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Large-Eddy Simulation of Separation Control for Compressible Flow over a Wall-Mounted Hump

机译:壁挂式驼峰压缩流动分离控制的大涡流模拟

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Compressible large-eddy simulations of turbulent flow over a wall-mounted hump with active flow control are performed and compared to previous experiments. We consider a range of Mach numbers from 0.1 to 0.6. Control is applied just before the natural separation point via steady suction and zero-net mass flux oscillatory forcing. Compared with the baseline flow, control shortens the separation bubble length, but is generally found to be less effective at compressible Mach numbers. The LES matches well to the available experimental data for the baseline and steady suction cases. With oscillatory forcing, the LES captures the major flow physics of the large scale shedding of vortical structures, but over-predicts the separation bubble length at low Mach numbers.
机译:对具有主动流量控制的壁挂式驼峰的可压缩大涡流模拟,并与先前的实验进行比较。我们认为一系列的马赫数从0.1到0.6。在通过稳定抽吸和零净质量磁通振荡强制锻炼的自然分离点之前应用了控制。与基线流量相比,控制缩短了分离气泡长度,但通常被发现在可压缩马赫数下不太有效。 LES与基线和稳定吸力箱的可用实验数据相匹配。随着振荡的迫使,LES捕获了大规模血管血管结构的主要流量物理,但在低马赫数下过度预测了分离气泡长度。

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