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Numerical investigation of the effects of fuel variability on the dynamics of syngas impinging jet flames

机译:燃料可变性对合成气撞击喷射火焰动力学影响的数值研究

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Numerical simulations using the Large-eddy simulation technique is presented to study the effects of fuel variability on the dynamics of hydrogen and syngas impinging flames. The compositions of CO and H_2 are varied in a syngas mixture, including a pure H_2 case as the baseline Case 1,20% CO with 80% H_2 for Case 2, 40% CO with 60% H_2 for Case 3, and 20% CO with 20% CO_2 and 60% H_2 for Case 4. The impinging flame configuration has a distance to nozzle diameter ratio of H/d = 20 and the inlet velocity of the fuel is 27 m/s. The fuel is issued from a circular nozzle and mixes with air in a non-premixed configuration. The results show that the flames develop vortical structures in the primary jet associated with the buoyancy and shear layer instability, and the wall jet progresses parallel to the impinging plate forming large-scale vortex rings at different locations and strengths as a consequence of the fuel compositions. A comprehensive analysis of vortical structures in the primary and secondary jet streams, along with a description of their effects on the near-wall heat transfer and instabilities of syngas flames is presented here. Pollutant emissions and species formations are also investigated in order to gain further insight into the syngas burning characteristics for future cleaner combustion systems.
机译:提出了使用大涡模拟技术的数值模拟,以研究燃料可变性对撞击氢气和合成气的动力学的影响。在合成气混合物中,CO和H_2的组成各不相同,包括纯H_2情况作为基线情况案例2,案例2中有80%H_2的有20%CO,案例3中有60%的H_2有40%CO,有20%CO对于情况4,CO 2为20%,H_2为60%。撞击的火焰结构与喷嘴直径的距离为H / d = 20,燃料的入口速度为27 m / s。燃料从圆形喷嘴中排出,并以非预混合的形式与空气混合。结果表明,火焰在一次射流中形成旋涡结构,与浮力和剪切层的不稳定性有关,壁射流平行于冲击板前进,由于燃料成分不同,在不同的位置和强度形成了大规模的涡旋环。本文介绍了一次喷射流和二次喷射流中旋涡结构的综合分析,以及它们对近壁传热和合成气火焰不稳定性的影响的描述。为了进一步了解未来清洁燃烧系统的合成气燃烧特性,还研究了污染物排放和物种形成。

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