DC Field | Value | Language |
---|---|---|
dc.contributor.author | Park, Sang Hyun | ko |
dc.contributor.author | Han, Jaeseong | ko |
dc.contributor.author | Kwon, Oh Joon | ko |
dc.date.accessioned | 2022-07-13T05:01:47Z | - |
dc.date.available | 2022-07-13T05:01:47Z | - |
dc.date.created | 2022-05-06 | - |
dc.date.created | 2022-05-06 | - |
dc.date.created | 2022-05-06 | - |
dc.date.issued | 2022-07 | - |
dc.identifier.citation | INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES, v.23, no.3, pp.461 - 470 | - |
dc.identifier.issn | 2093-274X | - |
dc.identifier.uri | http://hdl.handle.net/10203/297362 | - |
dc.description.abstract | In 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.language | English | - |
dc.publisher | SPRINGER | - |
dc.title | Prediction and Analysis of Transitional Crossflows Using gamma - Re-theta t - CF+ Model | - |
dc.title.alternative | Prediction and Analysis of Transitional Crossflows Using γ−Reθt−CF+ Model | - |
dc.type | Article | - |
dc.identifier.wosid | 000785688700001 | - |
dc.identifier.scopusid | 2-s2.0-85128768409 | - |
dc.type.rims | ART | - |
dc.citation.volume | 23 | - |
dc.citation.issue | 3 | - |
dc.citation.beginningpage | 461 | - |
dc.citation.endingpage | 470 | - |
dc.citation.publicationname | INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES | - |
dc.identifier.doi | 10.1007/s42405-022-00457-4 | - |
dc.identifier.kciid | ART002859959 | - |
dc.contributor.localauthor | Kwon, Oh Joon | - |
dc.description.isOpenAccess | N | - |
dc.type.journalArticle | Article | - |
dc.subject.keywordAuthor | gamma | - |
dc.subject.keywordAuthor | 6:1 prolate spheroid | - |
dc.subject.keywordAuthor | CRM model | - |
dc.subject.keywordAuthor | Unstructured meshes | - |
dc.subject.keywordAuthor | Re-theta t -CF+ transition model | - |
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