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Confined swirling jet impingement onto an adiabatic wall

机译:密闭旋流射流绝热壁

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摘要

Impinging swirling jets generate interesting flow fields and depending on the magnitude of the swirl velocity, circulation cells develop in the region close to the solid wall. Moreover, axial momentum of the jet is influenced by the magnitude of the swirl velocity. This, in turn, results in considerable entropy generation in the flow field. In the present study, confined swirling jet impingement onto an adiabatic wall is investigated. The flow and temperature fields are computed numerically for various flow configurations. Different jet exit velocity profiles are considered and their effects on the flow field are examined. The entropy production due to different flow configurations is computed and the ir-reversibility ratios due to fluid friction and heat transfer are determined. It is found that the jet axis tilts towards the radial direction as swirl velocity increases and reducing the velocity profile number enhances the entropy generation due to heat transfer. The irreversibility ratio variation with the velocity profile number behaves opposite for the fluid friction and heat transfer.
机译:撞击的旋流产生有趣的流场,并根据旋流速度的大小,在靠近固体壁的区域内形成循环单元。此外,射流的轴向动量受旋流速度的大小影响。反过来,这导致在流场中产生相当大的熵。在本研究中,研究了对绝热壁的密闭旋流射流冲击。对于各种流动配置,均会通过数值计算出流场和温度场。考虑不同的射流出口速度曲线,并检查它们对流场的影响。计算由于不同流动配置而产生的熵,并确定由于流体摩擦和热传递而产生的不可逆比。可以发现,随着涡旋速度的增加,射流轴朝径向方向倾斜,并且减小速度分布数会增加由于传热而产生的熵。不可逆比随速度分布数的变化在流体摩擦和热传递方面表现相反。

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