期刊文献+
共找到1篇文章
< 1 >
每页显示 20 50 100
Rolling Control Characteristic Experimental Investigation of a Canard Missile with Free-Spinning Tail 被引量:1
1
作者 雷娟棉 吴甲生 孟令涛 《Journal of Beijing Institute of Technology》 EI CAS 2006年第1期36-38,共3页
To study the rolling control characteristics of a canard-controlled missile, a series of wind tunnel experiment is conducted. The experimental method, the structure features of wind tunnel model and the experimental r... To study the rolling control characteristics of a canard-controlled missile, a series of wind tunnel experiment is conducted. The experimental method, the structure features of wind tunnel model and the experimental results are introduced in this paper. The experimental data show that the canard is an inefficient rolling control device for canard-controlled missile with fixed tail fins; but for the free-spinning tail fin configuration, the canard can conduct rolling control of the missile, and even have higher controlling efficiency under larger canard deflection angle. 展开更多
关键词 canard missile aerodynamic characteristics wind tunnel experiment free-spinning tail rolling control characteristics
下载PDF
上一页 1 下一页 到第
使用帮助 返回顶部