导弹转速调节片设计方法研究

A STUDY ON THE DESIGN FOR THE MISSILE ROTATIONAL SPEED ADJUSTMENT BOARDS

本文研究了导弹转速调节片的设计思路与方法。在对其设计思路和设计约束分析基础上 ,通过气动特性计算与转速特性仿真 ,对比研究了转速调节片偏折角度参数、长度参数与数目参数三项设计要素的设计效果 ,得出了其设计方法与步骤。研究结果表明 ,转速调节片的设计是综合弹体结构、气动与总体设计的一项系统工程。

The idea and method of design for the missile rotational speed adjustment boards were studied Based on the results of analysis of the design restrictions, parameters design schemes of the boards were proposed and compared by aerodynamics characteristic calculations and rotational speed simulations The method of design of the boards was finally concluded Study results showed that the design for missile rotational speed adjustment boards is a systematic engineering problem involving missile body structure, aerodynamics, and missile system design