Numerical simulation and analysis of the 3D transient muzzle flow field of underwater artillery

被引:6
|
作者
Zhang, Xuan [1 ]
Yu, Yonggang [1 ]
Zhang, Xinwei [1 ]
机构
[1] Nanjing Univ Sci & Technol, Sch Energy & Power Engn, Nanjing 210094, Jiangsu, Peoples R China
基金
中国博士后科学基金;
关键词
underwater sealed launch; Muzzle flow field; Mach disk; Numerical analysis; Gas jet;
D O I
10.1016/j.oceaneng.2023.115270
中图分类号
U6 [水路运输]; P75 [海洋工程];
学科分类号
0814 ; 081505 ; 0824 ; 082401 ;
摘要
The in-depth study of the muzzle flow field contributes to the improvement of the gun and the design of the projectile. This study establishes an unsteady muzzle multiphase flow model of the underwater sealed launch with a three-dimensional scale. Among that, the VOF model is employed to trace the two-phase interface and the gas-liquid turbulent mixing is described by the standard k-& epsilon; turbulence model. Also, the established numerical model was validated by comparing underwater sealed launching experimental results. On this basis, numerical analysis on the muzzle flow field of the 30 mm artillery under different launching conditions were carried out by coupling with revised interior ballistic equations. The results show that the "necking" phenomenon occurs during gas-expansion process due to the interaction between water and projectile. Then, a "bowl-shaped" shock area is obviously formed at the muzzle. In addition, the Mach disk diameter and the corresponding growth rate are closely related to the projectile head cavitation diameter. The growth rate of Mach disk diameter increases with an increase of the cavitation diameter. When the muzzle velocities are different, the positions of the Mach disk formed are also different, presenting that the Mach disk is farther away from the muzzle with the increase of muzzle velocity.
引用
收藏
页数:13
相关论文
共 50 条
  • [41] Simulation about 3D flow field of missile underwater motion and water-exit process
    Yang, Xiao-Guang
    Chen, Huan-Long
    Liu, Hua-Ping
    Zhao, Cheng-Jia
    Chen, Fu
    Dandao Xuebao/Journal of Ballistics, 2010, 22 (01): : 107 - 110
  • [42] 3D Numerical Simulation of the Transient Thermal Behavior of a Simplified Building Envelope Under External Flow
    Barmpas, F.
    Bouris, D.
    Moussiopoulos, N.
    JOURNAL OF SOLAR ENERGY ENGINEERING-TRANSACTIONS OF THE ASME, 2009, 131 (03): : 0310011 - 03100112
  • [43] Numerical Simulation of Transient Flows around a 3D Pitching Hydrofoil
    Wu, Qin
    Huang, Biao
    Wang, Guoyu
    ADVANCES IN MECHANICAL ENGINEERING, 2015, 7 (02):
  • [44] Simulation and Analysis of the Railgun Muzzle Flow Field Considering the Arc Plasma
    Gao, Yuan
    Xiao, Hongcheng
    Ni, Yanjie
    Xu, Yingtao
    Wan, Gang
    Li, Baoming
    IEEE TRANSACTIONS ON PLASMA SCIENCE, 2019, 47 (05) : 2242 - 2249
  • [45] Numerical Simulation and Analysis of Muzzle Flow During a Rarefaction Wave Gun Firing
    Wang, Guannan
    Cheng, Cheng
    Zhang, Xiaobing
    Huang, Xi
    PROPELLANTS EXPLOSIVES PYROTECHNICS, 2021, 46 (12) : 1902 - 1913
  • [46] NUMERICAL SIMULATION OF LAUNCH PROCESS OF STACKED PROJECTILE WEAPON CONSIDERING MUZZLE FLOW FIELD
    Luo, Qiao
    Zhang, Xiao-bing
    29TH INTERNATIONAL SYMPOSIUM ON BALLISTICS, VOLS 1 AND 2, 2016, : 888 - 894
  • [47] Application of algebraic multigrid method in numerical simulation of solid rocket 3D flow field
    Li, Z. (roy_lizheng@hotmail.com), 1600, Journal of Solid Rocket Technology (37):
  • [48] 3D Numerical Simulation of the Driver Effect of a Curved Scoop on the Flow Field in a Gas Centrifuge
    Huang, Dongyang
    Jiang, Dongjun
    JOURNAL OF ENGINEERING PHYSICS AND THERMOPHYSICS, 2024, 97 (06) : 1488 - 1502
  • [49] Numerical Investigation on Evolutionary Characteristics of Muzzle Flow Field of Ballistic Gun during Underwater Submerged Firing
    Zhang J.
    Yu Y.
    Binggong Xuebao/Acta Armamentarii, 2020, 41 (03): : 471 - 480
  • [50] Numerical investigation on the muzzle flow field of an underwater submerged launched ballistic gun at different water depths
    Zhang J.
    Yu Y.
    Baozha Yu Chongji/Explosion and Shock Waves, 2020, 40 (10):