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ZHAO Shi-ping, BI Feng-yang, LU Bing-ju, YUAN Xu-long, QIN Li-ping. Simulation on Underwater Salvo Load Characteristics of Multi-Slender Body Vehicles in Single Launching Tube[J]. Journal of Unmanned Undersea Systems, 2019, 27(1): 031-36. doi: 10.11993/j.issn.2096-3920.2019.01.006
Citation: ZHAO Shi-ping, BI Feng-yang, LU Bing-ju, YUAN Xu-long, QIN Li-ping. Simulation on Underwater Salvo Load Characteristics of Multi-Slender Body Vehicles in Single Launching Tube[J]. Journal of Unmanned Undersea Systems, 2019, 27(1): 031-36. doi: 10.11993/j.issn.2096-3920.2019.01.006

Simulation on Underwater Salvo Load Characteristics of Multi-Slender Body Vehicles in Single Launching Tube

doi: 10.11993/j.issn.2096-3920.2019.01.006
  • Received Date: 2018-08-10
  • Rev Recd Date: 2018-08-26
  • Publish Date: 2019-02-28
  • In respect of the underwater salvo adjacent tube effect caused by dense arrangement of several slender body vehicles in single launching tube, the volume of fluid(VOF) and multiphase flow methods are used to establish a three-dimensional unsteady multiphase flow simulation model for underwater vertical salvo, in which the dynamic grid technology for user-defined function(UDF) to control the motion of two vehicles is adopted and the influence of suspended flange, tube cover and submarine shape on the flow field characteristics of the tube mouth is considered. Then, the load characteristics of adjacent tube watertight head cover and water back-flow hammer are obtained. The influence of first-launched vehicle on the load characteristics of second-launched vehicle is analyzed, and conclusions are drawn as follows: 1) After launching of the first-launched vehicle, the flow field at the tube mouth tends to stabilize quickly, and the load of watertight head cover of the adjacent tube is slightly smaller than that of the first-launched vehicle but with similar law when the second vehicle is launched. That is, the flow field at the tube mouth of single tube has little effect on the salvo interval; 2) After launching, the flow field of launcher tends to stabilize quickly both inside and outside, and the amount of seawater poured back into the launcher is relatively small, which may affect the steering performance of the submarine; 3) Second-launched vehicle has great influence on the characteristics of water hammer load and flow field of first-launched vehicle in launching tube. This research may provide a reference for dense arrangement scheme demonstration of underwater multi-slender vehicle and safety analysis of salvo.

     

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  • [1]
    张义忠, 倪火才. 潜载导弹水下共架垂直发射方案探讨[J]. 舰船科学技术, 2005, 27(5): 55-60.

    Zhang Yi-zhong, Ni Huo-cai. The Concept of Submarine Launched Missile’s Common Frame, Modular and Vertical Launcher[J]. Ship Science and Technology, 2005, 27(5): 55-60.
    [2]
    倪火才. 潜载导弹水下发射技术的发展趋势分析[J]. 舰载武器, 2001(1): 8-16.
    [3]
    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.
    [4]
    王汉平, 吴菊花. 基于CFD的潜射导弹筒口压力场预测[J]. 弹道学报, 2008, 20(4): 73-76.

    Wang Han-ping, Wu Ju-hua. Forecast of Pressure Field Near Launch Canister Outlet for Underwater-launched Missile Based on CFD[J]. Journal of Ballistics, 2008, 20(4): 73-76.
    [5]
    张红军, 陆宏志, 裴胤, 等. 潜射导弹出筒过程的三维非定常数值模拟研究[J]. 水动力学研究与进展, 2010, 25(3): 406-415.

    Zhang Hong-jun, Lu Hong-zhi, Pei-yin, et al. Numerical Investigation to Vertical Launching of Submarine Launching Missile[J]. Chinese Journal of Hydrodynamics, 2010, 25(3): 406-415.
    [6]
    王汉平, 吴友生. 潜射导弹筒盖系统附加气室降载技术[J]. 弹道学报, 2011, 23(1): 102-106.

    Wang Han-ping, Wu You-sheng. Add-on Gas Chamber Technique for Depressing Load over Cover System of Underwater-launched Missile[J]. Journal of Ballistics, 2011, 23(1): 102-106.
    [7]
    张晓乐, 卢丙举, 胡仁海, 等. 水下航行体垂直发射筒口压力场L_E耦合数值模拟[J]. 舰船科学技术, 2016, 38(11): 151-155.

    Zhang Xiao-le, Lu Bing-ju, Hu Ren-hai, et al. L/E Coupling Numerical Simulation of Pressure Field Near Launch Canister Outlet for Underwater Vehicle Vertical Launch[J]. Ship Science and Technology, 2016, 38(11): 151-155.
    [8]
    王汉平, 吴友生. 潜射导弹筒盖系统附加气室降载技术[J]. 弹道学报, 2011, 23(1): 102-106.

    Wang Han-ping, Wu You-sheng. Add-on Gas Chamber Technique for Depressing Load over Cover System of Underwater-launched Missile[J]. Journal of Ballistics, 2011, 23(1): 102-106.
    [9]
    傅德彬, 于殿君, 张志勇. 潜射导弹离筒后海水倒灌效应数值分析[J]. 固体火箭技术, 2012, 35(2): 157-160.

    Fu De-bin, Yu Dian-jun, Zhang Zhi-yong. Numerical Simulation on Hydrodynamic Impact Effect after Submarine Launched Missile Leaves the Launcher[J]. Journal of Solid Rocket Technology, 2012, 35(2): 157-160.
    [10]
    殷崇一. 潜射导弹发射与出水载荷研究[D]. 西安: 西北工业大学, 2004.
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