水下超声速燃气射流的初期流场特性研究

张春;郁伟;王宝寿

兵工学报 ›› 2018, Vol. 39 ›› Issue (5) : 961-968.

EN 投稿 期刊 文章 图表 检索
高级检索

  • 主管：中国科学技术协会

    主编：许毅达

    ISSN 1000-1093

    　

  • 主办：中国兵工学会

    出版：《兵工学报》 编辑部

    CN 11-2176/TJ

《兵工学报》是我国国防科技领域最具影响力的学术期刊之一，创刊于1979年，目前被国内所有重要数据库收录，其综合评价指标近年来一直名列兵工技术类科技期刊的首位；《兵工学报》目前还被国际上著名的检索机构美国......
兵工学报 ›› 2018, Vol. 39 ›› Issue (5) : 961-968. DOI: 10.3969/j.issn.1000-1093.2018.05.016
论文

水下超声速燃气射流的初期流场特性研究

  • 张春， 郁伟， 王宝寿
作者信息 +

Research on the Initial Flow Field Characteristics of Underwater Supersonic Gas Jets

  • ZHANG Chun， YU Wei， WANG Bao-shou
Author information +
文章历史 +

摘要

针对超声速燃气射流在静水介质中扩展的复杂多相流动问题，在压力水筒中开展了固体火箭发动机水下点火实验；基于雷诺时均Navier-Stokes方法和流体体积模型，对相同工况进行了燃气与水耦合数值求解。研究结果表明：水下燃气射流迅速建立超声速流动后，高速射流的冲击作用导致燃气泡呈现出帽状特征，并逐渐演变为类椭球体的气囊，平均轴向扩展速度约为40 m/s；燃气泡内部流动结构复杂，存在两个剪切涡环与重复出现的激波胞格，射流边界与燃气泡边界的相互作用会导致射流后续演化的不稳定；燃气扩展时通过压力波在水流场中产生高压区，其压力峰值在振荡中逐渐与环境压力匹配，喷管堵盖打开压力、出口截面积是影响推力峰值的重要因素。

Abstract

To investigate the complex multiphase flow of supersonic gas jets in still water, an underwater ignition experiment of solid rocket motor is conducted in the pressure tank, and the numerically simulated results of gas-water coupling for the same case are obtained by using Reynolds-averaged Navier-Stokes(RANS) method and volume of fluid(VOF) model. The results show that, after underwater gas jets achieve supersonic flow, the gas bubble appears to be cap-like due to the jet impact effect. Then the gas bubble gradually evolves into an ellipsoid-shaped gasbag with average axial expansion velocity of about 40 m/s. The flow structures inside the gas bubble are very complex, where two shear vortex rings and repeated shock cells exist. The interaction between the boundaries of gas jet and gas bubble may induce the instability of gas jet in the subsequent evolution stage. It is also demonstrated that there exists a part of high pressure in the flow field, and the pressure peaks gradually match with the environmental pressure in the oscillation process. The pressure of opening nozzle closure and the area of nozzle outlet are the two important factors that affects thrust peak value.Key

关键词

水下燃气射流 / 超声速 / 动量射流 / 流场特性

Key words

underwatergasjet / supersonicspeed / momentumjet / flowfieldcharacteristic

引用本文

EndNote

Ris (Procite)

Bibtex

导出引用
张春， 郁伟， 王宝寿. 水下超声速燃气射流的初期流场特性研究. 兵工学报. 2018, 39(5): 961-968 https://doi.org/10.3969/j.issn.1000-1093.2018.05.016
ZHANG Chun， YU Wei， WANG Bao-shou. Research on the Initial Flow Field Characteristics of Underwater Supersonic Gas Jets. Acta Armamentarii. 2018, 39(5): 961-968 https://doi.org/10.3969/j.issn.1000-1093.2018.05.016

参考文献



［1］鲁传敬,陈方,樊泓,等.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, et al. The fluid dyna-micresearch on the underwater 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.不同发射深度下的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. The fluid dynamic simulation on the underwater ignition of missile in different depth[J]. Chinese Journal of Applied Mechanics, 1994, 11(3): 19-24. (in Chinese)
[3］王诚, 叶取源, 何友声. 导弹水下发射燃气泡计算[J]. 应用力学学报, 1997, 14(3): 1-8.
WANG Cheng, YE Qu-yuan, HE You-sheng. Calculation of an exhausted gas cavity behind an underwater launched missile[J]. Chinese Journal of Applied Mechanics, 1997, 14(3): 1-8. (in Chinese)
[4］张有为, 王晓宏, 杨举贤. 利用球形气泡模型研究导弹水下点火瞬间的推力状况[J]. 水动力学研究与进展, 2005, 20(5):636-640.
ZHANG You-wei, WANG Xiao-hong, YANG Ju-xian. Study on the working thrust for the missile launching under water using the spherical bubble model[J]. Journal of Hydrodynamics, 2005, 20(5):636-640. (in Chinese)
[5］王宝寿, 许晟, 易淑群, 等. 水下推力矢量特性试验研究[J]. 船舶力学, 2000, 4(5): 9-15.
WANG Bao-shou, XU Sheng, YI Shu-qun, et al. Test studies of underwater thrust vector control performance[J]. Journal of Ship Mechanics, 2000, 4(5): 9-15. (in Chinese)
[6］潘哲,王宝寿,宋志平.火箭发动机水下分离特性试验研究[J].船舶力学,2004,8(4):22-26.
PAN Zhe,WANG Bao-shou,SONG Zhi-ping.Research on underwater rocket separation performance[J].Journal of Ship Mecha-nics, 2004,8(4):22-26. (in Chinese)
[7］汤龙生,刘宇,吴智锋,等.水下超声速燃气射流气泡的生长及压力波传播特性实验研究[J].推进技术,2011,32(3):417-420.
TANG Long-sheng,LIU Yu,WU Zhi-feng, et al.Experimental study on characteristics of bubble growth and pressure wave propagation by supersonic gas jets under water[J].Journal of Propulsion Technology,2011,32(3):417-420.(in Chinese)
[8］贾有军,张胜敏,尤俊峰,等.固体发动机水下点火尾流变化过程试验研究[J].固体火箭技术,2015, 38(5): 660-678.
JIA You-jun, ZHANG Sheng-min, YOU Jun-feng, et al. Experimental research on the changing process of underwater ignition wake of solid rocket motor[J]. Journal of Solid Rocket Technology,2015,38(5):660-678. (in Chinese)
[9］施红辉,王柏懿, 戴振卿.水下超声速气体射流的力学机制研究[J].中国科学:物理学 力学 天文学, 2010, 40(1):92-100.
SHI Hong-hui, WANG Bo-yi, DAI Zhen-qing. Research on the mechanics of underwater supersonic gas jets[J].Scientia Sinica: PhysIcs, Mechanics & Astronomica, 2010,40(1):92-100. (in Chinese)
[10］施红辉, 汪剑锋, 陈帅, 等.水下超声速气体射流初期流场特性的实验研究[J].中国科学技术大学学报,2014,44(3): 233-237.
SHI Hong-hui,WANG Jian-feng,CHEN Shuai,et al.Experimental study on flow characteristics at the initial injection stage of underwater supersonic gas jets[J].Journal of University of Science and Technology of China,2014, 44(3): 233-237. (in Chinese)
[11］贺小艳，马汉东，纪楚群.水下气体射流初期数值研究[J].水动力学研究与进展：A 辑，2004，19（2） :207-212.
HE Xiao-yan, MA Han-dong, JI Chu-qun. Numerical simulation of gas jets in water[J].Journal of Hydrodynamics：Ser. A, 2004, 19(2): 207-212. (in Chinese)
[12］徐小强.水下燃气喷管高速射流问题研究[D].杭州：浙江大学,2004.
XU Xiao-qiang.Research on high-speed gas jet of nozzle underwater[D].Hangzhou: Zhejiang University, 2004.(in Chinese)
[13］曹嘉怡,鲁传敬,李杰,等.水下超音速燃气射流动力学特性研究[J].水动力学研究与进展：A辑, 2009, 24(5): 575-582.
CAO Jia-yi,LU Chuan-jing,LI Jie,et al.Research on dynamic characteristics of underwater supersonic gas jets[J].Journal of Hydrodynamics：Ser. A,2009, 24(5): 575-582.(in Chinese)
[14］Tang J N，Wang N F，Shyy W. Flow structures of gaseous jets injected into water for underwater propulsion[J]. Acta Mechanica Sinica，2011，27(4):461-472.
[15］朱卫兵, 陈宏, 黄舜.水下高速射流气泡变化过程数值研究[J].推进技术, 2010, 31(4): 496-502.
ZHU Wei-bing,CHEN Hong,HUANG Shun.Numerical study of the process of the evolution of bubble of high-speed jet underwater[J].Journal of Propulsion Technology, 2010, 31(4): 496-502. (in Chinese)
[16］唐云龙,李世鹏,谢侃,等.有相变的水下超音速燃气射流数值模拟[J].哈尔滨工程大学学报,2016,37(9): 1237-1243.
TANG Yun-long,LI Shi-peng,XIE Kan, et al.Numerical simulation of underwater supersonic gas jets with phase transitions[J].Journal of Harbin Engineering University, 2016, 37(9):1237-1243.(in Chinese)





第39卷
第5期2018年5月兵工学报ACTA
ARMAMENTARIIVol.39No.5May2018

350

Accesses

0

Citation

Detail
段落导航
相关文章

/

〈 〉