| 非圆截面弹体侧向动力学特性分析 |
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| 引用本文： | 赵兴锋,郭鸿武,彭学锋,郑志强. 非圆截面弹体侧向动力学特性分析[J]. 航空兵器, 2005, 0(4): 3-6 |
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| 作者姓名： | 赵兴锋 郭鸿武 彭学锋 郑志强 |
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| 作者单位： | 国防科技大学机电工程与自动化学院,长沙,410073 |
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| 摘 要： | 相对于常见的圆截面弹体的动力学特性分析而言,非圆截面弹体的动力学特性分析有其特殊之处;而对于飞航式导弹其侧向的动力学特性分析方法与一般的弹道式导弹相比较为复杂。本文研究了具有非圆截面弹体和大升阻比气动外形的某类型飞航式导弹的侧向动力学特性,对研究方法进行了尝试,对结果给出了讨论。
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| 关 键 词： | 非圆截面弹体 动力学特性分析 飞航式导弹 |
| 文章编号： | 41-1228(2005)04-0003-03 |
| 修稿时间： | 2005-01-26 |
Lateral Dynamical Property Analysis of Un-rounded Cross Section Airframe |
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| ZHAO Xing-feng,GUO Hong-wu,PENG Xue-feng,ZHENG Zhi-qiang. Lateral Dynamical Property Analysis of Un-rounded Cross Section Airframe[J]. Aero Weaponry, 2005, 0(4): 3-6 |
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| Authors: | ZHAO Xing-feng GUO Hong-wu PENG Xue-feng ZHENG Zhi-qiang |
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| Abstract: | Relative to familiar rounded cross section airframe, the dynamical property analysis of un-rounded cross section airframe has its particularity. Comparing with normal ballistic missile, the lateral dynamical property analysis for cruise missile is more complex. In this paper, the lateral dynamical property of an un-rounded cross section airframe was studied, the research method was attempted, and results were discussed. |
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| Keywords: | un-rounded cross section airframe dynamical property analysis cruise missile |
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