| 控制大迎角非对称力的头部旋转法 |
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| 引用本文： | 于欣芝,杨永年,巫泽,王达选,王宗栋.控制大迎角非对称力的头部旋转法[J].航空学报,1986,7(5):494-498. |
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| 作者姓名： | 于欣芝 杨永年 巫泽 王达选 王宗栋 |
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| 作者单位： | 西北工业大学 |
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| 摘 要： | 前言 细长体在大迎角飞行时,背风区旋涡的非对称分布对亚音速或中等超音速飞机和全方位导弹,可能引起严重的控制问题。多年来,在推迟非对称涡的发生以及减小非对称载荷方面进行了大量的实验研究,提出了多种方法。但它们属于被动控制范畴。
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| 收稿时间： | 1985-09-13; |
THE ROTATING NOSE METHOD FOR CONTROLING ASYMMETRIC FORCES AT HIGH ANGLE OF ATTACK |
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| Yu Xinzhi,Yang Yongnian,Wu Ze,WangDaxuan,Wang Zongdong.THE ROTATING NOSE METHOD FOR CONTROLING ASYMMETRIC FORCES AT HIGH ANGLE OF ATTACK[J].Acta Aeronautica et Astronautica Sinica,1986,7(5):494-498. |
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| Authors: | Yu Xinzhi Yang Yongnian Wu Ze WangDaxuan Wang Zongdong |
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| Institution: | Northwestern Pol ytechnical University |
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| Abstract: | The rotating nose method and its mechanism which control asymmetric forces at high angle of attack are discussed in this paper. A large number of tests have been done. The results of the tests show that the method is justifiable, the explanation of the mechanism is reasonable, and the asymmetric forces can be reduced to permissible range, even to zero. |
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