摘要
Detached-eddy simulation (DES) is applied to three airfoils with different stall types. The method combines the strong points of Reynolds-averaged Navier-Stokes and large eddy simulation approaches. Spalart-Allmaras model is basically used, which reduces to a RANS formulation near a solid surface and to a subgrid model away from the wall. LU-SGS implicit scheme is employed to solve the model in time. Comparing with the experimental data, it is found that stall angle can be reasonably predicted by the present method.
| 源语言 | 英语 |
|---|---|
| 页(从-至) | 406-410 |
| 页数 | 5 |
| 期刊 | Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica |
| 卷 | 26 |
| 期 | 4 |
| 出版状态 | 已出版 - 7月 2005 |
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