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不同间隙条件下的叶顶区流动 被引量:8

THE FLOW IN BLADE TIP REGION UNDER DIFFERENT CLEARANCE CONDITIONS
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摘要 本文用数值方法研究带有间隙的三维叶栅叶顶区的流动。对于不同大小的间隙及环壁静止与旋转的不同壁面条件,揭示了叶顶区流动的细节。计算结果表明,叶片当地厚度与间隙高度之比过大过小的情形均不易形成叶顶分离涡,相比轮毂静止的情形,轮毂转动时较不易形成叶顶分离涡。 The now in blade tip region 0f tne three-dimenstonal cascade was investigated, oy numerical method in this paper. The details of the flow in tip region were predicted under different clearance scale and the condition of both stationary and rotating hub. The computed results show that if the ratio between blade local thickness and clearance highness is too large or too small, the separation vortex will generate difficultly, and under the condition of rotating hub the separation vortex in tip region will generate more difficultly than under the condition of stationary hub.
出处 《工程热物理学报》 EI CAS CSCD 北大核心 2003年第2期228-230,共3页 Journal of Engineering Thermophysics
基金 国家重点基础研究项目(No.G1999022309) 国家自然科学基金资助项目(No.59976046)
关键词 叶轮机械 叶顶区 分离涡 叶顶分离涡 轮毂 turbomachinery different clearance blade tip region separation vortex
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参考文献5

  • 1[1]Denton J D. Loss Mechanisms in Turbomachines. ASME93-GT-435, 1993 被引量:1
  • 2[2]Heyes F J G, Hodson H P. Measurement and Prediction of Tip Clearance Flow in Linear Turbine Cascade. ASME Journal of Turbomachinery, 1993, 115(3) 被引量:1
  • 3[3]Moore J, Tilton J S. Tip Clearance Flow in a Linear Turbine Cascade. ASME Journal of Turbomachinery, 1988,110:301-309 被引量:1
  • 4[4]Storer J A, Cumpsty N A. Tip Leakage Flow in Axial Compressor. ASME 90-GT-127, 1990 被引量:1
  • 5[5]Wang Z, Jia X, Cai R. Influence of Blade Tip Clearance Shapes on Aerodynamic Performance of an Axial-Flow Compressor Stator. IMechE, Journal of Power and Energy, 2002, 216(A5), 395-401 被引量:1

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