Abstract

Autonomous underwater vehicle will be subjected to a huge impact load during high speed water entry, which will damage the structure and the internal instruments of the vehicle. Therefore, it is of great significance to study the buffer mechanism of the vehicle during the process of water-entry. In this paper, a kind of head-jetting device with disk cavitation is used. The complex cavitation forms, under the three-phase coupling of gas, liquid and solid, in the water entry process of the vehicle on which the device is installed. In this paper, the numerical simulation of high-speed water entry of the vehicle equipped with head jet device is carried out. Through the analysis of water entry cavitation under typical working conditions, the following conclusions are obtained. After the installation of head jet device, the water entry cavity of the vehicle changes gradually from cone to spindle shape. The air jet, compared with that without jet, can promote the formation of water inlet supercavitation, decrease the interaction area between the vehicle and water, and reduce the impact load during water entry. At the same water entry depth, the diameter of cavitation increases with the amount of air jet. The water entry velocity has a great influence on the difference of cavitation shape. The water entry depth closure phenomenon, when the water entry velocity is less than 100 m/s, can be observed in the depth of 3.5 times of the projectile length. The water entry angle has a significant effect on the cavitation shape. The cavity shows obvious asymmetry when the vehicle slants into the water, and the diameter and length of the bubbles decrease with the increase of the water entry angle. The research content of this paper provides technical support for the engineering practice of high-speed water entry and load reduction, and the conclusions are of great significance in related fields.

Highlights

  • Autonomous underwater vehicle will be subjected to a huge impact load during high speed water entry, which will damage the structure and the internal instruments of the vehicle

  • At the same water entry depth, the diameter of cavitation increases with the amount of air jet

  • The water entry velocity has a great influence on the difference of cavitation shape

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Summary

Introduction

西北工业大学学报 Journal of Northwestern Polytechnical University https: / / doi.org / 10.1051 / jnwpu / 20213940810 入水冲击载荷方面。 理论研究多基于势流理论 开展,最早由 von Karman[1] 提出了近似平板理论,这 成为后来很多学者研究相关问题的理论依据。 但是 该理论忽略了液面隆起现象的影响,之后 Wagner[2] 对其进行改进提出了自相似解法,得到了入水冲击 压强峰值与速度平方成正比的结论。 Pukhnachov[3] 提出了匹配渐进展开法来研究非线性因素在入水问 题中的影响。 Chuang[4⁃5] 对平底物体入水开展了试 验研究,发现了空气垫的存在。 陈震等[6] 通过数值 模拟,也得出了空气垫在平底物体入水冲击中具有 重要作用的结论。 律提出了空泡独立扩张原理,能够对空泡形态进行 理论预报。 Duclaux 等[8] 基于 Besant⁃Rayleigh 气泡 平衡理论推导了入水空泡半径与时间的函数关系, 得到了 与试验结果吻合较好的结果。 Worthington 等[9] 最早用闪光照相机开展了球体垂直入水的试 验 研 究, 并对其空泡形态进行了观测和描述。 Bell[10] 和 Maccoll[11] 通过对入水空泡试验进行观测,总结了空泡生成和演化过程中的流动特征,并分 析了空泡的形成机理。 马庆鹏等[12] 通过求解雷诺 时均的纳维斯托克斯方程,开展了锥头圆柱体高速 垂直入水的数值模拟研究,得到了不同锥角头型与 入水弹道和空泡半径等流场特性间的关系。 由上文可知,航行器入水过程中只有监测点 1, 2,3 和 7 有明显的压强变化,因此下面将分别对比 不同喷气量下监测点 1,2,3 和 7 压强曲线的变化, 分析喷 气量的改变对于航行器所受冲击压强的 影响。

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