Turbulent boundary layer control with a spanwise array of DBD plasma actuators

Yueqiang LI (李跃强); Chao GAO (高超); Bin WU (武斌); Yushuai WANG (王玉帅); Haibo ZHENG (郑海波); Ming XUE (薛明); Yuling WANG (王玉玲)

doi:10.1088/2058-6272/abce0d

Plasma Science and Technology > 2021 > 23(2): 25501-025501. > DOI: 10.1088/2058-6272/abce0d

Yueqiang LI (李跃强), Chao GAO (高超), Bin WU (武斌), Yushuai WANG (王玉帅), Haibo ZHENG (郑海波), Ming XUE (薛明), Yuling WANG (王玉玲). Turbulent boundary layer control with a spanwise array of DBD plasma actuators[J]. Plasma Science and Technology, 2021, 23(2): 25501-025501. DOI: 10.1088/2058-6272/abce0d

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Turbulent boundary layer control with a spanwise array of DBD plasma actuators

School of Aeronautics, Northwestern Polytechnical University, Xi'an 710072, People's Republic of China

Funds: The authors would like to acknowledge the financial support from the European Commission through the Research and Innovation action DRAGY (Drag Reduction via Turbulent Boundary Layer Flow Control), under Grant No. 690623, and the Ministry of Industry and Information Technology (MIIT) of the Chinese government, and support received from National Natural Science Foundation of China (No. 11572256).

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Received Date: July 29, 2020
Revised Date: November 23, 2020
Accepted Date: November 24, 2020

Graphical Abstract

Abstract

Abstract

The turbulent boundary layer control on NACA 0012 airfoil with Mach number ranging from 0.3 to 0.5 by a spanwise array of dielectric barrier discharge (DBD) plasma actuators by hot-film sensor technology is investigated. Due to temperature change mainly caused through heat produced along with plasma will lead to measurement error of shear stress measured by hot-film sensor, the correction method that takes account of the change measured by another sensor is used and works well. In order to achieve the value of shear stress change, we combine computational fluid dynamics computation with experiment to calibrate the hot-film sensor. To test the stability of the hot-film sensor, seven repeated measurements of shear stress at Ma = 0.3 are conducted and show that confidence interval of hot-film sensor measurement is from −0.18 to 0.18 Pa and the root mean square is 0.11 Pa giving a relative error 0.5% over all Mach numbers in this experiment. The research on the turbulent boundary layer control with DBD plasma actuators demonstrates that the control makes shear stress increase by about 6% over the three Mach numbers, which is thought to be reliable through comparing it with the relative error 0.5%, and the value is hardly affected by burst frequency and excitation voltage.
- turbulent boundary layer control DBD plasma actuators,
- hot-film sensor

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References

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Turbulent boundary layer control with a spanwise array of DBD plasma actuators