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风扇/轴流压气机裕度定制

STALL MARGIN CUSTOMIZING FOR FAN AND AXIAL COMPRESSOR
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摘要 从掌控风扇/轴流压气机裕度方法回顾入手,探析美国和俄罗斯裕度控制方法及相应特点,提出将掠因素全面包含入二维特性预估循环,并将对裕度控制机制的朴素认识嵌入CFD结果判读,形成裕度定制方法。 On basis of reviewing on methods of achieving the goal of stall margin in design process of fan or axial compressors,stall margin customizing(SMC)is put forward.It is divided into two design loops.One is two dimensional,which includes through flow design and blade making and through flow performance prediction.Here through flow performance prediction plays most important roles in achieving the stall margin goal,and its most distinct feature is that the sweep effect has been completely involved.Another loop of controlling stall margin is three dimensional,in which performance prediction with three dimensional CFD tools is highly relied on.The present stall margin customizing emphasizes the former two dimensional loop because it is somewhat beforehand.This is the reason that the technique of'SMC'comes from.
出处 《工程热物理学报》 EI CAS CSCD 北大核心 2006年第z1期105-108,共4页 Journal of Engineering Thermophysics
基金 国家自然科学基金(No.50376062)
关键词 风扇 轴流压气机 裕度定制 失速裕度 特性计算 fan axial compressor stall margin customizing stall margin performance calculation
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参考文献13

  • 1[1]Robbins W H,Dugan J F.Prediction of Off-Design Performance of Multistage Compressors.NASA SP-36,Charpter X,1965,297-310
  • 2[2]Howell A R,Bonham R P.Overall and Stage Characteristics of Axial-Flow Compressors.In:Proceedings of the Institution of Mechanical Engineers.London,1950.163:235-248
  • 3[3]Calvert W J,Ginder R B.A Quasi-Three-Dimensional Calculation System for the Flow within Transonic Compressor Blade Rows.ASME paper No.85-GT-22,1985
  • 4[4]Novak R A.Flow Field and Performance Map Computations for Axial-Flow Compressors and Turbines.AGARD Lecture Series,1976,(83):5-1-5-27
  • 5[5]Denton J D.The Use of a Distributed Body Force to Simulate Viscous Effects in 3D Flow Calculations.ASME paper 86-GT-144,1986
  • 6[6]Lieblein S.Aerodynamic Design of Axial Flow Compressors.NASA SP-36,1965
  • 7[7]Denton J D.The Calculation of Three Dimensional Viscous Flow Through Multistage Turbomachines.ASME paper 90-GT-19,1990
  • 8[8]Adamczyk J J.Model Equation for Simulating Flows in Multistage Turbomachinery.ASME paper 85-GT-220,1985
  • 9[9]Rhie C M,et al.Development and Application of a Multistage Navier-Stokes Solver,Part 1:Multistage Modeling Using Body-Forces and Deterministic Stresses.ASME paper 95-GT-342,1995
  • 10[10]Boyer K M,O'Brien W F.An Improved Streamline Curvature Approach for Off-Design Analysis of Transonic Axial Compression Systems.ASME paper GT-2002-30444,2002

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