Volume 28 Issue 7
Jul.  2013
Turn off MathJax
Article Contents
LI Xiao-peng, ZHANG Tai-chang, QI Li, FAN Xue-jun. Characteristic scales and influential factors in supersonic combustion[J]. Journal of Aerospace Power, 2013, 28(7): 1458-1466.
Citation: LI Xiao-peng, ZHANG Tai-chang, QI Li, FAN Xue-jun. Characteristic scales and influential factors in supersonic combustion[J]. Journal of Aerospace Power, 2013, 28(7): 1458-1466.

Characteristic scales and influential factors in supersonic combustion

  • Received Date: 2012-07-19
  • Publish Date: 2013-07-28
  • Using the hydrogen,ethylene and kerosene (chemically surrogated by a mixture of n-decane 0.8 and 1,2,4-trimethylbenzene 0.2 by mass fraction) as fuels,the characteristic scales in supersonic combustion and the related influence factors were analyzed,and the operating range of scramjet under the typical flight conditions was calculated.At last,the applicability of flamelet model for the numerical simulation of supersonic combustion was explored.The results show that the operating range of scramjet for these fuels decreases successively and Damkohler number(Da) varies boardly in the order of magnitude,and flamelet in eddies regime is usually the main part,where Taylor micro-scale plays an important role.At the same time,it is found that the flamelet model needs to be considered carefully in numerical simulation of supersonic combustion compared with subsonic combustion.

     

  • loading
  • [1]
    Corin S.The scramjet engine processes and characteristics[M].New York:Cambridge University Press,2009.
    [2]
    Lee S H.Characteristics of dual transverse injection in scramjet combustor:Part 2 combustion[J].Journal of Propulsion and Power,2006,22(5):1020-1026.
    [3]
    Keistler P G,Hassan H A,Xiao X.Simulation of supersonic combustion in three-dimensional configurations[J].Journal of Propulsion and Power,2009,25(6):1233-1239.
    [4]
    Jeong E,O'Byrne S,Jeung I S,et al.Investigation of supersonic combustion with angled injection in a cavity-based combustor[J].Journal of Propulsion and Power,2008,24(6):1258-1268.
    [5]
    Ben Y A,Mungal M G,Hanson R K.Time evolution and mixing characteristics of hydrogen and ethylene transverse jets in supersonic crossflows[J].Physics of Fluids,2006,18(2):026101.1-026101.16.
    [6]
    Rana Z A,Thornber B,Drikakis D.Transverse jet injection into a supersonic turbulent cross-flow[J].Physics of Fluids,2011,23(4):046103.1-046103.21.
    [7]
    Ferrante A,Matheou G,Dimotakis P E.LES of an inclined sonic jet into a turbulent crossflow at Mach 3.6[J].Journal of Turbulence,2011,12(2):1-32.
    [8]
    Cecere D,Ingenito A,Giacomazzi E,et al.Hydrogen/air supersonic combustion for future hypersonic vehicles[J].International Journal of Hydrogen Energy,2011,36(18):11969-11984.
    [9]
    Stephen R.燃烧学导论:概念与应用[M].姚强,李永清,王宇,译.北京:清华大学出版社,2009.
    [10]
    Kritsuk A G,Norman M L,Padoan P,et al.The statistics of supersonic isothermal turbulence[J].The Astrophysical Journal,2007,665(1):416-431.
    [11]
    Biagioni L,d'Agostino L.Measurement of energy spectra in weakly compressible turbulence [R].AIAA 99-3516,1999.
    [12]
    Ingenito A,Bruno C.Physics and regimes of supersonic combustion[J].AIAA Journal,2010,48(3):515-525.
    [13]
    庄礼贤,尹协远,马晖扬.流体力学[M].合肥:中国科学技术大学出版社,2009.
    [14]
    Gruber M,Donbar J,Jackson K,et al.Newly developed direct-connect high-enthalpy supersonic combustion research facility[J].Journal of Propulsion and Power,2001,17(6):1296-1304.
    [15]
    杨猛,袁越明,范学军.高速脉冲纹影系统在超声速燃烧室内流场显示中的初步应用 [R].CSTAM 2011-2769,2011.
    [16]
    杨猛.高速脉冲纹影技术及其在超声速燃烧室流场显示中的应用 [D].北京:中国科学院,2012. YANG Meng.High speed pulsed schlieren technology and its application to flow visualization in supersonic combustion [D].Beijing:Chinese Academy of Science,2012.(in Chinese)
    [17]
    Fan X J,Yu G,LI J G,et al.Investigation of vaporized kerosene injection and combustion in a supersonic model combustor[J].Journal of Propulsion and Power,2006,22(1):103-110.
    [18]
    MacBride B J,Gordon S,Reno M A.Coefficient for calculating thermodynamic and transport properties of individual species [R].NASA TM-4513,1993.
    [19]
    Svehla R A.Transport coefficients for the NASA lewis chemical equilibrium program [R].NASA TM-4647,1995.
    [20]
    Smith G P,Golden D M,Frenklach M,et al.Overview of CRI-mech [EB/OL].[2012-07-19].Http://www.me.berkeley.edu/gri_mech.
    [21]
    WANG Hai,YOU Xiaoqing,Ameya V J,et al.Law,USC mech:Version Ⅱ high-temperature combustion reaction model of H2/CO/C1-C4 compounds[EB/OL].[2012-07-19].Http://ignis.usc.edu/USC_mech_II.htm.
    [22]
    Honnet S,Seshadri K,Niemann U,et al.A surrogate fuel for kerosene[J].Proceedings of the Combustion Institute,2009,32(1):485-492.
    [23]
    吴子牛,王兵,周睿,等.空气动力学[M].北京:清华大学出版社,2008.
    [24]
    Peters N.Turbulent combustion [M].New York:Cambridge University Press,2000.
    [25]
    孙明波,范周琴,梁剑寒,等.部分预混超声速燃烧火焰面模式研究综述[J].力学进展,2010,40(6):634-641. SUN Mingbo,FAN Zhouqin,LIANG Jianhan,et al.Evaluation of partially premixed flamelet approach in supersonic combustion[J].Advances in Mechanics,2010,40(6):634-641.(in Chinese)
    [26]
    Balakrishnan G,Williams F A.Turbulent combustion regions for hypersonic propulsion employing hydrogen/air diffusion flames[J].Journal of Propulsion and Power,1993,10(3):434-436.
    [27]
    Williams F A.Progress in knowledge of flamelet structure and extinction[J].Progress in Energy Combustion Science,2000,26(4/5/6):657-682.
    [28]
    Eifler P,Kollmann W.PDF prediction of supersonic hydrogen flames [R].AIAA 93-0448,1993.
    [29]
    Fureby C.LES for supersonic combustion [R].AIAA 2012-5979,2012.
    [30]
    Fureby C.A comparative study of flamelet and finite rate chemistry LES for a swirl stabilized flame[J].Journal of Engineering for Gas Turbines and Power,2012,134(4):041503.1-041503.13.
  • 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

    Article Metrics

    Article views (2055) PDF downloads(1083) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return