Dynamic Simulation and Experimental Study of Deployment Process of Missile Folding-wing

doi:10.3969/j.issn.1000-1093.2016.08.010

Abstract

Abstract: The deployment process of transverse folding-wings of missiles is studied. The mathematical model and dynamic simulation model of deployment process of folding-wing in missile launching and ground tests are both established, in which the influences of friction and aerodynamic force are considered. The folding-wing were designed and manufactured. The images of deployment process of folding-wings are obtained using the high speed photography during ground test. The research results show that the test results are in good agreement with those of mathematic and dynamic simulation models. A value range of friction moment is also provided from the test results, which can support the design and application of folding-wing.

Key words: ordnance science and technology, folding-wing, deployment, dynamic simulation, experiment

CLC Number:

TJ760.13

ZHEN Wen-qiang, JI Yong-qiang, SHI Yun-guo. Dynamic Simulation and Experimental Study of Deployment Process of Missile Folding-wing[J]. Acta Armamentarii, 2016, 37(8): 1409-1414.

References

［1］余旭东, 葛金玉, 段德高, 等. 导弹现代结构设计［M］. 北京:国防工业出版社, 2007.
YU Xu-dong，GE Jin-yu，DUAN De-gao, et al. Modern structure design of missiles［M］. Beijing:National Defense Industry Press, 2007.(in Chinese)
［2］ Kroyer R．Wing mechanism analysis［J］． Computers and Structures, 1999, 72(2): 253-265．
［3］ Henry J I, Schwartz D R, Soukup M A. Design construction and testing of a folding-wing tube-launched micro air vehicle［C］∥43rd AIAA Aerospace Sciences Meeting and Exhibit. Reno，Nevada:AIAA, 2005:2005-1451．
［4］李莉, 任茶仙, 张铎. 折叠翼机构展开动力学仿真及优化［J］. 强度与环境, 2007, 34(1):17-21.
LI Li，REN Cha-xian，ZHANG Duo. Dynamic simulation and optimization design of deployment of folding-wing［J］. Structure & Environment Engineering, 2007, 34(1):17-21.(in Chinese)
［5］崔二巍, 于存贵, 李猛, 等. 某导弹折叠弹翼展开过程的仿真分析［J］. 兵工自动化, 2013, 32(12):12-14.
CUI Er-wei, YU Cun-gui, LI Meng, et al. Simulation analysis of a missile folding wing deployment process［J］. Ordnance Industry Automation, 2013, 32(12):12-14.(in Chinese)
［6］赵俊锋, 刘莉, 杨武, 等. 折叠弹翼展开动力学仿真及优化［J］. 弹箭与制导学报, 2012, 32(2):155-157.
ZHAO Jun-feng, LIU Li, YANG Wu, et al. Dynamic simulation and optimization design of folding wing deployment［J］. Journal of Projectiles, Rockets, Missiles and Guidance, 2012, 32(2):155-157. (in Chinese)
［7］吴俊全, 孙海文, 张晓旻. 折叠翼展开试验与动力学仿真研究［J］. 弹箭与制导学报, 2011, 32(3):164-166.
WU Jun-quan，SUN Hai-wen，ZHANG Xiao-min. The research on unfolding test and dynamic model of folding-wing［J］. Journal of Projectiles, Rockets, Missiles and Guidance, 2011, 32(3):164-166. (in Chinese)
［8］张钦, 聂宏, 张明, 等. 无人机折叠翼展开动力学分析［J］. 机械设计与制造工程, 2015, 44(2):12-16.
ZHANG Qin，NIE Hong，ZHANG Ming，et al. Dynamic analysis of UAV folding wing depolyment process［J］. Machine Design and Manufacturing Engineering Technology, 2015, 44(2):12-16. (in Chinese)
［9］胡文华, 张伟, 曹东兴. 折叠翼的理论建模与实验研究［J］. 动力学与控制学报, 2015, 13(3):230-234.
HU Wen-hua，ZHANG Wei, CAO Dong-xing. Research on theoretical model and experiments of folding wings［J］. Journal of Dynamics and Control, 2015，13(3):230-234.(in Chinese)
［10］雷歌, 邓飞, 刘权, 等. 水下航行器折叠翼展开机构设计与动力学仿真［J］. 鱼雷技术, 2013, 21(2):81-85.
LEI Ge，DENG Fei，LIU Quan，et al. Design and dynamic simulation of folding wing expansion mechanism of underwater vehicle［J］. Torpedo Technology, 2013, 21(2):81-85. (in Chinese)
［11］秦永明, 蔡琛芳, 董金刚. 机载导弹折叠舵展开气动特性试验研究［J］. 航空兵器, 2013(5):3-6.
QIN Yong-ming，CAI Chen-fang，DONG Jin-gang. Experimental study on aerodynamics of airborne missile folding rudder［J］. Aero Weaponry, 2013(5):3-6.(in Chinese)
［12］贾毅. 战术导弹折叠翼两种展开方法及测试结果比较［J］. 流体力学实验与测量, 2003, 17(2):70-73.
JIA Yi. The comparison between two deploying methods and results of folding wings for some tactical missiles［J］. Experiments and Measurements in Fluid Mechanics, 2003, 17(2):70-73.(in Chinese)
［13］李真, 董玉立, 冯成良, 等. 基于CFD-FASTRN的导弹折叠弹翼展开过程模拟［J］. 弹箭与制导学报, 2015, 35(2):5-8.
LI Zhen, DONG Yu-li, FENG Cheng-liang, et al. Simulation of deployment of missile folded wings based on CFD-FASTRAN［J］. Journal of Projectiles, Rocekets, Missiles and Guidance, 2015, 35(2):5-8.(in Chinese)

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