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兵工学报 ›› 2017, Vol. 38 ›› Issue (3): 476-482.doi: 10.3969/j.issn.1000-1093.2017.03.009

• 论文 • 上一篇    下一篇

NOx对甲烷点火延迟时间影响的数值研究

邓同晔1,2, 徐庆尧1, 沈双晏1   

  1. (1.装备学院 激光推进及其应用国家重点实验室, 北京 101416; 2.南京理工大学 机械工程学院, 江苏 南京 210094)
  • 收稿日期:2016-07-08 修回日期:2016-07-08 上线日期:2017-04-24
  • 作者简介:邓同晔(1991—), 男, 硕士研究生。E-mail: njustdty@outlook.com
  • 基金资助:
    国家自然科学基金项目(11372356)

Numerical Investigation on the Effect of NOx on Ignition Delay of Mathane

DENG Tong-ye1,2, XU Qing-yao1, SHEN Shuang-yan1   

  1. (1.State Key Laboratory of Laser Propulsion & Application,Equipment Academy,Beijing 101416,China;2.School of Mechanical Engineering, Nanjing University of Science and Technology, Nanjing 210094, Jiangsu, China)
  • Received:2016-07-08 Revised:2016-07-08 Online:2017-04-24

摘要: 点火延迟时间是超燃冲压发动机设计中的重要参数之一。为研究氮氧化物(NOx)对甲烷点火延迟时间的影响,在GRI-Mech 3.0机理的基础上添加R326、R327、R328 3个反应,利用CHEMKIN 化学动力学软件,对CH4/O2/NOx/Ar混合气体的点火过程进行数值计算,并将数值计算数据与文献\[6\]中的实验数据进行了对比。通过对比发现添加3个反应之后,GRI-Mech 3.0机理能够较好地模拟含NOx时甲烷的点火过程。研究结果表明:NO2缩短甲烷点火延迟时间的程度比N2O缩短甲烷点火延迟时间的程度大;CH4/O2/NOx/Ar预混气体在富氧条件下(燃气当量比为0.5)的点火延迟时间要比贫氧条件下(燃气当量比为2.0)的点火延迟时间短。

关键词: 兵器科学与技术, 点火延迟时间, 氮氧化物, 甲烷, 数值计算

Abstract: Ignition delay time is an important parameter in the design of scramjet engine. Three reactions are added to the GRI-Mech 3.0 mechanism to investigate the effect of NOx on ignition delay of methane. The ignition process of CH4/O2/NOx/Ar mixtures is numerically calculated using the CHEMKIN chemical kinetics software, and the numerical calculation data were compared with the experimental data in Ref.\[6\]. It is found that the GRI-Mech 3.0 mechanism could well simulate the ignition process of methane with NOx when the reactions R326,R327 and R328 are added. Numerically calculated result shows that the addition of NO2, to a lesser extent of N2O, leads to the reduction in the ignition delay time of CH4/O2/Ar mixtures, which is in good agreement with the experimental result of Mathieu, and the ignition delay time of CH4/O2/NOx/Ar mixtures under the oxygen poor condition (fuel-air equivalence ratio of 0.5) is shorter than that under the fuel rich condition (fuel-air equivalence ratio of 2.0). Key

Key words: ordnancescienceandtechnology, ignitiondelaytime, NOx, methane, numericalcalculation

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