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Numerical analysis of turbulence radiation interaction effect on radiative heat transfer in a swirling oxyfuel furnace

机译:湍流氧相互作用对旋流式富氧燃烧炉辐射传热影响的数值分析

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摘要

With the application of oxyfuel combustion technology, the status of radiative heat transfer in oxyfuel flames is prominent, and accurate description of it is essential. This study simulates the turbulence radiation interaction (TRI) in a swirling gas-fired furnace to understand the thermal radiation behavior under oxycombustion conditions. Employing the non-gray weighted sum of gray gases model calculates the radiative properties of the participating media and the TRI is modeled. The effects of TRI on the radiative heat transfer in the furnace under different oxycombustion conditions and swirl numbers are analyzed. The results show that the effects of thermal radiation on temperature fields are critical in the gas-fired furnace, especially for oxycombustion condition with high oxygen concentration, and the same is true for TRI effect. With the increase of O-2 concentration in O-2/CO2 oxidizer, the radiative heat flux on the chamber wall, the radiative heat flux contribution to total heat flux, and the net radiative heat loss are increased. Increasing swirl number can weaken the TRI effect. It is observed that with 35% O-2 in oxidizer, the radiation contribution to heat flux along the entire wall and local increase of radiative heat flux due to TRI effect are almost than 45% and 18%, respectively. (C) 2019 Elsevier Ltd. All rights reserved.
机译:随着含氧燃料燃烧技术的应用,含氧燃料火焰中辐射传热的状况日益突出,对其进行准确的描述至关重要。这项研究模拟了涡流燃气炉中的湍流辐射相互作用(TRI),以了解在氧燃烧条件下的热辐射行为。使用灰色气体的非灰色加权总和模型可以计算参与介质的辐射特性,并可以对TRI进行建模。分析了在不同的氧燃烧条件和旋流数下,TRI对炉内辐射换热的影响。结果表明,在燃气炉中,热辐射对温度场的影响至关重要,特别是对于高氧浓度的氧燃烧条件,TRI效应也是如此。随着O-2 / CO2氧化剂中O-2浓度的增加,腔室壁上的辐射热通量,辐射热通量对总热通量的贡献以及净辐射热损失都增加了。增加旋流数会削弱TRI效应。可以看出,在氧化剂中使用35%的O-2时,沿着整个壁的辐射对热通量的贡献和由于TRI效应引起的辐射热通量的局部增加分别接近于45%和18%。 (C)2019 Elsevier Ltd.保留所有权利。

著录项

  • 来源
    《International Journal of Heat and Mass Transfer》 |2019年第10期|1227-1237|共11页
  • 作者单位

    Harbin Inst Technol, Key Lab Aerosp Thermophys, Minist Ind & Informat Technol, Harbin 150001, Heilongjiang, Peoples R China|Harbin Inst Technol, Sch Energy Sci & Engn, Harbin 150001, Heilongjiang, Peoples R China;

    Harbin Inst Technol, Sch Energy Sci & Engn, Harbin 150001, Heilongjiang, Peoples R China;

    Harbin Inst Technol, Key Lab Aerosp Thermophys, Minist Ind & Informat Technol, Harbin 150001, Heilongjiang, Peoples R China|Harbin Inst Technol, Sch Energy Sci & Engn, Harbin 150001, Heilongjiang, Peoples R China;

    Harbin Inst Technol, Key Lab Aerosp Thermophys, Minist Ind & Informat Technol, Harbin 150001, Heilongjiang, Peoples R China|Harbin Inst Technol, Sch Energy Sci & Engn, Harbin 150001, Heilongjiang, Peoples R China;

    Harbin Inst Technol, Key Lab Aerosp Thermophys, Minist Ind & Informat Technol, Harbin 150001, Heilongjiang, Peoples R China|Harbin Inst Technol, Sch Energy Sci & Engn, Harbin 150001, Heilongjiang, 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

    Radiative heat transfer; Turbulence radiation interaction; Oxyfuel combustion; Swirl number;

    机译:辐射传热;湍流辐射相互作用;奥氧燃料燃烧;旋流号码;

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