Interior Ballistic Modeling and Simulation of Underwater Launched Missile Using Concentric Canister Launcher

YUAN Xu-long;WANG Ya-dong;LIU Wei

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    Published By: Journal Of Ballistics

    CN 32-1343/TJ

Journal Of Ballistics ›› 2013, Vol. 25 ›› Issue (2) : 48.

Interior Ballistic Modeling and Simulation of Underwater Launched Missile Using Concentric Canister Launcher

  • YUAN Xu-long, WANG Ya-dong, LIU Wei
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Abstract

To construct a fast calculation method of interior ballistics of underwater launched missile using Concentric Canister Launcher(CCL),a simulation model of CCL was established according to the first law of thermodynamics,and power characteristics and underwater environment were considered.The empirical parameters in this model were decided using CFD solutions,and they were verified by more calculations.The influences of design parameters on the interior ballistics were studied by the verified model.The simulation shows that the sizes of canister top and bottom restricting parts can be used to adjust launching velocity of missile; the size of canister bottom restricting part can be adapted to modify the acceleration of missile.It can increase the adjusting range of velocity to increase initial volumes of inner and outer canister.The simulation method and results offer reference for engineers.

Key words

concentric canister launcher / underwater launch / interior ballistics / parameter identification / simulation

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YUAN Xu-long, WANG Ya-dong, LIU Wei. Interior Ballistic Modeling and Simulation of Underwater Launched Missile Using Concentric Canister Launcher. Journal Of Ballistics. 2013, 25(2): 48

References

[1] 侯金瑛,谭大成,毕世华,等.同心筒发射潜载导弹过程数值研究[J].固体火箭技术,2011,34(1):9-13.
HOU Jin-ying,TAN Da-cheng,BI Shi-hua,et al.Numerical research on the process of launching submarine missile by concentric canister launcher[J].Journal of Solid Rocket Technology,2011,34(1):9-13.(in Chinese)
[2]苗佩云,袁曾凤.同心筒式发射时筒内流场机理及内外筒间隙的影响[J].战术导弹技术,2006(1):8-13.
MIAO Pei-yun,YUAN Zeng-feng.Effect of flow mechanism and annular sizes on concentric canister launcher[J].Tactical Missile Technology,2006(1):8-13.(in Chinese)
[3]傅德彬,刘琦,陈建伟,等.导弹发射过程数值模拟[J].弹道学报,2004,16(3):11-16.
FU De-bin,LIU Qi,CHEN Jian-wei,et al.Numerical simulation on missile launching process[J].Journal of Ballistics,2004,16(3):11-16.(in Chinese)
[4]王树宗,练永庆,陈一雕.气动式水下武器发射装置内弹道数学模型[J].弹道学报,2003,15(1):21-26.
WANG Shu-zong,LIAN Yong-qing,CHEN Yi-diao.Mathematic model of the underwater compressed-air launcher[J].Journal of Ballistics,2003,15(1):21-26.(in Chinese)
[5]肖虎斌.潜射导弹燃气蒸汽式发射装置的内弹道建模[J].舰船科学技术,2010,32(2):36-39.
XIAO Hu-bin.Interior ballistics modeling of submarin-based missile launching unit[J].Ship Science and Technology,2010,32(2):36-39.(in Chinese)
[6]芮守祯,邢玉明.几种导弹弹射动力系统内弹道性能比较[J].北京航空航天大学学报,2009,35(6):766-770.
RUI Shou-zhen,XING Yu-ming.Comparative studies of interior ballistic performance among several missile eject power systems[J].Journal of Beijing University of Aeronautics and Astronautics,2009,35(6):766-770.(in Chinese)
[7]张宇文.鱼雷弹道与弹道设计[M].西安:西北工业大学出版社,1998.
ZHANG Yu-wen.Torpedo ballistics and ballistic design[M].Xi’an:Northwestern Polytechnical University Press,1998.(in Chinese)

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