Experiment on Jet Flow Control by SDBD Plasma Actuator
Authors
Jinlong Li, Xiuqian LI, Zheng Zhang, Xueke Che, Wansheng Nie, Zhi Zheng
Corresponding Author
Jinlong Li
Available Online June 2017.
- DOI
- 10.2991/ammee-17.2017.113How to use a DOI?
- Keywords
- jet flow, plasma actuator, surface dielectric barrier discharge, flow control.
- Abstract
Single and twin jet flow control by surface dielectric barrier discharge plasma actuator is studied in this paper. The plasma actuator is placed on the exit of a rectangular nozzle and particle image velocimetry method is adopted to measure the jet flow velocity and conduct flow visualization. The test results prove that surface dielectric barrier discharge plasma actuator can disturb the boundary layer in the single jet, which changing the original symmetrical vortex structure, then the spreading performance can be improved. In the twin jet, the plasma actuator causes the shear layer instability, which can increase jet width significantly and show a mixing enhancement.
- Copyright
- © 2017, the Authors. Published by Atlantis Press.
- Open Access
- This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).
Cite this article
TY - CONF AU - Jinlong Li AU - Xiuqian LI AU - Zheng Zhang AU - Xueke Che AU - Wansheng Nie AU - Zhi Zheng PY - 2017/06 DA - 2017/06 TI - Experiment on Jet Flow Control by SDBD Plasma Actuator BT - Proceedings of the Advances in Materials, Machinery, Electrical Engineering (AMMEE 2017) PB - Atlantis Press SP - 578 EP - 582 SN - 2352-5401 UR - https://doi.org/10.2991/ammee-17.2017.113 DO - 10.2991/ammee-17.2017.113 ID - Li2017/06 ER -