导弹潜射多自由度模型及出筒水动力响应特性研究

RESEARCH ON MULTI-DEGREE-OF-FREEDOM MODEL AND HYDRODYNAMIC RESPONSE CHARACTERISTICS OF SUBMARINE-LAUNCHED MISSILES DURING BARREL-EXIT STAGE

  • 摘要: 导弹潜射分为出筒、水中运动及出水三个阶段,第一阶段导弹出筒后的运动和姿态直接影响入水和出水后的运动响应。此外,由于蒸汽-弹体-水介质相互作用,潜射出筒问题还涉及多物理场耦合。因此,构建导弹潜射多自由度模型,开展出筒过程水动力响应特性研究兼具科学价值和工程价值。针对导弹出筒阶段多物理场和多自由度运动耦合的强非线性问题,该文基于多自由度运动模型、空化模型和碰撞模型,建立了一种模拟导弹水下发射的二维数值模型:首先通过与静水发射实验数据对比验证了该模型的有效性;然后开展了横流对导弹出筒过程水动力响应特性研究。与出筒单自由度数值模型对比表明:多自由度模型在不同的横流速度下都能够很好的展现横流的影响;高速横流会引起导弹与发射筒的碰撞,流速越快碰撞的时刻越早,碰撞会使导弹无法出筒或出筒后姿态变差;多自由度模型对筒内海水倒灌形态的变化也能细致展现。

     

    Abstract: The launch process of submarine-launched missile is divided into three stages: barrel-exit stage, underwater motion stage, and water-exit stage. The motion and posture of the missile after the first barrel-exit stage directly influence its motion response after entering the water and exiting the water. Moreover, due to the interaction between steam and missile and water, the launch problem also involves multi-physics field coupling. Therefore, constructing a multi-degree-of-freedom model for missile launch and conducting research on the hydrodynamic response characteristics during the barrel-exit process have both scientific and engineering value. In response to the strong nonlinearity caused by the multi-physics field and multi-degree-of-freedom motion coupling during the barrel-exit stage, a 2D numerical model is established for simulating underwater launch based on a multi-degree-of-freedom motion model, a cavitation model, and a collision model. Firstly, the validity of model is verified by comparison with launch experimental data in still water. Then, research on the hydrodynamic response characteristics of a missile in crossflow is conducted. Comparison with the single-degree-of-freedom numerical model out of the barrel shows that the multi-degree-of-freedom model can well show the influence of crossflow well at different crossflow velocities; high-speed crossflow will cause the collision between the missile and the launch barrel, and the faster the flow rate, the sooner the collision will occur. The collision will make the missile unable to exit the barrel or its attitude will deteriorate after exiting the barrel; and the multi-degree-of-freedom model can also show in detail the changes in the backflow of seawater inside the barrel.

     

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