Effects of a Kind of Non-smooth Blade on the Unsteady Flow Field at the Exit of an Axial Fan

在一个轴流动的迷的一个出口的不稳定的流动地上的一种投出 streamwise 的片的效果的试验性的调查被执行。在从在中心的后面的边的 25% 弦 downstream 的流动领域以不同集体流动的条件用一根快反应的五洞的压力探针被测量。投出的片的不稳定的流动与光滑的片的相比。测量结果显示那：(1 ) 投出的片由 modulating 制止速度变化和压力变化片界面层，它在中心区域并且在转子贡献流动损失减小以设计条件弄醒区域；(2 ) 溪流明智的沟在在片界面层制止光线的迁居并且消除混合的尖端流动起一个重要作用，它以设计条件在尖端区域贡献流动损失减小；(3 ) 在近的货摊调节，投出的表面不能减少流动损失，当分离发生在片界面层时，甚至附近增加损失。

An experimental investigation of effects of a kind of streamwise-grooved blade on the unsteady flow field at an exit of an axial-flow fan was performed. The flow field at 25% chord downstream from the trailing edge at hub was measured using a fast-response five-hole pressure probe at different mass-flow conditions. The unsteady flow of the grooved blades was compared with that of the smooth blades. The measurement results indicate that： （1） the grooved blades restrain the velocity fluctuation and the pressure fluctuation by modulating the blade boundary layers, which contributes to the flow loss reduction in the hub region and in the rotor wake region at the design condition; （2） the stream-wise grooves play an important role in restraining the radial migration in the blade boundary layer and abating the tip flow mixing, which contributes to the flow loss reduction in the tip region at the design condition; （3） at the near stall condition, the grooved surface can not reduce the flow loss, even increase the loss nearby when the separation happens in the blade boundary layer.