{"title":"球面周围三维湍流分离的非结构网格计算研究","authors":"S. Rhee, T. Hino","doi":"10.2534/JJASNAOE1968.2000.188_1","DOIUrl":null,"url":null,"abstract":"Laminar and turbulent separated flows around a 6 : 1 prolate spheroid are investigated using an unstructured grid CFD method. The RANS equations are solved for incompressible viscous flows. The artificial compressibility is introduced in the continuity equation and cell-centered finite-volume method on unstructured grid is used for spatial discretization. The Spalart-Allmaras one-equation turbulence model is employed for the Reynolds stress. The computational results are compared with experimental data and the physics of three-dimensional turbulent flow separation is confirmed. A range of Reynolds numbers and angles of attack is considered and the effects are investigated. The modification of the Spalart-Allmaras model is added to improve the performance and examine the effects of turbulence model on the vortical flow structure.","PeriodicalId":321056,"journal":{"name":"Journal of the Society of Naval Architects of Japan","volume":"26 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2000-12-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"20","resultStr":"{\"title\":\"Computational Investigation of 3D Turbulent Flow Separation around a Spheroid using an Unstructured Grid Method\",\"authors\":\"S. Rhee, T. Hino\",\"doi\":\"10.2534/JJASNAOE1968.2000.188_1\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"Laminar and turbulent separated flows around a 6 : 1 prolate spheroid are investigated using an unstructured grid CFD method. The RANS equations are solved for incompressible viscous flows. The artificial compressibility is introduced in the continuity equation and cell-centered finite-volume method on unstructured grid is used for spatial discretization. The Spalart-Allmaras one-equation turbulence model is employed for the Reynolds stress. The computational results are compared with experimental data and the physics of three-dimensional turbulent flow separation is confirmed. A range of Reynolds numbers and angles of attack is considered and the effects are investigated. The modification of the Spalart-Allmaras model is added to improve the performance and examine the effects of turbulence model on the vortical flow structure.\",\"PeriodicalId\":321056,\"journal\":{\"name\":\"Journal of the Society of Naval Architects of Japan\",\"volume\":\"26 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2000-12-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"20\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Journal of the Society of Naval Architects of Japan\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.2534/JJASNAOE1968.2000.188_1\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Journal of the Society of Naval Architects of Japan","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.2534/JJASNAOE1968.2000.188_1","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Computational Investigation of 3D Turbulent Flow Separation around a Spheroid using an Unstructured Grid Method
Laminar and turbulent separated flows around a 6 : 1 prolate spheroid are investigated using an unstructured grid CFD method. The RANS equations are solved for incompressible viscous flows. The artificial compressibility is introduced in the continuity equation and cell-centered finite-volume method on unstructured grid is used for spatial discretization. The Spalart-Allmaras one-equation turbulence model is employed for the Reynolds stress. The computational results are compared with experimental data and the physics of three-dimensional turbulent flow separation is confirmed. A range of Reynolds numbers and angles of attack is considered and the effects are investigated. The modification of the Spalart-Allmaras model is added to improve the performance and examine the effects of turbulence model on the vortical flow structure.