潜射航行体连续发射筒口气泡及载荷特性研究

STUDY ON OUTLET BUBBLE AND LOADING CHARACTERISTICS OF SUBMARINE LAUNCHED VEHICLE DURING SUCCESSIVE LAUNCH

  • 摘要: 航行体水下连续发射筒口气泡演变及载荷突变对发射安全性具有重要影响。基于VOF多相流模型和动网格技术,建立一筒多航行体水下连续发射数值方法,研究了首发与次发航行体发射过程中筒口气泡形态及相邻设备载荷特性,分析了发射时间间隔对航行体水下连续发射筒口载荷的影响规律。研究表明:水下连续发射筒口流场在筒口结构特征以及首发筒口气泡等作用下呈非对称发展特征;当次发航行体离筒后,筒口气泡脉动特性更加复杂,出现“双筒倒灌”现象;筒口最大冲击载荷发生在首发航行体离筒气泡拉断后的收缩阶段,邻近测点压力幅值高达800 kPa,次发航行体发射过程中,筒口载荷脉动特征显著增大;发射时间间隔对筒口载荷影响较小,但随着发射间隔增加,发射筒底部受到的脉动压力显著增加;水下连发过程中相邻设备表面受到强烈的脉动载荷作用,且形成的载荷幅值随着远离发射筒中心呈减小趋势;在发射间隔Δt=3 s时,次发航行体离筒过程中相邻设备的载荷增幅较小。研究成果可为一筒多航行体水下发射安全性设计与分析提供参考。

     

    Abstract: The outlet bubble evolution and loading mutation during the underwater successive launch have significant impacts on the launch safety. A numerical method for the underwater successive launch of multiple vehicles in a launching tube has been established upon the VOF multiphase flow model and dynamic mesh technology. Studied are the shapes of outlet bubbles and the loading characteristics of adjacent equipment during the first and secondary vehicle launching process. Analyzed is the impact of launching time intervals on the load of the underwater successive launch. The results show that: the underwater continuous launch outlet flow field exhibits asymmetric development characteristics under the action of the structure characteristics of the outlet and the first outlet bubble; and after the secondary vehicle leaves the launching tube, the pulsation phenomenon of the outlet bubbles becomes more complex, resulting in the phenomenon of "double-tube seawater swarming". The maximum impact load on the opening of the launching tube occurs in the contraction stage after the bubble is pulled apart when the first vehicle leaves the launching tube, and the pressure amplitude at the adjacent measuring point can reach up to 800 kPa. During the launch process of the secondary vehicle, the fluctuation characteristics of the load on the opening of the launching tube significantly increase. The launching time intervals have little effect on the load of the the opening of the launching tube. However, with the increase of launching time interval, the pulsating load at the bottom of the launching tube increases. During the process of the underwater successive launch, the adjacent equipment such as the convex membranes and tube cover are subjected to strong pulsating loads. The impact of load on the hull wall is relatively small, and it decreases with the distance from the tube opening; and at the launch interval Δt=3 s, the load increase of adjacent equipment during the departure of the secondary vehicle is small. The research outcome can provide a reference for the safety design and analysis of the underwater launch of the multiple vehicles in a launching tube.

     

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