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NUMERICAL SIMULATION OF FLOW INDUCED BY MULTIPLE DBD PLASMA ACTUATORS

机译:多个DBD等离子体作动器引起的流动的数值模拟。

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Active flow separation control using dielectric barrier discharge (DBD) plasma actuators oriented in the spanwise direction has been successfully investigated by the authors using an integrated numerical simulation tool that couples the unsteady Reynolds averaged Navier-Stokes (URANS) or large eddy simulation (LES) solver for incompressible flows with the DBD electro-hydrodynamic (EHD) body force model. Although many experimental and numerical investigations have indicated that the spanwise-oriented DBD plasma actuator is an effective flow control method, the application is difficult to extend from model-scale to full-scale problems, partly due to the required high amplitude and high bandwidth excitation. Also, the flow control mechanism associated with a spanwise-oriented DBD actuator is mainly direct momentum injection, therefore, the effectiveness of actuation is sensitive to the location of the DBD actuator relative to the location of flow separation. On the other hand, a few experimental studies have shown promising results using the DBD Vortex Generator (DBD-VG) consisting of multiple plasma DBD actuators oriented in the streamwise direction. By generating streamwise vortices extending a long distance downstream, the DBD-VGs enhance the mixing of the inner and outer layers of turbulent boundary layer flows. As a result, the boundary layer can better withstand an adverse pressure gradient. When applied to flow separation control, the effectiveness of the DBD-VGs should be less sensitive to location of flow separation. The present work extends the capability of the integrated numerical simulation tool from a single spanwise-oriented DBD plasma actuator to multiple DBD plasma actuators oriented in any direction, including the streamwise direction. As a demonstration of the new capability in the DBD-URANS coupled solver, numerical simulations of flow induced by a DBD-VG actuator with an array of exposed electrodes in a quiescent environment, as well as in a turbulent boundary layer over a fiat plate, are carried out. The numerical simulation successfully reproduced the longitudinal vortices embedded in the boundary layer.
机译:作者已经成功地研究了使用沿跨展方向定向的电介质势垒放电(DBD)等离子体致动器进行的主动流分离控制,该方法使用了集成了非稳态雷诺平均Navier-Stokes(URANS)或大涡流仿真(LES)的集成数值模拟工具DBD电动流体动力学(EHD)体力模型的不可压缩流求解器。尽管许多实验和数值研究表明,面向翼展方向的DBD等离子体致动器是一种有效的流量控制方法,但由于部分应用需要高振幅和高带宽激励,因此该应用很难从模型范围扩展到全范围问题。而且,与沿翼展方向定向的DBD致动器相关联的流量控制机构主要是直接动量注入,因此,致动的有效性对DBD致动器的位置相对于流分离的位置敏感。另一方面,一些实验研究表明,使用DBD涡流发生器(DBD-VG)的结果令人鼓舞,该发生器由沿流向定向的多个等离子DBD致动器组成。通过产生向下游延伸很长距离的沿流涡流,DBD-VG增强了湍流边界层流的内层和外层的混合。结果,边界层可以更好地承受不利的压力梯度。当应用于流分离控制时,DBD-VG的有效性应对流分离的位置不那么敏感。本工作将集成数值模拟工具的功能从单个沿翼展方向定向的DBD等离子体致动器扩展到沿任何方向(包括流向)定向的多个DBD等离子体致动器。为了说明DBD-URANS耦合求解器的新功能,在静态环境中以及在平板上的湍流边界层中,由带有裸露电极阵列的DBD-VG执行器引起的流动的数值模拟,被执行。数值模拟成功地再现了嵌入边界层中的纵向涡旋。

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