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首页> 外文期刊>Fuel >A comparative numerical investigation of reactivity controlled compression ignition combustion using Large Eddy Simulation and Reynolds-Averaged Navier-Stokes approaches
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A comparative numerical investigation of reactivity controlled compression ignition combustion using Large Eddy Simulation and Reynolds-Averaged Navier-Stokes approaches

机译:使用大涡模拟和雷诺平均Navier-Stokes方法进行反应性控制的压燃燃烧的比较数值研究

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摘要

In this work, a comparative numerical study of Reactivity Controlled Compression Ignition (RCCI) combustion was conducted using both the Large Eddy Simulation (LES) and Reynolds-Averaged Navier-Stokes (RANS) approaches. In order to clarify the associated chemical kinetic processes, a data processing method that is able to calculate average reaction pathways, and identify representative reactions for the species creation, consumption, and heat release was adopted. The LES case yielded a wrinkled spray-flame structure, in contrast to the smoother and concentrated structure predicted by the RANS case. However, despite the different distribution features, both cases demonstrated similar reaction pathways and heat release characteristics. Modeling results showed that the low-temperature heat releases in RCCI combustion were controlled by the n-heptane spray-combustion process and dominated by the reactions R8 (C7H15O2 - 2 = C7H15 - 2 + O-2), R95 (CH3COCH2 + O-2 = CH3COCH2O2), and R285 (HCO + O-2 = CO + HO2). In addition, low-temperature consumption pathways of n-heptane led to the substantial formation of a hydroxyl radical, which enhanced the consumption of iso-octane. As the combustion process progressed, high-temperature ignition pockets were found near the piston rim edge and squish regions, where heat release was dominated by the reaction R285. Intense high-temperature heat release was observed instantly from the ignition pockets, resulting in a rapid propagation of the reactive surfaces.
机译:在这项工作中,使用大涡模拟(LES)和雷诺平均Navier-Stokes(RANS)方法进行了反应性控制压燃(RCCI)燃烧的比较数值研究。为了阐明相关的化学动力学过程,采用了一种能够计算平均反应路径并确定物种形成,消耗和放热反应的数据处理方法。 LES案例产生了起皱的喷射火焰结构,与RANS案例所预测的更为平滑和集中的结构相反。但是,尽管分布特征不同,但两种情况都显示出相似的反应路径和放热特性。建模结果表明,RCCI燃烧过程中的低温放热受正庚烷喷雾燃烧过程控制,并受反应R8(C7H15O2-2 = C7H15-2 + O-2),R95(CH3COCH2 + O- 2 = CH3COCH2O2)和R285(HCO + O-2 = CO + HO2)。另外,正庚烷的低温消耗途径导致羟基自由基的大量形成,这增加了异辛烷的消耗。随着燃烧过程的进行,在活塞边缘和挤压区域附近发现了高温点火腔,在该区域中热量释放主要受反应R285的控制。立即从点火腔中观察到强烈的高温放热,导致反应性表面迅速扩散。

著录项

  • 来源
    《Fuel 》 |2019年第1期| 116023.1-116023.17| 共17页
  • 作者单位

    Tianjin Univ State Key Lab Engines 92 Weijin Rd Tianjin 300072 Peoples R China|Univ Wisconsin Engine Res Ctr 1500 Engn Dr Madison WI 53705 USA;

    Univ Wisconsin Engine Res Ctr 1500 Engn Dr Madison WI 53705 USA;

    Tianjin Univ State Key Lab Engines 92 Weijin Rd Tianjin 300072 Peoples R China;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Large Eddy Simulation; RCCI; Flame structure; Optical engine; Chemical kinetics;

    机译:大涡模拟RCCI;火焰结构;光学引擎;化学动力学;

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