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Numerical Simulation on Effect of Tip Clearance on Inducer Performance

机译:尖端清除对诱导性能影响的数值模拟

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Effect of tip clearance on inducer performance is studied with numerical simulation.Five inducer models with different tip clearance from 0.5 mm to 1.5 mm are studied.Firstly, the detailed flow field is obtained was obtained by using RANS and SST κ-ω turbulence model as well as the SIMPLEC algorithm.Then, the performance of the inducer with different tip clearance and the pressure distributions in inducer were analyzed.The results show that the tip clearance affects the head and efficiency of the inducer obviously.When the tip clearance increases 1 mm,the head at the rated flow is reduced by 40 %, and the efficiency is reduced about 30 %.When the tip clearance is less than 0.8 mm, the pressure variation rate on the leading edge part of the blade is larger than that of the trailing edge part.When the tip clearance is larger than 0.8 mm, the pressure variation rate on the leading edge part of the blade is about the same as that of the trailing edge part.The low pressure area is located in the suction surface of the blade near the leading edge and the area decreases with the increase of tip clearance.With increasing of the tip clearance, the vortex core gradually moves toward the leading edge of the blade.
机译:上诱导性能叶尖间隙的效果进行了研究与数值simulation.Five诱导模型具有不同的端部间隙为0.5mm至被studied.Firstly,获得通过使用RANS和SSTκ-ω湍流模型所获得的详细流场1.5毫米还有SIMPLEC algorithm.Then,具有不同的顶端间隙和在导流器中的压力分布进行分析,结果表明,该端部间隙会影响诱导的头部和效率obviously.When顶端间隙增加1毫米诱导子的性能,头部在额定流降低40%,并且效率降低约30%。当尖端间隙小于0.8mm时,在叶片的前缘部分中的压力变化率比的较大后缘part.When顶端间隙是大于0.8mm,在叶片的前缘部分中的压力变化率是大约相同的后缘part.The低压区域的位于我n中的前缘附近的叶片和区域的抽吸表面与所述端部间隙的增加,涡流核心逐渐朝向叶片的前缘移动的增加尖端clearance.With的减小。

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