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跨声速风扇的流固耦合的颤振分析(英文)
引用本文:郑赟,杨慧.跨声速风扇的流固耦合的颤振分析(英文)[J].中国航空学报,2011(3):258-264.
作者姓名:郑赟  杨慧
作者单位:北京航空航天大学;
基金项目:Fan-Zhou Foundation of Beihang University (20090404); “111” Project (B08009)
摘    要:发展了时间推进的叶片颤振的数值方法,采用了时间推进求解流体和固体相互作用的过程。气动模型是基于求解三维雷诺平均的N-S方程,采用了多块结构化网格的有限体积格式,对流和耗散通量的计算使用了二阶迎风格式和中心格式。在变形的动网格上流体运动的守恒型方程的求解采用双时间步,隐式格式和多重网格方法。叶片振动采用了振型叠加的线性气动弹性模型。该方法在气动弹性标准算例4进行了验证,并用于求解跨音速风扇的颤振问题。

关 键 词:跨音速流动  非定常流动  颤振  跨音速风扇  流固耦合  叶轮机机械

Coupled Fluid-structure Flutter Analysis of a Transonic Fan
ZHENG Yun,YANG Hui School of Jet Propulsion,Beihang University,Beijing ,China.Coupled Fluid-structure Flutter Analysis of a Transonic Fan[J].Chinese Journal of Aeronautics,2011(3):258-264.
Authors:ZHENG Yun  YANG Hui School of Jet Propulsion  Beihang University  Beijing  China
Institution:ZHENG Yun,YANG Hui School of Jet Propulsion,Beihang University,Beijing 100191,China
Abstract:A coupled fluid-structure method is developed for flutter analysis of blade vibrations in turbomachinery.The approach is based on the time domain solution of the fluid-structure interaction in which the aerodynamic and structural equations are marched simultaneously in time.The three-dimensional (3D) unsteady Reynolds average Navier-Stokes (RANS) equations are solved with a multiblock finite volume scheme on dynamic deforming grids to evaluate the aerodynamic force.Dual time-stepping technique and an effici...
Keywords:transonic flow  unsteady flow  flutter  transonic fan  fluid-structure interaction  turbomachinery  
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