Prediction and Analysis of Transitional Crossflows Using gamma - Re-theta t - CF+ ModelPrediction and Analysis of Transitional Crossflows Using γ−Reθt−CF+ Model

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dc.contributor.authorPark, Sang Hyunko
dc.contributor.authorHan, Jaeseongko
dc.contributor.authorKwon, Oh Joonko
dc.date.accessioned2022-07-13T05:01:47Z-
dc.date.available2022-07-13T05:01:47Z-
dc.date.created2022-05-06-
dc.date.created2022-05-06-
dc.date.created2022-05-06-
dc.date.issued2022-07-
dc.identifier.citationINTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES, v.23, no.3, pp.461 - 470-
dc.identifier.issn2093-274X-
dc.identifier.urihttp://hdl.handle.net/10203/297362-
dc.description.abstractIn the present study, numerical assessment of the gamma - Re-theta t - CF+ transition model was carried out using a Reynolds-averaged Navier-Stokes (RANS) computational fluid dynamics (CFD) flow solver based on unstructured meshes. A three-dimensional bump-in-channel verification case was first tested in a fully turbulent manner to verify the implementation of the k - omega shear stress transport turbulence model, which was coupled with the laminar-turbulent transition model. In addition, to validate the gamma - Re-theta t - CF+ transition model, transition onset locations were compared with the experimental results for three angles-of-attack with a 6:1 prolate spheroid configuration. Then, the gamma - Re-theta t - CF+ transition model was utilized to predict the skin friction distributions, surface pressure distributions, and transition onset locations of the natural-laminar-flow version of the common research model (CRM-NLF). For this purpose, a grid-resolution study was carried out for a fixed angle-of-attack on coarse, medium, and fine meshes. The aerodynamic performance of the CRM-NFL was compared with the experimental for four angles of attack.-
dc.languageEnglish-
dc.publisherSPRINGER-
dc.titlePrediction and Analysis of Transitional Crossflows Using gamma - Re-theta t - CF+ Model-
dc.title.alternativePrediction and Analysis of Transitional Crossflows Using γ−Reθt−CF+ Model-
dc.typeArticle-
dc.identifier.wosid000785688700001-
dc.identifier.scopusid2-s2.0-85128768409-
dc.type.rimsART-
dc.citation.volume23-
dc.citation.issue3-
dc.citation.beginningpage461-
dc.citation.endingpage470-
dc.citation.publicationnameINTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES-
dc.identifier.doi10.1007/s42405-022-00457-4-
dc.identifier.kciidART002859959-
dc.contributor.localauthorKwon, Oh Joon-
dc.description.isOpenAccessN-
dc.type.journalArticleArticle-
dc.subject.keywordAuthorgamma-
dc.subject.keywordAuthor6:1 prolate spheroid-
dc.subject.keywordAuthorCRM model-
dc.subject.keywordAuthorUnstructured meshes-
dc.subject.keywordAuthorRe-theta t -CF+ transition model-
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AE-Journal Papers(저널논문)
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