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。
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.
出处
《航空兵器》
2005年第4期3-5,9,共4页
Aero Weaponry
关键词
非圆截面弹体
动力学特性分析
飞航式导弹
un-rounded cross section airframe
dynamical property analysis
cruise missile
