A study of steady laminar diffusion flames at buoyancy-induced low stretch rates in a spherical porous gas burner

IF 5.8 2区 工程技术 Q1 ENGINEERING, MECHANICAL
Shangqing Tao , Jun Fang , Yuhang Chen , Yahong Yang , Wei Chu , Jingwu Wang , Wenlong Wang , Longhua Hu
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Abstract

The steady combustion behavior and stability range of methane, ethylene, and propane in a low stretch spherical counterflow burner were investigated. Ethylene had the widest fuel mass flux (m˙) range of steady blue flame. A decreased buoyant stretch rate (ab) reduced this steady range. The critical m˙ at the extinction limit of the low stretch flames were lower than that of the normal gravity, and ethylene had the lowest critical m˙ at the lowest ab, indicating a wider steady fuel mass flux range for ethylene and a greater fire risk for microgravity low stretch flames. The ratio of the flame horizontal length to the vertical length (lf/yf) was quantified by a dimensionless parameter: Pe45(ΔFr)15(S+1)65, which considered the combined effects of burner properties (described by Péclet number Pe), gravity/buoyancy effect (described by expansion parameter Δ and Froude number Fr) and fuel combustion process (described by chemical reaction characteristic parameter S). The flame temperature Tf for the fuels increased with increasing uF and ab, whereas Tf increased slowly when uF was greater than the sooting limit uF due to incomplete combustion with appreciable heat loss. The low stretch flame temperatures of the three fuels rank as C2H4>C3H8>CH4 because of their different heats of combustion and heat losses. Both the gas-phase and solid-phase heat losses fractions were significant at low stretch rates. Solid-phase heat loss was vital to methane, which largely influenced its periodic flame hole instability near the extinction limit. This flame instability also extended the flammable range of methane at low stretch rates. This study can give instructions for microgravity combustion because a flame is usually initiated at low stretch rates under microgravity.
球形多孔气体燃烧器中浮力诱导低拉伸率稳定层流扩散火焰的研究
研究了甲烷、乙烯和丙烷在低拉伸球形逆流燃烧器中的稳定燃烧行为和稳定范围。乙烯具有最宽的燃料质量通量(m˙″)范围。下降的浮力拉伸率(ab)降低了这个稳定范围。低拉伸火焰熄灭极限的临界m˙″低于正常重力下的临界m˙″,而乙烯在最低ab处的临界m˙″最低,表明乙烯具有更宽的稳定燃料质量通量范围,而微重力低拉伸火焰具有更大的火灾风险。火焰水平长度与垂直长度之比(lf/yf)由一个无量纲参数Pe−45(ΔFr)−15(S+1)−65来量化,该参数考虑了燃烧器性能(由p 化学交换器数Pe描述)、重力/浮力效应(由膨胀参数Δ和弗劳德数Fr描述)和燃料燃烧过程(由化学反应特征参数S描述)的综合影响。燃料的火焰温度Tf随着uF和ab的增加而增加,而当uF大于燃灰极限uF时,由于燃烧不完全,热损失明显,Tf增加缓慢。由于三种燃料的燃烧热和热损失不同,其低拉伸火焰温度等级分别为C2H4>;C3H8>CH4。在低拉伸速率下,气相和固相热损失分数均显著。固相热损失对甲烷至关重要,它在很大程度上影响了甲烷在熄灭极限附近的周期性火焰孔不稳定性。这种火焰不稳定性也扩大了甲烷在低拉伸率下的可燃范围。这项研究可以为微重力燃烧提供指导,因为火焰通常在微重力下以低拉伸率启动。
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来源期刊
CiteScore
10.30
自引率
13.50%
发文量
1319
审稿时长
41 days
期刊介绍: International Journal of Heat and Mass Transfer is the vehicle for the exchange of basic ideas in heat and mass transfer between research workers and engineers throughout the world. It focuses on both analytical and experimental research, with an emphasis on contributions which increase the basic understanding of transfer processes and their application to engineering problems. Topics include: -New methods of measuring and/or correlating transport-property data -Energy engineering -Environmental applications of heat and/or mass transfer
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