Modal analysis of compressor cascades with sweeping jet actuator and pulsed jet for active flow control based on large Eddy simulation

Chen, Shaowen; Tu, Tianhong; Zeng, Cong; Meng, Qian

doi:10.1016/j.ast.2022.107997

Cited by 5 publications

(1 citation statement)

References 29 publications

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“…Now, the general conclusion is that the control position near the separation point is the best choice, but there is no final conclusion on such issues as where or within what range the specific position falls or what effect the change of position will have on the control effect. As another example, it is generally believed that the mechanism of suction is to eliminate the low-energy flow in the boundary layer (Liesner et al, 2010;Ma et al, 2018), and the jet can achieve the excitation effect by the principle of increasing momentum (Giorgi et al, 2015;Chen et al, 2022). However, the further problem is how these control methods specifically affect the coherent structures of turbulence and how they are coupled to the flow field to play a role in the separation/shedding vortex.…”

Section: Introductionmentioning

confidence: 99%

An unsteady flow control technique based on negative circulation conception and its application to a blade-divergent passage

Hong

Xiang

et al. 2023

Front. Energy Res.

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A two-dimensional vortex model is introduced in this paper in order to understand the characteristics of the shedding vortex in a blade-divergent passage and to mitigate or suppress it by appropriate methods. The performance of this model under the influence of three typical external factors is studied, namely, the main flow extrusion effect, viscous effect, and transport effect. Based on the analysis, a negative circulation unsteady flow control technique is proposed to compensate for the viscous effect, which is known as NCFC. Numerical simulation is performed to verify the effectiveness of the NCFC method. The results show that the NCFC method is superior to the conventional unsteady flow control for improving the performance of the blade-divergent passage in most cases. In addition, there is an optimum injection to suppress the shedding vortex with NCFC, which is about 0.2% of the main flow mass, and NCFC shows to be more efficient than conventional flow control in weakening the shedding vortex. Furthermore, NCFC can effectively inhibit separation flow and is shown to be insensitive to the injection flow mass. Finally, the NCFC method is highly recommended to adapt to the fact that the working conditions often change in practice.

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