锥头型双航行体并联高速垂直入水数值模拟研究

Numerical simulation study on parallel high-speed vertical water entry of cone-shaped double vehicles

  • 摘要:
    目的 多航行体的跨介质集群突防已成为各国研究热点,为了探究双航行体在高速入水时的载荷特性以及水动力干涉现象,对锥头型双体航行体高速入水过程进行数值模拟研究。
    方法 基于计算流体力学软件Star CCM+构建计算模型,采用基于雷诺平均Navier-Stokes方程的Realizable k-ε湍流模型,并结合重叠网格法,预报多体结构物与复杂流动的相互作用。同时,采用流体体积方法捕捉空泡演化特性,并引入Schnerr-Sauer 空腔模型以考虑水的相变行为。基于该数值模型,系统研究不同间距d条件下并行双航行体入水过程中空腔形态演化、头部压力载荷以及运动轨迹等流场动力学特性的影响。
    结果 研究结果表明,在航行体接触水面瞬间,不同间距下的航行体载荷和头部抨击压力急剧上升至峰值,随后迅速衰减。当间距d = 0.8DD为航行体直径)时,最大抨击载荷相比d = 1.6D时增加超过20%,而头部的最大抨击压力略有增加。当d≥1.6D时,间距对航行体的最大载荷和压力几乎没有影响。在入水过程中,双航行体头部内外两侧的压力分布呈现出不对称性。间距越小,这种相互干扰越显著,导致两侧载荷差异增大。外侧空腔自由发展,而内侧空腔则受到干扰,发展受限,进而使航行体尾部向内倾斜,产生尾拍现象。然而,随着间距的增加,双航行体内部空腔的发展和演化趋于平稳。
    结论 在双航行体并联结构入水时,空腔发展趋势显著,且其受到的相邻弹体的干扰程度与两者间距紧密相关,数值模拟成果为双航行体并联高速垂直入水载荷评估提供了重要的工程指导意义。

     

    Abstract:
    Objectives The cross-medium "swarm" penetration of multiple vehicles has attracted significant attention from researchers worldwide. To investigate the mutual interference between two vehicles during high-speed water entry, a numerical simulation is performed to analyze the high-speed water entry process of two parallel cone-shaped vehicles with varying spacing.
    Methods The present numerical model is based on Star CCM+. The turbulence calculations were performed using the Realizable kε turbulence model based on the Reynolds Averaged Navier-Stokes (RANS) approach. The volume of fluid (VOF) multiphase flow technique was employed to model the interaction of multiple fluids (air, water, and water vapor), capturing the motion of free surfaces within a single medium. The Schnerr-Sauer cavitation model was employed to calculate the vapor volume fraction, accounting for the phase change between water vapor and liquid. Additionally, the overset grid technology was applied to track the motion of the cylindrical projectile. The study explores the hydrodynamic characteristics, including the evolution of cavity shape, the pressure load on the head, and the motion trajectory of two parallel vehicles during water entry at different spacings d.
    Results Upon contact with the surface, the vehicle's load and the impulsive pressure on the head increase dramatically, reaching their maximum values instantly for different spacings, and then they quickly decrease. At a spacing of d = 0.8D, the maximum impact load is more than 20% greater than that at d = 1.6D, and the corresponding maximum impact pressure on the head slightly increases, where D is the diameter of the vehicle. However, when d≥1.6D, the spacing has little effect on the maximum load and pressure on the vehicle. During the water entry process, the pressure distribution on the inner and outer sides of the heads of the dual-body vehicles becomes unbalanced. The smaller the spacing, the more significant this mutual influence, resulting in greater load differences between the two sides. The cavity shape develops freely on the outer side but is restricted on the inner side due to interference. Consequently, the vehicle's tail tilts inward, producing a tail slap phenomenon. However, as the spacing increases, the development and evolution of the internal cavities of the dual-body vehicles become more gradual.
    Conclusions When the dual-body vehicle structure enters the water in parallel, the trend of cavity development becomes more pronounced. The degree of interference from adjacent projectiles is closely related to the distance between them. This numerical study provides engineering guidance for the load assessment of dual-body vehicles during high-speed vertical water entry.

     

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