机载导弹导轨式发射过程安全性分析

陈全龙;韩景龙;员海玮

振动与冲击 ›› 2013, Vol. 32 ›› Issue (20) : 41-47.

PDF(2342 KB)
PDF(2342 KB)
振动与冲击 ›› 2013, Vol. 32 ›› Issue (20) : 41-47.
论文

机载导弹导轨式发射过程安全性分析

  • 陈全龙,韩景龙,员海玮
作者信息 +

Security Analysis of Missile Rail Launching from Aircraft

  • CHEN Quan-Long HAN Jing-Long YUN Hai-Wei
Author information +
文章历史 +

摘要

基于吊挂与导轨之间的接触动力学,建立了一种机载导弹导轨式发射过程的有限元仿真分析模型,对发射过程的安全性进行深入研究。该方法能综合考虑载机的机动运动、吊挂与导轨之间的碰撞摩擦、导弹的气动载荷及发动机内压等各种因素的影响,来模拟导弹轨上运动的真实物理过程。对某一响尾蛇导弹的典型发射状态进行了仿真分析,并研究了侧向气动力、偏航气动力矩、机体的垂向过载和滚转角速度等对导弹轨上运动过程的影响,分析结果可为导弹设计提供重要参考。该方法具有较高的分析精度和工程实用性,为机载导弹发射过程的安全性问题提供了有效分析手段。

Abstract

Based on the contact dynamics of the hangers and rail, a finite element simulating method for missile rail launching from aircraft is presented, and the missile’s slip angle, shell stress and contact forces have been investigated. This method could consider the effects of aircraft’s movement, contact forces, aerodynamic forces and missile engine pressure, which can excellently simulate the real physical process of missile’s rail launching movement. The typical launching state of AIM-9 missile has been investigated, and the influences of aircraft’s vertical acceleration and roll rate, missile’s lateral aerodynamic force and yawing moment has been studied, the results can provide important basis for missile designing. This method is practical, accurate and easy to operate, it can be widely used in the security analysis of missile rail launching from aircraft.

关键词

导轨式发射 / 有限元仿真 / 接触碰撞 / 机载导弹 / 冲击应力

Key words

rail-launched / Finite element simulation / contact-impact / airborne missile / impact stress

引用本文

导出引用
陈全龙;韩景龙;员海玮. 机载导弹导轨式发射过程安全性分析[J]. 振动与冲击, 2013, 32(20): 41-47
CHEN Quan-Long HAN Jing-Long YUN Hai-Wei. Security Analysis of Missile Rail Launching from Aircraft[J]. Journal of Vibration and Shock, 2013, 32(20): 41-47

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