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NUMERICAL INVESTIGATION OF A SWEEPING JET ACTUATOR FOR ACTIVE FLOW CONTROL IN A COMPRESSOR CASCADE

机译:压气机叶栅主动流动控制的横扫射流致动器的数值研究

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Sweeping Jet Actuator (SJA) was introduced as a potential active flow control method for reducing three-dimension (3D) flow separations in a compressor cascade. Unlike some other actuators, SJA needs no valves or moving parts to convert its steady compressed air source into sweeping jets that oscillates from side to side through the millimeter-sized outlet nozzle. The rather simple and small structure makes it possible to place SJA into the blades. In this study, a 3D numerical simulation using unsteady RANS codes was conducted to investigate the effects of SJA on the flow pattern and the aerodynamic loss mechanism in a compressor cascade. Firstly, the reliability of a commercial Computational Fluid Dynamic (CFD) code was validated and the computed results showed good agreements with experimental data from the literature. Secondly, some possible affecting factors, such as actuating pressure, position of SJA exit and jet skew angle, were analyzed and discussed in detail. Moreover, the effectiveness of active flow control under different locations and stream directions of SJA was studied for obtaining a further understanding of the mechanism of SJA for controlling flow separations. In addition, the generation and interaction of internal secondary flows in the compressor cascade were also investigated, and the oscillating jet process of SJA was presented. The numerical results indicate that using SJA delays effectively the corner flow separation, thus decreases the aerodynamic loss of the compressor cascade. For the optimum scheme within the present research, the reduction of overall time-averaged total pressure loss coefficient achieves about 5.6% compared with the original case without SJA. The streamwise position of SJA has a more remarkable influence in improving performance than the other SJA schemes. The considerable improvements of flow separation in the corner region is considered to be one of the main reasons in overall performance increase.
机译:引入吹扫喷射执行器(SJA)作为一种潜在的主动流控制方法,用于减少压缩机级联中的三维(3D)流分离。与某些其他执行器不同,SJA无需阀门或移动部件即可将其稳定的压缩空气源转换为可通过毫米大小的出口喷嘴左右摆动的清扫喷嘴。相当简单和小巧的结构使得可以将SJA放置在刀片中。在这项研究中,进行了使用非稳态RANS代码的3D数值模拟,以研究SJA对压缩机叶栅中的流型和空气动力损失机理的影响。首先,验证了商业计算流体动力学(CFD)代码的可靠性,计算结果与文献中的实验数据吻合良好。其次,详细分析和讨论了一些可能的影响因素,如致动压力,SJA出口的位置和射流偏斜角。此外,研究了在SJA的不同位置和流向下进行主动流量控制的有效性,以进一步了解SJA用于控制流分离的机理。此外,还研究了压缩机级联中内部二次流的产生和相互作用,并提出了SJA的振荡射流过程。数值结果表明,使用SJA有效地延迟了角流分离,从而降低了压缩机叶栅的空气动力学损失。对于本研究中的最佳方案,与没有SJA的原始情况相比,总时间平均总压力损失系数的降低达到了约5.6%。与其他SJA方案相比,SJA的流向位置在提高性能方面具有更显着的影响。拐角区域中流动分离的显着改善被认为是整体性能提高的主要原因之一。

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