The Dsign of Jet Vane of Thrust Vector Control System

被引:0
作者
Wang, Liu Min [1 ]
Mo, Bo [1 ]
机构
[1] Beijing Inst Technol, Beijing 100081, Peoples R China
来源
MANUFACTURING ENGINEERING AND AUTOMATION II, PTS 1-3 | 2012年 / 591-593卷
关键词
Thrust Vector Control; Jet Vane; Engineering Calculation; Fluid Analysis;
D O I
10.4028/www.scientific.net/AMR.591-593.1743
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
According to the thrust vector control requirements of fast turn of the missile vertical launching, this design carries out the force analysis of the jet vane which is in the high temperature and high speed jet stream, and calculates the normal force which is generated by the vane, thus calculates the area of the jet vane.. At the same time, according to the aerodynamic theory and engineering experience, this design analyzes and calculates the aerodynamic shape of the jet vane. As a result, two types of jet vane are designed. On this basis, through the use of a fluid analysis software FLUENT, both of the two jet vane are simulated and get a jet vane which is more suitable for the practical applications.
引用
收藏
页码:1743 / 1747
页数:5
相关论文
共 4 条
[1]  
Lin M.F., 1981, THRUST VECTOR CONTRO, p196~200
[2]  
Liu Z.H., 1988, TACTICAL MISSILE TEC, p1~7
[3]  
Liu Zhiheng, 1995, MISSILES SPACE VEHIC, P9
[4]  
Yu C.L., 2008, J HENAN U SCI TECHNO, V29, p35~38