Improving 3D Synthetic Jet Modeling in a Crossflow

Howard Ho, E. Essel, Pierre E. Sullivan
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引用次数: 0

Abstract

Three different circular synthetic jet modeling inlet conditions are studied for a turbulent crossflow. The study examines the differences when modeling the whole SJA, neck-only or jet-slot-only under constant actuation frequency (f = 300 Hz) and crossflow blowing ratio (CB = 0.67). Phase-averaged and time-averaged results reveal that both whole SJA and neck-only methods generated nearly identical flow fields. For the neck-only case, a notable reduction in computational cost is achieved through the implementation of an analytical jet profile. The jet-slot-only method, on the other hand, introduces reversed flow during the ingestion cycle, leading to the injection of false-momentum into the crossflow. However, the false-momentum primarily affects the flow immediately downstream of the jet exit, with the boundary layer profile recovering rapidly. A parametric study highlights the importance of maintaining a volume ratio less than 1 of ingested to modeled neck volume to prevent the creation of false-momentum.
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改进横流中的三维合成射流建模
针对湍流横流,研究了三种不同的圆形合成射流建模入口条件。研究考察了在恒定启动频率(f = 300 Hz)和横流吹气比(CB = 0.67)条件下,整个 SJA、纯颈部或纯喷射槽建模的差异。阶段均值和时间均值结果显示,整个 SJA 和仅颈部方法产生的流场几乎相同。对于纯颈部方法,通过实施分析射流轮廓,计算成本显著降低。另一方面,纯射流槽方法在摄取周期中引入了反向流,导致向横流注入假动量。然而,假动量主要影响射流出口下游的流动,边界层剖面会迅速恢复。参数研究强调了保持摄取体积与建模颈部体积比小于 1 以防止产生假动量的重要性。
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