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叶顶间隙变化对轴流风扇性能影响的数值研究 被引量:3

Numerical simulation on axial flow fan performance with changing tip clearance
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摘要 运用三维粘性流动计算软件,对某含叶顶间隙的直叶片轴流风扇进行数值模拟。叶顶间隙按相对间隙进行取值,其大小分别为0、0.5%、1.0%、1.5%和2.0%,其它计算参数不变。通过对计算结果的对比分析,研究叶顶间隙变化对总体性能的影响。结果表明,叶顶间隙变化对轴流风扇性能有较大影响,随着叶顶间隙的增大,其效率、全压减小。 By using the 3-d viscous flow solver software,a numerical simulation on the effect of different tip clearance size on the performance of the axial flow fan was carried.The variable quantity of the simulation is the relative tip clearance.Five different sizes of the axial flow fan are 0,0.5%,1.0%,1.5% and 2.0%.The result indicates that the performance change obviously with the changing of the tip clearance.When the tip clearance is increased,the performance parameters such as the efficiency and total pressure will decrease seriously.
作者 张露 叶舟
出处 《机械研究与应用》 2011年第1期17-18,21,共3页 Mechanical Research & Application
关键词 轴流风扇 数值模拟 叶顶间隙 axial flow fan numerical tip clearance
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  • 1邓向阳,张宏武,朱俊强,陈静宜,黄伟光.压气机非定常叶顶间隙流的数值模拟研究[J].工程热物理学报,2006,27(2):229-231. 被引量:13
  • 2Denton J D. Loss mechanisms in turbomachines, ASME 93-GT- 435,1993
  • 3Hoying D A, Tan C S, HuuDue Vo, et al. Role of blade passage flow structure,in axial compressor rotating stall inception, ASME Journal of Turbomachinery, 1999 ; 121 (4) : 735-742
  • 4Kang S, Kirsh C. Experimental study of the three-dimensional flow within a compressor cascade with tip clearance: Part 1 The tip-leakage vortex. Journal of Turbomachinery,1993 ; 115 : 444-452
  • 5Kang S, Kirsh C. Tip leakage flow in a linear compressor cascade. Journal of Turbomachinery, 1994 ; 116 : 657-664
  • 6Inoue M, Kuroumaru M, Yoshida S. Effect of tip clearance on stall evolution process in a low-speed axial compressor stage. ASME GT2004-53354,2004
  • 7Wernet M P,Van Zante D,Tony J. Strazisar. Characterization of the tip clearance flow in an axial compressor using 3-D digital PIV. Experiments in Fluids,2005 ; 39(4) :743-753
  • 8Van Zante D E, Hathaway M D, Wood J R, et al,Recommendations for achieving accurate numerical simulation of tip clearance flows in transonic compressor rotors[R]. Indiana: International Gas Turbine Aeroengine Congress & Exhibition, 1999.
  • 9Hah C. A numerical modeling of endwall and tipclearance flow of an isolated compressor rotor[J].Journal of Engineering for Gas Turbines and Power,1986,108:15--21.
  • 10Dawes W N. A numerical analysis of the three-dimensional viscous flow in a transonic compressor rotor and comparison with experiment[J]. Journal ot Turbomachinery, 1987, 109:83--90.

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