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Comparative study of turbulence models for SF_6 arcs in a supersonic nozzle

机译:超音速喷嘴中SF_6弧的湍流模型的比较研究

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摘要

A comparative study of the two most popular turbulence models, the Prandtl mixing length model and the K-epsilon model, has been carried out for turbulent SF_6 arcs burning in a supersonic nozzle under direct current conditions. The computed radial temperature profiles are compared with those measured previously by Leseberg and Pietsch at currents of 100 A, 600 A and 1800 A, respectively. It has been found that the turbulence parameters of the K-epsilon model are dependent upon the arcing current while those of the Prandtl mixing length model are applicable for all the currents investigated. For turbulent SF_6 arcs in a supersonic nozzle, consideration of the range of applicability of the turbulence parameters and the cost of computation have made the Prandtl mixing length model preferable to the K-epsilon model.
机译:对于在直流条件下在超音速喷嘴中燃烧的SF_6电弧产生的湍流SF_6电弧,已对两种最流行的湍流模型(Prandtl混合长度模型和K-ε模型)进行了比较研究。将计算出的径向温度曲线与先前由Leseberg和Pietsch在100 A,600 A和1800 A的电流下测得的温度曲线进行比较。已经发现,K-ε模型的湍流参数取决于电弧电流,而普朗特混合长度模型的湍流参数适用于所有研究的电流。对于超音速喷嘴中的湍流SF_6弧,考虑到湍流参数的适用范围和计算成本,普朗特混合长度模型优于Kε模型。

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