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Numerical Analysis of Fluid Dynamics of Tip Leakage Vortex with Different Gap Widths in an Axial Flow Pump

机译:轴流泵中不同间隙宽度的尖端泄漏涡的流体动力学数值分析

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The effects of different tip clearance widths (including 0.15mm, 0.45mm,1.2mm) on the tip leakage vortex dynamics and related influences of main flow characteristics of an axial flow pump are investigated. The performance of the model pump obtained by simulation shows good agreement with experimental data. The flow structure in the tip region is analyzed by computing the distribution of vorticity, mean axial velocity and turbulent kinetic energy (TKE). In depicting the features of vortex core, the swirling strength method is adopted. Through comparison for the same tip clearance, it is concluded that axial velocity of leakage flow at X = 0.5 (a plane relative to blade) decelerates while axial velocity of mainstream flow increases as the flow rate increases. Distributions of TKE in the tip gap also have similar trends at different flow rates and tip widths, that is first increasing to a maximum value where tip separation vortex (TSV) occurs then decreasing close to zero near casing wall. Based on the analysis of the axial velocity and TKE contours, the mainstream most cannot go through tip clearance for 0.15mm tip and tip separation vortex only happens at the corner of blade pressure side. While for 1.2mm tip, tip separation vortex also appears in the tip clearance, connecting with shear layer and interacting with tip leakage vortex close to blade suction side, finally result in high intensity of vortex and entrained by tip leakage vortex (TLV). Additionally, the vortex core's vorticity along TLV trajectory reduces while the pressure increases for all tip widths, indicating cavitation would be prone to generate around the leading edge. Besides, the vorticity of the vortex core for the same flow rate increases at the same location when the tip width increases from 0.15mm to 1.2mm. The roll-up process of TLV is three-dimensional and different vorticity layer exist in the tip region that could feed the turbulence into TLV. As for different flow rates and tip widths the process is similar while the value differs greatly.
机译:研究了不同的叶尖间隙宽度(包括0.15mm,0.45mm,1.2mm)对叶尖泄漏涡流动力学的影响以及轴流泵的主要流量特性的相关影响。通过仿真得到的模型泵的性能与实验数据吻合良好。通过计算涡度,平均轴向速度和湍动能(TKE)的分布来分析尖端区域的流动结构。在描述涡旋核的特征时,采用了旋流强度法。通过比较相同的叶尖间隙,可以得出结论,在X = 0.5(相对于叶片的平面)处,泄漏流的轴向速度会降低,而主流的轴向速度会随着流速的增加而增加。在不同流速和尖端宽度下,尖端间隙中TKE的分布也具有相似的趋势,即先增大到出现尖端分离涡(TSV)的最大值,然后在套管壁附近减小至接近零。根据对轴向速度和TKE轮廓的分析,对于0.15mm的刀尖,主流多数不能通过刀尖间隙,而刀尖分离涡仅发生在叶片压力侧的拐角处。对于1.2mm的吸头,吸头间隙中也出现吸头分离涡流,与剪切层连接并与靠近刀片吸力侧的吸头漏气涡相互作用,最终导致高涡流并被吸头漏气涡流(TLV)夹带。另外,沿着TLV轨迹的旋涡芯的涡度降低,而所有尖端宽度的压力都增加,这表明在前缘附近容易产生气蚀现象。此外,当针尖宽度从0.15mm增加到1.2mm时,在相同位置的相同流速下,涡流芯的涡度会增加。 TLV的卷积过程是三维的,尖端区域存在不同的涡流层,可以将湍流馈入TLV。对于不同的流速和针尖宽度,该过程是相似的,而值却相差很大。

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