弹道修正引信鸭舵空气动力学设计和仿真

Aerodynamic Design and Simulation of Canard for Trajectory Corrected Fuze

在分析了现有弹道修正技术的前提下 ,提出了一种新型的弹道修正技术 ,即鸭舵的空气动力修正技术 ,并且根据空气动力学原理设计了出了一种用于某迫弹弹道修正的鸭舵 ,给出了设计依据及原则 ,最后利用空气动力学仿真软件对设计进行了验证 ,从而证明了设计。

A new concept trajectory correction technology based on canard control is presented in this paper and the design of the canard in accordance with principle of aerodynamics installed on the fuze is implemented.Guide line and priciple of the design of canard for trajectory corrected fuze are also presented,at last performance simulation of the canard with fluent proves the design.