Effect of glow discharge on hypersonic flat plate boundary layer

doi:10.1007/s10483-019-2424-9

Applied Mathematics and Mechanics (English Edition) ›› 2019, Vol. 40 ›› Issue (2): 249-260.doi: https://doi.org/10.1007/s10483-019-2424-9

Effect of glow discharge on hypersonic flat plate boundary layer

Chi LI^1,2, Yunchi ZHANG^1,2

1. State Key Laboratory for Turbulence and Complex Systems, Peking University, Beijing 100871, China;
2. Department of Aeronautics and Astronautics, College of Engineering, Peking University, Beijing 100871, China

收稿日期:2018-09-03 修回日期:2018-10-16 出版日期:2019-02-01 发布日期:2019-02-01
通讯作者: Chi LI E-mail:lichi@pku.edu.cn
基金资助:
Project supported by the National Natural Science Foundation of China (Nos. 10921202, 11221061, 11632002, 11521091, and 11602005)

Effect of glow discharge on hypersonic flat plate boundary layer

Chi LI^1,2, Yunchi ZHANG^1,2

1. State Key Laboratory for Turbulence and Complex Systems, Peking University, Beijing 100871, China;
2. Department of Aeronautics and Astronautics, College of Engineering, Peking University, Beijing 100871, China

Received:2018-09-03 Revised:2018-10-16 Online:2019-02-01 Published:2019-02-01
Contact: Chi LI E-mail:lichi@pku.edu.cn
Supported by:
Project supported by the National Natural Science Foundation of China (Nos. 10921202, 11221061, 11632002, 11521091, and 11602005)

摘要/Abstract

摘要： Glow discharge is introduced as an artificial disturbance to investigate the evolution of first-and second-mode instabilities in a hypersonic flat plate boundary layer. Experiments are conducted in a Mach 6.5 quiet wind tunnel using Rayleigh scattering visualization and particle image velocimetry (PIV). Detailed analysis of the experimental observations is provided. It is found that the artificially introduced 17 kHz disturbance, which belongs to the first-mode frequency band, can effectively enhance first-mode waves. Moreover, it can enhance second-mode waves even more intensely. Possible mechanisms to explain this phenomenon are discussed.

关键词: Singular perturbation, limit equation, elliptic equation, hypersonic, glow discharge, particle image velocimetry (PIV)

Abstract: Glow discharge is introduced as an artificial disturbance to investigate the evolution of first-and second-mode instabilities in a hypersonic flat plate boundary layer. Experiments are conducted in a Mach 6.5 quiet wind tunnel using Rayleigh scattering visualization and particle image velocimetry (PIV). Detailed analysis of the experimental observations is provided. It is found that the artificially introduced 17 kHz disturbance, which belongs to the first-mode frequency band, can effectively enhance first-mode waves. Moreover, it can enhance second-mode waves even more intensely. Possible mechanisms to explain this phenomenon are discussed.

Key words: Singular perturbation, limit equation, elliptic equation, particle image velocimetry (PIV), glow discharge, hypersonic

中图分类号:

76K05
76N20

Chi LI, Yunchi ZHANG. Effect of glow discharge on hypersonic flat plate boundary layer[J]. Applied Mathematics and Mechanics (English Edition), 2019, 40(2): 249-260.

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Effect of glow discharge on hypersonic flat plate boundary layer

Effect of glow discharge on hypersonic flat plate boundary layer

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