Comparative study on the high-speed water entry movement process of revolving bodies with different head shapes
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摘要: 跨介质回转体武器在对水下目标发动攻击时, 都要经历一个从空中弹道转变为水下弹道的跨介质入水过程, 这是一个时间极短的瞬态流动过程, 涉及到运动物体与气相和液相的复杂多相流动。文中基于雷诺时均方程, 并考虑自然空化现象的多相流模型, 建立了入水空泡动力学数值模型, 并研究了回转体垂直入水过程运动特性和流体动力的影响规律。通过数值仿真结果与文献中试验结果对比, 验证了模型和数值方法的有效性。结果表明, 不同头型回转体入水后的空泡特征与运动速度规律有很大的差异, 同时可知其相应瞬态阻力系数也表现出很大差异; 在空泡闭合前, 体现出明显的回射流效应, 并影响空泡形态与回转体阻力的变化; 回转体的入水速度对空泡尺寸和冲击载荷具有非常直接的影响, 入水速度较低时回转体速度衰减相对更快, 阻力系数相对更大。Abstract: For the high-speed vehicles moving from air to water, it involves multiphase flow of vapor, gas and liquid in a very short time. In this paper, numerical simulations are performed for understanding the vertical water entry process. In the numerical simulation, Reynolds Averaged Navier-Stokes(RANS) equations is solved to consider the influence of turbulence. Eulerian multiphase flow with cavitation is included for the moving body implemented by dynamical mesh. The numerical results are validated by the existing experimental results. The results show that the cavitation characteristics and the speed of different head-shaped aircraft after entering the water have a great influence. At the same time, it can be observed that the corresponding transient drag coefficients also show great differences. The back-jet effect is already evident before the cavity is closed, and affects the cavity shape and motion of the revolving body. The water entry speed of the revolving body has a very direct impact on the cavitation size and impact load. When the speed of entering the water is low, the speed of the object decays relatively faster, and its instantaneous drag coefficient is relatively larger.
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Key words:
- Revolving body /
- Water entry /
- Cavitation /
- Numerical simulation
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表 1 网格与时间步设置及最终速度误差
Table 1. Setup of grid number and time step, and its error
网格 网格数 内层网格
尺寸/mm时间步长
/10−7s误差
/%1 66万 0.05 1.18 0.20 2 46万 0.07 1.65 1.00 3 32万 0.10 2.36 4.00 4 22万 0.14 3.30 8.50 5 15万 0.20 4.72 13.80 -
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