The generalized aerodynamic force required in analysis is calculated by using horse shoe vortex— vibrational pressure doublet grid method, based on theory of subsonic unsteady lifting plane.

在颤振特性分析中所需要的广义气动力是根据亚音速非定常升力面理论，采用马蹄涡—振荡压力偶极子格网法计算的。

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A saddle point and horse shoe vortex were formed in the front of the hole because of the rigid body character of coolant jet near the hole.

射流在出口附近具有刚体的特性，并在射流前方形成了鞍点及马蹄涡。

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