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1·A predicting method of wing turbulent separation area and the influence of different turbulent models on the results of prediction are introduced.

介绍了机翼气流分离区的预测方法和不同湍流模型对其预测结果的影响。

2·Finally recent studies of turbulent boundary layer separation are also briefly reviewed.

最后简单介绍了目前在研究湍流边界层分离方面的进展。

3·A second filtering was applied to the convective and turbulent stress terms, and a new separation of the turbulent stresses was proposed.

对对流项和湍流应力项进行二次显式滤波，并对湍流应力的分解形式作了相应改进。