柱形充液室内多股燃气射流流场的气体与液体两相流场演化特性

doi:10.3969/j.issn.1000-1093.2016.10.012

摘要/Abstract

摘要： 基于水下枪炮发射的工程背景，对火药燃烧形成的多股高压燃气射流从模拟弹头头部喷入柱形充液室的过程进行了实验观测和数值模拟研究。实验观测采用高速录像记录，数值模型采用流体体积函数模型来描述液体环境中多个燃气泡的扩展，数值模拟结果与实验观测结果相符。数值仿真结果表明：喷孔轴线上的燃气压力经历下降和上升的过程后达到稳定值，空腔附近的水流场由于燃气作用出现压力峰，随后逐渐衰减；在燃气空腔扩展的过程中，离喷孔距离越远的截面上燃气-水流场的压力分布越均匀，截面平均压力随着空腔扩展逐渐下降；随着时间的增长，截面上气体组分分数可达70%.

关键词: 兵器科学与技术, 气体与液体相互作用, 多股燃气射流, 湍流掺混, 数值计算

Abstract: The injection process of multiple high-pressure combustion gas jets is observed experimentally and simulated numerically during gun firing underwater. The gas is generated by gunpowder burning and injected into a cylindrical water-filled chamber through simulated bullet. In experiment, a high-speed camera system is used to record the injecting process of air. The volume-of-fluid method is used to describe the expansion of the gas cavities in water. The numerical results show a good agreement with experimental observations. Numerical simulations show that the gas pressure along the axis of orifice reaches a steady value after declining and rising. A pressure peak appears in the water near the gas cavity under the effect of combustion gas, and then is gradually attenuated. During the expansion of the gas cavities, the pressure distribution of gas-water flow field on a cross section away from nozzle is relatively uniform, and the average pressure on the section decreases with the expansion in the cavity. The area fraction of gas on the section could be up to 70% over time.

Key words: ordnance science and technology, gas-water interaction, multiple combustion gas jet, turbulent mixing, numerical simulation

中图分类号:

O358

赵嘉俊，余永刚. 柱形充液室内多股燃气射流流场的气体与液体两相流场演化特性[J]. 兵工学报, 2016, 37(10): 1852-1859.

ZHAO Jia-jun, YU Yong-gang. The Evolution of Gas-liquid Flow of Multiple Combustion Gas Jets in a Cylindrical Water-filled Chamber[J]. Acta Armamentarii, 2016, 37(10): 1852-1859.

参考文献

［1］赵世平, 李江, 何国强, 等. 固体燃气发生器动力模拟水下发射试验研究[J]. 固体火箭技术, 2006, 29(1):5-8.
ZHAO Shi-ping, LI Jiang, HE Guo-qiang, et al. Investigation on simulated underwater projectile test by solid propellant gas generator[J]. Journal of Solid Rocket Technology, 2006, 29(1):5-8.(in Chinese)
[2］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)
[3］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 dynamic research on the under-water ignition of missile[J]. Acta Aeronautica et Astronautica Sinica, 1992, 13(4):124-130.(in Chinese)
[4］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, 138.
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, 138.(in Chinese)
[5］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):3-9, 147.
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):3-9, 147.(in Chinese)
[6］仲峰泉, 陆夕云, 庄礼贤. 火箭水下发射复杂流场的近似数值模拟[J]. 宇航学报, 2000, 21(2): 1-7.
ZHONG Feng-quan, LU Xi-yun, ZHUANG Li-xian. Numerical simulation of the complex flow field for rocket launch under water[J]. Journal of Astron Autics, 2000, 21(2):1-7.(in Chinese)
[7］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A辑, 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, Ser. A, 2007, 22(1):83-92.(in Chinese)
[8］ Cheng Y S, Liu H. Mathematical modeling of fluid flows for underwater missile launch[J]. Journal of Hydrodynamics, Ser. B, 2006, 18(3):492-497.
[9］ Lindau J W, Venkateswaran S, Kunz R F, et al. Multiphase computations for underwater propulsive flows[C]∥16th AIAA Computational Fluid Dynamics Conference. Orlando, FL, US:AIAA, 2003.
[10］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A辑, 2006, 21(6):752-759.
CAO Jia-yi, LU Chuan-jing, LI Jie, et al. Research on the vertical launching of direct ignition underwater missile[J]. Journal of Hydrodynamics, Ser. A, 2006, 21(6):752-759.(in Chinese)
[11］曹嘉怡, 鲁传敬, 李杰, 等. 水下超声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 dynamics characteristics of underwater supersonic gas jets[J]. Journal of Hydrodynamics, Ser. A, 2009, 24(5):575-582.(in Chinese)
[12］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 under water[J]. Journal of Solid Rocket Technology, 2007, 30(5):388-391.(in Chinese)
[13］陈焕龙, 王柠, 刘华坪, 等. 不同发射深度下喷管燃气射流特性研究[J]. 水动力学研究与进展A辑, 2012, 27(6):659-666.
CHEN Huan-long, WANG Ning, LIU Hua-ping, et al. Investigation of nozzle gas jet characteristics with different launch depth underwater[J]. Chinese Journal of Hydrodynamics, Ser. A, 2012, 27(6):659-666.(in Chinese)
[14］向敏, 吴雄, 张为华, 等. 水下固体发动机尾流场数值仿真[J]. 推进技术, 2009, 30(4): 479-483.
XIANG Min, WU Xiong, ZHANG Wei-hua, et al. Numerical simulation for underwater solid motor tail flow[J]. Journal of Propulsion Technology, 2009, 30(4):479-483.(in Chinese)
[15］唐嘉宁, 李世鹏, 王宁飞. 水下固体火箭发动机的负推力现象研究[J]. 固体火箭技术, 2012, 35(3):325-329, 343.
TANG Jia-ning, LI Shi-peng, WANG Ning-fei. Study of the negative thrust of the underwater solid rocket engines[J]. Journal of Solid Rocket Technology, 2012, 35(3):325-329, 343.(in Chinese)
[16］ Tang J, Wang N, Shyy W. Flow structures of gaseous jets injected into water for underwater propulsion[J]. Acta Mechanica Sinica, 2011, 27(4):461-472.
[17］刘传龙, 张宇文, 王亚东, 等. 考虑适配器弹性的潜射导弹出筒载荷特性研究[J]. 兵工学报, 2015, 36(2):379-384.
LIU Chuan-long, ZHANG Yu-wen, WANG Ya-dong, et al. Investigation into load characteristics of submarine-launched missile being ejected from launch tube considering the adapter elasticity[J]. Acta Armamentarii, 2015, 36(2):379-384.(in Chinese)
[18］莽珊珊, 余永刚. 边界形状对高压受限射流扩展稳定性影响[J]. 推进技术, 2011, 32(3): 334-338.
MANG Shan-shan, YU Yong-gang. Effects of chamber wall shape on high-pressure gas jet expansion stability in bulk-loaded liquid[J]. Journal of Propulsion Technology, 2011, 32(3):334- 338.(in Chinese)
[19］莽珊珊, 余永刚. 高压燃气射流在整装液体中扩展过程的实验和数值模拟[J]. 爆炸与冲击, 2011, 31(3): 300-305.
MANG Shan-shan, YU Yong-gang. Experiment and numerical simulation for high pressure combustible gas jet expansion process in a bulk-loaded liquid [J]. Explosion and Shock Waves, 2011, 31(3):300-305.(in Chinese)
[20］薛晓春, 余永刚, 张琦, 等. 渐扩边界形状对双股燃气射流扩展特性影响的实验研究[J]. 弹道学报, 2013, 25(2): 44-47.
XUE Xiao-chun, YU Yong-gang, ZHANG Qi, et al. Experimental study on effects of stepped-wall boundary on expansion characteristic of twin combustion-gas Jets[J]. Journal of Ballistics, 2013, 25(2):44-47.(in Chinese)
[21］薛晓春, 余永刚, 张琦. 双束燃气射流与整装式液体装药相互作用的实验和数值模拟[J]. 兵工学报, 2013, 34(6): 669-677.
XUE Xiao-chun, YU Yong-gang, ZHANG Qi. Experiment and numerical simulation for interaction of twin gas jets and bulk-loaded liquid charge[J]. Acta Armamentarii, 2013, 34(6):669-677. (in Chinese)
[22］ Evgenevna I E, Evgenevna I T, Viktorovich B P. Analysis of the application of turbulence models in the calculation of supersonic gas jet[J]. American Journal of Applied Sciences, 2014, 11(11): 1914-1920.
[23］ Shih T H, Liou W W, Shabbir A, et al. A new k-ε eddy viscosity model for high Reynolds number turbulent flows[J]. Computers & Fluids, 1995, 24(3):227-238.

[1]	官典, 李世鹏, 刘筑, 王宁飞. 横向过载对固体火箭发动机推进剂点火建压过程的影响[J]. 兵工学报, 2021, 42(9): 1877-1887.
[2]	祝昊，靳栓宝，王东，王公宝，魏应三，胡鹏飞，武星宇，何升阳，胡风革. 无轴泵喷推进器敞水特性[J]. 兵工学报, 2021, 42(4): 835-841.
[3]	胡雨博，余永刚. 充液圆管周向多股壁面燃气射流排水特性[J]. 兵工学报, 2020, 41(12): 2417-2423.
[4]	范薇，苏子舟，范天峰，张涛，张洪海，刘勇. C形一体电枢的结构设计及接触压力分析[J]. 兵工学报, 2019, 40(10): 1969-1976.
[5]	李科斌，李晓杰，王小红，闫鸿浩. 球形装药水下爆炸近场测量的连续探针法研究[J]. 兵工学报, 2019, 40(1): 1-7.
[6]	冯博声，薛晓春. 边界形状对4股燃气射流扩展稳定性影响的数值模拟[J]. 兵工学报, 2018, 39(9): 1692-1700.
[7]	娄伟鹏，郑长松，李和言，陈建文，张周立，马源. 高速《Symbol》v湿式换挡离合器排油阀临界开启和关闭压力研究[J]. 兵工学报, 2017, 38(9): 1665-1672.
[8]	王宪成，杨绍卿，马宁，赵文柱. 车辆柴油机缸套动载荷磨损计算模型研究[J]. 兵工学报, 2017, 38(9): 1673-1680.
[9]	孙皓泽，常天庆，王全东，孔德鹏，戴文君. 一种基于分层多尺度卷积特征提取的坦克装甲目标图像检测方法[J]. 兵工学报, 2017, 38(9): 1681-1691.
[10]	张玉燕，孙莎莎，王振春，曹海要，战再吉. 高速载流电枢表面瞬态温度场仿真与测量[J]. 兵工学报, 2017, 38(9): 1692-1698.
[11]	李臣明，宦超，石怀龙. 某箱式火箭炮对面目标分布式杀伤最优火力分配[J]. 兵工学报, 2017, 38(9): 1699-1704.
[12]	雷娟棉，张嘉炜，谭朝明. 小攻角下船尾外形对旋转弹丸马格努斯效应影响的数值研究[J]. 兵工学报, 2017, 38(9): 1705-1715.
[13]	李泽，闫晓鹏，栗苹，郝新红，王建涛. 扫频式干扰对调频多普勒引信的干扰机理研究[J]. 兵工学报, 2017, 38(9): 1716-1722.
[14]	张浩为，谢军伟，张昭建，宗彬锋，陈唐军. 基于混合自适应遗传算法的相控阵雷达任务调度[J]. 兵工学报, 2017, 38(9): 1761-1770.
[15]	李茂，侯海量，朱锡，黄晓明，李典，陈长海，胡年明. 结构间隙对芳纶纤维增强复合装甲结构抗侵彻性能的影响[J]. 兵工学报, 2017, 38(9): 1797-1805.