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跨声速风扇叶片变形对气动性能的影响
引用本文:郑赟,田晓,杨慧.跨声速风扇叶片变形对气动性能的影响[J].航空动力学报,2011,26(7):1621-1627.
作者姓名:郑赟  田晓  杨慧
作者单位:北京航空航天大学能源与动力工程学院航空发动机数值仿真研究中心,北京,100191
基金项目:"凡舟"基金(20090404)
摘    要:为了研究跨声速风扇叶片变形对气动性能的影响,发展了流固耦合方法计算风扇叶片在气动力作用下变形的数值程序,耦合求解了三维可压缩雷诺平均的Navier-Stokes(N-S)方程和描述叶片振动的结构动力学方程,并模拟了跨声速风扇Rotor 67转子叶片在气动载荷下的变形,重点分析了由于叶片变形带来的气动性能的变化.

关 键 词:风扇  叶片变形  流固耦合  静态气动弹性  非定常流动
收稿时间:2010/11/18 0:00:00
修稿时间:2011/2/12 0:00:00

Impact of blade deflection on aerodynamic performance of a transonic fan
ZHENG Yun,TIAN Xiao and YANG Hui.Impact of blade deflection on aerodynamic performance of a transonic fan[J].Journal of Aerospace Power,2011,26(7):1621-1627.
Authors:ZHENG Yun  TIAN Xiao and YANG Hui
Institution:Aeroengine Numerical Simulation Research Center,School of Jet Propulsion, Beijing University of Aeronautics and Astronautics,Beijing 100191,China;Aeroengine Numerical Simulation Research Center,School of Jet Propulsion, Beijing University of Aeronautics and Astronautics,Beijing 100191,China;Aeroengine Numerical Simulation Research Center,School of Jet Propulsion, Beijing University of Aeronautics and Astronautics,Beijing 100191,China
Abstract:In order to research the impact of blade deflection on aerodynamic performance of a transonic fan,a numeric program was developed to simulate the deflection of fan blades under aerodynamic loads with fluid-structural interaction method.The aerodynamic model of the fluid flow was based on solving the unsteady three-dimensional(3-D) compressible Reynolds averaged Navier-Stokes equation.The blade vibration was predicted with a linear aeroelasticity model by solving the structure dynamic equation simultaneously with aerodynamic equations.The blade deformation under unsteady aerodynamic loads of the NASA(National Aeronautics and Space Administration) Rotor 67 blade was computed,and the impact on the flowfield and aerodynamic performance was analyzed.
Keywords:fan  blade deflection  fluid-structure interaction  static aeroelasticity  unsteady flows
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