Influence of geometrical parameters on performance of plasma synthetic jet actuator

Plasma synthetic jet actuator (PSJA) has shown wide and promising application prospects in a high speed flow control field, due to its rapid response, high exhaust velocity, and non-moving components. In this paper, the total pressure profile of a plasma synthetic jet (PSJ) is measured and a new met...

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Bibliographic Details
Published in:Journal of physics. D, Applied physics Applied physics, 2015-11, Vol.49 (2), p.25504-25515
Main Authors: Zong, Hao-hua, Wu, Yun, Jia, Min, Song, Hui-min, Liang, Hua, Li, Ying-hong, Zhang, Zhi-bo
Format: Article
Language:English
Subjects:
Actuators
Arc discharges
characteristics
Discharge
Electrodes
flow control
geometrical parameters
High speed
plasma
Plasma (physics)
synthetic jet
Throats
Thrust
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Summary:Plasma synthetic jet actuator (PSJA) has shown wide and promising application prospects in a high speed flow control field, due to its rapid response, high exhaust velocity, and non-moving components. In this paper, the total pressure profile of a plasma synthetic jet (PSJ) is measured and a new method is developed to evaluate the pulsed thrust of the PSJA. The influence of geometrical parameters including the electrode distance, the orifice diameter, and the throat length on PSJA performance is analyzed based on the pulsed thrust, the discharge characteristics, and the schlieren images. When varying the electrode distance, the dominant factor determining the jet intensity is the heating volume instead of the discharge energy. For the arc discharge, the electrode distance should be extended to increase both the jet velocity and the jet duration time. The design of the orifice diameter should be based on the controlled flow field. A large orifice diameter produces a strong perturbation with short time duration, while a small orifice diameter induces a lasting jet with low mass flux. In order to obtain better high frequency performance, the throat length should be shortened on the condition that the structural strength of the PSJA is maintained, while there is almost no influence of the throat length on the single cycle performance of the PSJA. Once the discharge energy is fixed, the pulsed thrust remains almost unchanged with different orifice diameters and throat lengths. These three geometrical parameters are independent to some extent and can be optimized separately.
ISSN:0022-3727
1361-6463
DOI:10.1088/0022-3727/49/2/025504