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RP-3航空煤油燃烧的详细和简化化学动力学模型
引用本文:肖保国,杨顺华,赵慧勇,钱炜祺,乐嘉陵.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.
作者姓名:肖保国  杨顺华  赵慧勇  钱炜祺  乐嘉陵
作者单位:1. 中国空气动力研究与发展中心,计算空气动力学研究所,绵阳,621000
2. 中国空气动力研究与发展中心,计算空气动力学研究所,绵阳,621000;中国科学技术大学,物理学院,近代力学系,合肥,230026
基金项目:国家自然科学基金(90716017)
摘    要:建立了一个包含109组分和946个基元反应的煤油燃烧详细化学反应动力学模型,采用"准稳态"假设方法来对其进行简化,得到了包含22组分18步总包反应的简化反应模型.通过与典型实验结果和文献计算结果对比可以看出,简化模型具有较高的准确性,能够准确反映出RP-3航空煤油点火特性,能够用来对煤油燃烧问题进行准确的数值模拟.

关 键 词:航空煤油    化学动力学    简化化学动力学    “准稳态”假设    燃烧
收稿时间:8/3/2009 12:00:00 AM
修稿时间:2010/3/12 0:00:00

Detailed and reduced chemical kinetic mechanisms for RP-3 aviation kerosene combustion
XIAO Bao-guo,YANG Shun-hu,ZHAO Hui-yong,QIAN Wei-qi and LE Jia-ling.Detailed and reduced chemical kinetic mechanisms for RP-3 aviation kerosene combustion[J].Journal of Aerospace Power,2010,25(9):1948-1955.
Authors:XIAO Bao-guo  YANG Shun-hu  ZHAO Hui-yong  QIAN Wei-qi and LE Jia-ling
Institution:Institute of Computational Aerodynamics,China Aerodynamics Research and Development Center,Mianyang 621000,China;;Institute of Computational Aerodynamics,China Aerodynamics Research and Development Center,Mianyang 621000,China;Department of Modern Mechanics,School of Physical Sciences,University of Science and Technology of China,Hefei 230026,China;Institute of Computational Aerodynamics,China Aerodynamics Research and Development Center,Mianyang 621000,China;;Institute of Computational Aerodynamics,China Aerodynamics Research and Development Center,Mianyang 621000,China;;Institute of Computational Aerodynamics,China Aerodynamics Research and Development Center,Mianyang 621000,China;
Abstract:A detailed chemical kinetic mechanism containing 109 species and 946 elementary reactions for kerosene combustion was developed.With the use of quasi-stationary state approximation(QSSA) method,a reduced chemical kinetic mechanism including 22 species and 18 global reactions was obtained from the detailed kinetics.By comparing the reduced mechanisms with the typical experimental results and reference results,high precision of the reduced mechanisms is shown,which can be used to represent the ignition characteristic of RP-3 aviation kerosene fuel,and also simulate accurately the combustion of kerosene.
Keywords:aviation kerosene  chemical kinetics  reduced chemical kinetics  quasi-stationary state approximation  combustion
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