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Numerical investigation of tip flow dynamics and main flow characteristics with varying tip clearance widths for an axial-flow pump

机译:尖端流动动力学的数值研究和轴流泵不同尖端间隙宽度的主流特性

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The effects of varying tip clearance widths on tip flows dynamics and main flows characteristics for an axial-flow pump are studied employing computational fluid dynamics method. An analysis is presented for the distributions of turbulent kinetic energy, mean axial velocity, and mean vorticity magnitude at the specific flow rate of 0.7Q(BEP) , focusing on flow patterns in the tip region with different tip clearance widths and associated flows. From the simulation results we find that the flow structure of tip vortex and its transportation strongly depend on the tip clearance width, especially for the extension of tip leakage vortex, appearance of induced vortex and the area of tip separation vortex. For a small clearance of 0.15 mm at 0.7Q(BEP), there is no tip separation vortex at the tip. When tip clearance width becomes larger, a tip separation vortex attaches more on the surface of blade tip as well as vortex intensity of tip flows increases. For tip clearances of 0.9 and 1.2 mm, there is a small part of induced vortex near the blade leading edge. Meanwhile, no induced vortex can be captured for tip clearances of 0.15 and 0.45 mm. The relative angle between the blade chord and tip leakage vortex trajectory reduces gradually when tip clearance width increases from 0.45 to 1.2 mm. Additionally, the radial position of tip leakage vortex core moves inwards as tip clearance width increases. Furthermore, a larger tip clearance width has greater effects on the main-stream characteristics especially near the shroud, which is due to more energy being exchanged between tip flows and main flows. At the flow rate 0.7Q(BEP), both the efficiency and head of the pump reduce with an increasing tip clearance because of greater energy loss.
机译:研究采用计算流体动力学方法,研究了不同尖端间隙宽度对尖端流动动力学的影响和轴流泵的主流特性。湍流动能,平均轴向速度和平均涡度幅度的分布呈现了分析,以0.7Q(BEP)的特定流速,聚焦在具有不同尖端间隙宽度和相关流的尖端区域中的流动图案。从仿真结果中,我们发现尖端涡旋的流动结构和其运输的强烈依赖于尖端间隙宽度,特别是对于尖端泄漏涡流的延伸,诱导涡流的外观以及尖端分离涡旋面积。对于0.7q(bep)的小间隙为0.15毫米,尖端没有尖端分离涡流。当尖端间隙宽度变大时,尖端分离涡流在叶片尖端的表面上有更多内存,以及尖端流的涡流强度增加。对于0.9和1.2mm的尖端间隙,叶片前缘附近的诱导涡流的一小部分。同时,没有诱导涡流可捕获0.15和0.45毫米的尖端间隙。当尖端间隙宽度从0.45增加到1.2mm时,叶片弦和尖端泄漏涡流轨迹之间的相对角度逐渐降低。另外,作为尖端间隙宽度增加,尖端泄漏涡旋芯的径向位置向内移动。此外,较大的尖端间隙宽度对尤其靠近护罩的主流特性具有更大的影响,这是由于在尖端流和主流之间交换的更多能量。在流速0.7Q(BEP)中,由于更大的能量损失,泵的效率和头部都随着尖端间隙的增加而减小。

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