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Full Length Article | Open Access

A collisional-radiative model for atmospheric-pressure low-temperature air discharges

Ximing ZHUa, Lu WANGa( ), Wei CUIb, Bangdou HUANGc( ), Yun WUb, Min JIAb, Yang ZHAOa, Bowen ZHENGa, Ji LIa, Desheng ZHOUa, Daren YUa
School of Energy Science and Engineering, Harbin Institute of Technology, Harbin 150001, China
National Key Lab of Aerospace Power System and Plasma Technology, Air Force Engineering University, Xi’an 710038, China
Beijing International S&T Cooperation Base for Plasma Science and Energy Conversion, Institute of Electrical Engineering, Chinese Academy of Sciences, Beijing 100190, China

Peer review under responsibility of Editorial Committee of CJA

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Abstract

Plasma-assisted combustion technology has been a hot spot in aero-engines and scramjet-engines. The electron density is a key discharge parameter related to the active-particle density. The latter has been considered playing an important role in the above applications by the kinetic effect. In this work, an atmospheric pressure air plasma collisional-radiative model considering the excited states of atomic nitrogen and oxygen is built based on previous widely kinetic investigations of molecules and radicals, as well as their excited states. The excited states, especially the atomic nitrogen and oxygen states were less investigated in previous works. The emission intensity distributions from the model have a good agreement with those measured in the glide arc plasma with two discharge modes, as well as the microwave plasma. Based on the kinetics of molecular and atomic emitting states, the line-ratio method is presented to determine the electron density. The N2(337 nm)/O(844 nm) and N2(337 nm)/NO(γ) line ratios are used for the glide arc plasma and microwave plasma torch, respectively. Besides, the kinetics of the excited states involved with two line-ratios are also investigated in the two types of discharges. Combined with the atmospheric pressure actinometry method, the kinetic effect of the plasma-assisted combustion can be revealed quantitatively in the future.

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Chinese Journal of Aeronautics

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Cite this article:
ZHU X, WANG L, CUI W, et al. A collisional-radiative model for atmospheric-pressure low-temperature air discharges. Chinese Journal of Aeronautics, 2025, 38(4). https://doi.org/10.1016/j.cja.2024.11.006

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Received: 11 March 2024
Revised: 19 May 2024
Accepted: 28 July 2024
Published: 08 November 2024
© 2024 The Author(s). Chinese Society of Aeronautics and Astronautics.

This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).