本文实验研究了细长体模型在中等迎角下的初始分离问题。
The starting separation on the slender bodies was investigated at the moderate angles of attack.
作为例子，本文数值计算了细长体的水动力导数，给出了结果。
As an example, the hydrodynamic derivations of a slender-body of revolution are calculated.
研究了在大迎角下，后掠翼对细长体绕流结构和气动力特性的影响。
The influence on flow structure and aerodynamic of a slender by sweep wing at high Angle of attack was studied.
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