Please use this identifier to cite or link to this item:
Full metadata record
DC FieldValueLanguage
dc.contributor.authorSingh, Satyviren_US
dc.identifier.citationSingh, S. (2020). Role of Atwood number on flow morphology of a planar shock-accelerated square bubble : a numerical study. Physics of Fluids, 32(12), 126112-.
dc.description.abstractThe Atwood number plays a critical role in describing the physics of fluids behind the hydrodynamic instabilities in gas dynamics. In order to investigate the impacts of the Atwood number (At), the evolution of a shock-accelerated square bubble containing either SF6, Kr, Ar, Ne, or He and surrounded by N2 is investigated numerically. For this purpose, the unsteady compressible Navier-Stokes-Fourier equations are solved using an explicit modal discontinuous Galerkin method. For validation, the numerical results are compared with available experimental results and are found to be in good agreement. The results demonstrate that the Atwood number has a significant influence on flow morphology with wave patterns, vortex creation, vorticity generation, and bubble deformation. For At > 0, the speed of the shock wave traveling along with the bubble inner surface is often less than that of the incident shock wave and greater than that of the transmitted shock wave. Moreover, vortex pairs from the upstream and downstream corners are generated, and the former vortex pair ultimately dominates the flow morphology. For At ≈ 0, the incident and transmitted shock waves move at the same speeds, whereas for At < 0, the transmitted shock wave travels faster than the incident shock wave. Moreover, only one vortex pair at the upstream corners is generated, which dominates the flow morphology. Furthermore, a detailed study of Atwood number impacts is investigated through the vorticity generation at interfaces. A quantitative analysis based on the shock trajectories, the interface features, and the integral diagnostics is also studied in detail to investigate the impacts of the Atwood number on the flow structure. Finally, a comparative study of the flow physics between the shock-accelerated square and cylindrical bubbles is conducted to examine their natural differences.en_US
dc.description.sponsorshipNanyang Technological Universityen_US
dc.relationNAP, M408074en_US
dc.relation.ispartofPhysics of Fluidsen_US
dc.rights© 2020 The Author(s). All rights reserved. This paper was published by AIP Publishing in Physics of Fluids and is made available with permission of The Author(s).en_US
dc.subjectEngineering::Mechanical engineering::Fluid mechanicsen_US
dc.titleRole of Atwood number on flow morphology of a planar shock-accelerated square bubble : a numerical studyen_US
dc.typeJournal Articleen
dc.contributor.schoolSchool of Physical and Mathematical Sciencesen_US
dc.description.versionPublished versionen_US
dc.subject.keywordsFluid Instabilitiesen_US
dc.subject.keywordsFluid Mechanicsen_US
dc.description.acknowledgementThe author acknowledges the financial support provided by the Nanyang Technological University, Singapore, through the NAP-SUG grant.en_US
item.fulltextWith Fulltext-
Appears in Collections:SPMS Journal Articles
Files in This Item:
File Description SizeFormat 
role of atwood.pdf17.47 MBAdobe PDFThumbnail

Citations 20

Updated on Mar 18, 2023

Web of ScienceTM
Citations 20

Updated on Mar 20, 2023

Page view(s)

Updated on Mar 20, 2023

Download(s) 50

Updated on Mar 20, 2023

Google ScholarTM




Items in DR-NTU are protected by copyright, with all rights reserved, unless otherwise indicated.