Please use this identifier to cite or link to this item: http://hdl.handle.net/10397/93023
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dc.contributorDepartment of Mechanical Engineeringen_US
dc.contributorDepartment of Aeronautical and Aviation Engineeringen_US
dc.creatorGuan, Ben_US
dc.creatorWang, Den_US
dc.creatorWang, Gen_US
dc.creatorFan, Een_US
dc.creatorWen, CYen_US
dc.date.accessioned2022-05-30T07:40:08Z-
dc.date.available2022-05-30T07:40:08Z-
dc.identifier.issn1070-6631en_US
dc.identifier.urihttp://hdl.handle.net/10397/93023-
dc.language.isoenen_US
dc.publisherAmerican Institute of Physicsen_US
dc.rights© 2020 Author(s).en_US
dc.rightsThis article may be downloaded for personal use only. Any otheruse requires prior permission of the author and AIP Publishing. This article appeared in Guan, B., Wang, D., Wang, G., Fan, E., & Wen, C. Y. (2020). Numerical study of the Richtmyer–Meshkov instability of a three-dimensional minimum-surface featured SF6/air interface. Physics of Fluids, 32(2), 024108 and may be found at https://doi.org/10.1063/1.5141783.en_US
dc.titleNumerical study of the richtmyer-meshkov instability of a three-dimensional minimum-surface featured SF6/air interfaceen_US
dc.typeJournal/Magazine Articleen_US
dc.identifier.volume32en_US
dc.identifier.issue2en_US
dc.identifier.doi10.1063/1.5141783en_US
dcterms.abstractThe Richtmyer-Meshkov instability of a three-dimensional (3D) minimum-surface featured SF6/air interface subjected to a planar weak incident shock is numerically studied. The focus is placed on presenting more intuitive details of the complex shock-interface interactions. In the present work, 3D Euler equations are solved. The fifth-order weighted essentially non-oscillatory scheme and the level-set method combined with the real ghost fluid method are adopted. The gas interface morphologies are precisely reproduced according to the previous experimental images, the wave systems in 3D space are illustrated, and the velocity distribution in a characteristic plane is depicted. Based on which, the unknown lagging structure in the previous experiment can be reasonably explained. It is actually the soap fog driven by the flow field. The baroclinic vorticity generation and the perturbation amplitude growth histories are measured. The present numerical study well confirms the 3D curvature effect and supports the extended 3D theoretical model for the heavy/light interface scenario.en_US
dcterms.accessRightsopen accessen_US
dcterms.bibliographicCitationPhysics of fluids, Feb. 2020, v. 32, no. 2, 24108en_US
dcterms.isPartOfPhysics of fluidsen_US
dcterms.issued2020-02-
dc.identifier.scopus2-s2.0-85079779590-
dc.identifier.eissn1089-7666en_US
dc.identifier.artn24108en_US
dc.description.validate202205 bchyen_US
dc.description.oaVersion of Recorden_US
dc.identifier.FolderNumberME-0305-
dc.description.fundingSourceOthersen_US
dc.description.fundingTextNational Natural Science Foundation of Chinaen_US
dc.description.pubStatusPublisheden_US
dc.identifier.OPUS20514899-
dc.description.oaCategoryVoR alloweden_US
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