摘要:
为揭示入水角度与尾翼对高速入水弹体横向冲击载荷和弹道特性影响规律,本文基于流体域体积(Volume of Fluid, VOF)多相流方法、改进的延迟分离涡模拟(Improved Delayed Detached-Eddy Simulation, IDDES)湍流模型及Schnerr-Sauer空化模型,建立了弹体倾斜入水的数值仿真模型,并通过水平入水实验验证数值仿真模型。通过数值模拟系统研究了入水角度、弹体密度及尾翼结构有无对弹体高速倾斜入水过程的影响。研究结果表明:不同入水角度弹体在水下均经历多周期尾拍运动,小角度入水具有更低的水下环境压力因而提升水下侵彻距离;提升弹体密度可增加尾拍次数,延长尾拍周期从而提升侵彻距离;弹体密度的提升降低了弹体横向过载,速度衰减更慢,尾拍阶段的侵彻距离大幅提升。
关键词:
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水下运动 /
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尾翼 /
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冲击载荷 /
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空泡 /
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尾拍
Abstract:
Based on the VOF multiphase flow method, IDDES turbulence model and Schnerr-Sauer cavitation model, a numerical simulation model of a projectile with tail fins inclined into the water is established to reveal the influence of water entry angle and tail fins on the transverse impact load and ballistic characteristics of high-speed projectiles. Horizontal water entry tests were conducted using a 120-mm balanced gun launcher, an assembled water tank, a high-speed camera system, and acceleration recorders. The test projectile consisted of a nose cavitator, a middle conical section, an aft cylindrical section, and tail fins. The underwater motion attitude and cavity evolution of the projectile were captured, and the triaxial impact load histories were recorded. By comparing the cavity evolution and transverse impact load time histories between the experiment and simulation, the computational accuracy of the simulation model was validated. And the mesh independence of the simulation model was verified. The validated model was then used to investigate the effects of different water entry angles, projectile densities, and the presence or absence of tail fins on the transverse impact loads and ballistic characteristics during high-speed oblique water entry of a cylinder-cone projectile with an angle of attack. The results show that the projectiles with different entry angles underwater all undergo several tail-slapping motions, with the low-angle entry has lower underwater environmental pressure, thus increasing the underwater penetration distance. Increasing the projectile density increases the number of tail slaps and prolongs the tail-slap period, thereby increasing the penetration distance. Increasing the projectile density also reduces the transverse overload and leads to slower velocity attenuation, substantially increasing the penetration distance during the tail-slap stage.