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弹箭在直升机旋翼下洗流场作用下运动规律研究
引用本文:周克栋,李自勇,赫雷,乐贵高.弹箭在直升机旋翼下洗流场作用下运动规律研究[J].兵工学报,2003,24(2):204-208.
作者姓名:周克栋  李自勇  赫雷  乐贵高
作者单位:南京理工大学机械工程学院,江苏南京,210094
摘    要:本文详细分析了弹箭在直升机旋翼下洗流场作用下所受的力及力矩,推导并获得了各力及力矩的表达式,在此基础上建立了弹箭在直升机旋翼下洗流场作用下的数理模型。通过数值仿真获得了弹箭在该下洗流场作用下的运动规律以及部分参数对弹箭运动的影响规律。研究结果为弹箭的弹道控制与修改提供了依据,具有重要意义。

关 键 词:火箭  导弹  武装直升机  旋翼下洗流场  运动方程  力矩  发射参数  弹道控制

A STUDY ON THE MOVEMENT OF ROCKET UNDER DOWN-WASH FLOW OF A HELICOPTER'S ROTOR
Zhou Kedong,Li Ziyong,He Lei,Le Guigao.A STUDY ON THE MOVEMENT OF ROCKET UNDER DOWN-WASH FLOW OF A HELICOPTER''''S ROTOR[J].Acta Armamentarii,2003,24(2):204-208.
Authors:Zhou Kedong  Li Ziyong  He Lei  Le Guigao
Abstract:Forces and moments exerted on rockets under the down wash flow of a helicopter's rotor were analyzed in detail. The corresponding formulae for the aforementioned forces and moments were deduced. Based on above mentioned formulae the mathematical and physical model of a rocket under helicopter rotor's down wash flow was established. With numerical simulation, the regularities of a rocket under helicopter rotor's down wash flow and the effects of launching parameters upon the rocket movement were obtained. These results provide a basis for further studies on rocket ballistic control and modification and were thus of reference value.
Keywords:fluid mechanics  down  wash flow  ballistic control  numerical simulation  
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