摘要
研究了非圆截面导弹前体的气动力,探讨了这种导弹因上洗引起的翼体干扰因子——K_(W(B))值。分析了相对于导弹弹体中心线的弹翼垂直位置和弹体横截面形状对K_(W_(B))值的影响。
The aerodynamic forces on the noncircular cross section fuselage are studied. The wing-body interference factor K_(W(B)) Caused by upwash is discussed. The effects made by the vertical position of wing ralative to the missile fuselage centerline and the shape of fwselage cross section are analyzed.
出处
《战术导弹技术》
1997年第2期21-27,共7页
Tactical Missile Technology
关键词
气动力
导弹
非圆截面导弹
Aerodynamic shape Aerodynamic force Missile
