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Active Vortex Generation using Dielectric-Barrier Discharge Plasmas

机译:使用介质阻隔放电等离子体的主动涡流产生

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The main objective of this study is to investigate the active and sustained vortex generation in a laminar boundary layer using spanwise acting plasma actuators. The wind tunnel experiments are conducted on a flate plate with a freestream velocity of U_∞, = 8m/s, with the streamwise length of the electrodes significantly longer than in previous studies. As a result of longitudinal counter-rotating vortices, the boundary layer is modulated with streaks of higher and lower velocity. The amplitudes of the induced high and low-speed streaks in the boundary layer, measured with hot-wire probes downstream of the actuator arrays, provide a measure for the flow control success. Several geometric parameters and different operation modes have been investigated and reveal the complex interaction of all operating parameters. In a second set of experiments a proof of concept is presented, showing the attenuation of the amplitude of TS waves by streamwise streaks generated by a plasma actuator vortex generator array.
机译:本研究的主要目的是使用翼展用法等离子体致动器研究层层边界层中的主动和持续的涡流。风隧道实验在具有U_∞,= 8m / s的自由流速度的束板上进行,电极的流动长度明显长于先前的研究。由于纵向反向旋转涡流,边界层用速度较高和较低的条纹调制。用致动器阵列下游的热线探针测量的边界层中诱导的高和低速条纹的幅度为流量控制成功提供了一种措施。已经研究了几种几何参数和不同的操作模式,并揭示了所有操作参数的复杂相互作用。在第二组实验中,提出了概念证明,示出了通过等离子体致动器涡流发生器阵列产生的流动条纹的TS波的幅度的衰减。

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