[1] Beal T R. Dynamic stability of flexible missile under constant and pulsating thrust [J]. AIAA Journal, 1965, 3(3):486-494. [2] Ohshima T, Sugiyama Y. Dynamic stability of free-free beam subjected to end rocket thrust and carrying a heavy payload at its nose [C]∥2003 International Conference on Physics and Control. Saint Petersburg,Russia:IEEE, 2003:1115-1120. [3] Pourtakdoust S H, Assadian N. Investigation of thrust effect on the vibrational characteristics of flexible guided missiles [J]. Journal of Sound and Vibration, 2004, 272(1):287-299. [4] 宋健. 在推力和阻力作用下飞行器横向振动分析[J]. 中国工程科学,2000,2(10):63-72. SONG Jian. Lateral vibration analyses of flying vehicle under thrust and drag [J]. Engineering Science, 2000, 2(10):63-72. (in Chinese) [5] 许赟,谢长川,杨超. 推力作用下细长弹箭横向振动及稳定性分析[J]. 工程力学,2009,26(12):211-215. XU Yun, XIE Chang-chuan, YANG Chao. Transverse vibration and dynamic stability analysis of slender projects under thrust [J]. Engineering Mechanics, 2009, 26(12): 211-215. (in Chinese) [6] 王良明. 细长弹箭气动弹性稳定性研究[J]. 兵工学报,2001,22(1):31-33. WANG Liang-ming. Aeroelastic stability conditions for large L/D ration rockets [J]. Acta Armamentarii, 2001, 22(1):31-33. (in Chinese) [7] 吴小胜, 黄晓鹏. 大长细比导弹气动弹性数值计算研究[J]. 北京理工大学学报,2010, 30(4):379-383. WU Xiao-sheng, HUANG Xiao-peng. Numerical study on the areoelasticity of a large fineness ratio projectile [J]. Transactions of Beijing Institute of Technology, 2010, 30(4):379-383.(in Chinese) [8] Wu Lei, Xie Chang-chuan, Yang Chao. Aeroelastic stability of a slender missile with constant thrust [J]. Procedia Engineering,2012,31:128-135. [9] 吴志刚, 杨超. 弹性导弹的连续与离散阵风响应[J]. 北京航空航天大学学报, 2007, 33(2):136-140. WU Zhi-gang, YANG Chao. Continuous and discrete gust responses of elastic missiles [J]. Journal of Beijing University of Aeronautics and Astronautics, 2007, 33(2):136-140. (in Chinese) [10] 张雷,彭程, 王永, 等. 大长径比导弹两自由度H∞减振跟踪控制器设计[J]. 弹道学报,2010,22(4):1-5. ZHANG Lei, PENG Cheng, WANG Yong, et al. Two-degree-of-freedom H∞ controller design for vibration attenuation and tracking of high length-to-diameter ratio missile [J]. Journal of Ballistics, 2010, 22(4):1-5. (in Chinese) [11] 吴志刚,楚龙飞,杨超,等. 推力耦合的高超声速飞行器气动伺服弹性研究[J]. 航空学报,2012,33(8):1355-1363. WU Zhi-gang, CHU Long-fei, YANG Chao, et al.Study on aeroservoelasticity of hypersonic vehicles with thrust coupling [J]. Acta Aeronautica et Astronautica Sinica, 2012, 33(8):1355-1363. (in Chinese) [12] 陈劲松,曹军. 超声速和高超声速翼型非定常气动力的一种近似计算方法[J]. 空气动力学学报,1990,8(3):339-343. CHEN Jing-song, CAO Jun. An approximate calculating method of supersonic/hypersonic unsteady aerodynamic forces of airfoils [J]. Acta Aerodynamica Sinica, 1990,8(3):339-343. (in Chinese) [13] 杨炳渊,宋伟力. 用当地流活塞理论计算大攻角翼面超音速颤振[J]. 振动与冲击,1995,14(2):60-63. YANG Bing-yuan, SONG Wei-li. Supersonic flutter calculation of a wing with attack angle by local flow piston theory [J]. Journal of Vibration and Shock, 1995, 14(2):60-63. (in Chinese) [14] Zhang Wei-wei, Ye Zheng-yin, Zhang Chen-an. Supersonic flutter analysis based on a local piston theory [J]. AIAA Journal, 2009, 47(10):2321-2328. [15] 张陈安,张伟伟,叶正寅. 基于当地流活塞理论的气动弹性稳定性分析方法研究[J]. 工程力学,2007,24(2):22-27. ZHANG Chen-an, ZHANG Wei-wei, YE Zheng-yin. Aeroelastic analysis methods based on local piston theory[J]. Engineering Mechanics, 2007, 24(2):22-27. (in Chinese) [16] 张陈安,张伟伟,叶正寅. 一种基于当地流活塞理论的超音速导弹气动伺服弹性分析方法[J]. 宇航学报,2007,28(1):141-146. ZHANG Chen-an, ZHANG Wei-wei, YE Zheng-yin. An aeroservoelastic analysis method for supersonic missiles based on local piston theory [J]. Journal of Astronautics, 2007,28(1):141-146. (in Chinese) |