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有头部攻角的弹丸气动性能的数值计算
引用本文:王飞,吴国东,王志军,康晓慧. 有头部攻角的弹丸气动性能的数值计算[J]. 中北大学学报(自然科学版), 2005, 26(3): 177-179
作者姓名:王飞  吴国东  王志军  康晓慧
作者单位:中北大学机械电子工程系 山西太原030051(王飞,吴国东,王志军),中国人民解放军驻247厂军代室 030009(康晓慧)
摘    要:运用流体力学数值计算软件对有头部攻角的弹丸气动性能进行了数值计算,分析了有头部攻角弹丸周围流场和作用在弹丸表面的空气动力.结果表明,弹头部相对弹体部有一定转角,能产生较大的控制力和力矩,为发展自适应弹箭提供了数值计算方法.

关 键 词:头部攻角  空气动力性能  数值计算
文章编号:1006-5431(2005)03-0177-03
修稿时间:2004-09-07

Numerical Calculation of Aerodynamic Characteristics of Shell with Attack Angle at the Shell Head
WANG Fei,WU Guo-dong,WANG Zhi-jun,KANG Xiao-hui. Numerical Calculation of Aerodynamic Characteristics of Shell with Attack Angle at the Shell Head[J]. Journal of North University of China, 2005, 26(3): 177-179
Authors:WANG Fei  WU Guo-dong  WANG Zhi-jun  KANG Xiao-hui
Affiliation:WANG Fei~1,WU Guo-dong~1,WANG Zhi-jun~1,KANG Xiao-hui~2
Abstract:A numerical simulation of aerodynamic characteristics of shell with angle of attack at the shell head is given by using Compational Fluids Dynamics(CFD) software. The aerodynamic dynamical software of the flow field around the shell with angle of attack at the shell head is analysed. The result characterictic showed that the considerable control force and moment was produced by shell head having an angle relative to body. This paper provides the numerical calculation method of developing self-adapt shell.
Keywords:shell head attack angle  aerodynamic characteristics  numerical calculation
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