Articles

Effect of glow discharge on hypersonic flat plate boundary layer

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  • 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 date: 2018-09-03

  Revised date: 2018-10-16

  Online published: 2019-02-01

Supported by

Project supported by the National Natural Science Foundation of China (Nos. 10921202, 11221061, 11632002, 11521091, and 11602005)

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.

Cite this article

Chi LI, Yunchi ZHANG . Effect of glow discharge on hypersonic flat plate boundary layer[J]. Applied Mathematics and Mechanics, 2019 , 40(2) : 249 -260 . DOI: 10.1007/s10483-019-2424-9

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