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

    颤振特性分析所需要广义气动力根据亚音速非定常升力面理论采用马蹄振荡压力偶极子格计算的。

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  • The gas and particle phase in the gas solid two phase plane mixing layers flow is numerically simulated using the discrete vortex method and trajectory method respectively.

    平板混合流动采用离散方法模拟气相场,轨道跟踪颗粒运动。

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  • The obtained velocity vector distribution in the measured plane coincided with the flow visualization results under the same test condition. In addition these vortex flow field was analysed.

    截面内的速度矢量分布相同实验条件态显示结果相符合,对涡流场加以分析。

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  • This paper presents an experiment on two-dimensional interaction of a plane moving shock with a vortex.

    本文介绍平面运动激波和单个旋涡相互作用实验

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  • In the experiment, a simplified aircraft model (with tail wing) is employed to construct a 4-vortex wake system consisting of a pair of tip vortices and a pair of counter rotating tail plane vortices.

    试验采用简化飞机模型(尾翼),建立了包含一对翼尖一对反向旋转的尾翼涡(通过以负迎角安装尾翼得到)的4涡尾流系统

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  • In the experiment, a simplified aircraft model (with tail wing) is employed to construct a 4-vortex wake system consisting of a pair of tip vortices and a pair of counter rotating tail plane vortices.

    试验采用简化飞机模型(尾翼),建立了包含一对翼尖一对反向旋转的尾翼涡(通过以负迎角安装尾翼得到)的4涡尾流系统

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