Abstract
This paper presents a systematic numerical investigation of different Implicit Large-Eddy Simulations (ILES) for massively separated flows. Three numerical schemes, a third-order MUSCL scheme, a fifth-order MUSCL scheme and a ninth-order accurate WENO method, are tested in the context of separation from a gently curved surface. The case considered here is a simple wall-bounded flow that consists of a channel with hill-type curvature on the lower wall. The separation and reattachment locations, velocity and stress profiles are presented and compared against solutions from classical LES simulations.
| Original language | English |
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| Publication status | Published - 10 Jan 2008 |
| Event | 46th AIAA Aerospace Sciences Meeting and Exhibit - Reno, NV, United States Duration: 7 Jan 2008 → 10 Jan 2008 |
Conference
| Conference | 46th AIAA Aerospace Sciences Meeting and Exhibit |
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| Country/Territory | United States |
| City | Reno, NV |
| Period | 7/01/08 → 10/01/08 |
Keywords
- aerospace engineering
- large eddy simulation
- curved surfaces
- internal flows
- massively separated flow
- numerical investigations
- numerical scheme
- stress profile