Observation of Turbulent Mixing in Lean-Direct-Injection Combustion at Elevated Pressure

被引:7
作者
Kojima, Jun [1 ]
Nguyen, Quang-Viet [2 ]
机构
[1] Ohio Aerosp Inst, Turbomachinery & Prop Syst Team, Cleveland, OH 44142 USA
[2] NASA, John H Glenn Res Ctr Lewis Field, Combust Branch, Cleveland, OH 44135 USA
关键词
D O I
10.2514/1.37433
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
We report the first quantitative single-shot multiscalar data obtained from a realistic air-fed lean-direct-injection burner operating on gaseous methane (CH4) fuel at elevated pressure (5 atm) using single-shot spontaneous Raman spectroscopy. From a statistical analysis of the multiscalar data, we present spatially mapped probability density functions of the concentration of CH4 and O-2, and the instantaneous temperature. The measured three-scalar correlations and probability density functions provide insights into the nature and extent of the mixing process and its impact on the subsequent combustion process. The data will also be useful for comparison with the various turbulence-chemistry interaction models such as large-eddy simulation. The swirl-stabilized flame investigated in this paper was characterized as operating in a partially premixed combustion regime that was dominated by turbulent mixing provided by the lean-direct-injection configuration. Although a majority of the single-shot data indicated complete or near-complete reactions including stoichiometric combustion, a considerable number of the data points exhibited incomplete combustion characterized by a substantial amount of residual fuel at intermediate temperatures or were simply unreacted with little or no preheating of the mixture.
引用
收藏
页码:3116 / 3127
页数:12
相关论文
共 51 条
  • [1] ARCHER S, 2003, 20031343 AIAA
  • [2] Laser diagnostics and their interplay with computations to understand turbulent combustion
    Barlow, Robert S.
    [J]. PROCEEDINGS OF THE COMBUSTION INSTITUTE, 2007, 31 : 49 - 75
  • [3] A shutter-based line-imaging system for single-shot Raman scattering measurements of gradients in mixture fraction
    Barlow, RS
    Miles, PC
    [J]. PROCEEDINGS OF THE COMBUSTION INSTITUTE, 2000, 28 : 269 - 277
  • [4] BARLOW RS, 2006, TNF8 WORKSH P SAND N
  • [5] Comparisons of laser-saturated, laser-induced, and planar laser-induced fluorescence measurements of nitric oxide in a lean direct-injection spray flame
    Cooper, CS
    Ravikrishna, RV
    Laurendeau, NM
    [J]. APPLIED OPTICS, 1998, 37 (21): : 4823 - 4833
  • [6] THE SPONTANEOUS RAMAN-SCATTERING TECHNIQUE APPLIED TO NONPREMIXED FLAMES OF METHANE
    DIBBLE, RW
    MASRI, AR
    BILGER, RW
    [J]. COMBUSTION AND FLAME, 1987, 67 (03) : 189 - 206
  • [7] An experimental and computational study of a multi-swirl gas turbine combustor
    Fureby, C.
    Grinstein, F. F.
    Li, G.
    Gutmark, E. J.
    [J]. PROCEEDINGS OF THE COMBUSTION INSTITUTE, 2007, 31 : 3107 - 3114
  • [8] Turbulent opposed-jet flames: A critical benchmark experiment for combustion LES
    Geyer, D
    Kempf, A
    Dreizler, A
    Janicka, J
    [J]. COMBUSTION AND FLAME, 2005, 143 (04) : 524 - 548
  • [9] Introduction: Combustion modeling and large eddy simulation: Development and validation needs for gas turbines
    Grinstein, FF
    Liu, NS
    Oefelein, JC
    [J]. AIAA JOURNAL, 2006, 44 (04) : 673 - 673
  • [10] Flow dynamics in a swirl combustor
    Grinstein, FF
    Young, TR
    Gutmark, EJ
    Li, GQ
    Hsiao, G
    Mongia, HC
    [J]. JOURNAL OF TURBULENCE, 2002, 3