摘要
对全张式变壁厚卷弧翼的动力学特性进行了分析与研究。并通过对某火箭弹的飞行试验验证了设计结果的合理性和可行性。为此可对同类产品的飞行稳定性设计提供一定的参考依据。
Study and analysis on dynamic characteristics of spread variable thickness arc-shaped fin is proceeded. Through the flight test of certain rocket projectile,the reasonability and reliability of the design be testified and certain reference foundation on flight stability design of the products isoprovided.
出处
《弹箭与制导学报》
CSCD
北大核心
2004年第S1期162-164,共3页
Journal of Projectiles,Rockets,Missiles and Guidance
关键词
变壁厚
卷弧翼
动力学特性
variable thickness
arc-shaped fin
dynamic characteristics
