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FLAME STABILIZATION OVER ATSUJI BURNER BY FOUR-STEP CHEMICAL REACTION

机译:四步化学反应稳定化燃烧器上的火焰

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This investigation applies a four-step chemical kinetics mechanism to implement the original combustion model developed by Chen and Weng (Combustion Science and Technology, Vol. 73, pp. 427-446, 1990). Comparing the blowoff curve of Tsuji (Progress in Energy and Combustion Science, Vol. 8, p. 93, 1982) with that of Chen and Weng reveals that this study yields a much better prediction than that in the latter reference. Also, the data in this study has an excellent agreement with the measured data of Dreier et al. (Berichtc der Bunsen-Gesetlschaft―Physical Chemistry, Vol. 90, pp. 1010-1015, 1986). The interested parameter is the inflow velocity U_(in). As U_(in) increases, the envelope diffusion flame, wake flame, liftoff flame, and another wake flame appear in that order before complete extinction. The formal wake flame is transformed from the envelope diffusion flame and the other is from the liftoff flame. The existence of a liftoff flame is verified by a corresponding experimental observation (Tsa et al., 2003). The maximal liftoff height is 1.7D when U_(in) is 1.05 m/s, and this height is maintained up to U_(in)= 1.09 m/s. Then the height declines gradually as the inflow velocity increases, which is a process that can be regarded as flashback. No recirculation flow exists behind the cylindrical burner for these liftoff flames. A transition from liftoff to wake flame occurs between 1.13 to 1.15 m/s. The wake flame reappears at U_(in)=1.16 m/s. Finally, the flame is extinguished completely when U_(in) > 2.12 m/s. The flame's lifting and dropping back is explained.
机译:这项研究采用了四步化学动力学机制来实现Chen和Weng(燃烧科学与技术,第73卷,第427-446页,1990年)开发的原始燃烧模型。将Tsuji(能源与燃烧科学进展,第8卷,第93页,1982年)与Chen和Weng的排放曲线进行比较,发现该研究的预测要好于后者。而且,这项研究中的数据与Dreier等人的测量数据有很好的一致性。 (Berichtc der Bunsen-Gesetlschaft-Physical Chemistry,第90卷,第1010-1015页,1986年)。感兴趣的参数是流入速度U_(in)。随着U_(in)的增加,包络扩散火焰,尾流火焰,升空火焰和另一尾流火焰按此顺序出现,然后完全熄灭。形式上的尾流火焰由包络扩散火焰转化而另一种则由升空火焰转化。剥离火焰的存在通过相应的实验观察得到证实(Tsa等,2003)。当U_(in)为1.05 m / s时,最大升空高度为1.7D,并且该高度一直保持到U_(in)= 1.09 m / s。然后,高度随着流入速度的增加而逐渐降低,这一过程可以被视为反冲。在圆柱形燃烧器后面没有用于这些提升火焰的再循环流。从升空到尾焰的转变发生在1.13至1.15 m / s之间。尾焰以U_(in)= 1.16 m / s的速度重新出现。最后,当U_(in)> 2.12 m / s时,火焰完全熄灭。解释了火焰的上升和下降。

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