不同点火时间导弹滑弹一体式发射数值模拟  

Numerical Simulation of Missiles Launched by Rail-catapult Integrated Launcher with Different Firing Time

作　　者：王博[1] 马贵春[1] 陈阳[1] 

机构地区：[1]中北大学机电工程学院,山西太原030051

出　　处：《山西冶金》2016年第2期8-10,共3页Shanxi Metallurgy

摘　　要：使用计算流体力学软件Fluent对导弹滑弹一体式发射的过程进行模拟研究。通过对比导弹弹射后不同点火时间对机翼的气动干扰情况,找出使用滑弹一体式发射装置时合适的导弹发动机点火时间。The process of missile launched by rail- catapult integrated launching is simulated by the use of computational fluid dynamics software Fluent. By comparing the aerodynamic interference of the wing with different ignition time after the missile ejection, the appropriate missile engine ignition time is found.

关 键 词：无人机 滑弹一体式发射装置 尾喷流 

分 类 号：TJ760.13[兵器科学与技术—武器系统与运用工程]