Numerical Analysis for Supercavitation Characteristics around Underwater Vehicle according to Ventilated Gas Temperature

Hyun-Cheol Hwang, W. Park, N. V. Tu, Donghyun Kim, Nguyen Duy Trong
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Abstract

Supercavitation is a phenomenon in which the cavity covers the entire underwater vehicle. The purpose of this paper is to compare and analyze the thermal effect on the cavity characteristics by changing the ventilated gas temperature through computational analysis. For this study, a homogeneous mixture model based on the 3D Navier-Stokes equation was used. As a phase change model, it is its own code considering both pressure change and temperature change. A dimensionless number Tm was presented to analyze the numerical results, and as the Tm increased, the cavity length increased by about 3.6 times and the cavity width by about 3.3 times at 393.15 K compared to room temperature. Analyzing these thermal effects, it was confirmed that rapid heat exchange and heat transfer between the gas phase and the liquid phase occurred at the location where the ventilated gas was sprayed, affecting the cavity characteristics. In addition, it can be confirmed that the initial cavity surface becomes unstable as the ventilated gas temperature increases, and it can be confirmed based on the numerical analysis results that the critical temperature at which the cavity surface becomes unstable is 373.15 K.
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基于通风气体温度的水下航行器超空泡特性数值分析
超空化是一种空腔覆盖整个水下航行器的现象。本文的目的是通过计算分析,比较和分析改变通风气体温度对空腔特性的热效应。本研究采用基于三维Navier-Stokes方程的均匀混合模型。作为相变模型,它有自己的代码,同时考虑了压力变化和温度变化。采用无因次数Tm对数值结果进行分析,在393.15 K下,随着Tm的增大,腔长比室温增大约3.6倍,腔宽增加约3.3倍。通过对这些热效应的分析,证实了在通风气体喷射的位置,气相和液相之间发生了快速的换热和换热,影响了空腔的特性。另外,可以确定随着通风气体温度的升高,初始空腔表面变得不稳定,根据数值分析结果可以确定空腔表面变得不稳定的临界温度为373.15 K。
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