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Shapes of nonbuoyant round hydrocarbon-fueled laminar-jet diffusion flames in still air

机译:静止空气中非浮力的圆形烃类燃料层流射流扩散火焰的形状

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摘要

The soot-luminosity boundaries (near the laminar smoke-point condition) of steady nonbuoyant round hydrocarbon/air laminar-jet diffusion flames at micrograv'ity were found from color video images obtained on orbit during three flights of the Space Shuttle Columbia (flights STS-83, STS-94, and STS-107); these test conditions included ethylene- and propane-fueled flames burning in still air at an ambient temperature of 300 K, ambient pressures of 35-130 kPa, jet exit diameters of 0.40-2.70 mm, and jet exit Reynolds numbers of 46-1186 to yield steady round flames, with most of the flames near the laminar smoke-point condition (including flames both emitting and not emitting soot). These results were supplemented by observations of the flame-sheet locations (locations where the local mixture fraction is stoichiometric) of nonbuoyant round soot-free and soot-containing hydrocarbon/air laminar-jet diffusion flames at microgravity found from filtered color images (at the CH line or 430 ± 5 nm) obtained using a 2.2-s free-fall facility; these test conditions included methane-, ethane-, and propane-fueled flames burning in still air at an ambient temperature of 300 K, ambient pressures of 25-98 kPa, jet exit diameters of 0.42-3.25 mm, and jet exit Reynolds numbers of 10-625. Simplified expressions to estimate soot-luminosity boundaries (near the laminar smoke-point condition) and flame-sheet locations were obtained using the classic analysis of D.B. Spalding (Combustion and Mass Transfer, Pergamon, New York, 1979, p. 185), extended empirically to account for the presence of soot luminosity for flames near the laminar smoke-point condition. The extended Spalding analysis provided good correlations of both soot-luminosity boundaries (near the laminar smoke-point condition) and flame-sheet locations for flames having short characteristic residence times where radiative heat losses from the flames were small. These results showed that soot-luminosity lengths near the laminar smoke-point condition were roughly twice as long as the flame-sheet location for both soot-free (blue) and soot-containing flames under comparable conditions due to the presence of luminous soot particles beyond the flame sheet within the fuel-lean portion of the flames.
机译:从哥伦比亚航天飞机三趟飞行中在轨道上获得的彩色视频图像中发现了微重力下稳定的非浮力圆形碳氢化合物/空气层流射流扩散火焰的烟尘光度边界(在层流烟点条件附近)。 -83,STS-94和STS-107);这些测试条件包括以乙烯和丙烷为燃料的火焰在环境温度为300 K的静止空气中燃烧,环境压力为35-130 kPa,射流出口直径为0.40-2.70 mm,射流雷诺数为46-1186至产生稳定的圆形火焰,大多数火焰接近层状烟点状态(包括同时发射和不发射烟灰的火焰)。通过观察从过滤后的彩色图像中发现的微重力下的无浮力的圆形无烟灰和含烟灰的碳氢化合物/空气层流扩散火焰的火焰片位置(局部混合比为化学计量的位置),可以补充这些结果。 CH线或430±5 nm)使用2.2-s自由落体设备获得;这些测试条件包括在环境温度为300 K,在静止空气中燃烧的甲烷,乙烷和丙烷为燃料的火焰,环境压力为25-98 kPa,射流出口直径为0.42-3.25 mm,射流雷诺数为10-625。使用D.B.的经典分析方法获得了简化的表达式,以估算烟灰光度边界(接近层状烟点条件)和火焰片位置。 Spalding(燃烧与传质,Pergamon,纽约,1979年,第185页)从经验上进行了扩展,以说明层流烟点条件附近火焰存在烟灰光度。对于具有短特征停留时间的火焰(火焰辐射热损失很小),扩展的Spalding分析提供了烟灰光度边界(靠近层状烟点条件)和火焰片位置的良好关联。这些结果表明,在类似条件下,由于存在发光的烟尘颗粒,层流烟点条件附近的烟尘发光长度大约是无烟尘(蓝色)和含烟尘火焰的火焰片位置长度的两倍。超出火焰薄层内的火焰。

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