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1·The panel method was used to predict the wake flow field of propeller.

利用单斜丝热线旋转进行水平轴风力机模型的尾迹流场测量。

2·A wake flow with relatively lower pressure and recirculation zone exists on the lee side of the injector.

在喷口后的背风区，存在具有低压和回流区的尾迹。

3·In this paper, plasma wake flow of hypersonic reentry vehicle and radar scattering characteristics have been studied.

对再入飞行器等离子体尾迹及其雷达散射特性进行了分析、研究和大量的计算。

4·The result shows that there exists neither flow separation nor apparent wake flow within an non-overload centrifugal impeller.

结果表明，无过载离心叶轮内部流动既没有出现分离，也没有明显的尾迹区存在。

5·The near wake flow fields are calculated by simultaneously solving the viscous shear layer and the inviscid rotational region.

本文采用联立求解粘性剪切层和有旋无粘区的方法计算了再入钝头体层流近尾流场。

6·A plasma wake flow field is studied by analyzing the saturated ionic current of multiple scanning probes with the method of chaos dynamics.

用混沌动力学方法对多道扫描静电探针的离子饱和电流信号进行分析，研究了等离子体尾迹流场。

7·Unsteady flow in the rotor is simulated and contrast between the flow field with wake flow at the inlet and that with uniform one is presented.

对尾迹干扰下的转子非定常流场进行数值模拟，与传统设计定常流动假设下均匀进气的流场对比分析了尾迹干扰的影响。

8·The scaling of the longitudinal and transverse velocity structure functions is studied experimentally for turbulent jet and cylindrical wake flow.

实验测量了射流与圆柱尾流纵、横向的湍流速度脉动，计算了这两种方向的湍流速度结构函数的标度规律。

9·By the method of water flow pattern visualization with hydrogen bubbles, the near wake flow behind a slit bluff body has been experimentally studied.

采用水模拟氢气泡流动显示的方法对开缝钝体近尾流结构进行了实验研究。

10·A dynamic model of the towed system was established in the non-uniform wake flow field, and the shape of the towed system was investigated by finite difference method.

建立了水下拖曳系统在非均匀流场中的力学模型，用有限差分法计算收放缆时拖缆的姿态。

尾流

1·The scaling of the longitudinal and transverse velocity structure functions is studied experimentally for turbulent jet and cylindrical wake flow.

实验测量了射流与圆柱尾流纵、横向的湍流速度脉动，计算了这两种方向的湍流速度结构函数的标度规律。