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An experimental study of a radial wall jet formed by the normal impingement of a round synthetic jet

机译:由圆形合成射流的法向撞击形成的径向壁射流的实验研究

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The flow field of a radial wall jet created by the impingement of a round synthetic jet normal to a flat surface was characterized using hot-wire anemometry. In the synthetic wall jets the width of the outer layer was observed to increase linearly with the radial distance along the wall, while the local maximum velocity varied inversely. The synthetic wall jet exhibits self-similar behavior as distinguished by the collapse of the mean and rms velocity profiles when normalized by the outer layer scaling variables. Increasing the actuator driving amplitude at a fixed frequency (i) increased the growth rate of the outer layer, and (ii) decreased the decay rate of the local velocity maximum. The flow field of the synthetic wall jet was dominated by vortical structures associated with the actuator driving frequency, and harmonics connected with the interaction of the produced vortex structures. For the actuator conditions investigated, neither the classical laminar nor fully turbulent analytical solutions for continuous wall jets were amenable to modeling the synthetic wall jet profile due to the transitional and unsteady nature of the synthetic wall jet.
机译:使用热线风速测定法对由垂直于平面的圆形合成射流撞击产生的径向壁射流的流场进行了表征。在合成壁射流中,观察到外层的宽度随沿壁的径向距离呈线性增加,而局部最大速度则成反比。合成壁射流表现出自相似的行为,通过外层缩放变量进行归一化时,均值和均方根速度曲线的崩溃表现出明显差异。以固定频率增加执行机构的驱动幅度(i)增加外层的增长率,(ii)降低局部速度最大值的衰减率。合成壁射流的流场以与致动器驱动频率相关的涡旋结构为主,而谐波与产生的涡旋结构的相互作用有关。对于所研究的执行器条件,由于合成壁射流的过渡性和不稳定特性,对于连续壁射流,传统的层流分析方法或完全湍流的解析方法都不适合对合成壁射流的轮廓进行建模。

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