首页> 外文期刊>Experimental Thermal and Fluid Science: International Journal of Experimental Heat Transfer, Thermodynamics, and Fluid Mechanics >The effect of jet velocity ratio on aerodynamics of a rectangular slot-burner in the presence of cross-flow
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The effect of jet velocity ratio on aerodynamics of a rectangular slot-burner in the presence of cross-flow

机译:错流条件下射流速度比对矩形狭缝燃烧器空气动力学的影响

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In a typical coal-fired power station boiler the ignition and the combustion of the fuel is largely controlled by burner aerodynamics. An experimental and numerical study of the rectangular slot-burners widely used on power stations in Victoria, Australia has been conducted to improve understanding of jet development within the boiler. The 1: 15 scale model burner consisted of a central (primary) rectangular fuel nozzle with two (secondary) rectangular air jets positioned above and below it. The burner jets entered the measurement vessel at an angle of 60 degrees to the wall. A cross-flow jet was attached to the wall of the vessel to simulate the recirculation prevalent in power station boilers. Experiments were conducted using a primary to cross-flow jet velocity ratio (phi) of 1.0 and secondary to primary jet velocity ratios (phi) of 1.0 and 3.0. Laser Doppler Anemometry (LDA) was used to measure mean and turbulent velocity components in the near field and downstream regions of the jets. Cross-flow significantly influenced the near field flow development from the slot-burner by deviating both primary and secondary jets from their geometric axes towards the wall. The degree of deviation was greater for phi = 1.0 since the higher velocity secondary jets increased the overall momentum of the primary jet for phi = 3.0. A numerical investigation of the rectangular slot-burner was also performed. First, the numerical results were validated against the experimental results and then visualization of the developing flow field was used to reveal the finer details of the cross-flow/burner jet interaction. Agreement between numerical and experimental jet features was good, although the numerical results predicted a primary jet that was marginally too narrow. Also the predicted downstream behaviour for phi = 3.0 deviated more significantly from experimental observation. Using the SST turbulence model, the numerical results suggested that a twin vortex was generated behind the initial region of the primary jet and this would aid in mixing of gas and fuel between primary and secondary jets. (c) 2007 Published by Elsevier Inc.
机译:在典型的燃煤电站锅炉中,燃料的着火和燃烧很大程度上由燃烧器的空气动力学来控制。已对澳大利亚维多利亚州的发电站中广泛使用的矩形狭槽燃烧器进行了实验和数值研究,以增进对锅炉内射流发展的了解。 1:15比例模型燃烧器由一个中央(主要)矩形燃料喷嘴和两个位于上方和下方的(次级)矩形空气喷嘴组成。燃烧器喷头与壁成60度角进入测量容器。错流射流连接到容器壁,以模拟电站锅炉中普遍存在的再循环。实验是使用1.0的一次流与横流速度比(phi)和1.0和3.0的二次流与一次射流速度比(phi)进行的。激光多普勒风速仪(LDA)用于测量射流近场和下游区域的平均和湍流速度分量。横流通过使一次喷射和二次喷射均从其几何轴向壁偏离,从而极大地影响了从狭缝燃烧器产生的近场气流。对于phi = 1.0,偏差程度更大,因为在phi = 3.0时,较高的速度的次级射流会增加初级射流的总动量。还对矩形槽式燃烧器进行了数值研究。首先,将数值结果与实验结果进行验证,然后使用显影流场的可视化来揭示错流/燃烧器射流相互作用的更详细信息。数值和实验射流特征之间的一致性很好,尽管数值结果预测一次射流略窄。而且,phi = 3.0的预测下游行为与实验观察结果相比有较大差异。使用SST湍流模型,数值结果表明在一次喷射的初始区域之后产生了一个双涡旋,这将有助于在一次喷射和二次喷射之间混合气体和燃料。 (c)2007年由Elsevier Inc.发布。

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