摘要
Numerical method based on turbulence model to predict flow transition is studied. By using k-ω SST two-equation model to simulate the flat plate boundary layer, it is shown that the k-ω SST model can capture the transition phenomena but the predicted transition point is far prior to the measured position. So, the mixing length scale in the k-ω SST model is modified according to the characteristic of transition flow and a modified k-ω SST two-equation model taking account of intermittence function effect is put forward. By using this modified k-ω SST model to simulate the flat plate boundary layer and the flow past NACA0012 at different incidences, it is seen that rational results are obtained and the modified model can predict the transition position with certain accuracy.
源语言 | 英语 |
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页(从-至) | 502-507 |
页数 | 6 |
期刊 | Kongqi Donglixue Xuebao/Acta Aerodynamica Sinica |
卷 | 24 |
期 | 4 |
出版状态 | 已出版 - 12月 2006 |