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Active Vortex Generation using Dielectric-Barrier Discharge Plasmas

机译:使用介电势垒放电等离子体产生主动涡流

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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:这项研究的主要目的是研究使用翼展方向作用的等离子体致动器在层状边界层中产生主动和持续的涡流。风洞实验是在平板上进行的,自由流速度为U_∞,= 8m / s,电极的沿流方向的长度明显长于以前的研究。由于纵向反向旋转涡流,边界层被较高和较低速度的条纹调制。用致动器阵列下游的热线探针测量边界层中感应的高速和低速条纹的幅度,可作为流量控制成功与否的量度。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,显示了由等离子体致动器涡流发生器阵列产生的沿流条纹对TS波振幅的衰减。

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