{"title":"可压缩超音速流动激波/湍流边界层相互作用的数值模拟","authors":"Bahia Dris, Barkani Jamal","doi":"10.1109/ISACS48493.2019.9068904","DOIUrl":null,"url":null,"abstract":"This paper is devoted to the numerical study of two-dimensional systems of conservation laws describing unsteady flows, supersonic, compressible and turbulent. The structured grids finite volume method is adopted here as well as the algebraic model of Baldwin and Lomax is used for the modelling of eddy viscosity. This model of turbulence was examined on two applications: the isothermal flat plate and the compression corner of 10°.","PeriodicalId":312521,"journal":{"name":"2019 International Conference on Intelligent Systems and Advanced Computing Sciences (ISACS)","volume":"66 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2019-12-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Numerical Modelling Of The Interaction Shock / Turbulent Boundary Layer For A Compressible Supersonic Flow\",\"authors\":\"Bahia Dris, Barkani Jamal\",\"doi\":\"10.1109/ISACS48493.2019.9068904\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"This paper is devoted to the numerical study of two-dimensional systems of conservation laws describing unsteady flows, supersonic, compressible and turbulent. The structured grids finite volume method is adopted here as well as the algebraic model of Baldwin and Lomax is used for the modelling of eddy viscosity. This model of turbulence was examined on two applications: the isothermal flat plate and the compression corner of 10°.\",\"PeriodicalId\":312521,\"journal\":{\"name\":\"2019 International Conference on Intelligent Systems and Advanced Computing Sciences (ISACS)\",\"volume\":\"66 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2019-12-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2019 International Conference on Intelligent Systems and Advanced Computing Sciences (ISACS)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/ISACS48493.2019.9068904\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2019 International Conference on Intelligent Systems and Advanced Computing Sciences (ISACS)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/ISACS48493.2019.9068904","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Numerical Modelling Of The Interaction Shock / Turbulent Boundary Layer For A Compressible Supersonic Flow
This paper is devoted to the numerical study of two-dimensional systems of conservation laws describing unsteady flows, supersonic, compressible and turbulent. The structured grids finite volume method is adopted here as well as the algebraic model of Baldwin and Lomax is used for the modelling of eddy viscosity. This model of turbulence was examined on two applications: the isothermal flat plate and the compression corner of 10°.
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