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

被引:0
作者
Ximing ZHU [1 ]
Lu WANG [1 ]
Wei CUI [2 ]
Bangdou HUANG [3 ]
Yun WU [2 ]
Min JIA [2 ]
Yang ZHAO [1 ]
Bowen ZHENG [1 ]
Ji LI [1 ]
Desheng ZHOU [1 ]
Daren YU [1 ]
机构
[1] School of Energy Science and Engineering, Harbin Institute of Technology
[2] National Key Lab of Aerospace Power System and Plasma Technology, Air Force Engineering University
[3] Beijing International S&T Cooperation Base for Plasma Science and Energy Conversion, Institute of Electrical Engineering,Chinese Academy of Sciences
关键词
D O I
暂无
中图分类号
V23 [航空发动机(推进系统)];
学科分类号
082502 ;
摘要
Plasma-assisted combustion technology has been a hot spot in aero-engines andscramjet-engines. The electron density is a key discharge parameter related to the active-particledensity. The latter has been considered playing an important role in the above applications bythe kinetic effect. In this work, an atmospheric pressure air plasma collisional-radiative model con-sidering the excited states of atomic nitrogen and oxygen is built based on previous widely kineticinvestigations of molecules and radicals, as well as their excited states. The excited states, especiallythe atomic nitrogen and oxygen states were less investigated in previous works. The emission inten-sity distributions from the model have a good agreement with those measured in the glide arcplasma with two discharge modes, as well as the microwave plasma. Based on the kinetics of molec-ular 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 andmicrowave plasma torch, respectively. Besides, the kinetics of the excited states involved with twoline-ratios are also investigated in the two types of discharges. Combined with the atmospheric pres-sure actinometry method, the kinetic effect of the plasma-assisted combustion can be revealed quan-titatively in the future.
引用
收藏
页码:59 / 73
页数:15
相关论文
共 65 条
[1]  
Experimental investigation of a gliding discharge plasma jet igniter.[J].Min JIA;Zhibo ZHANG;Wei CUI;Huimin SONG;Zhangkai HUANG;.Chinese Journal of Aeronautics.2022, 06
[2]   旋转滑动弧放电等离子体滑动放电模式的实验研究 [J].
雷健平 ;
何立明 ;
陈一 ;
陈高成 ;
赵兵兵 ;
赵志宇 ;
张华磊 ;
邓俊 ;
费力 .
物理学报, 2020, 69 (19) :232-243
[3]  
Experimental study of rotating gliding arc discharge plasma-assisted combustion in an aero-engine combustion chamber.[J].Liming HE;Yi CHEN;Jun DENG;Jianping LEI;Li FEI;Pengfei LIU;.Chinese Journal of Aeronautics.2019, 02
[4]  
Characteristics of pulsed plasma synthetic jet and its control effect on supersonic flow.[J].Jin Di;Cui Wei;Li Yinghong;Li Fanyu;Jia Min;Sun Quan;Zhang Bailing;.Chinese Journal of Aeronautics.2015, 01
[5]  
A combined atomic nitrogen?oxygen OES line-ratios method to determine the low-energy and high-energy electron temperature in non-equilibrium atmospheric pressure air glide arc plasmas.[J].Xi Ming Zhu;Lu Wang;Wei Cui;Yun Wu;Min Jia;Yang Zhao;Bang Dou Huang.Spectrochimica Acta Part B: Atomic Spectroscopy.2024,
[6]  
A xenon collisional-radiative model applicable to electric propulsion devices: III. Determination of the ionization fraction in low-temperature xenon plasma by using ionic and atomic 6 lines.[J].Zhu Xi-Ming;Wang Yan-Fei;Meng Sheng-Feng;Wang Yang;Ning Zhong-Xi;Yu Da-Ren;Bartschat Klaus.Plasma Sources Science and Technology.2023, 9
[7]   Partial EEDF analysis and electron diagnostics of atmospheric-pressure argon and argon-helium DBD plasma [J].
van der Gaag, Thijs ;
Nezu, Atsushi ;
Akatsuka, Hiroshi .
JOURNAL OF PHYSICS D-APPLIED PHYSICS, 2023, 56 (30)
[8]   Enhancement of blowout limit in a Mach 2.92 cavity-based scramjet combustor by a gliding arc discharge [J].
Tian, Yifu ;
Zhu, Jiajian ;
Sun, Mingbo ;
Wang, Hongbo ;
Huang, Yuhui ;
Feng, Rong ;
Yan, Bo ;
Sun, Yongchao ;
Cai, Zun .
PROCEEDINGS OF THE COMBUSTION INSTITUTE, 2023, 39 (01) :5697-5705
[9]   Dual-frequency plasma promoting flameholding in a supersonic combustion chamber [J].
Li, Ji ;
Tang, Jingfeng ;
Zhang, Haoran ;
Zhou, Desheng ;
Ji, Tianyuan ;
Yu, Daren ;
Zhu, Ximing .
AEROSPACE SCIENCE AND TECHNOLOGY, 2022, 127
[10]   Suppression of combustion mode transitions in a hydrogen-fueled scramjet combustor by a multi-channel gliding arc plasma [J].
Feng, Rong ;
Zhu, Jiajian ;
Wang, Zhenguo ;
Zhang, Fan ;
Ban, Yangyang ;
Zhao, Guoyan ;
Tian, Yifu ;
Wang, Chenglong ;
Wang, Hongbo ;
Cai, Zun ;
Sun, Mingbo .
COMBUSTION AND FLAME, 2022, 237