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A direct numerical simulation study of the influence of flame-generated vorticity on reaction-zone-surface area in weakly turbulent premixed combustion

机译:火焰产生涡度对弱湍流预混燃烧反应区表面积影响的直接数值模拟研究

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摘要

Direct numerical simulation data obtained from two statistically stationary, one-dimensional, planar, weakly turbulent, premixed flames are analyzed in order to examine the influence of flame-generated vorticity on the surface area of the reaction zone. The two flames are associated with the flamelet combustion regime and are characterized by two significantly different density ratios sigma = 7.53 and 2.5, with all other things being roughly equal. The obtained results indicate that generation of vorticity due to baroclinic torque within flamelets can impede wrinkling of the reaction surface, reduce its area, and, hence, decrease the burning rate. Thus, these results call for revisiting the widely accepted concept of combustion acceleration due to flame-generated turbulence. In particular, in the case of sigma = 7.53, the local stretch rate, which quantifies the local rate of increase or decrease in the surface area, is predominantly negative in regions characterized by a large magnitude of enstrophy or a large magnitude of the baroclinic torque term in the enstrophy transport equation, with the effect being more pronounced at larger values of the mean combustion progress variable. If the density ratio is low, e.g., sigma = 2.5, the baroclinic torque weakly affects the vorticity field within the mean flame brush and the aforementioned effect is not pronounced. Published under license by ATP Publishing.
机译:分析了从两个统计静止,一维,平面,弱湍流,预混合的火焰中获得的直接数值模拟数据,以检查火焰产生的涡度对反应区的表面积的影响。这两个火焰与燧发燧发燃烧制度相关,其特征在于两个显着不同的密度比σ= 7.53和2.5,所有其他东西大致相等。所获得的结果表明,由于絮状物内的倒核扭矩引起的涡度产生涡流可以阻碍反应表面的皱纹,降低其面积,并且因此降低燃烧速率。因此,这些结果要求重新探测由于火焰产生的湍流引起的广泛接受的燃烧加速概念。特别地,在Sigma = 7.53的情况下,定量局部区域的局部拉伸速率,其在表面积中的局部区域中的局部是负的,其特征在于敌意的大小的敌意或曲金扭矩的大量大小术语在敌意传输方程中,效果在较大的平均燃烧进度变量的较大值下更明显。如果密度比为低,例如Sigma = 2.5,曲金扭矩弱地影响平均火焰刷内的涡度场,并且上述效果并不明显。由ATP发布在许可证下发布。

著录项

  • 来源
    《Physics of fluids》 |2019年第5期|共15页
  • 作者单位

    Chalmers Univ Technol Dept Mech &

    Maritime Sci S-41296 Gothenburg Sweden;

    ONERA French Aerosp Lab F-91761 Palaiseau France;

    Kagoshima Univ Dept Mech Engn Kagoshima 8900065 Japan;

    Nagoya Univ Inst Mat &

    Syst Sustainabil Nagoya Aichi 4648603 Japan;

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  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 流体力学;
  • 关键词

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