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The Optimum Wavelength of Spanwise Segmented Plasma Actuator Forcing of a Circular Cylinder Wake

机译:圆弧尾束的翼展式分段等离子作动器的最佳波长

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A study on three dimensional forcing of a cylinder wake was conducted in order to determine the optimum spanwise forcing wavelength. The forcing was implemented by mounting dielectric barrier discharge plasma actuators on the cylinder in a square wave pattern. Actuators of wavelength 1d, 74, Ad and 6d (d = cylinder diameter) were used to study the influence of forcing on the wake at a Reynolds number of 4700. The actuators were operated at two distinct power levels. Drag measured at an intermediate wake distance showed that maximum drag reduction was obtained when the Ad actuator was operated at a high power setting. The strength of vortex shedding was considerably attenuated in the near wake during forcing with the Ad actuator in the high power case. Forcing with 6d actuators caused significant variation in the spanwise properties of the wake which was evident even at a streamwise distance of 40 cylinder diameters. Particle image velocimetry was used to obtain cross flow images in the near wake. It was found that forcing with the Ad actuator created distinct patterns of streamwise vorticity in the wake with a spanwise wavelength of Ad which resembled mode A structures. It is argued that the effectiveness of the Ad actuator compared to other wavelengths was due to the formation of streamwise mode A structures in the near wake which hindered the development of spanwise Karman vortices.
机译:为了确定最佳的翼展方向强迫波长,进行了圆柱尾流的三维强迫研究。通过以方波模式在圆柱体上安装电介质势垒放电等离子体致动器来实现强制作用。使用波长为1d,74,Ad和6d(d =圆柱直径)的执行器研究雷诺数为4700时强迫对尾流的影响。这些执行器在两个不同的功率水平下运行。在中等唤醒距离下测得的阻力表明,当Ad执行器在高功率设置下运行时,可获得最大的阻力减小。在大功率情况下,在使用Ad执行器强迫时,近尾流中涡旋脱落的强度会大大减弱。用6d促动器强制迫使尾流的翼展方向特性发生显着变化,即使在沿直径40的圆柱流方向上也很明显。粒子图像测速仪用于获得近尾流的横流图像。已经发现,利用Ad致动器的强迫在尾流中产生了独特的沿流向涡流的模式,其Ad的跨向波长类似于模式A结构。有人认为,与其他波长相比,Ad致动器的有效性是由于在近尾流中形成了流向模式A结构,从而阻碍了跨向卡尔曼涡旋的发展。

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