Large-scale separation flow control on airfoil with synthetic jet

2018 ◽  
Vol 32 (2-3) ◽  
pp. 104-120 ◽  
Author(s):  
Z. L. Tang ◽  
J. D. Sheng ◽  
G. D. Zhang ◽  
J. Periaux
2021 ◽  
Vol 2119 (1) ◽  
pp. 012025
Author(s):  
A. S. Lebedev ◽  
M. I. Sorokin ◽  
D. M. Markovich

Abstract The development of methods of active separation flow control is of great applied importance for many technical and engineering applications. Understanding the conditions for the flow separation from the surface of a bluff body is essential for the design of aircrafts, cars, hydro and gas turbines, bridges and buildings. Drag, acoustic noise, vibrations and active flow mixing depend drastically on the parameters of the vortex separation process. We investigated the possibility of reducing the longitudinal length of a reverse-flow region using the method of «synthetic jet» active separation flow control. The experiment was carried out on a compact straight-through wind channel with a 1-m long test section of a cross-section of 125x125 mm. The jet was placed at the rear stagnation point of a circular cylinder. The Reynolds number, based on the cylinder diameter and the free-stream velocity, was 5000 and the von Kármán street shedding frequency without the synthetic jet was equal to 64.8 Hz. For the first time, for such a set of parameters, we applied high speed PIV to demonstrate that the injection of the synthetic jet into the cylinder wake region leads to a significant reduction in the longitudinal length of the reverse-flow region.


Author(s):  
Lu Weiyu ◽  
Huang Guoping ◽  
Fu Xin ◽  
Wang Jinchun ◽  
Hong Shuli

Vibration wall is a kind of important active flow control method, while the interaction between the vibration wall and unsteady separation flow is so complex for researchers to discover the corresponding mechanism. Current researches imply that the better controlled flow is the more ordered flow. At first, the effect of the different control parameters of vibration wall on the total pressure loss was studied by numerical simulation to reveal the control mechanism of vibration wall. Numerical results show that when the vibration frequency reaches the separation vortex frequency, with the amplitude of 0.1 characteristic length, the best flow control is resulted. Furthermore, it can be seen that, the vibration wall with effective parameters can make the large-scale vortices more dominant, while small-scales ones (or clutters) appear less in the pattern. This observation indicates that the flow field tends to be more orderly. Moreover, to further explain this ordering mechanism, a simplified model is established and analyzed, showing that valid external excitement can strengthen the dominated frequency of K-H wave which forms the large-scale separation vortices, and restrains small-scale ones. The flow field is then more orderly and less chaotic, resulting in reduction of flow loss.


Author(s):  
H. Shigefuji ◽  
F. Shimizu ◽  
K. Tanaka ◽  
K. Tokuda

The siphon phenomenon is widely used for the transportation system of water and it is very economical and ecological because the natural energy of water is only used for the power source of the transportation system. The siphon phenomenon is continued while the water is supplied with from the entrance, and a large-scale separation flow forms near the entrance of a siphon tube. The appearance, the growth, the movement and the disappearance of a swirling vortex are observed inside the siphon tube, and the flow field near the entrance becomes very complex. In the present paper, the flow pattern behind a sharp edge of the entrance was investigated experimentally using the PIV measurement.


Author(s):  
V Zander ◽  
M Hecklau ◽  
W Nitsche ◽  
A Huppertz ◽  
M Swoboda

This article presents the potential of active flow control to increase the aerodynamic performance of highly loaded turbomachinery compressor blades. Experimental investigations on a large-scale compressor cascade equipped with 30 synthetic jet actuators mounted to the sidewalls and the blades themselves have been carried out. Results for a variation of the inflow angle, the jet amplitude, and the actuation frequency are presented. The wake measurements show total pressure loss reductions of nearly 10 per cent for the synthetic jet actuation. An efficiency calculation reveals that the energy saved by actuation is nearly twice the energy consumption of the synthetic jets.


2006 ◽  
Vol 1115 (1-2) ◽  
pp. 267-270 ◽  
Author(s):  
Xiao Wang ◽  
Yanling Geng ◽  
Fuwei Li ◽  
Xingang Shi ◽  
Jianhua Liu

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