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拟压缩性方法数值模拟绕弹体的不可压缩层流脱体涡流动
引用本文:蔡晋生.拟压缩性方法数值模拟绕弹体的不可压缩层流脱体涡流动[J].空气动力学学报,1996,14(2):234-238.
作者姓名:蔡晋生
作者单位:西北工业大学
摘    要:本文应用在连续生方程中增加压力对时间导数项的拟压缩性方法,数值求解三维定常不可压缩Navier-Stokes方程。数值求解过程采用隐式的Beam-Warming近似因式分解格式。计算绕尖头旋成柱体的大迎角脱体涡流动,得到与实验相符的结果。

关 键 词:拟压缩性方法  近似因式分解  脱体涡  N-S方程

On the Method of Pseudo Compressibility for Numerical Solution of the Steady incompressible Laminar Vortical Flows over a Tangent-Ogive-Cylinder
Cai Jinsheng.On the Method of Pseudo Compressibility for Numerical Solution of the Steady incompressible Laminar Vortical Flows over a Tangent-Ogive-Cylinder[J].Acta Aerodynamica Sinica,1996,14(2):234-238.
Authors:Cai Jinsheng
Institution:Northwestern Polytechnical University
Abstract:The method of pseudo compressibility in which a time deriyatiye pressure term is introduced into the mass conservation equation has been used for numerically solving the three-dimensional steady incompressible Navier-Stokes equations. The solution procedure employs BeamWarming implicit approximate factorization scheme. The laminar incompressible Navier-Stokes equations is used to numerically simulate high incidence. vortical flows about a tangent-ogiye-cylinder, the numerical results are in good agreement with experiment.
Keywords:pseudocompressibility approach  Navier-Stokes equations  approximate factorization scheme  vortical flows  
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