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Coalescence Characteristics of Supersonic Jets From Multi-Nozzle Oxygen Lance in Steelmaking BOF

机译:炼钢转炉多喷嘴氧气喷枪超音速射流的聚结特性

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Hydrodynamic behaviors of multiple supersonic jets, especially their coalescence, are of paramount importance to effective design and operation of the oxygen lance in steelmaking basic oxygen furnace (BOF) but not well understood. This paper presents a numerical study on the coalescence of supersonic jets from the multi-nozzle oxygen lance at a practical Mach number by a compressible and non-isothermal computational fluid dynamics model. The model is firstly validated and then used to study the effects of key variables (i.e. ambient temperature and arrangement of nozzles including inclination angle and number) on coalescence behavior under various operational conditions. The results show that the jets prefer to deviate from their own nozzle axes and tend to coalescence with decreasing ambient temperatureozzle inclination angle or increasing nozzle number. The attenuations of the velocity and dynamic pressure at the jet centerline are delayed with the increase of ambient temperature or the decrease of nozzle number/inclination angle. The critical condition where the jets are free from interaction is identified with increasing nozzle inclination angle, and the critical value is 258 for the four-nozzle lance considered. The simulation results are then used to estimate the cavity shape and splashing modes in BOFs.
机译:多个超音速射流的流体动力学行为,尤其是它们的合并,对于炼钢基础氧气炉(BOF)中氧枪的有效设计和操作至关重要,但尚未广为人知。本文通过可压缩的非等温计算流体动力学模型,对以实际马赫数计算的多喷嘴氧气喷枪的超音速喷射流的聚结进行了数值研究。首先验证该模型,然后将其用于研究关键变量(即环境温度和喷嘴的布置,包括倾斜角度和数量)在各种操作条件下对聚结行为的影响。结果表明,随着环境温度/喷嘴倾斜角的减小或喷嘴数量的增加,喷嘴倾向于偏离其自身的喷嘴轴线并趋于聚结。随着环境温度的升高或喷嘴数量/倾角的减小,射流中心线速度和动压力的衰减会延迟。通过增加喷嘴的倾斜角度来确定射流没有相互作用的临界条件,对于考虑的四喷嘴喷枪,临界值为258。然后将仿真结果用于估算BOF中的空腔形状和飞溅模式。

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