摘要
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. 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.
源语言 | 英语 |
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页(从-至) | 36-38 |
页数 | 3 |
期刊 | Journal of Beijing Institute of Technology (English Edition) |
卷 | 15 |
期 | 1 |
出版状态 | 已出版 - 3月 2006 |