Low-current gliding DC discharge in high-speed flows

IF 3.1 3区 物理与天体物理 Q2 PHYSICS, APPLIED
K N Kornev, A A Logunov, S A Dvinin
{"title":"Low-current gliding DC discharge in high-speed flows","authors":"K N Kornev, A A Logunov, S A Dvinin","doi":"10.1088/1361-6463/ad726e","DOIUrl":null,"url":null,"abstract":"A low-current gliding discharge (current range 1–5 A) in high-speed air flows of 100–250 m s<sup>−1</sup> was experimentally studied. A high-voltage direct current source with a maximum voltage of 4.5 kV was used to create the discharge. The average electron concentration <italic toggle=\"yes\">n</italic><sub>e</sub> ∼ 10<sup>14</sup> cm<sup>−3</sup> and the plasma ionization degree were determined by measuring the Stark broadening of the hydrogen H<italic toggle=\"yes\"><sub>β</sub></italic> line (<italic toggle=\"yes\">λ</italic><sub>H<italic toggle=\"yes\">β</italic></sub> = 486.1 nm). The estimates of the electric field (<italic toggle=\"yes\">E</italic> ∼ 100 V cm <sup>−1</sup> ÷ 600 V cm<sup>−1</sup>) in the discharge positive column were found using time-synchronized high-speed video recordings and oscillograms. The gas rotational temperature <italic toggle=\"yes\">T</italic><sub>g</sub> = 7000–9500 K and the vibrational temperature <italic toggle=\"yes\">T</italic><sub>v</sub> = 7000–11 000 K were estimated using optical emission spectroscopy. Time-resolved spectroscopy is used to investigate the effective plasma channel spatial regions from which the N, NH, N<sub>2</sub><sup>+</sup>, O and OH molecules radiate. The difference of the obtained radii indicates the presence of a radial temperature gradient and inhomogeneous plasma composition in the discharge cross section. The possibility of using of gliding discharge to ignite hydrocarbon-air mixtures in the ramjet engines combustors has been experimentally demonstrated.","PeriodicalId":16789,"journal":{"name":"Journal of Physics D: Applied Physics","volume":"5 1","pages":""},"PeriodicalIF":3.1000,"publicationDate":"2024-09-02","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Journal of Physics D: Applied Physics","FirstCategoryId":"101","ListUrlMain":"https://doi.org/10.1088/1361-6463/ad726e","RegionNum":3,"RegionCategory":"物理与天体物理","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q2","JCRName":"PHYSICS, APPLIED","Score":null,"Total":0}
引用次数: 0

Abstract

A low-current gliding discharge (current range 1–5 A) in high-speed air flows of 100–250 m s−1 was experimentally studied. A high-voltage direct current source with a maximum voltage of 4.5 kV was used to create the discharge. The average electron concentration ne ∼ 1014 cm−3 and the plasma ionization degree were determined by measuring the Stark broadening of the hydrogen Hβ line (λHβ = 486.1 nm). The estimates of the electric field (E ∼ 100 V cm −1 ÷ 600 V cm−1) in the discharge positive column were found using time-synchronized high-speed video recordings and oscillograms. The gas rotational temperature Tg = 7000–9500 K and the vibrational temperature Tv = 7000–11 000 K were estimated using optical emission spectroscopy. Time-resolved spectroscopy is used to investigate the effective plasma channel spatial regions from which the N, NH, N2+, O and OH molecules radiate. The difference of the obtained radii indicates the presence of a radial temperature gradient and inhomogeneous plasma composition in the discharge cross section. The possibility of using of gliding discharge to ignite hydrocarbon-air mixtures in the ramjet engines combustors has been experimentally demonstrated.
高速水流中的低电流滑行直流放电
实验研究了 100-250 m s-1 高速气流中的低电流滑行放电(电流范围 1-5 A)。产生放电的是一个最大电压为 4.5 kV 的高压直流电源。通过测量氢 Hβ 线的斯塔克展宽(λHβ = 486.1 nm),确定了平均电子浓度 ne ∼ 1014 cm-3 和等离子体电离度。放电正柱中的电场(E ∼ 100 V cm -1 ÷ 600 V cm-1)是通过时间同步的高速视频记录和振荡图估算出来的。气体旋转温度 Tg = 7000-9500 K 和振动温度 Tv = 7000-11000 K 是通过光学发射光谱估算的。时间分辨光谱法用于研究 N、NH、N2+、O 和 OH 分子辐射的有效等离子体通道空间区域。获得的半径差异表明放电截面存在径向温度梯度和不均匀等离子体成分。实验证明了在冲压式喷气发动机燃烧器中使用滑行放电点燃碳氢化合物-空气混合物的可能性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
求助全文
约1分钟内获得全文 求助全文
来源期刊
Journal of Physics D: Applied Physics
Journal of Physics D: Applied Physics 物理-物理:应用
CiteScore
6.80
自引率
8.80%
发文量
835
审稿时长
2.1 months
期刊介绍: This journal is concerned with all aspects of applied physics research, from biophysics, magnetism, plasmas and semiconductors to the structure and properties of matter.
×
引用
GB/T 7714-2015
复制
MLA
复制
APA
复制
导出至
BibTeX EndNote RefMan NoteFirst NoteExpress
×
提示
您的信息不完整,为了账户安全,请先补充。
现在去补充
×
提示
您因"违规操作"
具体请查看互助需知
我知道了
×
提示
确定
请完成安全验证×
copy
已复制链接
快去分享给好友吧!
我知道了
右上角分享
点击右上角分享
0
联系我们:info@booksci.cn Book学术提供免费学术资源搜索服务,方便国内外学者检索中英文文献。致力于提供最便捷和优质的服务体验。 Copyright © 2023 布克学术 All rights reserved.
京ICP备2023020795号-1
ghs 京公网安备 11010802042870号
Book学术文献互助
Book学术文献互助群
群 号:481959085
Book学术官方微信