Volume 31 Issue 9
Sep.  2016
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LIU Yu, ZENG Wen, MA Hong-an, CHEN Bao-dong. Combustion reaction mechanism of three-component simulation surrogate fuel for RP-3 kerosene[J]. Journal of Aerospace Power, 2016, 31(9): 2055-2064. doi: 10.13224/j.cnki.jasp.2016.09.002
Citation: LIU Yu, ZENG Wen, MA Hong-an, CHEN Bao-dong. Combustion reaction mechanism of three-component simulation surrogate fuel for RP-3 kerosene[J]. Journal of Aerospace Power, 2016, 31(9): 2055-2064. doi: 10.13224/j.cnki.jasp.2016.09.002
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Combustion reaction mechanism of three-component simulation surrogate fuel for RP-3 kerosene

doi: 10.13224/j.cnki.jasp.2016.09.002

  • Faculty of Aerospace Engineering, Shenyang Aerospace University, Shenyang 110136, China

  • Received Date: 2015-10-20
  • Publish Date: 2016-09-28
    Abstract
  • A kind of combustion reaction mechanism of surrogate fuel was developed, including 65% n-decane, 10% toluene and 25% propyl cyclohexane for RP-3 kerosene. The mechanism consisted of 150 species and 591 elementary reactions. The ignition and combustion characteristics of surrogate fuel at various conditions were simulated by this reaction mechanism, and the simulation results were compared with those of another one-component surrogate fuel (n-decane) and the experimental data, respectively. Results show that the chemical reaction mechanism of three-component surrogate fuel can accurately calculate the ignition and combustion characteristics of RP-3 kerosene. The calculation deviation of the ignition delay time can be controlled within 5%, and the calculation error of the laminar burning velocity can be controlled within 10%, better than those of n-decane. The combustion reaction mechanism of three-component surrogate fuel was also modified by sensitivity analysis, showing that the calculation error of the laminar burning velocity was improved from 10% to 5%. This means the modified mechanism can predict the ignition delay time and laminar burning velocity of RP-3 kerosene better.

     

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    • References(20)
  • [1]
    刘涛,纪军,卫海桥,等.先进发动机燃烧基础研究的进展和关键科学问题[J].中国科学基金,2012,26(1):325-329. LIU Tao,JI Jun,WEI Haiqiao,et al.Progress and key scientific issues on advanced engine combustion research[J].Bulletin of National Natural Science Foundation of China,2012,26(1):325-329.(in Chinese)
    [2]
    Dagaut P,Cathonnet M.The ignition,oxidation,and combustion of kerosene:a review of experimental and kinetic modeling[J].Progress in Energy and Combustion Science,2006,32(1):48-92.
    [3]
    You X,Egolfopoulos F N,Wang H.Detailed and simplified kinetic models of n-dodecane oxidation:the role of cracking in aliphatic hydrocarbon combustion[J].Proceedings of the Combustion Institute,2009,32(1):403-410.
    [4]
    Honnet S,Seshadri K,Niemann U,et al.A surrogate fuel for kerosene[J].Proceedings of the Combustion Institute,2009,32(1):485-492.
    [5]
    范学军,俞刚.大庆RP-3航空煤油热物性分析[J].推进技术,2006,27(2):187-192. FAN Xuejun,YU Gang.Analysis of thermophysical properties of Daqing RP-3 aviation kerosene[J].Journal of Propulsion Technology,2006,27(2):187-192.(in Chinese)
    [6]
    肖保国,杨顺华,赵慧勇,等.RP-3航空煤油燃烧的详细和简化化学动力学模型[J].航空动力学报,2010,25(9):1948-1955. XIAO Baoguo,YANG Shunhua,ZHAO Huiyong,et al.Detailed and reduced chemical kinetic mechanisms for RP-3 aviation kerosene combustion[J].Journal of Aerospace Power,2010,25(9):1948-1955.(in Chinese)
    [7]
    ZHANG Ruoling,JIANG Jing,LE Jialing.The simulation of endothermic fuel flow in cooling channels of scramjet[R].[S.l.]:International Conference on Methods of Aerophysical Research,2008.
    [8]
    徐佳琪,郭俊江,刘爱科,等.RP-3替代燃料自点火燃烧机理构建及动力学模拟[J].物理化学学报,2015,31(4):643-652. XU Jiaqi,GUO Junjiang,LIU Aike,et al.Construction of autoignition mechanisms for the combustion of RP-3 surrogate fuel and kinetics simulation[J].Acta Physico-Chimica Sinica,2015,31(4):643-652.(in Chinese)
    [9]
    郑东,于维铭,钟北京.RP-3航空煤油替代燃料及其化学反应动力学模型[J].物理化学学报,2015,31(4):636-642. ZHENG Dong,YU Weiming,ZHONG Beijing.RP-3 aviation kerosene surrogate fuel and the chemical reaction kinetic model[J].Acta Physico-Chimica Sinica,2015,31(4):636-642.(in Chinese)
    [10]
    曾文,李海霞,马洪安,等.RP-3航空煤油着火特性的实验[J].航空动力学报,2014,29(3):481-488. ZENG Wen,LI Haixia,MA Hongan,et al.Experiment of ignition characteristics of RP-3 kerosene[J].Journal of Aerospace Power,2014,29(3):481-488.(in Chinese)
    [11]
    曾文,李海霞,马洪安,等.RP-3航空煤油模拟替代燃料的化学反应详细机理[J].航空动力学报,2014,29(12):2810-2816. ZENG Wen,LI Haixia,MA Hongan,et al.Detailed chemical reaction mechanism of surrogate fuel for RP-3 kerosene[J].Journal of Aerospace Power,2014,29(12):2810-2816.(in Chinese)
    [12]
    曾文,李海霞,马洪安,等.RP-3航空煤油模拟替代燃料的化学反应简化机理[J].推进技术,2014,35(8):1139-1145. ZENG Wen,LI Haixia,MA Hongan,et al.Reduced chemical reaction mechanism of surrogate fuel for RP-3 kerosene[J].Journal of Propulsion Technology,2014,35(8):1139-1145.(in Chinese)
    [13]
    Bikas G,Peters N.Kinetic modelling of n-decane combustion and autoignition[J].Combustion and Flame,2001,126(1/2):1456-1475.
    [14]
    Honnet S,Seshadri K,Niemann U,et al.A surrogate fuel for kerosene[J].Proceedings of the Combustion Institute,2009,32(1):485-492.
    [15]
    李海霞.RP-3航空煤油着火特性的实验与反应动力学研究[D].沈阳:沈阳航空航天大学,2013. LI Haixia.The experiment on ignition characteristic and research on reaction kinetics of RP-3 kerosene[D].Shenyang:Shenyang Aerospace University,2013.(in Chinese)
    [16]
    Dagaut P.On the kinetics of hydrocarbon oxidation from natural gas to kerosene and diesel fuel[J].Physical Chemistry Chemical Physics,2002,4(1):2079-2094.
    [17]
    张英佳,黄佐华,王金华,等.激波管研究煤油/空气混合气的自着火特性[J].科学通报,2011,56(1):85-93. ZHANG Yingjia,HUANG Zuohua,WANG Jinhua,et al.Shock tube study on auto-ignition characteristics of kerosene/air mixtures[J].Chinese Science Bulletin,2011,56(1):85-93.(in Chinese)
    [18]
    Hu E J,Huang Z H,He J J,et al.Experimental and numerical study on laminar burning characteristics of premixed methane-hydrogen-air flames[J].International Journal of Hydrogen Energy,2009,34(11):4876-4888.
    [19]
    Lamoureux N,Djebäýli-Chaumeix N,Paillard C E.Laminar flame velocity determination for H2-air-He-CO2 mixtures using the spherical bomb method[J].Experimental Thermal and Fluid Science,2003,27(4):385-393.
    [20]
    Bradley D,Gaskell PH,Gu X J.Burning velocities,Markstein lengths,and flame quenching for spherical methane-air flames:a computational study[J].Combustion and Flame,1996,104(1/2):176-198.
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