Citation: | Jing Zhiwei, Wu Zhigang, Yang Chaoet al. Rudder flutter analysis method of missile with jet vane[J]. Journal of Beijing University of Aeronautics and Astronautics, 2010, 36(8): 991-995. (in Chinese) |
[1] Lauzon M.5DOF dynamic loads on a jet vane .AlAA-90-2382,1990 [2] 刘志珩.燃气舵的气动设计[J].战术导弹技术,1983(2):1-7 Liu Zhiheng.Aerodynamics design of jet vane[J].Tactics Missile Technology ,1983(2):1-7(in Chinese) [3] 王文亮,杜作润.结构振动与动态子结构方法[M].上海:复旦大学出版社,1985 Wang Wenliang,Du Zuorun.Structural vibration and dynamic sub-structure method[M].Shanghai:Fudan University Press,1985(in Chinese) [4] 王永岩.动态子结构方法理论与应用[M].北京:科学出版社,1999 Wang Yongyan.The theory and application of dynamic sub-structure method[M].Beijing:Science Press,1999(in Chinese) [5] Facciano A B,Seybold K G,Westberry-Kutz T L,et al.Evolved seasparrow missile jet vane control system prototype hardware development[J].Journal of Spacecraft and Rockets,2002,39(4) : 522-531 [6] 管德.非定常空气动力计算[M].北京:北京航空航天大学出版社,1991 Guan De.Unsteady aerodynamics calculation[M].Beijing:Beijing University of Aeronautics and Astronautics Press,1991(in Chinese) [7] 余超志.导弹概论[M].北京:北京工业学院出版社,1986 Yu Chaozhi.Introductions to missiles[M].Beijing:Beijing Industry Institute Press,1986(in Chinese)
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