Citation: | LI Cheng, HUANG Xiaolong, LI Ning, LIU Wei, WENG Chunsheng. Experimental study on effects of nozzles on gas bubble shapes and pressure characteristics of underwater detonation[J]. Explosion And Shock Waves, 2023, 43(3): 032202. doi: 10.11883/bzycj-2022-0268 |
[1] |
ROSATO D A, THORNTON M, SOSA J, et al. Stabilized detonation for hypersonic propulsion [J]. Proceedings of the National Academy of Sciences of the United States of America, 2021, 118(20): e2102244118. DOI: 10.1073/pnas.2102244118.
|
[2] |
潘振华, 范宝春, 归明月, 等. 流动系统中爆轰波传播特性的数值模拟 [J]. 爆炸与冲击, 2010, 30(6): 593–597. DOI: 10.11883/1001-1455(2010)06-0593-05.
PAN Z H, FAN B C, GUI M Y, et al. Numerical simulation of detonation wave propagation in a flow system [J]. Explosion and Shock Waves, 2010, 30(6): 593–597. DOI: 10.11883/1001-1455(2010)06-0593-05.
|
[3] |
王兵, 谢峤峰, 闻浩诚, 等. 爆震发动机研究进展 [J]. 推进技术, 2021, 42(4): 721–737. DOI: 10.13675/j.cnki.tjjs.210109.
WANG B, XIE Q F, WEN H C, et al. Research progress of detonation engines [J]. Journal of Propulsion Technology, 2021, 42(4): 721–737. DOI: 10.13675/j.cnki.tjjs.210109.
|
[4] |
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 [J]. 兵工学报, 2018, 39(5): 961–968. DOI: 10.3969/j.issn.1000-1093.2018.05.016.
ZHANG C, YU W, WANG B S. Research on the initial flow field characteristics of underwater supersonic gas jets [J]. Acta Armamentarii, 2018, 39(5): 961–968. DOI: 10.3969/j.issn.1000-1093.2018.05.016.
|
[5] |
王乐勤, 郝宗睿, 吴大转. 水下气体射流初期流场的数值研究 [J]. 工程热物理学报, 2009, 30(7): 1132–1135. DOI: 10.3321/j.issn:0253-231X.2009.07.014.
WANG L Q, HAO Z R, WU D Z. Numerical simulation of initial flow field of underwater gas jet [J]. Journal of Engineering Thermophysics, 2009, 30(7): 1132–1135. DOI: 10.3321/j.issn:0253-231X.2009.07.014.
|
[6] |
张焕好, 郭则庆, 王瑞琦, 等. 水下超声速气体射流的初始流动特性研究 [J]. 振动与冲击, 2019, 38(6): 88–93; 131. DOI: 10.13465/j.cnki.jvs.2019.06.013.
ZHANG H H, GUO Z Q, WANG R Q, et al. Initial flow characteristics of an underwater supersonic gas jet [J]. Journal of Vibration and Shock, 2019, 38(6): 88–93; 131. DOI: 10.13465/j.cnki.jvs.2019.06.013.
|
[7] |
ZHANG Q B, FAN W, WANG K, et al. Impact of nozzles on a valveless pulse detonation rocket engine without the purge process [J]. Applied Thermal Engineering, 2016, 100: 1161–1168. DOI: 10.1016/j.applthermaleng.2016.02.135.
|
[8] |
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. DOI: 10.3969/j.issn1000-4874.2012.06.005.
CHEN H L, WANG N, LIU H P, et al. Investigation of nozzle gas jet characteristics with different launch depth underwater [J]. Chinese Journal of Hydrodynamics, 2012, 27(6): 659–666. DOI: 10.3969/j.issn1000-4874.2012.06.005.
|
[9] |
FROLOV S M, AVDEEV K A, AKSENOV V S, et al. Pulsed detonation hydroramjet: simulations and experiments [J]. Shock Waves, 2020, 30(3): 221–234. DOI: 10.1007/s00193-019-00906-2.
|
[10] |
FROLOV S M, AVDEEV K A, AKSENOV V S, et al. Experimental and computational studies of shock wave-to-bubbly water momentum transfer [J]. International Journal of Multiphase Flow, 2017, 92: 20–38. DOI: 10.1016/j.ijmultiphaseflow.2017.01.016.
|
[11] |
LIU W, LI N, WENG C S, et al. Bubble dynamics and pressure field characteristics of underwater detonation gas jet generated by a detonation tube [J]. Physics of Fluids, 2021, 33(2): 023302. DOI: 10.1063/5.0029729.
|
[12] |
LIU W, LI N, HUANG X L, et al. Experimental study of underwater pulse detonation gas jets: bubble velocity field and time-frequency characteristics of pressure field [J]. Physics of Fluids, 2021, 33(8): 083324. DOI: 10.1063/5.0060686.
|
[13] |
侯子伟, 翁春生, 贾芳, 等. 水下爆轰燃气泡形态与激波传播过程研究 [J]. 推进技术, 2021, 42(4): 755–764. DOI: 10.13675/j.cnki.tjjs.200390.
HOU Z W, WENG C S, JIA F, et al. Gas bubble shape and shock wave propagation process of underwater detonation [J]. Journal of Propulsion Technology, 2021, 42(4): 755–764. DOI: 10.13675/j.cnki.tjjs.200390.
|
[14] |
HOU Z W, LI N, HUANG X L, et al. Experimental study on pressure evolution of detonation waves penetrating into water [J]. Physics of Fluids, 2022, 34(7): 076110. DOI: 10.1063/5.0100446.
|
[15] |
李旭东, 王春, 姜宗林. 喷管对脉冲爆轰发动机性能的影响 [J]. 力学学报, 2011, 43(1): 1–10. DOI: 10.6052/0459-1879-2011-1-lxxb2009-754.
LI X D, WANG C, JIANG Z L. Nozzle effects on performance of pulse detonation engines [J]. Chinese Journal of Theoretical and Applied Mechanics, 2011, 43(1): 1–10. DOI: 10.6052/0459-1879-2011-1-lxxb2009-754.
|
[16] |
YUNGSTER S. Analysis of nozzle and ejector effects on pulse detonation engine performance [C]//Proceedings of the 41st Aerospace Sciences Meeting and Exhibit. Reno, Nevada, USA: AIAA, 2003: 1316. DOI: 10.2514/6.2003-1316.
|
[17] |
范玮, 严传俊, 李强, 等. 脉冲爆震发动机尾喷管的实验 [J]. 航空动力学报, 2007, 22(6): 869–872. DOI: 10.3969/j.issn.1000-8055.2007.06.004.
FAN W, YAN C J, LI Q, et al. Experimental investigation on pulse detonation engine nozzles [J]. Journal of Aerospace Power, 2007, 22(6): 869–872. DOI: 10.3969/j.issn.1000-8055.2007.06.004.
|
[18] |
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. DOI: 10.13675/j.cnki.tjjs.2011.03.002.
TANG L S, LIU Y, WU Z F, 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. DOI: 10.13675/j.cnki.tjjs.2011.03.002.
|
[19] |
LINCK M, GUPTA A, BOURHIS G, et al. Combustion characteristics of pressurized swirling spray flame and unsteady two-phase exhaust jet [C]//Proceedings of the 44th AIAA Aerospace Sciences Meeting and Exhibit. Reno, Nevada, USA: AIAA, 2006: 377. DOI: 10.2514/6.2006-377.
|
[20] |
唐嘉宁, 刘向阳, 李世鹏, 等. 水下固体火箭发动机推力特性研究 [J]. 导弹与航天运载技术, 2012(5): 15–21. DOI: 10.3969/j.issn.1006-2793.2012.03.008.
TANG J N, LIU X Y, LI S P, et al. Study on the thrust characteristics of the underwater solid rocket motor [J]. Missiles and Space Vehicles, 2012(5): 15–21. DOI: 10.3969/j.issn.1006-2793.2012.03.008.
|
[21] |
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. DOI: 10.1007/s10409-011-0474-4.
|
[22] |
王利利, 刘影, 李达钦, 等. 固体火箭发动机水下超音速射流数值研究 [J]. 兵工学报, 2019, 40(6): 1161–1170. DOI: 10.3969/j.issn.1000-1093.2019.06.006.
WANG L L, LIU Y, LI D Q, et al. Numerical study of underwater supersonic gas jets for solid rocket engine [J]. Acta Armamentarii, 2019, 40(6): 1161–1170. DOI: 10.3969/j.issn.1000-1093.2019.06.006.
|
[23] |
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. DOI: 10.16076/j.cnki.cjhd.2009.05.003.
CAO J Y, LU C J, LI J, et al. Research on dynamic characteristics of underwater superasonic gas jets [J]. Journal of Hydrodynamics, 2009, 24(5): 575–582. DOI: 10.16076/j.cnki.cjhd.2009.05.003.
|
[24] |
GONG Z X, LU C J, LI J, et al. The gas jet behavior in submerged Laval nozzle flow [J]. Journal of Hydrodynamics, Ser. B, 2017, 29(6): 1035–1043. DOI: 10.1016/S1001-6058(16)60817-X.
|
[25] |
BLOCH G, KUCZATY J, SATTELMAYER T. Application of high-speed digital holographic interferometry for the analysis of temperature distributions and velocity fields in subcooled flow boiling [J]. Experiments in Fluids, 2014, 55(2): 1678. DOI: 10.1007/s00348-014-1678-8.
|
[26] |
GORDON S, MCBRIDE B J. Computer program for calculation of complex chemical equilibrium compositions and applications. Part 1: analysis: NASA 1311 [R]. Washington, USA: National Aeronautics and Space Administration, 1994: 39–40.
|