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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 1986, Vol. 7 ›› Issue (5): 494-498.
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Yu Xinzhi, Yang Yongnian, Wu Ze, WangDaxuan, Wang Zongdong
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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.
Yu Xinzhi;Yang Yongnian;Wu Ze;WangDaxuan;Wang Zongdong . THE ROTATING NOSE METHOD FOR CONTROLING ASYMMETRIC FORCES AT HIGH ANGLE OF ATTACK[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1986, 7(5): 494-498.
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https://hkxb.buaa.edu.cn/EN/Y1986/V7/I5/494