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首页> 外文期刊>Combustion and Flame >Turbulent burning velocities of premixed CH_4/diluent/air flames in intense isotropic turbulence with consideration of radiation losses
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Turbulent burning velocities of premixed CH_4/diluent/air flames in intense isotropic turbulence with consideration of radiation losses

机译:考虑辐射损失的强等向性湍流中预混合CH_4 /稀释剂/空气火焰的湍流燃烧速度

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摘要

This paper presents turbulent burning velocities, S_T, of several premixed CH_4/diluent/air flames at the same laminar burning velocity S_L = 0.1 m/s for two equivalence ratios φ = 0.7 and 1.4 near flammability limits with consideration of radiation heat losses from small (N_2 diluted) to large (CO_2 diluted). Experiments are carried out in a cruciform burner, in which the long vertical vessel is used to provide a downward propagating premixed flame and the large horizontal vessel equipped with a pair of counterrotating fans and perforated plates can be used to generate an intense isotropic turbulence in the central region between the two perforated plates. Turbulent flame speeds are measured by four different arrangements of pairs of ion-probe sensors at different positions from the top to the bottom of the central region in the burner. It is found that the effect of gas velocity on S_T measured in the central region can be neglected. Simultaneous measurements using the pressure transducer and ion-probe sensors show that the pressure rise due to turbulent burning has little influence on S_T. These measurements prove the accuracy of the S_T data. At φ = 0.7, the percentage of [(S_T/S_L)_(CO_2) - (S_T/S_L)_(N_2)]/(S_T/S_L)_(N_2) decreases gradually from —4 to —17% when values of u'/S_L increase from 4 to 46, while at φ = 1.4 such decrease is much more abrupt from —19 to —53% when values of u'/S_L only increase from 4 to 18. The larger the radiation losses, the smaller the values of S_T. This decreasing effect is augmented by increasing u'/S_L and is particularly pronounced for rich CH_4 flames. When u'/S_L = 18, lean CO_2 and/or N_2-diluted CH_4 flames have much higher, 3.6 and/or 1.8 times higher, values of S_T/S_L than rich CO_2 and/or N_2-diluted CH_4 flames, respectively. It is found that lean (φ = 0.7) CH_4 flames are very difficult to quench globally even when methane mixtures are diluted with 41% CO_2 having large radiation losses. Moreover, measurements of chemiluminescence intensities for these turbulent propagating CH_4/diluent/air flames using the photomultiplier are carried out. The peak light intensities of CH~* and C_2~* emitters are found to be qualitatively correlated with these aforementioned S_T data of lean and rich turbulent CH_4/diluent/air propagating flames, respectively. Finally, the scatter plot of S_T/S_L as a function of u'/S_L for tne aforementioned N_2- and CO_2-diluted CH_4 flames can be well compressed and approximated by a general correlation of turbulent burning velocities in a form of (S_T — S_L)/u' = 0.06 Da~(0.58), where Da is the turbulent Damkoehler number.
机译:本文提出了几种预混合CH_4 /稀释剂/空气火焰在相同层流燃烧速度S_L = 0.1 m / s下的湍流燃烧速度S_T,其中两个当量比φ= 0.7和1.4在易燃极限附近,同时考虑了小辐射热损失(N_2稀释)到大(CO_2稀释)。实验是在十字形燃烧器中进行的,其中长的垂直容器用于提供向下传播的预混火焰,大型水平容器配有一对反向风扇和穿孔板,可在燃烧室中产生强烈的各向同性湍流。两个穿孔板之间的中心区域。湍流火焰速度是通过在燃烧器中心区域的顶部到底部的不同位置,通过成对的离子探针传感器的四种不同布置来测量的。发现在中心区域测量的气体速度对S_T的影响可以忽略。使用压力传感器和离子探针传感器的同时测量表明,由于湍流燃烧而引起的压力升高对S_T影响很小。这些测量证明了S_T数据的准确性。在φ= 0.7时,[(S_T / S_L)_(CO_2)-(S_T / S_L)_(N_2)] /(S_T / S_L)_(N_2)的百分比从-4逐渐减小到-17% u'/ S_L的值从4增加到46,而在φ= 1.4时,当u'/ S_L的值仅从4增加到18时,这种减小从#19突然变到-53%。辐射损耗越大,减小S_T的值。通过增加u'/ S_L可以增强这种降低的效果,对于浓CH_4火焰尤为明显。当u'/ S_L = 18时,稀CO_2和/或N_2稀释的CH_4火焰的S_T / S_L值分别比浓CO_2和/或N_2稀释的CH_4火焰高得多,分别为3.6和/或1.8倍。发现稀薄的(φ= 0.7)CH_4火焰即使在甲烷混合物中被41%具有较大辐射损失的CO_2稀释时,也很难完全熄灭。此外,使用光电倍增管测量了这些湍流传播的CH_4 /稀释剂/空气火焰的化学发光强度。发现CH〜*和C_2〜*发射器的峰值光强度分别与稀薄和浓湍流CH_4 /稀释剂/空气传播火焰的上述S_T数据定性相关。最后,对于上述N_2和CO_2稀释的CH_4火焰,S_T / S_L的散射图作为u'/ S_L的函数可以通过(S_T_S_L)形式的湍流燃烧速度的一般相关性很好地压缩和近似)/ u'= 0.06 Da〜(0.58),其中Da是湍流的Damkoehler数。

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