Numerical Calculation of Aerodynamic Characteristics of Shell with Attack Angle at the Shell Head
|更新时间:2026-09-14
|
Numerical Calculation of Aerodynamic Characteristics of Shell with Attack Angle at the Shell Head
有头部攻角的弹丸气动性能的数值计算
Issue 3, Pages: 177-179(2005)
作者机构:
1. ,山西,太原,030051
2. 中北大学机械电子工程系
3. 中国人民解放军驻247厂军代室,山西,太原,030051
作者简介:
基金信息:
DOI:
CLC:
Published:2005
稿件说明:
移动端阅览
王飞, 吴国东, 王志军, et al. Numerical Calculation of Aerodynamic Characteristics of Shell with Attack Angle at the Shell Head[J]. 2005, (3): 177-179.
DOI:
王飞, 吴国东, 王志军, et al. Numerical Calculation of Aerodynamic Characteristics of Shell with Attack Angle at the Shell Head[J]. 2005, (3): 177-179.DOI:
Numerical Calculation of Aerodynamic Characteristics of Shell with Attack Angle at the Shell Head
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.
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.