Please use this identifier to cite or link to this item: http://hdl.handle.net/10397/101421
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dc.contributorDepartment of Aeronautical and Aviation Engineeringen_US
dc.creatorLong, Ten_US
dc.creatorGuo, Pen_US
dc.creatorZhao, Ren_US
dc.creatorWen, Cen_US
dc.creatorJi, Fen_US
dc.date.accessioned2023-09-18T02:25:39Z-
dc.date.available2023-09-18T02:25:39Z-
dc.identifier.issn1070-6631en_US
dc.identifier.urihttp://hdl.handle.net/10397/101421-
dc.language.isoenen_US
dc.publisherAmerican Institute of Physicsen_US
dc.rights© 2023 Author(s). Published under an exclusive license by AIP Publishing.en_US
dc.rightsThis article may be downloaded for personal use only. Any other use requires prior permission of the author and AIP Publishing. This article appeared in Tiehan Long, Peixu Guo, Rui Zhao, Chihyung Wen, Feng Ji; Energy growth of vortical, acoustic, and entropic components of the second-mode instability in the hypersonic boundary layer. Physics of Fluids 1 May 2023; 35 (5): 054104 and may be found at https://dx.doi.org/10.1063/5.0141414.en_US
dc.titleEnergy growth of vortical, acoustic, and entropic components of the second-mode instability in the hypersonic boundary layeren_US
dc.typeJournal/Magazine Articleen_US
dc.identifier.volume35en_US
dc.identifier.issue5en_US
dc.identifier.doi10.1063/5.0141414en_US
dcterms.abstractThe acoustic, vortical, and entropic (thermal) components of the second-mode instability, regarded as an asymptotic behavior of the free-stream counterparts, were found to interact with each other in a well-defined way. However, the mechanisms of the energy growth of each component and the resulting second mode instability remain to be clarified. The present paper provides a quantitative energy analysis of the key sources responsible for the modal growth in the momentum potential theory framework. The acoustic, vortical, and entropic components are governed by energy source effects and interexchange effects, characterized by explicit transport terms and relationships between the growth rate and the energy source. The thermal-acoustic source, induced by the interaction between the fluctuation pressure and the fluctuation entropy, is revealed to be the most pronounced cause of the second-mode instability in the hypersonic boundary layer. The thermal-acoustic source is further decomposed into the dissipative (viscous) part and the non-dissipative (inviscid) part. The dissipative thermal-acoustic source is dominant near the wall surface and destabilizes the second mode. The non-dissipative thermal-acoustic source destabilizes the second mode significantly at the critical layer, while the dissipative thermal-acoustic source stabilizes the second mode in this region.en_US
dcterms.accessRightsopen accessen_US
dcterms.bibliographicCitationPhysics of fluids, May 2023, v. 35, no. 5, 054104en_US
dcterms.isPartOfPhysics of fluidsen_US
dcterms.issued2023-05-
dc.identifier.scopus2-s2.0-85158816455-
dc.identifier.ros2022001753-
dc.identifier.eissn1089-7666en_US
dc.identifier.artn054104en_US
dc.description.validate202309 bckwen_US
dc.description.oaVersion of Recorden_US
dc.identifier.FolderNumberCDCF_2022-2023-
dc.description.fundingSourceRGCen_US
dc.description.fundingSourceOthersen_US
dc.description.fundingTextNational Natural Science Foundation of Chinaen_US
dc.description.pubStatusPublisheden_US
dc.description.oaCategoryVoR alloweden_US
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