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Turbulent diffusion flames of a low-calorific value syngas under varying turbulator angles

机译:低湍流角下低热值合成气的湍流扩散火焰

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This study investigates how changes in turbulator angles affect on combustion characteristics of a low calorific value syngas in a generated syngas burner integrated with a combustor. Turbulator angles were changed from 15 degrees to 45 degrees at intervals of 15 degrees. Simulations have been performed by using a CFD code. PDF/Mixture Fraction combustion and k-epsilon standard turbulence models were used during the modellings. Temperature predictions of the syngas flame are compared with the existing temperature measurements. It is determined that these predictions are satisfactorily in good agreement with the measurements. Then, modellings were made under turbulator angles of 30 degrees and 45 degrees combustion conditions and compared with each other. It is revealed that change in turbulator angles affects highly the temperature, emission and velocity gradients of the syngas flame throughout the combustor whereas pressure drop is slightly influenced near the burner inlet zone. It is also concluded that the high temperature zone of the syngas flame moves to the upstream of the burner due to effect of the tangential velocity as the turbulator angle is increased. Predicted axial velocity values of the syngas flame decrease at the center of the combustor slightly because of the change in the turbulator angle. (C) 2017 Elsevier Ltd. All rights reserved.
机译:这项研究研究了在集成了燃烧器的合成气燃烧器中,湍流器角度的变化如何影响低热值合成气的燃烧特性。涡轮角度以15度的间隔从15度更改为45度。通过使用CFD代码进行了仿真。在建模过程中,使用了PDF /混合物分数燃烧和k-ε标准湍流模型。将合成气火焰的温度预测值与现有温度测量值进行比较。确定这些预测与测量结果令人满意。然后,在30度和45度燃烧条件下的湍流角下进行建模,并进行相互比较。揭示了湍流器角度的变化对整个燃烧器中的合成气火焰的温度,排放和速度梯度有很大的影响,而在燃烧器入口区域附近的压降受到的影响很小。还得出结论,随着湍流器角度的增加,由于切向速度的影响,合成气火焰的高温区域移至燃烧器的上游。由于湍流器角度的变化,合成气火焰的预计轴向速度值会在燃烧器的中心稍微降低。 (C)2017 Elsevier Ltd.保留所有权利。

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