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The influence of micro air jets on mixing augmentation of transverse hydrogen jet in supersonic flow

机译:微型空气射流对超音速流动中横向氢射流混合增强的影响

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In this paper, numerical simulation is performed to investigate the effects of micro air jets on mixing of the micro hydrogen jet in a transverse supersonic flow. The fundamental flow feature of the interaction between an array of fuel and air jets is investigated in a Mach 4.0 crossflow with a fuel global equivalence ratio of 0.5. Parametric studies were conducted on the various air jet conditions by using the Reynolds-averaged Navier Stokes equations with Menter's Shear Stress Transport (SST) turbulence model. Numerical study of eight streamwise transverse sonic fuel and air jets in a fully turbulent supersonic flow revealed an extremely complex feature of fuel and air jet interaction. The results present various flow features depending upon the number and mass flow rate of micro air jets. These flow features were found to have significant effects on the mixing of hydrogen jets. Results also show a different flow structure as air jet is presented in the downstream of each fuel jet. According to the obtained results, mixing rate is low in micro fuel jets without air jets. When the air jets are injected in the downstream of each fuel jet, the mixing of the hydrogen jet significantly increases (more than 60%) in the downstream. As the number of air jets is increased, the mixing performance of the fuel jet is increased more than 150%. Therefore, an enhanced mixing zone is obtained in downstream of the injection slots which leads to flame-holding. (C) 2016 Hydrogen Energy Publications LLC. Published by Elsevier Ltd. All rights reserved.
机译:在本文中,进行了数值模拟,以研究微空气射流对超音速横向流动中微氢射流混合的影响。燃料与空气射流之间相互作用的基本流动特征是在4.0马赫错流中进行的,燃料的整体当量比为0.5。使用雷诺平均的Navier Stokes方程和Menter的剪切应力传递(SST)湍流模型,对各种空气喷射条件进行了参数研究。在完全湍流的超音速流中对八个沿流向的横向声波燃料和空气射流进行的数值研究揭示了燃料和空气射流相互作用的极其复杂的特征。结果呈现出各种流动特征,这取决于微型空气喷嘴的数量和质量流率。发现这些流动特征对氢射流的混合具有显着影响。结果还显示出不同的流动结构,因为在每个燃料喷嘴的下游都出现了空气喷嘴。根据获得的结果,在没有空气喷射器的微型燃料喷射器中混合速率低。当将空气射流注入每个燃料射流的下游时,氢射流的混合会在下游显着增加(超过60%)。随着空气射流数量的增加,燃料射流的混合性能提高了150%以上。因此,在喷射槽的下游获得了增强的混合区域,这导致了火焰的保持。 (C)2016氢能出版物有限公司。由Elsevier Ltd.出版。保留所有权利。

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