Advanced Search
Volume 38 Issue 12
Dec.  2012
Turn off MathJax
Article Contents
Abstract
References
Journal of Beijing University of Aeronautics and Astronautics  > 2012  >  38(12): 1572-1576.
Li Minjiang, Gui Xingmin. Staggered finite volume method for turbomachinery viscous flow field numerical investigation[J]. Journal of Beijing University of Aeronautics and Astronautics, 2004, 30(06): 577-582. (in Chinese)
Citation: Wei Baoxi, Ou Dong, Yan Minglei, et al. Ignition and flame holding ability of plasma torch igniter in a supersonic flow[J]. Journal of Beijing University of Aeronautics and Astronautics, 2012, 38(12): 1572-1576. (in Chinese)
shu

Ignition and flame holding ability of plasma torch igniter in a supersonic flow

  • School of Astronautics, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

  • Received Date: 15 May 2011
  • Publish Date: 30 Dec 2012
    Abstract
  • In order to study the application of plasma torch igniter in the scramjet engine, a numerical and experimental study was conducted in a Mach 2 supersonic flow with the ethylene and hydrogen. A detailed analysis of ignition and flame holding characteristics was done at the fuel equivalence ratio from 0.1 to 0.55, and the total temperature between 1 500 K and 1 950 K. The results show that the plasma torch has a positive effect on the ignition process, but the promotion on combustion efficiency is unapparent. An 8 step 9 species and a 3 step 6 species reaction model were used to simulate the ethylene supersonic combustion. The numerical results of 8 step reaction model agrees well with the experimental results.

     

    • FullText(HTML)
    • References(11)
  • [1]
    Do H,Seong-kyun I,Cappelli M A,et al.Plasma assisted flame ignition of supersonic flows over a flat wall[J].Combustion and Flame,2010,157(12):2298-2305
    [2]
    Hyungrok D,Cappelli M A,Godfrey M M.Plasma assisted cavity flame ignition in supersonic flows[J].Combustion and Flame,2010,157(9):1783-1794
    [3]
    Leonov S B,Kochetov I V,Napartovich A P,et al.Plasma-induced ethylene ignition and flameholding in confined supersonic air flow at low temperatures[J].IEEE Transactions on Plasma Science,2011,39(2):781-787
    [4]
    Jacobsen L S.Toward plasma-assisted ignition in scramjets .AIAA-2003-0871,2003
    [5]
    Kimura I,Aoki H,Kato M.The use of a plasma jet for flame stabilization and promotion of combustion in supersonic air flows[J].Combustion and Flame,1981,42:297-305
    [6]
    宋文艳,刘伟雄,贺伟,等．超声速燃烧室等离子体点火实验研究[J]．实验流体力学,2006,20(4):20-24 Song Wenyan,Liu Weixiong,He Wei,et al.Experimental investigation of plasma ignition in supersonic combustor [J].Experiments and Measur in Fluid Mechanics,2006,20(4):20-24(in Chinese)
    [7]
    王辽.超燃冲压发动机燃烧室燃料喷射与火焰稳定的试验研究 .北京:北京航空航天大学宇航学院,2008 Wang Liao.Experimental investigation of fuel injection and flame stabilization in scramjet combustor .Beijing:School of Astronautics,Beijing University of Aeronautics and Astronautics,2008(in Chinese)
    [8]
    Baurle R A,Eklund D R.Analysis of dual-mode hydrocarbon scramjet operation at Mach 4-6.5[J].Journal of Propulsion and Power,2002,18(5):990-1002
    [9]
    Mawid M A,Sekar B.Kinetic modeling of ethylene oxidation in high speed reacting flows .AIAA-1997-326,1997
    [10]
    Wang Haixing,Chen Xi,Pan Wenxia.Modeling study on the entrainment of ambient air into subsonic laminar and turbulent Argon plasma jets[J].Plasma Chemistry and Plasma Processing,2007,27(2):141-162
    [11]
    Minato R,Niioka T,Sugiyama H,et al.Numerical analysis of supersonic combustion by a plasma torch .AIAA-2005-3424,2005
    • Relative Articles

  • Relative Articles

    [1]TANG X H，DOU Y R. Design and verification of airworthiness compliance of equivalent endurance test cycle of turbofan engine[J]. Journal of Beijing University of Aeronautics and Astronautics，2025，51（1）：133-140 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0953.
    [2]HUANG X G，WU Y F，LIU D Y. Position analysis of seven-link Barranov truss based on conformal geometric algebra[J]. Journal of Beijing University of Aeronautics and Astronautics，2025，51（1）：265-271 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0961.
    [3]CAI Y，SI Y H，WANG Y Z，et al. Analysis and control of influencing factors of cross coupling of flexible gyro[J]. Journal of Beijing University of Aeronautics and Astronautics，2025，51（1）：141-151 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0968.
    [4]XU J M，HUANG Z G，LI R. LEO satellite positioning method and simulation verification aided by airborne navigation equipment[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（10）：3230-3238 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0759.
    [5]FU Honglan, ZHANG Hao. Close robust rendezvous on distant retrograde orbits[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0560
    [6]CHENG Y，QIU B W，YU L，et al. Influence of maneuvering modes on flared landing performance of parafoil system[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（12）：3940-3946 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0914.
    [7]ZHEN X D，WANG Z A，HU R C，et al. Aircraft flight qualities of short take-off and vertical landing[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（5）：1576-1585 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0413.
    [8]NIU G C，WANG X N. A multi-task traffic scene detection model based on cross-attention[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（5）：1491-1499 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0610.
    [9]YANG Z J，ZHANG C F，ZHAO R J，et al. Thermal deformation analysis and experimental verification of spatial deployable antenna hinge[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（1）：243-249 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0219.
    [10]HUANG Mengdie, WANG Lufeng, HUANG Xuxing, LI Shuang. Space target collision risk analysis algorithm based on the square Mahalanobis distance[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0167
    [11]ZHANG Y X，WANG X J，WANG S P，et al. Mechanism of butterfly forward flight and prototype verification based on characteristic motion observation[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（7）：1651-1660 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0497.
    [12]HAN Xiao, ZHOU Ying, HUANG Hai, SHAO Jing-yi. Design and Verification of High-precision Dynamic Temperature Control System[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0297
    [13]ZHANG P，CHI H H，LI J B，et al. Lattice based strong designated verifier signature scheme[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（6）：1294-1300 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0445.
    [14]XIE C C，ZHANG D Y，AN C. Reduced order method for large flexible wing structure based on dynamic response data[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（6）：1319-1330 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0439.
    [15]HAN X L，SHANGGUAN H，ZHANG X，et al. A low-dose CT image denoising method based on artifact estimation[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（2）：491-502 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0263.
    [16]LIU M，AN J S. Research and design of SpaceWire multi-priority hierarchical scheduling crossbar[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（12）：3386-3396 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0101.
    [17]XIAO R Y，YU J，MA Z X. Applicability of convolutional autoencoder in reduced-order model of unsteady compressible flows[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（12）：3445-3455 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0085.
    [18]HU G，LI Z X，ZHANG F M，et al. Dimension reduction of multivariate time series based on two-dimensional inter-class marginal Fisher analysis[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（12）：3537-3546 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0128.
    [19]GUO Tai, QIAN Xin, GONG Qi, REN Wenming, YANG Shuanbao, XU Qinggang. Methodology for model based verification requirements capturing and application in civil aircraft development[J]. Journal of Beijing University of Aeronautics and Astronautics, 2022, 48(10): 1933-1942. doi: 10.13700/j.bh.1001-5965.2021.0047
    [20]WANG Shaoping, CHEN Rentong, ZHANG Chao. Reliability estimation for aircraft hydraulic pump based on bivariate performance degradation analysis[J]. Journal of Beijing University of Aeronautics and Astronautics, 2022, 48(9): 1613-1623. doi: 10.13700/j.bh.1001-5965.2022.0297
    • Supplements(0)
    • Cited By

  • Cited by

    Periodical cited type(6)

    1. 唐冬来，李擎宇，周强，龚奕宇，谢飞，周朋，康乐. 基于故障因子的用电采集设备状态评估方法. 供用电. 2024(09): 98-106 .
    2. 尧阳烽，余永华，王康，聂方，胡嘉，徐德峰. 基于多源信号融合的往复式压缩机气阀健康评估. 机电工程. 2024(11): 2003-2011 .
    3. 刘莉萍，冯清贤，余志斌. 基于改进的ISODATA的超球覆盖仿生模式分类算法. 计算机应用研究. 2023(03): 689-695 .
    4. 文静，俞卫琴. 基于马氏距离的半监督近邻传播聚类算法. 软件导刊. 2023(07): 59-65 .
    5. 狄谱旭，李旭鹏，张润，张博，原昱，张璐. 应用FTIR技术对尸体内外精液留存时间的研究. 中国法医学杂志. 2023(06): 677-682 .
    6. 孔进，曹从咏，吴至锦，王晨. 一种改进的轨道车辆牵引电机性能评价方法研究. 电机技术. 2022(05): 20-25 .

    Other cited types(5)

  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索
    Get Citation
    PDF
    XML

    Article Metrics

    Article views(2255) PDF downloads(913) Cited by(11)
    Proportional views
    Related

    Copyright © Journal of Beijing University of Aeronautics and Astronautics

    Address: Editorial Department of Journal of Beijing University of Aeronautics and Astronautics, 37 Xueyuan Road, Haidian District, Beijing Post Code: 100191 Email: jbuaa@buaa.edu.cn

    Supported by: Beijing Renhe Information Technology Co., Ltd.    

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return