导弹气动力系数的一种计算方法  

A KIND OF COMPUTING METHOD FOR MISSILE AERODYNAMIC FORCE COEFFICIENT

作　　者：韩品尧[1] 

机构地区：[1]哈尔滨工业大学

出　　处：《战术导弹技术》1996年第2期36-40,共5页Tactical Missile Technology

摘　　要：主要研究在大攻角下,气流分离现象所产生的非线性项对法向力系数和俯仰力矩系数的相互影响及其计算程序。通过实例证明,该方法及程序有较好的工程实用价值。The influence of nonlinear term to normal force coefficient and pitching moment coefficient caused by the detached air flow phenomenon in high angle of attack is mainly studied.The computing program related to this research is developed.The example proves that this method as well as its program ars valuable in engineering.

关 键 词：导弹 气动力系数 计算方法 

分 类 号：TJ760.11[兵器科学与技术—武器系统与运用工程]