Numerical Simulation of the Interaction between a Planar Shock Wave and a Cylindrical Bubble

IF 1.8
Modelling Pub Date : 2024-04-16 DOI:10.3390/modelling5020026
S. Onwuegbu, Zhiyin Yang, Jianfei Xie
{"title":"Numerical Simulation of the Interaction between a Planar Shock Wave and a Cylindrical Bubble","authors":"S. Onwuegbu, Zhiyin Yang, Jianfei Xie","doi":"10.3390/modelling5020026","DOIUrl":null,"url":null,"abstract":"Three-dimensional (3D) computational fluid dynamics (CFD) simulations have been carried out to investigate the complex interaction of a planar shock wave (Ma = 1.22) with a cylindrical bubble. The unsteady Reynolds-averaged Navier–Stokes (URANS) approach with a level set coupled with volume of fluid (LSVOF) method has been applied in the present study. The predicted velocities of refracted wave, transmitted wave, upstream interface, downstream interface, jet, and vortex filaments are in very good agreement with the experimental data. The predicted non-dimensional bubble and vortex velocities also have great concordance with the experimental data compared with a simple model of shock-induced Rayleigh–Taylor instability (i.e., Richtmyer–Meshkov instability) and other theoretical models. The simulated changes in the bubble shape and size (length and width) against time agree very well with the experimental results. Comprehensive flow analysis has shown the shock–bubble interaction (SBI) process clearly from the onset of bubble compression up to the formation of vortex filaments, especially elucidating the mechanism on the air–jet formation and its development. It is demonstrated for the first time that turbulence is generated at the early phase of the shock cylindrical bubble interaction process, with the maximum turbulence intensity reaching about 20% around the vortex filament regions at the later phase of the interaction process.","PeriodicalId":504049,"journal":{"name":"Modelling","volume":"11 16","pages":""},"PeriodicalIF":1.8000,"publicationDate":"2024-04-16","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Modelling","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.3390/modelling5020026","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 0

Abstract

Three-dimensional (3D) computational fluid dynamics (CFD) simulations have been carried out to investigate the complex interaction of a planar shock wave (Ma = 1.22) with a cylindrical bubble. The unsteady Reynolds-averaged Navier–Stokes (URANS) approach with a level set coupled with volume of fluid (LSVOF) method has been applied in the present study. The predicted velocities of refracted wave, transmitted wave, upstream interface, downstream interface, jet, and vortex filaments are in very good agreement with the experimental data. The predicted non-dimensional bubble and vortex velocities also have great concordance with the experimental data compared with a simple model of shock-induced Rayleigh–Taylor instability (i.e., Richtmyer–Meshkov instability) and other theoretical models. The simulated changes in the bubble shape and size (length and width) against time agree very well with the experimental results. Comprehensive flow analysis has shown the shock–bubble interaction (SBI) process clearly from the onset of bubble compression up to the formation of vortex filaments, especially elucidating the mechanism on the air–jet formation and its development. It is demonstrated for the first time that turbulence is generated at the early phase of the shock cylindrical bubble interaction process, with the maximum turbulence intensity reaching about 20% around the vortex filament regions at the later phase of the interaction process.
平面冲击波与圆柱形气泡相互作用的数值模拟
为研究平面冲击波(Ma = 1.22)与圆柱形气泡的复杂相互作用,我们进行了三维计算流体动力学(CFD)模拟。本研究采用了带有液位集耦合流体体积(LSVOF)方法的非稳态雷诺平均纳维-斯托克斯(URANS)方法。折射波、透射波、上游界面、下游界面、射流和涡丝的预测速度与实验数据非常吻合。与冲击诱导的雷利-泰勒不稳定性简单模型(即 Richtmyer-Meshkov 不稳定性)和其他理论模型相比,预测的非尺寸气泡和涡流速度与实验数据也非常一致。模拟的气泡形状和大小(长度和宽度)随时间的变化与实验结果非常吻合。全面的流动分析清楚地显示了从气泡压缩开始到涡旋丝形成的冲击-气泡相互作用(SBI)过程,特别是阐明了气流形成及其发展的机制。研究首次证明,湍流产生于冲击圆柱气泡相互作用过程的早期阶段,在相互作用过程的后期阶段,涡旋丝区域周围的最大湍流强度达到约 20%。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
求助全文
约1分钟内获得全文 求助全文
来源期刊
CiteScore
2.70
自引率
0.00%
发文量
0
×
引用
GB/T 7714-2015
复制
MLA
复制
APA
复制
导出至
BibTeX EndNote RefMan NoteFirst NoteExpress
×
提示
您的信息不完整,为了账户安全,请先补充。
现在去补充
×
提示
您因"违规操作"
具体请查看互助需知
我知道了
×
提示
确定
请完成安全验证×
copy
已复制链接
快去分享给好友吧!
我知道了
右上角分享
点击右上角分享
0
联系我们:info@booksci.cn Book学术提供免费学术资源搜索服务,方便国内外学者检索中英文文献。致力于提供最便捷和优质的服务体验。 Copyright © 2023 布克学术 All rights reserved.
京ICP备2023020795号-1
ghs 京公网安备 11010802042870号
Book学术文献互助
Book学术文献互助群
群 号:604180095
Book学术官方微信
小红书