摘要
以减小无控火箭弹方向散布为主要目标,建立了火箭弹气动外形优化设计数学模型.给出了相应的计算方法,编制了计算机程序.以某尾翼式火箭弹为例验证了模型的精度和程序的可靠性.
This paper mainly aims at reducing the leteral dispersion of fin—stabilized unguidedrockets,and gives the mathematical model of optimized aerodynamic design of the rockets,itssolution and the computer program.The accuracy of the model and the correctness of theprogram are tested by an example.
出处
《弹道学报》
EI
CSCD
1992年第4期29-32,共4页
Journal of Ballistics
关键词
火箭弹
气动外形
优化设计
Unguided Rockets
Aerodynamic Configurations
Optimum Design
