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风扇通流设计中环量分布形式的探讨 被引量:5

EFFECT OF SWIRL DISTRIBUTION ON FAN THROUGHFLOW DESIGN
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摘要 本文以时间推进通流设计方法为工具,设计了两个压比3.0级别的风扇转子,探讨了环量轴向分布形式对设计的影响。两个设计采用不同的环量分布,一为环量沿轴向线性变化,另一为环量沿轴向按余弦曲线变化,三维粘性计算结果表明,在峰值效率点,后者压比、效率和流量都高于前者。后者叶尖形成预压缩效果更为显著的叶型,对激波有更好的控制,激波后分离区小,更适合用于高负荷风扇的设计。 To explore the effect of swirl axial distribution on fan design, two fan rotors with high pressure ratio about 3.0 are designed using time-marching throughflow method. In throughflow design, swirl is prescribed according linear distribution along axial direction for one rotor, but cosine curve distribution for another rotor. 3D viscous analysis results show that the latter one has higher pressure ratio, efficiency and mass flow in peak efficiency point. Particularly the cosine curve distribution of swirl causes more pre-compression for the profiles of supersonic sections, which is of great benefit to weakening the intensity of shock wave and suppressing the flow separation after shock wave. The cosine type of swirl distribution along axial direction in throughflow design is more suitable for highly-loaded fan.
出处 《工程热物理学报》 EI CAS CSCD 北大核心 2008年第1期43-45,共3页 Journal of Engineering Thermophysics
基金 国家自然科学基金(No.10577002) 北京航空航天大学博士生创新基金
关键词 风扇 通流设计 环量分布 fan throughflow design swirl distribution
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参考文献5

  • 1Spurr, A, The Prediction of 3D Transonic Flow in Turbomachinery Using a Combined Through-flow and Bladeto-Blade Time Marching Method, International Journal of Heat and Fluid Flow, 1980, 2(4): 189 199.
  • 2Dawes W N, Toward Improved Throughflow Capability: The Use of Three-Dimensional Viscous Flow Solver in a Multistage Environment. Transaction of the ASME, Journal of Turbomachinery 1992, 114:8-17.
  • 3季路成,孟庆国,周盛.叶轮机通流计算的时间推进方法[J].航空动力学报,1999,14(1):23-26. 被引量:6
  • 4Jameson A, Schmidt W, Turkel E. Numerical Solutions of the Euler Equations by Finite Volume Methods Us- ing Runge-Kutta Time Stepping Schemes. AIAA paper 81-1259, 1981.
  • 5Damle S V. Throughflow Method for Turbomaehines Using Euler Solvers. AIAA-96-0010, 1996.

二级参考文献3

  • 1杨玉东.超音通风扇气动设计问题初探[M].北京航空航天大学,1996..
  • 2杨玉东,硕士学位论文,1996年
  • 3Wu C H,NACATN2604(1952)

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