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跨声速无粘流绕振动翼型流动的数值模拟
引用本文:李锋,汪翼云.跨声速无粘流绕振动翼型流动的数值模拟[J].空气动力学学报,1992,10(1):111-116.
作者姓名:李锋  汪翼云
作者单位:北京空气动力研究所,北京空气动力研究所,北京空气动力研究所 北京 100074,北京 100074,北京 100074
摘    要:本文从Euler方程出发,利用LU-ADI格式对绕二元振动翼型跨声速流场进行了数值模拟。文章中给出了绕NACA0012和NACA 64A 010翼型不同状态的几组数值结果,在同某些实验和其它文献结果基本吻合的前提下,研究了振动对翼型表面压力、激波位置的非定常效应以及其它振动参数对流场非定常效应的影响。

关 键 词:振动翼  非定常效应  激波  数值模拟

The Numerical Simulation of Transonic Inviscid Flow over Oscillating Airfoils
Li Feng Wang Yiyun Cui Erjie.The Numerical Simulation of Transonic Inviscid Flow over Oscillating Airfoils[J].Acta Aerodynamica Sinica,1992,10(1):111-116.
Authors:Li Feng Wang Yiyun Cui Erjie
Institution:Beijing Institute of Aerodynamics
Abstract:The dynamic process is numerically simulated on two-dimensional airfoils oscillating sinusoidally. The Euler equations are required to solve with the implicit factored finite difference algorithm (LU-ADI). In this paper, numerical results of NACA0012 and NACA-64A010 airfoils are presented, some of them agree with experimental data and the results of reference4]. By the numerical simulation, some unsteady effects are investigated.
Keywords:oscillating airfoil  unsteady effect  shock wave  numerical simulation    
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