Calculation of Glow Discharge Parameters in a Supersonic Axisymmetric Helium Flow

The parameters of a glow discharge in helium with a nonuniform distribution of the density of neutral particles along the discharge gap have been calculated for a one-dimensional axisymmetric geometry. This formulation of the problem corresponds to the condition of generating a discharge between a Laval nozzle with a central body, which is the anode, and a ring cathode located coaxially to the central body at low pressures. In this case, a supersonic gas flow is generated through the Laval nozzle, which creates an increased gas pressure near the central body (anode), and high vacuum is maintained outside the supersonic jet. Thus, the internal structure of this discharge will depend on the density of gas particles in different regions of the interelectrode space. It has been established that this method of organizing a glow discharge in a supersonic gas flow makes it possible to control the spatial distribution of the internal characteristics of the discharge.

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Publication Details

Journal
Physics of Atomic Nuclei
Published
2024-12-01
DOI
https://doi.org/10.1134/s1063778824090424
Citations
2
Primary Topic
Plasma and Flow Control in Aerodynamics
Type
article
Field-Weighted Citation Impact
2.60
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article

Calculation of Glow Discharge Parameters in a Supersonic Axisymmetric Helium Flow

A I Sayfutdinov, O. A. Petrova, Б. А. Тимеркаев, Д. И. Исрафилов
2 citations
Physics of Atomic Nuclei
Plasma and Flow Control in Aerodynamics
2.60
article

Calculation of Glow Discharge Parameters in a Supersonic Axisymmetric Helium Flow

A I Sayfutdinov, O. A. Petrova, Б. А. Тимеркаев, Д. И. Исрафилов
article en
2 citations

Abstract

The parameters of a glow discharge in helium with a nonuniform distribution of the density of neutral particles along the discharge gap have been calculated for a one-dimensional axisymmetric geometry. This formulation of the problem corresponds to the condition of generating a discharge between a Laval nozzle with a central body, which is the anode, and a ring cathode located coaxially to the central body at low pressures. In this case, a supersonic gas flow is generated through the Laval nozzle, which creates an increased gas pressure near the central body (anode), and high vacuum is maintained outside the supersonic jet. Thus, the internal structure of this discharge will depend on the density of gas particles in different regions of the interelectrode space. It has been established that this method of organizing a glow discharge in a supersonic gas flow makes it possible to control the spatial distribution of the internal characteristics of the discharge.

Physics of Atomic NucleiVol. 87(9)
Kazan Federal University (RU), Kazan State Technical University named after A. N. Tupolev (RU)
Openalex Percentile: Top 7%
Plasma and Flow Control in Aerodynamics
2.60
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