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同心简垂直发射装置底部导流分析
引用本文:唐洪,乐贵高,王辉,胡晓磊. 同心简垂直发射装置底部导流分析[J]. 江苏机械制造与自动化, 2014, 0(1): 14-16
作者姓名:唐洪  乐贵高  王辉  胡晓磊
作者单位:[1]南京理工大学机械工程学院,江苏南京210094 [2]四川航天技术研究院,四川成都610100
摘    要:研究了在同心筒垂直发射装置发射过程中导弹周围高温燃气环境对导弹产生的影响.通过同心筒底部导流结构的设计,减少高温燃气的反射,促进高温燃气的排导,从而减少高温燃气对导弹底部的烧蚀.采用数值仿真方法对两种导流方式进行计算模拟和对比.结果表明,采用导流锥型同心筒对导弹发射过程中的压力和热环境有一定效果.

关 键 词:同心筒  燃气射流  导流锥

Research on Jet Exhaust at Bottom of Concentric Launch Canister
TANG Hong. Research on Jet Exhaust at Bottom of Concentric Launch Canister[J]. Jiangsu Machine Building & Automation, 2014, 0(1): 14-16
Authors:TANG Hong
Affiliation:TANG Hong(Department of Mechanical Engieering,Nanjing University of Science and Technology, Nanjing 210094, China) LE Gui-gao(Department of Mechanical Engieering,Nanjing University of Science and Technology, Nanjing 210094, China) WANG Hui(Sichuan Academy of Aerospace Technology, Chengdu 610100, China) HU Xiao-lei(Department of Mechanical Engieering,Nanjing University of Science and Technology, Nanjing 210094, China)
Abstract:This paper makes a study of the influence of the high temperature jet environment around the missile on the missile during the launching of the missile launcher with a concentric vertical launching device.Through the design of the bottom part of the outside cylinder of the concentric system,the reflection of the high temperature jet can be reduced,thus decreasing the scorch of the high temperature jet point of the missile launching cylinder.The paper also makes use of the numerical value method to give a numerical simulation with the two measures.The result shows that the two measures bring a certain effect in improving the heat and pressure environment during the missile launching.
Keywords:CCL  jet flow  jet-guide cone
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