Detached-eddy simulation for airfoil stall

Dong Li, Yu Qin Jiao, Igor Men'shov, Yoshiaki Nakamura

科研成果: 期刊稿件文章同行评审

9 引用 (Scopus)

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
26
4
出版状态已出版 - 7月 2005

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