristics upon the optimum design results has been found through analysing and comparing dozens of design. |
| |
| Keywords: | Optimization Design Finite-element method Missile Wing surface |
| 本文献已被 CNKI 维普 等数据库收录！ |
