The Model of Combustion Gas Bubble of Submarine launched Missile and Numerical Simulation

LI Jie;LU Chuan jing

CN Submission Journal Articles Figures Search
Adv. Search

  • Sponsored by:

    Editor-In-Chief:

    ISSN 1004-499X

    　

  • Hosted By:

    Published By: Journal Of Ballistics

    CN 32-1343/TJ

Journal Of Ballistics ›› 2009, Vol. 21 ›› Issue (4) : 6-8.

The Model of Combustion Gas Bubble of Submarine launched Missile and Numerical Simulation

  • LI Jie1, LU Chuan jing1,2
Author information +
History +

Abstract

Rayleigh Plesset equation was applied to establish the model of combustion gas bubble and investigate the pressure change. The effect of combustion gas bubble on underwater trajectory of vertical launching submarine launched missile was studied by combined solution of gas bubble equation and missile motion equation. The result shows that because of the change of environment pressure, the tail pressure fluctuates at a small range. The fluctuation period becomes shorter and shorter as the reduction of bubble’s dimension.

Key words

submarine launched missile / underwater trajectory / combustion gas effect

Cite this article

EndNote

Ris (Procite)

Bibtex

Download Citations
LI Jie, LU Chuan jing. The Model of Combustion Gas Bubble of Submarine launched Missile and Numerical Simulation. Journal Of Ballistics. 2009, 21(4): 6-8

References

[1]鲁传敬,陈方,樊泓. 导弹水下点火的流体动力研究[J]. 航空学报,1992,13(4):124-130. LU Chuan jing, CHEN Fang, FAN Hong. The fluid dynamic research on the under water ignition of missile[J]. Acta Aeronautica ET Astronautica Sinica, 1992,13(4):124-130.(in Chinese)
[2]黄建春,叶取源,朱世权. 不同发射深度下导弹水下点火气水流体动力计算[J]. 应用力学学报,1994,11(3):19-24. HUANG Jian chun, YE Qu yuan, ZHU Shi quan. Gas water dynamic calculation for the underwater ignition of a missile at different depths[J]. Chinese Journal of Applied Mechanics,1994,11(3):19-24.(in Chinese)
[3]王诚,叶取源,何有声. 导弹水下发射燃气泡计算[J]. 应用力学学报,1997,14(3):1-7. WANG Cheng, YE Qu yuan, HE You sheng. Calculation of an exhausted gas cavity behind an under water launched missile[J]. Chinese Journal of Applied Mechanics, 1997, 14(3): 1-7.(in Chinese)
[4]单雪雄,杨荣国,叶取源. 具有推力矢量控制系统的导弹流体动力[J]. 上海交通大学学报,2001,35(4):625-629. SHAN Xue xiong, YANG Rong guo, YE Qu yuan. Fluid forces on a missile with control system of vectorial thrust[J]. Journal of Shanghai Jiaotong University, 2001, 35(4): 625-629.(in Chinese)
[5]程用胜,刘桦. 喷管不同摆角对水下发射导弹受力的影响[J]. 水动力学研究与进展,2007,22(1):83-92. CHENG Yong sheng, LIU Hua. The effects of nozzle deflection angles on a missile launched underwater[J]. Journal of Hydrodynamics, 2007, 22(1): 83-92.(in Chinese)
[6]王建儒,赵仕厂. 水下固体火箭发动机尾流场计算[J]. 固体火箭技术,2007,30(5):388-391. WANG Jian ru, ZHAO Shi chang. Computations for solid rocket moter tail flow underwater[J]. Journal of Solid Rocket Technology, 2007, 30(5): 388-391.(in Chinese)
[7]曹嘉怡,鲁传敬,李杰,等. 潜射导弹水下垂直自抛发射过程研究[J]. 水动力学研究与进展,2006,21(6):752-758. CAO Jia yi, LU Chuan jing, LI Jie, et al. Research on the vertical launching of direct igniting underwater missile[J]. Journal of Hydrodynamics, 2006, 21(6): 752-758.(in Chinese)

7

Accesses

0

Citation

Detail
Sections
Recommended

/

〈 〉