摘要
文中对矩形截面弹身—尾翼组合体的亚音速气动特性进行了数值计算,计算条件为 M=0.4～0.9,α=0°～10°,给出气功特性曲线,并与风洞试验结果进行了比较。
In this paper,the subsonic aerodynamics of rectangular cross-sectional boby-tail configurations is researched by numerical simulation.The condition of computation is M=0.4～0.9 and α=0°～10°.The aerodynamic parameters is obtained,and compared with experimental data..
出处
《弹箭与制导学报》
CSCD
北大核心
2002年第S1期164-167,共4页
Journal of Projectiles,Rockets,Missiles and Guidance
关键词
非圆截面导弹
数值模拟
气动特性
noncircular cross-sectional missiles
numerical simulation
aerodynamic characteristics
