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A comprehensive study of flamelet tabulation methods for pulverized coal combustion in a turbulent mixing layer-Part Ⅱ: Strong heat losses and multi-mode combustion

机译:湍流混合层粉碎煤燃烧爆破煤燃烧的综合研究Ⅱ:强热损耗和多模燃烧

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摘要

This paper is a continuation of our work done in Part I, in which the a priori and budget analyses were conducted, Wen et al. (2019). In this work, we focus on addressing specific and recurring issues in flamelet modeling for pulverized coal combustion, including strong heat losses, multi-mode combustion and reaction progress variable definition. First, extended flamelet formulations are developed that can take into account strong heat loss effects in pulverized coal combustion systems. Then, to characterize multi-mode combustion in pulverized coal flames, a coupled premixed and non-premixed flamelet model is developed using the combustion mode index. Finally, the effects of reaction progress variable definition on the flamelet predictions are quantified. A state-of-the-art direct numerical simulation database is employed to challenge the newly developed flamelet models. The tabulated thermo-chemical quantities are compared with the reference direct numerical simulation results through a priori analyses. Comparisons show that the newly developed flamelet models which take into account strong heat loss effects can predict the gas temperature and species mass fractions correctly. The adiabatic flamelet models overpredict the corresponding thermo-chemical quantities in regions where the interphase heat transfer is significant. Coupled with a linear extrapolation method, the prediction of the gas temperature with the adiabatic flamelet models can be improved. The performance of the multi-mode flamelet model depends on whether the local combustion mode can be correctly identified. The conventional combustion mode index based on the gradients of fuel and oxidizer species mass fractions cannot correctly identify the combustion mode in the entire combustion field. (C) 2019 The Combustion Institute. Published by Elsevier Inc. All rights reserved.
机译:本文是我们在第一部分中完成的工作的延续,其中进行了先验和预算分析,Wen等人。 (2019)。在这项工作中,我们专注于解决粉煤燃烧的轰炸机型燃烧的特定和经常性问题,包括强烈的热损失,多模燃烧和反应进度变量定义。首先,开发出扩展的爆炸制剂,其可以考虑粉煤燃烧系统中的强烈的热损失效应。然后,为了在粉煤火焰中表征多模式燃烧,使用燃烧模式指数开发耦合的预混合和未预混的燧发塞模型。最后,量化了反应进度变量定义对燧发士预测的影响。采用最先进的直接数值模拟数据库来挑战新开发的击败模型。通过先验分析将制表的热化学量与参考直接数值模拟结果进行比较。比较表明,新开发了考虑到强烈的热量损失效应的爆发模型可以正确预测气体温度和物种质量级分。绝热燧发物质模型过度地估计相互传热显着的区域中的相应热化学量。耦合与线性外推法,可以提高与绝热燧发燧弹模型的气体温度的预测。多模式爆发模型的性能取决于是否可以正确识别本地燃烧模式。基于燃料和氧化剂物质质量级别的梯度的常规燃烧模式指数不能正确地识别整个燃烧场中的燃烧模式。 (c)2019燃烧研究所。由elsevier Inc.出版的所有权利保留。

著录项

  • 来源
    《Combustion and Flame》 |2020年第6期|453-467|共15页
  • 作者单位

    Tech Univ Darmstadt Simulat React Thermofluid Syst STFS D-64827 Darmstadt Germany|Zhejiang Univ State Key Lab Clean Energy Utilizat Hangzhou 310027 Peoples R China;

    Univ Duisburg Essen Inst Combust & Gasdynam IVG Chair Fluid Dynam D-47057 Duisburg Germany;

    Tech Univ Darmstadt Simulat React Thermofluid Syst STFS D-64827 Darmstadt Germany;

    Univ Stuttgart Inst Tech Verbrennung ITV Herdweg 51 D-70174 Stuttgart Germany;

    Zhejiang Univ State Key Lab Clean Energy Utilizat Hangzhou 310027 Peoples R China;

    Zhejiang Univ State Key Lab Clean Energy Utilizat Hangzhou 310027 Peoples R China;

    Univ Stuttgart Inst Tech Verbrennung ITV Herdweg 51 D-70174 Stuttgart Germany;

    Zhejiang Univ State Key Lab Clean Energy Utilizat Hangzhou 310027 Peoples R China;

    Tech Univ Darmstadt Simulat React Thermofluid Syst STFS D-64827 Darmstadt Germany;

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

    Pulverized coal combustion; Turbulent mixing layer; Flamelet tabulation methods; Strong heat losses; Multi-mode combustion;

    机译:煤粉燃烧;湍流混合层;爆炸式制表方法;强热损失;多模燃烧;

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