Abstract
Simulations of compressible boundary layer flow at three different Reynolds numbers (Reδ = 5.59×104, 1.78×105, and 1.58×106) are performed using a hybrid large-eddy/Reynolds- averaged Navier-Stokes method. Variations in the recycling/rescaling method, the higher-order extension, the choice of primitive variables, the RANS/LES transition parameters, and the mesh resolution are considered in order to assess the model. The results indicate that the present model can provide good predictions of the mean flow properties and second-moment statistics of the boundary layers considered. Normalized Reynolds stresses in the outer layer are found to be independent of Reynolds number, similar to incompressible turbulent boundary layers.
| Original language | English |
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| Title of host publication | 38th AIAA Fluid Dynamics Conference and Exhibit |
| Publication status | Published - 2008 Dec 1 |
| Event | 38th AIAA Fluid Dynamics Conference and Exhibit - Seattle, WA, United States Duration: 2008 Jun 23 → 2008 Jun 26 |
Publication series
| Name | 38th AIAA Fluid Dynamics Conference and Exhibit |
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Other
| Other | 38th AIAA Fluid Dynamics Conference and Exhibit |
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| Country | United States |
| City | Seattle, WA |
| Period | 08/6/23 → 08/6/26 |
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All Science Journal Classification (ASJC) codes
- Engineering(all)
Cite this
Choi, J. I., Edwards, J. R., & Baurle, R. A. (2008). Compressible boundary layer predictions at high Reynolds number using hybrid LES/RANS methods. In 38th AIAA Fluid Dynamics Conference and Exhibit [2008-4175] (38th AIAA Fluid Dynamics Conference and Exhibit).