首页> 外文期刊>Experimental Thermal and Fluid Science: International Journal of Experimental Heat Transfer, Thermodynamics, and Fluid Mechanics >Near field flow structure of isothermal swirling flows and reacting non-premixed swirling flames
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Near field flow structure of isothermal swirling flows and reacting non-premixed swirling flames

机译:等温回旋流与未预混回旋火焰反应的近场流结构

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Two confined lean non-premixed swirl-stabilized flame typologies were investigated in order to achieve detailed information on the thermal and aerodynamic field in the close vicinity of the burner throat and provide correlation with the exhaust emissions. Previous finding indicated the generation of a partially premixed flame with radial fuel injection and a purely diffusive flame with co-axial injection in a swirling co-flow. In the present work, the experimental study is reported which has been conducted on a straight exit laboratory burner with no quarl cone, fuelled by natural gas and air, and fired vertically upwards with the flame stabilized at the end of two concentric pipes with the annulus supplying swirled air and the central pipe delivering the fuel. Two fuel injection typologies, co-axial and radial (i.e., transverse), leading to different mixing mechanisms, have been characterized through different techniques: particle image velocimetry (PIV) and laser Doppler velocimetry (LDV) for a comprehensive analysis of the velocity field, still photography for the detection of flame front and main visible features, and thermocouples for the temperature distribution. Isothermal flow conditions have been included in the experimental investigation to provide a basic picture of the flow field and to comprehend the modifications induced by the combustion process. The results indicated that, although the global mixing process and the main flame structure are governed by the swirl motion imparted to the air stream, the two different fuel injection methodologies play an important role on mixture formation and flame stabilization in the primary mixing zone. Particularly, it has been found that, in case of axial injection, the turbulent interaction between the central fuel jet and the backflow generated by the swirl can induce an intermittent fuel penetration in the recirculated hot products and the formation of a central sooting luminous plume, a phenomenon totally absent in the case of radial injection. (c) 2006 Elsevier Inc. All rights reserved.
机译:为了获得有关燃烧器喉道附近的热力和空气动力场的详细信息,并提供与废气排放的相关性,研究了两种密闭的稀薄非预混合旋流稳定火焰类型。先前的发现表明,在径向同流的情况下,通过径向燃料喷射产生了部分预混火焰,而在同轴流下通过同轴注入产生了纯扩散火焰。在目前的工作中,据报道进行了实验研究,该实验是在没有夸脱锥的直出口实验室燃烧器上进行的,该燃烧器由天然气和空气提供燃料,并在火焰稳定的情况下垂直向上燃烧,在带有环形空间的两个同心管末端供应涡旋空气,中央管道输送燃料。通过不同的技术对两种导致不同混合机制的燃料喷射类型(同轴和径向)进行了表征:粒子图像测速(PIV)和激光多普勒测速(LDV),用于对速度场进行全面分析,用于检测火焰前缘和主要可见特征的静态照片以及用于温度分布的热电偶。等温流动条件已包括在实验研究中,以提供流场的基本情况并理解由燃烧过程引起的变化。结果表明,尽管整体混合过程和主要火焰结构受赋予空气流的涡旋运动控制,但两种不同的燃料喷射方法在主要混合区的混合物形成和火焰稳定方面起着重要作用。特别地,已经发现,在轴向喷射的情况下,中央燃料射流与旋流产生的回流之间的湍流相互作用可以引起燃料在间歇性地渗透到再循环的热产物中,并形成中央的烟灰发光烟羽。在径向注射的情况下完全没有这种现象。 (c)2006 Elsevier Inc.保留所有权利。

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