Philip L. Lederer, Xaver Mooslechner, Joachim Schöberl
{"title":"基于高阶投影的上风法模拟过渡湍流","authors":"Philip L. Lederer, Xaver Mooslechner, Joachim Schöberl","doi":"arxiv-2408.06698","DOIUrl":null,"url":null,"abstract":"We present a scalable, high-order implicit large-eddy simulation (ILES)\napproach for incompressible transitional flows. This method employs the\nmass-conserving mixed stress (MCS) method for discretizing the Navier-Stokes\nequations. The MCS method's low dissipation characteristics, combined with the\nintroduced operator-splitting solution technique, result in a high-order solver\noptimized for efficient and parallel computation of under-resolved turbulent\nflows. We further enhance the inherent capabilities of the ILES model by\nincorporating high-order upwind fluxes and are examining its approximation\nbehaviour in transitional aerodynamic flow problems. In this study, we use\nflows over the Eppler 387 airfoil at Reynolds numbers up to $3 \\cdot 10^5$ as\nbenchmarks for our simulations.","PeriodicalId":501309,"journal":{"name":"arXiv - CS - Computational Engineering, Finance, and Science","volume":null,"pages":null},"PeriodicalIF":0.0000,"publicationDate":"2024-08-13","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"High-order projection-based upwind method for simulation of transitional turbulent flows\",\"authors\":\"Philip L. Lederer, Xaver Mooslechner, Joachim Schöberl\",\"doi\":\"arxiv-2408.06698\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"We present a scalable, high-order implicit large-eddy simulation (ILES)\\napproach for incompressible transitional flows. This method employs the\\nmass-conserving mixed stress (MCS) method for discretizing the Navier-Stokes\\nequations. The MCS method's low dissipation characteristics, combined with the\\nintroduced operator-splitting solution technique, result in a high-order solver\\noptimized for efficient and parallel computation of under-resolved turbulent\\nflows. We further enhance the inherent capabilities of the ILES model by\\nincorporating high-order upwind fluxes and are examining its approximation\\nbehaviour in transitional aerodynamic flow problems. In this study, we use\\nflows over the Eppler 387 airfoil at Reynolds numbers up to $3 \\\\cdot 10^5$ as\\nbenchmarks for our simulations.\",\"PeriodicalId\":501309,\"journal\":{\"name\":\"arXiv - CS - Computational Engineering, Finance, and Science\",\"volume\":null,\"pages\":null},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2024-08-13\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"arXiv - CS - Computational Engineering, Finance, and Science\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/arxiv-2408.06698\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"arXiv - CS - Computational Engineering, Finance, and Science","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/arxiv-2408.06698","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
High-order projection-based upwind method for simulation of transitional turbulent flows
We present a scalable, high-order implicit large-eddy simulation (ILES)
approach for incompressible transitional flows. This method employs the
mass-conserving mixed stress (MCS) method for discretizing the Navier-Stokes
equations. The MCS method's low dissipation characteristics, combined with the
introduced operator-splitting solution technique, result in a high-order solver
optimized for efficient and parallel computation of under-resolved turbulent
flows. We further enhance the inherent capabilities of the ILES model by
incorporating high-order upwind fluxes and are examining its approximation
behaviour in transitional aerodynamic flow problems. In this study, we use
flows over the Eppler 387 airfoil at Reynolds numbers up to $3 \cdot 10^5$ as
benchmarks for our simulations.